plan equatorial inclination

add node(time:Seconds + 300, 0, 0, 0).
lock lat to body:geopositionof(positionat(ship, time:seconds + nextnode:eta)):lat.


set step to 0.1.

set last to abs(lat).
until abs(lat) > last {set last to abs(lat). set nextnode:eta to nextnode:eta + step. wait 0. print lat.}


set last to abs(lat).
set step to step /-2.
until abs(lat) > last {set last to abs(lat). set nextnode:eta to nextnode:eta + step. wait 0. print lat.}
set nextnode:eta to nextnode:eta - step.

set step to 1.
lock inc to abs(nextnode:obt:inclination).
set last to inc.
until inc > last
{
    set last to inc.
    set nextnode:normal to nextnode:normal + step.
    wait 0.
    print inc.
}

set step to step / -2.
set last to inc.
until inc > last
{
    set last to inc.
    set nextnode:normal to nextnode:normal + step.
    wait 0.
    print inc.
}
set nextnode:normal to nextnode:normal - step.
print nextnode:orbit:inclination.