DECAYED

CZ-2F DEB, 61685 (Decayed)

Orbit data source: Space-Track

CZ-2F DEB, 61685 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 DEB details

Identifier	61685, 2024-194C
Orbit	Decayed
Last TLE update	2 months ago
Origin	CALT (CN / PRC)
Manufacturer	CALT?
Mission	Decayed spacecraft
Bus & Motor	Unknown
Mass	1 kg wet, 1 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	Small (<0.1 m²)

Expand to show TLE details & history

TLE from 2 months ago

0 OBJECT C
1 61685U 24194C   24304.53447202  .10360189  69059-5  81270-2 0  9998
2 61685  41.5666 336.9773 0196838 141.4270 221.5742 15.84571849   104

Epoch: 2024-10-30T12:49Z

Definitive object data (Epoch: 2024-10-30T12:49:38.382Z)

Latitude	0.96583°
Longitude	106.32003°
Altitude	416.715 km
Speed	7.606 km/s
True Right ascension	22h 32m 14s
True Declination	0° 57' 35"
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	451.611 km
Perigee altitude	187.93 km
Semi-major axis	6,697.908 km
Eccentricity	0.0196838
Inclination	41.5666°
RAAN	336.9773°
Arg. of periapsis	141.427°
True anomaly	220.10464°
Mean anomaly	221.5742°
Eccentric anomaly	220.83673°
Mean motion	3.95945 °/min
BSTAR	0.008127
Orbital period	90.92 mins