EKRAN 2 DEB, 59987

Orbit data source: Space-Track

EKRAN 2 DEB, 59987 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	59987, 1977-092N
Orbit	GEO
Last TLE update	2 days 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	RCS unknown

Expand to show TLE details & history

TLE from 2 days ago

0 EKRAN 2 DEB
1 59987U 77092N   25034.77236572 -.00000221  00000-0  00000-0 0  9992
2 59987   5.4074 280.6740 0013027 211.4085   7.4711  1.00383273 58113

Epoch: 2025-02-03T18:32Z

Definitive object data (Epoch: 2025-02-03T18:32:12.398Z)

Latitude	-3.38196°
Longitude	87.24163°
Altitude	35,700.738 km
Speed	3.08 km/s
True Right ascension	09h 17m 55s
True Declination	-3° 22' 43"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	4.62554°
Longitude	-72.51948°
Altitude	35,803.264 km
Speed	3.072 km/s
Apparent Right ascension	22h 33m 31s
Apparent Declination	0° 49' 22"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	09:47:16
Azimuth	342.018° N
Elevation	-49.513°
Doppler factor	1

Orbital elements

Apogee altitude	35,811.316 km
Perigee altitude	35,701.538 km
Semi-major axis	42,134.564 km
Eccentricity	0.0013027
Inclination	5.4074°
RAAN	280.674°
Arg. of periapsis	211.4085°
True anomaly	7.49054°
Mean anomaly	7.4711°
Eccentric anomaly	7.48082°
Mean motion	0.25095 °/min
BSTAR	Unknown
Orbital period	1434.55 mins