CZ-6A DEB, 61166
Orbit data source: Space-Track
CZ-6A DEB, 61166 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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61166 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, 0.1 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 61166U 24140RL 25312.40184301 .00028639 00000-0 43167-2 0 9996
2 61166 88.9687 294.3674 0081047 281.1659 78.0456 14.72022267 64187Epoch: 2025-11-08T09:38Z
TLE epoch observation values (Epoch: 2025-11-08T09:38:39.236Z)
Latitude
-0.00004°
Longitude
101.87194°
Altitude
646.381 km
Speed
7.541 km/s
True Right ascension
19h 37m 28s
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
04:52:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
708.47 km
Perigee altitude
594.523 km
Semi-major axis
7,029.634 km
Eccentricity
0.0081
Inclination
88.9687°
RAAN
294.3674°
Arg. of periapsis
281.1659°
True anomaly
78.95606°
Mean anomaly
78.0456°
Eccentric anomaly
78.50064°
Mean motion
3.68251 °/min
Orbital period
97.76 mins
BSTAR
0.0043167
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-10 11:09:43.146Z | 1.132° NNE | 2025-11-10 11:13:43.146Z | 103.364° ESE | 44.999° | 2025-11-10 11:17:43.146Z | 182.027° SSW |
| 5 mins | 2025-11-10 22:09:43.146Z | 107.143° ESE | 2025-11-10 22:11:43.146Z | 77.246° E | 17.289° | 2025-11-10 22:14:43.146Z | 36.586° NE |
| 6 mins | 2025-11-10 23:46:43.146Z | 215.979° SW | 2025-11-10 23:48:43.146Z | 257.45° W | 33.178° | 2025-11-10 23:52:43.146Z | 339.686° 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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