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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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, 1.6 m
Radar Cross Section
8.984 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 BEIDOU 3M22
1 44794U 19078B 26274.00336417 -.00000013 00000-0 00000-0 0 9993
2 44794 53.8109 296.0536 0002773 25.9353 334.1182 1.86227801 46628Epoch: 2026-10-01T00:04Z
TLE epoch observation values (Epoch: 2026-10-01T00:04:50.664Z)
Latitude
0.00004°
Longitude
-74.89201°
Altitude
21,521.658 km
Speed
3.78 km/s
True Right ascension
19h 44m 15s
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
08:37:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,536.163 km
Perigee altitude
21,520.686 km
Semi-major axis
27,906.561 km
Eccentricity
0.00028
Inclination
53.8109°
RAAN
296.0536°
Arg. of periapsis
25.9353°
True anomaly
334.10432°
Mean anomaly
334.1182°
Eccentric anomaly
334.11126°
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. |
|---|---|---|---|---|---|---|---|
| 59 mins | 2026-10-01 16:55:51.818Z | 315.468° NNW | 2026-10-01 17:24:51.818Z | 305.098° NW | 11.503° | 2026-10-01 17:54:51.818Z | 293.923° NW |
| 383 mins | 2026-10-02 00:38:51.818Z | 180.828° SSW | 2026-10-02 03:33:51.818Z | 109.121° ESE | 79.17° | 2026-10-02 07:01:51.818Z | 72.333° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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