The mean radius of earth is R, its angular speed on its own axis is `omega` and the acceleration due to gravity at earth's surface is g. What will be the radius of the orbit of a geostationary satellite ?

Options

A. `(R^(2)g//omega^(2))^(1//3)`
B. `(Rg//omega^(2))^(1//3)`
C. `(R^(2)omega^(2)//g)^(1//3)`
D. `(R^(2)g//omega)^(1//3)`

Answer

A