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: 6 hours ago
TLE from 6 hours ago
0 FENGYUN 3G
1 56232U 23055A 25355.59820326 .00026800 00000-0 40936-3 0 9999
2 56232 49.9916 181.7239 0009317 188.4553 171.6259 15.54132205152404Epoch: 2025-12-21T14:21Z
TLE epoch observation values (Epoch: 2025-12-21T14:21:24.761Z)
Latitude
-0.00004°
Longitude
-124.03766°
Altitude
411.488 km
Speed
7.662 km/s
True Right ascension
12h 06m 53s
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
19:09:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
411.78 km
Perigee altitude
399.139 km
Semi-major axis
6,783.597 km
Eccentricity
0.00093
Inclination
49.9916°
RAAN
181.7239°
Arg. of periapsis
188.4553°
True anomaly
171.64143°
Mean anomaly
171.6259°
Eccentric anomaly
171.63367°
Mean motion
3.88466 °/min
Orbital period
92.67 mins
BSTAR
0.00040936
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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 | 2025-12-21 20:58:30.158Z | 325.45° NNW | 2025-12-21 21:00:30.158Z | 10.728° NNE | 26.052° | 2025-12-21 21:03:30.158Z | 85.992° E |
| 5 mins | 2025-12-22 15:14:30.158Z | 213.98° SW | 2025-12-22 15:16:30.158Z | 142.151° SSE | 39.392° | 2025-12-22 15:19:30.158Z | 63.984° ENE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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