FENGYUN 4A, 41882
Orbit data source: Space-Track
FENGYUN 4A, 41882 is a payload satellite owned by CNMSC (CN) in GEO that was launched on Sat, 10 Dec 2016 UTC via a CHANG ZHENG 3B launch vehicle from the Xichang Space Center, China (XSC). 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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41882 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-4, LAE?
Mass
5,380 kg wet, ~3,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 5.0 m
Radar Cross Section
24.437 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FENGYUN 4A
1 41882U 16077A 25311.91376016 -.00000352 00000-0 00000-0 0 9990
2 41882 1.7584 82.6928 0005147 153.6673 263.7452 1.00274490 32712Epoch: 2025-11-07T21:55Z
TLE epoch observation values (Epoch: 2025-11-07T21:55:48.877Z)
Latitude
1.46756°
Longitude
123.70111°
Altitude
35,787.524 km
Speed
3.075 km/s
True Right ascension
09h 20m 01s
True Declination
1° 27' 58"
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
21:37:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,808.608 km
Perigee altitude
35,765.203 km
Semi-major axis
42,165.043 km
Eccentricity
0.00051
Inclination
1.7584°
RAAN
82.6928°
Arg. of periapsis
153.6673°
True anomaly
263.68657°
Mean anomaly
263.7452°
Eccentric anomaly
263.71589°
Mean motion
0.25068 °/min
Orbital period
1,436.11 mins
BSTAR
0
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Other satellites on launch #77 in the year 2016 (2016-12-10 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 4A Visibility
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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. |
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| FENGYUN 4A is likely not visible in the next few days. |
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41882 neighbors
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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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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