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: 6 hours ago
TLE from 6 hours ago
0 FENGYUN 3D
1 43010U 17072A 25357.30990396 .00000404 00000-0 21291-3 0 9992
2 43010 98.9907 323.7786 0001433 151.7224 208.4030 14.19688251420032Epoch: 2025-12-23T07:26Z
TLE epoch observation values (Epoch: 2025-12-23T07:26:15.702Z)
Latitude
0.00005°
Longitude
120.11768°
Altitude
830.221 km
Speed
7.437 km/s
True Right ascension
21h 35m 06s
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
12:42:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
824.612 km
Perigee altitude
822.548 km
Semi-major axis
7,201.717 km
Eccentricity
0.00014
Inclination
98.9907°
RAAN
323.7786°
Arg. of periapsis
151.7224°
True anomaly
208.39519°
Mean anomaly
208.403°
Eccentric anomaly
208.3991°
Mean motion
3.55131 °/min
Orbital period
101.37 mins
BSTAR
0.00021291
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-23 21:06:10.644Z | 128.001° SE | 2025-12-23 21:10:10.644Z | 71.825° E | 29.591° | 2025-12-23 21:14:10.644Z | 9.661° NNE |
| 7 mins | 2025-12-23 22:47:10.644Z | 213.245° SW | 2025-12-23 22:50:10.644Z | 257.023° W | 25.89° | 2025-12-23 22:54:10.644Z | 316.958° NNW |
| 9 mins | 2025-12-24 11:05:10.644Z | 7.545° NNE | 2025-12-24 11:09:10.644Z | 286.81° WNW | 43.525° | 2025-12-24 11:14:10.644Z | 203.879° SW |
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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