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)
LES 2 AKM details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 4 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 4 days ago
0 LES 2 AKM
1 02529U 65034D 24365.33157028 -.00000049 00000-0 00000-0 0 9999
2 02529 32.2137 330.2364 3971637 302.9961 24.8470 4.64844554995726Epoch: 2024-12-30T07:57Z
Definitive object data (Epoch: 2024-12-30T07:57:27.672Z)
| Latitude | -0.00008° |
| Longitude | 111.60409° |
| Altitude | 4,118.968 km |
| Speed | 7.047 km/s |
| True Right ascension | 22h 00m 53s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -16.54994° |
| Longitude | -42.42324° |
| Altitude | 6,760.469 km |
| Speed | 5.866 km/s |
| Apparent Right ascension | 11h 24m 16s |
| Apparent Declination | -24° 15' 27" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 22:31:07 |
| Azimuth | 320.503° NNW |
| Elevation | -70.763° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 14,813.896 km |
| Perigee altitude | 2,765.621 km |
| Semi-major axis | 15,167.896 km |
| Eccentricity | 0.3971637 |
| Inclination | 32.2137° |
| RAAN | 330.2364° |
| Arg. of periapsis | 302.9961° |
| True anomaly | 56.98008° |
| Mean anomaly | 24.847° |
| Eccentric anomaly | 39.24237° |
| 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, 2529 |
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. |
|---|---|---|---|---|---|---|---|
| 138 mins | 2025-01-02 23:44:19.729Z | 213.579° SW | 2025-01-03 00:13:19.729Z | 137.581° SSE | 39.852° | 2025-01-03 02:02:19.729Z | 80.135° E |
| 199 mins | 2025-01-03 05:25:19.729Z | 274.102° WNW | 2025-01-03 06:57:19.729Z | 212.585° SW | 43.054° | 2025-01-03 08:44:19.729Z | 142.324° SSE |
| 21 mins | 2025-01-03 20:27:19.729Z | 128.393° SE | 2025-01-03 20:35:19.729Z | 110.067° ESE | 12.235° | 2025-01-03 20:48:19.729Z | 89.764° E |
Authenticating...
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