A setellite os revolving very close to ...

A setellite os revolving very close to a planet of density p. The period of revolution of satellite is

A

`sqrt((3pirho)/G)`

B

`sqrt((3pi)/(2rhoG))`

C

`sqrt((3pi)/(Grho))`

D

`sqrt((3piG)/rho)`

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The correct Answer is:

C

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