EKRAN 2 DEB, 29014
Orbit data source: Space-Track
EKRAN 2 DEB, 29014 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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29014 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 EKRAN 2 DEB
1 29014U 77092K 26171.21162073 -.00000053 00000-0 00000+0 0 9998
2 29014 4.1256 274.2224 0019612 347.8516 252.0329 1.00158958 47306Epoch: 2026-06-20T05:04Z
TLE epoch observation values (Epoch: 2026-06-20T05:04:44.031Z)
Latitude
-3.55813°
Longitude
169.22089°
Altitude
35,844.138 km
Speed
3.072 km/s
True Right ascension
10h 15m 20s
True Declination
-3° 33' 16"
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
01:06:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,902.073 km
Perigee altitude
35,736.558 km
Semi-major axis
42,197.453 km
Eccentricity
0.00196
Inclination
4.1256°
RAAN
274.2224°
Arg. of periapsis
347.8516°
True anomaly
251.81928°
Mean anomaly
252.0329°
Eccentric anomaly
251.92608°
Mean motion
0.25039 °/min
Orbital period
1,437.77 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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29014 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 descending 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 descending order |
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