Orbital period calculator
Period depends only on the semi-major axis and the mass of what you are orbiting, not on the mass of the satellite.
m3/s2
Orbital period
92.414minutes
- Period
- 1:32:25
- Orbital speed
- 7672.60
- Orbits per day
- 15.5820
- Escape speed at that radius
- 10 850.69
- Orbital radius
- 6 771 000.0
- Angular rate
- 0.001 133 16 rad/s
Show the working
- Gravitational parameter of the primary = 398 600 000 000 000
- Radius of the primary = 6371
- Orbit altitude = 400
- Orbital radius = 6371 * 1000 + 400 * 1000 = 6 771 000
- Orbital speed = sqrt(398 600 000 000 000 / 6 771 000) = 7672.6
- Period = 2 * pi * sqrt(6 771 000^3 / 398 600 000 000 000) = 5544.86
- Orbital period = 5544.86 / 60 = 92.4143
- Orbits per day = 5544.86 > 0 ? 86400 / 5544.86 : 0 = 15.582
- Escape speed at that radius = 7672.6 * sqrt(2) = 10 850.7
- Angular rate = 6 771 000 > 0 ? 7672.6 / 6 771 000 : 0 = 0.001 133 16
Values are shown to six significant figures here; the arithmetic itself runs on exact fractions and is only rounded where a number is printed.
Scenarios & local history
Compare a saved scenario
Recent calculations
The formula
- T = 2 pi sqrt(a^3 / GM)
- v = sqrt(GM / a)
The International Space Station at 400 km orbits in about 92.6 minutes, which this reproduces.
Geostationary orbit is where the period equals the sidereal day of 23 h 56 m 4 s: 35 786 km above the equator.
Related calculators
- Earth gravity and escape velocity
- Rocket equation
- Gravitational force
- Pallas gravity and escape velocity
- Phobos gravity and escape velocity
- Pluto gravity and escape velocity
- Redshift and distance
- Rhea gravity and escape velocity
- Saturn gravity and escape velocity
- Sidereal day
- Solar flux by distance
- Stellar magnitude
- All astronomy & space calculators →