FENGYUN 2E DEB, 40987
Orbit data source: Space-Track
FENGYUN 2E DEB, 40987 is space debris in GEO originally from a launch on Tue, 23 Dec 2008 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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40987 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 FENGYUN 2E DEB
1 40987U 08066D 26058.62600715 .00000055 00000-0 00000-0 0 9996
2 40987 9.9514 45.6569 0178156 15.6248 344.9936 1.00280833 61366Epoch: 2026-02-27T15:01Z
TLE epoch observation values (Epoch: 2026-02-27T15:01:27.017Z)
Latitude
0°
Longitude
22.93755°
Altitude
35,062.303 km
Speed
3.128 km/s
True Right ascension
03h 03m 02s
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
21:25:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,536.246 km
Perigee altitude
35,033.92 km
Semi-major axis
42,163.22 km
Eccentricity
0.01782
Inclination
9.9514°
RAAN
45.6569°
Arg. of periapsis
15.6248°
True anomaly
344.45339°
Mean anomaly
344.9936°
Eccentric anomaly
344.72467°
Mean motion
0.25069 °/min
Orbital period
1,436.02 mins
BSTAR
0
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Other satellites on launch #66 in the year 2008 (2008-12-23 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 2E DEB 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 2E DEB is likely not visible in the next few days. |
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40987 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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