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LES 1, 1002

Orbit data source: Space-Track

LES 1, 1002 is a payload satellite owned by USAF SSD (US) in LEO that was launched on Thu, 11 Feb 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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Identifier
1002, 1965-008C
Orbit
LEO
Last TLE update
11 hours ago
Origin
Manufacturer
MIT-LL
Mission
Defense Communications
Bus & Motor
LES, STAR 13A
Mass
158 kg wet, 31 kg dry
Launch date (UTC)
1965-02-11 (60 years ago)
Launch vehicle
TITAN IIIA
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Poly, 0.6 m
Radar Cross Section
0.411 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 11 hours ago
0 LES 1
1 01002U 65008C   25184.92989403 -.00000003  00000-0 -14264-2 0  9990
2 01002  32.1393 149.7109 0015347  95.9667 264.2579  9.88354922181734
Epoch: 2025-07-03T22:19Z
TLE epoch observation values (Epoch: 2025-07-03T22:19:02.844Z)
Latitude
-0.00002°
Longitude
-107.24057°
Altitude
2,794.166 km
Speed
6.594 km/s
True Right ascension
09h 58m 50s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-15.70649°
Longitude
98.13008°
Altitude
2,801.563 km
Speed
6.589 km/s
Apparent Right ascension
01h 42m 36s
Apparent Declination
-49° 07' 47"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
21:16:16
Azimuth
141.2° SSE
Elevation
-16.606°
Doppler factor
1
Orbital elements
Apogee altitude
2,810.625 km
Perigee altitude
2,782.464 km
Semi-major axis
9,174.682 km
Eccentricity
0.00153
Inclination
32.1393°
RAAN
149.7109°
Arg. of periapsis
95.9667°
True anomaly
Unknown
Mean anomaly
264.2579°
Eccentric anomaly
Unknown
Mean motion
2.46977 °/min
Orbital period
145.76 mins
BSTAR
-0.0014264
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Other satellites on launch #8 in the year 1965 (1965-02-11 UTC)

LES 1 Visibility forecast

Observer location: undefined°, undefined°

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.
21 mins2025-07-04 22:38:09.284Z184.673° SSW2025-07-04 22:48:09.284Z142.746° SSE21.681°2025-07-04 22:59:09.284Z96.816° ESE
28 mins2025-07-05 01:11:09.284Z227.829° WSW2025-07-05 01:25:09.284Z157.086° SSE38.181°2025-07-05 01:39:09.284Z89.808° E
30 mins2025-07-05 03:48:09.284Z257.557° W2025-07-05 04:02:09.284Z188.945° SSW42.235°2025-07-05 04:18:09.284Z104.076° ESE
27 mins2025-07-05 06:27:09.284Z268.989° W2025-07-05 06:40:09.284Z203.32° SW37.026°2025-07-05 06:54:09.284Z135.606° SSE
18 mins2025-07-05 09:08:09.284Z255.667° W2025-07-05 09:16:09.284Z222.162° SW19.242°2025-07-05 09:26:09.284Z180.793° SSW
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