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File:Orbital elements.svg

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P2 Ecliptic plane
♈ Vernal point
S Primary, e.g. Sun
P1 Orbital plane
a Semi-major axis
☊ Ascending node
Ω Longitude of the ascending node
i Inclination
P Periapsis
ω Argument of periapsis

Summary

Description Schematics showing the orbital elements of an heliocentric orbit.
Date Modified 3. Mar. 2006.
Source This is a modified version of Bahnelemente.svg (GFDL) by ArtMechanic. The original version has been "internationalised", no sentences in any language are present.
Author Brandir
Permission
(Reusing this file)		 Brandir put it under the GFDL
Other versions Image:Bahnelemente.svg

Licensing

GNU head Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License.
w:en:Creative Commons
attribution share alike 		This file is licensed under the Creative Commons Attribution-Share Alike 3.0 Unported license.
You are free:
  • to share – to copy, distribute and transmit the work
  • to remix – to adapt the work
Under the following conditions:
  • attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use.
  • share alike – If you remix, transform, or build upon the material, you must distribute your contributions under the same or compatible license as the original.
This licensing tag was added to this file as part of the GFDL licensing update.

Notes

  • The longitude of periapsis is defined as the sum of the longitude of the ascending node and the argument of periapsis. It is a numerically convenient way of expressing the same quantity, but which does not have a direct geometrical meaning.
  • The orbital focus S has been set here to the primary's position, which is the way orbits are defined in astronomy. It is also possible to express the orbital mechanics by setting S to the system's centre of mass (a barycentric orbit), in which case the semi-major axis will be smaller by a factor of up to 2.

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Date/TimeThumbnailDimensionsUserComment
current22:59, 3 March 2006Thumbnail for version as of 22:59, 3 March 2006815 × 653 (15 KB)Brandir~commonswikiNew version.Corrects a rendernig error of the SVG file
22:15, 3 March 2006Thumbnail for version as of 22:15, 3 March 2006815 × 653 (15 KB)Brandir~commonswiki{{Information| |Description = Animation showing the motion of a satellite in a Geostationary Orbit (Green) in relation with a point in the surface of the Earth (Brown), in a 24-hour cycle. |Source = Own work. Rendered with PovRay-3.0, the pov file is

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