Orbital Period Calculator (Kepler's Third Law)
Calculate orbital period from semi-major axis using Kepler's third law.
Supports the Sun, Earth, Jupiter, or any custom central body.
Kepler’s Third Law, published by Johannes Kepler in 1619, states that the square of the orbital period is proportional to the cube of the semi-major axis. Isaac Newton later showed why: it follows directly from the inverse-square law of gravity.
For any central body:
T = 2π √(a³ / GM)
Simplified for the Solar System (a in AU, T in years):
T (years) = a (AU)^(3/2)
This works because it is normalized to Earth’s orbit (1 AU, 1 year, central mass = 1 M☉).
Parameters:
- a = semi-major axis (half the longest diameter of the elliptical orbit)
- G = 6.674 × 10⁻¹¹ N·m²/kg²
- M = mass of the central body
Solar system examples (using T = a^1.5):
- Mercury: a = 0.387 AU → T = 0.241 years (88 days)
- Venus: a = 0.723 AU → T = 0.615 years (225 days)
- Mars: a = 1.524 AU → T = 1.881 years (687 days)
- Jupiter: a = 5.203 AU → T = 11.86 years
- Saturn: a = 9.537 AU → T = 29.46 years
- Halley’s Comet: a = 17.8 AU → T = 75.3 years
Why does mass of the orbiting body not matter? The orbital period depends only on the mass of the central body and the semi-major axis. A satellite and the Space Shuttle orbit at the same speed if at the same altitude. (This assumes M_central » M_orbiting — valid for planets around stars and satellites around planets.)
Checking the formula against known orbits
The International Space Station orbits at about 408 km altitude (6,778 km from Earth’s center) and completes one orbit in 92.68 minutes; plug those into T = 2π√(a³/GM) and you get 92.6 minutes. The Moon at 384,400 km gives 27.3 days, the actual sidereal period. Geostationary orbit sits at exactly 35,786 km altitude (42,164 km from Earth’s center), yielding precisely 24 hours; this is why GPS, weather, and broadcast satellites sit there and appear fixed over one spot.
Elliptical orbits
For elliptical orbits, use the semi-major axis a (half the longest diameter of the ellipse) rather than a circular radius. The period depends only on the semi-major axis, not on the eccentricity. A nearly circular orbit and a wildly elongated comet orbit with the same semi-major axis have exactly the same period.
How we build and check this calculator
This calculator runs entirely in your browser, so the numbers you enter stay on your device. The math behind it is written by hand and tested against worked examples and standard references before the page goes live.
SuperGlobalCalculator is independently built and maintained. See how we build and verify our calculators.