Which has longer period of revolution, a satellite revolving close or away from the surface of earth?

Obtain an equation for the period of revolution of an artifical satellite revolving at height .h. from the surface of Earth.

What is the relation between the period of revolution of a satellite (revolving close to the earth surface) and the density of the earth?

Calculate the period of revolution of a polar satellite orbiting close to the surface of the Earth.

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 periodic times of a satellite revolving very close to the surface of the earth, of density rho ?

Find the period of revolution of a satellite revolving the earth at a height of 200km above earth's surface ? Radius of earth = 6400 km

The period of revolution of a satellite orbiting Earth at a height 4R above the surface of Warth is x hrs, where R is the radius of earth. The period of another satellite at a height 1.5R from the surface of the Earth is

The period of revolution of a satellite orbiting Earth at a height 4R above the surface of Warth is x hrs, where R is the radius of earth. The period of another satellite at a height 1.5R from the surface of the Earth is

Assertion : The time period of a satellite revolving very close to the surface of earth is less. Reason : According to Kepler's law, square of time period of revolution is directly proportional to the cube of semi-major axis.

If rho is the mean density of the earth and R is its radius, then the critical speed of a satellite revolving very close to the surface of earth is :