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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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 FENGYUN 3G
1 56232U 23055A 25303.87629336 .00047078 00000-0 74482-3 0 9994
2 56232 49.9940 88.4804 0020504 310.8081 49.1107 15.52691061144365Epoch: 2025-10-30T21:01Z
TLE epoch observation values (Epoch: 2025-10-30T21:01:51.746Z)
Latitude
-0.00003°
Longitude
93.58597°
Altitude
400.34 km
Speed
7.677 km/s
True Right ascension
05h 53m 55s
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
00:17:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
423.573 km
Perigee altitude
395.737 km
Semi-major axis
6,787.792 km
Eccentricity
0.00205
Inclination
49.994°
RAAN
88.4804°
Arg. of periapsis
310.8081°
True anomaly
49.28862°
Mean anomaly
49.1107°
Eccentric anomaly
49.19963°
Mean motion
3.88106 °/min
Orbital period
92.76 mins
BSTAR
0.00074482
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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 | 2025-10-31 12:39:48.798Z | 222.511° SW | 2025-10-31 12:42:48.798Z | 109.26° ESE | 40.547° | 2025-10-31 12:44:48.798Z | 64.29° ENE |
| 4 mins | 2025-10-31 14:17:48.798Z | 298.741° NW | 2025-10-31 14:19:48.798Z | 351.163° N | 21.585° | 2025-10-31 14:21:48.798Z | 32.205° NE |
| 5 mins | 2025-10-31 19:09:48.798Z | 292.682° NW | 2025-10-31 19:11:48.798Z | 188.243° SSW | 41.305° | 2025-10-31 19:14:48.798Z | 135.563° SSE |
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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