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!bgcolor="lightsteelblue" colspan="2"|Planetary mean orbits | !bgcolor="lightsteelblue" colspan="2"|Planetary mean orbits | ||
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| − | |width="30%"|Epoch||align="right" width="50%"| | + | |width="30%"|Epoch||align="right" width="50%"|1976.606435 (1976 August 10.00 TT) |
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| − | |width="30%"|Semimajor axis (a)||align="right" width="50%"| | + | |width="30%"|Semimajor axis (a)||align="right" width="50%"|4.218×10<sup>8</sup> m |
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| − | |width="30%"|Eccentricity (e)||align="right" width="30%"|0. | + | |width="30%"|Eccentricity (e)||align="right" width="30%"|0.0041 |
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| − | |width="30%"|Inclination (i)||align="right" width="30%"| | + | |width="30%"|Inclination (i)||align="right" width="30%"|0.36519° <br> (0.0006458 radian) |
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| − | |width="30%"|Longitude of the ascending node (LAN, ☊)||align="right" width="30%"| | + | |width="30%"|Longitude of the ascending node (LAN, ☊)||align="right" width="30%"|312.9810604° <br> (5.46255 radian) |
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| − | |width="30%"|Longitude of periapsis (ϖ)||align="right" width="30%"| | + | |width="30%"|Longitude of periapsis (ϖ)||align="right" width="30%"|97.73514° <br> (1.7058 radian) |
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| − | |width="30%"|Mean longitude (L)||align="right" width="30%"| | + | |width="30%"|Mean longitude (L)||align="right" width="30%"|106.724849° <br> (1.8627 radian) |
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!bgcolor="lightsteelblue" colspan="2"|Selected physical parameters | !bgcolor="lightsteelblue" colspan="2"|Selected physical parameters | ||
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|width="30%"|Mass||align="right" width="30%"|8.93×10<sup>22</sup> kg | |width="30%"|Mass||align="right" width="30%"|8.93×10<sup>22</sup> kg | ||
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| − | + | |width="30%"|Note||align="right" width="30%"|*Elements given are from Io.cfg (2002) | |
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| − | |width="30%"|Note||align="right" width="30%"|*Elements given are from Io.cfg ( | ||
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== Io in Orbiter == | == Io in Orbiter == | ||
Io was introduced to [[Orbiter]] in the Orbiter 2002 release, and each version after that. Io's orbit was governed by the Io.cfg file in Orbiter 2002 and later versions until Orbiter 2005 when Vsop87.dll governed Io's orbit. Io is modeled as a sphere 48806 km in diameter with a mass of 8.93×10<sup>22</sup> kg. | Io was introduced to [[Orbiter]] in the Orbiter 2002 release, and each version after that. Io's orbit was governed by the Io.cfg file in Orbiter 2002 and later versions until Orbiter 2005 when Vsop87.dll governed Io's orbit. Io is modeled as a sphere 48806 km in diameter with a mass of 8.93×10<sup>22</sup> kg. | ||
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== See also == | == See also == | ||
*[[w:Io (moon)|Io]] in [[w:Wikipedia|Wikipedia]] | *[[w:Io (moon)|Io]] in [[w:Wikipedia|Wikipedia]] | ||
| − | + | [[Category: Articles]] | |
| − | + | [[Category: Celestial bodies]] | |
| − | + | [[Category: Natural satellites]] | |
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| − | [[Category:Articles]] | ||
| − | [[Category:Celestial bodies | ||
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| − | [[Category:Natural satellites | ||
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{{JupiterSat}} | {{JupiterSat}} | ||
{{SolarSystem}} | {{SolarSystem}} | ||