METEOR 2-5 DEB, 28554 (Decayed)
Orbit data source: Space-Track
METEOR 2-5 DEB, 28554 was space debris in LEO originally from a launch on Wed, 31 Oct 1979 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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28554 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 METEOR 2-5 DEB
1 28554U 79095C 25014.43858491 .00103829 00000-0 82290-2 0 9994
2 28554 81.1756 75.0108 0015688 178.3603 181.7672 14.99943006537227Epoch: 2025-01-14T10:31Z
TLE epoch observation values (Epoch: 2025-01-14T10:31:33.736Z)
Latitude
0.00005°
Longitude
162.97497°
Altitude
580.984 km
Speed
7.564 km/s
True Right ascension
05h 00m 02s
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
03:18:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.022 km
Perigee altitude
553.24 km
Semi-major axis
6,942.268 km
Eccentricity
0.00157
Inclination
81.1756°
RAAN
75.0108°
Arg. of periapsis
178.3603°
True anomaly
181.76167°
Mean anomaly
181.7672°
Eccentric anomaly
181.76443°
Mean motion
3.75224 °/min
Orbital period
95.94 mins
BSTAR
0.008229
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Other satellites on launch #95 in the year 1979 (1979-10-31 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.METEOR 2-5 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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