CZ-2F R/B, 66264 (Decayed)
Orbit data source: Space-Track
CZ-2F R/B, 66264 was space debris in LEO originally from a launch on Fri, 31 Oct 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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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT?
Mission
Decayed spacecraft
Bus & Motor
CZ-2F, Unknown motor
Mass
5,500 kg wet, 5,500 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
44.450 m²
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 CZ-2F R/B
1 66264U 25246B 25316.02352218 .12378867 81186-5 13685-3 0 9990
2 66264 41.4424 197.4583 0019761 232.0549 127.8536 16.48584502 1849Epoch: 2025-11-12T00:33Z
TLE epoch observation values (Epoch: 2025-11-12T00:33:52.316Z)
Latitude
0.00005°
Longitude
137.5887°
Altitude
150.569 km
Speed
7.813 km/s
True Right ascension
13h 09m 50s
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
05:23:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
158.277 km
Perigee altitude
132.495 km
Semi-major axis
6,523.523 km
Eccentricity
0.00198
Inclination
41.4424°
RAAN
197.4583°
Arg. of periapsis
232.0549°
True anomaly
128.03213°
Mean anomaly
127.8536°
Eccentric anomaly
127.94289°
Mean motion
4.11927 °/min
Orbital period
87.39 mins
BSTAR
0.00013685
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Other satellites on launch #246 in the year 2025 (2025-10-31 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-2F 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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