BEIDOU 3M21, 44793
Orbit data source: Space-Track
BEIDOU 3M21, 44793 is a payload satellite owned by CNSA (CN) in MEO that was launched on Sat, 23 Nov 2019 UTC via a CHANG ZHENG 3B/YZ-1 launch vehicle from the Xichang Space Center, China (XSC). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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44793 intel report (Beta)
BEIDOU 3M21 details
| Identifier | |
| Orbit | MEO |
| Last TLE update | 23 hours ago |
| Origin | |
| Manufacturer | SECM |
| Mission | Operational Defense Navigation |
| Bus & Motor | BD-3M2, Unknown motor |
| Mass | 1,014 kg wet, ~850 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, Unknown HBR |
| Radar Cross Section | 8.984 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 23 hours ago
0 BEIDOU 3M21
1 44793U 19078A 24361.05754953 -.00000089 00000-0 00000-0 0 9994
2 44793 54.4132 318.6880 0006118 13.8569 346.1534 1.86232082 34623Epoch: 2024-12-26T01:22Z
Definitive object data (Epoch: 2024-12-26T01:22:52.279Z)
| Latitude | -0.00002° |
| Longitude | -157.09157° |
| Altitude | 21,511.65 km |
| Speed | 3.782 km/s |
| True Right ascension | 21h 14m 40s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -52.69578° |
| Longitude | 133.19761° |
| Altitude | 21,547.642 km |
| Speed | 3.778 km/s |
| Apparent Right ascension | 15h 38m 50s |
| Apparent Declination | -54° 08' 01" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 23:45:39 |
| Azimuth | 229.617° WSW |
| Elevation | -49.127° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 21,545.046 km |
| Perigee altitude | 21,510.9 km |
| Semi-major axis | 27,906.11 km |
| Eccentricity | 0.0006118 |
| Inclination | 54.4132° |
| RAAN | 318.688° |
| Arg. of periapsis | 13.8569° |
| True anomaly | 346.13661° |
| Mean anomaly | 346.1534° |
| Eccentric anomaly | 346.14501° |
| Mean motion | 0.46558 °/min |
| BSTAR | Unknown |
| Orbital period | 773.23 mins |
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Other satellites on launch #78 in the year 2019 (2019-11-23 UTC)
| BEIDOU 3M21, 44793 |
| BEIDOU 3M22, 44794 |
| YZ-1 R/B, 44795 |
| CZ-3B R/B, 44796 |
BEIDOU 3M21 Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 398 mins | 2024-12-27 04:09:10.748Z | 280.329° WNW | 2024-12-27 07:49:10.748Z | 244.291° WSW | 44.903° | 2024-12-27 10:47:10.748Z | 173.76° S |
Authenticating...
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