If the period of revolution of an artificial satellite just above the earth's surface is T and the density of earth is p, then `pT^(2)` is

If the period of revolution of an artificial satellite above the earth's surface be T and the density of earth be p, then prove that p T^(2) is a universal constant. Also calculate the value of this constant. Given G= 6.67xx10^(-11)m^(3) kg^(-1)s^(-2)

If the period of revolution of an artificial satellite just above the earth be T second and the density of earth be rho , kg//m^(3) then (G = 6.67 xx 10^(-11) m^(3)//kg . "second"^(2) )

If T is the period of revolution of an artificial satellite orbiting very close to the earth's surface and rho is the density of the earth, then show that rho T^2 is a universal constant.

The period of geostationary artificial satellite of the earth is

Calculate the period of revolution of a polar satellite orbiting close to the surface of the Earth.

Artificial satellite moving around the earth is just like a

what is the time period of revolution of a geostationary Satellite of earth?