EKRAN 2 DEB, 12996
Orbit data source: Space-Track
EKRAN 2 DEB, 12996 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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12996 intel report (Beta)
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Edit Public Description
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TLE from 14 hours ago
0 EKRAN 2 DEB
1 12996U 77092J 25199.38359017 .00000140 00000-0 00000-0 0 9999
2 12996 5.1641 279.2916 0018878 264.2625 97.1456 1.00043784 81177
Epoch: 2025-07-18T09:12Z
TLE epoch observation values (Epoch: 2025-07-18T09:12:22.19Z)
Latitude
0.12809°
Longitude
-153.62012°
Altitude
35,860.33 km
Speed
3.072 km/s
True Right ascension
18h 43m 37s
True Declination
0° 07' 41"
Sunlit
Visualization orbit readout
Latitude
-2.74625°
Longitude
57.03609°
Altitude
35,801.208 km
Speed
3.076 km/s
Apparent Right ascension
08h 24m 25s
Apparent Declination
-8° 50' 50"
Sunlit
Visualization observer readout
Local Sidereal Time
12:04:06
Azimuth
239.184° WSW
Elevation
19.686°
Doppler factor
1
Orbital elements
Apogee altitude
35,931.411 km
Perigee altitude
35,771.968 km
Semi-major axis
42,229.826 km
Eccentricity
0.00189
Inclination
5.1641°
RAAN
279.2916°
Arg. of periapsis
264.2625°
True anomaly
97.36018°
Mean anomaly
97.1456°
Eccentric anomaly
97.2529°
Mean motion
0.2501 °/min
Orbital period
1,439.42 mins
BSTAR
0
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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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1440 mins | 2025-07-18 23:16:31.145Z | 239.17° WSW | 2025-07-19 15:04:31.145Z | 245.666° WSW | 23.405° | 2025-07-19 23:16:31.145Z | 239.852° WSW |
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12996 neighbors
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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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