A satellite of mass \(m\) initially moves in a stable circular orbit of radius \(R\) around a planet of mass \(M\), where \(M \gg m\). The satellite's thrusters are fired to perform an orbital transition maneuver that places the satellite into a larger circular orbit of radius \(2R\). Which row in the table correctly indicates the change in kinetic energy \(\Delta K\), the change in gravitational potential energy \(\Delta U\), and the work \(W_{\text{thrust}}\) done on the satellite by the thrusters during the transition from the initial orbit to the final orbit?