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: 14 hours ago
TLE from 14 hours ago
0 FENGYUN 3D
1 43010U 17072A 25261.31824568 .00000089 00000-0 63931-4 0 9991
2 43010 98.9736 226.4088 0002534 96.4395 263.7069 14.19642777406418Epoch: 2025-09-18T07:38Z
TLE epoch observation values (Epoch: 2025-09-18T07:38:16.426Z)
Latitude
-0.00004°
Longitude
114.3588°
Altitude
829.667 km
Speed
7.438 km/s
True Right ascension
15h 05m 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
14:26:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
825.558 km
Perigee altitude
821.908 km
Semi-major axis
7,201.87 km
Eccentricity
0.00025
Inclination
98.9736°
RAAN
226.4088°
Arg. of periapsis
96.4395°
True anomaly
263.67804°
Mean anomaly
263.7069°
Eccentric anomaly
263.69247°
Mean motion
3.5512 °/min
Orbital period
101.37 mins
BSTAR
0.000063931
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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 | 2025-09-18 22:59:49.888Z | 233.87° WSW | 2025-09-18 23:02:49.888Z | 272.781° WNW | 17.165° | 2025-09-18 23:05:49.888Z | 308.048° NW |
| 6 mins | 2025-09-19 09:37:49.888Z | 56.376° ENE | 2025-09-19 09:40:49.888Z | 99.695° ESE | 20.895° | 2025-09-19 09:43:49.888Z | 138.746° SSE |
| 9 mins | 2025-09-19 11:16:49.888Z | 356.314° N | 2025-09-19 11:20:49.888Z | 290.722° WNW | 34.975° | 2025-09-19 11:25:49.888Z | 219.815° SW |
| 8 mins | 2025-09-19 20:59:49.888Z | 125° SE | 2025-09-19 21:02:49.888Z | 77.255° E | 30.964° | 2025-09-19 21:07:49.888Z | 3.735° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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