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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CZ-2D DEB details

Identifier	35272, 2005-024L
Orbit	SSO
Last TLE update	1 day ago
Origin	CASC (CN / PRC)
Manufacturer	Unknown
Mission	Spacecraft
Bus & Motor	Unknown
Mass	Unknown
Launch date (UTC)	2005-07-05 (19 years ago)
Launch vehicle	Unknown
Launch site	Jiuquan Satellite Launch Center, China (JSC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 CZ-2D DEB
1 35272U 05024L   24360.33615375  .00031493  00000-0  75275-3 0  9997
2 35272  97.2234  19.7818 0005862 332.0653  28.0278 15.41418502 55395

Epoch: 2024-12-25T08:04Z

Definitive object data (Epoch: 2024-12-25T08:04:03.683Z)

Latitude	-0.00013°
Longitude	164.43511°
Altitude	441.517 km
Speed	7.649 km/s
True Right ascension	01h 19m 07s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	73.91049°
Longitude	11.52128°
Altitude	457.32 km
Speed	7.643 km/s
Apparent Right ascension	22h 30m 13s
Apparent Declination	32° 26' 21"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	11:55:19
Azimuth	18.483° NNE
Elevation	-15.011°
Doppler factor	1

Orbital elements

Apogee altitude	442.848 km
Perigee altitude	434.855 km
Semi-major axis	6,816.989 km
Eccentricity	0.0005862
Inclination	97.2234°
RAAN	19.7818°
Arg. of periapsis	332.0653°
True anomaly	28.05939°
Mean anomaly	28.0278°
Eccentric anomaly	28.04359°
Mean motion	3.85615 °/min
BSTAR	0.00075275
Orbital period	93.36 mins