CZ-3B DEB, 40162

Orbit data source: Space-Track

CZ-3B DEB, 40162 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	40162, 2010-042P
Orbit	HEO
Last TLE update	1 day 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 1 day ago

0 CZ-3B DEB
1 40162U 10042P   24360.53837132 -.00000004  00000-0  00000-0 0  9992
2 40162  27.2724  24.6192 7207709 143.4813 298.9930  1.92036709 77853

Epoch: 2024-12-25T12:55Z

Definitive object data (Epoch: 2024-12-25T12:55:15.282Z)

Latitude	0.00002°
Longitude	96.29108°
Altitude	24,837.812 km
Speed	3.31 km/s
True Right ascension	01h 38m 32s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-25.56922°
Longitude	28.00727°
Altitude	26,224.749 km
Speed	3.142 km/s
Apparent Right ascension	21h 38m 19s
Apparent Declination	-34° 15' 55"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	17:41:20
Azimuth	134.708° SE
Elevation	-2.129°
Doppler factor	1

Orbital elements

Apogee altitude	40,674.968 km
Perigee altitude	1,257.16 km
Semi-major axis	27,344.201 km
Eccentricity	0.7207709
Inclination	27.2724°
RAAN	24.6192°
Arg. of periapsis	143.4813°
True anomaly	216.44841°
Mean anomaly	298.993°
Eccentric anomaly	258.52179°
Mean motion	0.48 °/min
BSTAR	Unknown
Orbital period	749.99 mins