A planet moving along an elliptical orbit is closest to the sun at a distance $r_1$ and farthest away at a distance of $r_2$. If $v_1$ and $v_2$ are the linear velocities at these points respectively, then the ratio $\frac{v_1}{v_2}$ is

  • [AIPMT 2011]
  • A

    $\frac{r_2}{r_1}$

  • B

    $\left(\frac{r_2}{r_1}\right)^2$

  • C

    $\frac{r_1}{r_2}$

  • D

    $\left(\frac{r_1}{r_2}\right)^2$

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