A planet of mass \(m\) moves in an elliptical orbit around the Sun of mass \(M\). Let \(r_{1}\) be the distance at aphelion and \(r_{2}\) be the distance at perihelion. If \(v_{1}\) and \(v_{2}\) are the velocities of the planet at these points, then ratio of kinetic energy at aphelion to kinetic energy at perihelion is