1. two simultaneous equations, substitute the 2nd into the first.
2. Force balance to get your equations...
Fnet = Fgrav, Keplar's 3rd law...
After deriving, you will get something like:
T²/R³ = (4 * pi²)/(G * Mearth) Assuming circular orbit.
R = Rmoon, Rsat = X * Rmoon where X = some fraction of the radius of Rmoon which is given in your problem statement.
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