EKRAN 2 DEB, 59988
Orbit data source: Space-Track
EKRAN 2 DEB, 59988 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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59988 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
3 days 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 3 days ago
0 EKRAN 2 DEB
1 59988U 77092P 25127.47336146 -.00000354 00000-0 00000-0 0 9998
2 59988 4.9751 277.4184 0046090 75.7505 149.6985 1.00881921 70951Epoch: 2025-05-07T11:21Z
Definitive object data (Epoch: 2025-05-07T11:21:38.43Z)
Latitude
-3.58354°
Longitude
107.05607°
Altitude
35,783.332 km
Speed
3.069 km/s
True Right ascension
09h 32m 05s
True Declination
-3° 34' 48"
Sunlit
Visualization TLE readout
Latitude
4.99495°
Longitude
-27.83541°
Altitude
35,428.647 km
Speed
3.095 km/s
Apparent Right ascension
00h 17m 24s
Apparent Declination
0° 32' 45"
Sunlit
Visualization observer readout
Local Sidereal Time
10:01:07
Azimuth
313.097° NW
Elevation
-39.896°
Doppler factor
1
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59988 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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