A) \[2E\]
B) \[-2E\]
C) \[E\]
D) \[-E\]
Correct Answer: A
Solution :
Potential energy of satellite \[U=-\frac{GMm}{r}\] and total energy of satellite \[E=-\frac{GMm}{2r}\] Therefore, \[U=2\,E\]You need to login to perform this action.
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