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: 9 hours ago
TLE from 9 hours ago
0 FENGYUN 3D
1 43010U 17072A 25260.33153056 .00000081 00000-0 60070-4 0 9992
2 43010 98.9733 225.4089 0002521 98.1454 262.0007 14.19642470406274Epoch: 2025-09-17T07:57Z
TLE epoch observation values (Epoch: 2025-09-17T07:57:24.24Z)
Latitude
-0.00006°
Longitude
109.5489°
Altitude
829.721 km
Speed
7.438 km/s
True Right ascension
15h 01m 38s
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
10:05:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
825.55 km
Perigee altitude
821.918 km
Semi-major axis
7,201.871 km
Eccentricity
0.00025
Inclination
98.9733°
RAAN
225.4089°
Arg. of periapsis
98.1454°
True anomaly
261.97209°
Mean anomaly
262.0007°
Eccentric anomaly
261.9864°
Mean motion
3.5512 °/min
Orbital period
101.37 mins
BSTAR
0.00006007
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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 | 2025-09-17 21:37:21.510Z | 159.64° S | 2025-09-17 21:40:21.510Z | 132.818° SE | 43.944° | 2025-09-17 21:45:21.510Z | 348.505° N |
| 7 mins | 2025-09-18 09:56:21.510Z | 44.63° NE | 2025-09-18 09:59:21.510Z | 93.386° ESE | 28.829° | 2025-09-18 10:03:21.510Z | 155.402° SSE |
| 7 mins | 2025-09-18 11:36:21.510Z | 343.493° N | 2025-09-18 11:39:21.510Z | 298.418° NW | 26.819° | 2025-09-18 11:43:21.510Z | 239.047° WSW |
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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