Kepler's Third Law Calculator

Calculate orbital periods, distances, and central masses using Kepler's Third Law with solar system verification and unit conversions.

Kepler's Third Law Calculator

AU
Orbital Period
1.0000 years
365.26 days (8,766.1 hours)
Semi-Major Axis
1.000000 AU
149,600,000.00 km
Central Mass
1.000000 M☉
1.989e+30 kg
Orbital Velocity
29.785 km/s
Average circular orbital velocity
T²/a³ Ratio
1.000000
Should equal 1/M (in solar-mass AU-year units)
Distance
149,600,000.00 km
1.581e-5 light-years
T²/a³ Ratio Verification
Expected: 1.000000 — Actual: 1.000000

Solar System Verification

Planeta (AU)T (years)T²/a³Predicted TEccentricity
Mercury0.3870.2411.00210.2410.206
Venus0.7230.6151.00080.6150.007
Earth111.00001.0000.017
Mars1.5241.8810.99961.8810.093
Jupiter5.20311.8620.999011.8680.049
Saturn9.53729.4571.000329.4520.054
Uranus19.19184.0110.998684.0710.047
Neptune30.069164.80.9990164.8840.009

Unit Conversions

QuantityValue
Period (years)1.000000
Period (days)365.2560
Period (hours)8,766.14
Distance (AU)1.000000
Distance (km)149,600,000.00
Distance (miles)92,957,101.60
Planning notes, formulas, and examples

About the Kepler's Third Law Calculator

Kepler's Third Law of Planetary Motion, published by Johannes Kepler in 1619, states that the square of a planet's orbital period is proportional to the cube of its semi-major axis. Refined by Newton with the inclusion of the central body's mass, this relationship is one of the most powerful tools in astronomy: T² = (4π²/GM) × a³.

In convenient units where distance is in AU, period in years, and mass in solar masses, the law simplifies beautifully to T² = a³/M. This means that for any object orbiting the Sun, the ratio T²/a³ equals exactly 1. For objects orbiting other bodies, the ratio equals the inverse of the central mass in solar masses.

This calculator lets you solve for any one of the three variables—orbital period, orbital distance, or central mass—given the other two. It includes a verification table showing Kepler's Third Law holds precisely for all eight planets of our solar system, complete with eccentricity data and predicted periods.

When This Page Helps

This calculator brings one of astronomy's most fundamental laws to life. It's invaluable for students studying orbital mechanics, for verifying astronomical data, and for quickly computing orbital parameters for any two-body gravitational system.

How to Use the Inputs

  1. Select what to solve for: orbital period, distance (semi-major axis), or central body mass.
  2. Enter the known values in the input fields.
  3. Choose the mass unit: solar masses, Earth masses, or kilograms.
  4. Use preset buttons for common scenarios like Earth orbiting the Sun or the ISS.
  5. Review the output cards including period, distance, velocity, and T²/a³ ratio.
  6. Check the solar system verification table to confirm Kepler's law.
Formula used
Kepler's Third Law: T² = a³/M (in AU-year-solar mass units). General form: T² = (4π²a³)/(GM). Orbital velocity: v = 2πa/T. Where T is orbital period, a is semi-major axis, M is central body mass, G is gravitational constant.

Example Calculation

Result: T ≈ 11.862 years

Jupiter orbits at 5.203 AU from the Sun. Kepler's Third Law predicts T = √(5.203³) ≈ 11.862 years, matching the observed orbital period almost exactly.

Tips & Best Practices

  • T²/a³ should always equal 1/M (in solar mass units) — use this to verify results.
  • The law is exact regardless of orbital eccentricity.
  • To find a planet's mass, observe the orbit of its moon and solve for M.
  • For the Moon orbiting Earth, use Earth masses for the central body.
  • The ISS orbits at only 0.0000452 AU but completes an orbit in about 92 minutes.

When To Use This Calculator

Calculate orbital periods, distances, and central masses using Kepler's Third Law with solar system verification and unit conversions. Use it when you need a repeatable calculation in the physics / astronomy category and want the setup, result, and supporting values kept together. This is especially helpful when small input changes, unit choices, or rounding decisions can change the final number.

How To Check The Result

Start by confirming that the inputs match the formula shown on the page. Then compare the main output with the worked example and any secondary values shown by the calculator. If the result will be used in another calculation, keep extra precision until the final step and record the assumptions beside the number.

Practical Notes

Treat the result as a calculation aid rather than a substitute for context. For schoolwork, include the formula and substitution steps. For planning, technical, financial, or health-related decisions, verify important numbers against primary records, current rules, or a qualified professional before acting on them.

Sources & Methodology

Last updated:

Frequently Asked Questions

  • It states that the square of a planet's orbital period is proportional to the cube of its semi-major axis. For solar orbits: T² = a³ (in AU and years).