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Longitude of the ascending node

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Defining the orbit of an object in space
The longitude of theascending node (bright green) as a part of a diagram oforbital parameters.

Thelongitude of the ascending node, also known as theright ascension of the ascending node, is one of theorbital elements used to specify theorbit of an object in space. Denoted with the symbolΩ, it is the angle from a specified reference direction, called theorigin of longitude, to the direction of theascending node (☊), as measured in a specifiedreference plane.[1] The ascending node is the point where the orbit of the object passes through the plane of reference, as seen in the adjacent image.

Types

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Commonly used reference planes and origins of longitude include:

In the case of abinary star known only from visual observations, it is not possible to tell which node is ascending and which is descending. In this case the orbital parameter which is recorded is simply labeledlongitude of the node, ☊, and represents the longitude of whichever node has a longitude between 0 and 180 degrees.[5], chap. 17;[4], p. 72.

Calculation from state vectors

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Inastrodynamics, the longitude of the ascending node can be calculated from thespecific relative angular momentum vectorh as follows:

n=k×h=(hy,hx,0)Ω={arccosnx|n|,ny0;2πarccosnx|n|,ny<0.{\displaystyle {\begin{aligned}\mathbf {n} &=\mathbf {k} \times \mathbf {h} =(-h_{y},h_{x},0)\\\Omega &={\begin{cases}\arccos {{n_{x}} \over {\mathbf {\left|n\right|} }},&n_{y}\geq 0;\\2\pi -\arccos {{n_{x}} \over {\mathbf {\left|n\right|} }},&n_{y}<0.\end{cases}}\end{aligned}}}

Here,n = ⟨nx,ny,nz⟩ is a vector pointing towards theascending node. The reference plane is assumed to be thexy-plane, and the origin of longitude is taken to be the positivex-axis.k is the unit vector (0, 0, 1), which is the normal vector to thexy reference plane.

Fornon-inclined orbits (withinclination equal to zero), ☊ is undefined. For computation it is then, by convention, set equal to zero; that is, the ascending node is placed in the reference direction, which is equivalent to lettingn point towards the positivex-axis.

See also

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References

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  1. ^Parameters Describing Elliptical Orbits, web page, accessed May 17, 2007.
  2. ^abOrbital Elements and Astronomical TermsArchived 2007-04-03 at theWayback Machine, Robert A. Egler, Dept. of Physics,North Carolina State University. Web page, accessed May 17, 2007.
  3. ^Keplerian Elements TutorialArchived 2002-10-14 at theWayback Machine, amsat.org, accessed May 17, 2007.
  4. ^abThe Binary Stars, R. G. Aitken, New York: Semi-Centennial Publications of the University of California, 1918.
  5. ^abCelestial Mechanics,Jeremy B. Tatum, on line, accessed May 17, 2007.
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