[" A satellite is revolving in a circular orbit at a height t' from the earth's surface (R is "],[" radius of the earth,h.

A satellite is revolving in a circular orbit at a height 'h' from the earth's surface (radius of earth R, h <

A satellite is revolving in a circular orbit at a height h from the earth's surface (radius of earth R,h lt lt R ). The minimum increase in its orbital velocity required so that the satellite could escape from the earth's gravitational field , is close to :(Neglect the effect of atmosphere)

A satellite is revolving in a circular orbit at a height 'h' from the earth's surface (radius of earth R, h ltlt R). The minimum increase in its orbital velocity required, So that the satellite could escape from the erth's gravitational field, is close to :(Neglect the effect of atomsphere.)

A satellite is revolving in a circular orbit at a height 'h' from the earth's surface (radius of earth R, h ltltR). The minimum increase in its orbital velocity required, So that the satellite could escape from the erth's gravitational field, is close to :(Neglect the effect of atomsphere.)

A satellite is revolving in a circular orbit at a height h from the earths surface (radius of earth R, h lt lt R ). The minimum increase in its orbital velocity required, so that the satellite could escape from the earths gravitational field, is close to :(Neglect the effect of atmosphere.)

A satellite is revolving in a circular orbit at a height 'h' from the earth's surface (radius of earth R). The minimum increase in its orbital velocity required, So that the satellite could escape from the earth's gravitational field, is close to :(Neglect the effect of atomsphere.)

An earth satellite of mass m revolves in a circular orbit at a height h from the surface of the earth. R is the radius of the earth and g is acceleration due to gravity at the surface of the earth. The velocity of the satellite in the orbit is given by