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?
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Sign up to join this communityIn 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?