FENGYUN 2G AKM, 40369
Orbit data source: Space-Track
FENGYUN 2G AKM, 40369 is space debris in GEO originally from a launch on Wed, 31 Dec 2014 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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40369 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 FENGYUN 2G AKM
1 40369U 14090C 26061.40865723 -.00000328 00000-0 00000+0 0 9999
2 40369 7.2883 69.9033 0047987 172.3861 187.8726 0.99588215 40577Epoch: 2026-03-02T09:48Z
TLE epoch observation values (Epoch: 2026-03-02T09:48:27.984Z)
Latitude
0°
Longitude
122.79038°
Altitude
36,179.064 km
Speed
3.053 km/s
True Right ascension
04h 40m 26s
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
07:36:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,183.626 km
Perigee altitude
35,777.095 km
Semi-major axis
42,358.497 km
Eccentricity
0.0048
Inclination
7.2883°
RAAN
69.9033°
Arg. of periapsis
172.3861°
True anomaly
187.79773°
Mean anomaly
187.8726°
Eccentric anomaly
187.83512°
Mean motion
0.24896 °/min
Orbital period
1,446.01 mins
BSTAR
0
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Other satellites on launch #90 in the year 2014 (2014-12-31 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 2G AKM 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 2G AKM is likely not visible in the next few days. |
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40369 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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