FENGYUN 2B AKM, 26460
Orbit data source: Space-Track
FENGYUN 2B AKM, 26460 is space debris in GEO originally from a launch on Sun, 25 Jun 2000 UTC launched from the Xichang Space Center, China (XSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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26460 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
China ARMT
Mission
Spacecraft
Bus & Motor
SHANXI AKM, Unknown motor
Mass
729 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + Cone, 0.8 m
Radar Cross Section
1.571 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 FENGYUN 2B AKM
1 26460U 00032C 25258.34297425 -.00000077 00000-0 00000-0 0 9996
2 26460 14.2932 8.3438 0021246 40.1023 320.0781 1.00135116119439Epoch: 2025-09-15T08:13Z
TLE epoch observation values (Epoch: 2025-09-15T08:13:52.975Z)
Latitude
0°
Longitude
-109.66442°
Altitude
35,755.764 km
Speed
3.078 km/s
True Right ascension
00h 33m 25s
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
15:49:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,915.593 km
Perigee altitude
35,736.259 km
Semi-major axis
42,204.063 km
Eccentricity
0.00212
Inclination
14.2932°
RAAN
8.3438°
Arg. of periapsis
40.1023°
True anomaly
319.92154°
Mean anomaly
320.0781°
Eccentric anomaly
319.99985°
Mean motion
0.25033 °/min
Orbital period
1,438.11 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 AKM 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-09-15 23:09:43.129Z | 187.206° SSW | 2025-09-16 14:16:43.129Z | 190.584° SSW | 40.795° | 2025-09-16 23:09:43.129Z | 187.827° SSW |
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26460 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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