If ` v_(0)` be the orbital velocity of a satellite in a circular orbit close to the earth's surface and `v_(e)` is the escape velocity from the earth , then relation between the two is

If v_(0) orbital velocity of a surface to a circular orbital close in the earth's surface and v_(1) scape velocity from earth then relation between the two is

The orbital velocity of a satellite in a circular orbit close to the earth is v_0 , If the escape velocity of an object projected from the earth be v_e , then the ratio of these two velocities is.

The orbital velocity f a satellite in a circular orbit close to the earth is v_0 . If the escape velocity of an object projected from the earth be v_e , then the ratio of these two velocities is

What is the orbital velocity for a satellite orbiting close to the surface of earth?

Find the orbital velocity of an artifical satellite of the earth in an orbital close to the earth?

If v_(e) is escape velocity and v_(0) , is orbital velocity of satellite for orbit close to the earth's surface. Then are related by