The correct formula for the height $h$ of a satellite from the Earth's surface is:

  • A
    $\left(\frac{T^2 R^2 g}{4 \pi^2}\right)^{1 / 3}-R$
  • B
    $\left(\frac{T^2 R^2 g}{4 \pi^2}\right)^{1 / 2}-R$
  • C
    $\left(\frac{T^2 R^2}{4 \pi^2 g}\right)^{1 / 3}-R$
  • D
    $\left(\frac{T^2 R^2}{4 \pi^2}\right)^{-1 / 3}+R$

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