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: 1 week ago
TLE from 1 week ago
0 LES 2
1 01360U 65034B 25327.94933094 .00000011 00000-0 00000-0 0 9990
2 01360 32.1047 141.9486 3961779 230.3386 87.4729 4.64830697 28328Epoch: 2025-11-23T22:47Z
TLE epoch observation values (Epoch: 2025-11-23T22:47:02.193Z)
Latitude
-0.00006°
Longitude
97.01746°
Altitude
10,731.571 km
Speed
4.507 km/s
True Right ascension
09h 27m 43s
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
16:54:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
14,799.374 km
Perigee altitude
2,780.76 km
Semi-major axis
15,168.204 km
Eccentricity
0.39618
Inclination
32.1047°
RAAN
141.9486°
Arg. of periapsis
230.3386°
True anomaly
129.69235°
Mean anomaly
87.4729°
Eccentric anomaly
108.94289°
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. |
|---|---|---|---|---|---|---|---|
| 75 mins | 2025-12-03 22:36:00.481Z | 288.544° WNW | 2025-12-03 23:30:00.481Z | 243.106° WSW | 24.538° | 2025-12-03 23:51:00.481Z | 189.985° SSW |
| 192 mins | 2025-12-04 11:21:00.481Z | 201.886° SSW | 2025-12-04 12:45:00.481Z | 130.092° SE | 40.045° | 2025-12-04 14:33:00.481Z | 78.626° E |
| 93 mins | 2025-12-04 17:31:00.481Z | 268.587° W | 2025-12-04 19:04:00.481Z | 263.313° W | 37.975° | 2025-12-04 19:04:00.481Z | 263.313° W |
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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