DECAYED

ZQ-2E R/B, 64054 (Decayed)

Orbit data source: Space-Track

ZQ-2E R/B, 64054 was space debris in LEO originally from a launch on Sat, 17 May 2025 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
Identifier
64054, 2025-103G
Orbit
Decayed
Last TLE update
2 weeks ago
Origin
Flag of CNLandspace (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)
2025-05-17 (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 weeks ago
0 ZQ-2E R/B
1 64054U 25103G   25156.48638369  .15733274  23782-5  19690-3 0  9993
2 64054  96.0687 229.0499 0043283  12.2432 114.5443 16.44901597  3063
Epoch: 2025-06-05T11:40Z
TLE epoch observation values (Epoch: 2025-06-05T11:40:23.55Z)
Latitude
52.45167°
Longitude
-12.2983°
Altitude
173.315 km
Speed
7.8 km/s
True Right ascension
03h 47m 48s
True Declination
52° 16' 14"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
177.796 km
Perigee altitude
121.289 km
Semi-major axis
6,527.679 km
Eccentricity
0.00433
Inclination
96.0687°
RAAN
229.0499°
Arg. of periapsis
12.2432°
True anomaly
Unknown
Mean anomaly
114.5443°
Eccentric anomaly
Unknown
Mean motion
4.11533 °/min
Orbital period
87.48 mins
BSTAR
0.0001969
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Other satellites on launch #103 in the year 2025 (2025-05-17 UTC)

ZQ-2E R/B Visibility

Observer location: undefined°, undefined°

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