EKRAN 2 DEB, 59988

Orbit data source: Space-Track

EKRAN 2 DEB, 59988 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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EKRAN 2 DEB details

Identifier	59988, 1977-092P
Orbit	GEO
Last TLE update	23 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 23 hours ago

0 EKRAN 2 DEB
1 59988U 77092P   25035.23628352 -.00000212  00000-0  00000-0 0  9996
2 59988   5.2134 278.7074 0050400  48.4732 157.4221  1.00884055 70020

Epoch: 2025-02-04T05:40Z

Definitive object data (Epoch: 2025-02-04T05:40:14.896Z)

Latitude	-2.28379°
Longitude	-94.94529°
Altitude	35,812.145 km
Speed	3.067 km/s
True Right ascension	08h 19m 02s
True Declination	-2° 16' 53"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-1.48484°
Longitude	-104.38018°
Altitude	35,795.973 km
Speed	3.068 km/s
Apparent Right ascension	07h 47m 45s
Apparent Declination	-7° 51' 40"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	06:51:38
Azimuth	161.593° S
Elevation	40.493°
Doppler factor	1

Orbital elements

Apogee altitude	35,828.539 km
Perigee altitude	35,405.229 km
Semi-major axis	41,995.021 km
Eccentricity	0.00504
Inclination	5.2134°
RAAN	278.7074°
Arg. of periapsis	48.4732°
True anomaly	157.64256°
Mean anomaly	157.4221°
Eccentric anomaly	157.53246°
Mean motion	0.2522 °/min
BSTAR	Unknown
Orbital period	1427.43 mins