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: 8 hours ago
TLE from 8 hours ago
0 FENGYUN 3D
1 43010U 17072A 25325.66540912 .00000122 00000-0 79635-4 0 9994
2 43010 98.9862 291.6632 0000611 311.7572 48.3551 14.19674767415542Epoch: 2025-11-21T15:58Z
TLE epoch observation values (Epoch: 2025-11-21T15:58:11.347Z)
Latitude
-0.00006°
Longitude
-8.78924°
Altitude
829.065 km
Speed
7.439 km/s
True Right ascension
19h 26m 39s
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
21:06:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
824.065 km
Perigee altitude
823.185 km
Semi-major axis
7,201.762 km
Eccentricity
0.00006
Inclination
98.9862°
RAAN
291.6632°
Arg. of periapsis
311.7572°
True anomaly
48.36033°
Mean anomaly
48.3551°
Eccentric anomaly
48.35772°
Mean motion
3.55128 °/min
Orbital period
101.37 mins
BSTAR
0.000079635
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-22 09:30:29.364Z | 61.072° ENE | 2025-11-22 09:33:29.364Z | 98.509° ESE | 15.683° | 2025-11-22 09:35:29.364Z | 122.642° SE |
| 9 mins | 2025-11-22 11:09:29.364Z | 3.398° NNE | 2025-11-22 11:13:29.364Z | 291.56° WNW | 41.009° | 2025-11-22 11:18:29.364Z | 209.866° SW |
| 7 mins | 2025-11-22 20:52:29.364Z | 115.476° SE | 2025-11-22 20:55:29.364Z | 74.048° E | 24.998° | 2025-11-22 20:59:29.364Z | 15.022° NNE |
| 8 mins | 2025-11-22 22:32:29.364Z | 204.444° SW | 2025-11-22 22:35:29.364Z | 251.32° W | 30.535° | 2025-11-22 22:40:29.364Z | 327.073° 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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