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 25325.22993907 .00035707 00000-0 58734-3 0 9993
2 56232 49.9954 338.2966 0009005 48.7981 311.3761 15.51929077147682Epoch: 2025-11-21T05:31Z
TLE epoch observation values (Epoch: 2025-11-21T05:31:06.735Z)
Latitude
-0.00002°
Longitude
-164.95743°
Altitude
407.616 km
Speed
7.67 km/s
True Right ascension
22h 33m 11s
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
10:55:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
417.99 km
Perigee altitude
405.762 km
Semi-major axis
6,790.013 km
Eccentricity
0.0009
Inclination
49.9954°
RAAN
338.2966°
Arg. of periapsis
48.7981°
True anomaly
311.29861°
Mean anomaly
311.3761°
Eccentric anomaly
311.33736°
Mean motion
3.87916 °/min
Orbital period
92.8 mins
BSTAR
0.00058734
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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 | 2025-11-22 03:19:13.411Z | 201.016° SSW | 2025-11-22 03:22:13.411Z | 127.22° SE | 27.237° | 2025-11-22 03:24:13.411Z | 79.578° E |
| 4 mins | 2025-11-22 04:57:13.411Z | 286.141° WNW | 2025-11-22 04:58:13.411Z | 315.025° NNW | 27.597° | 2025-11-22 05:01:13.411Z | 37.784° NE |
| 5 mins | 2025-11-22 09:49:13.411Z | 313.739° NW | 2025-11-22 09:51:13.411Z | 56.005° ENE | 42.355° | 2025-11-22 09:54:13.411Z | 116.189° SE |
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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