Mean Longitude
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Mean longitude is the ecliptic longitude at which an
orbit In celestial mechanics, an orbit (also known as orbital revolution) is the curved trajectory of an object such as the trajectory of a planet around a star, or of a natural satellite around a planet, or of an artificial satellite around an ...
ing body could be found if its orbit were circular and free of perturbations. While nominally a simple longitude, in practice the mean longitude does not correspond to any one physical angle.


Definition

* Define a reference direction, ♈︎, along the
ecliptic The ecliptic or ecliptic plane is the orbital plane of Earth's orbit, Earth around the Sun. It was a central concept in a number of ancient sciences, providing the framework for key measurements in astronomy, astrology and calendar-making. Fr ...
. Typically, this is the direction of the March
equinox A solar equinox is a moment in time when the Sun appears directly above the equator, rather than to its north or south. On the day of the equinox, the Sun appears to rise directly east and set directly west. This occurs twice each year, arou ...
. At this point, ecliptic longitude is 0°. * The body's orbit is generally inclined to the ecliptic, therefore define the angular distance from ♈︎ to the place where the orbit crosses the ecliptic from south to north as the '' longitude of the ascending node'', . * Define the angular distance along the plane of the orbit from the ascending node to the pericenter as the '' argument of periapsis,'' . * Define the ''
mean anomaly In celestial mechanics, the mean anomaly is the fraction of an elliptical orbit's period that has elapsed since the orbiting body passed periapsis, expressed as an angle which can be used in calculating the position of that body in the classical ...
'', , as the angular distance from the periapsis which the body would have if it moved in a circular orbit, in the same orbital period as the actual body in its elliptical orbit. From these definitions, the ''mean longitude'', , is the angular distance the body would have from the reference direction if it moved with uniform speed, :L=\Omega+\omega+M, measured along the ecliptic from ♈︎ to the ascending node, then up along the plane of the body's orbit to its mean position. Sometimes the value defined in this way is called the "mean mean longitude", and the term "mean longitude" is used for a value that does have short-term variations (such as over a synodic month or a year in the case of the moon) but does not include the correction due to the difference between true anomaly and mean anomaly. Also, sometimes the mean longitude (or mean mean longitude) is considered to be a slowly varying function, modeled with a Maclaurin series, rather than a simple linear function of time. The true longitude is a separate value that corresponds to the actual angular distance from the reference direction, taking into account the varying speed and non-circular shape of the orbit. It is the analogue to the
true anomaly In celestial mechanics, true anomaly is an angular parameter that defines the position of a body moving along a Keplerian orbit. It is the angle between the direction of periapsis and the current position of the body, as seen from the main focus ...
, which is measured relative to periapsis like the mean anomaly.


Discussion

Mean longitude, like
mean anomaly In celestial mechanics, the mean anomaly is the fraction of an elliptical orbit's period that has elapsed since the orbiting body passed periapsis, expressed as an angle which can be used in calculating the position of that body in the classical ...
, does not measure an angle between any physical objects. It is simply a convenient uniform measure of how far around its orbit a body has progressed since passing the reference direction. While mean longitude measures a mean position and assumes constant speed, true longitude measures the actual longitude and assumes the body has moved with its actual speed, which varies around its
elliptical orbit In astrodynamics or celestial mechanics, an elliptical orbit or eccentric orbit is an orbit with an orbital eccentricity, eccentricity of less than 1; this includes the special case of a circular orbit, with eccentricity equal to 0. Some or ...
. The difference between the two is known as the equation of the center.Meeus, Jean (1991). p. 222


Formulae

From the above definitions, define the '' longitude of periapsis'' :\varpi = \Omega + \omega. Then mean longitude is also :''L=\varpi+M''. Another form often seen is the ''mean longitude at epoch'', . This is simply the mean longitude at a reference time , known as the
epoch In chronology and periodization, an epoch or reference epoch is an instant in time chosen as the origin of a particular calendar era. The "epoch" serves as a reference point from which time is measured. The moment of epoch is usually decided b ...
. Mean longitude can then be expressed, :L=\epsilon + n(t-t_0), or :L=\epsilon + nt, if is measured relative to the epoch . where ''n'' is the '' mean angular motion'' and ''t'' is any arbitrary time. In some sets of
orbital elements Orbital elements are the parameters required to uniquely identify a specific orbit. In celestial mechanics these elements are considered in two-body systems using a Kepler orbit. There are many different ways to mathematically describe the same o ...
, ''ε'' is one of the six elements.


See also

*
Mean motion In orbital mechanics, mean motion (represented by ''n'') is the angular speed required for a body to complete one orbit, assuming constant speed in a circular orbit which completes in the same time as the variable speed, elliptical orbit of the a ...
*
Orbital elements Orbital elements are the parameters required to uniquely identify a specific orbit. In celestial mechanics these elements are considered in two-body systems using a Kepler orbit. There are many different ways to mathematically describe the same o ...
* True longitude


References

{{DEFAULTSORT:Mean Longitude Orbits