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
Spacecraft
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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 LES 1
1 01002U 65008C   26125.38021759  .00000000  00000-0 -11275-2 0  9992
2 01002  32.1380 146.1157 0015342 116.3544 243.8529  9.88355306211954
Epoch: 2026-05-05T09:07Z
TLE epoch observation values (Epoch: 2026-05-05T09:07:30.799Z)
Latitude
-0.00005°
Longitude
145.9814°
Altitude
2,798.951 km
Speed
6.59 km/s
True Right ascension
09h 44m 27s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
22:41:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,810.618 km
Perigee altitude
2,782.467 km
Semi-major axis
9,174.68 km
Eccentricity
0.00153
Inclination
32.138°
RAAN
146.1157°
Arg. of periapsis
116.3544°
True anomaly
243.69522°
Mean anomaly
243.8529°
Eccentric anomaly
243.77405°
Mean motion
2.46977 °/min
Orbital period
145.76 mins
BSTAR
-0.0011275
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
|