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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Edit Public Description
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
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 EKRAN 2 DEB
1 29014U 77092K 25255.86395267 -.00000284 00000-0 00000-0 0 9991
2 29014 4.8511 278.0012 0019700 336.4793 5.2550 1.00138495 44498Epoch: 2025-09-12T20:44Z
TLE epoch observation values (Epoch: 2025-09-12T20:44:05.51Z)
Latitude
-1.50029°
Longitude
-43.31347°
Altitude
35,741.27 km
Speed
3.079 km/s
True Right ascension
17h 19m 15s
True Declination
-1° 29' 56"
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
21:24:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,908.201 km
Perigee altitude
35,741.92 km
Semi-major axis
42,203.198 km
Eccentricity
0.00197
Inclination
4.8511°
RAAN
278.0012°
Arg. of periapsis
336.4793°
True anomaly
5.27573°
Mean anomaly
5.255°
Eccentric anomaly
5.26536°
Mean motion
0.25034 °/min
Orbital period
1,438.06 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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 561 mins | 2025-09-13 04:55:26.233Z | 105.259° ESE | 2025-09-13 04:55:26.233Z | 105.259° ESE | 15.499° | 2025-09-13 14:16:26.233Z | 112.859° SE |
| 659 mins | 2025-09-13 17:56:26.233Z | 112.562° SE | 2025-09-14 03:56:26.233Z | 105.476° ESE | 15.927° | 2025-09-14 04:55:26.233Z | 105.621° ESE |
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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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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