$A$ satellite is revolving very close to a planet of density $\rho$. The period of revolution of the satellite is

  • A
    $\sqrt{\frac{3 \pi \rho}{G}}$
  • B
    $\sqrt{\frac{3 \pi}{2 \rho G}}$
  • C
    $\sqrt{\frac{3 \pi}{\rho G}}$
  • D
    $\sqrt{\frac{3 \pi G}{\rho}}$

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