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: 3 weeks ago
TLE from 3 weeks ago
0 LES 2
1 01360U 65034B 25303.44486447 -.00000001 00000-0 00000-0 0 9994
2 01360 32.1004 156.0095 3959177 208.8319 121.9904 4.64830648 27187Epoch: 2025-10-30T10:40Z
TLE epoch observation values (Epoch: 2025-10-30T10:40:36.290Z)
Latitude
-0.00002°
Longitude
-43.13641°
Altitude
13,200.606 km
Speed
3.8 km/s
True Right ascension
10h 24m 04s
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
13:10:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
14,795.428 km
Perigee altitude
2,784.707 km
Semi-major axis
15,168.204 km
Eccentricity
0.39592
Inclination
32.1004°
RAAN
156.0095°
Arg. of periapsis
208.8319°
True anomaly
151.19941°
Mean anomaly
121.9904°
Eccentric anomaly
137.35736°
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. |
|---|---|---|---|---|---|---|---|
| 153 mins | 2025-11-19 16:14:55.588Z | 234.036° WSW | 2025-11-19 17:46:55.588Z | 172.074° S | 44.295° | 2025-11-19 18:47:55.588Z | 97.81° ESE |
| 81 mins | 2025-11-19 22:57:55.588Z | 287.867° WNW | 2025-11-19 23:57:55.588Z | 234.859° WSW | 30.901° | 2025-11-20 00:18:55.588Z | 170.388° S |
| 187 mins | 2025-11-20 11:48:55.588Z | 190.508° SSW | 2025-11-20 13:18:55.588Z | 123.278° SE | 37.055° | 2025-11-20 14:55:55.588Z | 75.097° E |
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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