Correct formula for height of a satellite from earths surface is:
\( \left( \dfrac{T^2 R^2 g}{4 \pi} \right)^{1/2} - R \)
\( \left( \dfrac{T^2R^2 g}{4 \pi^2} \right)^{1/3} - R \)
\( \left( \dfrac{T^2 R^2 g}{4 \pi^2} \right)^{-1/3} + R \)
\( \left( \dfrac{R^2T^2 }{4 \pi^2g} \right)^{1/3} - R \)