A satellite is projected with a velocity `sqrt(1.5)` times the orbital velocity just above the surface of earth. Initial velocity of the satellite is perpendicular to the surface of earth. The maximum distance of the satellite from surface of earth will be -

What is the orbital velocity for a satellite orbiting close to the surface of earth?

A satellite is put in an orbit just above the earth's atmosphere with a velocity sqrt(1.5) times the velocity for a circular orbit at the that height. The initial velocity imparted is horizontal. What would be the maximum distance of the satellite from the earth, when it is in the orbit.

The orbit period for an earth satellite near the surface of earth is

The orbit velocity of a satellite at a height R above the surface of Earth is v . The escape velocity from the location is

What is the time period of satellite near the earth's surface? (neglect height of the orbit of satellite from the surface of the earth)?