Kepler's Third Law Calculator

Kepler's Third Law Diagram
Central Mass Orbiting Body Semi-Major Axis T² ∝ a³

Kepler's Third Law Calculator

What is Kepler's Third Law?

Kepler's Third Law, also known as the Law of Periods, is a fundamental principle in astronomy that describes the relationship between the orbital period of a planet and its average distance from the sun. This law applies to any system where one body orbits another under the influence of gravity.

Formula

Kepler's Third Law is expressed mathematically as:

T2a3=4π2GM

Where:

  • T is the orbital period of the planet (in seconds)
  • a is the semi-major axis of the orbit (in meters)
  • G is the gravitational constant (6.67430×1011 m3 kg1 s2)
  • M is the mass of the central body (in kilograms)

Calculation Steps

Let's calculate the orbital period of Earth around the Sun:

  1. Given:
    • Semi-major axis of Earth's orbit (a) = 1.496×1011 m
    • Mass of the Sun (M) = 1.989×1030 kg
  2. Rearrange Kepler's Third Law to solve for T: T=4π2a3GM
  3. Substitute the known values: T=4π2(1.496×1011 m)3(6.67430×1011 m3 kg1 s2)(1.989×1030 kg)
  4. Perform the calculation: T3.156×107 s
  5. Convert to years: T1.000 year

Example and Visual Representation

Let's visualize Kepler's Third Law for the inner planets of our solar system:

Orbital Distance (not to scale) Orbital Period Kepler's Third Law: T² ∝ a³

This diagram illustrates:

  • The Sun at the center (yellow)
  • The orbits of Mercury (red), Venus (green), Earth (blue), and Mars (orange)
  • As the orbital distance increases, the orbital period increases more rapidly (proportional to a³/²)