The mean radius of earth is R, its angular speed on its own axis is w 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