The time period of revolution of a satellite $(T)$ around the earth depends on the radius of the circular orbit $(R)$,mass of the earth $(M)$,and universal gravitational constant $(G)$. The expression for $T$,using dimensional analysis is ($K$ is a constant of proportionality):

  • A
    $K \sqrt{\frac{R^2}{GM}}$
  • B
    $K \sqrt{\frac{R}{GM}}$
  • C
    $K \sqrt{\frac{R^3}{GM}}$
  • D
    $K \sqrt{\frac{R^3}{GM^2}}$

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