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Amsat.org IV - By Zero

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  1.  
  2. Table: satellites
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  5. | satID | weight | period | apogee | website | updated | perigee | imgFile | decay_date | dimensions | common_name | launch_date | inclination | description | norad_number | oscar_number | organization | launch_vehicle | alternate_name | satellite_type | launch_location | OSCAR_designation | international_designator |
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  7. | 49 | 48.700 | 100.69 | 799.00 | <blank> | 1142970683 | 784.00 | po28.gif | 0000-00-00 | 35 x 35 x 65 cm | POSAT | 1993-09-26 | 98.26 | Launched alongside HealthSat-2 on the September 1993, PoSAT-1 is Portugal\\'s first satellite achieved through a technology transfer program with Surrey Satellite Technology, Ltd. (SSTL). PoSAT-1 was built at the University of Surrey in a collaborative program between a consortium of Portuguese academia and industry LNETI, EFACEC, OGMA, MARCONI, ALCATEL, IST, UBI & CEDINTEC). The Portugese consortium sent 4 engineers to Surrey to participate in on-the-job training. Like KITSAT-1, PoSAT-1 carries a wide range of technology experiments, including earth imaging cameras, DSP and space-radiation experiments. In addition, PoSAT-1 carries the first microsatellite GPS experiment and an ultra-low-cost CCD star sensor. PoSAT-1 is operated jointly by the University of Surrey command station at Guildford and the Portugese command station at Sintra.\r\n\r\n<b><i>Please note - SpaceTrack wrongly identifies this object as EyeSat A</i></b>\r\n\r\nPoSAT was operated on amateur frequencies for several weeks in early 1994. OSCAR News 105 (February 1994, p. 35) carried a letter from CT1DBS reporting that an agreement was signed by AMSAT-PO and the PoSAT Consortium on December 6, 1993 stating \\"The name of PoSat-1, when in use by the amateur radio community will be PoSAT OSCAR 28, OSCAR 28 or PO-28.\\" Presently, PoSAT-1 is not open for amateur operations. \r\n\r\n<span class=\\"h4span\\">Star Sensor</span>\r\n\r\nThe star sensor is based on the same technology as the EIS, but is optimised for imaging the faint light from stars for use as part of the spacecraft\\'s attitude determination system. The star-field image is analysed by the Transputer Data Processing Experiment and the resulting measurement data returned on the On-Board-Computer.\r\n\r\n<span class=\\"h4span\\">GPS Navigation</span>\r\n\r\nPoSAT-1 carries a Global Positioning System (GPS) receiver based on the Trimble TANS-II receiver. The received data is decoded and filtered by the Transputer Data Processing Experiment to provide the satellite position and velocity as well as an accurate on-board time reference. This enables the satellite to generate its own orbital element set, provide scheduling and synchronisation to other on-board computers, and allow groundstations equipped with a GPS receiver to experiment with applications for real-time differential GPS data.\r\n\r\n<span class=\\"h4span\\">Cosmic Ray Experiment (CRE)</span>\r\n\r\nThe CRE monitors the space radiation environment experienced in orbit by the satellite and enables analysis of its effect on spacecraft semiconductor electronics. The CRE contains a large area PIN diode and multi-channel analyser capable of detecting energetic particles with a wide range of Linear Energy Transfer to build up a spectrum of observed energies of particles within the spacecraft. Special RADFET\\'s are also incorporated to monitor the accumulated ionising dose. The larger memory devices in the on-board computers are regularly \\'washed\\' to detect and log Single Event Upset (SEU) information.\r\nDigital Signal Processing Experiment (DSPE)\r\n\r\nThe DSPE consists of two Texas Instruments processors from the TMS320 series, the C25 and C30. The DSPE can be used as a programmable communications modem to modulate the downlink data from, or demodulate uplink data for the OBC, thus enabling experiments with new modulation techniques optimised for Low Earth Orbit satellite mobile communications.\r\n\r\n<span class=\\"h4span\\">Store and Forward Communications</span>\r\n\r\nThe main On-Board Computer (OBC), based on an 80C186 8MHz processor with 16MByte of Static RAM, also supports digital Store and Forward communications using AX25 packet protocols and communications links optimised for communications using very low cost, simple and portable groundstations. The Store and Forward system employs a 9.6kbps uplink and 9.6 and 38.4kbps downlink data rates. | 22829 | PO-28 | Portuguese Consortium | Ariane 4 | POSAT 1 | Microsatellite | French Guiana | POSAT-OSCAR 28 | 1993-061G |
  8. | 50 | 11.200 | 100.72 | 799.00 | http://www.itamsat.org/ | 1219515006 | 786.00 | microsatellite.gif | 0000-00-00 | ~25cm cube | ITAMSAT | 1993-09-26 | 98.26 | ITAMSAT was the first Italian Amateur satellite designed, built and operated by a small team of AMSAT members from Italy. Its mission is to store and forward amateur radio messages like AO-16, LO-19, UO-22, KO-23 and KO-25. IO-26\\'s operation is identical to AO-16 and LO-19.\r\n\r\n<b><i>Please note: SpaceTrack identifies this object as POSAT 1</i></b>\r\n\r\nThe ITAMSAT Command Team can be contacted via internet: Alberto Zagni, I2KBD, or Luca Bertagnolio, IK2OVV.\r\n\r\nIt was launched on the 26th Steptember 1993 from the ESA spaceport of Kourou (French Guyana) with an Ariane 4 launcher, and was succesfully switched on from the command station in Milano at 09:11 UTC. | 22826 | IO-26 | AMSAT-IT | Ariane 4 | <blank> | Microsatellite | French Guiana | Italy-OSCAR-26 | 1993-061D |
  9. | 51 | 48.700 | 101.15 | 815.00 | <blank> | 1161099232 | 810.00 | to31.gif | 0000-00-00 | 35 x 35 x 65 cm | TMSAT-1 | 1998-07-10 | 98.49 | Launched July 10, 1998 from the Russian Baikonur Cosmodrome into a circular sun-synchronous 822x821km orbit inclined 98.1 degrees. It carried a Mode JD 9600 FSK digital transponder, GPS receiver, and imaging subsystem.\r\n\r\nTO-31\\'s features included:<ul><li>Similar to KITSAT-OSCAR-23 in construction.</li><li>9600 bps AX.25 protocol store-and-forward PACSAT Protocol Suite communications system.</li><li>Digital Signal Processing Experiment (DSPE)</li><li>GPS receiver</li><li>Earth Imaging Subsystem</li><li>On-Board Computer 186 (OBC186) and 386 (OBC386)</li></ul>\r\nTO-31 could take multispectral images. They were produced by combining data from the Narrow Angle Camera, sensing in the green, red, and near-IR spectra. Each image has 1020 x 1020 pixels, covering an area of 100 x 100 km at mean ground resolution of 98 meters / pixel. Red areas indicate healthy vegetation (due to the strong near-IR reflectance of chlorophyll). Urban areas were generally blue-grey. The different colors of fields provided an indication of the state of vegetation (bare soil, marsh, young or mature vegetation, etc). | 25396 | TO-31 | Mahanakorn University of Technology | RESURS-01 | <blank> | Microsatellite | Baikonur Cosmodrome | Thai-Microsatellite-OSCAR 31 | 1998-043C |
  10. | 52 | 36.000 | 100.83 | 1054.00 | http://www.seds.org/sedsat/ | 1142971654 | 543.00 | so-33.gif | 0000-00-00 | <blank> | SEDSat | 1998-10-24 | 31.44 | The University of Huntsville, Alabama, in conjunction with Students for the Exploration and Development of Space (SEDS) USA, designed and constructed SEDSAT-1.\r\nSEDSAT-1, signifying Students for the Exploration and Development of Space Satellite number one, was developed at the University of Alabama in Huntsville. The SEDSAT-1 project grew from two students and their mentors to an international project funded by NASA, DARPA, and major corporations. SEDSAT-1 was launched on a Delta II from Vandenberg AFB on 24 October 1998 as a secondary payload on the JPL DS-1 mission. \r\n\r\nOn-orbit, SEDSAT-1 was be a unique resource for education and research. In its orbital configuration the satellite:<ul>\r\n<li type=\\"disc\\">Provided multi-spectral remote sensing to the broadest possible community. The cameras collected in narrow wave bands chosen to coordinate with ground based observations across the U.S. Unlike other remote sensing systems, the data was broadly accessible because it was entirely in the public domain, and because its communication system was integrated into the World-Wide-Web.\r\n<li type=\\"disc\\">Served as a development platform for advanced microsatellite position determination and control algorithms. The satellite demonstrated a unique attitude determination system and new technology in active microsatellite control.\r\n<li type=\\"disc\\">Provided the amateur radio community with digital packet store-and-forward and analog repeater systems\r\n<li type=\\"disc\\">Generated new data on the space performance of NiMh batteries and advanced electronic components.\r\n<li type=\\"disc\\">Provided additional opportunities for space studies because of its extensive reprogrammability, on board GPS, and other flexible instruments. \r\n</ul> | 25509 | SO-33 | Students for the Exploration and Development of Space | Delta II | <blank> | Microsatellite | Vandenberg, AFB | SEDSat-OSCAR 33 | 1998-061B |
  11. | 53 | 0.000 | 99.77 | 854.00 | <blank> | 1142543724 | 641.00 | so35.jpg | 0000-00-00 | <blank> | SUNSAT | 1999-02-23 | 96.48 | Sunsat was a micro-satellite built by post-graduate engineering students in the Electronic Systems Laboratory, in the Department of Electrical and Electronic Engineering at the University of Stellenbosch. It was launched in 1999 on a Delta II Launch Vehicle. Payloads included NASA experiments, Radio Amateur communications, a high resolution imager, precision attitude control, and school experiments. SUNSAT was launched on the 11th attempt at 10h29:45 GMT on 23 February 1999.\r\n\r\nSunsat was operational for almost two years, until late February 2001, when contact from the ground station for the last time.\r\n\r\nThe project was so successful that numerous subsystems was sold to satellite programs in South Korea, Germany and Australia. This prompted the creation of SunSpace Information Systems, a spinoff company that now develops and manufactures satellites, and satellite subsystems commercially. | 25636 | SO-35 | University of Stellenbosch | Delta II | <blank> | Microsatellite | Vandenberg, AFB | SUNSAT-OSCAR 35 | 1999-008C |
  12. | 54 | 6.000 | 100.29 | 799.00 | <blank> | 1142710507 | 746.00 | ao37.jpg | 0000-00-00 | <blank> | ASUSAT | 2000-01-27 | 100.19 | Launched January 27, 2000 from Vandenburg AFB in California. ASUSat-1 contained an amateur packet hardware system and a 2-meter/70-cm FM voice repeater.\r\n\r\n Approximately 50 minutes after launch, ASUSat1 was heard when an amateur radio operator in South Africa heard two beacons on its frequency. This reception matched the expected transmission pattern of ASUSat1. The contact confirmed that ASUSat had been successfully deployed from the rocket and that the satellite was functioning on orbit.\r\n\r\nThe last report received from ASUSat 1 was by the SunSat Team at fourteen hours into the mission. This reception included a telemetry frame that confirmed that the satellite did indeed have a critical problem in the power system. Unfortunately, this problem prevented the solar arrays from supplying power. Predicted lifetime of the satellite on battery power alone was estimated to be fifteen hours.\r\n\r\nASUSat1 was a project of the Aerospace Research Center at Arizona State University, Tempe, Arizona. | 26065 | AO-37 | Arizona State University | Minotaur-1 | <blank> | Nanosatellite | Vandenberg, AFB | ASU-OSCAR 37 | 2000-004E |
  13. | 55 | 0.000 | 100.30 | 799.00 | <blank> | 1142632593 | 746.00 | oo38.gif | 0000-00-00 | <blank> | OPAL | 2000-01-27 | 100.19 | Launched January 27, 2000 from Vandenburg AFB in California.\r\n\r\nStanford Aeronautics and Astronautics - Stanford University, Stanford, California Satellite Systems Development Laboratory (SSDL) | 26063 | OO-38 | Stanford Aeronautics and Astronautics | <blank> | SQUIRT | Microsatellite | Vandenberg, AFB | OPAL-Oscar 38 | 2000-004C |
  14. | 56 | 0.000 | 100.10 | 788.00 | <blank> | 1142547572 | 738.00 | wo39.jpg | 0000-00-00 | <blank> | JAWSAT | 2000-01-27 | 100.19 | JAWSAT stands for Joint Air Force Weber Satellite which was a joint project between the U.S. Air Force and Weber State University.\r\n\r\nLaunched January 27, 2000 from Vandenburg AFB in California.\r\n\r\nJAWSAT served as a bus for several deployable payloads and the Plasma Experiment Satellite Test experiment -- called PEST. The telemetry stream from JAWSAT, including data from the PEST project, was to be transmitted on Amateur Radio frequencies. | 26061 | WO-39 | Weber State University | Minotaur-1 | <blank> | Microsatellite | AFWTR | Weber-OSCAR 39 | 2000-004A |
  15. | 57 | 0.000 | 97.36 | 675.00 | <blank> | 1142988153 | 589.00 | so42.jpg | 0000-00-00 | <blank> | Saudisat 1B | 2000-09-26 | 64.56 | Launched: September 26, 2000 aboard a converted Soviet ballistic missile from the Baikonur Cosmodrome. SaudiSat-1b was one of three Amateur Radio satellites on the same launch.\r\n\r\nSaudiSat-1B can operate as 9600 baud digital store-and-forward systems as well analog FM repeater mode capability. One of two new ham satellites from the Kingdom of Saudi Arabia built by the Space Research Institute at the King Abdulaziz City for Science and Technology.\r\n\r\nSaudisat-1B was one of the first Saudi Arabian micro satellites. It was designed and built by the Space Research Institute at King Abdulaziz City for Science and Technology, Riyadh, Saudi Arabia.\r\n\r\nSaudiSat-1B is a low Earth orbiting Satellites designed to provide store-and-forward communications and carry several space experiments. They carry amateur radio communications payload. When opened to the public, the amateur payload will operate in mode-J. | 26549 | SO-42 | King Abdulaziz University for Science & Technology | Dnepr | <blank> | Nanosatellite | Baikonur Cosmodrome | Saudi-OSCAR 42 | 2000-057E |
  16. | 58 | 91.000 | 87.21 | 138.00 | <blank> | 1143054765 | 135.00 | so43.jpg | 2003-01-21 | 95cm sphere | Starshine 3 | 2001-09-30 | 67.01 | Launched September 30, 2001 from the Kodiak Launch Complex on Kodiak Island, Alaska aboard Athena I. Orbit: 500 km, 67 degree circular.\r\n\r\nStarshine 3 is nearly a meter in diameter (37 inches), weighs 91 kilograms (200 pounds) and carries 1,500 aluminum mirrors polished by an estimated 40,000 student volunteers in the United States and 25 other countries.\r\n\r\nProject Starshine is currently seeking volunteer amateur radio operators and students worldwide to monitor and report telemetry from the Starshine 3 satellite. Science data supporting an experimental solar cell experiment mounted on the surface of the satellite is being downlinked in a manner that allows students and radio amateurs to participate in collecting the data. Starshine 3 transmits 9600 bps AX.25 packet telemetry at 145.825 MHz every 2 minutes. An attractive QSL card is available to all those reporting telemetry to Project Starshine.\r\n\r\nStarshine 3\\'s primary mission is to involve and educate school children from around the world in space and radio sciences. In addition to helping build Starshine 3, students will also visually track the satellite during morning and evening passes by recording its telltale mirror flashes and reporting their observations to Project Starshine. Almost every child on earth is within visual and radio range of Starshine 3 thanks to the high inclination orbit provided by the Kodiak launch. Visual Data gathered by Project Starshine will be used to determine the effects of the atmospheric drag on the spacecraft. | 26929 | SO-43 | U.S. Naval Research Laboratory | Athena I | <blank> | Microsatellite | Kodiak WTR | Starshine-OSCAR 43 | 2001-043A |
  17. | 59 | 0.000 | 100.73 | 799.00 | <blank> | 1142619469 | 788.00 | no45.jpg | 0000-00-00 | <blank> | Sapphire | 2001-09-30 | 67.06 | Launched September 30, 2001 from the Kodiak Launch Complex on Kodiak Island, Alaska aboard Athena I.\r\n\r\nSapphire is a micro-satellite designed and built by students at Stanford University and Washington University-St. Louis. The primary mission of Sapphire is to space-qualify two sets of \\"Tunneling Horizon Detector\\" infrared sensors designed and built by the Jet Propulsion Laboratory and Stanford University. Secondary experiments include a digital camera and voice synthesizer.\r\n\r\nSapphire has three payloads; the primary is our paying customer and as such has the highest operational priority. The other two are student interests. There are some tertiary \\"payloads\\" which have to do with student research and analysis projects - these deal more with interpreted data and spacecraft operations. (These elements are explained in much greater detail in our mission operations guide.)\r\n\r\n<b>Primary</b>\r\nThe primary mission for Sapphire was to characterize the functionality and operation of the THD sensors in space.\r\n\r\n<b>Secondary</b>\r\nThe secondary mission of Sapphire was to take a picture of Northern Hemisphere and display it on the Sapphire web site. This mission was accomplished and photos are posted. Sapphire also broadcast a digitalked message to a designated audience.\r\n\r\n<b>Tertiary</b>\r\nThe tertiary mission of Sapphire was to download solar panel and power subsystem telemetry to perform the ODDSS algorithm, collect telemetry (sensor) data and deliver as requested, schedule data requests and deliver the data through the ASSET operations system, and operate the Sapphire beacon notification system through the ASSET operations system. \r\n\r\n<b>Continuing Amateur Operations</b>\r\nAfter mission experiments were completed Sapphire was turned over to amateur use primarily as an APRS digipeater and packet BBS (non-PacSat). This continued until Sapphire was declared non-operational in 2005. | 26932 | NO-45 | Stanford University Washington University - St. Louis | Athena I | <blank> | Microsatellite | Kodiak WTR | Navy-OSCAR 45 | 2001-043D |
  18. | 60 | 0.000 | 100.82 | 807.00 | <blank> | 1142639319 | 788.00 | bo48.jpg | 0000-00-00 | <blank> | IDEFIX CU1 | 2002-05-04 | 98.60 | Launched May 3, 2002 from Kourou, French Guiana on an Ariane 4 flight V151 carrying SPOT 5 as the primary payload. \r\n\r\nTwo picosats, designed and built by AMSAT-France, were battery powered and estimated to operate approximately 40 days. They remained fastened to the Ariane 4 third stage with an orbit of 800 km. Both picosats transmitted NBFM voice recorded messages and digital telemetry data. BO-47 on 145.840 MHz and BO-48 on 435.270 MHz. Telemetry data was transmitted in 400 bps BPSK, similar to AO-40\\'s telemetry beacon.\r\n\r\nBO-47 (CU1) stopped transmitting after 32 days of operation. Final reports came from Japan.\r\n\r\nBO-48 (CU2) stopped transmitting after 14 days of operation. Final reports came from Japan indicating that the battery voltage had dropped to 7V and the RF output dropped to -6dB of its normal level.\r\n\r\nBoth satellites were equipped with 600 Watt-hour batteries. BO-48, transmitting on 435 MHz, had an output power 10 times higher that BO-47.\r\n\r\nThe IDEFIX B0-47/48 team would like to thank everyone who spent time listening to the picosats and submitted telemetry data. The whole set of collected telemetry data is available upon request for educational purposes. Contact Jean-Louis F6AGR, President AMSAT-F. | 27422 | BO-47 | AMSAT-FR | Ariane 4 | <blank> | Payload | French Guiana | BreizhSAT-OSCAR 47 | 2002-021B |
  19. | 61 | 0.000 | 97.81 | 693.00 | <blank> | 1142630158 | 615.00 | ao49.gif | 0000-00-00 | <blank> | RUBIN 2 | 2002-12-20 | 64.56 | AO-49 was launched December 20, 2002 aboard a converted Soviet ballistic missile from the Baikonur Cosmodrome.\r\n\r\nAO-49 (SAFIR-M) is a German amateur radio payload onboard the small German scientific satellite \\"RUBIN-2\\".\r\n\r\nAO-49 was built by the German amateur radio association \\"AATiS e.V.\\" (German acronym for \\"Arbeitskreis Amateurfunk und Telekommunikation in der Schule\\", which means: \\'working group for amateur radio and telecommunications in schools\\'). AO-49 is designed as a \\"store and broadcast\\" system for APRS based messages, dedicated for the use of schools in combination with the existing WX-Net and planned buoy experiments in Germany. | 27605 | AO-49 | OHB, Bremen | Dnepr | SAFIR-M | Payload | Baikonur Cosmodrome | AATiS-OSCAR 49 | 2002-058A |
  20. | 63 | 50.000 | 115.71 | 1497.00 | <blank> | 1142710345 | 1479.00 | fo20.jpg | 0000-00-00 | 40 x 40 x 47 cm | JAS 1 | 1986-08-12 | 50.02 | Fuji-OSCAR 12 was launched August 12, 1986 by the first test flight of the H-I launcher. FO-12 was launched piggyback with a Japanese experimental geodetic satellite Ajisai (EGS). Weight 50 kg. Orbit circular 1479 x 1497 km. Inclination 50 degrees. 26-sided polyhedron, 40 x 40 x 47 cm.\r\n\r\nFO-12 was the first Japanese amateur satellite developed by the Japan Amateur Radio League (English version) with system design and integration performed at NEC. FO-12 was taken out of service November 5, 1989 because of battery failure. | 16909 | FO-12 | Japan Amateur Radio League | H-I launcher | FUJI 1 | Microsatellite | Japan | Fuji-OSCAR 12 | 1986-061B |
  21. | 64 | 50.000 | 112.21 | 1744.00 | <blank> | 1142710332 | 912.00 | fo20.jpg | 0000-00-00 | 47 x 44 x 44 spheroid | JAS 1B | 1990-02-07 | 99.05 | Fuji-OSCAR-20 was the second in a series of Japanese Amateur communications satellites having both analog and digital Mode J transponders. The first spacecraft, Fuji-OSCAR-12 was launched on August 12, 1986, and was the first OSCAR satellite to utilize the AX.25 packet radio communications protocol. It was followed by the currently active Fuji-OSCAR-20 several months after FO-12 had to be removed from service due to a deteriorating power budget.\r\n \r\nFuji-OSCAR-20 was launched on February 7, 1990 at 01:33 UTC from the Tanegashima Space Center, National Space Development Agency of Japan (NASDA) on an H-1 two-stage rocket. Its orbit differed slightly from most current OSCAR satellites, being slightly elliptical with a high inclination. This assureed that the satellite will remain in sunlight for the majority of its orbit all year long.\r\n\r\nThe physical structure of FO-20 was that of a 26 sided polyhedron, with a weight of approximately 50 kg, so it was much larger than the Microsat satellites. Although Fuji-OSCAR-20 used Mode J AX.25 packet radio communications links as the Microsat satellites do, one big difference between FO-20 and the Microsats was that FO-20\\'s packet radio could be accessed without the need for special Microsat terminal software. Any computer or terminal that could be used to access terrestrial packet radio bulletin board systems (BBSs) could be used to access the FO-20 mailbox.\r\n\r\nThe other big difference between FO-20 and the Microsat satellites was that in addition to the packet mailbox features of the satellite, FO-20 also supported a Mode J analog transponder for SSB and CW communications. \r\n \r\n<hr noshade><h4>Fuji-OSCAR-20 System Specifications</h4>FO-20 carried two beacon transmitters. The Mode JA beacon was active during periods of analog transponder operation. It operated on a frequency of 435.795 MHz with 100 mW of power, and could carry CW or BPSK information, or could be configured for A0 for Doppler shift experiments.\r\n\r\nThe Mode JD beacon served as the single AX.25 Mode JD downlink to ground stations, and also carried telemetry in either a ASCII (most often used), or binary formats. The Mode JD beacon operated on a frequency of 435.910 MHz with 1 watt of output power, and used BPSK modulation. \r\n\r\nThe CW telemetry carried 12 analog status items and 33 status items, while the BPSK packet telemetry beacon carried 29 analog items, plus 33 status items. \r\n\r\nThe Mode JA analog transponder system consisted of an inverting heterodyne transponder with a bandwidth of 100 KHz, with an uplink in the 145 MHz band, and a downlink in the 435 Mhz band. An uplink power of about 100 watts EIRP was required for access to the transponder, but of course, the more sensitive your downlink receiver is, the less uplink power was required to achieve an adequate downlink signal-to-noise ratio. \r\n\r\nThe Mode JD digital transponder system functioned as a mailbox using the AX.25 level 2 protocol. It receiveed Manchester encoded FSK on any one of four uplink frequencies, and transmitted on a single downlink frequency of 435.910 MHz at 1200 bps using BPSK modulation. An uplink of about 100 watts EIRP was the minimum required for Mode JD transponder access. The satellite transmitted with 1 watt of transmitter power. \r\n\r\nFuji-OSCAR-20 used circular antenna polarization on all uplink receivers and all downlink transmitters and beacons. The 145 MHz uplink antenna is a ring turnstile antenna mounted below the bottom side panels of the spacecraft, and exhibited a maximum gain of about +0.5 dBi. The 435 MHz transmitting antenna was a turnstile array mounted on the top of the spacecraft, and exhibited a maximum gain of about +4 dBi.\r\n | 20480 | FO-20 | Japan Amateur Radio League | H-1 | Fuji 2 | Microsatellite | Tanegashima Space Center | Fuji-OSCAR 20 | 1990-013C |
  22. | 65 | 0.000 | 104.73 | 1008.00 | <blank> | 1142983861 | 955.00 | ao21.jpg | 0000-00-00 | <blank> | RS-14 | 1991-01-29 | 82.94 | RS-14/AO-21 was launched on January 29, 1991, the results of a joint venture between AMSAT-U and AMSAT-DL. The amateur equipment rode piggyback on the INFORMATOR-1, an experimental geological satellite. The Russian amateur radio satellite club Orbita and the Adventure Club of Moscow built Radio M-1 as a joint project with German hams at Marburg, Munich and Hannover. The collaboration led to dual names for the new amateur radio satellite once it arrived in orbit: AMSAT-OSCAR-21 (AO-21) and Radiosputnik-14 (RS-14)\r\n\r\nAs of September 16, 1994 the spacecraft was switched off, including the amateur equipment onboard. The reasons cited were those of cost in maintaining the craft in space when the usefulness of the primary payload was exhausted. The amateur community lost a valuable asset. \r\n\r\nRS-14/AO-21 was a very popular satellite with the radio amateurs. The equipment to communicate through RS-14/AO-21 was simple and easy to operate. RS-14/AO-21 functioned as a \\"repeater in the sky\\" and routinely transmitted digitally recorded voice messages commemorating events like the 25th anniversary of the first landing on the moon by broadcasting Neil Armstrong\\'s first words as he stepped on the moon.\r\n\r\nAltogether four different receiving channels within 70 cm the range could process differently modulated signals (BPSK, AFSK, FSK, RSM, FM) by the computer. Eight different modes transmitted:<ul><li>1200 bps, BPSK, NRZI (Fuji mode)<li>400 bps, BPSK, Biphase s, (Phase-3 mode)<li>2400 bps, BPSK, Biphase s, (Rudak-1 mode)<li>4800 bps, RSM, NRZIC<li>9600 bpses, RSM, NRZI + Scrambler<li>CW <li>FSK for RTTY, SSTV, FAX transmissions<li>FM-modulated through a DSO RISC Processor</ul> | 21087 | AO-21 | AMSAT-U/AMSAT-DL | <blank> | Radio Sputnik 14 | Payload | Plesetsk | AMSAT-OSCAR 21 | 1991-006A |
  23. +-------+--------+--------+---------+-----------------------------+------------+---------+--------------------+------------+-----------------------+--------------+-------------+-------------+--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+--------------+--------------+-------------------------------------------------------+----------------+------------------+----------------+--------------------------+------------------------------+--------------------------+
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  30. Table: satellites
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  33. | satID | weight | period | apogee | website | updated | perigee | imgFile | decay_date | dimensions | common_name | launch_date | inclination | description | norad_number | oscar_number | organization | launch_vehicle | alternate_name | satellite_type | launch_location | OSCAR_designation | international_designator |
  34. +-------+---------+----------+----------+------------------------------------------------------+------------+----------+--------------------------+------------+-----------------+------------------+-------------+-------------+---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+--------------+--------------+--------------------------------------------+--------------------+----------------+----------------+------------------------+---------------------+--------------------------+
  35. | 66 | 0.000 | 1012.62 | 36822.00 | <blank> | 1249780534 | 17228.00 | ao24.gif | 0000-00-00 | <blank> | Arsene | 1993-05-12 | 5.77 | Arsene-OSCAR 24 was launched May 13, 1993 by a Ariane V-56A from Kourou, French Guiana. Orbit elliptical, equatorial. Mode B (145.975 MHz downlink (1200 bps FM AFSK)) and Mode S (2446.54 MHz downlink transponders).\r\n\r\nArsene was a French packet relay satellite built by French Radio Amateur Club de l\\'Espace. The packet system was never implemented because the 2 meter transponder failed soon after launch. Arsene was then used to relay SSB and CW signals on 2.4 GHz for several months until this transponder failed as well. | 22654 | AO-24 | Radio Amateur Club de l\\'Espace | Ariane V-56A | <blank> | Microsatellite | French Guiana | Arsene-OSCAR 24 | 1993-031B |
  36. | 67 | 0.000 | 94.95 | 520.00 | http://www.sp.nps.navy.mil/pansat/ | 1142989104 | 512.00 | po-34.jpg | 0000-00-00 | 48 cm sphere | PAN SAT | 1998-10-29 | 28.46 | Launched October 30, 1998. PANSAT is a microsatellite design that will provide an amateur radio store-and-forward message system. Designed and built at the Naval Postgraduate School in Monterey, California. This amateur satellite was unique among the PACSAT style satellites in that it employed direct sequence spread-spectrum communications.\r\n\r\nThe spacecraft itself provided store-and-forward (packet radio) digital communications using direct sequence spread spectrum modulation. PANSAT operated in the amateur radio 70 cm band with center frequency at 436.5 MHz, a bit rate of 9842 bits per second and 9 MB of message storage. | 25520 | PO-34 | Naval Posgraduate School, Monterey | STS-95 (Discovery) | <blank> | Microsatellite | Kennedy Space Center | Pansat-OSCAR 34 | 1998-064B |
  37. | 68 | 300.000 | 97.39 | 638.00 | <blank> | 1142710489 | 629.00 | uo36.gif | 0000-00-00 | <blank> | UOSAT 12 | 1999-04-21 | 64.56 | UoSAT-12 carried a number of imaging payloads (Earth Imaging System;up to 10 meter resolution). It carried a propulsion system for orbital housekeeping experiments. The S-band downlink can run at speeds up to 1Mb/s for downloading imaging data.\r\n\r\nEquipped with 2 cameras (10 m resolution panchromatic, 40 m multispectral). CCDs are from Eastman Kodak. Also has a colour wide angle camera.\r\n\r\nUoSAT-12 carried a newly developed Space GPS receiver, the SGR, that was designed to provide an experimental testbed for orbit and attitude determination. It had 5 antennas to accurately calculate the spacecraft attitude through applying interferometry techniques to the phase difference measurements.\r\n\r\nResistojet was a new propulsion technology on-board UoSat-12. Nitrous oxide is heated by an electrical element powered by the spacecraft\\'s batteries. The thrust from the Resistojet can be used to adjust the spacecraft\\'s orbit. A 60-minute Resistojet firing period will raise the 650km orbit of the spacecraft by 3km. UoSAT-12 carries 2.5kg of nitrous oxide, sufficient for 14 hours running, in an expulsion system developed for Surrey in collaboration with Polyflex Aerospace of Cheltenham, UK.\r\n\r\nNASA demonstrated on UO-36 the ability to use standard Internet protocols to communicate with an orbiting spacecraft (just like any node on the Internet). NASA developed this project working with the commercial payload onboard UoSAT-12. | 25693 | UO-36 | University of Surrey | Dnepr | <blank> | Microsatellite | Baikonur Cosmodrome | UoSAT-OSCAR 36 | 1999-021A |
  38. | 69 | 1.000 | 101.38 | 831.00 | http://lss.mes.titech.ac.jp/ssp/cubesat/index_e.html | 1142833266 | 816.00 | cute1.gif | 0000-00-00 | 10 x 10 x 10 cm | Cute-1 | 2003-06-30 | 98.72 | The Cute 1 mission is:<ul><li>CW-transmitter of CubeSat transmits CW-telemetry, and we receive the signal at ground station.</li><li>FM-transmitter of CubeSat transmits FM-telemetry by two different protocol (Ax.25 and TITech original(Simple Radio Link Layer protocol, SRLL)), and we receive the signal at ground station.</li><li>Change the communication protocol by command uplink.</li><li>Broadcasting service of CW-telemetry data and FM-telemetry data on WWW</li><li>Measure the accelerarion, angular velocity and temperature of CubeSat on orbit, and then store and transmit the data.</li><li>Deploy the solar battery paddle by command uplink.</li></ul> | 27844 | CO-55 | Tokyo Institute of Technology Matunaga LSS | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | CubeSat-OSCAR 55 | 2003-031E |
  39. | 70 | 10.000 | 94.74 | 711.00 | http://lss.mes.titech.ac.jp/ssp/cute1.7/index_e.html | 1256753471 | 299.00 | cute1_7.gif | 2009-10-25 | 10 x 10 x 20cm | Cute-1.7 | 2006-02-21 | 98.18 | Cute-1.7+APD is the successor of the Cute-1 nano-satellite, developed and built by the second generation of students of the Tokyo Institute of Technology Matunaga Laboratory for Space System (LSS). The Avalanche Photo Diode sensor module, or APD experiment on this double-cube nano-satellite was also developed by the Tokyo Institute of Technology Kawaii Laboratory.\r\n\r\n\\"Cute-1.7+APD\\"-#1 was launched on the JAXA M-V-#8 Rocket from the Kagoshima Space Center on 21 February 2006 into a 712 x 300 km elliptical orbit. The lifetime of \\"Cute-1.7 + APD \\" is estimated much less than one year for the shortest due to atmospheric reentry. \r\n\r\nThe separation mechanism for release in orbit was also developed at the Tokyo Institute of Technology Matunaga Laboratory for Space System. \r\n\r\nCute-1.7 + APD project is a satellite project developed mainly by students at Laboratory for Space Systems, Tokyo Institute of Technology. To launch our satellite in 2006, the project has started in January, 2004. It is the second satellite made in Tokyo Institute of Technology after the first one, CUTE-I, was launched in June, 2003.\r\n\r\nThis project is based on the international CubeSat project.\r\n | 28941 | CO-56 | Tokyo Institute of Technology Matunaga LSS | JAXA M-V 8 | Cute 1.7 + APD | Cubesat | Kagoshima Space Center | CubeSat-OSCAR 56 | 2006-005C |
  40. | 71 | 81.000 | 95.00 | 520.00 | http://www.amsatsa.org.za/SZASAT.htm | 1300548810 | 498.00 | zasat.gif | 0000-00-00 | <blank> | SumbandilaSat | 2009-09-17 | 97.30 | This satellite was launched 17 September 2009 on a Soyuz launch vehicle.\r\n\r\nZASAT is a project initiated and ZASAT is a project initiated and funded by the Department of Science and Technology. The department recently launched a competition to find a suitable name for the satellite but until such time as a name is chosen the project designation is ZASAT.\r\n\r\nThe Amateur Radio Payload is operating in conjunction with the University of Stellenbosch Software Defined Receiver project as it will share the VHF receiver and UHF transmitter used by the SDR project. SA AMSAT designed and built a control system to facilitate the following operations:<ul><li>V/U voice transponder with an uplink in the 2 metre band and a downlink in the 70cm band.</li><li>A parrot repeater (voice digipeater)</li><li>A voice beacon</li></ul>\r\n\r\nCurrently the repeater is scheduled for 15 minute activations over a different region each week. Currently North and South America are during the first week of the month.\r\n\r\nVarious other payload options were considered but due to limited real estate, available power and the short time frame, the above configuration was decided on. | 35870 | SO-67 | AMSAT-SA | Soyuz-2-B/Fregat | SO-67 | Microsatellite | Baikonur | Sumbandila Oscar 67 | <blank> |
  41. | 72 | 0.000 | 0.00 | 0.00 | http://www.kiwisat.org | 1221484833 | 0.00 | kiwisat_flight_model.jpg | 0000-00-00 | <blank> | KiwiSat | 0000-00-00 | 0.00 | KiwiSat is a microsatellite under construction by AMSAT-ZL. It will have a 1W linear U/V linear transponder and additional experiments including FM repeater and data transmission. The latest news from Terry ZL2BAC is that the engineering version of the Data/FM transmitter was running 1 Watt output and was being tested with some decent test gear.\r\n\r\nIARU has coordinated the KiwiSat frequencies shown above. | 0 | <blank> | AMSAT-ZL | <blank> | <blank> | Microsatellite | <blank> | <blank> | <blank> |
  42. | 73 | 25.000 | 103.00 | 1450.00 | http://www.almasat.org/ | 1329142222 | 354.00 | ALMASat.gif | 0000-00-00 | 30 x 30 x 30 | ALMASat | 2012-02-13 | 71.00 | The AlMaSat project, started in 2003 at University of Bologna in Forl\xec, Italy and is coordinated by Dr. Paolo Tortora. The first ALMASat (ALma MAter SATellite) demonstration mission is expected to launch on the maiden VEGA flight. Among the possible future applications, there is the on-orbit experimentation of a passive electro-dynamic de-orbiting system, jointly developed by Alenia Spazio (Turin plant) and the University of Rome \x93la Sapienza\x94. | 0 | <blank> | University of Bologna | Vega | <blank> | Microsatellite | Kourou | <blank> | <blank> |
  43. | 74 | 15.000 | 0.00 | 0.00 | http://www.bluesat.unsw.edu.au/ | 1221417720 | 0.00 | microsatellite.gif | 0000-00-00 | 22 x 22 x 22 cm | BLUESAT | 0000-00-00 | 0.00 | Launch Date is To Be Determined\r\n\r\nBLUEsat (Basic LEO UNSW Experimental Satellite) is a Student Project managed and run entirely by students at The University of New South Wales (UNSW). It is part of The UNSW Laboratory for Student Space Development (ULSSD), a student-led umbrella body whose purpose is to foster the development of space-related projects in UNSW.\r\n\r\nBLUEsat is a 10 kg microsatellite. A microsatellite is a classification for a satellite between 10 and 100kg in mass. The primary mission of BLUEsat is to act as a packetstore- and-forward amateur radio satellite. In addition to this BLUEsat also carries an experimental GPUS unit for positioning and testing purposes, and imager to take photographs of the earth and a materials experiment provided by the Mars Society to test the UV resistance of the material Lexan in vacuum. Finally, the satellite contains multiple sensors to monitor the orbital environment and the health of the satellite.<h4>Structure</h4>The BLUEsat structure is based on an old AMSAT-NA design that has been modified to better suit our needs. The basic design is a five tray stack \x96 the satellite consists of five trays which house the various payloads and systems. The trays stack on top of each other to form a cubical satellite structure. The structure is made from Aluminium 7075-T651, an aluminium alloy that is commonly used in defence and aerospace applications.<h4>Power</h4>Power for the satellite is provided by solar panels mounted on the six sides of the structure. Rechargeable battery packs are also used to provide power when the satellite is in the earths\x92 shadow.<h4>Communications</h4>A transmitter, receiver and a beacon will be mounted on the satellite. These components will provide communication between BLUEsat and the ground station. The beacon is in place as insurance for the worst case scenario, where every system apart from power fail: the beacon will still transmit essential telemetry data and prove the existence of BLUEsat\r\nin orbit.\r\n\r\nAmateur packet communication is the primary mission of BLUEsat, and it uses the ubiquitous AX.25 protocol. You will be able to work BLUEsat using a Kantronics KPC-9612 or similiar 9600 baud TNC. BLUEsat uses the J-mode configuration like most modern amateur satellites.<h4>Flight Computer</h4>The BLUEsat flight computer is based around an Intel SA1100 StrongARM processor. It is responsible for managing the various payloads the satellite carries, including the primary PACSAT payload. The flight computer is also responsible for collecting telemetry data from sensors placed throughout the satellite and packaging the telemetry\r\nfor transmission down to earth stations. | 0 | <blank> | University of New South Wales | TBD | <blank> | Microsatellite | TBD | <blank> | <blank> |
  44. | 75 | 60.000 | 50400.00 | 35000.00 | http://www.amsat.org/amsat-new/eagle/ | 1326230289 | 700.00 | eagle.gif | 0000-00-00 | 60 x 60 x 60cm | AMSAT-Eagle | 0000-00-00 | 15.00 | AMSAT-Eagle was a high earth orbit satellite project in the planning stages by AMSAT-NA. The project has been suspended due to HEO launch costs and uncertainty. | 0 | <blank> | AMSAT-NA | <blank> | <blank> | Satellite | Kennedy Space Center | <blank> | <blank> |
  45. | 76 | 0.000 | 98.43 | 693.00 | <blank> | 1186369156 | 675.00 | <blank> | 0000-00-00 | <blank> | RS-22 | 2003-09-27 | 98.10 | RS-22 a training satellite built by the Mozhaisky military academy in St. Petersburg, Russia. It was launched into a 693 x 675km orbit. RS-22 carries a CW beacon on 70cm that sends telemetry in the form of 16 groups of 5 to 7 characters framed by \\"rs22\\". Code is sent at ~5wpm with a pause of approximately 10 seconds between each group. | 27939 | <blank> | Mozhaisky Military Space University | Dnepr | Mozhayets 4 | Payload | Baikonur Cosmodrome | <blank> | 2003-042A |
  46. | 77 | 0.000 | 104.77 | 1006.00 | <blank> | 1144103602 | 961.00 | rs-10.gif | 0000-00-00 | <blank> | Radio Sputnik 12 | 1991-02-05 | 82.92 | RS 12/13 was launched February 5, 1991 on board a Russian Cosmos C launcher. RS-12/13 rode piggyback on a primary spacecraft on a COSMOS 2123 Russian Navigation Satellite. Each satellite had two radio amateur transponders onboard. Only one was switched on at a time.\r\n\r\nBoth satellites had a 40 kHz wide linear transponder allowing for CW and SSB contacts. One unique feature of both these satellites was the ROBOT autotransponder. The autotransponders made it possible to carry on a CW telegraphy contact with the ROBOT computer carried on the spacecraft. Upon calling the satellite on the ROBOT uplink frequency, the computer would return with a short message and issue a QSO number.\r\n\r\nIt is thought that after superpower proton flashes from the Sun about July/August 2002 caused damaged to the COSMOS2123 and RS-12/13 transponders (thanks Jerry, K5OE/3).\r\n\r\nIn addition to the operating modes listed, RS-12 supported two additional modes<ul><li>Mode KT: 21 MHz uplink into 29 and 145 MHz downlinks</li><li>Mode KA: 21 MHz and 145 MHz uplinks into a common 29 MHz downlink</li></ul>\r\n | 21089 | RS-12 | Radio Sport Federation | Cosmos C | Cosmos 2123 | Payload | Plesetsk MSC | <blank> | 1991-007A |
  47. | 78 | 100.000 | 0.00 | 0.00 | www.esa.int/education | 1262141180 | 0.00 | eseographic.JPG | 0000-00-00 | 60 x 60 x 70cm | ESEO | 0000-00-00 | 0.00 | The European Student Earth Orbiter is a \x93hands on project\x94 from the ESA Education Office. Current details may be found at http://esamultimedia.esa.int/SPECIALS/Education/SEM4DLPR4CF_0.html\r\n The satellite is being designed and constructed by students from 13 universities together with members of AMSAT-UK. The project is managed by Carlo Gavazzi Spa. based in Milan Italy http://www.cgspace.it \r\n\r\nESEO will be completed in 2011 and is planned for a launch into LEO in 2012. It has a primary communications system using transmit and receive frequencies in the commercial space allocation at 2 / 2.2GHz.\r\n\r\nThe configuration of this planned LEO satellite project has now been changed and, as a result, the AMSAT-UK hardware will now be a payload rather than a redundant communications system and payload.\r\n\r\nThe new configuration employs three solar panels - two of which are deployed and the spacecraft will be sunpointing with a slow rotation around the Y axis.\r\nThis change has enabled our system to be slightly simplified and is now planned to consist of:\r\nC Band CW beacon\r\nU/V linear transponder with approx 3 watts output\r\nV Band 1200bps BPSK FEC telemetry downlink\r\nU/S Single channel FM transponder with approx 3 watts output\r\n\r\nThanks David G0MRF and Graham G3VZV for this information\r\n | 0 | <blank> | ESA Education Office | <blank> | <blank> | Microsatellite | <blank> | <blank> | <blank> |
  48. | 79 | 1.000 | 0.00 | 0.00 | http://polysat.calpoly.edu/ | 1154118990 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | K7RR-Sat | 2006-07-26 | 0.00 | K7RR-Sat (CP1) is a Cubesat built by California Polytechnic Institute. It was originally designated CP1) but was redesignated K7RR-Sat in memory of AMSAT member and CubeSat team mentor Clifford Buttschardt.\r\n\r\nK7RR-Sat was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. \r\n\r\n | 0 | <blank> | California Polytechnic University | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  49. | 80 | 1.000 | 0.00 | 0.00 | http://polysat.calpoly.edu/ | 1154112657 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | CP2 | 2006-07-26 | 0.00 | CP2 is a Cubesat built by California Polytechnic Institute. CP2 was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | California Polytechnic University | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  50. +-------+---------+----------+----------+------------------------------------------------------+------------+----------+--------------------------+------------+-----------------+------------------+-------------+-------------+---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+--------------+--------------+--------------------------------------------+--------------------+----------------+----------------+------------------------+---------------------+--------------------------+
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  55.  
  56.  
  57. Table: satellites
  58.  
  59. +-------+---------+--------+---------+-----------------------------------------------------------------+------------+---------+----------------+------------+-------------------------+------------------+-------------+-------------+-------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+--------------+--------------+-----------------------------------+----------------+----------------+----------------+----------------------------------+-------------------+--------------------------+
  60. | satID | weight | period | apogee | website | updated | perigee | imgFile | decay_date | dimensions | common_name | launch_date | inclination | description | norad_number | oscar_number | organization | launch_vehicle | alternate_name | satellite_type | launch_location | OSCAR_designation | international_designator |
  61. +-------+---------+--------+---------+-----------------------------------------------------------------+------------+---------+----------------+------------+-------------------------+------------------+-------------+-------------+-------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+--------------+--------------+-----------------------------------+----------------+----------------+----------------+----------------------------------+-------------------+--------------------------+
  62. | 81 | 1.000 | 0.00 | 0.00 | http://134.75.55.85/new_version/english/hausat_1/index.php | 1154112700 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | HAUSAT1 | 2006-07-26 | 0.00 | HAUSAT1 is a Cubesat built by Hankuk Aviation University. It was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | Hankuk Aviation University | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  63. | 82 | 1.000 | 0.00 | 0.00 | http://www.mae.cornell.edu/cubesat/ | 1154112750 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | ICE Cube 1 | 2006-07-26 | 0.00 | ICE Cube 1 is a Cubesat built by Cornell University. It was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | Cornell University | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  64. | 83 | 1.000 | 0.00 | 0.00 | http://www.mae.cornell.edu/cubesat/ | 1154112781 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | ICE Cube 2 | 2006-07-26 | 0.00 | ICE Cube 2 is a Cubesat built by Cornell University. It was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | Cornell University | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  65. | 84 | 3.000 | 0.00 | 0.00 | http://courses.ece.uiuc.edu/cubesat/ | 1154112805 | 0.00 | doublecube.jpg | 0000-00-00 | 10 x 10 x 20cm | ION | 2006-07-26 | 0.00 | ION is a double-Cubesat built by University of Illinois. It was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | University of Illinois | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  66. | 85 | 1.000 | 0.00 | 0.00 | http://www.engr.ku.edu/ae/kutesat.htm | 1154112829 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | KUTEsat | 2006-07-26 | 0.00 | KUTEsat is a Cubesat built by University of Kansas. It was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | University of Kansas | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  67. | 86 | 1.000 | 0.00 | 0.00 | http://www.ssel.montana.edu/merope/ | 1154112851 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | MEROPE | 2006-07-26 | 0.00 | MEROPE is a Cubesat built by Montana State University. It was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | Montana State University | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  68. | 87 | 1.000 | 0.00 | 0.00 | http://128.39.102.180/index.html | 1154112873 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | nCUBE1 | 2006-07-26 | 0.00 | nCUBE1 is a Cubesat built by University of Technology. It was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | University of Technology | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  69. | 88 | 1.000 | 0.00 | 0.00 | http://cubesat.arizona.edu/rincon_sat/ | 1154112946 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | RINCON | 2006-07-26 | 0.00 | RINCON is a Cubesat built by University of Arizona. It was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | University of Arizona | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  70. | 89 | 1.000 | 0.00 | 0.00 | http://cubesat.arizona.edu/sacred_sat/ | 1154112969 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | SACRED | 2006-07-26 | 0.00 | SACRED is a Cubesat built by University of Arizona. It was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | University of Arizona | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  71. | 90 | 1.000 | 0.00 | 0.00 | http://forth.aero.cst.nihon-u.ac.jp/projects/Cubesat/index.htm | 1154112989 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | SEEDS | 2006-07-26 | 0.00 | SEEDS is a Cubesat built by Nihon University. It was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | Nihon University | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  72. | 91 | 1.000 | 0.00 | 0.00 | http://www-ee.eng.hawaii.edu/%7Ecubesat/ | 1154113036 | 0.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | Voyager | 2006-07-26 | 0.00 | Mea Huaka is a Cubesat built by University of Hawaii. It was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | University of Hawaii | Dnepr | Mea Huaka | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  73. | 92 | 1.000 | 99.20 | 799.80 | http://polysat.calpoly.edu/ | 1220582571 | 652.30 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | CP3 | 2007-04-17 | 98.00 | CP3 is a Cubesat built by California Polytechnic Institute. | 0 | <blank> | California Polytechnic University | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | <blank> |
  74. | 111 | 2.200 | 97.20 | 642.10 | http://www.delfic3.nl/index.php | 1253806064 | 621.60 | delfi-c3.jpg | 0000-00-00 | 10cm x 10cm x 34cm | Delfi-C3 | 2008-04-28 | 98.00 | For the past decade, satellite design has been an important discipline at the faculty of Aerospace Engineering at Delft University of Technology. A major change of the predominantly theoretical nature of the satellite projects came into being in 2004, with the completion of an in-house Class 100.000 Clean Room. Along with equipment in laboratories located at the faculty of Electrical Engineering, this facility enables Delft University to not only design, but to produce and assemble a small student satellite in house as well.\r\n\r\nLearning about this affordable access to space, the space company Dutch Space approached the faculty of Aerospace Engineering to discuss the possibility to test a new type of thin film solar cells in the space environment. In addition, the Dutch research institute TNO Science and Industry showed interest to join the initiative with an autonomous Sun Sensor using a wireless link for data transfer. A third new technology tested during the Delfi-C3 mission is an advanced high efficiency transceiver sized for application in pico- and nanosatellites. With these three new technologies as primary payloads and the space proven CubeSat concept as a basic principle of design, the Delfi-C3 nanosatellite is to be the first satellite that is designed and realized at Delft University of Technology. Delfi-C3 is scheduled for a piggyback launch by December 2007. | 32789 | DO-64 | Delft University of Technology | PSLV | <blank> | Nanosatellite | Satish Dawan Space Center, India | Delfi OSCAR-64 | <blank> |
  75. | 93 | 995.000 | 99.00 | 787.50 | http://www.usergioarboleda.edu.co/proyecto_espacial/index.htm | 1189073878 | 659.56 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | LIBERTAD-1 | 2007-04-17 | 98.00 | LIBERTAD-1 is a Cubesat built by Universidad Sergio Arboleda.\r\n\r\nThis satellite is possibly a duplicate entry for CP3. | 0 | <blank> | Universidad Sergio Arboleda | Dnepr | <blank> | Picosatellite | Baikonur Cosmodrome | <blank> | <blank> |
  76. | 94 | 0.879 | 99.20 | 800.20 | http://cape.louisiana.edu/ | 1220535463 | 652.40 | cubesat.gif | 0000-00-00 | 10 x 10 x 10cm | CAPE-1 | 2007-04-17 | 98.00 | The primary goal of the C.A.P.E program is to provide students the opportunity to design, develop and build satellite systems and perform experiments from a low earth orbit, LEO, using small and inexpensive satellites. We are a team of both graduate and undergraduate students working to make the University of Louisiana at Lafayette the first Louisiana university to place a satellite into orbit. In the process we are gaining invaluable experience in the design and implementation of space and communications systems.\r\n\r\nMore information on the telemetry including an explanation of the CW beacons can be found at <a href=\\"http://ulcape.org/wiki/CAPE1_Telemetry\\">http://ulcape.org/wiki/CAPE1_Telemetry</a>.\r\n\r\nCAPE-1 is the first satellite designed and built by a Louisiana university and to our knowledge the first satellite designed and built in the state of Louisiana. | 31130 | <blank> | University of Louisiana | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | <blank> | 2007-12P |
  77. | 96 | 1.000 | 101.39 | 832.00 | http://www.space.t.u-tokyo.ac.jp/cubesat/index-e.html | 1143166353 | 817.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10 cm | CubeSat XI-IV | 2003-06-30 | 98.72 | Cubesat XI-IV (pronounced Sai-Four) was launched from the Baikonure Cosmodrome into a sun-synchronous orbit approximately 832 x 817 km. Cubesat systems are:\r\n\r\n<UL><LI>OBC PIC16F877 4MHz, SEL protection circuit included</LI><LI>256kbytes EEPROM data recorder</LI><LI>CMOS image sensor</LI><LI>Telemetry Transmitter Nishimusen 430MHz band FM FSK AX25 1200bps</LI><LI>Command Receiver Nishimusen 140MHz band FM FSK AX25 1200bps</LI><LI>Beacon Transmitter Nishimusen 430MHz band CW 50WPM</LI><LI>Li-ion secondary battery, charged from solar cell</LI><LI>Permanent magnet,Libration damper</LI><LI>Sensors: Solar cell current,voltage, Battery voltage, Charge current, Cunsuming current, Temperature, RSSI</LI></UL> | 27848 | CO-57 | University of Tokyo | Dnepr | <blank> | Cubesat | Baikonur Cosmodrome | CubeSat-OSCAR 57 | 2003-031J |
  78. | 97 | 1.000 | 98.67 | 709.00 | http://www.space.t.u-tokyo.ac.jp/cubesat/mission/V/index-e.html | 1154757195 | 682.00 | cubesat.gif | 0000-00-00 | 10 x 10 x 10 cm | Cubesat XI-V | 2005-10-27 | 98.18 | Cubesat XI-V was launched from the Plesetsk MSC as part of the SSETI Express (XO-53) mission. \r\n\r\nIt carried the same payload as it\\'s predecessor Cubesat XI-IV:<UL><LI>OBC PIC16F877 4MHz, SEL protection circuit included</LI><LI>256kbytes EEPROM data recorder</LI><LI>CMOS image sensor</LI><LI>Telemetry Transmitter Nishimusen 430MHz band FM FSK AX25 1200bps</LI><LI>Command Receiver Nishimusen 140MHz band FM FSK AX25 1200bps</LI><LI>Beacon Transmitter Nishimusen 430MHz band CW 50WPM</LI><LI>Li-ion secondary battery, charged from solar cell</LI><LI>Permanent magnet,Vibration damper</LI><LI>Sensors: Solar cell current,voltage, Battery voltage, Charge current, Consuming current, Temperature, RSSI</LI></UL> | 28895 | CO-58 | University of Tokyo | Cosmos | <blank> | Cubesat | Plesetsk MSC | CubeSat-OSCAR 58 | 2005-043F |
  79. | 122 | 63.000 | 91.48 | 351.00 | https://goby.nrl.navy.mil/ANDE/Castor.html | 1286484840 | 343.00 | castor.jpg | 2010-08-18 | 19 inch diameter sphere | Castor | 2009-07-30 | 51.64 | <blank> | 0 | <blank> | Naval Research Laboratory | STS-127 | <blank> | Other | Kennedy Space Center | <blank> | <blank> |
  80. | 123 | 63.000 | 91.48 | 351.00 | https://goby.nrl.navy.mil/ANDE/Pollux.html | 1253805529 | 343.00 | pollox.jpg | 0000-00-00 | 19 inch diameter sphere | Pollux | 2009-07-30 | 51.64 | <blank> | 0 | <blank> | Naval Research Laboratory | STS-127 | <blank> | <blank> | Kennedy Space Center | <blank> | <blank> |
  81. | 99 | 0.000 | 104.77 | 1006.00 | <blank> | 1155263981 | 961.00 | rs-10.gif | 0000-00-00 | <blank> | Radio Sputnik 13 | 1991-02-05 | 82.92 | RS 12/13 was launched February 5, 1991 on board a Russian Cosmos C launcher. RS-12/13 rode piggyback on a primary spacecraft on a COSMOS 2123 Russian Navigation Satellite. Each satellite had two radio amateur transponders onboard. Only one was switched on at a time.\r\n\r\nBoth satellites had a 40 kHz wide linear transponder allowing for CW and SSB contacts. One unique feature of both these satellites was the ROBOT autotransponder. The autotransponders made it possible to carry on a CW telegraphy contact with the ROBOT computer carried on the spacecraft. Upon calling the satellite on the ROBOT uplink frequency, the computer would return with a short message and issue a QSO number.\r\n\r\nIt is thought that after superpower proton flashes from the Sun about July/August 2002 caused damaged to the COSMOS2123 and RS-12/13 transponders (thanks Jerry, K5OE/3).\r\n\r\nIn addition to the operating modes listed, RS-13 supported two additional modes<ul><li>Mode KT: 21 MHz uplink into 29 and 145 MHz downlinks</li><li>Mode KA: 21 MHz and 145 MHz uplinks into a common 29 MHz downlink</li></ul>\r\n | 21089 | RS-13 | Radio Sport Federation | Cosmos C | Cosmos 2123 | Payload | Plesetsk | <blank> | 1991-007A |
  82. +-------+---------+--------+---------+-----------------------------------------------------------------+------------+---------+----------------+------------+-------------------------+------------------+-------------+-------------+-------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+--------------+--------------+-----------------------------------+----------------+----------------+----------------+----------------------------------+-------------------+--------------------------+
  83.  
  84.  
  85.  
  86.  
  87.  
  88. Table: satellites
  89.  
  90. +-------+--------+--------+--------+-----------------------------------------------------------------------------------------+------------+---------+----------------+------------+--------------------+-------------+-------------+-------------+-----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+--------------+--------------+----------------------------------+----------------+----------------+----------------+------------------------------+-------------------+--------------------------+
  91. | satID | weight | period | apogee | website | updated | perigee | imgFile | decay_date | dimensions | common_name | launch_date | inclination | description | norad_number | oscar_number | organization | launch_vehicle | alternate_name | satellite_type | launch_location | OSCAR_designation | international_designator |
  92. +-------+--------+--------+--------+-----------------------------------------------------------------------------------------+------------+---------+----------------+------------+--------------------+-------------+-------------+-------------+-----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+--------------+--------------+----------------------------------+----------------+----------------+----------------+------------------------------+-------------------+--------------------------+
  93. | 100 | 1.000 | 101.34 | 829.00 | http://www.utias-sfl.net/nanosatellites/CanX1/ | 1256388769 | 815.00 | canx-1.gif | 0000-00-00 | 10x10x10cm | CanX-1 | 2003-06-30 | 98.71 | The Canadian Advanced Nanospace eXperiment 1 (CanX-1) is Canada\\'s first nanosatellite. It was built by graduate students of the Space Flight Laboratory (SFL) at University of Toronto Institute for Aerospace Studies (UTIAS).\r\n\r\nLaunched on June 30, 2003 at 14:15 UTC by Eurockot Launch Services from Plesetsk, Russia, CanX-1 is one of the smallest satellites ever built. It has a mass under 1 kg, fits in a 10 cm cube, and operates with less than 2 W of power. Its mission is to evaluate several novel technologies in space, including a low-cost CMOS horizon sensor and star-tracker, active three-axis magnetic stabilization, GPS-based position determination, and an ARM7 central computer. \r\n\r\nCanX-1 was not heard after launch. | 27847 | <blank> | University of Toronto, SFL | Rockot | <blank> | Cubesat | Plesetsk MSC | <blank> | 2003-031H |
  94. | 101 | 1.000 | 101.35 | 830.00 | http://dtusat1.dtusat.dtu.dk/group.php?c_gid=1 | 1253114600 | 816.00 | DTUSat1.jpg | 0000-00-00 | 10x10x10cm | DTUSat | 2003-06-30 | 98.72 | DTUsat is a picosatellite designed and built by students from the Technical University of Denmark, DTU.\r\n\r\nThe main payload of DTUsat is an electrodynamic tether for dumping the satellite. The tether is deployed using a novel yo-yo system, greatly simplifying construction and deployment. A calibrated test transmitter is flown as secondary payload. The satellite is 3-axis stabilized using magnetorquers, while attitude determination is done by a combination of a 3-axis magnetometer and 5 chip scale dual-axis sun angle sensors designed and built for this satellite. The mass of each sun angle sensor including supporting electronics is only 3 g. All flight electronics is designed using modern 3.3V CMOS integrated circuits, lowering total power consumption to about 400 mW while providing about 10 MIPS for application software.\r\n\r\nAll electronics in DTUsat is commercial 3.3V small-geometry CMOS to conserve power. We have tested for Total Ionizing Dose, which caused a maximum of 50% power consumption increase over the projected radiation dose. This is well within the power envelope of the system. The first chips are tested to fail at a total ionizing dose of about 7 krad, which translates to about a year given our shielding and orbit. This is sufficient for the mission. We do not yet know the rate of Single Event Upsets, but we have designed a global protection system, that shuts down and reboots the entire satellite by turning off the power supply if a latch-up is detected. Latch-up detection is decentralized to local sensors. Due to lack of power, weight, and time, we have opted for a simple configuration with little redundancy. | 27842 | <blank> | Technical University of Denmark | Rockot | <blank> | Cubesat | Plesetsk MSC | <blank> | 2003-031C |
  95. | 102 | 1.000 | 101.35 | 830.00 | http://www.cubesat.auc.dk/ | 1161099421 | 815.00 | AAUCubeSat.jpg | 0000-00-00 | 10x10x10cm | AAU Cubesat | 2003-06-30 | 98.72 | AAU CubeSat is a student satellite project at the University of Aalborg, Denmark, which was initiated in the Summer of 2001. The satellite project is a joint venture of the following institutes: <ul><li>Institute of Electronic Systems<li>Institute of Mechanical Engineering<li>Institute of Computer Science<li>Institute of Energy Technology</ul>\r\n\r\nAAU Cubesat was weakly heard after launch. The last known reception was on 26 July 2003. | 27846 | <blank> | Aalborg University | Rockot | <blank> | Cubesat | Plesetsk MSC | <blank> | 2003-031G |
  96. | 103 | 1.000 | 98.67 | 707.00 | http://www7.informatik.uni-wuerzburg.de/cubesat/index.php?option=com_frontpage&Itemid=1 | 1148346667 | 684.00 | UWE-1.jpg | 0000-00-00 | 10x10x10cm | UWE-1 | 2005-10-27 | 98.17 | UWE-1 was one of three CubeSats deployed by SSETI-Express. The first contact was 27 October 2005 when the satellite was copied by the University of W\xfcrzburg ground control station at approximately 11:08 UTC. It operated for approximately 21 days before contact was lost.\r\n\r\nUWE-1 is a complete satellite with the following subsystems:<ul><li>CubeSat</li><li>Communications (Telemetry, Tracking and Command)</li><li>Electronics (inc. Sensors)</li><li>Power Supply</li><li>Orbit and Attitude Determination </li><li>Integration (inc. Release mechanism) and Test</li><li>GroundStation</li><li>Hardware (Antenna, Radio, Modem)</li><li>Software (Tracking, Control)</li><li>Communications (Network)</li><li>Onboard Software</li></ul>\r\n\t\t\t | 28892 | <blank> | University of W\xfcrzburg | Kosmos-3M | <blank> | Cubesat | Plesetsk MSC | <blank> | 2005-043C |
  97. | 104 | 1.000 | 98.66 | 706.00 | http://www.ncube.no/ | 1148348555 | 683.00 | NCube2.gif | 0000-00-00 | 10x10x10cm | NCube-2 | 2005-10-27 | 98.17 | Note: nCube-2 is listed in Space-Track as SSETI-Express Deb(ris).\r\n\r\nAfter a successful launch of SSETI Express and NCube-2, the groundstations in Narvik and at Svalbard did not receive any confirmed signal from NCUBE-2, 14 days into the mission. With no reports from radio amateurs establishing contact either, it seems that the satellite is not sending any signals or is somehow prevented from doing so.\r\n\r\nOn 22 December 2006 SpaceTrack observed a new object near SSETI Express and assigned it the number 28897. It is assumed (but not confirmed) that this is NCube-2. | 28897 | <blank> | University of Oslo (and others) | Kosmos-3M | <blank> | Cubesat | Plesetsk MSC | <blank> | 2003-043H |
  98. | 105 | 0.000 | 0.00 | 0.00 | http://polimage.polito.it/picpot/html/index.shtml | 1154113100 | 0.00 | cubesat.gif | 0000-00-00 | 10 | PicPot | 2006-07-26 | 0.00 | PicPot is a cubesat designed by Politecnico di Torino. It contains several on-board cameras and telemetry system that will be transmitting on either a 437MHz (9600 FSK AX.25) or 2440MHz (10Kbps GFSK, +/-125KHz deviation) link. \r\n\r\nPicPot was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. | 0 | <blank> | Politecnico di Torino, Italy | Dnepr | <blank> | Nanosatellite | Baiknour Cosmodrome | PicPot | <blank> |
  99. | 106 | 2.700 | 94.02 | 663.00 | http://www.hit.ac.jp/~satori/hitsat/index-e.html | 1216946265 | 279.00 | hitsat.jpg | 2008-06-18 | 10x10x10 | HITSat | 2006-09-22 | 98.32 | <blank> | 29484 | HO-59 | Hokkaido Institute of Technology | JAXA M-V | <blank> | Cubesat | Kagoshima Space Center | HITSat-OSCAR 59 | 2006-041F |
  100. | 107 | 4.500 | 91.93 | 370.00 | http://www.genesat1.org | 1344106535 | 368.00 | <blank> | 2010-08-04 | 10cm x 10cm x 30cm | GeneSat-1 | 2006-12-16 | 40.02 | GeneSat-1 launched from the Mid-Atlantic Regional Spaceport (MARS) at NASA Wallops Flight Facility on December 16, 2006, as a secondary payload aboard a Minotaur launch. GeneSat-1 is a 10 x 10 x 30 cm. spacecraft, which will conduct a cellular biology technology demonstration.\r\n\r\nOf particular interest to the amateur radio satellite community, is the GeneSat-1 beacon. Operating at 437.075 MHz FM, the beacon sends an AX.25 packet at 1200 baud every 5 seconds; the packet contains data about the spacecraft systems operation. The beacon will initiate transmission as soon as the spacecraft is deployed from its carrier on the 4th stage of the launch vehicle.\r\n\r\nTo foster interest in the amateur community, and to support amateur radio and space technology outreach to secondary and higher education student groups, the GeneSat University Mission Ops Team is sponsoring a contest, with recognition and awards . Click <a href=\\"http://www.crestnrp.org/genesat1/ahc.html\\">here</a> for full details.\r\n\r\nPlease contact Mike Miller for more information.\r\nmmiller@inwspace.org\r\nKE7EGC | 29655 | <blank> | <blank> | Minotaur-1 | <blank> | Cubesat | NASA Wallops Flight Facility | <blank> | <blank> |
  101. | 108 | 0.000 | 0.00 | 0.00 | http://www.ew.usna.edu/~bruninga/ande-raft-ops.html | 1211903835 | 0.00 | <blank> | 2007-12-25 | <blank> | ANDE | 2006-12-21 | 0.00 | ANDE was deployed 21 Dec 2006 from the payload bay of STS-116 and after an hour or so of being stuck in its cannister, finally separated and became operational as ANDE-1 and ANDE-2 with an APRS digipeater on 145.825 MHz. | 29664 | NO-61 | US Naval Academy | STS-116 | <blank> | Microsatellite | Cape Canaveral, FL | Navy-OSCAR 61 | <blank> |
  102. | 109 | 0.000 | 0.00 | 0.00 | http://www.ew.usna.edu/~bruninga/ande-raft-ops.html | 1211903820 | 0.00 | <blank> | 2007-05-30 | <blank> | RAFT | 2006-12-21 | 0.00 | RAFT was deployed 21 Dec 2006 from the payload bay of STS-116 but separated with a high tumble rate of over 39 RPM. It had slowed to 25 RPM a month later. It has a weak signal, but supports an APRS digipeater on 145.825 MHz. It also has a packet-to-voice synthesizer, a PSK-31 transponder with 28.120 LSB uplink and a radar fence receiver on 216.98 MHz. | 0 | NO-60 | US Naval Academy | STS-116 | <blank> | Cubesat | Cape Canaveral, FL | Navy OSCAR-60 | <blank> |
  103. +-------+--------+--------+--------+-----------------------------------------------------------------------------------------+------------+---------+----------------+------------+--------------------+-------------+-------------+-------------+-----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+--------------+--------------+----------------------------------+----------------+----------------+----------------+------------------------------+-------------------+--------------------------+
  104.  
  105.  
  106.  
  107.  
  108.  
  109. Table: summary
  110.  
  111. +--------------+------------------------------------------------------------------------------------+
  112. | Column | Type |
  113. +--------------+------------------------------------------------------------------------------------+
  114. | APRS | tinyint(3) unsigned |
  115. | beacon | tinyint(3) unsigned |
  116. | C | tinyint(3) unsigned |
  117. | H | tinyint(3) unsigned |
  118. | K | tinyint(3) unsigned |
  119. | L | tinyint(3) unsigned |
  120. | overall | enum('Operational','Semi-Operational','Non-Operational','Future Launch','Unknown') |
  121. | PKT | tinyint(3) unsigned |
  122. | report | tinyint(1) |
  123. | S | tinyint(3) unsigned |
  124. | satID | bigint(20) unsigned |
  125. | schedule | tinytext |
  126. | scheduleURL | tinytext |
  127. | U | tinyint(3) unsigned |
  128. | updated | bigint(20) unsigned |
  129. | V | tinyint(3) unsigned |
  130. | wsr_comments | text |
  131. | X | tinyint(3) unsigned |
  132. +--------------+------------------------------------------------------------------------------------+
  133.  
  134.  
  135.  
  136.  
  137. Table: summary
  138.  
  139. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+------------------+----------------------------+-----------------------------------------------------------------+---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
  140. | satID | C | H | K | L | S | U | V | X | PKT | APRS | beacon | report | updated | overall | schedule | scheduleURL | wsr_comments |
  141. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+------------------+----------------------------+-----------------------------------------------------------------+---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
  142. | 24 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 1 | 1144611755 | Non-Operational | <blank> | <blank> | <blank> |
  143. | 2 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | 0 | 0 | 0 | 1 | 1 | 1331808309 | Operational | <blank> | <blank> | Current Mode: U/V - Dutch Transponder\r\n\r\nTo know what transponder is switched on please listen for the beacon that is\r\nactive. Each transponder has a different beacon, see below:\r\n\r\nIndian transponder - unmodulated carrier on 145.936MHz.\r\nDutch Transponder - CW message on 145.860MHz. |
  144. | 1 | 0 | 3 | 0 | 3 | 3 | 3 | 3 | 0 | 3 | 0 | 3 | 1 | 1323708479 | Non-Operational | AO-51 Schedule | http://www.amsat.org/amsat-new/echo/ControlTeam.php | November 29, 2011\r\n\r\nIt is with a heavy heart I report that AO-51 has ceased transmission and is not responding to commands. The last telemetry data indicated that the third of six batteries was approaching failure to short, and observations indicate the voltage from three cells is insufficient to power the UHF transmitters. The IHU may continue to be operative. Initial tests with the S band transmitter were also not positive, although more attempts are in order. We have tried leaving the satellite in an expected state where if voltages climb high enough, the 435.150 transmitter may possibly be heard.\r\n\r\nThe command team will regularly attempt communications with the satellite over the coming months (and years). There is always the possibility that a cell will open and we could once again talk to our friend while illuminated. Thanks to all who helped fund, design, build, launch, command, and operate AO-51. It\\'s 7 year mission has been extraordinary. Please support AMSAT\\'s Fox-1 project, and other AMSAT projects worldwide with your time and money.\r\n\r\nFor the AO-51 Command Team,\r\n\r\n73, Drew KO4MA\r\nAMSAT-NA VP Operations\r\n\r\nOctober 16, 2011\r\n\r\nCurrently we are running the repeater on 435.150 down, 145.880 up. Somehow, we\\'ve found a sweet spot where it will run through eclipse, despite 2 of the 6 cells in the battery being shorted. Enjoy it while it lasts!\r\n\r\nMay 6, 2011\r\n\r\nWe are having a difficult time trying to restore AO-51 to operation. Currently, the satellite will not retain the upload of the flight software across eclipse. The batteries are in very poor condition. We have a few more things to try, but with eclipses peaking around July at ~27 minutes, the long term situation is grim. There is a brief period around November where eclipses are as short as 16 minutes, but past that it is a long climb to 30 minutes or longer eclipses for many years. We have no expected \\"return to service\\" date. If you have 9k6 digital capability, you can listen in on our attempts at recovery on 435.150 on many passes over the US.\r\n\r\nPlease support AMSAT-NA and the other AMSAT groups around the world, and help us get new satellites into orbit. Projects like Fox, FunCube, P3E, and Kiwisat need your financial support to keep our amateur satellite fleet flying.\r\n\r\n73, Drew KO4MA\r\nAMSAT-NA VP Operations |
  145. | 3 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  146. | 6 | 0 | 5 | 0 | 0 | 0 | 0 | 5 | 0 | 0 | 0 | 2 | 0 | 1230598507 | Semi-Operational | <blank> | <blank> | W7OIL has reported that the 10-meter beacon is only operational when the satellite is illuminated. |
  147. | 5 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | 0 | 3 | 0 | 1 | 1 | 1326128110 | Operational | <blank> | <blank> | January 2012: FO-29 is reported to be operational again. Please check AMSAT-bb for reports.\r\n\r\n-----\r\n\r\nPlease send reception reports to lab2 \\'at\\' jarl.or.jp.\r\nPlease use the subject line: \\'FO-29 reception report\\'.\r\n\r\nMineo, JE9PEL, has an FO-29 satellite telemetry analysis program that will automatically analyze all digital telemetry from the satellite (such as current, voltage and temperature). FO29CWTE is available at:\r\n<a href=\\"http://www.ne.jp/asahi/hamradio/je9pel/\\">http://www.ne.jp/asahi/hamradio/je9pel/\r\n</a>\r\n\r\n |
  148. | 139 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | 1318428001 | Operational | <blank> | <blank> | <blank> |
  149. | 140 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | 1318427962 | Operational | <blank> | <blank> | <blank> |
  150. | 7 | 0 | 0 | 0 | 0 | 0 | 2 | 2 | 0 | 0 | 0 | 0 | 1 | 1349806795 | Semi-Operational | AO-27 Website | http://www.ao27.org | AO-27 is currently recovering from a software crash. Please do not transmit to the satellite until the repeater function is restored.\r\n\r\nThe latest information on AO-27 from control operator Michael Wyrick, N3UC (former N4USI), can be found at:\r\n<a href=\\"http://www.ao27.org\\">http://www.ao27.org</a>\r\n\r\nAn AO-27 question-and-answer page is available on the AMSAT-NA web site, with updates by Ray, W2RS. The URL is:\r\n<a href=\\"http://www.amsat.org/amsat/intro/ao27faq.html\\">http://www.amsat.org/amsat/intro/ao27faq.html</a>.\r\n\r\n----\r\n\r\nOn July 1st, 2007 during the 20:00 UTC pass over North America, AO-27 was again providing a new round of enjoyment for Amateur satellite experimenters. Thirteen years ago, AO-27, which coined the term \\"Easy Sat\\" by employing an FM bent pipe in space, provided many hams the ability to use a satellite without the expense of multi mode radios.\r\n\r\nThis time around, AO-27 was used to provide the first D-Star via Satellite contact between Michael, N3UC, FM-18 in Haymarket VA and Robin, AA4RC, EM-73 in Atlanta GA. Signals were reported as strong and easy to copy. Call signs were received digitally on both sides of the link. Communications were possible for most of the pass. Both Robin and Michael were surprised at just how well the digital link was received.\r\n\r\nThe Analogue repeater on-board AO-27 is well suited for D-Star work. The radios were designed to pass 1200-19200 baud GMSK data. The Analogue mode was not a primary mode of operation in the design. Using a free switch setting in the switching board, the design team hooked up the output of the receiver to the input the transmitter to create the Analogue mode. There is not the normal low frequency filtering that is found in normal FM Repeaters. This means the Analogue mode passes the low frequencies required by D-Star.\r\n\r\nThe equipment for the contact were IC-2200s on the Uplink at both N3UC and AA4RC, an IC-2820 on the downlink at N3UC, and an IC-91AD on the downlink at AA4RC. Doppler shift did prove to be a minor problem while using these radios. The D-Star signal would decode out to about 1.5 KHz in frequency error. The IC-2820 would only tune on 5 KHz spacing (the 6.25 KHz channels did not fall in the right locations to help.) so at times we could not decode the digital signals.\r\n\r\nFor others that want to try D-Star via Satellite we have a few things to keep in mind. \r\n\r\n 1) Remember that the FM users can\\'t hear you on the bird. \r\n They hear a strong \\"noise\\" but can\\'t decode you. So please keep the D-Star transmitting short. \r\n If you can monitor the FM side, you can time your transmitting as to not step on them. \r\n Please try to schedule with other D-Star users instead of calling CQ for the entire pass.\r\n \r\n 2) Watch the doppler, at times you may not be able to decode a signal even if the other station can decode you.\r\n Keep your uplink on 145.850 for the entire pass. Program your radio call signs the same as for simplex, AO-27 does not have a D-Star call sign. You don\\'t need to set up your radio for repeater use.\r\n \r\n 3) Before using other satellites besides AO-27, please check with the control operators of those satellites. Every\r\n FM satellite may not pass the D-Star signal nor may the control operators wish to have D-Star traffic on the bird.\r\n \r\n 4) If you here us on the Bird, please give us a call. We would love to have as many D-Star users on AO-27 as possible.\r\n \r\n\r\nThe AO-27 Control Operators fully support and encourage the use of D-Star via Satellite on AO-27.\r\n\r\nMichael\r\nN3UC\r\nAO-27 Control Operator\r\n |
  151. | 122 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 3 | 0 | 1286484860 | Non-Operational | Castor Webpage | https://goby.nrl.navy.mil/ANDE/Castor.html | <blank> |
  152. | 123 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 3 | 0 | 1253723902 | Non-Operational | Pollux Webpage | https://goby.nrl.navy.mil/ANDE/Pollux.html | Reported non-operational mid-September on AMSAT-bb. |
  153. | 4 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | 0 | 0 | 0 | 0 | 1 | 1144610845 | Operational | <blank> | <blank> | There have been unconfirmed reports on the amsat-bb remailer that SO-50 has\r\nshifted downlink frequency as much as 5khz up. This both from Europe.\r\n\r\nTo switch the transmitter on, you need to send a CTCSS tone of 74.4 Hz. The order of operation is thus: (allow for Doppler as necessary)\r\n\r\n1) Transmit on 145.850 MHz with a tone of 74.4 Hz to arm the 10 minute timer on board the spacecraft.\r\n2) Now transmit on 145.850 MHz (FM Voice) using 67.0 Hz to PT the repeater on and off within the 10 Minute window.\r\n3) Sending the 74.4 tone again within the 10 minute window will reset the 10 minute timer. |
  154. | 8 | 0 | 3 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 3 | 0 | 1 | 1160932965 | Non-Operational | PCSAT2 Design Page | http://web.usna.navy.mil/~bruninga/pcsat2.html | Official Webpage: http://web.usna.navy.mil/~bruninga/pcsat2.html\r\nPCSAT2 APRS Packet page: http://www.findu.com/cgi-bin/pcsat2.cgi\r\n\r\n |
  155. | 106 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 3 | 0 | 3 | 1 | 1216946460 | Non-Operational | HIT-SAT HO-59 Webpage | http://www.hit.ac.jp/~satori/hitsat/index-e.html | From the HIT-SAT HO-59 command team blog:\r\n\r\n2008/6/20&#65306;End of operation \r\nHIT-SAT was decay orbit on June 18 2008. We would like to express our heartfelt gratitude to you for many reception report. We take the project forward into its next stage. Last CW voice by HIT-SAT ground staiton(MP3 sounds)here.\r\nThank you very much. \r\n&#65288;16:00&#65289;JST \r\n |
  156. | 9 | 0 | 2 | 0 | 0 | 3 | 2 | 2 | 0 | 0 | 0 | 2 | 1 | 1311603862 | Operational | AO-7 Log and Resource Site | http://www.planetemily.com/ao7/ | In mid 1981 AO-7 ceased operation due to battery failures. It was thought at that time that the batteries had shorted. However on June 21, 2002, at least one of the shorted batteries went open-circuit, allowing the satellite to waken whenever it is in sunlight, and randomly begin operation in one of 4 modes.\r\n\r\nAccording to the log this old warrior is still supporting transponder action in mode A and mode B as recently as 9/10/09, and on a regular basis, whenever it is in sunlight.\r\n\r\nWhen the satellite is in sunlight for extended periods of time, the 24-hour timer still switches the bird between modes A and B. Listen for the corresponding beacon to determine which mode the satellite is currently operating in, or refer to the abovementioned web page to see what mode has recently supported QSO\\\\\\'s as the best estimate of what is the current mode of operation.\r\n\r\nPlease remember, there are no (functional) batteries, so the satellite\\\\\\'s power input is limited to whatever output can be generated by the ancient solar panels. Use the least uplink power possible to minimize your downlink power usage, and maximize the number of simultaneous QSO\\\\\\'s supported in the passband. Linear transponder birds are a scarce commodity these days, so please use AO-7 responsibly, but please DO enjoy her!\r\n |
  157. | 20 | 0 | 0 | 0 | 0 | 3 | 3 | 3 | 0 | 0 | 0 | 3 | 1 | 1144611725 | Non-Operational | <blank> | http://www.amsat.org/amsat-new/satellites/sat_summary/SSETI.php | SSETI Express was launched Plesetsk Cosmodrome in Russia is currently in orbit. The local time of the ascending node is approximately mid morning. SSETI was assigned the OSCAR number XO-53, and the NORAD ID number 28894. Please see the SSETI project page for additional details and links to downloads and mission information.\r\n\r\nShortly after deployment SSETI entered safe mode and began to send 9k6 baud and carrier pulse telemetry. Many hams reported hearing it. It deployed it\\'s three Cubesats. Somewhere around orbit 6 it was reported that SSETI was toggling between safe mode and recovery mode, and that the bus voltage was oscillating between 24V and 0V. Since that time contact with SSETI has been lost, though the control station is hopeful for recovery.\r\n\r\nSome additional information about SSETI. Data modes will be primarily used for downlinking telemetry and data from the satellites experiments. ESA will be providing telemetry capture software for amateurs to use and will be offering a prize to the amateur station who provides them with the most telemtry after launch. The mode U/S FM voice transponder will require 67Hz tone access in a similar way to AO51 and will provide three channels of 256 bit telemetry encoded as DTMF tone bursts. S Band output is 3 Watts to 3 x 8dBic RHCP patch antennas.\r\n\r\nLatest information including integration photographs and a webcam in the cleanroom is at http://www.sseti.net - click on \\"missions\\" and then \\"express\\". The Mission Operations website is also accessable from this page. \r\n |
  158. | 10 | 0 | 0 | 0 | 0 | 3 | 0 | 2 | 0 | 0 | 0 | 2 | 1 | 1259606860 | Operational | <blank> | <blank> | From Clive, G3CWV:\r\n22 November 2009\r\n\r\nI have received two reports from Keith N4ZQ (EL88ob) that he has heard\r\nUO-11 on 19 November at 13:33 - 13:43, and on 22 November at 13:02 UTC.\r\n\r\nHe has sent me a WAV file of the second pass. Unfortunately, it\\'s a \r\nvery low elevation pass, and probably will be difficult to decode, as it \r\ncontains a lot of noise. However it\\'s definitely UO-11.\r\n\r\nI\\'ll be interested in receiving any other reports. The frequency is \r\n145.826 MHz. Mode is FM. Further details are on my OLD website \r\nwww.users.zetnet.co.uk/clivew There is an audio clip to help identify \r\nthe satellite.\r\n\r\nPlease e-mail me via the AMSAT reflector, or post to this bulletin board.\r\n\r\nFrom Clive, G3CWV:\r\n13 September 2007\r\n\r\nNothing heard from OSCAR-11 recently.. Eclipses finished on 20 August,\r\nalthough previous observations had suggested that sustained operation\r\ncould have been supported any time after 10 August.\r\n\r\nI would appreciate any reception reports of the satellite. Please post\r\nto AMSAT-BB or directly to g3cwv@amsat.org .\r\n\r\nIf you are able to record as a WAV file, please do so, and make a note\r\nof the exact time of the start of recording in UTC. Please let me know\r\nwhat you have, but PLEASE DO NOT send recordings without further\r\ndiscussion.\r\n\r\nThe frequency of the VHF beacon is 145.825 MHz, mode FM.\r\n\r\nIf you require further information, or need to hear what the satellite\r\nsounds like, please visit my website -\r\n\r\nwww.users.zetnet.co.uk/clivew\r\n\r\n\r\n----\r\n\r\n\r\nThis from Clive, G3CWV:\r\n27 March 2006\r\n\r\nOn 01 March OSCAR-11 achieved 22 years in orbit, and in spite of numerous problems, it still continues to transmit good signals.\r\n\r\nDuring the period 14 February to 26 March 2006 the VHF beacon on 145.826 MHz has been heard from 22 February to 04 March, and from 14 to 24 March.\r\n\r\nSignals have been very consistent and excellent copy has been obtained on all passes received. If the current mode of operation continues, the beacon should switch ON around 04 April 2006.\r\n\r\nThe on-board clock continues to show a very large accumulated error. On 24 March it was 22.14308 days slow. However, the clock is now very stable. During the last month it gained 2.5 seconds, which is approximately half the monthly gain, observed when the satellite was fully operational! The observations of clock errors suggest that the clock may slow or stop when the battery voltage is low.\r\n\r\nAll the analogue telemetry channels, 0 to 59 are zero, ie they have failed. The status channels 60 to 67 are still working.\r\n\r\nThe satellite is now in continuous sunlight until around 06 May, when eclipses will start again. This should help the satellite to continue transmitting, although continuous sunlight can cause problems due to excessive temperatures. Power supply problems can be caused by poor pointing attitude, ie the sunlight illuminating the ends of the satellite, instead of the solar arrays.\r\n\r\nThe watchdog timer now appears to have resumed operation on the 20 day cycle. During the last two months the ON/OFF times have been very consistent, and many observations show this to be 20.7 days, ie. 10.3 days ON followed by 10.4 days OFF. However, at any time, poor solar attitude, and battery problems, may result in a low 14 volt line supply, which may cause the beacon to switch OFF prematurely, and reset the watchdog timer cycle.\r\n\r\nI am indebted to Bob G4VRC, Gustavo LW2DTZ, Mike DK3WN, John K7RQN and John G4PWG for their reception reports. All have reported good signals from the VHF beacon. Many thanks for those reports.\r\n\r\nThe Beacon frequencies are -\r\n\r\nVHF 145.826 MHz. AFSK FM ASCII Telemetry\r\n\r\nUHF 435.025 MHz. OFF\r\n\r\nS-band 2401.5 MHz. OFF\r\n\r\nListeners to OSCAR-11 may be interested in visiting my website which contains an archive of news & telemetry data. It also contains details about using a soundcard or hardware demodulators for data capture. There is software for capturing data, and decoding ASCII telemetry. The URL is: http://www.users.zetnet.co.uk/clivew/ |
  159. | 11 | 0 | 0 | 0 | 0 | 3 | 3 | 3 | 0 | 0 | 0 | 0 | 1 | 1317820491 | Non-Operational | <blank> | <blank> | <blank> |
  160. | 117 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 1230438291 | Non-Operational | <blank> | <blank> | Reentered. |
  161. | 118 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 1230438745 | Non-Operational | <blank> | <blank> | <blank> |
  162. | 119 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 1232763093 | Operational | <blank> | <blank> | <blank> |
  163. | 120 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 1232763070 | Operational | <blank> | <blank> | <blank> |
  164. | 121 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 1232763162 | Operational | <blank> | <blank> | <blank> |
  165. | 124 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 0 | 1271902859 | Non-Operational | Aggiesat Webpage | http://aggiesat.org/ | This satellite is not IARU coordinated. |
  166. | 125 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 0 | 1286484656 | Non-Operational | Paradigm Webpage | http://paradigm.ae.utexas.edu/ | From the BEVO-1 website:\r\n\r\nAn example of a BEVO1 beacon string is given by \\"BEVO1 E6 D080704 I0754 TN05 BA73 BB73\\". The first five characters are the callsign BEVO1. The number following the \\"E\\" represents an error code, where zero indicates no error. The numbers following the \\"D\\" represent the current date as determined by the satellite and follows the format \\"YYMMDD\\". The numbers following the \\"I\\" represent the current time as determined by the satellite and follows the format \\"HHMM\\". The characters following the \\"T\\" represent the current satellite temperature in degrees Celsius, where \\"N\\" is negative and \\"P\\" is positive and the two numbers following indicate the magnitude of the temperature. The numbers following \\"BA\\" and \\"BB\\" indicate the battery voltage of packs \\"A\\" and \\"B\\", respectively, where the voltage in Volts has been multiplied by ten.\r\n |
  167. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+------------------+----------------------------+-----------------------------------------------------------------+---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
  168.  
  169.  
  170.  
  171.  
  172.  
  173. Table: summary
  174.  
  175. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+------------------+---------------------------+----------------------------------------------------------------------------------------------------------+--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
  176. | satID | C | H | K | L | S | U | V | X | PKT | APRS | beacon | report | updated | overall | schedule | scheduleURL | wsr_comments |
  177. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+------------------+---------------------------+----------------------------------------------------------------------------------------------------------+--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
  178. | 12 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 3 | 1 | 1256752640 | Non-Operational | <blank> | <blank> | The CW beacon went silent October 21, 2009.\r\n\r\n* The CW beacon is sending eight telemetry channels and one status channel on 437.126 MHz. \r\n* No BBS service is available. \r\n* The digipeater is not active. \r\n\r\nGeneral information and telemetry samples can be found at:\r\nwww.telecable.es/personales/ea1bcu |
  179. | 13 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  180. | 14 | 0 | 0 | 0 | 5 | 0 | 2 | 5 | 0 | 2 | 3 | 0 | 1 | 1287849186 | Semi-Operational | GO-32 Site | http://www.technion.ac.il/ASRI/techsat/ | GO-32 is in bootloader mode, and is not expected to return to service (de KO4MA 10/23/2010)\r\n\r\n |
  181. | 131 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 1290812547 | Operational | <blank> | <blank> | <blank> |
  182. | 15 | 3 | 3 | 3 | 3 | 3 | 3 | 3 | 3 | 3 | 0 | 3 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | AO-40 has suffered a catastrophic failure, and although recovery efforts continue it is not likely to return to service. |
  183. | 16 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | SO-41 was in operation when turned on by an internal timer that appears to be programmed to turn it on over major land areas. The repeater was operational in September 2003 but has not been heard since that time. |
  184. | 17 | 0 | 0 | 0 | 0 | 0 | 3 | 2 | 0 | 0 | 0 | 0 | 1 | 1287533540 | Semi-Operational | <blank> | http://web.usna.navy.mil/%7ebruninga/pcsat.html | <blank> |
  185. | 132 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 1290812536 | Operational | <blank> | <blank> | <blank> |
  186. | 133 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1308577397 | Non-Operational | Beacon Information | http://rax.engin.umich.edu/?page_id=311 | <blank> |
  187. | 134 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 1290812431 | Operational | <blank> | <blank> | <blank> |
  188. | 135 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 0 | 1296417693 | Non-Operational | <blank> | <blank> | <blank> |
  189. | 136 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 3 | 0 | 1325862309 | Non-Operational | Deployed August 3, 2011 | www.amsat.org | ARISSat-1 reentered on January 4, 2012. |
  190. | 18 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1147549310 | Non-Operational | <blank> | <blank> | Presumed non-operational. |
  191. | 19 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | 0 | 1 | 1 | 0 | 1 | 1258931002 | Operational | See link for current mode | http://www.issfanclub.com/ | \t \r\nWhile the system is in cross-band repeat mode the packet system is turned off and vice-versa.\r\n\r\nThe ISS daily crew schedule can be found at <a href=\\"http://spaceflight.nasa.gov/station/timelines/\\">http://spaceflight.nasa.gov/station/timelines/</a>. Remember that the crew operates on UTC time. The timelines are sent to the crew in Russian, and partially translated for ground controllers in America. No all-English translations are available at this time.\r\n\r\nCurrent ARISS News is available at the <a href=\\"http://www.amsat.org/amsat-new/ariss/\\">ARISS page</a>. Additional information is available at: <a href=\\"http://www.issfanclub.com/\\">http://www.issfanclub.com/</a>.\r\n\r\n |
  192. | 115 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | 1222303469 | Operational | <blank> | <blank> | <blank> |
  193. | 116 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 3 | 0 | 1 | 0 | 1300549118 | Operational | CAMSAT schedule | http://www.camsat.cn/ | Operation is currently beacon only while a scheduling fault is investigated. |
  194. | 137 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 1300549130 | Non-Operational | <blank> | <blank> | <blank> |
  195. | 126 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | 1253716003 | Operational | EPFL Swisscube website | http://swisscube.epfl.ch/ | <blank> |
  196. | 127 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 0 | 0 | 0 | 1 | 0 | 1264607671 | Operational | ITU Space Systems Lab | http://usl.itu.edu.tr/ | <blank> |
  197. | 128 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 0 | 1262093377 | Operational | UWE-2 Website | http://www7.informatik.uni-wuerzburg.de/forschung/space_exploration/projekte/cubesat/uwe-2/get_involved/ | <blank> |
  198. | 129 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | 1312119939 | Operational | T.U. Berlin | http://www.raumfahrttechnik.tu-berlin.de/beesat | <blank> |
  199. | 21 | 4 | 4 | 4 | 4 | 4 | 4 | 4 | 0 | 0 | 0 | 0 | 0 | 1248897335 | Future Launch | <blank> | <blank> | AMSAT-Phase 3E is a project of AMSAT-DL and will operate with similar goals as AO-40. Launch is not yet identified. Additional information can be found at http://www.amsat-dl.org/p3e/. |
  200. | 99 | 0 | 3 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 3 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  201. | 26 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  202. | 25 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  203. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+------------------+---------------------------+----------------------------------------------------------------------------------------------------------+--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
  204.  
  205.  
  206.  
  207.  
  208.  
  209. Table: summary
  210.  
  211. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+------------------+----------+-------------+--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
  212. | satID | C | H | K | L | S | U | V | X | PKT | APRS | beacon | report | updated | overall | schedule | scheduleURL | wsr_comments |
  213. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+------------------+----------+-------------+--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
  214. | 52 | 0 | 3 | 0 | 3 | 0 | 2 | 3 | 0 | 0 | 0 | 2 | 0 | 1147549161 | Semi-Operational | <blank> | <blank> | Reports have indicated that SO-33 is active on 437.910. A short FSK burst can be heard about once per minute. |
  215. | 48 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  216. | 59 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  217. | 61 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | The website <a href=\\"http://hft.fh-pforzheim.de/ao49/\\" target=\\"_blank\\">http://hft.fh-pforzheim.de/ao49/</a> reports that the downlink is operational when the satellite is in direct sunlight however it also reports that:\r\n\r\n\\"<i>On Jan. 30 [2003] SAFIR-M was switched off continously. On Jan. 31 it transmitted sometimes. On Feb. 1 no transmission is logged. We hope normal operation will restart soon.<i>\\" |
  218. | 60 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  219. | 58 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  220. | 57 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1147549261 | Non-Operational | <blank> | <blank> | Presumed to be non-operational or not operating in the amateur band. |
  221. | 54 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  222. | 55 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  223. | 56 | 0 | 0 | 0 | 0 | 3 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  224. | 53 | 0 | 0 | 0 | 3 | 3 | 3 | 3 | 0 | 3 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  225. | 51 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  226. | 40 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  227. | 49 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 1 | 1221680526 | Non-Operational | <blank> | <blank> | PO-28 is reported as non-operational due to battery issues. |
  228. | 50 | 0 | 0 | 0 | 0 | 0 | 2 | 3 | 0 | 0 | 0 | 0 | 1 | 1144610845 | Semi-Operational | <blank> | <blank> | IO-26 is semi-operational - only the downlink is available |
  229. | 45 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  230. | 47 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  231. | 42 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 3 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  232. | 43 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  233. | 44 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  234. | 29 | 0 | 3 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  235. | 28 | 0 | 3 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  236. | 27 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  237. | 30 | 0 | 3 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  238. | 31 | 0 | 3 | 0 | 0 | 3 | 3 | 3 | 3 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  239. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+------------------+----------+-------------+--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
  240.  
  241.  
  242.  
  243.  
  244.  
  245. Table: summary
  246.  
  247. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+-----------------+---------------------+----------------------------+-----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
  248. | satID | C | H | K | L | S | U | V | X | PKT | APRS | beacon | report | updated | overall | schedule | scheduleURL | wsr_comments |
  249. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+-----------------+---------------------+----------------------------+-----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
  250. | 32 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 2 | 1 | 1230598397 | Non-Operational | <blank> | <blank> | AO-10 has been locked into a Mode-B, 70-cm uplink and\r\n2-meter downlink for several years.\r\n\r\nW4SM has more information about the satellite at the following URL:\r\nhttp://www.cstone.net/~w4sm/AO-10.html\r\n |
  251. | 39 | 0 | 3 | 0 | 3 | 3 | 3 | 3 | 0 | 0 | 0 | 3 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  252. | 62 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  253. | 63 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 3 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  254. | 65 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 3 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  255. | 68 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 3 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  256. | 67 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  257. | 66 | 0 | 0 | 0 | 0 | 3 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  258. | 64 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 3 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  259. | 69 | 0 | 0 | 0 | 0 | 0 | 1 | 0 | 0 | 1 | 0 | 1 | 1 | 1233963289 | Operational | <blank> | <blank> | CW beacon copied 2/6/2009 by KO4MA\r\n\r\nInformation webpage:\r\nhttp://lss.mes.titech.ac.jp/ssp/spacerium/cute1blog/\r\n |
  260. | 70 | 0 | 0 | 0 | 5 | 0 | 3 | 0 | 0 | 0 | 0 | 3 | 1 | 1256753516 | Non-Operational | <blank> | <blank> | CO-56 reentered in late October 2009. |
  261. | 71 | 0 | 0 | 0 | 0 | 0 | 3 | 3 | 0 | 0 | 0 | 3 | 0 | 1323372612 | Non-Operational | Activation Schedule | http://www.amsatsa.org.za/ | September 2011 - SO-67 off air temporarily. From SA-AMSAT:\r\n\r\n\\"SO67 SAFE BUT PROBLEMATIC\\"\r\n\r\n\\"The Ground Control Station Engineers at SunSpace in Stellenbosch are still working to restore SO67.\\"\r\n\r\n\\"SumbandilaSat developed a problem with the Power Distribution Unit, similar to what happened some time back. The other sub-systems are in a healthy state and SO67 is in no immediate danger.\\"\r\n\r\nend quote\r\n\r\nSpacecraft is only available for amateurs on schedule.Check http://www.amsatsa.org.za/ for schedules and http://sumbandilamission.blogspot.com/ for commissioning updates. |
  262. | 72 | 0 | 0 | 0 | 4 | 0 | 4 | 4 | 0 | 0 | 0 | 4 | 0 | 1198771220 | Future Launch | <blank> | <blank> | <blank> |
  263. | 73 | 0 | 0 | 0 | 0 | 5 | 3 | 5 | 0 | 0 | 0 | 0 | 0 | 1342020805 | Non-Operational | <blank> | <blank> | <blank> |
  264. | 74 | 0 | 0 | 0 | 0 | 0 | 4 | 4 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Future Launch | <blank> | <blank> | <blank> |
  265. | 75 | 4 | 0 | 0 | 4 | 4 | 4 | 4 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Future Launch | <blank> | <blank> | <blank> |
  266. | 76 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | 1175871841 | Operational | <blank> | <blank> | <blank> |
  267. | 77 | 0 | 3 | 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | 0 | 0 | 1144610845 | Non-Operational | <blank> | <blank> | <blank> |
  268. | 78 | 4 | 0 | 0 | 0 | 4 | 4 | 4 | 0 | 0 | 0 | 0 | 0 | 1251742777 | Future Launch | <blank> | <blank> | <blank> |
  269. | 79 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1154112724 | Non-Operational | <blank> | <blank> | K7RR-Sat was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. |
  270. | 80 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1154112731 | Non-Operational | <blank> | <blank> | CP2 was launched aboard a DNEPR-1 on 26 July 2006. According to mission control officials, the engines of the Dnepr rocket shut down 86 seconds into its flight. The rocket crashed some 25km (15 miles) away, without causing injuries on the ground, but all satellites on board were destroyed. |
  271. | 81 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1154112714 | Non-Operational | <blank> | <blank> | <blank> |
  272. | 82 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1154112759 | Non-Operational | <blank> | <blank> | <blank> |
  273. | 83 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1154112791 | Non-Operational | <blank> | <blank> | <blank> |
  274. | 84 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 3 | 0 | 1154112818 | Non-Operational | <blank> | <blank> | <blank> |
  275. +-------+---+---+---+---+---+---+---+---+-----+------+--------+--------+------------+-----------------+---------------------+----------------------------+-----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------+
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