Assuming the radius of the earth to be `6.5 xx 10^(6)` m. What is the time period T and speed of satellite for equatorial orbit at `1.4 xx 10^(3)` km above the surface of the earth.

Assuming the radius of the earth to be 6.4xx10^(6) m calculate the time period T of a satellite for equatorial orbit at 1.4xx10^(3) km above the surface of the earth and the speed of the satellite in this orbit ?

Assume the radius of the earth to be 6.4xx10^(6)m a. Calculate the time period T of a satellite on equational orbit at 1.4xx10^(e)m above the surface of the earth. b. What is the speed of the satellite in this orbit? c. If the satellite is travelling in the same direction as the rotation of the earth i.e. west to east, what is the interval between two successie times at which it will appear vertically overhead to an observed at a fixed point on the equator?

Assume the radius of the earth to be 6.4xx10^(6)m a. Calculate the time period T of a satellite on equational orbit at 1.4xx10^(e)m above the surface of the earth. b. What is the speed of the satellite in this orbit? c. If the satellite is travelling in the same direction as the rotation of the earth i.e. west to east, what is the interval between two successie times at which it will appear vertically overhead to an observed at a fixed point on the equator?

A geostationary satellite is orbiting the earth at a height of 6R above the surface of the earth, where R is the radius of the earth. The time period of another satellite at a height of 2.5 R from the surface of the earth is …… hours.

A geostationary satellite is orbiting the earth at a height of 6R above the surface of the earth, where R is the radius of the earth. The time period of another satellite at a height of 2.5 R from the surface of the earth is …… hours.

A geostationary satellite is orbiting the earth at a height of 6R above the surface of the earth, where R is the radius of the earth. The time period of another satellite at a height of 2.5 R from the surface of the earth is …… hours.

A geostationary satellite is orbiting the earth at a height of 6R above the surface of the earth, where R is the radius of the earth. The time period of another satellite at a height of 2.5 R from the surface of the earth is …… hours.

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)