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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59986 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 EKRAN 2 DEB
1 59986U 77092M 25305.68565771 .00000145 00000-0 00000-0 0 9992
2 59986 4.3614 274.3558 0036514 107.3122 285.9953 1.00935026 44236Epoch: 2025-11-01T16:27Z
TLE epoch observation values (Epoch: 2025-11-01T16:27:20.826Z)
Latitude
2.38916°
Longitude
19.09159°
Altitude
35,559.4 km
Speed
3.085 km/s
True Right ascension
20h 28m 33s
True Declination
2° 23' 12"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:10:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,756.038 km
Perigee altitude
35,449.46 km
Semi-major axis
41,980.886 km
Eccentricity
0.00365
Inclination
4.3614°
RAAN
274.3558°
Arg. of periapsis
107.3122°
True anomaly
285.59258°
Mean anomaly
285.9953°
Eccentric anomaly
285.79399°
Mean motion
0.25233 °/min
Orbital period
1,426.71 mins
BSTAR
0
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Other satellites on launch #92 in the year 1977 (1977-09-20 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.EKRAN 2 DEB Visibility
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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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| EKRAN 2 DEB is likely not visible in the next few days. |
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59986 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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