CZ-6A DEB, 61389
Orbit data source: Space-Track
CZ-6A DEB, 61389 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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61389 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 61389U 24140XE 25312.45164992 .00003733 00000-0 17035-2 0 9995
2 61389 89.0400 301.7749 0054060 189.9093 170.1037 14.20631214 60947Epoch: 2025-11-08T10:50Z
TLE epoch observation values (Epoch: 2025-11-08T10:50:22.553Z)
Latitude
0.00003°
Longitude
91.29986°
Altitude
864.639 km
Speed
7.4 km/s
True Right ascension
20h 07m 05s
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
19:40:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
859.083 km
Perigee altitude
781.255 km
Semi-major axis
7,198.306 km
Eccentricity
0.00541
Inclination
89.04°
RAAN
301.7749°
Arg. of periapsis
189.9093°
True anomaly
170.20946°
Mean anomaly
170.1037°
Eccentric anomaly
170.15665°
Mean motion
3.55384 °/min
Orbital period
101.3 mins
BSTAR
0.0017035
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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 00:08:24.697Z | 193.892° SSW | 2025-11-10 00:13:24.697Z | 285.911° WNW | 40.396° | 2025-11-10 00:18:24.697Z | 350.769° N |
| 7 mins | 2025-11-10 10:46:24.697Z | 32.744° NE | 2025-11-10 10:49:24.697Z | 75.525° E | 24.784° | 2025-11-10 10:53:24.697Z | 135.36° SSE |
| 7 mins | 2025-11-10 12:28:24.697Z | 326.262° NNW | 2025-11-10 12:31:24.697Z | 272.415° WNW | 27.735° | 2025-11-10 12:35:24.697Z | 219.635° SW |
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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