Prove that in the case of an artificial satellite revolving around a spherical planet, its minimum time period of revolution depends only on the mean density of the planet.

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 .

The time period of revolution of an artificial satellite in an orbit just outside the equatorial plane depends only on the mean density of the earth. Is this statement true or false ?

What is the orbital period of revolution of an artificial satellite revolving in geostionary orbit?

The centripetal force necessary for an artificial satellite revolving along its orbit around the earth is delivered by

Two small artificial satellite are revolving around the earth in two circular orbits of radii r and (r+Deltar) . If their time periods of revolution are T and T+Delta T , then (Deltar lt lt r, DeltaT lt lt T)

An artificial satellite is revolving around the earth at an altitude h above the surface of the earth. Show that the orbital speed and the time period of revolution of the satellite is independent of its mass.

Show that the time period of revolution for any planet T^2propr^3 [r = radius of the circular path]

An artificial satellite takes 90 minutes to complete its revolution around the earth. The angular speed of the satellite is

The radii of the orbits of two satellite A and B revolving around a planet are 4R and R respectively . If the velocity of A is 3v, the velocity of B will be