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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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: 12 hours ago
TLE from 12 hours ago
0 FENGYUN 2B
1 26382U 00032A 26074.00244358 .00000123 00000-0 00000-0 0 9997
2 26382 13.1794 17.5971 0004061 296.1047 250.6800 1.00085518 93986Epoch: 2026-03-15T00:03Z
TLE epoch observation values (Epoch: 2026-03-15T00:03:31.125Z)
Latitude
-1.53171°
Longitude
30.68°
Altitude
35,844.413 km
Speed
3.072 km/s
True Right ascension
13h 36m 42s
True Declination
-1° 31' 49"
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
16:26:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,857.026 km
Perigee altitude
35,822.736 km
Semi-major axis
42,218.018 km
Eccentricity
0.00041
Inclination
13.1794°
RAAN
17.5971°
Arg. of periapsis
296.1047°
True anomaly
250.63609°
Mean anomaly
250.68°
Eccentric anomaly
250.65805°
Mean motion
0.25021 °/min
Orbital period
1,438.82 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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