[" A satellite is revolving in a circular orbit at "],[" a height h from the earth surface,such that "],[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 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, h <

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 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). 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.)

A satelite is revolving in a circular orbit at a height h above the surface of the earth of radius R. The speed of the satellite in its orbit is one-fourth the escape velocity from the surface of the earth. The relation between h and R is