Posted by Cora on Monday, May 2, 2011 at 7:56pm.
You need the orbit radius, and that is
R = 1.74*10^6 m + 0.111*10^6 m
= 1.85*10^6 m
Gravity pull = centripetal force
G*Mm*m/R^2 = m*V^2/R
Satellite mass m cancels out.
V = sqrt(G*Mm/R)
Period = 2 pi R/V
Substitute the previous equation for R.
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