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Orbital Period Calculator — Kepler's Third Law | T = 2π√(a³/GM) | Planets, Satellites & Binary Stars

Calculate the orbital period of any planet, moon, satellite, or binary star system using Kepler's Third Law T = 2π√(a³/GM). Supports metric (AU, km, m; solar masses, Earth masses, kg) and American (AU, miles, ft; lb) unit systems. Solar System presets included.

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What Is the Orbital Period? – Orbit Definition

When we talk about orbits, we are firmly in the realm of astronomy and celestial mechanics. An orbit is the curved path that one object follows as it moves around another under the influence of gravity. Earth's orbit around the Sun, the Moon's orbit around Earth, and even the International Space Station's path around our planet are all examples of orbits.

The orbital period is simply the time it takes a body to complete one full orbit around another object. For Earth, that is one year — roughly 365.25 days. For the ISS, it is only about 92 minutes. The orbital period depends on two things: the size of the orbit (the semi-major axis) and the mass of the central body (or, in a binary system, the combined mass of both objects).

Johannes Kepler's Laws of Planetary Motion – Elliptical Orbits

Johannes Kepler (1571–1630) was a German astronomer who derived three fundamental laws describing how planets move around the Sun. He based his work on decades of precise observational data collected by Tycho Brahe and applied mathematical analysis to find the underlying rules.

  • First Law: Planets move in ellipses with the Sun at one focus — not circles. This was a radical departure from the ancient view of perfect circular orbits.
  • Second Law (Equal Areas): A line joining a planet to the Sun sweeps out equal areas in equal times. This means planets move faster when they are closer to the Sun and slower when they are farther away.
  • Third Law (Harmonic Law): The square of the orbital period is proportional to the cube of the semi-major axis: T² ∝ a³. This is the law used by our Orbital Period Calculator.

Kepler's third law can be derived from Newton's law of universal gravitation and gives us the exact relationship:

T = 2π × √(a³ / (G × M))

where G = 6.674 × 10⁻¹¹ m³ kg⁻¹ s⁻² is the gravitational constant, a is the semi-major axis of the elliptical orbit in meters, and M is the mass of the central body in kilograms.

Types of Orbits: LEO, Geostationary, Binary Stars, and More

Low Earth Orbit (LEO)

Low Earth Orbit spans roughly 160–2,000 km above Earth's surface. The International Space Station orbits at about 420 km altitude, giving it a semi-major axis of approximately 6,791 km from Earth's center and an orbital period of ~92 minutes. Most Earth-observation satellites, the Hubble Space Telescope, and crewed spacecraft operate in LEO. With thousands of active satellites and debris objects, LEO is the most populated region of near-Earth space.

Geosynchronous and Geostationary Orbits (GEO)

A geosynchronous orbit has a period equal to Earth's rotation period (about 23 hours 56 minutes). A satellite in a circular geosynchronous orbit directly above the equator appears to hover over the same point on Earth — this is called a geostationary orbit, at an altitude of about 35,786 km. Most telecommunications and weather satellites occupy GEO.

Binary Star Systems

About half of all stars in the Milky Way are in binary (or multiple) star systems, where two stars orbit their common center of mass. For a binary system the orbital period formula uses the total mass of both stars:

T = 2π × √(a³ / (G × (M₁ + M₂)))

Here a is the distance between the two stars (the semi-major axis of the relative orbit), M₁ and M₂ are the individual stellar masses. Alpha Centauri AB, the closest star system to the Sun, is a well-known binary: its two Sun-like stars orbit each other over a period of about 79.9 years at a mean separation of 23.4 AU.

How to Use the Orbital Period Calculator

Our calculator handles both the single-body case (a planet, moon, or satellite orbiting one central mass) and the binary-star case. Here is how to get your result in seconds:

  1. Choose the calculation mode: "Single Body" for a planet/satellite around one central body, or "Binary Star System" for two bodies orbiting each other.
  2. Select your unit system: Metric (AU, km, m; solar masses, Earth masses, kg) or American Imperial (AU, miles, ft; solar masses, Earth masses, lb).
  3. Enter the semi-major axis of the orbit. This is half the longest diameter of the ellipse. For a circular orbit it equals the orbital radius.
  4. Enter the central body mass (single mode) or the masses of both bodies (binary mode).
  5. Click Calculate. The result is shown in seconds, minutes, hours, days, and years, alongside a comparison table with Solar System objects.

You can also choose a preset (Mercury, Earth, ISS, Moon, Alpha Centauri AB, etc.) to fill in known values instantly.

How Many Satellites Orbit the Earth?

As of 2025, more than 10,000 active satellites orbit Earth, with tens of thousands more pieces of tracked debris. The vast majority are in Low Earth Orbit. Mega-constellations such as SpaceX Starlink (internet) and Amazon Kuiper have added thousands of satellites, dramatically increasing the population of LEO. All of these objects obey Kepler's third law: the lower the orbit, the shorter the period and the faster the satellite moves.

Solar System Quick Reference

Body Semi-major axis Orbital period
ISS6,771 km~92 min
Moon384,400 km27.32 days
Mercury0.387 AU87.97 days
Venus0.723 AU224.70 days
Earth1.000 AU365.25 days
Mars1.524 AU686.97 days
Jupiter5.203 AU11.86 yr
Saturn9.537 AU29.46 yr
Uranus19.19 AU84.01 yr
Neptune30.07 AU164.79 yr
Alpha Cen AB (binary)23.4 AU~79.9 yr

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