EKRAN 2 DEB, 59986
Orbit data source: Space-Track
EKRAN 2 DEB, 59986 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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59986 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
12 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
RCS unknown
Expand to show TLE details & history
TLE from 12 hours ago
0 EKRAN 2 DEB
1 59986U 77092M 25187.58337576 -.00000315 00000-0 00000-0 0 9999
2 59986 4.6608 276.0693 0040100 109.8581 206.0100 1.00941560 43038Epoch: 2025-07-06T14:00Z
TLE epoch observation values (Epoch: 2025-07-06T14:00:03.665Z)
Latitude
-3.27639°
Longitude
97.0067°
Altitude
35,750.931 km
Speed
3.07 km/s
True Right ascension
15h 27m 18s
True Declination
-3° 16' 23"
Sunlit
Visualization orbit readout
Latitude
2.88754°
Longitude
-76.64041°
Altitude
35,456.682 km
Speed
3.092 km/s
Apparent Right ascension
03h 42m 55s
Apparent Declination
-2° 25' 50"
Sunlit
Visualization observer readout
Local Sidereal Time
14:17:31
Azimuth
327.205° NNW
Elevation
-47.809°
Doppler factor
1
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Other satellites on launch #92 in the year 1977 (1977-09-20 UTC)
EKRAN 2 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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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