Low-earth orbit the satellites elevation above the earths

Consider a satellite in circular, low-Earth orbit: the satellite's elevation above the Earth's surface if h<

A) Show the orbital period (P) for such a satellite is approximately:

\(P=C(1+\frac{3h}{2R})\)

where C is some constant.

B) What is the numerical constant C?

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Low-earth orbit the satellites elevation above the earths : consider a satellite in circular low-earth orbit the satellites elevation above the earths surface if hlta show the

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