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 25311.27581660 .00040059 00000-0 62220-3 0 9993
2 56232 49.9958 50.3350 0020471 343.0176 17.0104 15.53274241145511Epoch: 2025-11-07T06:37Z
TLE epoch observation values (Epoch: 2025-11-07T06:37:10.554Z)
Latitude
-0.00001°
Longitude
-95.68109°
Altitude
394.455 km
Speed
7.683 km/s
True Right ascension
03h 21m 20s
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
11:01:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
421.848 km
Perigee altitude
394.064 km
Semi-major axis
6,786.093 km
Eccentricity
0.00205
Inclination
49.9958°
RAAN
50.335°
Arg. of periapsis
343.0176°
True anomaly
17.07919°
Mean anomaly
17.0104°
Eccentric anomaly
17.04478°
Mean motion
3.88252 °/min
Orbital period
92.72 mins
BSTAR
0.0006222
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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 | 2025-11-07 16:22:58.265Z | 294.901° NW | 2025-11-07 16:24:58.265Z | 254.571° W | 39.045° | 2025-11-07 16:27:58.265Z | 139.743° SSE |
| 4 mins | 2025-11-08 10:39:58.265Z | 285.684° WNW | 2025-11-08 10:41:58.265Z | 349.803° N | 26.74° | 2025-11-08 10:43:58.265Z | 35.136° NE |
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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