Kepler’s third law of planetary motion states that the square of the orbital period (T) of a planet is directly proportional to the cube of the semi-major axis (r) of its orbit. This relationship can be expressed mathematically as:
This formula allows us to calculate the orbital period of a satellite or planet given its distance from the central body and the mass of that body.
What is the formula for calculating orbital period?
How do I use this calculator to find the orbital period?
What does Kepler’s third law state?
Can this calculator be used for any celestial body?
What is the gravitational constant (G) in the formula?
How accurate is this orbital period calculator?
What units should I use for the inputs?
Results are for informational purposes only and do not constitute professional advice.
