Official name OTS 2
Alternative name OTS 2
Cospar ID 1978-044A
Norad ID 10855
Launch date 1978-05-11
Launch site AFETR
Launch vehicle Delta-3914
Country/Organization International
Type application Communication
Operator ESA
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 1452.54
Inclination (deg) 8.84
Perigee (km) 36075
Apogee (km) 36140
Eccentricity 0.0009000900090009
Mean motion (revs. per day) 0.991366847040357
Semi-Major axis (km) 42485.635
Raan (deg) 306.7493
Arg of perigee (deg) 355.5959
Shape Hex Cyl
Mass (kg) 440.04
Diameter (m) 2.4
Height (m) 1.6
Span (m^2) 2.4
Contractors British Aerospace
Equipment 6 Ku-band transponders
Propulsion SVM-7
Configuration OTS Bus
Power 2 deployable solar arrays, batteries

OTS 1 and 2 (Orbital Test Satellite) were an experimental communications satellites inherited by ESA in 1975 from its predecessor, the European Space Research Organization (ESRO).

These were the first GEO communications satellites to carry six Ku-band (14/11 GHz) transponders and were capable of handling 7,200 telephone circuits. With a mass of approximately 445 kg on station, the OTS bus was hexagonal with overall dimensions of 2.4 m by 2.1 m. Two solar panels with a span of 9.3 m provided 0.6 kW of electrical power. British Aerospace was the prime contractor from the European MESH consortium which developed the OTS vehicle.

The OTS 1 was lost at launch in September 1977. OTS 2 was successfully launched in May 1978. It completed its primary mission in 1984 after which the spacecraft was involved in a 6-year program of experiments, including the testing of a new attitude control technique taking advantage of solar wind forces. OTS 2 was moved out of the geostationary ring and into a graveyard orbit.

Satellite COSPAR Date LS Launch Vehicle Remarks
OTS 2 1978-044A 1978-05-11 AFETR Delta-3914