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If r represents the radius of the orbit of a satellite of mass m moving around a planet of mass M , the velocity of the satellite is given byA. `v^(2)="g" (M)/(R)`B. `v^(2)=(GMm)/(R)`C. `v=(GM)/(r)`D. `v^(2)=(GM)/(r)` |
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Answer» Correct Answer - D |
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