Geostationary satellite orbit
A geostationary satellite orbit is a circular path above Earth's equator where a satellite moves at the same rate as Earth's rotation, appearing stationary over one longitude.
Also known as: geostationary orbit period, GEO period
How big is it?
23.93 h · orbital period
Orbital period · specified
A little perspective
Geostationary satellite orbit vs A workday: duration comparison
The orbital period of a geostationary satellite orbit is about 2.99 times the duration of a workday.
ELAPSED TIME
A geostationary satellite orbit is a circular path above Earth's equator where a satellite moves at the same rate as Earth's rotation, appearing stationary over one longitude.
Measurements, assumptions & sources +
Geostationary satellite orbit
Orbital period: 23.93 h; specified.
A geostationary satellite’s orbital period matches Earth’s sidereal rotation, about 86,164.09 seconds. Maintaining a fixed apparent longitude also requires a circular equatorial prograde orbit.
NASA — Catalogue of Earth satellite orbits
The marked orbital period is calibrated. Unmeasured illustration details are representative.
A workday
Time: 8 h; reference interval.
A chosen eight-hour working day.
Defined examples — our methodology
The marked time is calibrated. Unmeasured illustration details are representative.
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Why this measurement?
Why we use 23.93 h
We compare the orbital period of a geostationary satellite orbit. This value follows a stated specification; check its scope in the notes.
A geostationary satellite’s orbital period matches Earth’s sidereal rotation, about 86,164.09 seconds. Maintaining a fixed apparent longitude also requires a circular equatorial prograde orbit.
The picture identifies the subject; the diagram compares the recorded values. How calibrated comparisons work →
Recorded properties
Dimensions and measurements
| Property | Selected value | Recorded range | Basis |
|---|---|---|---|
| 23.93 h | Not recorded | specified |
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Sources and method
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- NASA — Catalogue of Earth satellite orbitsA geostationary orbit matches Earth’s sidereal rotation and requires circular equatorial prograde motion.
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