BEIDOU 3M11, 43602
Orbit data source: Space-Track
BEIDOU 3M11, 43602 is a payload satellite owned by CNSA (CN) in MEO that was launched on Fri, 24 Aug 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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43602 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, 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 3M11
1 43602U 18067A 26257.04418277 .00000009 00000-0 00000-0 0 9991
2 43602 54.1783 178.0285 0008838 36.5274 323.5501 1.86227497 54778Epoch: 2026-09-14T01:03Z
TLE epoch observation values (Epoch: 2026-09-14T01:03:37.391Z)
Latitude
0.00003°
Longitude
169.09113°
Altitude
21,508.816 km
Speed
3.782 km/s
True Right ascension
11h 52m 06s
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
01:46:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,553.104 km
Perigee altitude
21,503.777 km
Semi-major axis
27,906.577 km
Eccentricity
0.00088
Inclination
54.1783°
RAAN
178.0285°
Arg. of periapsis
36.5274°
True anomaly
323.48988°
Mean anomaly
323.5501°
Eccentric anomaly
323.51999°
Mean motion
0.46557 °/min
Orbital period
773.25 mins
BSTAR
0
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Other satellites on launch #67 in the year 2018 (2018-08-24 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 3M11 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 | 2026-09-15 09:09:11.568Z | 224.504° SW | 2026-09-15 09:09:11.568Z | 224.504° SW | 32.593° | 2026-09-15 10:14:11.568Z | 208.694° SW |
| 229 mins | 2026-09-15 15:27:11.568Z | 120.911° SE | 2026-09-15 17:24:11.568Z | 74.353° E | 32.897° | 2026-09-15 19:16:11.568Z | 39.061° NE |
| 91 mins | 2026-09-16 07:38:11.568Z | 321.85° NNW | 2026-09-16 09:09:11.568Z | 293.587° NW | 28.283° | 2026-09-16 09:09:11.568Z | 293.587° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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