The orbital speed of a satellite revolving around planet in a circular orbit is v0. if its speed is increased by 10%, then
Centripetal force = gravitational force
mv02r=GmMr2
From the above relations, we can conclude that:
The centripetal force balancing the gravitational force on the satellite is directly proportional to the velocity and inversely proportional to the radius of the orbit.
Thus;
i. If the velocity increases, the centripetal force will also increase and to counter that, the radius of the orbit should decrease.
ii. If we keep the radius unaltered in the equation, the centripetal force will increase more than the gravitational force and the satellite will escape.