FENGYUN 2D DEB, 33458
Orbit data source: Space-Track
FENGYUN 2D DEB, 33458 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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33458 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FENGYUN 2D DEB
1 33458U 06053D 25342.65298454 -.00000090 00000-0 00000-0 0 9996
2 33458 11.3221 38.7522 0021505 345.6907 2.5696 1.00244190 63467Epoch: 2025-12-08T15:40Z
TLE epoch observation values (Epoch: 2025-12-08T15:40:17.864Z)
Latitude
-2.28445°
Longitude
74.52064°
Altitude
35,703.744 km
Speed
3.081 km/s
True Right ascension
01h 48m 58s
True Declination
-2° 16' 56"
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
19:54:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,886.037 km
Perigee altitude
35,704.648 km
Semi-major axis
42,173.479 km
Eccentricity
0.00215
Inclination
11.3221°
RAAN
38.7522°
Arg. of periapsis
345.6907°
True anomaly
2.58068°
Mean anomaly
2.5696°
Eccentric anomaly
2.57514°
Mean motion
0.2506 °/min
Orbital period
1,436.54 mins
BSTAR
0
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Other satellites on launch #53 in the year 2006 (2006-12-08 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 2D 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 2D DEB is likely not visible in the next few days. |
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33458 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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