EKRAN 2 DEB, 11581
Orbit data source: Space-Track
EKRAN 2 DEB, 11581 is space debris in GEO originally from a launch on Tue, 20 Sep 1977 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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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11581 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
23 hours ago
Origin
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
Large (>1 m²)
Expand to show TLE details & history
TLE from 23 hours ago
0 EKRAN 2 DEB
1 11581U 77092H 25129.10439425 .00000150 00000-0 00000-0 0 9994
2 11581 5.1756 279.5335 0009093 213.2249 172.6665 1.00191710100318Epoch: 2025-05-09T02:30Z
Definitive object data (Epoch: 2025-05-09T02:30:19.663Z)
Latitude
2.27981°
Longitude
40.5868°
Altitude
35,846.15 km
Speed
3.071 km/s
True Right ascension
20h 21m 20s
True Declination
2° 16' 39"
Sunlit
Visualization TLE readout
Latitude
1.04455°
Longitude
26.2037°
Altitude
35,843.735 km
Speed
3.071 km/s
Apparent Right ascension
19h 37m 32s
Apparent Declination
-4° 04' 34"
Sunlit
Visualization observer readout
Local Sidereal Time
09:41:48
Azimuth
46.197° ENE
Elevation
-44.499°
Doppler factor
1
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11581 neighbors
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Other satellites on launch #92 in the year 1977 (1977-09-20 UTC)
EKRAN 2 DEB Visibility forecast
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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