CZ-4C R/B, 44623

Orbit data source: Space-Track

CZ-4C R/B, 44623 is space debris in LEO originally from a launch on Fri, 04 Oct 2019 UTC launched from the Taiyaun Space Center, China (TSC). 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-4C R/B details

Identifier	44623, 2019-066B
Orbit	LEO
Last TLE update	18 hours ago
Origin	CNSA (CN / PRC)
Manufacturer	SAST
Mission	Spacecraft
Bus & Motor	CZ-4 STAGE 3, Unknown motor
Mass	~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)	2019-10-04 (5 years ago)
Launch vehicle	Unknown
Launch site	Taiyaun Space Center, China (TSC)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 2.9 m
Radar Cross Section	7.676 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 18 hours ago

0 CZ-4C R/B
1 44623U 19066B   24338.69600143  .00036937  00000-0  68603-3 0  9994
2 44623  97.8277  30.1418 0067292 340.3882  19.4779 15.46305315286862

Epoch: 2024-12-03T16:42Z

Definitive object data (Epoch: 2024-12-03T16:42:14.523Z)

Latitude	-0.00003°
Longitude	66.57949°
Altitude	387.508 km
Speed	7.702 km/s
True Right ascension	02h 00m 34s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude	62.88934°
Longitude	-97.1411°
Altitude	472.302 km
Speed	7.617 km/s
Apparent Right ascension	18h 18m 04s
Apparent Declination	17° 23' 15"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	08:11:39
Azimuth	30.581° NE
Elevation	-26.881°
Doppler factor	1

Orbital elements

Apogee altitude	470.271 km
Perigee altitude	378.718 km
Semi-major axis	6,802.632 km
Eccentricity	0.0067292
Inclination	97.8277°
RAAN	30.1418°
Arg. of periapsis	340.3882°
True anomaly	19.73708°
Mean anomaly	19.4779°
Eccentric anomaly	19.60728°
Mean motion	3.86837 °/min
BSTAR	0.00068603
Orbital period	93.06 mins