A satellite of mass “m” orbits a planet “P” in an elliptical orbit. The satellite is then transferred to another circular orbit of radius “r” as shown in the figure. Which of the following hold true in this scenario?
The kinetic energy of a satellite is;
KE = (1/2) x (G x m x M)/r
The potential energy of a satellite is;
PE = – (G x m x M)/r
Due to an increase in “r” the kinetic energy is decreased. The potential energy increases for the same reason as well due to the presence of a negative sign.