Orbital Period Calculator

Calculate orbital period using Kepler's Third Law.

Period (seconds)
Period (days)
Period (years)

Kepler's Third Law

Kepler's Third Law states that the square of a planet's orbital period is proportional to the cube of its semi-major axis: T^2 ? a^3. More precisely, T = 2pisqrt(a^3/GM), where T is period, a is semi-major axis, G is gravitational constant, and M is central body mass. For planets orbiting the Sun, if a is in AU and T in years, then T^2 = a^3 (when M = 1 M?). Earth orbits at 1 AU with 1-year period. Mars at 1.52 AU has T = sqrt(1.52^3) = 1.88 years.

Understanding Orbital Mechanics

Orbital period depends on distance and central mass. Objects farther from the center orbit more slowly. More massive central bodies cause faster orbits at the same distance. The Moon orbits Earth in 27.3 days. The International Space Station orbits every 90 minutes due to proximity. Geostationary satellites orbit at 35,786 km, matching Earth's rotation period (24 hours). Understanding orbital periods is essential for satellite deployment, space mission planning, and studying planetary systems.

Applications in Space Science

Kepler's laws are fundamental to astronomy and astronautics. Astronomers discover exoplanets by observing periodic brightness dips (transits) or star wobbles with periods revealing orbital distances. Mission planners use orbital mechanics to design trajectories and timing for spacecraft. Satellite operators maintain specific orbits for communication, navigation, and observation. Understanding periods helps predict planetary positions, plan spacecraft flybys, and study binary star systems. GPS satellites use precise orbital mechanics combining Kepler's laws with relativity corrections.

Quick Tips

  • Always verify units are consistent
  • Use scientific notation for very large/small numbers
  • Results are approximations — real conditions may vary

Frequently Asked Questions

The semi-major axis is half the longest diameter of an elliptical orbit. For circular orbits, it's the radius. For Earth's nearly circular orbit, semi-major axis is about 1 AU (150 million km). It's the average orbital distance.

Kepler's laws are approximations assuming one planet orbiting a much more massive star. They work well for planets but need corrections for: binary stars, planetary perturbations, relativistic effects near massive objects, and non-point masses.

One AU is Earth's average distance from the Sun: 149,597,870.7 km (about 150 million km or 93 million miles). It's a convenient unit for Solar System distances. Jupiter is 5.2 AU, Neptune 30 AU.

Mercury: 88 days, Venus: 225 days, Mars: 687 days, Jupiter: 11.9 years, Saturn: 29.5 years, Uranus: 84 years, Neptune: 165 years. Period increases with distance as T^2 = a^3.

Geostationary satellites orbit above the equator at 35,786 km altitude with 24-hour period, matching Earth's rotation. They appear stationary in the sky, ideal for communication and weather satellites covering specific regions.