METEOR 2-6 DEB, 28987
Orbit data source: Space-Track
METEOR 2-6 DEB, 28987 is space debris in LEO originally from a launch on Tue, 09 Sep 1980 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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28987 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Unknown
Mission
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 2-6 DEB
1 28987U 80073D 24256.56012434 .00127396 00000-0 31494-1 0 9996
2 28987 81.2089 196.2217 0028514 64.7240 295.6903 14.50948629 49886Epoch: 2024-09-12T13:26Z
TLE epoch observation values (Epoch: 2024-09-12T13:26:34.742Z)
Latitude
-0.00005°
Longitude
2.53214°
Altitude
716.774 km
Speed
7.502 km/s
True Right ascension
13h 04m 53s
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
07:44:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
739.912 km
Perigee altitude
699.434 km
Semi-major axis
7,097.81 km
Eccentricity
0.00285
Inclination
81.2089°
RAAN
196.2217°
Arg. of periapsis
64.724°
True anomaly
295.3954°
Mean anomaly
295.6903°
Eccentric anomaly
295.54289°
Mean motion
3.62958 °/min
Orbital period
99.18 mins
BSTAR
0.031494
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Other satellites on launch #73 in the year 1980 (1980-09-09 UTC)
METEOR 2-6 DEB Visibility
Observer location: undefined°, undefined°
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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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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Authenticating...
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