The minimum amount of energy required for a satellite to escape from earth's gravitational influence is called as Binding Energy of a satellite. r is a radius of orbit i.e. Radius of earth + height at which satellite is orbiting the earth
Let the mass of satellite is m and r is the radius of the circular orbit. the satellite moves in the circumference of circular orbit around the earth.
now, at equilibrium condition,
centripetal force = gravitational force
mV2/r = GMm/ r2
mV2 = GMm/ r
½ mV2 = GMm/ 2r
KE = GMm/ 2r
now, potential energy between satellite and the earth is given by
PE = - GMm/ r
[ here negative sign indicates force acts between satellite and earth is attractive]
TE = KE+PE
TE = GMm/ 2r + - GMm/ r
TE = - GMm/2r
Er = - GMm/ r
here negative sign indicates that the satellite is bound to the earth by attractive force and cannot leave it on its own. To move the satellite to infinity, so, the binding energy of a satellite revolving in a circular orbit around the earth is