A satellite is revolving in a circular orbit at a height $$‘h'$$ from the earth's surface (radius of earth $$R;h < < R$$ ). 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.)
If $$g$$ is the acceleration due to gravity on the earth’s surface, the gain in the potential energy of an object of mass $$m$$ raised from the surface of the earth to a height equal to the radius $$R$$ of the earth, is-
A geo-stationary satellite orbits around the earth in a circular orbit of radius $$36,000 \,km.$$ Then, the time period of a spy satellite orbiting a few hundred km above the earth's surface $$\left( {{R_{earth}} = 6400\,km} \right)$$ will approximately be-