Two satellites are revolving around the Earth with orbital velocities $v_1$ and $v_2$ at radii $r_1$ and $r_2$ respectively,where $r_1 > r_2$. Then:

  • A
    $v_1 = v_2$
  • B
    $v_1 > v_2$
  • C
    $v_1 < v_2$
  • D
    $\frac{v_1}{r_1} = \frac{v_2}{r_2}$

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