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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Identifier
12996, 1977-092J
Orbit
GEO
Last TLE update
14 hours ago
Origin
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1977-09-20 (48 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

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
Object was in daylight at epoch
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
Object is in daylight
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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