CZ-7A R/B, 66314 (Decayed)
Orbit data source: Space-Track
CZ-7A R/B, 66314 was space debris in LEO originally from a launch on Mon, 03 Nov 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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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, 8.0 m
Radar Cross Section
32.704 m²
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 CZ-7A R/B
1 66314U 25250B 25345.38346150 .56994747 -13468-4 10408-2 0 9996
2 66314 19.8970 337.6381 0578962 23.6109 338.9826 15.20787468 4152Epoch: 2025-12-11T09:12Z
TLE epoch observation values (Epoch: 2025-12-11T09:12:11.073Z)
Latitude
-0°
Longitude
119.25173°
Altitude
132.453 km
Speed
8.036 km/s
True Right ascension
22h 30m 33s
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
05:24:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
907.513 km
Perigee altitude
110.059 km
Semi-major axis
6,886.923 km
Eccentricity
0.0579
Inclination
19.897°
RAAN
337.6381°
Arg. of periapsis
23.6109°
True anomaly
336.43216°
Mean anomaly
338.9826°
Eccentric anomaly
337.72522°
Mean motion
3.79757 °/min
Orbital period
94.8 mins
BSTAR
0.0010408
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Other satellites on launch #250 in the year 2025 (2025-11-03 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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