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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59988 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 16 hours ago
0 EKRAN 2 DEB
1 59988U 77092P 25199.32349705 -.00000202 00000-0 00000-0 0 9998
2 59988 4.7946 276.3322 0039157 77.4401 322.7217 1.00883778 71682
Epoch: 2025-07-18T07:45Z
TLE epoch observation values (Epoch: 2025-07-18T07:45:50.145Z)
Latitude
3.05786°
Longitude
-96.7093°
Altitude
35,484.417 km
Speed
3.091 km/s
True Right ascension
21h 04m 30s
True Declination
3° 03' 17"
Sunlit
Visualization orbit readout
Latitude
-4.70662°
Longitude
144.47445°
Altitude
35,766.302 km
Speed
3.07 km/s
Apparent Right ascension
13h 14m 32s
Apparent Declination
-11° 26' 22"
Sunlit
Visualization observer readout
Local Sidereal Time
12:28:50
Azimuth
165.827° S
Elevation
37.56°
Doppler factor
1
Orbital elements
Apogee altitude
35,781.403 km
Perigee altitude
35,452.522 km
Semi-major axis
41,995.1 km
Eccentricity
0.00392
Inclination
4.7946°
RAAN
276.3322°
Arg. of periapsis
77.4401°
True anomaly
322.44886°
Mean anomaly
322.7217°
Eccentric anomaly
322.58539°
Mean motion
0.2522 °/min
Orbital period
1,427.44 mins
BSTAR
0
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Other satellites on launch #92 in the year 1977 (1977-09-20 UTC)
EKRAN 2 DEB Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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1440 mins | 2025-07-18 23:41:11.859Z | 165.832° S | 2025-07-19 10:41:11.859Z | 160.829° S | 36.406° | 2025-07-19 23:41:11.859Z | 162.831° S |
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59988 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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