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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Identifier
26460, 2000-032C
Orbit
GEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
China ARMT
Mission
Spacecraft
Bus & Motor
SHANXI AKM, Unknown motor
Mass
729 kg wet, ~50 kg dry
Launch date (UTC)
2000-06-25 (25 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + Cone, 0.8 m
Radar Cross Section
1.571 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 FENGYUN 2B AKM
1 26460U 00032C   25351.20448438  .00000115  00000-0  00000-0 0  9999
2 26460  14.3394   7.6502 0020869  34.3074 325.8236  1.00162527120365
Epoch: 2025-12-17T04:54Z
TLE epoch observation values (Epoch: 2025-12-17T04:54:27.450Z)
Latitude
-0°
Longitude
-152.05653°
Altitude
35,744.194 km
Speed
3.079 km/s
True Right ascension
00h 30m 32s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
03:03:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,906.285 km
Perigee altitude
35,730.166 km
Semi-major axis
42,196.362 km
Eccentricity
0.00209
Inclination
14.3394°
RAAN
7.6502°
Arg. of periapsis
34.3074°
True anomaly
325.68897°
Mean anomaly
325.8236°
Eccentric anomaly
325.75632°
Mean motion
0.2504 °/min
Orbital period
1,437.71 mins
BSTAR
0
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Other satellites on launch #32 in the year 2000 (2000-06-25 UTC)

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