EKRAN 2 DEB, 29014

Orbit data source: Space-Track

EKRAN 2 DEB, 29014 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.

Not visible in the next 10 days

EKRAN 2 DEB details

Identifier	29014, 1977-092K
Orbit	GEO
Last TLE update	1 day ago
Origin	GUKOS RVSN (CIS)
Manufacturer	Unknown
Mission	Spacecraft
Bus & Motor	Unknown
Mass	Unknown
Launch date (UTC)	1977-09-20 (47 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 1 day ago

0 EKRAN 2 DEB
1 29014U 77092K   25035.12481587  .00000057  00000-0  00000-0 0  9994
2 29014   5.4134 280.9206 0019122 333.7385 348.3248  1.00102860 42285

Epoch: 2025-02-04T02:59Z

Definitive object data (Epoch: 2025-02-04T02:59:44.091Z)

Latitude	-3.32543°
Longitude	63.62255°
Altitude	35,755.192 km
Speed	3.079 km/s
True Right ascension	16h 12m 21s
True Declination	-3° 19' 19"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	3.13671°
Longitude	136.95735°
Altitude	35,794.748 km
Speed	3.076 km/s
Apparent Right ascension	21h 10m 40s
Apparent Declination	-2° 09' 19"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	09:53:41
Azimuth	17.23° NNE
Elevation	-50.998°
Doppler factor	1

Orbital elements

Apogee altitude	35,915.793 km
Perigee altitude	35,754.353 km
Semi-major axis	42,213.21 km
Eccentricity	0.0019122
Inclination	5.4134°
RAAN	280.9206°
Arg. of periapsis	333.7385°
True anomaly	348.28035°
Mean anomaly	348.3248°
Eccentric anomaly	348.30259°
Mean motion	0.25025 °/min
BSTAR	Unknown
Orbital period	1438.57 mins