ZQ-2E DEB, 69631
Orbit data source: Space-Track
ZQ-2E DEB, 69631 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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69631 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Lanjian Hangtian
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ZQ-2E DEB
1 69631U 26128F 26171.41806628 .00135193 00000-0 14112-2 0 9999
2 69631 54.5280 288.9503 0067983 332.6012 27.1441 15.60722305 1681Epoch: 2026-06-20T10:02Z
TLE epoch observation values (Epoch: 2026-06-20T10:02:00.926Z)
Latitude
-0.00001°
Longitude
-130.18654°
Altitude
345.777 km
Speed
7.726 km/s
True Right ascension
19h 15m 48s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:12:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.589 km
Perigee altitude
339.625 km
Semi-major axis
6,763.744 km
Eccentricity
0.0068
Inclination
54.528°
RAAN
288.9503°
Arg. of periapsis
332.6012°
True anomaly
27.50222°
Mean anomaly
27.1441°
Eccentric anomaly
27.32289°
Mean motion
3.90178 °/min
Orbital period
92.27 mins
BSTAR
0.0014112
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Other satellites on launch #128 in the year 2026 (2026-06-09 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ZQ-2E DEB Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 10:49:57.238Z | 259.527° W | 2026-06-21 10:51:57.238Z | 344.188° N | 33.276° | 2026-06-21 10:53:57.238Z | 32.06° NE |
| 5 mins | 2026-06-21 17:16:57.238Z | 319.321° NNW | 2026-06-21 17:18:57.238Z | 87.217° E | 43.181° | 2026-06-21 17:21:57.238Z | 127.848° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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