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Question #74790
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Question
What is the value of the constant $ k $ in Kepler’s third law for Earth satellites?
A. $ \frac{GM_E}{4\pi^2} $
B. $ \frac{4\pi^2}{gR_E} $
C. $ \frac{g}{R_E} $
D. $ \frac{4\pi^2}{GM_E} $
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