DECAYED

CZ-2F DEB, 61684 (Decayed)

Orbit data source: Space-Track

CZ-2F DEB, 61684 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	61684, 2024-194B
Orbit	Decayed
Last TLE update	1 month 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	Large (>1 m²)

Expand to show TLE details & history

TLE from 1 month ago

0 CZ-2F DEB
1 61684U 24194B   24327.96353995  .00465987  65563-5  48903-3 0  9998
2 61684  41.3237 193.5705 0257846 294.4302  62.9836 15.68300172  3788

Epoch: 2024-11-22T23:07Z

Definitive object data (Epoch: 2024-11-22T23:07:29.851Z)

Latitude	-0.00008°
Longitude	144.27265°
Altitude	288.015 km
Speed	7.78 km/s
True Right ascension	12h 54m 16s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-29.55222°
Longitude	152.22365°
Altitude	208.968 km
Speed	7.824 km/s
Apparent Right ascension	17h 18m 49s
Apparent Declination	-64° 13' 60"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	10:55:20
Azimuth	146.855° SSE
Elevation	-37.732°
Doppler factor	1

Orbital elements

Apogee altitude	539.927 km
Perigee altitude	192.136 km
Semi-major axis	6,744.168 km
Eccentricity	0.0257846
Inclination	41.3237°
RAAN	193.5705°
Arg. of periapsis	294.4302°
True anomaly	65.65399°
Mean anomaly	62.9836°
Eccentric anomaly	64.31497°
Mean motion	3.91878 °/min
BSTAR	0.00048903
Orbital period	91.87 mins