CZ-2D DEB, 35272
Orbit data source: Space-Track
CZ-2D DEB, 35272 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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35272 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CZ-2D DEB
1 35272U 05024L 25242.81327275 .00039310 00000-0 57572-3 0 9995
2 35272 97.2024 268.0064 0008649 122.6862 237.5228 15.55435533 93858Epoch: 2025-08-30T19:31Z
TLE epoch observation values (Epoch: 2025-08-30T19:31:06.765Z)
Latitude
-0.00004°
Longitude
-4.01397°
Altitude
407.184 km
Speed
7.665 km/s
True Right ascension
17h 52m 01s
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
12:51:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
403.657 km
Perigee altitude
391.936 km
Semi-major axis
6,775.934 km
Eccentricity
0.00086
Inclination
97.2024°
RAAN
268.0064°
Arg. of periapsis
122.6862°
True anomaly
237.43924°
Mean anomaly
237.5228°
Eccentric anomaly
237.48101°
Mean motion
3.89125 °/min
Orbital period
92.52 mins
BSTAR
0.00057572
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Other satellites on launch #24 in the year 2005 (2005-07-05 UTC)
CZ-2D DEB Visibility
Observer location: undefined°, undefined°
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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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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Authenticating...
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