CZ-2D DEB, 35273
Orbit data source: Space-Track
CZ-2D DEB, 35273 is space debris in SSO 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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35273 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 CZ-2D DEB
1 35273U 05024M 25290.88483392 .00134267 00000-0 90157-3 0 9992
2 35273 97.1604 324.1193 0002576 222.6347 137.4719 15.74810158140454
Epoch: 2025-10-17T21:14Z
TLE epoch observation values (Epoch: 2025-10-17T21:14:09.650Z)
Latitude
-0.00001°
Longitude
-21.0447°
Altitude
349.62 km
Speed
7.698 km/s
True Right ascension
21h 36m 28s
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
07:09:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
343.785 km
Perigee altitude
340.323 km
Semi-major axis
6,720.191 km
Eccentricity
0.00026
Inclination
97.1604°
RAAN
324.1193°
Arg. of periapsis
222.6347°
True anomaly
137.49185°
Mean anomaly
137.4719°
Eccentric anomaly
137.48187°
Mean motion
3.93977 °/min
Orbital period
91.38 mins
BSTAR
0.00090157
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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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CZ-2D DEB is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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