COSMOS 1275 DEB, 42168
Orbit data source: Space-Track
COSMOS 1275 DEB, 42168 is space debris in LEO originally from a launch on Thu, 04 Jun 1981 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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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42168 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 COSMOS 1275 DEB
1 42168U 81053SG 24244.18236854 .00069334 00000-0 11748-1 0 9998
2 42168 82.7880 45.7953 0008919 236.3536 123.6822 14.68857209567332
Epoch: 2024-08-31T04:22Z
TLE epoch observation values (Epoch: 2024-08-31T04:22:36.641Z)
Latitude
-0°
Longitude
0.29794°
Altitude
671.233 km
Speed
7.519 km/s
True Right ascension
03h 03m 10s
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
08:10:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
668.024 km
Perigee altitude
655.466 km
Semi-major axis
7,039.882 km
Eccentricity
0.00089
Inclination
82.788°
RAAN
45.7953°
Arg. of periapsis
236.3536°
True anomaly
123.76719°
Mean anomaly
123.6822°
Eccentric anomaly
123.7247°
Mean motion
3.67447 °/min
Orbital period
97.97 mins
BSTAR
0.011748
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Other satellites on launch #53 in the year 1981 (1981-06-04 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.COSMOS 1275 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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COSMOS 1275 DEB is likely not visible in the next few days. |
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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