A satellite of mass \(m\) travels in an elliptical orbit around Earth, which is located at one focus of the ellipse.

Point \(P\) is at periapsis (closest approach to Earth).
Point \(M\) is at one endpoint of the minor axis.
Point \(A\) is at apoapsis (farthest distance from Earth).

Which of the following correctly ranks the magnitude of the rate of change of the satellite's kinetic energy, \(\left|\dfrac{dK}{dt}\right|\), at points \(P\), \(M\), and \(A\)?