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.

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Identifier
59986, 1977-092M
Orbit
GEO
Country
Flag of CISCIS
Related business
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
RCS unknown

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 EKRAN 2 DEB
1 59986U 77092M   25255.49592520 -.00000208  00000-0  00000-0 0  9998
2 59986   4.4915 275.0768 0037011 109.8556  44.9328  1.00942123 43721
Epoch: 2025-09-12T11:54Z
TLE epoch observation values (Epoch: 2025-09-12T11:54:07.937Z)
Latitude
1.87216°
Longitude
-100.04201°
Altitude
35,489.542 km
Speed
3.09 km/s
True Right ascension
04h 40m 56s
True Declination
1° 52' 13"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:25:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,756.149 km
Perigee altitude
35,445.413 km
Semi-major axis
41,978.918 km
Eccentricity
0.0037
Inclination
4.4915°
RAAN
275.0768°
Arg. of periapsis
109.8556°
True anomaly
45.23333°
Mean anomaly
44.9328°
Eccentric anomaly
45.08296°
Mean motion
0.25235 °/min
Orbital period
1,426.61 mins
BSTAR
0
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