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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
56232 intel report (Beta)
Focus sentinelFocus sentinel
Edit Public Description
Focus sentinelFocus sentinel
Create New Watchlist
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 26050.50002811 .00027695 00000-0 43495-3 0 9990
2 56232 49.9920 232.8934 0010445 292.5114 67.4748 15.53332589161718Epoch: 2026-02-19T12:00Z
TLE epoch observation values (Epoch: 2026-02-19T12:00:02.428Z)
Latitude
0.00002°
Longitude
-96.56713°
Altitude
404.855 km
Speed
7.671 km/s
True Right ascension
15h 31m 34s
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
00:17:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
414.875 km
Perigee altitude
400.699 km
Semi-major axis
6,785.924 km
Eccentricity
0.00104
Inclination
49.992°
RAAN
232.8934°
Arg. of periapsis
292.5114°
True anomaly
67.58542°
Mean anomaly
67.4748°
Eccentric anomaly
67.5301°
Mean motion
3.88266 °/min
Orbital period
92.72 mins
BSTAR
0.00043495
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #55 in the year 2023 (2023-04-16 UTC)
Did you know?
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
Loading observer location...
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 | 2026-02-19 21:45:31.089Z | 295.408° NW | 2026-02-19 21:48:31.089Z | 209.565° SW | 39.128° | 2026-02-19 21:51:31.089Z | 140.527° SSE |
| 4 mins | 2026-02-20 14:26:31.089Z | 190.559° SSW | 2026-02-20 14:27:31.089Z | 159.029° S | 30.678° | 2026-02-20 14:30:31.089Z | 72.791° E |
| 4 mins | 2026-02-20 16:03:31.089Z | 298.772° NW | 2026-02-20 16:04:31.089Z | 331.317° NNW | 26.572° | 2026-02-20 16:07:31.089Z | 39.502° NE |
| 5 mins | 2026-02-20 20:54:31.089Z | 307.565° NW | 2026-02-20 20:56:31.089Z | 338.927° N | 43.733° | 2026-02-20 20:59:31.089Z | 120.872° SE |
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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|