MHT CET Physics question
The potential energy of a circularly orbiting satellite around the earth at height 'h' from the earth's surface, is given by P. E. = x(K. E.) where K. E. is the kinetic energy of this satellite. The value of 'x' is [MHT-CET 2021]
Answer: (C)
Solution
For a circular orbit and \frac{GMm}{r}$ =
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