**LES 8 9/SOL 11A B DEB *, 13753**

Orbit data source: Space-Track

LES 8 9/SOL 11A B DEB *, 13753 is space debris in GEO originally from a launch on Mon, 15 Mar 1976 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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LES 8 9/SOL 11A B DEB * details

Identifier	13753, 1976-023K
Orbit	GEO
Last TLE update	1 day ago
Origin	SAMSO (US)
Manufacturer	Unknown
Mission	LES 9 operational debris"
Bus & Motor	Unknown
Mass	Unknown
Launch date (UTC)	1976-03-15 (49 years ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 LES 8 9/SOL 11A B DEB *
1 13753U 76023K   25035.30526662 -.00000191  00000-0  00000-0 0  9994
2 13753   6.0619 286.3891 0003179  34.7586 176.1218  1.01345611117460

Epoch: 2025-02-04T07:19Z

Definitive object data (Epoch: 2025-02-04T07:19:35.035Z)

Latitude	-3.09763°
Longitude	-107.44599°
Altitude	35,501.519 km
Speed	3.085 km/s
True Right ascension	09h 08m 38s
True Declination	-3° 05' 40"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-2.97451°
Longitude	-108.78563°
Altitude	35,501.469 km
Speed	3.085 km/s
Apparent Right ascension	09h 04m 04s
Apparent Declination	-9° 35' 39"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	08:57:22
Azimuth	177.83° S
Elevation	40.465°
Doppler factor	1

Orbital elements

Apogee altitude	35,502.593 km
Perigee altitude	35,475.974 km
Semi-major axis	41,867.421 km
Eccentricity	0.0003179
Inclination	6.0619°
RAAN	286.3891°
Arg. of periapsis	34.7586°
True anomaly	176.12426°
Mean anomaly	176.1218°
Eccentric anomaly	176.12303°
Mean motion	0.25335 °/min
BSTAR	Unknown
Orbital period	1420.93 mins