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: 1 day ago
TLE from 1 day ago
0 BEIDOU 3M22
1 44794U 19078B 25260.44615037 -.00000051 00000-0 00000-0 0 9995
2 44794 54.1570 309.3808 0002720 22.9955 337.0834 1.86227769 39576Epoch: 2025-09-17T10:42Z
TLE epoch observation values (Epoch: 2025-09-17T10:42:27.391Z)
Latitude
-0.00001°
Longitude
152.16526°
Altitude
21,521.628 km
Speed
3.78 km/s
True Right ascension
20h 37m 36s
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
14:13:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,536.005 km
Perigee altitude
21,520.823 km
Semi-major axis
27,906.551 km
Eccentricity
0.00027
Inclination
54.157°
RAAN
309.3808°
Arg. of periapsis
22.9955°
True anomaly
337.07126°
Mean anomaly
337.0834°
Eccentric anomaly
337.07733°
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. |
|---|---|---|---|---|---|---|---|
| 290 mins | 2025-09-19 00:32:13.003Z | 144.623° SSE | 2025-09-19 02:58:13.003Z | 85.264° E | 36.57° | 2025-09-19 05:22:13.003Z | 44.938° NE |
| 112 mins | 2025-09-19 17:52:13.003Z | 320.19° NNW | 2025-09-19 18:46:13.003Z | 301.272° NW | 14.983° | 2025-09-19 19:44:13.003Z | 279.206° WNW |
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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