DECAYED

CZ-2C R/B, 61620 (Decayed)

Orbit data source: Space-Track

CZ-2C R/B, 61620 was space debris in LEO originally from a launch on Wed, 23 Oct 2024 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.

Not visible in the next 10 days

CZ-2C R/B details

Identifier	61620, 2024-190D
Orbit	Decayed
Last TLE update	1 month ago
Origin	CASC (CN / PRC)
Manufacturer	CALT
Mission	Decayed spacecraft
Bus & Motor	CZ-2 STAGE 2, Unknown motor
Mass	~3,800 kg wet, ~3,800 kg dry
Launch date (UTC)	2024-10-23 (2 months ago)
Launch vehicle	Unknown
Launch site	Xichang Space Center, China (XSC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 1 month ago

0 CZ-2C R/B
1 61620U 24190D   24325.87196646  .05332485  15058-5  50849-3 0  9997
2 61620  34.9970 184.6356 0040246 310.7409 119.6211 16.34319024  4516

Epoch: 2024-11-20T20:55Z

Definitive object data (Epoch: 2024-11-20T20:55:37.902Z)

Latitude	32.9322°
Longitude	-122.73039°
Altitude	194.193 km
Speed	7.788 km/s
True Right ascension	16h 46m 09s
True Declination	32° 45' 43"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	210.777 km
Perigee altitude	157.954 km
Semi-major axis	6,562.502 km
Eccentricity	0.0040246
Inclination	34.997°
RAAN	184.6356°
Arg. of periapsis	310.7409°
True anomaly	120.02102°
Mean anomaly	119.6211°
Eccentric anomaly	119.82116°
Mean motion	4.08262 °/min
BSTAR	0.00050849
Orbital period	88.18 mins