[" If "L" is the angular momentum of a satellite revolving "],[" around earth is a circular orbit of radius "r" with "],[" speed "v" ,then "]

When a satellite going around the earth in a circular orbit of radius r and speed v loses some of its energy, then

Angular momentum of a satellite revolving round the earth in a circular orbit at a height R above the surface is L . Here R is radius of the earth. The magnitude of angular momentum of another satellite of the same mass revolving very close to the surface of the earth is

The orbital speed of a satellite revolving around a planet in a circular orbit is v_(0) . If its speed is increased by 10 % ,then

The orbital speed of a satellite revolving around a planet in a circular orbit is v_(0) . If its speed is increased by 10 % ,then

A satellite is moving around the earth with speed v in a circular orbit of radius r. IF the orbit radius is decreased by 1%, its speed will

An artificial satellite is revolving around the earth in a circular orbit of radius r. If the time period of revolution of the satellite is T, show that T^2 prop r^3 .