BEIDOU 3M10, 43582
Orbit data source: Space-Track
BEIDOU 3M10, 43582 is a payload satellite owned by CNSA (CN) in MEO that was launched on Sun, 29 Jul 2018 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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43582 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, 5.0 m
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 3M10
1 43582U 18062B 25258.04922265 -.00000012 00000-0 00000-0 0 9995
2 43582 54.0947 191.6486 0005845 21.0621 338.9537 1.86229643 48519Epoch: 2025-09-15T01:10Z
TLE epoch observation values (Epoch: 2025-09-15T01:10:52.836Z)
Latitude
-0°
Longitude
179.66225°
Altitude
21,513.215 km
Speed
3.781 km/s
True Right ascension
12h 46m 34s
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
20:48:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,544.541 km
Perigee altitude
21,511.918 km
Semi-major axis
27,906.366 km
Eccentricity
0.00058
Inclination
54.0947°
RAAN
191.6486°
Arg. of periapsis
21.0621°
True anomaly
338.92963°
Mean anomaly
338.9537°
Eccentric anomaly
338.94167°
Mean motion
0.46557 °/min
Orbital period
773.24 mins
BSTAR
0
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Other satellites on launch #62 in the year 2018 (2018-07-29 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 3M10 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. |
|---|---|---|---|---|---|---|---|
| 336 mins | 2025-09-16 04:54:27.642Z | 305.26° NW | 2025-09-16 07:47:27.642Z | 264.227° W | 41.688° | 2025-09-16 10:30:27.642Z | 196.929° SSW |
| 181 mins | 2025-09-16 16:04:27.642Z | 103.482° ESE | 2025-09-16 17:37:27.642Z | 67.145° ENE | 22.298° | 2025-09-16 19:05:27.642Z | 37.899° 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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