BEIDOU 6
Satellite information BEIDOU 6 - Beidou DW 6
| Spacetrack Directory Name | BEIDOU 6 |
| Alternative name | Beidou DW 6 |
| Group | BEIDOU |
| Follow BEIDOU 6 | BEIDOU 6 Tracker |
| Group follow BEIDOU | Tracker BEIDOU |
| Pass predictions BEIDOU 6 | Pass predictions BEIDOU 6 |
| Orbit launches |
2010-10-31 (15 years ago)
|
| Days in orbit | 5782 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Type | Satellite |
| Categories | |
| Perigee | 35758 km |
| Apogee | 35814 km |
| Orbit slope (inclination) | 3.82° |
| Laps per day | 1 |
| Orbit | GEO |
| Height BEIDOU 6 | 35786.16 km |
Additional information BEIDOU 6
The BEIDOU-2 G4 satellite, also known as Beidou DW 6, is operated by CNSA and serves a navigation mission. It was launched on October 31, 2010, from Xichang Satellite Launch Center (LC2) using the Chang Zheng 3C launch vehicle. The spacecraft has dimensions of 3 meters in length, 1.7 meters in diameter, and an overall span of 18 meters when fully deployed. It has a dry mass of 1700 kg and was launched with a total mass of 3060 kg. BEIDOU-2 G4 is equipped with two deployable solar arrays and batteries for power generation. The satellites configuration follows the DFH-3 Bus design, manufactured by CAST, and its shape consists of a box with two panels. It features an RCS of 19.9526 and uses a FY-25 motor. Its operational lifetime is expected to be eight years.
satellite BEIDOU 6 Date of exalting 31.10.2010y. Average height of ISS BEIDOU 6 hundred 35786.16 km. Average velocity BEIDOU 6 is 11068.98 km/h. Inclination BEIDOU 6 satellite 3.37°.TLE
Average velocity BEIDOU 6
Average inclination BEIDOU 6
Mean right ascension of the ascending node (RAAN) BEIDOU 6
Mean argument of perigee BEIDOU 6
Mean semi-major axis of the orbit BEIDOU 6
Mean orbital eccentricity BEIDOU 6
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