$A$ satellite of mass $m$ is orbiting the Earth (of radius $R$) at a height equal to the radius of the Earth. The total energy of the satellite in terms of $g$ (acceleration due to gravity on Earth's surface) is

  • A
    $-\frac{mgR}{3}$
  • B
    $-\frac{mgR}{4}$
  • C
    $-\frac{mgR}{2}$
  • D
    $-\frac{mgR}{5}$

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