GNSS Satellites Orbit - Revision history

Claudia.Prajanu at 21:17, 21 July 2018

2018-07-21T21:17:54Z

← Older revision		Revision as of 21:17, 21 July 2018
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	In the following articles, orbital elements are defined, the navigation message is introduced, and the algorithms for satellite coordinate calculation from the GNSS ([[GPS]],[[GLONASS General Introduction\|GLONASS]] and [[~~GALILEO~~\|Galileo]]) broadcast and precise ephemeris are detailed.		In the following articles, orbital elements are defined, the navigation message is introduced, and the algorithms for satellite coordinate calculation from the GNSS ([[GPS]],[[GLONASS General Introduction\|GLONASS]] and [[Galileo General Introduction\|Galileo]]) broadcast and precise ephemeris are detailed.

	:* [[Two-body Problem]]		:* [[Two-body Problem]]

Carlos.Lopez at 11:33, 23 February 2012

2012-02-23T11:33:15Z

← Older revision		Revision as of 11:33, 23 February 2012
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	\|Level=Basic		\|Level=Basic
	\|YearOfPublication=2011		\|YearOfPublication=2011
	~~\|Logo=gAGE~~
	\|Title={{PAGENAME}}		\|Title={{PAGENAME}}
	}}		}}

Jaume.Sanz at 13:34, 26 January 2012

2012-01-26T13:34:30Z

← Older revision		Revision as of 13:34, 26 January 2012
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	{{Article Infobox2		{{Article Infobox2
	\|Category=Fundamentals		\|Category=Fundamentals
	\|Authors=J. Sanz Subirana, JM. Juan Zornoza and M. ~~Hernandez~~-Pajares, University of ~~Catalunia~~, Spain.		\|Authors=J. Sanz Subirana, J.M. Juan Zornoza and M. Hernández-Pajares, Technical University of Catalonia, Spain.
	\|Level=Basic		\|Level=Basic
	\|YearOfPublication=2011		\|YearOfPublication=2011
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	\|Title={{PAGENAME}}		\|Title={{PAGENAME}}
	}}		}}
	The knowledge of the orbits and clocks of the satellites is fundamental to have a right positioning. Any error in the GNSS} satellite coordinates or satellite clock will affect the positioning accuracy. Information about orbital parameters and clocks is transmitted in the navigation message. Precise ephemeris and clocks are also provided by some organisations as IGS.		The knowledge of the orbits and clocks of the satellites is fundamental to have a right positioning. Any error in the GNSS satellite coordinates or satellite clock will affect the positioning accuracy. Information about orbital parameters and clocks is transmitted in the navigation message. Precise ephemeris and clocks are also provided by some organisations as IGS.

Rui.Pereira at 15:18, 24 January 2012

2012-01-24T15:18:47Z

← Older revision		Revision as of 15:18, 24 January 2012
Line 1:		Line 1:
	{{Article Infobox2		{{Article Infobox2
	\|Category=Fundamentals		\|Category=Fundamentals
	~~\|Title={{PAGENAME}}~~		\|Authors=J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain.
	\|Authors= J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain.
	\|Level=Basic		\|Level=Basic
	\|YearOfPublication=2011		\|YearOfPublication=2011
	\|Logo=gAGE		\|Logo=gAGE
			\|Title={{PAGENAME}}
	}}		}}

	The knowledge of the orbits and clocks of the satellites is fundamental to have a right positioning. Any error in the GNSS} satellite coordinates or satellite clock will affect the positioning accuracy. Information about orbital parameters and clocks is transmitted in the navigation message. Precise ephemeris and clocks are also provided by some organisations as IGS.		The knowledge of the orbits and clocks of the satellites is fundamental to have a right positioning. Any error in the GNSS} satellite coordinates or satellite clock will affect the positioning accuracy. Information about orbital parameters and clocks is transmitted in the navigation message. Precise ephemeris and clocks are also provided by some organisations as IGS.


	In the following articles, orbital elements are defined, the navigation message is introduced, and the algorithms for satellite coordinate calculation from the GNSS ([[GPS]],[[GLONASS]] and [[GALILEO\|Galileo]]) broadcast and precise ephemeris are detailed.		In the following articles, orbital elements are defined, the navigation message is introduced, and the algorithms for satellite coordinate calculation from the GNSS ([[GPS]],[[GLONASS General Introduction\|GLONASS]] and [[GALILEO\|Galileo]]) broadcast and precise ephemeris are detailed.

	:* [[Two-body Problem]]		:* [[Two-body Problem]]

Carlos.Lopez at 15:37, 27 October 2011

2011-10-27T15:37:44Z

← Older revision		Revision as of 15:37, 27 October 2011
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	\|Title={{PAGENAME}}		\|Title={{PAGENAME}}
	\|Authors= J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain.		\|Authors= J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain.
	\|Level=~~Medium~~		\|Level=Basic
	\|YearOfPublication=2011		\|YearOfPublication=2011
	\|Logo=gAGE		\|Logo=gAGE

Carlos.Lopez at 15:13, 8 August 2011

2011-08-08T15:13:59Z

← Older revision		Revision as of 15:13, 8 August 2011
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	[[Category:Fundamentals]]		[[Category:Fundamentals]]
			[[Category:GNSS Time Reference, Coordinate Frames and Orbits]]

Carlos.Lopez at 09:23, 5 August 2011

2011-08-05T09:23:16Z

← Older revision		Revision as of 09:23, 5 August 2011
Line 9:		Line 9:

	The knowledge of the orbits and clocks of the satellites is fundamental to have a right positioning. Any error in the GNSS} satellite coordinates or satellite clock will affect the positioning accuracy. Information about orbital parameters and clocks is transmitted in the navigation message. Precise ephemeris and clocks are also provided by some organisations as IGS.		The knowledge of the orbits and clocks of the satellites is fundamental to have a right positioning. Any error in the GNSS} satellite coordinates or satellite clock will affect the positioning accuracy. Information about orbital parameters and clocks is transmitted in the navigation message. Precise ephemeris and clocks are also provided by some organisations as IGS.


	In the following articles, orbital elements are defined, the navigation message is introduced, and the algorithms for satellite coordinate calculation from the GNSS ([[GPS]],[[GLONASS]] and [[GALILEO\|Galileo]]) broadcast and precise ephemeris are detailed.		In the following articles, orbital elements are defined, the navigation message is introduced, and the algorithms for satellite coordinate calculation from the GNSS ([[GPS]],[[GLONASS]] and [[GALILEO\|Galileo]]) broadcast and precise ephemeris are detailed.

	* [[Two-body Problem]]		:* [[Two-body Problem]]
	* [[Perturbed Motion]]		:* [[Perturbed Motion]]
	* [[GNSS Broadcast Orbits]]		:* [[GNSS Broadcast Orbits]]


	[[Category:Fundamentals]]		[[Category:Fundamentals]]

Carlos.Lopez at 11:00, 22 June 2011

2011-06-22T11:00:16Z

← Older revision		Revision as of 11:00, 22 June 2011
Line 10:		Line 10:
	The knowledge of the orbits and clocks of the satellites is fundamental to have a right positioning. Any error in the GNSS} satellite coordinates or satellite clock will affect the positioning accuracy. Information about orbital parameters and clocks is transmitted in the navigation message. Precise ephemeris and clocks are also provided by some organisations as IGS.		The knowledge of the orbits and clocks of the satellites is fundamental to have a right positioning. Any error in the GNSS} satellite coordinates or satellite clock will affect the positioning accuracy. Information about orbital parameters and clocks is transmitted in the navigation message. Precise ephemeris and clocks are also provided by some organisations as IGS.

	In the following articles, orbital elements are defined, the navigation message is introduced, and the algorithms for satellite coordinate calculation from the GNSS ([[GPS]],[[GLONASS]] and [[GALILEO\|Galileo}}) broadcast and precise ephemeris are detailed.		In the following articles, orbital elements are defined, the navigation message is introduced, and the algorithms for satellite coordinate calculation from the GNSS ([[GPS]],[[GLONASS]] and [[GALILEO\|Galileo]]) broadcast and precise ephemeris are detailed.

	* [[Two-body Problem]]		* [[Two-body Problem]]
	* [[Perturbed ~~motion~~]]		* [[Perturbed Motion]]
	* [[GNSS ~~broadcast orbits~~]]		* [[GNSS Broadcast Orbits]]


	[[Category:Fundamentals]]		[[Category:Fundamentals]]

Carlos.Lopez: Created page with "{{Article Infobox2 |Category=Fundamentals |Title={{PAGENAME}} |Authors= J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain. |Level=Medium..."

2011-06-22T10:59:31Z

Created page with "{{Article Infobox2 |Category=Fundamentals |Title={{PAGENAME}} |Authors= J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain. |Level=Medium..."

New page

{{Article Infobox2
|Category=Fundamentals
|Title={{PAGENAME}}
|Authors= J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain.
|Level=Medium
|YearOfPublication=2011
|Logo=gAGE
}}

The knowledge of the orbits and clocks of the satellites is fundamental to have a right positioning. Any error in the GNSS} satellite coordinates or satellite clock will affect the positioning accuracy. Information about orbital parameters and clocks is transmitted in the navigation message. Precise ephemeris and clocks are also provided by some organisations as IGS.

In the following articles, orbital elements are defined, the navigation message is introduced, and the algorithms for satellite coordinate calculation from the GNSS ([[GPS]],[[GLONASS]] and [[GALILEO|Galileo}}) broadcast and precise ephemeris are detailed.

* [[Two-body Problem]]
* [[Perturbed motion]]
* [[GNSS broadcast orbits]]

[[Category:Fundamentals]]