EKRAN 2 DEB, 59986

Orbit data source: Space-Track

EKRAN 2 DEB, 59986 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	59986, 1977-092M
Orbit	GEO
Last TLE update	18 hours 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 18 hours ago

0 EKRAN 2 DEB
1 59986U 77092M   25035.55939207 -.00000320  00000-0  00000-0 0  9993
2 59986   5.0506 278.2805 0040512  97.0117  53.9381  1.00942064 41509

Epoch: 2025-02-04T13:25Z

Definitive object data (Epoch: 2025-02-04T13:25:31.474Z)

Latitude	2.41906°
Longitude	93.38776°
Altitude	35,500.07 km
Speed	3.089 km/s
True Right ascension	04h 38m 55s
True Declination	2° 24' 60"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	4.66775°
Longitude	9.86069°
Altitude	35,450.013 km
Speed	3.093 km/s
Apparent Right ascension	22h 56m 41s
Apparent Declination	0° 49' 44"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	09:46:31
Azimuth	333.351° NNW
Elevation	-47.775°
Doppler factor	1

Orbital elements

Apogee altitude	35,770.86 km
Perigee altitude	35,430.73 km
Semi-major axis	41,978.932 km
Eccentricity	0.0040512
Inclination	5.0506°
RAAN	278.2805°
Arg. of periapsis	97.0117°
True anomaly	54.3145°
Mean anomaly	53.9381°
Eccentric anomaly	54.12619°
Mean motion	0.25235 °/min
BSTAR	Unknown
Orbital period	1426.61 mins