The time period of the earth's satellite revolving at a height of 35800 km is

The time period of a geostationary satellite at a height 36000 km is 24 h a spy satellite orbits vergy close to earth surface (R=6400 km ) what will be its time period ?

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

A geostationary satellite is orbiting the earth at height 11R above surface of the earth. R being radius of earth. If the time period of this satellite is 24hr find out time period of another satellite which is revolving at 2R from surface of earth

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

Radius of a geostationary satellite revolving round the earth is 'r'. Then period of revolution of another satellite revolving in an orbit of radius r/2 is

A geostationary satellite orbits around the earth in a circular orbit of radius 36,000 km. then the time period of a spy satellite orbiting a few hundred km (600 km) above the earth's surface (R=6400 km) will approximately be

A geostationary satellite orbits around the earth in a circular orbit of radius 36,000 km. then the time period of a spy satellite orbiting a frw hundred km (600 km) above the earth's surface (R=6400 km) will approximately be

Calculate the time taken by a satellite for one revolution revolution revolving at a height of 6400 km above the earth's surface with velocity 5.6 km/s .

Calculate the time taken by a satellite for one revolution revolution revolving at a height of 6400 km above the earth's surface with velocity 5.6 km/s .