The maximum possible velocity of a satellite orbiting round the earth in a stable orbit is

Obtain the relation between escape velocity and critical velocity when satellite is orbiting very close to earth. OR Show//prove that the escape velocity of a satellite orbiting round the earth is equal to sqrt2 time its critical velocity. OR Show that V_e = sqrt2. V_c for a satellite orbiting round the earth.

A satellite is revolving round the earth in an elliptical orbit :

A satellite is revolving round the earth in circular orbit

A satellite is revolving round the earth in circular orbit

A satellite is revolving round the earth in circular orbit

The binding energy of a system of earth and its satellite orbiting round the earth in a circular orbit is E. If m of that satellite, its linear speed in that orbit is

A satellite is revolving round the earth in an elliptical orbit. Its speed will be

The orbital velocity of a satellite close to the earth is v. Then the orbital velocity at a height (1//4)^("th") of earth's radius is

What is the orbital velocity of an artifical satellite revolving round the earth at a height 100 km?

The energy of a satellite revolving round the earth in a circular orbit is increased but keeping its energy less than zero, then the average radius of the new orbit of the satellite will