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: 9 hours ago
TLE from 9 hours ago
0 FENGYUN 3D
1 43010U 17072A 26052.21521053 -.00000071 00000-0 -11913-4 0 9998
2 43010 99.0004 24.6213 0002285 43.4110 316.7245 14.19708817428536Epoch: 2026-02-21T05:09Z
TLE epoch observation values (Epoch: 2026-02-21T05:09:54.189Z)
Latitude
-0.00005°
Longitude
156.00452°
Altitude
828.044 km
Speed
7.44 km/s
True Right ascension
01h 38m 29s
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
16:47:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
825.156 km
Perigee altitude
821.865 km
Semi-major axis
7,201.648 km
Eccentricity
0.00023
Inclination
99.0004°
RAAN
24.6213°
Arg. of periapsis
43.411°
True anomaly
316.70655°
Mean anomaly
316.7245°
Eccentric anomaly
316.71552°
Mean motion
3.55137 °/min
Orbital period
101.37 mins
BSTAR
-0.000011913
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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 | 2026-02-21 20:34:01.760Z | 89.555° E | 2026-02-21 20:36:01.760Z | 65.897° ENE | 14.98° | 2026-02-21 20:39:01.760Z | 29.703° NE |
| 9 mins | 2026-02-21 22:12:01.760Z | 175.335° S | 2026-02-21 22:16:01.760Z | 260.557° W | 43.393° | 2026-02-21 22:21:01.760Z | 341.167° N |
| 8 mins | 2026-02-22 10:31:01.760Z | 31.984° NE | 2026-02-22 10:35:01.760Z | 108.575° ESE | 36.4° | 2026-02-22 10:39:01.760Z | 170.479° S |
| 6 mins | 2026-02-22 12:12:01.760Z | 332.601° NNW | 2026-02-22 12:15:01.760Z | 289.447° WNW | 20.572° | 2026-02-22 12:18:01.760Z | 251.89° W |
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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