FENGYUN 2B, 26382
Orbit data source: Space-Track
FENGYUN 2B, 26382 is a payload satellite owned by CNMSC (CN) in GEO that was launched on Sun, 25 Jun 2000 UTC via a CHANG ZHENG 3 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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26382 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SISE
Mission
Non-operational Civil Weather
Bus & Motor
FY-2, SHANXI AKM
Mass
651 kg wet, ~600 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl, 1.5 m
Radar Cross Section
6.680 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FENGYUN 2B
1 26382U 00032A 25348.04975476 -.00000254 00000-0 00000-0 0 9992
2 26382 13.0877 18.2555 0003932 269.2006 270.2919 1.00071185 93079Epoch: 2025-12-14T01:11Z
TLE epoch observation values (Epoch: 2025-12-14T01:11:38.811Z)
Latitude
0.11943°
Longitude
96.84088°
Altitude
35,842.309 km
Speed
3.073 km/s
True Right ascension
13h 10m 53s
True Declination
0° 07' 10"
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
06:37:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,860.515 km
Perigee altitude
35,827.311 km
Semi-major axis
42,222.05 km
Eccentricity
0.00039
Inclination
13.0877°
RAAN
18.2555°
Arg. of periapsis
269.2006°
True anomaly
270.24684°
Mean anomaly
270.2919°
Eccentric anomaly
270.26937°
Mean motion
0.25017 °/min
Orbital period
1,439.02 mins
BSTAR
0
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Other satellites on launch #32 in the year 2000 (2000-06-25 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 2B 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 2B is likely not visible in the next few days. |
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26382 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 descending 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 descending order |
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