The ratio of the energy required to raise a satellite upto a height h above the surface of earth to that the kinetic energy of the satellite into the orbit there is (R=radius of earth)

The ratio of energy required to raise a satellite to a height h above the earth surface to that required to put it into the orbit is

The ratio of energy required to raise a satellite to a height h above the earth surface to that required to put it into the orbit is

The ratio of energy required to raise a satellite to a height h above the earth surface to that required to put it into the orbit is

The kinetic energy of the satellite orbiting around the Earth is

A geostationary satellite is at a height h above the surface of earth. If earth radius is R -

Let E be the energy required to raise a satellite to height h above earth's surface and E' be the energy required to put the same satellite into orbit at that height. Then E//E' is equal to

Let E be the energy required to raise a satellite to height h above earth's surface and E' be the energy required to put the same satellite into orbit at that height. Then E//E' is equal to