CZ-3B DEB, 42458

Orbit data source: Space-Track

CZ-3B DEB, 42458 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	42458, 2010-042Z
Orbit	HEO
Last TLE update	3 days 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 3 days ago

0 CZ-3B DEB
1 42458U 10042Z   24345.23984457 -.00000023  00000-0  12288-1 0  9998
2 42458  31.1007  26.0411 7479017  21.5362 358.0900  1.81272596 66429

Epoch: 2024-12-10T05:45Z

Definitive object data (Epoch: 2024-12-10T05:45:22.57Z)

Latitude	-0.00018°
Longitude	-139.73068°
Altitude	983.122 km
Speed	9.709 km/s
True Right ascension	01h 44m 15s
True Declination	0° 00' 01"
Sunlit	Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude	-21.40647°
Longitude	79.94892°
Altitude	34,420.487 km
Speed	2.348 km/s
Apparent Right ascension	16h 47m 09s
Apparent Declination	-25° 00' 56"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	08:26:07
Azimuth	89.123° E
Elevation	-42.265°
Doppler factor	1

Orbital elements

Apogee altitude	43,290.197 km
Perigee altitude	785.482 km
Semi-major axis	28,415.977 km
Eccentricity	0.7479017
Inclination	31.1007°
RAAN	26.0411°
Arg. of periapsis	21.5362°
True anomaly	340.38378°
Mean anomaly	358.09°
Eccentric anomaly	352.4874°
Mean motion	0.45311 °/min
BSTAR	0.012288
Orbital period	794.52 mins