Compute orbital period (T) from semi-major axis (a) or vice versa, according to Kepler's harmonic law. Includes central body mass scaling, interactive orbit visualization, and real solar system presets.
Johannes Kepler (1571–1630) discovered his third law of planetary motion in 1619, stating that the square of the orbital period of a planet is directly proportional to the cube of the semi-major axis of its orbit. Mathematically, T² ∝ a³. This law unified the solar system's architecture and later became fundamental to Newton's law of universal gravitation.
Kepler's Third Law (exact form)
$$ T^2 = \frac{4\pi^2}{G (M + m)} \cdot a^3 \approx \frac{4\pi^2}{G M} \cdot a^3 $$ (when M ≫ m)
For our solar system in convenient units: T (years) = √( a³ / M_☉ ) with a in AU and M_☉ = central mass (solar masses).
Newton generalized Kepler’s law by incorporating gravitational physics. For a small body orbiting a much larger mass M, the centripetal force equals gravitational force: GMm / r² = m v² / r. Substituting v = 2πa / T and simplifying gives T² = (4π² / GM) a³. The constant 4π²/GM is the same for all satellites around the same primary. Our calculator uses the exact relation: T (years) = √[ a³ / (M_rel) ], where M_rel = M / M_☉, a is in AU, T in Earth years. This works because for Earth (a=1, M=1, T=1) the identity holds. For different masses, the period scales as 1/√(M_rel).
The table below shows how Kepler's third law governs the orbital harmony of our solar system:
| Planet | Semi-major axis (AU) | Orbital Period (years) | T² / a³ |
|---|---|---|---|
| Mercury | 0.387 | 0.241 | 1.000 |
| Venus | 0.723 | 0.615 | 1.000 |
| Earth | 1.000 | 1.000 | 1.000 |
| Mars | 1.524 | 1.881 | 0.999 |
| Jupiter | 5.203 | 11.862 | 0.999 |
| Saturn | 9.537 | 29.457 | 1.000 |
A geostationary satellite orbits Earth once per day (T = 1 sidereal day ≈ 0.9973 days). Using Kepler's law with Earth mass (M = 3.986×10¹⁴ m³/s²) and converting units yields a semi-major axis of approximately 42,164 km from Earth’s center. Our calculator can be adapted (by setting central mass to Earth relative to Sun? We provide methodology). For Earth satellites, use the general formula with appropriate constants. This demonstrates how orbital mechanics governs telecommunications and GPS networks.