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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: 1 day ago

TLE from 1 day ago
0 LES 8
1 08746U 76023A   25331.20342023 -.00000109  00000-0  00000-0 0  9994
2 08746  22.0242  39.6135 0033239 154.2307 203.0087  1.00272852127656
Epoch: 2025-11-27T04:52Z
TLE epoch observation values (Epoch: 2025-11-27T04:52:55.507Z)
Latitude
-1.09516°
Longitude
-102.69552°
Altitude
35,915.226 km
Speed
3.065 km/s
True Right ascension
02h 27m 35s
True Declination
-1° 05' 39"
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
09:49:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,927.299 km
Perigee altitude
35,646.993 km
Semi-major axis
42,165.283 km
Eccentricity
0.00332
Inclination
22.0242°
RAAN
39.6135°
Arg. of periapsis
154.2307°
True anomaly
202.86039°
Mean anomaly
203.0087°
Eccentric anomaly
202.93449°
Mean motion
0.25067 °/min
Orbital period
1,436.12 mins
BSTAR
0
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