Orbital period



         


planet (or another object) to make one full orbit.

There are several kinds of orbital periods for objects around the Sun:

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Relation between sidereal and synodic period

Copernicus devised a mathematical formula to calculate a planet's sidereal period from its synodic period.

Using the abbreviations

E = the sidereal period of Earth (a sidereal year, not the same as a tropical year)
P = the sidereal period of the other planet
S = the synodic period of the other planet (wrt Earth)

During the time S, the Earth moves over an angle of (360°/E)S (assuming a circular orbit) and the planet moves (360°/P)S.

Let us consider the case of an inferior planet, i.e. a planet that will complete one orbit more than Earth before the two return to the same position relative to the sun.

<math> \frac{S}{P} 360^\circ = \frac{S}{E} 360^\circ + 360^\circ <math>

and using algebra we obtain

<math> P = \frac1{\frac1E + \frac1S} <math>

For a superior planet one derives likewise:

<math> P = \frac1{\frac1E - \frac1S} <math>

The above formulæ are easily understood by considering the angular velocities of the Earth and the object: the object's apparent angular velocity is its true (sidereal) angular velocity minus the Earth's, and the synodic period is then simply a full circle divided by that apparent angular velocity.

Table of synodic periods in the Solar System, relative to Earth:


  Sid. P. (a) Syn. P. (a) Syn. P. (d)
Mercury 0.241 0.317 115.9
Venus 0.615 1.599 583.9
Earth 1
Moon 0.0748 0.0809 29.5306
Mars 1.881 2.135 780.0
1 Ceres 4.600 1.278 466.7
Jupiter 11.87 1.092 398.9
Saturn 29.45 1.035 378.1
Uranus 84.07 1.012 369.7
Neptune 164.9 1.006 367.5
Pluto 248.1 1.004 366.7


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Calculation

In astrodynamics orbital period <math>T\,<math> of small body orbiting central body is calculated as follows:

<math>T = 2\pi\sqrt{a^3/\mu}<math>

and

<math> \mu = GM \,<math>

where:


In celestial mechanics when both orbiting bodies' masses have to be taken into account orbital period <math>P\,<math> can be calculated as follows:

<math>P = 2\pi\sqrt{\frac{a^3}{G \left(M_1 + M_2\right)}}<math>

where:

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).

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