An artificial satellite moving in a circular orbit around the earth has a total (kinetic + potential) energy E0. Its potential energy is

(a) –E

(b) 15E

(c) 2E0 

(d) E0

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1 Answers

Correct Option (c) 2E0 

Explanation :

For a satellite, we have

Kinetic energy = GmM/2r

Potential energy = -GmM/r

Total energy E0 = KE + PE

= GmMr/2r - GmM/r = GmM/2r = PE/2

or PE = 2E0

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