BEIDOU 3M1
Satellite information BEIDOU 3M1 - BEIDOU-3 M1
| Spacetrack Directory Name | BEIDOU 3M1 |
| Alternative name | BEIDOU-3 M1 |
| Group | BEIDOU |
| Follow BEIDOU 3M1 | BEIDOU 3M1 Tracker |
| Group follow BEIDOU | Tracker BEIDOU |
| Pass predictions BEIDOU 3M1 | Pass predictions BEIDOU 3M1 |
| Orbit launches |
2017-11-05 (8 years ago)
|
| Days in orbit | 3241 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Type | Satellite |
| WWW | Here |
| Categories | |
| Perigee | 21507 km |
| Apogee | 21549 km |
| Orbit slope (inclination) | 56.78° |
| Laps per day | 2 |
| Orbit | MEO |
| Height BEIDOU 3M1 | 21535.54 km |
Additional information BEIDOU 3M1
The BEIDOU-3 M1 satellite, also known as Beidou DW 24, is a Chinese navigation satellite launched on November 5, 2017, from the Xichang Satellite Launch Center (LC3) using the Chang Zheng 3B/YZ-1 launch vehicle. It has dimensions of 2.2 meters in length and 1.7 meters in diameter with a span of 10 meters. The satellites dry mass is 850 kilograms, while its launch mass was 1014 kilograms. BEIDOU-3 M1, manufactured by CAST for the China National Space Administration (CNSA), has a mission lifespan of 12 years and utilizes two deployable solar arrays and batteries for power supply. The satellites structure is described as Box + 2 Pan in shape, with its primary purpose being navigation within the Beidou-3 constellation.
satellite BEIDOU 3M1 Date of exalting 05.11.2017y. Average height of ISS BEIDOU 3M1 hundred 21535.54 km. Average velocity BEIDOU 3M1 is 13605.68 km/h. Inclination BEIDOU 3M1 satellite 56.61°.TLE
Average velocity BEIDOU 3M1
Average inclination BEIDOU 3M1
Mean right ascension of the ascending node (RAAN) BEIDOU 3M1
Mean argument of perigee BEIDOU 3M1
Mean semi-major axis of the orbit BEIDOU 3M1
Mean orbital eccentricity BEIDOU 3M1
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