CZ-3B DEB, 38748

Orbit data source: Space-Track

CZ-3B DEB, 38748 is space debris in HEO originally from a launch on Sat, 04 Sep 2010 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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CZ-3B DEB details

Identifier	38748, 2010-042C
Orbit	HEO
Last TLE update	6 months ago
Origin	CASC (CN / PRC)
Manufacturer	CALT
Mission	Spacecraft
Bus & Motor	Unknown
Mass	Unknown
Launch date (UTC)	2010-09-04 (14 years ago)
Launch vehicle	Unknown
Launch site	Xichang Space Center, China (XSC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 6 months ago

0 CZ-3B DEB
1 38748U 10042C   24168.06014989  .00002786  00000-0  66677-2 0  9992
2 38748  24.1882 332.1271 7267159 224.8517  46.4547  2.22791523 97483

Epoch: 2024-06-16T01:26Z

Definitive object data (Epoch: 2024-06-16T01:26:36.95Z)

Latitude	-0.00025°
Longitude	45.63191°
Altitude	17,716.415 km
Speed	4.122 km/s
True Right ascension	22h 08m 24s
True Declination	0° 00' 01"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	9.90381°
Longitude	133.06523°
Altitude	34,611.79 km
Speed	1.816 km/s
Apparent Right ascension	03h 44m 34s
Apparent Declination	3° 48' 49"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	13:47:53
Azimuth	321.436° NNW
Elevation	-38.721°
Doppler factor	1

Orbital elements

Apogee altitude	36,387.592 km
Perigee altitude	390.315 km
Semi-major axis	24,767.091 km
Eccentricity	0.7267159
Inclination	24.1882°
RAAN	332.1271°
Arg. of periapsis	224.8517°
True anomaly	135.26865°
Mean anomaly	46.4547°
Eccentric anomaly	88.0688°
Mean motion	0.55684 °/min
BSTAR	0.0066677
Orbital period	646.5 mins