The rotation period of an earth satellite close to the surface of the earth is 83 minutes. The time period of another earth satellite in an orbit at a distance of three earth radii from its surface will be

The period of revolution of an earth's satellite close to the surface of the earth is 60 minute. The period of another the earth's satellite in an orbit at a distance of three times earth's radius from its surface will be (in minutes)

The period of revolution of an earth satellite close to surface of earth is 90min. The time period of aother satellite in an orbit at a distance of three times the radius of earth from its surface will be

For a stellite orbiting close to the surface of earth the period of revolution is 84 min . The time period of another satellite orbiting at a geight three times the radius of earth from its surface will be

The distance of two satellites from the surface of the earth R and 7R . There time periods of rotation are in the ratio

If T is the period of a satellite revolving very close to the surface of the earth and if rho is the density of the earth, then

The orbital speed of an artificial satellite very close to the surface of the earth is V_(o) . Then the orbital speed of another artificial satellite at a height equal to three times the radius of the earth is

Time period of a satellite to very close to earth s surface, around the earth is approximately

Time period of pendulum, on a satellite orbiting the earth, is

If height of a satellite from the surface of earth is increased , then its