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Orbital Period Calculator

How long an orbit takes and how fast the orbiting body moves — Kepler's third law.

Kepler's third law says the square of the orbital period is proportional to the cube of the semi-major axis.

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Results
Orbital period
92.41 minutes
Orbital velocity
Orbital radius from the centre
Orbits per day
Escape velocity at that altitude
Worth knowing
Reviewed September 2026. Orbital mechanics and optics: identical everywhere, with no market variation of any kind. Greenwich defines the prime meridian from which longitude and Universal Time are measured.
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About orbital period

How the orbital period calculator works

Kepler's third law says the square of the orbital period is proportional to the cube of the semi-major axis. It falls straight out of Newtonian gravity, and it means orbital period depends only on the central mass and the orbit's size — not on the mass of the orbiting object.

That last point is worth sitting with. A grain of dust and a space station at the same altitude orbit in exactly the same time. It is the same reason everything falls at the same rate in a vacuum.

Geostationary orbit is the case everyone meets: the altitude at which the period is exactly one sidereal day, 35,786 km above the equator, so a satellite appears to hang still.

Formula: T = 2π√(a³/GM); v = √(GM/a)

Worked examples

InputsOrbital periodNote
The ISS at 400 km92.41 minutesabout 92.6 minutes
Geostationary orbit23.93 hoursone sidereal day
Low Mars orbit118.04 minutesabout 2 hours

Frequently asked questions

How long does the ISS take to orbit Earth?

About 92.6 minutes at 400 km, so roughly 15.5 orbits a day.

What is geostationary orbit?

35,786 km above the equator, where the orbital period equals one sidereal day so the satellite appears stationary.

Does a heavier satellite orbit more slowly?

No. The orbiting mass cancels out entirely — a dust grain and a space station at the same altitude have the same period.

What is Kepler's third law?

Period squared is proportional to semi-major axis cubed, with the constant set by the central mass.

Why does the ISS need reboosting?

At 400 km there is still enough atmosphere to cause drag, which lowers the orbit by a couple of kilometres a month.

Where these figures come from

Last checked: September 2026. Constants are CODATA 2018 (G, c) and IAU 2015 nominal values (solar and planetary parameters).