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{{Article Infobox2 | {{Article Infobox2 | ||
|Category= | |Category=BEIDOU | ||
| | |Editors=GMV | ||
|Level=Basic | |Level=Basic | ||
|YearOfPublication=2011 | |YearOfPublication=2011 | ||
|Logo=GMV | |Logo=GMV | ||
|Title={{PAGENAME}} | |||
}} | }} | ||
The BeiDou Space Segment consists of a constellation of 35 satellites, which include 5 geostationary orbit (GEO) satellites and 30 non-GSO satellites. The system is currently under development [[BeiDou_Future_and_Evolutions|evolving]] from a regional system called [[Other Regional Systems#BeiDou-1|BeiDou-1]], and in the first phase will provide global navigation services by 2020, similarly to the [[GPS General Introduction|GPS]], [[GLONASS General Introduction|GLONASS]] or [[GALILEO General Introduction|Galileo]] systems. | |||
==BeiDou Space Segment== | |||
The | The BeiDou Space Segment will consist of a constellation of 35 satellites, which include 5 geostationary orbit (GEO) satellites and 30 non-GSO satellites; 27 in Medium Earth Orbit (MEO) and 3 in Inclined Geosynchronous Orbit (IGSO), with a worldwide coverage.<ref name=BEIDOU_MUNICH_2011>China Satellite Navigation Office, Development of BeiDou Navigation Satellite System, Munich Satellite Navigation Summit, 2011</ref><ref name=BeiDou_Wiki>[http://en.wikipedia.org/wiki/Beidou_Navigation_Satellite_System BeiDou Navigation Satellite System in Wikipedia]</ref> | ||
[[File:CompassConstellation.jpg|BeiDou Space Segment|250px|thumb]] | |||
As of December 2011, the Initial Operation Service was officially declared providing initial passive positioning navigation and timing services for China service area<ref name=BeiDou_Wiki />. | |||
{| class="wikitable" | The nominal constellation includes 35 satellites, 5 GEOs, 3 IGSOs and 27 MEOs. | ||
The number of IGSO orbits is 3, with one IGSO per plane. The intersection node is 118E. The MEOs are deployed as a Walker constellation; 24 MEOs in 3 planes plus 3 spares. The orbital parameters of the final constellation are shown in the following table:<ref name=BEIDOU_MUNICH_2011/> | |||
{| class="wikitable" align="center" | |||
|+align="bottom" |''Final BeiDou Constellation'' | |||
|- | |- | ||
!Orbit parmts. | |||
|- | !GEO | ||
!IGSO | |||
| | !MEO | ||
| | |-align="center" | ||
|- | !Semi-Major Axis (Km) | ||
| | |42164 | ||
| | |42164 | ||
| | |27878 | ||
|- | |-align="center" | ||
| | !Eccentricity | ||
|- | |0 | ||
| | |0 | ||
|0 | |||
| | |-align="center" | ||
| | !Inclination (deg) | ||
| | |0 | ||
|55 | |||
|55 | |||
|-align="center" | |||
!RAAN (deg) | |||
|158.75E, 180E, 210.5E, 240E,260E | |||
|218E,98E,338E | |||
|rowspan="3"|-- | |||
|-align="center" | |||
!Argument Perigee | |||
|0 | |||
|0 | |||
|-align="center" | |||
!Mean anomaly (deg) | |||
|0 | |||
|218E:0,98E:120,338E:240 | |||
|-align="center" | |||
!# Sats | |||
|5 | |||
|3 | |||
|27 | |||
|-align="center" | |||
!# Planes | |||
|1 | |||
|3 | |||
|3 | |||
|} | |} | ||
==References== | ==References== | ||
<references/> | <references/> | ||
[[Category: | [[Category:BEIDOU]] |
Latest revision as of 17:20, 18 September 2014
BEIDOU | |
---|---|
Title | BeiDou Space Segment |
Edited by | GMV |
Level | Basic |
Year of Publication | 2011 |
The BeiDou Space Segment consists of a constellation of 35 satellites, which include 5 geostationary orbit (GEO) satellites and 30 non-GSO satellites. The system is currently under development evolving from a regional system called BeiDou-1, and in the first phase will provide global navigation services by 2020, similarly to the GPS, GLONASS or Galileo systems.
BeiDou Space Segment
The BeiDou Space Segment will consist of a constellation of 35 satellites, which include 5 geostationary orbit (GEO) satellites and 30 non-GSO satellites; 27 in Medium Earth Orbit (MEO) and 3 in Inclined Geosynchronous Orbit (IGSO), with a worldwide coverage.[1][2]
As of December 2011, the Initial Operation Service was officially declared providing initial passive positioning navigation and timing services for China service area[2].
The nominal constellation includes 35 satellites, 5 GEOs, 3 IGSOs and 27 MEOs. The number of IGSO orbits is 3, with one IGSO per plane. The intersection node is 118E. The MEOs are deployed as a Walker constellation; 24 MEOs in 3 planes plus 3 spares. The orbital parameters of the final constellation are shown in the following table:[1]
Orbit parmts. | GEO | IGSO | MEO |
---|---|---|---|
Semi-Major Axis (Km) | 42164 | 42164 | 27878 |
Eccentricity | 0 | 0 | 0 |
Inclination (deg) | 0 | 55 | 55 |
RAAN (deg) | 158.75E, 180E, 210.5E, 240E,260E | 218E,98E,338E | -- |
Argument Perigee | 0 | 0 | |
Mean anomaly (deg) | 0 | 218E:0,98E:120,338E:240 | |
# Sats | 5 | 3 | 27 |
# Planes | 1 | 3 | 3 |
References
- ^ a b China Satellite Navigation Office, Development of BeiDou Navigation Satellite System, Munich Satellite Navigation Summit, 2011
- ^ a b BeiDou Navigation Satellite System in Wikipedia