The correct answer is:
D. The average orbital radius of the orbiting object.
Kepler's Third Law states that the square of the period of orbit (T^2) of a planet is directly proportional to the cube of the semi-major axis of its orbit (r^3). In this context, "r" refers to the average distance from the central body (such as the Sun) to the orbiting object, which is often represented by the semi-major axis of the elliptical orbit.