METEOR 2-7 DEB, 36875 (Decayed)
Orbit data source: Space-Track
METEOR 2-7 DEB, 36875 was space debris in LEO originally from a launch on Thu, 14 May 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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36875 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 METEOR 2-7 DEB
1 36875U 81043N 24131.76546284 .00075839 00000-0 88281-2 0 9999
2 36875 81.2364 147.0032 0005462 117.9200 242.2566 14.84868314 63664Epoch: 2024-05-10T18:22Z
TLE epoch observation values (Epoch: 2024-05-10T18:22:15.989Z)
Latitude
0.00003°
Longitude
2.39532°
Altitude
618.78 km
Speed
7.549 km/s
True Right ascension
09h 48m 00s
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
00:37:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.892 km
Perigee altitude
607.257 km
Semi-major axis
6,989.211 km
Eccentricity
0.00055
Inclination
81.2364°
RAAN
147.0032°
Arg. of periapsis
117.92°
True anomaly
242.20122°
Mean anomaly
242.2566°
Eccentric anomaly
242.22891°
Mean motion
3.7145 °/min
Orbital period
96.92 mins
BSTAR
0.0088281
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Other satellites on launch #43 in the year 1981 (1981-05-14 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 2-7 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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