CZ-2D DEB, 35272 (Decayed)
Orbit data source: Space-Track
CZ-2D DEB, 35272 was space debris in LEO originally from a launch on Tue, 05 Jul 2005 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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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35272 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 CZ-2D DEB
1 35272U 05024L 26146.33357357 .01156223 22843-5 69454-3 0 9990
2 35272 97.1603 185.0172 0009225 211.3999 148.6740 16.18313523136073Epoch: 2026-05-26T08:00Z
TLE epoch observation values (Epoch: 2026-05-26T08:00:20.756Z)
Latitude
-0.00002°
Longitude
-178.97779°
Altitude
232.57 km
Speed
7.764 km/s
True Right ascension
12h 20m 04s
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
02:14:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
227.048 km
Perigee altitude
214.872 km
Semi-major axis
6,599.097 km
Eccentricity
0.00092
Inclination
97.1603°
RAAN
185.0172°
Arg. of periapsis
211.3999°
True anomaly
148.72891°
Mean anomaly
148.674°
Eccentric anomaly
148.70146°
Mean motion
4.04871 °/min
Orbital period
88.92 mins
BSTAR
0.00069454
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Other satellites on launch #24 in the year 2005 (2005-07-05 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.CZ-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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| This satellite is decayed. |
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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