FENGYUN 2F AKM, 38072
Orbit data source: Space-Track
FENGYUN 2F AKM, 38072 is space debris in GEO originally from a launch on Fri, 13 Jan 2012 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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38072 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 FENGYUN 2F AKM
1 38072U 12002C 26133.70279596 -.00000295 00000-0 00000-0 0 9992
2 38072 9.0885 58.1433 0061841 206.7910 348.7998 0.99397319 51498Epoch: 2026-05-13T16:52Z
TLE epoch observation values (Epoch: 2026-05-13T16:52:01.570Z)
Latitude
-2.42902°
Longitude
128.94453°
Altitude
35,775.585 km
Speed
3.084 km/s
True Right ascension
16h 53m 38s
True Declination
-2° 25' 36"
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
16:29:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,296.845 km
Perigee altitude
35,772.276 km
Semi-major axis
42,412.698 km
Eccentricity
0.00618
Inclination
9.0885°
RAAN
58.1433°
Arg. of periapsis
206.791°
True anomaly
348.6611°
Mean anomaly
348.7998°
Eccentric anomaly
348.73056°
Mean motion
0.24848 °/min
Orbital period
1,448.78 mins
BSTAR
0
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Other satellites on launch #2 in the year 2012 (2012-01-13 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 2F 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 2F AKM is likely not visible in the next few days. |
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38072 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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