The satellite of mass $m$ revolving in a circular orbit of radius $r$ around the earth has kinetic energy $E$. Then its angular momentum will be

  • A

    $\sqrt {\frac{E}{{m{r^2}}}} $

  • B

    ${\frac{E}{{2m{r^2}}}}$

  • C

    $\sqrt {2Em{r^2}} $

  • D

    $\sqrt {2Emr} $

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