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A satellite of mass M revolving in a cir...

A satellite of mass M revolving in a circular orbit of radius `r_(s)` around the earth of mass M has a total energy E. then, its angular momentum will be

A

`(2E m_(S)r_(S))^(1/2)`

B

`(2E m_(S)r_(S))`

C

`(2E m_(S)r_(S)^(2))^(1/2)`

D

`(2E m_(S)r_(S)^(2))`

Text Solution

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The correct Answer is:
C
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