$A$ satellite is orbiting the Earth with an orbital velocity $v_0$. If it is suddenly stopped and allowed to fall onto the Earth,what will be its velocity when it hits the Earth's surface? (Let $v_e$ be the escape velocity from the Earth's surface.)

  • A
    $\frac{v_e^2}{v_0}$
  • B
    $v_0$
  • C
    $\sqrt{v_e^2 - v_0^2}$
  • D
    $\sqrt{v_e^2 - 2v_0^2}$

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