FENGYUN 3D, 43010
Orbit data source: Space-Track
FENGYUN 3D, 43010 is a payload satellite owned by CNMSC (CN) in SSO that was launched on Tue, 14 Nov 2017 UTC via a CHANG ZHENG 4C launch vehicle from the Taiyaun Space Center, China (TSC). 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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43010 intel report (Beta)
FENGYUN 3D details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 9 hours ago |
| Origin | |
| Manufacturer | SISE |
| Mission | Operational Civil Weather |
| Bus & Motor | FY-3, Unknown motor |
| Mass | 2,450 kg wet, 2,250 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 9 hours ago
0 FENGYUN 3D
1 43010U 17072A 24361.10942619 .00000316 00000-0 17140-3 0 9999
2 43010 98.9390 317.1573 0002148 123.3967 236.7414 14.19527601368641Epoch: 2024-12-26T02:37Z
Definitive object data (Epoch: 2024-12-26T02:37:34.422Z)
| Latitude | -0.00006° |
| Longitude | -177.32965° |
| Altitude | 830.706 km |
| Speed | 7.437 km/s |
| True Right ascension | 21h 08m 37s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -9.8292° |
| Longitude | 1.51003° |
| Altitude | 831.064 km |
| Speed | 7.437 km/s |
| Apparent Right ascension | 06h 16m 00s |
| Apparent Declination | -52° 17' 16" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 11:19:57 |
| Azimuth | 220.221° SW |
| Elevation | -23.205° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 825.668 km |
| Perigee altitude | 822.574 km |
| Semi-major axis | 7,202.258 km |
| Eccentricity | 0.0002148 |
| Inclination | 98.939° |
| RAAN | 317.1573° |
| Arg. of periapsis | 123.3967° |
| True anomaly | 236.72082° |
| Mean anomaly | 236.7414° |
| Eccentric anomaly | 236.73111° |
| Mean motion | 3.55091 °/min |
| BSTAR | 0.0001714 |
| Orbital period | 101.38 mins |
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Other satellites on launch #72 in the year 2017 (2017-11-14 UTC)
| FENGYUN 3D, 43010 |
| HEAD-1, 43011 |
| CZ-4C R/B, 43012 |
| CZ-4C DEB, 44613 |
| CZ-4C DEB, 44614 |
FENGYUN 3D Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-26 19:43:31.732Z | 86.72° E | 2024-12-26 19:45:31.732Z | 63.879° ENE | 13.641° | 2024-12-26 19:47:31.732Z | 39.759° NE |
| 9 mins | 2024-12-26 21:21:31.732Z | 171.002° S | 2024-12-26 21:25:31.732Z | 281.736° WNW | 44.359° | 2024-12-26 21:30:31.732Z | 343.53° N |
| 8 mins | 2024-12-27 09:40:31.732Z | 34.636° NE | 2024-12-27 09:44:31.732Z | 108.392° ESE | 34.214° | 2024-12-27 09:48:31.732Z | 167.144° S |
| 6 mins | 2024-12-27 11:21:31.732Z | 333.807° NNW | 2024-12-27 11:24:31.732Z | 288.634° WNW | 22.148° | 2024-12-27 11:27:31.732Z | 249.444° W |
Authenticating...
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