If the speed of a satellite orbiting near the surface of the earth is changed from `v_(c)` to `sqrt(1.5)v_(c)`. What is likely to happen?

The orbit period for an earth satellite near the surface of earth is

What is the orbiting speed of an artificial satellite close to the surface of the Earth .

The orbital speed for an earth satellite near the surface of the earth is 7km//sec . If the radius of the orbit is 4 times the radius of the earth, the orbital speed would be

A satellite is revolving near the earth's surface, Its orbit velocity is

The orbital speed for an earth satellite near the surface of the earth 7km-s^-1 ,. If the radius of the orbit is 4 times the radius of the earth is the orbital speed would be

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?

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?