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: 2 days ago
TLE from 2 days ago
0 BEIDOU 3M10
1 43582U 18062B 25288.11867049 -.00000040 00000-0 00000-0 0 9995
2 43582 54.0908 190.6268 0006633 32.2708 327.8130 1.86229764 49071Epoch: 2025-10-15T02:50Z
TLE epoch observation values (Epoch: 2025-10-15T02:50:53.130Z)
Latitude
0.00006°
Longitude
124.00827°
Altitude
21,512.762 km
Speed
3.782 km/s
True Right ascension
12h 42m 30s
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
16:04:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,546.728 km
Perigee altitude
21,509.707 km
Semi-major axis
27,906.354 km
Eccentricity
0.00066
Inclination
54.0908°
RAAN
190.6268°
Arg. of periapsis
32.2708°
True anomaly
327.77248°
Mean anomaly
327.813°
Eccentric anomaly
327.79274°
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. |
|---|---|---|---|---|---|---|---|
| 65 mins | 2025-10-16 21:22:30.976Z | 53.38° ENE | 2025-10-16 21:22:30.976Z | 53.38° ENE | 27.204° | 2025-10-16 22:27:30.976Z | 66.152° ENE |
| 187 mins | 2025-10-17 18:15:30.976Z | 202.653° SW | 2025-10-17 21:22:30.976Z | 305.826° NW | 44.642° | 2025-10-17 21:22:30.976Z | 305.826° NW |
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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