ZQ-2E R/B, 69537
Orbit data source: Space-Track
ZQ-2E R/B, 69537 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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69537 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Lanjian Hangtian
Mission
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
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ZQ-2E R/B
1 69537U 26128C 26166.53429116 .00037083 00000-0 36627-3 0 9999
2 69537 54.5310 311.6959 0066041 339.7233 20.1178 15.62792458 964Epoch: 2026-06-15T12:49Z
TLE epoch observation values (Epoch: 2026-06-15T12:49:22.756Z)
Latitude
-0.00006°
Longitude
-144.46826°
Altitude
338.785 km
Speed
7.73 km/s
True Right ascension
20h 46m 47s
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
04:57:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
424.261 km
Perigee altitude
335.003 km
Semi-major axis
6,757.769 km
Eccentricity
0.0066
Inclination
54.531°
RAAN
311.6959°
Arg. of periapsis
339.7233°
True anomaly
20.38013°
Mean anomaly
20.1178°
Eccentric anomaly
20.24876°
Mean motion
3.90695 °/min
Orbital period
92.14 mins
BSTAR
0.00036627
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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 R/B 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-15 19:27:47.611Z | 318.591° NNW | 2026-06-15 19:29:47.611Z | 355.993° N | 42.004° | 2026-06-15 19:32:47.611Z | 124.971° SE |
| 4 mins | 2026-06-16 12:01:47.611Z | 211.422° SW | 2026-06-16 12:03:47.611Z | 101.692° ESE | 40.372° | 2026-06-16 12:05:47.611Z | 55.814° ENE |
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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