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	2 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 2 days ago

0 CZ-3B DEB
1 42458U 10042Z   24360.13370770 -.00000269  00000-0 -48143-2 0  9994
2 42458  31.1267  22.5171 7478606  27.0309 357.5503  1.81277212 66698

Epoch: 2024-12-25T03:12Z

Definitive object data (Epoch: 2024-12-25T03:12:32.345Z)

Latitude	0.00014°
Longitude	-119.73257°
Altitude	1,129.687 km
Speed	9.599 km/s
True Right ascension	01h 30m 08s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-12.81879°
Longitude	81.92742°
Altitude	43,153.31 km
Speed	1.437 km/s
Apparent Right ascension	14h 44m 31s
Apparent Declination	-16° 01' 39"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	00:37:27
Azimuth	301.705° NW
Elevation	-53.505°
Doppler factor	1

Orbital elements

Apogee altitude	43,288.179 km
Perigee altitude	786.528 km
Semi-major axis	28,415.491 km
Eccentricity	0.7478606
Inclination	31.1267°
RAAN	22.5171°
Arg. of periapsis	27.0309°
True anomaly	335.10824°
Mean anomaly	357.5503°
Eccentric anomaly	350.41669°
Mean motion	0.45312 °/min
BSTAR	-0.0048143
Orbital period	794.5 mins