Kepler's Third Law
Statement
For a bound orbit (ellipse) of semi-major axis around a total mass , the orbital period satisfies .
Why is it true?
This links the size of an orbit directly to how long it takes to complete, with no dependence on eccentricity — a fact used every time astronomers weigh a star or planet by timing a smaller body's orbit around it.
Proof sketch
By Theorem 1, the areal sweep rate is constant, so integrating over one full period gives the total enclosed area . For an ellipse with semi-major axis and semi-minor axis , geometry gives . Equating the two: .
Next, tie to the shape via Binet's equation: the semi-latus rectum of the orbit is , and for an ellipse the standard relations and hold. Combining with gives , so .
Substitute this expression for into and solve for : . Squaring both sides gives , which is Kepler's third law — and it holds for every ellipse regardless of , since canceled out completely.
Topics that use this theorem
Step-by-step proofs
No step-by-step proof yet for this theorem.
References
- Carl D. Murray, Stanley F. Dermott (1999). Solar System Dynamics
- Alain Chenciner, Richard Montgomery (2000). A remarkable periodic solution of the three-body problem in the case of equal masses
- NASA Science (2024). Webb's Orbit at Sun-Earth Lagrange Point 2 (L2)
- NASA Science (2024). Basics of Spaceflight: A Gravity Assist Primer