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For a satellite moving in a circular orbit around the earth, the ratio of its potential energy to kinetic energy isA. `1`B. `-1`C. `2`D. `-2` |
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Answer» Correct Answer - D Kinetic energy of the satellite, `K=(GM_(E)m)/(2r)` Potential energy of the satellite, `U=-(GM_(E)m)/r` Their corresponding ratio is `U/K=-2` |
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