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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1$\begingroup$ not an answer but there is some related information at Delta-V of Starlink Sattelites $\endgroup$ – uhoh Jun 5 '20 at 10:11
