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 25359.24690839 -.00000053 00000-0 00000+0 0 9996
2 44794 54.0703 305.9129 0004304 12.6939 347.3266 1.86227898 41411Epoch: 2025-12-25T05:55Z
TLE epoch observation values (Epoch: 2025-12-25T05:55:32.884Z)
Latitude
0.00001°
Longitude
123.00449°
Altitude
21,516.897 km
Speed
3.781 km/s
True Right ascension
20h 23m 35s
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
09:41:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,540.416 km
Perigee altitude
21,516.394 km
Semi-major axis
27,906.542 km
Eccentricity
0.00043
Inclination
54.0703°
RAAN
305.9129°
Arg. of periapsis
12.6939°
True anomaly
347.31577°
Mean anomaly
347.3266°
Eccentric anomaly
347.32119°
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. |
|---|---|---|---|---|---|---|---|
| 101 mins | 2025-12-26 11:22:41.927Z | 319.537° NNW | 2025-12-26 12:12:41.927Z | 301.921° NW | 14.024° | 2025-12-26 13:03:41.927Z | 282.612° WNW |
| 371 mins | 2025-12-26 19:23:41.927Z | 176.672° S | 2025-12-26 22:15:41.927Z | 105.072° ESE | 44.083° | 2025-12-27 01:34:41.927Z | 67.274° ENE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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