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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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: 3 hours ago
TLE from 3 hours ago
0 FENGYUN 3D
1 43010U 17072A 26306.55864266 .00000317 00000-0 17160-3 0 9993
2 43010 99.0332 283.6072 0002123 40.2858 319.8475 14.19765664464627Epoch: 2026-11-02T13:24Z
TLE epoch observation values (Epoch: 2026-11-02T13:24:26.725Z)
Latitude
0.00003°
Longitude
40.66191°
Altitude
827.88 km
Speed
7.44 km/s
True Right ascension
18h 54m 25s
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
12:27:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
824.849 km
Perigee altitude
821.791 km
Semi-major axis
7,201.457 km
Eccentricity
0.00021
Inclination
99.0332°
RAAN
283.6072°
Arg. of periapsis
40.2858°
True anomaly
319.83181°
Mean anomaly
319.8475°
Eccentric anomaly
319.83966°
Mean motion
3.55151 °/min
Orbital period
101.37 mins
BSTAR
0.0001716
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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 | 2026-11-02 21:59:27.343Z | 137.876° SSE | 2026-11-02 22:03:27.343Z | 79.745° E | 44.767° | 2026-11-02 22:08:27.343Z | 0.256° NNE |
| 6 mins | 2026-11-02 23:41:27.343Z | 228.451° WSW | 2026-11-02 23:44:27.343Z | 271.585° WNW | 22.129° | 2026-11-02 23:47:27.343Z | 310.046° NW |
| 5 mins | 2026-11-03 10:20:27.343Z | 69.643° E | 2026-11-03 10:22:27.343Z | 97.098° ESE | 18.374° | 2026-11-03 10:25:27.343Z | 133.02° SE |
| 9 mins | 2026-11-03 11:58:27.343Z | 1.406° NNE | 2026-11-03 12:02:27.343Z | 296.273° NW | 54.343° | 2026-11-03 12:07:27.343Z | 213.699° 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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