How many times is escape velocity `(V_(e))` , of orbital velocity `(V_(0))` for a satellite revolving near earth

How many times is escape velocity (v_e) or orbital velocity (v_0) for a satellite revolving near earth?

What is the ratio of the escape velocity to the orbital velocity for a satellite revolving near the earth's surface?

If upsilon_e denotes escape velocity and V_0 denotes orbital velocity of a satellite revolving around a planet of radius R, then

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

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

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

The relation between the escape velocity v_e and orbital velocity v_0 is given by