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: 9 hours ago
TLE from 9 hours ago
0 FENGYUN 3G
1 56232U 23055A 26140.51219608 .00018860 00000-0 29871-3 0 9991
2 56232 49.9915 128.8018 0005789 68.8262 291.3324 15.53386886175703Epoch: 2026-05-20T12:17Z
TLE epoch observation values (Epoch: 2026-05-20T12:17:33.741Z)
Latitude
0.00003°
Longitude
66.24055°
Altitude
405.979 km
Speed
7.669 km/s
True Right ascension
08h 35m 12s
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
05:51:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
411.557 km
Perigee altitude
403.701 km
Semi-major axis
6,785.766 km
Eccentricity
0.00058
Inclination
49.9915°
RAAN
128.8018°
Arg. of periapsis
68.8262°
True anomaly
291.27059°
Mean anomaly
291.3324°
Eccentric anomaly
291.3015°
Mean motion
3.8828 °/min
Orbital period
92.72 mins
BSTAR
0.00029871
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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 | 2026-05-21 02:23:32.331Z | 234.357° WSW | 2026-05-21 02:25:32.331Z | 231.158° WSW | 43.996° | 2026-05-21 02:28:32.331Z | 55.954° ENE |
| 4 mins | 2026-05-21 07:16:32.331Z | 344.098° N | 2026-05-21 07:17:32.331Z | 12.998° NNE | 24.347° | 2026-05-21 07:20:32.331Z | 82.853° E |
| 5 mins | 2026-05-21 08:52:32.331Z | 285.457° WNW | 2026-05-21 08:54:32.331Z | 222.23° SW | 34.837° | 2026-05-21 08:57:32.331Z | 147.069° 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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