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If an artificial satellite is moving in a circular orbit around earth with speed equal to one fourth of `V_(e)` from earth, then height of the satellite above the surface of the earth isA. `7R`B. `4R`C. `3R`D. `R` |
Answer» Correct Answer - A `v_(0)=(v_(e))/4, V_(0)=(sqrt((GM)/(R+h)))` |
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