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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Identifier
2529, 1965-034D
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 13, STAR 13
Mass
~127 kg wet, ~97 kg dry
Launch date (UTC)
1965-05-06 (61 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
SPHERE + CONE, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 LES 2 AKM
1 02529U 65034D   26276.40360461 -.00000032  00000-0  00000-0 0  9999
2 02529  32.1957 321.2252 3965262 146.0644 247.1799  4.64837776 25549
Epoch: 2026-10-03T09:41Z
TLE epoch observation values (Epoch: 2026-10-03T09:41:11.438Z)
Latitude
-0.00003°
Longitude
163.82375°
Altitude
12,665.463 km
Speed
3.948 km/s
True Right ascension
21h 24m 55s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:55:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
14,804.432 km
Perigee altitude
2,775.379 km
Semi-major axis
15,168.043 km
Eccentricity
0.39653
Inclination
32.1957°
RAAN
321.2252°
Arg. of periapsis
146.0644°
True anomaly
213.95353°
Mean anomaly
247.1799°
Eccentric anomaly
229.8215°
Mean motion
1.16185 °/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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