LES 6, 3431
Orbit data source: Space-Track
LES 6, 3431 is a payload satellite owned by SAMSO (US) in GEO that was launched on Thu, 26 Sep 1968 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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3431 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
MIT-LL
Mission
Non-operational spacecraft
Bus & Motor
LES, Unknown motor
Mass
169 kg wet, ~149 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 LES 6
1 03431U 68081D 26070.61525031 .00000129 00000-0 00000-0 0 9994
2 03431 1.3730 34.8730 0010302 300.6559 266.5182 1.00283360119808Epoch: 2026-03-11T14:45Z
TLE epoch observation values (Epoch: 2026-03-11T14:45:57.626Z)
Latitude
-0.60753°
Longitude
-148.82631°
Altitude
35,785.667 km
Speed
3.075 km/s
True Right ascension
16h 07m 45s
True Declination
0° 36' 25"
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
08:22:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,827.856 km
Perigee altitude
35,740.984 km
Semi-major axis
42,162.557 km
Eccentricity
0.00103
Inclination
1.373°
RAAN
34.873°
Arg. of periapsis
300.6559°
True anomaly
266.40037°
Mean anomaly
266.5182°
Eccentric anomaly
266.45929°
Mean motion
0.2507 °/min
Orbital period
1,435.98 mins
BSTAR
0
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Other satellites on launch #81 in the year 1968 (1968-09-26 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 6 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-03-12 04:03:29.148Z | 236.672° WSW | 2026-03-12 06:55:29.148Z | 237.001° WSW | 24.517° | 2026-03-13 04:03:29.148Z | 236.646° WSW |
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3431 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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