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: 7 hours ago
TLE from 7 hours ago
0 FENGYUN 3G
1 56232U 23055A 26313.19103449 .00029583 00000-0 45875-3 0 9998
2 56232 49.9925 318.3542 0009265 329.3907 30.6519 15.53659994202542Epoch: 2026-11-09T04:35Z
TLE epoch observation values (Epoch: 2026-11-09T04:35:05.379Z)
Latitude
-0.00004°
Longitude
-158.78937°
Altitude
401.205 km
Speed
7.674 km/s
True Right ascension
21h 13m 25s
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
08:14:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
413.12 km
Perigee altitude
400.547 km
Semi-major axis
6,784.971 km
Eccentricity
0.00093
Inclination
49.9925°
RAAN
318.3542°
Arg. of periapsis
329.3907°
True anomaly
30.70608°
Mean anomaly
30.6519°
Eccentric anomaly
30.67899°
Mean motion
3.88348 °/min
Orbital period
92.7 mins
BSTAR
0.00045875
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-10 02:21:28.006Z | 175.582° S | 2026-11-10 02:23:28.006Z | 134.926° SE | 17.984° | 2026-11-10 02:25:28.006Z | 93.456° ESE |
| 4 mins | 2026-11-10 03:58:28.006Z | 265.422° W | 2026-11-10 03:59:28.006Z | 297.885° NW | 47.698° | 2026-11-10 04:02:28.006Z | 44.894° NE |
| 4 mins | 2026-11-10 08:50:28.006Z | 332.264° NNW | 2026-11-10 08:52:28.006Z | 50.331° ENE | 37.391° | 2026-11-10 08:54:28.006Z | 94.293° ESE |
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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