MCQ
The mean radius of the earth is $R$, its angular speed on its own axis is $\omega $ and the acceleration due to gravity at earth's surface is $g$. The cube of the radius of the orbit of a geostationary satellite will be
- A${R^2}g/\omega $
- B${R^2}{\omega ^2}/g$
- C$Rg/{\omega ^2}$
- ✓${R^2}g/{\omega ^2}$