CZ-6A DEB, 60777 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 60777 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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60777 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 6 months ago
0 CZ-6A DEB
1 60777U 24140FC 25025.32439955 .09719731 -11184-5 42151-2 0 9995
2 60777 89.4576 340.0535 0032155 132.6673 227.7345 16.21245910 23941
Epoch: 2025-01-25T07:47Z
TLE epoch observation values (Epoch: 2025-01-25T07:47:08.121Z)
Latitude
-0.00003°
Longitude
98.39481°
Altitude
233.81 km
Speed
7.758 km/s
True Right ascension
22h 40m 12s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
No trajectory is available.
Visualization observer readout
No trajectory is available.
Orbital elements
Apogee altitude
234.031 km
Perigee altitude
191.645 km
Semi-major axis
6,590.975 km
Eccentricity
0.00322
Inclination
89.4576°
RAAN
340.0535°
Arg. of periapsis
132.6673°
True anomaly
227.46256°
Mean anomaly
227.7345°
Eccentric anomaly
227.59845°
Mean motion
4.05619 °/min
Orbital period
88.75 mins
BSTAR
0.0042151
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Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)
CZ-6A DEB Visibility
Observer location: undefined°, undefined°
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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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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Authenticating...
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