CZ-6A DEB, 60680
Orbit data source: Space-Track
CZ-6A DEB, 60680 is 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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60680 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 CZ-6A DEB
1 60680U 24140CH 25312.45891007 .00001118 00000-0 35517-3 0 9993
2 60680 88.9685 296.7800 0125788 245.7366 113.0650 14.34900713 65427Epoch: 2025-11-08T11:00Z
TLE epoch observation values (Epoch: 2025-11-08T11:00:49.830Z)
Latitude
-0°
Longitude
83.68415°
Altitude
814.683 km
Speed
7.427 km/s
True Right ascension
19h 47m 07s
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
00:37:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
862.27 km
Perigee altitude
682.381 km
Semi-major axis
7,150.463 km
Eccentricity
0.01258
Inclination
88.9685°
RAAN
296.78°
Arg. of periapsis
245.7366°
True anomaly
114.38296°
Mean anomaly
113.065°
Eccentric anomaly
113.7248°
Mean motion
3.58957 °/min
Orbital period
100.29 mins
BSTAR
0.00035517
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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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-10 10:27:37.873Z | 22.746° NE | 2025-11-10 10:32:37.873Z | 90.8° ESE | 25.762° | 2025-11-10 10:36:37.873Z | 142.384° SSE |
| 7 mins | 2025-11-10 12:09:37.873Z | 327.742° NNW | 2025-11-10 12:12:37.873Z | 277.925° WNW | 27.012° | 2025-11-10 12:16:37.873Z | 222.117° SW |
| 9 mins | 2025-11-10 23:23:37.873Z | 176.612° S | 2025-11-10 23:27:37.873Z | 7.874° NNE | 44.573° | 2025-11-10 23:32:37.873Z | 359.592° N |
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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