CZ-6A DEB, 61309
Orbit data source: Space-Track
CZ-6A DEB, 61309 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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61309 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 61309U 24140TW 25312.23840450 .00005493 00000-0 21757-2 0 9994
2 61309 88.9752 297.8740 0024006 144.0774 216.2041 14.28622921 62344Epoch: 2025-11-08T05:43Z
TLE epoch observation values (Epoch: 2025-11-08T05:43:18.148Z)
Latitude
-0.00001°
Longitude
164.3775°
Altitude
813.318 km
Speed
7.439 km/s
True Right ascension
19h 51m 29s
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
02:32:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
810.492 km
Perigee altitude
776.061 km
Semi-major axis
7,171.414 km
Eccentricity
0.0024
Inclination
88.9752°
RAAN
297.874°
Arg. of periapsis
144.0774°
True anomaly
216.04201°
Mean anomaly
216.2041°
Eccentric anomaly
216.12301°
Mean motion
3.57385 °/min
Orbital period
100.73 mins
BSTAR
0.0021757
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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 | 2025-11-10 10:25:29.811Z | 33.457° NE | 2025-11-10 10:28:29.811Z | 73.765° E | 22.354° | 2025-11-10 10:32:29.811Z | 131.448° SE |
| 7 mins | 2025-11-10 12:06:29.811Z | 334.278° NNW | 2025-11-10 12:09:29.811Z | 285.865° WNW | 29.869° | 2025-11-10 12:13:29.811Z | 219.485° SW |
| 8 mins | 2025-11-10 23:24:29.811Z | 173.068° S | 2025-11-10 23:28:29.811Z | 25.46° NE | 43.791° | 2025-11-10 23:32:29.811Z | 1.388° NNE |
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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