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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Identifier
Orbit
Country
USRelated business
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
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 LES 2 AKM
1 2529U 65034D 26057.48338796 -.00000012 00000-0 00000+0 0 9997
2 2529 32.1331 86.9588 3972514 314.1917 19.3013 4.64843932 15369Epoch: 2026-02-26T11:36Z
TLE epoch observation values (Epoch: 2026-02-26T11:36:04.719Z)
Latitude
-0°
Longitude
116.6214°
Altitude
3,630.533 km
Speed
7.306 km/s
True Right ascension
05h 47m 53s
True Declination
0° 00' 00"
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
04:17:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
14,815.256 km
Perigee altitude
2,764.304 km
Semi-major axis
15,167.917 km
Eccentricity
0.39725
Inclination
32.1331°
RAAN
86.9588°
Arg. of periapsis
314.1917°
True anomaly
45.83327°
Mean anomaly
19.3013°
Eccentric anomaly
31.03638°
Mean motion
1.16186 °/min
Orbital period
309.85 mins
BSTAR
0
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Other satellites on launch #34 in the year 1965 (1965-05-06 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.LES 2 AKM 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. |
|---|---|---|---|---|---|---|---|
| 60 mins | 2026-03-04 01:48:58.969Z | 178.417° S | 2026-03-04 02:05:58.969Z | 122.157° SE | 26.473° | 2026-03-04 02:48:58.969Z | 72.711° E |
| 187 mins | 2026-03-04 07:16:58.969Z | 258.026° W | 2026-03-04 08:04:58.969Z | 179.067° S | 44.345° | 2026-03-04 10:23:58.969Z | 118.256° SE |
| 166 mins | 2026-03-04 13:19:58.969Z | 287.283° WNW | 2026-03-04 14:43:58.969Z | 249.8° W | 27.42° | 2026-03-04 16:05:58.969Z | 194.319° SSW |
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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