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A satellite is in a circular orbit 29000 km above the Earth’s surface; i.e., it moves on a circular path under the influence of nothing but the Earth’s gravity. Find the speed of the satellite. The radius of the Earth is 6.37 × 10 6 m, and the acceleration of gravity at the satellite’s altitude is 0.318952 m/s 2 .
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\[M*V^2/R=M*a \]\[R=r+h\]\[V=\sqrt{a(r+h)}=\sqrt{0.319*(2.9+6.37)*10^6}=1.72*10^3 m/s\]
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