Orbital period
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 (nonrotating) 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).
Contents
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^{[1]} (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 
99942 Apophis (nearEarth asteroid)  0.886  7.769  2,837.6 
Mars  1.881  2.135  779.9 
4 Vesta  3.629  1.380  504.0 
1 Ceres  4.600  1.278  466.7 
10 Hygiea  5.557  1.219  445.4 
Jupiter  11.86  1.092  398.9 
Saturn  29.46  1.035  378.1 
Uranus  84.01  1.012  369.7 
Neptune  164.8  1.006  367.5 
134340 Pluto  248.1  1.004  366.7 
136199 Eris  557  1.002  365.9 
90377 Sedna  12050  1.00001  365.1 
In the case of a planet's moon, the synodic period usually means the Sunsynodic 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.
Calculation
Small body orbiting a central body
According to Kepler's Third Law, the orbital period T\, (in seconds) of two bodies orbiting each other in a circular or elliptic orbit is:
 T = 2\pi\sqrt{a^3/\mu}
where:
 a\, is the orbit's semimajor axis, typically in kilometers

\mu = GM \, is the standard gravitational parameter, typically in km^3/s^2
 G \, is the gravitational constant,
 M \, is the mass of the more massive body.
For all ellipses with a given semimajor 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/m^{3}), the above equation simplifies to (since M = \rho V = \rho {\frac {4}{3}} \pi a^3):
 T = \sqrt{ \frac {3\pi}{G \rho} }
So, for the Earth as the central body (or any other spherically symmetric body with the same mean density, about 5515 kg/m^{3})^{[2]} we get:
 T = 1.41 hours
and for a body made of water (ρ≈1000 kg/m^{3})^{[3]}
 T = 3.30 hours
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
In celestial mechanics, when both orbiting bodies' masses have to be taken into account, the orbital period T\, can be calculated as follows:^{[4]}
 T= 2\pi\sqrt{\frac{a^3}{G \left(M_1 + M_2\right)}}
where:
 a\, is the sum of the semimajor axes of the ellipses in which the centers of the bodies move, or equivalently, the semimajor 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),
 M_1+M_2\, is the sum of the masses of the two bodies,
 G\, is the gravitational constant.
Note that the orbital period is independent of size: for a scale model it would be the same, when densities are the same (see also Orbit#Scaling in gravity).
In a parabolic or hyperbolic trajectory, the motion is not periodic, and the duration of the full trajectory is infinite.
Synodic period
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 P_1 and P_2, so that P_1 < P_2, their synodic period is given by
 \frac{1}{P_{syn}}=\frac{1}{P_1}\frac{1}{P_2}
Tangential velocities at altitude
orbit 
Centertocenter distance 
Altitude above the Earth's surface 
Speed  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 stars
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 
See also
 Geosynchronous orbit derivation
 Sidereal time
 Sidereal year
 Opposition (astronomy)
 List of periodic comets
Notes
External links

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