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, 5.0 m
Radar Cross Section
15.104 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FENGYUN 3G
1 56232U 23055A 25259.99461184 .00028557 00000-0 43006-3 0 9991
2 56232 49.9954 314.7046 0016338 108.6548 251.6196 15.54383632137548Epoch: 2025-09-16T23:52Z
TLE epoch observation values (Epoch: 2025-09-16T23:52:14.462Z)
Latitude
0.00001°
Longitude
-39.53257°
Altitude
408.016 km
Speed
7.665 km/s
True Right ascension
20h 58m 49s
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
11:34:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
415.809 km
Perigee altitude
393.646 km
Semi-major axis
6,782.865 km
Eccentricity
0.00163
Inclination
49.9954°
RAAN
314.7046°
Arg. of periapsis
108.6548°
True anomaly
251.44205°
Mean anomaly
251.6196°
Eccentric anomaly
251.53081°
Mean motion
3.88529 °/min
Orbital period
92.66 mins
BSTAR
0.00043006
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-19 06:03:09.815Z | 227.443° WSW | 2025-09-19 06:06:09.815Z | 155.195° SSE | 43.387° | 2025-09-19 06:09:09.815Z | 59.795° ENE |
| 4 mins | 2025-09-19 12:33:09.815Z | 287.125° WNW | 2025-09-19 12:35:09.815Z | 181.252° SSW | 37.27° | 2025-09-19 12:37:09.815Z | 141.928° SSE |
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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