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). Payloads include a variety of satellites, spacecraft, and rockets 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
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FENGYUN 3G details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 12 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 10 m |
| Radar Cross Section | 15.104 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 12 hours ago
0 FENGYUN 3G
1 56232U 23055A 24288.12871814 .00049615 00000-0 78505-3 0 9992
2 56232 49.9954 257.2205 0023054 195.4688 164.5577 15.52600265 85020Epoch: 2024-10-14T03:05Z
Definitive object data (Epoch: 2024-10-14T03:05:21.247Z)
| Latitude | -0.00001° |
| Longitude | -172.27833° |
| Altitude | 424.782 km |
| Speed | 7.649 km/s |
| True Right ascension | 17h 08m 52s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | 17.32075° |
| Longitude | -159.86746° |
| Altitude | 424.499 km |
| Speed | 7.651 km/s |
| Apparent Right ascension | 19h 43m 23s |
| Apparent Declination | -11° 51' 39" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 10:06:50 |
| Azimuth | 58.504° ENE |
| Elevation | -47.748° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 425.569 km |
| Perigee | 394.27 km |
| Semi-major axis | 6,788.056 km |
| Eccentricity | 0.0023054 |
| Inclination | 49.9954° |
| RAAN | 257.2205° |
| Arg. of periapsis | 195.4688° |
| True anomaly | 164.62785° |
| Mean anomaly | 164.5577° |
| Eccentric anomaly | 164.59279° |
| Mean motion | 3.88083 °/min |
| BSTAR | 0.00078505 |
| Period | 92.76 mins |
No data available
No data available
Other satellites on launch #55 in the year 2023 (2023-04-16 UTC)
| FENGYUN 3G, 56232 |
| CZ-4C R/B, 56233 (Decayed) |
FENGYUN 3G Visibility forecast
Observer location: 39.9160978°, -105.1181434
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 | 2024-10-15 00:53:37.948Z | 224.378° SW | 2024-10-15 00:56:37.948Z | 167.233° S | 41.584° | 2024-10-15 00:59:37.948Z | 62.148° ENE |
| 4 mins | 2024-10-15 07:24:37.948Z | 286.869° WNW | 2024-10-15 07:25:37.948Z | 245.828° WSW | 40.801° | 2024-10-15 07:28:37.948Z | 137.319° SSE |