METEOR 2-7 DEB, 28599 (Decayed)
Orbit data source: Space-Track
METEOR 2-7 DEB, 28599 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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28599 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 28599U 81043H 24251.55762310 .00808792 00000-0 22954-1 0 9999
2 28599 81.1962 341.9106 0031102 268.6768 91.0907 15.33400417156912Epoch: 2024-09-07T13:22Z
TLE epoch observation values (Epoch: 2024-09-07T13:22:58.635Z)
Latitude
-0.00004°
Longitude
154.05219°
Altitude
469.212 km
Speed
7.631 km/s
True Right ascension
22h 47m 38s
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
00:38:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.966 km
Perigee altitude
441.413 km
Semi-major axis
6,840.826 km
Eccentricity
0.00311
Inclination
81.1962°
RAAN
341.9106°
Arg. of periapsis
268.6768°
True anomaly
91.44701°
Mean anomaly
91.0907°
Eccentric anomaly
91.26886°
Mean motion
3.83602 °/min
Orbital period
93.85 mins
BSTAR
0.022954
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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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