CZ-2F R/B, 66264
Orbit data source: Space-Track
CZ-2F R/B, 66264 is space debris in LEO originally from a launch on Fri, 31 Oct 2025 UTC via a CHANG ZHENG 2F 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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66264 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT?
Mission
Spacecraft
Bus & Motor
CZ-2F, Unknown motor
Mass
5,500 kg wet, 5,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 CZ-2F R/B
1 66264U 25246B 25311.23026155 .01388549 76297-5 59777-3 0 9991
2 66264 41.4631 229.5206 0078688 176.8975 183.2385 16.14147756 1060Epoch: 2025-11-07T05:31Z
TLE epoch observation values (Epoch: 2025-11-07T05:31:34.597Z)
Latitude
-0.00005°
Longitude
99.94917°
Altitude
287.03 km
Speed
7.707 km/s
True Right ascension
15h 18m 04s
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
17:47:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
289.833 km
Perigee altitude
185.715 km
Semi-major axis
6,615.911 km
Eccentricity
0.00787
Inclination
41.4631°
RAAN
229.5206°
Arg. of periapsis
176.8975°
True anomaly
183.18806°
Mean anomaly
183.2385°
Eccentric anomaly
183.21323°
Mean motion
4.03328 °/min
Orbital period
89.26 mins
BSTAR
0.00059777
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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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| CZ-2F 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
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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