A satellite orbiting above the equator of the earth is geosynchronous if the period is T = 24 hours (in this case, the satellite staysover a fixed point on the equator). Use Kepler’s Third Law to showthat in a circular geosynchronous orbit, the distance from the center ofthe earth is R ≈ 42,246 km. Then compute the altitude h of the orbitabove the earth’s surface. The earth has mass M ≈ 5.974 × 1024 kgand radius R ≈ 6371 km.

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ISBN:9781305952300
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Chapter1: Units, Trigonometry. And Vectors
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A satellite orbiting above the equator of the earth is geosynchronous if the period is T = 24 hours (in this case, the satellite stays
over a fixed point on the equator). Use Kepler’s Third Law to show
that in a circular geosynchronous orbit, the distance from the center of
the earth is R ≈ 42,246 km. Then compute the altitude h of the orbit
above the earth’s surface. The earth has mass M ≈ 5.974 × 1024 kg
and radius R ≈ 6371 km.

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