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LES 8, 8746

Orbit data source: Space-Track

LES 8, 8746 is a payload satellite owned by SAMSO (US) in GEO that was launched on Mon, 15 Mar 1976 UTC via a TITAN IIIC launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
8746, 1976-023A
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
MIT-LL
Mission
Non-operational spacecraft
Bus & Motor
LES, Unknown motor
Mass
420 kg wet, 366 kg dry
Launch date (UTC)
1976-03-15 (50 years ago)
Launch vehicle
TITAN IIIC
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
Last TLE update: 2 days ago

TLE from 2 days ago
0 LES 8
1 08746U 76023A   25357.13927816 -.00000112  00000-0  00000-0 0  9997
2 08746  22.0716  39.2810 0032915 155.2534 204.7250  1.00271960127919
Epoch: 2025-12-23T03:20Z
TLE epoch observation values (Epoch: 2025-12-23T03:20:33.633Z)
Latitude
-0.08127°
Longitude
-102.95857°
Altitude
35,911.795 km
Speed
3.066 km/s
True Right ascension
02h 36m 26s
True Declination
0° 04' 52"
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
08:28:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,926.183 km
Perigee altitude
35,648.607 km
Semi-major axis
42,165.532 km
Eccentricity
0.00329
Inclination
22.0716°
RAAN
39.281°
Arg. of periapsis
155.2534°
True anomaly
204.56783°
Mean anomaly
204.725°
Eccentric anomaly
204.64636°
Mean motion
0.25067 °/min
Orbital period
1,436.14 mins
BSTAR
0
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