Official name LES 1
Alternative name LES 1
Cospar ID 1965-008C
Norad ID 1002
Launch date 1965-02-11
Launch site AFETR
Launch vehicle Titan-3A [Star-13A]
Country/Organization USA
Type application Experimental communication
Operator MIT Lincoln Laboratory, USAF
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 145.7
Inclination (deg) 32.14
Perigee (km) 2779
Apogee (km) 2808
Eccentricity 0.00519062108466082
Mean motion (revs. per day) 9.88332189430336
Semi-Major axis (km) 9171.635
Raan (deg) 242.6252
Arg of perigee (deg) 314.0445
Shape Poly
Mass (kg) 158
Height (m) 0.6
Width (m) 0.6
Depth (m) 0.6
Span (m^2) 0.6
Contractors MIT Lincoln Laboratory
Equipment ?
Propulsion ?
Configuration ?
Power Solar cells

LES 1 and 2 (Lincoln Experimental Satellite 1 and 2) were essentially identical experimental communications satellites. Both featured a single X-band transponder and an 8-horn electronically switched antenna. Additionally, attitude control and sensing experiments were conducted.

The initial program objective was to build, launch, and field a system to demonstrate practical military satellite communications. The availability of Project West Ford's advanced superhigh-frequency (SHF) technology (at seven to eight gigahertz) contributed to the decision to design the system for that band. The Department of Defense's concurrent procurement of a series of SHF satellites and terminals, commencing with the Initial Defense Communications Satellite Program (IDCSP), meant that lessons learned from the experiments would find an additional application.

LES-1, launched from Cape Canaveral on 11 February 1965, accomplished only a few of its objectives. Apparently because of miswiring of the ordnance circuitry, the satellite never left circular orbit and ceased transmitting in 1967. 46 years after it fell silent, in 2013 the satellite began again transmitting, likely due to the batteries have failed in a manner that allows them to carry charge directly through to the transmitter, when the satellite receives sunlight.

LES-2, the twin of LES-1 achieved its planned final orbit on 6 May 1965.

Satellite COSPAR Date LS Launch Vehicle Remarks
LES 1 1965-008C 1965-02-11 AFETR Titan-3A [Star-13A] Star-13A failed
LES 2 1965-034B 1965-05-06 AFETR Titan-3A [Star-13A] with LCS 1