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.
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64054 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
2 months ago
Origin
Landspace (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)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 6.0 m
Radar Cross Section
35.980 m², Large (>1 m²)
Expand to show TLE details & history
TLE from 2 months 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 3063Epoch: 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
Visualization orbit readout
No trajectory is available.
Visualization observer readout
No trajectory is available.
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
114.99445°
Mean anomaly
114.5443°
Eccentric anomaly
114.76948°
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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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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