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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
22 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 22 hours ago
0 LES 1
1 01002U 65008C   25128.42857052  .00000008  00000-0 -42175-4 0  9995
2 01002  32.1453 283.5687 0015590 252.4908 107.3885  9.88354664176146
Epoch: 2025-05-08T10:17Z
Definitive object data (Epoch: 2025-05-08T10:17:08.492Z)
Latitude
-0.00002°
Longitude
-97.21593°
Altitude
2,797.031 km
Speed
6.592 km/s
True Right ascension
18h 54m 16s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude
8.08239°
Longitude
-86.3766°
Altitude
2,799.09 km
Speed
6.59 km/s
Apparent Right ascension
21h 46m 19s
Apparent Declination
-21° 55' 22"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
16:22:22
Azimuth
112.507° SE
Elevation
-7.358°
Doppler factor
1
Orbital elements
Apogee altitude
2,810.849 km
Perigee altitude
2,782.242 km
Semi-major axis
9,174.683 km
Eccentricity
0.001559
Inclination
32.1453°
RAAN
283.5687°
Arg. of periapsis
252.4908°
True anomaly
107.55888°
Mean anomaly
107.3885°
Eccentric anomaly
107.4737°
Mean motion
2.46977 °/min
BSTAR
-0.000042175
Orbital period
145.76 mins
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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.
15 mins2025-05-09 10:36:15.230Z167.418° S2025-05-09 10:43:15.230Z139.59° SSE15.657°2025-05-09 10:51:15.230Z107.649° ESE
27 mins2025-05-09 13:07:15.230Z216.275° SW2025-05-09 13:20:15.230Z151.568° SSE35.064°2025-05-09 13:34:15.230Z88.406° E
30 mins2025-05-09 15:43:15.230Z250.665° W2025-05-09 15:57:15.230Z178.672° S42.14°2025-05-09 16:13:15.230Z98.07° ESE
29 mins2025-05-09 18:21:15.230Z268.549° W2025-05-09 18:35:15.230Z198.12° SSW39.664°2025-05-09 18:50:15.230Z125.323° SE
23 mins2025-05-09 21:01:15.230Z263.747° W2025-05-09 21:12:15.230Z215.224° SW25.211°2025-05-09 21:24:15.230Z164.734° S
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