Posted by Nancy on Friday, February 15, 2008 at 3:27pm.
V^2/R = a = 1.11 m/s^2
For R, use the distance from the center of the Moon, 1.70*10^6 m + 4*10^5 m.
Solve for V
For the period P, solve
V*P = 2 pi R, the orbit circumference
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