CZ-6A DEB, 60814
Orbit data source: Space-Track
CZ-6A DEB, 60814 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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60814 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: 1 day ago
TLE from 1 day ago
0 CZ-6A DEB
1 60814U 24140GR 25353.37112076 .00000704 00000-0 37351-3 0 9998
2 60814 89.0674 299.7305 0091834 75.1743 285.9593 14.10361458 69573Epoch: 2025-12-19T08:54Z
TLE epoch observation values (Epoch: 2025-12-19T08:54:24.833Z)
Latitude
0.00001°
Longitude
77.91379°
Altitude
843.466 km
Speed
7.44 km/s
True Right ascension
19h 58m 55s
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
10:34:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
921.525 km
Perigee altitude
788.674 km
Semi-major axis
7,233.236 km
Eccentricity
0.00918
Inclination
89.0674°
RAAN
299.7305°
Arg. of periapsis
75.1743°
True anomaly
284.94437°
Mean anomaly
285.9593°
Eccentric anomaly
285.45215°
Mean motion
3.52813 °/min
Orbital period
102.04 mins
BSTAR
0.00037351
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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 | 2025-12-20 20:46:37.350Z | 167.553° S | 2025-12-20 20:50:37.350Z | 121.835° SE | 42.369° | 2025-12-20 20:55:37.350Z | 4.883° NNE |
| 5 mins | 2025-12-21 07:29:37.350Z | 53.314° ENE | 2025-12-21 07:31:37.350Z | 77.913° E | 15.392° | 2025-12-21 07:34:37.350Z | 112.703° SE |
| 8 mins | 2025-12-21 09:10:37.350Z | 348.032° N | 2025-12-21 09:14:37.350Z | 250.404° W | 40.211° | 2025-12-21 09:18:37.350Z | 198.565° SSW |
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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