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Galileo Space Segment: Difference between revisions
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{{Article Infobox2 | |||
|Category=GALILEO | |||
|Title={{PAGENAME}} | |||
|Authors=GMV | |||
|Level=Basic | |||
|YearOfPublication=2011 | |||
|Logo=GMV | |||
}} | |||
The Galileo space segment will comprise 30 satellites in a Walker constellation with three orbital planes at 56° nominal inclination. Each plane will contain nine operational satellites, equally spaced, 40° apart, plus one spare satellite to replace any of the operational satellites in case of failures. | The Galileo space segment will comprise 30 satellites in a Walker constellation with three orbital planes at 56° nominal inclination. Each plane will contain nine operational satellites, equally spaced, 40° apart, plus one spare satellite to replace any of the operational satellites in case of failures. | ||
[[File:Galileo Space Segment.jpg|none|thumb|400px|alt=galileo space segment|Galileo Space Segment]] | [[File:Galileo Space Segment.jpg|none|thumb|400px|alt=galileo space segment|Galileo Space Segment]] | ||
The orbit altitude of 23 222 km results in a repeat a constellation repeat cycle of ten days during which each satellite has completed seventeen revolutions. | The orbit altitude of 23 222 km results in a repeat a constellation repeat cycle of ten days during which each satellite has completed seventeen revolutions. |
Revision as of 09:33, 11 April 2011
GALILEO | |
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Title | Galileo Space Segment |
Author(s) | GMV |
Level | Basic |
Year of Publication | 2011 |
The Galileo space segment will comprise 30 satellites in a Walker constellation with three orbital planes at 56° nominal inclination. Each plane will contain nine operational satellites, equally spaced, 40° apart, plus one spare satellite to replace any of the operational satellites in case of failures.
The orbit altitude of 23 222 km results in a repeat a constellation repeat cycle of ten days during which each satellite has completed seventeen revolutions.