CZ-3B DEB, 40161

Orbit data source: Space-Track

CZ-3B DEB, 40161 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.

Loading next visibility...

CZ-3B DEB details

Identifier	40161, 2010-042N
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 40161U 10042N   24359.56705699  .00001162  00000-0  87159-2 0  9991
2 40161  27.1872 156.9869 7405672 116.9143 353.9965  1.99688707 97664

Epoch: 2024-12-24T13:36Z

Definitive object data (Epoch: 2024-12-24T13:36:33.723Z)

Latitude	24.37162°
Longitude	-79.33487°
Altitude	1,901.094 km
Speed	9.02 km/s
True Right ascension	14h 33m 30s
True Declination	24° 15' 38"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-24.50721°
Longitude	100.85581°
Altitude	15,218.191 km
Speed	4.685 km/s
Apparent Right ascension	02h 36m 55s
Apparent Declination	-41° 24' 07"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	02:26:19
Azimuth	177.991° S
Elevation	8.646°
Doppler factor	1

Orbital elements

Apogee altitude	39,993.41 km
Perigee altitude	533.576 km
Semi-major axis	26,641.63 km
Eccentricity	0.7405672
Inclination	27.1872°
RAAN	156.9869°
Arg. of periapsis	116.9143°
True anomaly	307.24859°
Mean anomaly	353.9965°
Eccentric anomaly	338.32449°
Mean motion	0.49912 °/min
BSTAR	0.0087159
Orbital period	721.27 mins