20 Oct
2014
20 Oct
'14
2:06 p.m.
Hello, I was just wondering if the 4M mission's orbit could be simulated using g3ruh's Cowell integrator, provided that orbit injection state vectors were available...
I've found some videos (luxspace cloud) with this simulation and I was wondering if I could do the same...
Can anybody help ?
73s Fabio
iz5xrc