The mean radius of earth is $R$, and its angular speed on its axis is $\omega$. What will be the radius of orbit of a geostationary satellite?
The mean radius of earth is $R$, and its angular speed on its axis is $\omega$. What will be the radius of orbit of a geostationary satellite?
- A
$\left(\frac{R g}{\omega^2}\right)^{1 / 3}$
- B
$\left(\frac{R^2 g}{\omega^2}\right)^{1 / 3}$
- C
$\left(\frac{R^2 g}{\omega}\right)^{1 / 3}$
- D
$\left(\frac{R^2 \omega^2}{g}\right)^{1 / 3}$
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