FENGYUN 3G, 56232
Orbit data source: Space-Track
FENGYUN 3G, 56232 is a payload satellite owned by CNMSC (CN) in LEO that was launched on Sun, 16 Apr 2023 UTC via a CHANG ZHENG 4B launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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56232 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SISE
Mission
Operational Civil Weather
Bus & Motor
SAST-3000, Unknown motor
Mass
3,850 kg wet, 3,110 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 6.8 m
Radar Cross Section
27.688 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 FENGYUN 3G
1 56232U 23055A 26133.17836701 .00015514 00000-0 24933-3 0 9991
2 56232 49.9917 166.6274 0006005 34.5952 325.5405 15.53138629174560Epoch: 2026-05-13T04:16Z
TLE epoch observation values (Epoch: 2026-05-13T04:16:50.909Z)
Latitude
-0.00003°
Longitude
-128.52686°
Altitude
404.77 km
Speed
7.671 km/s
True Right ascension
11h 06m 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
18:19:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
412.427 km
Perigee altitude
404.276 km
Semi-major axis
6,786.489 km
Eccentricity
0.0006
Inclination
49.9917°
RAAN
166.6274°
Arg. of periapsis
34.5952°
True anomaly
325.50154°
Mean anomaly
325.5405°
Eccentric anomaly
325.52102°
Mean motion
3.88218 °/min
Orbital period
92.73 mins
BSTAR
0.00024933
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Other satellites on launch #55 in the year 2023 (2023-04-16 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.FENGYUN 3G 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-13 10:54:36.733Z | 318.093° NNW | 2026-05-13 10:57:36.733Z | 42.443° NE | 32.212° | 2026-05-13 10:59:36.733Z | 93.341° ESE |
| 5 mins | 2026-05-14 05:11:36.733Z | 233.124° WSW | 2026-05-14 05:13:36.733Z | 182.16° SSW | 44.924° | 2026-05-14 05:16:36.733Z | 56.442° ENE |
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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