A satellite of mass m is orbiting the earth (of radius R) at a height h from its surface. The total energy of the satellite in terms of g₀, the value of acceleration due to gravity at the earth's surface, is
(1) (mg₀R²)/2(R + h)
(2) - (mg₀R²)/2(R + h)
(3) (2mg₀R²)/(R + h)
(4) - (2mg₀R²)/(R + h)
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option (2) is correct answer of your question.
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