ZQ-2E R/B, 62113

Orbit data source: Space-Track

ZQ-2E R/B, 62113 is space debris in LEO originally from a launch on Wed, 27 Nov 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

ZQ-2E R/B details

Identifier	62113, 2024-221C
Orbit	LEO
Last TLE update	2 days ago
Origin	Lanjian Hangtian (CN / PRC)
Manufacturer	Lanjian Hangtian
Mission	Decayed spacecraft
Bus & Motor	ZQ-2 ST 2, Unknown motor
Mass	~5,000 kg wet, ~5,000 kg dry
Launch date (UTC)	2024-11-27 (1 month 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 days ago

0 ZQ-2E R/B
1 62113U 24221C   24359.27350825  .17063427  11656-4  23207-3 0  9999
2 62113  49.8914 275.2215 0042979 178.2700 320.2910 16.43889986  4294

Epoch: 2024-12-24T06:33Z

Definitive object data (Epoch: 2024-12-24T06:33:51.112Z)

Latitude	30.72693°
Longitude	-126.37869°
Altitude	135.37 km
Speed	7.842 km/s
True Right ascension	04h 21m 28s
True Declination	30° 33' 42"
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	184.39 km
Perigee altitude	128.221 km
Semi-major axis	6,534.442 km
Eccentricity	0.0042979
Inclination	49.8914°
RAAN	275.2215°
Arg. of periapsis	178.27°
True anomaly	319.97504°
Mean anomaly	320.291°
Eccentric anomaly	320.13315°
Mean motion	4.10895 °/min
BSTAR	0.00023207
Orbital period	87.61 mins