LES 2 AKM, 2529
Orbit data source: Space-Track
LES 2 AKM, 2529 is space debris in HEO originally from a launch on Thu, 06 May 1965 UTC launched from the Air Force Eastern Test Range (AFETR). 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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2529 intel report (Beta)
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Edit Public Description
| Identifier | |
| Orbit | HEO |
| Last TLE update | 2 days ago |
| Origin | |
| Manufacturer | Thiokol/TE |
| Mission | Spacecraft |
| Bus & Motor | STAR 13, STAR 13 |
| Mass | ~127 kg wet, ~97 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Sphere + Cone, 1 m |
| Radar Cross Section | 0.464 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 2 days ago
0 LES 2 AKM
1 02529U 65034D 25076.54454318 -.00000025 00000-0 00000-0 0 9998
2 02529 32.1501 285.8878 3970727 10.7202 355.7789 4.64844114999316Epoch: 2025-03-17T13:04Z
Definitive object data (Epoch: 2025-03-17T13:04:08.53Z)
| Latitude | -0.00004° |
| Longitude | -85.50831° |
| Altitude | 2,812.814 km |
| Speed | 7.776 km/s |
| True Right ascension | 19h 03m 32s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 24.71734° |
| Longitude | 46.6426° |
| Altitude | 9,112.467 km |
| Speed | 5.019 km/s |
| Apparent Right ascension | 02h 37m 39s |
| Apparent Declination | 11° 51' 06" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 07:03:55 |
| Azimuth | 264.136° W |
| Elevation | 25.487° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 14,812.537 km |
| Perigee altitude | 2,767.01 km |
| Semi-major axis | 15,167.911 km |
| Eccentricity | 0.3970727 |
| Inclination | 32.1501° |
| RAAN | 285.8878° |
| Arg. of periapsis | 10.7202° |
| True anomaly | 349.37762° |
| Mean anomaly | 355.7789° |
| Eccentric anomaly | 353.0104° |
| Mean motion | 1.16186 °/min |
| BSTAR | Unknown |
| Orbital period | 309.85 mins |
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Other satellites on launch #34 in the year 1965 (1965-05-06 UTC)
| TITAN 3A TRANSTAGE R/B, 1359 |
| LES 2, 1360 |
| LCS 1, 1361 |
LES 2 AKM 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. |
|---|---|---|---|---|---|---|---|
| 146 mins | 2025-03-19 02:16:50.696Z | 264.079° W | 2025-03-19 02:52:50.696Z | 230.208° WSW | 30.487° | 2025-03-19 04:42:50.696Z | 180.232° SSW |
| 41 mins | 2025-03-19 16:48:50.696Z | 219.063° SW | 2025-03-19 17:01:50.696Z | 145.214° SSE | 37.614° | 2025-03-19 17:29:50.696Z | 80.421° E |
| 145 mins | 2025-03-19 22:19:50.696Z | 273.285° WNW | 2025-03-19 22:48:50.696Z | 197.814° SSW | 42.547° | 2025-03-20 00:44:50.696Z | 136.231° SSE |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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