BEIDOU 3G1, 43683
Orbit data source: Space-Track
BEIDOU 3G1, 43683 is a payload satellite owned by CNSA (CN) in GEO that was launched on Thu, 01 Nov 2018 UTC via a CHANG ZHENG 3B 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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43683 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Defense Navigation
Bus & Motor
DFH-3B, FY-25
Mass
~3,060 kg wet, 1,700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 9.0 m
Radar Cross Section
13.998 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 BEIDOU 3G1
1 43683U 18085A 25302.92695174 -.00000265 00000-0 00000-0 0 9995
2 43683 2.4937 104.4318 0002820 46.8732 0.9148 1.00278812 25754Epoch: 2025-10-29T22:14Z
TLE epoch observation values (Epoch: 2025-10-29T22:14:48.630Z)
Latitude
1.82956°
Longitude
139.96115°
Altitude
35,772.039 km
Speed
3.076 km/s
True Right ascension
10h 08m 37s
True Declination
1° 49' 40"
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
14:24:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,797.583 km
Perigee altitude
35,773.802 km
Semi-major axis
42,163.83 km
Eccentricity
0.00028
Inclination
2.4937°
RAAN
104.4318°
Arg. of periapsis
46.8732°
True anomaly
0.91532°
Mean anomaly
0.9148°
Eccentric anomaly
0.91506°
Mean motion
0.25069 °/min
Orbital period
1,436.05 mins
BSTAR
0
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Other satellites on launch #85 in the year 2018 (2018-11-01 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 3G1 Visibility
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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. |
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| BEIDOU 3G1 is likely not visible in the next few days. |
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43683 neighbors
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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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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