CZ-6A DEB, 61489
Orbit data source: Space-Track
CZ-6A DEB, 61489 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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61489 intel report (Beta)
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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, 1.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 CZ-6A DEB
1 61489U 24140AAX 26116.93918539 .00017846 00000-0 24290-2 0 9997
2 61489 89.2171 292.9045 0072186 335.8809 23.9037 14.76846887 85421Epoch: 2026-04-26T22:32Z
TLE epoch observation values (Epoch: 2026-04-26T22:32:25.617Z)
Latitude
-0.00005°
Longitude
99.86175°
Altitude
596.169 km
Speed
7.587 km/s
True Right ascension
19h 31m 37s
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
18:10:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
686.797 km
Perigee altitude
585.53 km
Semi-major axis
7,014.301 km
Eccentricity
0.00722
Inclination
89.2171°
RAAN
292.9045°
Arg. of periapsis
335.8809°
True anomaly
24.24166°
Mean anomaly
23.9037°
Eccentric anomaly
24.0724°
Mean motion
3.69459 °/min
Orbital period
97.44 mins
BSTAR
0.002429
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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 | 2026-04-27 11:40:46.012Z | 147.05° SSE | 2026-04-27 11:43:46.012Z | 83.522° E | 33.294° | 2026-04-27 11:47:46.012Z | 14.064° NNE |
| 7 mins | 2026-04-27 23:30:46.012Z | 23.718° NE | 2026-04-27 23:33:46.012Z | 81.466° E | 33.405° | 2026-04-27 23:37:46.012Z | 154.7° SSE |
| 4 mins | 2026-04-28 01:09:46.012Z | 303.375° NW | 2026-04-28 01:10:46.012Z | 287.651° WNW | 17.523° | 2026-04-28 01:13:46.012Z | 244.507° WSW |
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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