What are the values of orbital speed and time period of revolution of an artificial satellite revolving very close to the earth's surface ?

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

What is the value of the time period of revolution of a geostationary satellite ?

If T is the period of revolution of an artificial satellite orbiting very close to the earth's surface and rho is the density of the earth, then show that rho T^2 is a universal constant.

The ratio of the magnitudes of the kinetic energy and the potential energy of an artificial satellite revolving around the earth is

A person inside an artificial satellite revolving around the earth feels weightless- true or false ?

The radius of the earth = R. if a geostationary satellite is revolving along a circular path at an altitude of 6R above the surface of the earth, what will be the time period of revolution of another satellite revolving around the earth at an altitude of 2.5R ?

If the orbital speed of an artificial satellite revolving very close to the earth is v and the escape velocity from the surface of the earth is v_e then v_e =……….. X v .[Fill in the blanks]

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.

Find out the expression for the speed of an artificial satellite revolving around the earth in a circular path.

Is Archimedes' principle applicable inside an artificial satellite revolving around the earth?