FENGYUN 2D AKM, 29642
Orbit data source: Space-Track
FENGYUN 2D AKM, 29642 is space debris in GEO originally from a launch on Fri, 08 Dec 2006 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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29642 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 FENGYUN 2D AKM
1 29642U 06053C 25241.07232906 .00000028 00000-0 00000-0 0 9990
2 29642 11.2693 40.1965 0107741 41.2515 148.3773 0.99353828 43355
Epoch: 2025-08-29T01:44Z
TLE epoch observation values (Epoch: 2025-08-29T01:44:09.23Z)
Latitude
-1.98361°
Longitude
-133.29962°
Altitude
36,434.164 km
Speed
3.037 km/s
True Right ascension
15h 21m 03s
True Declination
-1° 58' 54"
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
14:15:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,504.008 km
Perigee altitude
35,589.824 km
Semi-major axis
42,425.053 km
Eccentricity
0.01077
Inclination
11.2693°
RAAN
40.1965°
Arg. of periapsis
41.2515°
True anomaly
149.01728°
Mean anomaly
148.3773°
Eccentric anomaly
148.69802°
Mean motion
0.24838 °/min
Orbital period
1,449.42 mins
BSTAR
0
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Other satellites on launch #53 in the year 2006 (2006-12-08 UTC)
FENGYUN 2D AKM Visibility forecast
Observer location: undefined°, undefined°
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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1440 mins | 2025-08-29 22:42:37.068Z | 226.788° WSW | 2025-08-30 19:42:37.068Z | 235.013° WSW | 34.043° | 2025-08-30 22:42:37.068Z | 230.954° WSW |
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29642 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
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