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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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: 15 hours ago
TLE from 15 hours ago
0 BEIDOU 3M10
1 43582U 18062B 26256.03169091 .00000005 00000-0 00000-0 0 9994
2 43582 54.0825 179.3081 0006493 29.0996 330.9452 1.86227960 55270Epoch: 2026-09-13T00:45Z
TLE epoch observation values (Epoch: 2026-09-13T00:45:38.094Z)
Latitude
0.00002°
Longitude
175.86445°
Altitude
21,512.764 km
Speed
3.782 km/s
True Right ascension
11h 57m 13s
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
08:09:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,546.518 km
Perigee altitude
21,510.278 km
Semi-major axis
27,906.535 km
Eccentricity
0.00065
Inclination
54.0825°
RAAN
179.3081°
Arg. of periapsis
29.0996°
True anomaly
330.90904°
Mean anomaly
330.9452°
Eccentric anomaly
330.92712°
Mean motion
0.46557 °/min
Orbital period
773.25 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. |
|---|---|---|---|---|---|---|---|
| 327 mins | 2026-09-14 04:35:55.382Z | 307.951° NW | 2026-09-14 07:22:55.382Z | 266.627° W | 59.317° | 2026-09-14 10:02:55.382Z | 200.977° SSW |
| 12 mins | 2026-09-14 15:26:55.382Z | 110.217° ESE | 2026-09-14 15:38:55.382Z | 106.366° ESE | 13.426° | 2026-09-14 15:38:55.382Z | 106.366° ESE |
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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