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The orbital period is the time taken for a given object to make one complete orbit around another object.
When mentioned without further qualification in astronomy this refers to the sidereal period of an astronomical object, which is calculated with respect to the stars.
There are several kinds of orbital periods for objects around the Sun (or other celestial objects):
- The sidereal period is the temporal cycle that it takes an object to make a full orbit, relative to the stars. This is the orbital period in an inertial (non-rotating) frame of reference.
- The synodic period is the temporal interval that it takes for an object to reappear at the same point in relation to two or more other objects, e.g. when the Moon relative to the Sun as observed from Earth returns to the same illumination phase. The synodic period is the time that elapses between two successive conjunctions with the Sun–Earth line in the same linear order. The synodic period differs from the sidereal period due to the Earth's orbiting around the Sun.
- The draconitic period, or draconic period, is the time that elapses between two passages of the object through its ascending node, the point of its orbit where it crosses the ecliptic from the southern to the northern hemisphere. This period differs from the sidereal period because both the orbital plane of the object and the plane of the ecliptic precess with respect to the fixed stars, so their intersection, the line of nodes, also precesses with respect to the fixed stars. Although the plane of the ecliptic is often held fixed at the position it occupied at a specific epoch, the orbital plane of the object still precesses causing the draconitic period to differ from the sidereal period.
- The anomalistic period is the time that elapses between two passages of an object at its periapsis (in the case of the planets in the solar system, called the perihelion), the point of its closest approach to the attracting body. It differs from the sidereal period because the object's semimajor axis typically advances slowly.
- Also, the Earth's tropical period (or simply its "year") is the time that elapses between two alignments of its axis of rotation with the Sun, also viewed as two passages of the object at right ascension zero. One Earth year has a slightly shorter interval than the solar orbit (sidereal period) because the inclined axis and equatorial plane slowly precesses (rotates in sidereal terms), realigning before orbit completes with an interval equal to the inverse of the precession cycle (about 25,770 years).
- 1 Relation between the sidereal and synodic periods
- 2 Calculation
- 3 Tangential velocities at altitude
- 4 Binary stars
- 5 See also
- 6 Notes
- 7 External links
Relation between the sidereal and synodic periods
Table of synodic periods in the Solar System, relative to Earth:
|Object||Sidereal period (yr)||Synodic period (yr)||Synodic period (d)|
|Solar surface||0.069 (25.3 days)||0.074||27.3|
|Mercury||0.240846 (87.9691 days)||0.317||115.88|
|Venus||0.615 (225 days)||1.599||583.9|
|Earth||1 (365.25636 solar days)||—||—|
|Moon||0.0748 (27.32 days)||0.0809||29.5306|
|Apophis (near-Earth asteroid)||0.886||7.769||2,837.6|
|90377 Sedna||12050||1.00001||365.1|
In the case of a planet's moon, the synodic period usually means the Sun-synodic period, namely, the time it takes the moon to complete its illumination phases, completing the solar phases for an astronomer on the planet's surface. The Earth's motion does not determine this value for other planets because an Earth observer is not orbited by the moons in question. For example, Deimos's synodic period is 1.2648 days, 0.18% longer than Deimos's sidereal period of 1.2624 d.
Small body orbiting a central body
- is the orbit's semi-major axis, typically in kilometers
- is the standard gravitational parameter, typically in
- is the gravitational constant,
- is the mass of the more massive body.
For all ellipses with a given semi-major axis the orbital period is the same, regardless of eccentricity.
Orbital period as a function of central body's density
When a very small body is in a circular orbit barely above the surface of a sphere of any radius and mean density ρ (in kg/m3), the above equation simplifies to (since ):
So, for the Earth as the central body (or any other spherically symmetric body with the same mean density, about 5515 kg/m3) we get:
and for a body made of water (ρ≈1000 kg/m3)
Thus, as an alternative for using a very small number like G, the strength of universal gravity can be described using some reference material, like water: the orbital period for an orbit just above the surface of a spherical body of water is 3 hours and 18 minutes. Conversely, this can be used as a kind of "universal" unit of time if we have a unit of mass, a unit of length and a unit of density.
Two bodies orbiting each other
- is the sum of the semi-major axes of the ellipses in which the centers of the bodies move, or equivalently, the semi-major axis of the ellipse in which one body moves, in the frame of reference with the other body at the origin (which is equal to their constant separation for circular orbits),
- is the sum of the masses of the two bodies,
- is the gravitational constant.
In a parabolic or hyperbolic trajectory, the motion is not periodic, and the duration of the full trajectory is infinite.
When two bodies orbit a third body in different orbits, and thus different orbital periods, their respective, synodic period can be found. If the orbital periods of the two bodies around the third are called and , so that , their synodic period is given by
Tangential velocities at altitude
the Earth's surface
|speed(relative to Earth's surface)||Orbital period||specific orbital energy|
|Standing on Earth's surface at the equator (for comparison -- not an orbit)||6,378 km||0 km||465.1 m/s (1,040 mph)||1 day (24h)||−62.6 MJ/kg|
|Orbiting at Earth's surface (equator)||6,378 km||0 km||7.9 km/s (17,672 mph)||1 h 24 min 18 sec||−31.2 MJ/kg|
|Low Earth orbit||6,600 to 8,400 km||200 to 2,000 km||circular orbit: 6.9 to 7.8 km/s (15,430 mph to 17,450 mph) respectively
elliptic orbit: 6.5 to 8.2 km/s respectively
|1 h 29 min to 2 h 8 min||−29.8 MJ/kg|
|Molniya orbit||6,900 to 46,300 km||500 to 39,900 km||1.5 to 10.0 km/s (3,335 mph to 22,370 mph) respectively||11 h 58 min||−4.7 MJ/kg|
|Geostationary||42,000 km||35,786 km||3.1 km/s (6,935 mph)||23 h 56 min||−4.6 MJ/kg|
|Orbit of the Moon||363,000 to 406,000 km||357,000 to 399,000 km||0.97 to 1.08 km/s (2,170 to 2,416 mph) respectively||27.3 days||−0.5 MJ/kg|
|Binary star||Orbital period|
|AM Canum Venaticorum||17.146 minutes|
|Beta Lyrae AB||12.9075 days|
|Alpha Centauri AB||79.91 years|
|Proxima Centauri - Alpha Centauri AB||500,000 years or more|
- Geosynchronous orbit derivation
- Sidereal time
- Sidereal year
- Opposition (astronomy)
- List of periodic comets
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