CZ-12A R/B, 67231
Orbit data source: Space-Track
CZ-12A R/B, 67231 is space debris in LEO originally from a launch on Tue, 23 Dec 2025 UTC via a CHANG ZHENG 12A launch vehicle 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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67231 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CZ-12A R/B
1 67231U 25308A 25362.77966721 .11863649 47688-5 10694-3 0 9999
2 67231 69.6966 46.2284 0006373 167.5134 192.6259 16.51512804 934Epoch: 2025-12-28T18:42Z
TLE epoch observation values (Epoch: 2025-12-28T18:42:43.246Z)
Latitude
-0.00012°
Longitude
28.06142°
Altitude
141.97 km
Speed
7.819 km/s
True Right ascension
03h 04m 54s
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
21:36:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
137.349 km
Perigee altitude
129.05 km
Semi-major axis
6,511.337 km
Eccentricity
0.00064
Inclination
69.6966°
RAAN
46.2284°
Arg. of periapsis
167.5134°
True anomaly
192.60995°
Mean anomaly
192.6259°
Eccentric anomaly
192.61792°
Mean motion
4.13084 °/min
Orbital period
87.15 mins
BSTAR
0.00010694
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Other satellites on launch #308 in the year 2025 (2025-12-23 UTC)
No other RSOs were in this launch
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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.CZ-12A 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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| CZ-12A R/B is likely not visible in the next few days. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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