CZ-12B R/B, 69327
Orbit data source: Space-Track
CZ-12B R/B, 69327 is space debris in LEO originally from a launch on Mon, 01 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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69327 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-12 STAGE 2, YF-115
Mass
~6,000 kg wet, ~6,000 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 days ago
TLE from 6 days ago
0 CZ-12B R/B
1 69327U 26121C 26154.97511481 .00000469 00000-0 24140-3 0 9996
2 69327 89.0307 301.8428 0196606 48.9718 312.8273 14.04083962 370Epoch: 2026-06-03T23:24Z
TLE epoch observation values (Epoch: 2026-06-03T23:24:09.919Z)
Latitude
0°
Longitude
58.37545°
Altitude
787.236 km
Speed
7.509 km/s
True Right ascension
20h 07m 22s
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
14:06:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,019.293 km
Perigee altitude
734.026 km
Semi-major axis
7,254.797 km
Eccentricity
0.01966
Inclination
89.0307°
RAAN
301.8428°
Arg. of periapsis
48.9718°
True anomaly
311.14717°
Mean anomaly
312.8273°
Eccentric anomaly
311.99004°
Mean motion
3.51241 °/min
Orbital period
102.49 mins
BSTAR
0.0002414
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Other satellites on launch #121 in the year 2026 (2026-06-01 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.CZ-12B 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-10 09:26:34.745Z | 159.466° S | 2026-06-10 09:30:34.745Z | 102.839° ESE | 38.248° | 2026-06-10 09:35:34.745Z | 9.349° NNE |
| 5 mins | 2026-06-10 20:12:34.745Z | 58.395° ENE | 2026-06-10 20:14:34.745Z | 81.297° E | 15.077° | 2026-06-10 20:17:34.745Z | 112.003° ESE |
| 9 mins | 2026-06-10 21:53:34.745Z | 352.758° N | 2026-06-10 21:57:34.745Z | 251.507° W | 43.224° | 2026-06-10 22:02:34.745Z | 192.092° SSW |
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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