KZ-11 R/B, 67071 (Decayed)
Orbit data source: Space-Track
KZ-11 R/B, 67071 was space debris in LEO originally from a launch on Sat, 13 Dec 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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67071 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CASIC
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 8.0 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 KZ-11 R/B
1 67071U 25296C 25358.32930095 .10609436 77667-5 38975-3 0 9991
2 67071 41.3001 37.0775 0331507 35.4688 326.7718 15.73894626 1695Epoch: 2025-12-24T07:54Z
TLE epoch observation values (Epoch: 2025-12-24T07:54:11.602Z)
Latitude
0.00001°
Longitude
-174.57108°
Altitude
163.185 km
Speed
7.916 km/s
True Right ascension
02h 28m 18s
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
12:12:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.101 km
Perigee altitude
127.012 km
Semi-major axis
6,728.193 km
Eccentricity
0.03315
Inclination
41.3001°
RAAN
37.0775°
Arg. of periapsis
35.4688°
True anomaly
324.61603°
Mean anomaly
326.7718°
Eccentric anomaly
325.70148°
Mean motion
3.93274 °/min
Orbital period
91.54 mins
BSTAR
0.00038975
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Other satellites on launch #296 in the year 2025 (2025-12-13 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.KZ-11 R/B Visibility
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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. |
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| This satellite is decayed. |
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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