An earth satellite moves in a circular orbit at a speed of 5,800 m/s. What is its orbital period in minutes?
orbital distance
v^2 = GM / R
5800^2 = 6.67* 10^-11* 5.98* 10^24 / R
R = 1.1857* 10^7 m
now
T = 2 pi R / v
T = 213.97 mins
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