ZK-1A R/B, 65264 (Decayed)
Orbit data source: Space-Track
ZK-1A R/B, 65264 was space debris in LEO originally from a launch on Tue, 19 Aug 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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65264 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAS
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
500 kg wet, 500 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
5.880 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 ZK-1A R/B
1 65264U 25180F 25320.03940694 .15044729 26788-5 15560-3 0 9994
2 65264 97.5630 94.5870 0014285 52.4913 307.7687 16.50119008 13959Epoch: 2025-11-16T00:56Z
TLE epoch observation values (Epoch: 2025-11-16T00:56:44.759Z)
Latitude
-0.00006°
Longitude
25.04059°
Altitude
136.587 km
Speed
7.828 km/s
True Right ascension
06h 18m 20s
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
07:19:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
145.129 km
Perigee altitude
126.519 km
Semi-major axis
6,513.961 km
Eccentricity
0.00143
Inclination
97.563°
RAAN
94.587°
Arg. of periapsis
52.4913°
True anomaly
307.63916°
Mean anomaly
307.7687°
Eccentric anomaly
307.70394°
Mean motion
4.12834 °/min
Orbital period
87.2 mins
BSTAR
0.0001556
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Other satellites on launch #180 in the year 2025 (2025-08-19 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.ZK-1A 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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