Kepler’s three laws of planetary motion:
Law of Ellipses
Law of Equal Area in Equal Time
Law of the Period , where T is the period (time to complete one full revolution) and a is the semimajor axis (Figure 7).
According to Newton’s Universal Law of Gravitation and Second Law of Motion, the position vector r(t) of a planet satisfies the differential equation
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Properties of J = r(t) × r′(t):
J is a constant of planetary motion.
Let J = ∥J∥. Then J = r(t)2θ′(t).
The planet sweeps out area at the rate .
A planetary orbit has polar equation , where e is the eccentricity of the orbit.