Image:Orbital elements.svg

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Orbital_elements.svg‎ (Fichier SVG, résolution de 815 × 653 pixels, taille : 15 Kio)

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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

[edit] Summary

Description

Schematics showing the orbital elements of an heliocentric orbit.
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.
Date

Modified 3. Mar. 2006.
Author

Brandir
Permission
(Reusing this image)

Brandir put it under the GFDL
Other versions Image:Bahnelemente.svg

[edit] 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".

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[edit] 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.

Historique du fichier

Cliquer sur une date et une heure pour voir le fichier tel qu’il était à ce moment-là

Date et heureDimensionsUtilisateurCommentaire
actuel4 mars 2006 à 00:59815×653 (15 Kio)Brandir (New version.Corrects a rendernig error of the SVG file)
4 mars 2006 à 00:15815×653 (15 Kio)Brandir ({{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 )