METEOR 2-5 DEB, 35254 (Decayed)
Orbit data source: Space-Track
METEOR 2-5 DEB, 35254 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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35254 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 METEOR 2-5 DEB
1 35254U 79095V 25266.76251132 .00582778 00000-0 10032-1 0 9991
2 35254 81.1824 77.1480 0005072 310.5547 49.5257 15.48943637636907
Epoch: 2025-09-23T18:18Z
TLE epoch observation values (Epoch: 2025-09-23T18:18:00.978Z)
Latitude
-0.00002°
Longitude
159.79623°
Altitude
420.662 km
Speed
7.66 km/s
True Right ascension
05h 08m 35s
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
11:24:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
420.256 km
Perigee altitude
413.363 km
Semi-major axis
6,794.946 km
Eccentricity
0.00051
Inclination
81.1824°
RAAN
77.148°
Arg. of periapsis
310.5547°
True anomaly
49.56993°
Mean anomaly
49.5257°
Eccentric anomaly
49.54781°
Mean motion
3.87493 °/min
Orbital period
92.9 mins
BSTAR
0.010032
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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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