Showing default

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.

Loading next visibility...
Identifier
1002, 1965-008C
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
MIT-LL
Mission
Defense Communications
Bus & Motor
LES, STAR 13A
Mass
158 kg wet, 31 kg dry
Launch date (UTC)
1965-02-11 (61 years ago)
Launch vehicle
TITAN IIIA
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Poly, 0.3 m
Radar Cross Section
0.411 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 LES 1
1 01002U 65008C   25242.03749936  .00000004  00000-0 -53911-3 0  9995
2 01002  32.1490  14.4291 0015818 301.2667  58.6281  9.88354541187387
Epoch: 2025-08-30T00:53Z
TLE epoch observation values (Epoch: 2025-08-30T00:53:59.944Z)
Latitude
-0.00001°
Longitude
22.45177°
Altitude
2,785.204 km
Speed
6.6 km/s
True Right ascension
00h 57m 42s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
16:00:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,811.059 km
Perigee altitude
2,782.034 km
Semi-major axis
9,174.683 km
Eccentricity
0.00158
Inclination
32.149°
RAAN
14.4291°
Arg. of periapsis
301.2667°
True anomaly
58.78302°
Mean anomaly
58.6281°
Eccentric anomaly
58.70554°
Mean motion
2.46977 °/min
Orbital period
145.76 mins
BSTAR
-0.00053911
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #8 in the year 1965 (1965-02-11 UTC)

Documentation

Showing up to 5 results
|