CZ-7A R/B, 60180 (Decayed)
Orbit data source: Space-Track
CZ-7A R/B, 60180 was space debris in LEO originally from a launch on Sat, 29 Jun 2024 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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60180 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, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 CZ-7A R/B
1 60180U 24122B 25300.66340045 .62402491 -23197-4 84548-3 0 9991
2 60180 15.4945 81.6223 0612875 208.6395 147.8905 15.15203706 17911Epoch: 2025-10-27T15:55Z
TLE epoch observation values (Epoch: 2025-10-27T15:55:17.798Z)
Latitude
0°
Longitude
166.53614°
Altitude
882.367 km
Speed
7.216 km/s
True Right ascension
05h 26m 29s
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
19:11:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
949.245 km
Perigee altitude
102.958 km
Semi-major axis
6,904.238 km
Eccentricity
0.06129
Inclination
15.4945°
RAAN
81.6223°
Arg. of periapsis
208.6395°
True anomaly
151.39337°
Mean anomaly
147.8905°
Eccentric anomaly
149.66406°
Mean motion
3.78329 °/min
Orbital period
95.16 mins
BSTAR
0.00084548
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Other satellites on launch #122 in the year 2024 (2024-06-29 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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