BEIDOU 3M14
Satellite information BEIDOU 3M14 - BEIDOU-3 M14
| Spacetrack Directory Name | BEIDOU 3M14 |
| Alternative name | BEIDOU-3 M14 |
| Group | BEIDOU |
| Follow BEIDOU 3M14 | BEIDOU 3M14 Tracker |
| Group follow BEIDOU | Tracker BEIDOU |
| Pass predictions BEIDOU 3M14 | Pass predictions BEIDOU 3M14 |
| Orbit launches |
2018-09-19 (8 years ago)
|
| Days in orbit | 2969 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Type | Satellite |
| WWW | Here |
| Perigee | 21520 km |
| Apogee | 21536 km |
| Orbit slope (inclination) | 56.75° |
| Laps per day | 2 |
| Height BEIDOU 3M14 | 21535.54 km |
Additional information BEIDOU 3M14
BEIDOU-3 M14, also known as Beidou DW 38, is a navigation satellite operated by CNSA (China National Space Administration). Launched on September 19, 2018, from the Xichang Satellite Launch Centers LC2 launch pad using the Chang Zheng 3B/YZ-1 vehicle, this satellite has a bus configuration of BD-3M/SAR and was manufactured by CAST. The spacecraft measures 2.2 meters in length, with a diameter of 1.7 meters and a span of 10 meters when its components are deployed. It had a launch mass of 1014 kg and a dry mass of 850 kg. Equipped with two deployable solar arrays and batteries for power generation, the satellite is designed to serve a navigation mission with an expected lifetime of 12 years.
satellite BEIDOU 3M14 Date of exalting 19.09.2018y. Average height of ISS BEIDOU 3M14 hundred 21535.54 km. Average velocity BEIDOU 3M14 is 13605.68 km/h. Inclination BEIDOU 3M14 satellite 56.59°.TLE
Average velocity BEIDOU 3M14
Average inclination BEIDOU 3M14
Mean right ascension of the ascending node (RAAN) BEIDOU 3M14
Mean argument of perigee BEIDOU 3M14
Mean semi-major axis of the orbit BEIDOU 3M14
Mean orbital eccentricity BEIDOU 3M14
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