BEIDOU 3M20, 44865
Orbit data source: Space-Track
BEIDOU 3M20, 44865 is a payload satellite owned by CNSA (CN) in MEO that was launched on Mon, 16 Dec 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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44865 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Defense Navigation
Bus & Motor
BD-3M, 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: 12 hours ago
TLE from 12 hours ago
0 BEIDOU 3M20
1 44865U 19090B 25312.10110218 -.00000026 00000-0 00000+0 0 9991
2 44865 56.3658 70.1440 0013725 298.8284 57.8329 1.86231061 40092Epoch: 2025-11-08T02:25Z
TLE epoch observation values (Epoch: 2025-11-08T02:25:35.228Z)
Latitude
-2.658°
Longitude
-15.56838°
Altitude
21,508.374 km
Speed
3.782 km/s
True Right ascension
04h 33m 27s
True Declination
-2° 39' 14"
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
10:17:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,566.301 km
Perigee altitude
21,489.699 km
Semi-major axis
27,906.137 km
Eccentricity
0.00137
Inclination
56.3658°
RAAN
70.144°
Arg. of periapsis
298.8284°
True anomaly
57.96616°
Mean anomaly
57.8329°
Eccentric anomaly
57.89952°
Mean motion
0.46558 °/min
Orbital period
773.23 mins
BSTAR
0
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Other satellites on launch #90 in the year 2019 (2019-12-16 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 3M20 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. |
|---|---|---|---|---|---|---|---|
| 330 mins | 2025-11-08 17:26:09.067Z | 308.403° NW | 2025-11-08 20:16:09.067Z | 267.447° W | 41.794° | 2025-11-08 22:56:09.067Z | 199.656° SSW |
| 193 mins | 2025-11-09 04:28:09.067Z | 105.982° ESE | 2025-11-09 06:07:09.067Z | 66.317° ENE | 24.47° | 2025-11-09 07:41:09.067Z | 35.078° NE |
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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