The orbital velocity of an satellite in a circular orbit just above the earth's surface is `v`. For a satellite orbiting at an altitude of half of the earth's radius, the orbital velocity is

The orbital velocity of an artifical satellite in a circular orbit just above the earth's surface is V_(0) . For a satellite orbiting at an altitude of half of earth's radius, the orbital velocity is

The orbital velocity of an artifical satellite in a cirular orbit above the earth's surface at a distance equal to radiu of earth is v. For a satellite orbiting at an altitude half of earth's radius, orbital velocity is

The orbital velocity of a satellite very near to the surface of earth is v. What will be its orbital velocity at an altitude 7 times the radius of the earth?

If a satellite orbits as close to the earth's surface as possible,

if a satellite orbits as close to the earth's surface as possible.

The orbit velocity of a satellite at a height R above the surface of Earth is v . The escape velocity from the location is