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: 12 hours ago
TLE from 12 hours ago
0 FENGYUN 3G
1 56232U 23055A 26042.90817036 .00030624 00000-0 48785-3 0 9991
2 56232 49.9932 272.0413 0010192 260.4081 99.5735 15.52886106160534Epoch: 2026-02-11T21:47Z
TLE epoch observation values (Epoch: 2026-02-11T21:47:45.919Z)
Latitude
0.00002°
Longitude
163.13245°
Altitude
410.022 km
Speed
7.666 km/s
True Right ascension
18h 08m 09s
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
12:01:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
416.005 km
Perigee altitude
402.169 km
Semi-major axis
6,787.224 km
Eccentricity
0.00102
Inclination
49.9932°
RAAN
272.0413°
Arg. of periapsis
260.4081°
True anomaly
99.68864°
Mean anomaly
99.5735°
Eccentric anomaly
99.63107°
Mean motion
3.88155 °/min
Orbital period
92.75 mins
BSTAR
0.00048785
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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 | 2026-02-12 18:04:12.470Z | 224.866° SW | 2026-02-12 18:06:12.470Z | 183.099° SSW | 42.276° | 2026-02-12 18:09:12.470Z | 60.584° ENE |
| 4 mins | 2026-02-12 22:57:12.470Z | 343.343° N | 2026-02-12 22:58:12.470Z | 9.142° NNE | 22.312° | 2026-02-12 23:01:12.470Z | 76.864° E |
| 4 mins | 2026-02-13 00:34:12.470Z | 283.002° WNW | 2026-02-13 00:35:12.470Z | 242.207° WSW | 39.344° | 2026-02-13 00:38:12.470Z | 140.425° 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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