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: 5 hours ago
TLE from 5 hours ago
0 FENGYUN 3D
1 43010U 17072A 26142.28305782 .00000166 00000-0 10026-3 0 9990
2 43010 99.0119 116.2404 0002451 105.0257 255.1190 14.19733304441310Epoch: 2026-05-22T06:47Z
TLE epoch observation values (Epoch: 2026-05-22T06:47:36.195Z)
Latitude
-0.00001°
Longitude
134.42346°
Altitude
829.613 km
Speed
7.438 km/s
True Right ascension
07h 44m 57s
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
21:14:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
825.194 km
Perigee altitude
821.663 km
Semi-major axis
7,201.566 km
Eccentricity
0.00025
Inclination
99.0119°
RAAN
116.2404°
Arg. of periapsis
105.0257°
True anomaly
255.09186°
Mean anomaly
255.119°
Eccentric anomaly
255.10543°
Mean motion
3.55143 °/min
Orbital period
101.37 mins
BSTAR
0.00010026
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-22 12:26:45.476Z | 337.537° N | 2026-05-22 12:29:45.476Z | 299.408° NW | 19.339° | 2026-05-22 12:32:45.476Z | 259.371° W |
| 8 mins | 2026-05-22 22:08:45.476Z | 161.762° S | 2026-05-22 22:12:45.476Z | 8.159° NNE | 44.327° | 2026-05-22 22:16:45.476Z | 347.548° N |
| 8 mins | 2026-05-23 10:27:45.476Z | 42.394° NE | 2026-05-23 10:30:45.476Z | 89.451° E | 29.433° | 2026-05-23 10:35:45.476Z | 161.774° S |
| 7 mins | 2026-05-23 12:07:45.476Z | 344.177° N | 2026-05-23 12:10:45.476Z | 301.391° NW | 26.029° | 2026-05-23 12:14:45.476Z | 241.214° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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