ZQ-2E DEB, 69629

Orbit data source: Space-Track

ZQ-2E DEB, 69629 is space debris in LEO originally from a launch on Tue, 09 Jun 2026 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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Identifier
69629, 2026-128D
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Flag of CNLandspace (CN)
Manufacturer
Lanjian Hangtian
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-06-09 (2 weeks ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 ZQ-2E  DEB
1 69629U 26128D   26171.45733233  .00349842  00000-0  29518-2 0  9995
2 69629  54.5260 288.5704 0055728 327.4549  32.3053 15.66250669  1701
Epoch: 2026-06-20T10:58Z
TLE epoch observation values (Epoch: 2026-06-20T10:58:33.513Z)
Latitude
-0.00008°
Longitude
-144.74097°
Altitude
338.983 km
Speed
7.725 km/s
True Right ascension
19h 14m 16s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:11:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
407.286 km
Perigee altitude
332.078 km
Semi-major axis
6,747.819 km
Eccentricity
0.00557
Inclination
54.526°
RAAN
288.5704°
Arg. of periapsis
327.4549°
True anomaly
32.6486°
Mean anomaly
32.3053°
Eccentric anomaly
32.47675°
Mean motion
3.9156 °/min
Orbital period
91.94 mins
BSTAR
0.0029518
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