KZ-11 R/B, 54589 (Decayed)
Orbit data source: Space-Track
KZ-11 R/B, 54589 was space debris in LEO originally from a launch on Wed, 07 Dec 2022 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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54589 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, 1.6 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 KZ-11 R/B
1 54589U 22164B 25132.23195171 .14148882 31844-5 67094-4 0 9999
2 54589 98.2925 297.6606 0020141 243.3044 294.7012 16.55468382136500Epoch: 2025-05-12T05:34Z
TLE epoch observation values (Epoch: 2025-05-12T05:34:00.627Z)
Latitude
2.06627°
Longitude
164.20954°
Altitude
122.521 km
Speed
7.836 km/s
True Right ascension
07h 51m 50s
True Declination
2° 03' 10"
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
21:23:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
134.897 km
Perigee altitude
108.714 km
Semi-major axis
6,499.942 km
Eccentricity
0.00201
Inclination
98.2925°
RAAN
297.6606°
Arg. of periapsis
243.3044°
True anomaly
294.4913°
Mean anomaly
294.7012°
Eccentric anomaly
294.59627°
Mean motion
4.1417 °/min
Orbital period
86.92 mins
BSTAR
0.000067094
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Other satellites on launch #164 in the year 2022 (2022-12-07 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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