DECAYED

CZ-2F R/B, 61686 (Decayed)

Orbit data source: Space-Track

CZ-2F R/B, 61686 was space debris in LEO originally from a launch on Tue, 29 Oct 2024 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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-2F R/B details

Identifier	61686, 2024-194D
Orbit	Decayed
Last TLE update	2 months ago
Origin	CALT (CN / PRC)
Manufacturer	CALT?
Mission	Decayed spacecraft
Bus & Motor	CZ-2F, Unknown motor
Mass	5,500 kg wet, 5,500 kg dry
Launch date (UTC)	2024-10-29 (2 months ago)
Launch vehicle	Unknown
Launch site	Jiuquan Satellite Launch Center, China (JSC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 2 months ago

0 OBJECT D
1 61686U 24194D   24312.41093039  .05262063  78099-5  37845-3 0  9990
2 61686  41.4558 285.2074 0036233 194.5499 344.2276 16.36423738  1330

Epoch: 2024-11-07T09:51Z

Definitive object data (Epoch: 2024-11-07T09:51:44.385Z)

Latitude	0.83222°
Longitude	-90.75832°
Altitude	151.973 km
Speed	7.831 km/s
True Right ascension	06h 57m 04s
True Declination	0° 49' 36"
Sunlit	Object was in full shadow 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	201.393 km
Perigee altitude	153.886 km
Semi-major axis	6,555.777 km
Eccentricity	0.0036233
Inclination	41.4558°
RAAN	285.2074°
Arg. of periapsis	194.5499°
True anomaly	344.11425°
Mean anomaly	344.2276°
Eccentric anomaly	344.17097°
Mean motion	4.0889 °/min
BSTAR	0.00037845
Orbital period	88.04 mins