What is the relationship between the orbiting period of a satellite and its distance from the earth ?
If T is Orbital period of a satellite & r is the distance between satellite and the earth is given by T = (4 pi^2 r^3/ GM) whole on right hand side is under square root here, M is mass of earth, G is universal gravitational constant which is equal to 6.67*10^-11 Nm^2 kg^-2. And pi =3.14. You can also T= 2pi(r^3/GM) bracket content is under square root. Hope it Helps u Gudia.
