CZ-6A DEB, 61302
Orbit data source: Space-Track
CZ-6A DEB, 61302 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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61302 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 61302U 24140TP 25311.95427450 .00016043 00000-0 36346-2 0 9999
2 61302 88.8926 291.2143 0062148 320.7308 38.9401 14.54848418 63293Epoch: 2025-11-07T22:54Z
TLE epoch observation values (Epoch: 2025-11-07T22:54:09.316Z)
Latitude
-0.00006°
Longitude
-99.71535°
Altitude
678.798 km
Speed
7.535 km/s
True Right ascension
19h 24m 51s
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
05:20:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
750.79 km
Perigee altitude
662.728 km
Semi-major axis
7,084.896 km
Eccentricity
0.00621
Inclination
88.8926°
RAAN
291.2143°
Arg. of periapsis
320.7308°
True anomaly
39.39042°
Mean anomaly
38.9401°
Eccentric anomaly
39.16499°
Mean motion
3.63951 °/min
Orbital period
98.91 mins
BSTAR
0.0036346
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-10 10:53:17.080Z | 1.815° NNE | 2025-11-10 10:58:17.080Z | 80.28° E | 44.903° | 2025-11-10 11:03:17.080Z | 180.391° SSW |
| 5 mins | 2025-11-10 22:02:17.080Z | 108.717° ESE | 2025-11-10 22:04:17.080Z | 76.484° E | 19.698° | 2025-11-10 22:07:17.080Z | 34.508° NE |
| 7 mins | 2025-11-10 23:40:17.080Z | 220.562° SW | 2025-11-10 23:43:17.080Z | 285.922° WNW | 30.631° | 2025-11-10 23:47:17.080Z | 341.705° 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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