The orbit of a heat capacity mapping satellite 385 miles above the surface of Earth

Chapter 12, Problem 71

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Orbital Speed In Exercises 69-72, use the result of Exercise 68 to find the speed necessary for the given circular orbit around Earth. Let \(G M=9.56 \times 10^{4}\) cubic miles per second per second, and assume the radius of Earth is 4000 miles.

The orbit of a heat capacity mapping satellite 385 miles above the surface of Earth

Text Transcription:

GM=9.56 times 10^4

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