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). 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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43010 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
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
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: 17 hours ago
TLE from 17 hours ago
0 FENGYUN 3D
1 43010U 17072A 25310.23067854 .00000134 00000-0 85276-4 0 9991
2 43010 98.9837 276.0038 0001362 8.1387 351.9810 14.19666345413357Epoch: 2025-11-06T05:32Z
TLE epoch observation values (Epoch: 2025-11-06T05:32:10.625Z)
Latitude
-0.00007°
Longitude
147.26757°
Altitude
828.415 km
Speed
7.439 km/s
True Right ascension
18h 24m 00s
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
18:58:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
824.635 km
Perigee altitude
822.673 km
Semi-major axis
7,201.791 km
Eccentricity
0.00014
Inclination
98.9837°
RAAN
276.0038°
Arg. of periapsis
8.1387°
True anomaly
351.97882°
Mean anomaly
351.981°
Eccentric anomaly
351.97991°
Mean motion
3.55126 °/min
Orbital period
101.37 mins
BSTAR
0.000085276
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Other satellites on launch #72 in the year 2017 (2017-11-14 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 3D 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-07 10:52:57.242Z | 11.264° NNE | 2025-11-07 10:56:57.242Z | 239.84° WSW | 44.519° | 2025-11-07 11:01:57.242Z | 198.676° SSW |
| 6 mins | 2025-11-07 20:36:57.242Z | 94.861° ESE | 2025-11-07 20:38:57.242Z | 66.979° ENE | 19.756° | 2025-11-07 20:42:57.242Z | 17.193° NNE |
| 9 mins | 2025-11-07 22:14:57.242Z | 188.393° SSW | 2025-11-07 22:18:57.242Z | 258.801° W | 37.753° | 2025-11-07 22:23:57.242Z | 334.724° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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