CZ-6A DEB, 56615 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 56615 was space debris in SSO originally from a launch on Fri, 11 Nov 2022 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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56615 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 CZ-6A DEB
1 56615U 22151AEP 25244.19887737 .03724912 14698-1 19048-1 0 9991
2 56615 98.6162 323.8303 0025591 300.8726 59.0023 15.84458493 56862Epoch: 2025-09-01T04:46Z
TLE epoch observation values (Epoch: 2025-09-01T04:46:23.004Z)
Latitude
-0.00006°
Longitude
-88.37344°
Altitude
312.194 km
Speed
7.726 km/s
True Right ascension
21h 35m 19s
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
15:07:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
331.916 km
Perigee altitude
297.66 km
Semi-major axis
6,692.925 km
Eccentricity
0.00256
Inclination
98.6162°
RAAN
323.8303°
Arg. of periapsis
300.8726°
True anomaly
59.25409°
Mean anomaly
59.0023°
Eccentric anomaly
59.12815°
Mean motion
3.96387 °/min
Orbital period
90.82 mins
BSTAR
0.019048
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Other satellites on launch #151 in the year 2022 (2022-11-11 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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