COSMOS 2499 DEB, 60619 (Decayed)
Orbit data source: Space-Track
COSMOS 2499 DEB, 60619 was space debris in LEO originally from a launch on Fri, 23 May 2014 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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60619 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 2499 DEB
1 60619U 14028CF 24365.21377028 .00340160 00000-0 17403+0 0 9995
2 60619 82.3166 177.0861 0257196 281.7148 75.5267 13.98020424 95156Epoch: 2024-12-30T05:07Z
TLE epoch observation values (Epoch: 2024-12-30T05:07:49.752Z)
Latitude
-0.00004°
Longitude
0.98982°
Altitude
861.335 km
Speed
7.443 km/s
True Right ascension
11h 48m 20s
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
03:22:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,084.932 km
Perigee altitude
710.663 km
Semi-major axis
7,275.935 km
Eccentricity
0.02572
Inclination
82.3166°
RAAN
177.0861°
Arg. of periapsis
281.7148°
True anomaly
78.40231°
Mean anomaly
75.5267°
Eccentric anomaly
76.96234°
Mean motion
3.49712 °/min
Orbital period
102.94 mins
BSTAR
0.17403
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Other satellites on launch #28 in the year 2014 (2014-05-23 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 2499 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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