CZ-6A DEB, 60717
Orbit data source: Space-Track
CZ-6A DEB, 60717 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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60717 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 CZ-6A DEB
1 60717U 24140DW 25346.29260068 .00025908 00000-0 34180-2 0 9997
2 60717 88.9157 287.1392 0167601 83.9700 278.0588 14.70555208 71071Epoch: 2025-12-12T07:01Z
TLE epoch observation values (Epoch: 2025-12-12T07:01:20.698Z)
Latitude
-0.00008°
Longitude
100.56664°
Altitude
647.828 km
Speed
7.542 km/s
True Right ascension
19h 08m 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
14:13:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
774.07 km
Perigee altitude
538.279 km
Semi-major axis
7,034.312 km
Eccentricity
0.01676
Inclination
88.9157°
RAAN
287.1392°
Arg. of periapsis
83.97°
True anomaly
276.15195°
Mean anomaly
278.0588°
Eccentric anomaly
277.10589°
Mean motion
3.67884 °/min
Orbital period
97.86 mins
BSTAR
0.003418
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-12 20:12:25.010Z | 151.128° SSE | 2025-12-12 20:16:25.010Z | 68.089° E | 31.094° | 2025-12-12 20:19:25.010Z | 17.411° NNE |
| 6 mins | 2025-12-13 08:05:25.010Z | 22.944° NE | 2025-12-13 08:08:25.010Z | 94.358° ESE | 33.481° | 2025-12-13 08:11:25.010Z | 153.848° SSE |
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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