mv2/R = GMem/R2 Rearranging
v = sqrt(GMe/R) where G is 6.67 x 10-11 Nm2/kg2, and R = 3.89*(6.37x106 m)
Jake M.
asked 05/08/22Find the speed of a satellite in a circular orbit around the Earth with a radius 3.89 times the mean radius of the Earth; RE= 6.37·103 km ME= 5.98·1024 kg
mv2/R = GMem/R2 Rearranging
v = sqrt(GMe/R) where G is 6.67 x 10-11 Nm2/kg2, and R = 3.89*(6.37x106 m)
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