BEIDOU 3M22, 44794
Orbit data source: Space-Track
BEIDOU 3M22, 44794 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). Payload-class satellites include a variety of spacecraft 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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44794 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
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
Shape & HBR
Box + 2 Pan, Unknown HBR
Radar Cross Section
8.984 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 BEIDOU 3M22
1 44794U 19078B 25258.29830132 -.00000051 00000-0 00000-0 0 9990
2 44794 54.1589 309.4562 0002724 22.8239 337.2513 1.86227689 39535Epoch: 2025-09-15T07:09Z
TLE epoch observation values (Epoch: 2025-09-15T07:09:33.234Z)
Latitude
-0.00005°
Longitude
-152.41951°
Altitude
21,521.619 km
Speed
3.78 km/s
True Right ascension
20h 37m 53s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
19:55:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,536.024 km
Perigee altitude
21,520.82 km
Semi-major axis
27,906.559 km
Eccentricity
0.00027
Inclination
54.1589°
RAAN
309.4562°
Arg. of periapsis
22.8239°
True anomaly
337.23923°
Mean anomaly
337.2513°
Eccentric anomaly
337.24526°
Mean motion
0.46557 °/min
Orbital period
773.25 mins
BSTAR
0
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Other satellites on launch #78 in the year 2019 (2019-11-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.BEIDOU 3M22 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 251 mins | 2025-09-18 15:13:29.448Z | 319.48° NNW | 2025-09-18 17:16:29.448Z | 282.044° WNW | 31.327° | 2025-09-18 19:24:29.448Z | 230.957° WSW |
| 153 mins | 2025-09-19 00:33:29.448Z | 144.324° SSE | 2025-09-19 02:58:29.448Z | 85.092° E | 36.57° | 2025-09-19 03:06:29.448Z | 80.038° E |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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