A satellite is to revolve roudn the earth in as circle of radius 8000 km. With what speed should this stelite be projefted into orbit? What will be the time period?
Take g t the surface `=9.8ms^-2` and radius of the earth =6400 km.

A satellite is to revolve round the earth in as circle of radius 8000 km. With what speed should this satellite be projected into orbit? What will be the time period? Take g at the surface =9.8ms^-2 and radius of the earth =6400 km.

A satellite is to revolve round the earth in as circle of radius 8000 km. With what speed should this satellite be projected into orbit? What will be the time period? Take g at the surface =9.8ms^-2 and radius of the earth =6400 km.

A satellite is to revolve around the Earth in a circle of radius 8000 km. The speed at which this satellite be projected into an orbit, will be:

An artificial satellite revolves around the earth in a circular orbit and is at a height of 300 km above the surface of the earth. Find the orbital speed and the time period of the satellite. The radius of the earth=6400 km, g=980 cm*s^(-2) .

A satellite is revolving round the earth at a height of 600 km. find a. the speed f the satelite and b. the time period of thesatellit. Radius of the earth =6400 km and mass of the earth =6xx10^24kg .

A Geo-stationary satellite bits around the earth in a circular of radius 36, 000 km then what will be the time period of a spy satellite orbiting a few hundred km above the earth's surface (R_("earth") = 6400 km)

A geostationary satellite orbites around the earth in a circular orbit of radius 36000 km Then, the time period of a spy satellite orbiting a few hundred km above the earths surface (R_(e)=6400km) will approximately be

A geo-stationary satellite orbits around the earth in a circular orbit of radius 36000 km. Then, the time period of a spy satellite orbiting a few hundred kilometers above the earth's surface (R_("Earth") = 6400 " km") will approximately be