CZ-6A DEB, 60985 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 60985 was space debris in LEO originally from a launch on Tue, 06 Aug 2024 UTC launched from the Taiyaun Space Center, China (TSC). 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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60985 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 CZ-6A DEB
1 60985U 24140ML 26019.75049837 .00737147 19913-3 32164-2 0 9993
2 60985 89.0505 287.2425 0030215 206.2628 153.7122 15.84007483 78022Epoch: 2026-01-19T18:00Z
TLE epoch observation values (Epoch: 2026-01-19T18:00:43.059Z)
Latitude
-0.00002°
Longitude
-102.07915°
Altitude
340.565 km
Speed
7.694 km/s
True Right ascension
19h 08m 58s
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
14:27:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
336.067 km
Perigee altitude
295.615 km
Semi-major axis
6,693.978 km
Eccentricity
0.00302
Inclination
89.0505°
RAAN
287.2425°
Arg. of periapsis
206.2628°
True anomaly
153.86502°
Mean anomaly
153.7122°
Eccentric anomaly
153.78866°
Mean motion
3.96293 °/min
Orbital period
90.84 mins
BSTAR
0.0032164
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Other satellites on launch #140 in the year 2024 (2024-08-06 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-6A DEB 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
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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