In terms of launch, initial orbit correction, stationkeeping, deorbiting, etc. for a typical 100-200 kg LEO satellite?
Is there any source online with specifications for non-private Earth-orbiting satellites?
In terms of launch, initial orbit correction, stationkeeping, deorbiting, etc. for a typical 100-200 kg LEO satellite?
Is there any source online with specifications for non-private Earth-orbiting satellites?