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Question #74693
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Question
How is Kepler’s third law expressed for satellites orbiting Earth?
A. $ T = k(R_E + h)^2 $
B. $ T^3 = k(R_E + h)^2 $
C. $ T^2 = k(R_E + h)^3 $
D. $ T^2 = k(R_E + h)^2 $
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