CZ-7A R/B, 65564 (Decayed)
Orbit data source: Space-Track
CZ-7A R/B, 65564 was space debris in LEO originally from a launch on Tue, 09 Sep 2025 UTC launched from the Wenchang Satellite Launch Center (WSC). 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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65564 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 1.1 m
Radar Cross Section
32.704 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 CZ-7A R/B
1 65564U 25202B 25302.09724866 .23107890 -12538-4 82846-3 0 9996
2 65564 20.0158 218.2273 0920381 88.6180 281.9344 14.36108296 5256Epoch: 2025-10-29T02:20Z
TLE epoch observation values (Epoch: 2025-10-29T02:20:02.284Z)
Latitude
0.00001°
Longitude
145.54254°
Altitude
692.293 km
Speed
7.553 km/s
True Right ascension
14h 32m 54s
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
10:18:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,435.038 km
Perigee altitude
118.033 km
Semi-major axis
7,154.673 km
Eccentricity
0.09204
Inclination
20.0158°
RAAN
218.2273°
Arg. of periapsis
88.618°
True anomaly
271.42378°
Mean anomaly
281.9344°
Eccentric anomaly
276.69699°
Mean motion
3.5864 °/min
Orbital period
100.38 mins
BSTAR
0.00082846
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Other satellites on launch #202 in the year 2025 (2025-09-09 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-7A 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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