CZ-6A DEB, 61797 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 61797 was 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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61797 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Decayed 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: 6 months ago
TLE from 6 months ago
0 CZ-6A DEB
1 61797U 24140ABM 25106.33559159 .00212034 00000-0 12110-1 0 9993
2 61797 89.1572 325.2580 0057779 251.6888 107.8061 15.10356390 34140Epoch: 2025-04-16T08:03Z
TLE epoch observation values (Epoch: 2025-04-16T08:03:15.113Z)
Latitude
-0.00004°
Longitude
-0.27829°
Altitude
550.72 km
Speed
7.58 km/s
True Right ascension
21h 41m 01s
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
23:13:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.86 km
Perigee altitude
492.009 km
Semi-major axis
6,910.071 km
Eccentricity
0.00578
Inclination
89.1572°
RAAN
325.258°
Arg. of periapsis
251.6888°
True anomaly
108.43508°
Mean anomaly
107.8061°
Eccentric anomaly
108.12073°
Mean motion
3.7785 °/min
Orbital period
95.28 mins
BSTAR
0.01211
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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
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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