LES 2, 1360
Orbit data source: Space-Track
LES 2, 1360 is a payload satellite owned by USAF SSD (US) in HEO that was launched on Thu, 06 May 1965 UTC via a TITAN IIIA 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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1360 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
MIT-LL
Mission
Spacecraft
Bus & Motor
LES, STAR 13A
Mass
37 kg wet, 37 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LES 2
1 01360U 65034B 25292.91387953 -.00000011 00000-0 00000-0 0 9996
2 01360 32.0797 162.0761 3958287 199.5626 139.5710 4.64830466 26693Epoch: 2025-10-19T21:55Z
TLE epoch observation values (Epoch: 2025-10-19T21:55:59.191Z)
Latitude
0.00001°
Longitude
164.47063°
Altitude
14,020.077 km
Speed
3.578 km/s
True Right ascension
10h 48m 21s
True Declination
0° 00' 00"
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
09:47:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
14,794.086 km
Perigee altitude
2,786.06 km
Semi-major axis
15,168.21 km
Eccentricity
0.39583
Inclination
32.0797°
RAAN
162.0761°
Arg. of periapsis
199.5626°
True anomaly
160.46761°
Mean anomaly
139.571°
Eccentric anomaly
150.67759°
Mean motion
1.16183 °/min
Orbital period
309.86 mins
BSTAR
0
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Other satellites on launch #34 in the year 1965 (1965-05-06 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 2 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. |
|---|---|---|---|---|---|---|---|
| 25 mins | 2025-10-20 14:50:12.342Z | 89.455° E | 2025-10-20 14:50:12.342Z | 89.455° E | 19.129° | 2025-10-20 15:15:12.342Z | 76.45° E |
| 176 mins | 2025-10-20 18:20:12.342Z | 233.981° WSW | 2025-10-20 20:35:12.342Z | 172.166° S | 44.064° | 2025-10-20 21:16:12.342Z | 93.677° ESE |
| 52 mins | 2025-10-21 01:53:12.342Z | 284.89° WNW | 2025-10-21 02:30:12.342Z | 226.526° WSW | 31.359° | 2025-10-21 02:45:12.342Z | 163.613° S |
| 24 mins | 2025-10-21 14:26:12.342Z | 189.893° SSW | 2025-10-21 14:50:12.342Z | 177.704° S | 22.995° | 2025-10-21 14:50:12.342Z | 177.704° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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