Official name NATO 2B
Alternative name NATO IIB
Cospar ID 1971-009A
Norad ID 4902
Launch date 1971-02-03
Launch site AFETR
Launch vehicle Delta-M
Country/Organization USA
Type application Military communication
Operator NATO
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.1
Inclination (deg) 2.12
Perigee (km) 35771
Apogee (km) 35802
Eccentricity 0.000433124222821455
Mean motion (revs. per day) 1.00271568832254
Semi-Major axis (km) 42164.635
Raan (deg) 261.5731
Arg of perigee (deg) 210.0686
Shape Cyl
Mass (kg) 127.85
Diameter (m) 0.8
Height (m) 1.4
Span (m^2) 1.4
Lifetime 5 years
Contractors Philco Ford Space & Reentry Systems Division
Equipment One 2 MHz and one 20 MHz bandwidth double-conversion repeater
Propulsion Star-17A
Configuration Skynet-1 Bus
Power Solar cells (body mounted), batteries

NATO 2A and 2B were the first generation communication satellites to provide immediate communications links between officials of the various NATO nations.

Both the UK's Skynet-1 and the NATO's NATO-2 satellite programs resulted from the US invitation to join the IDCSP communicaten satellites system. The satellites were to be interoperable with the IDCSP svstern. and the program was initially called IDCSP/A (for augmentation).

The satellites were develloped by Philco Ford Space & Reentry Systems Division. The satellite technology was based on the IDCSP near synchronous satellites, with several improvements implemented. They featured a mechanically despun antenna, that provided increased gain relative to IDCSP and both 2 and 20 MHz channels. The only difference between the Skynet and NATO satelliteswas the antenna pattern which in case of Skynet provided a uniform global pattern and in case of NATO was shaped to cover only the NATO nations, from the eastern coast of North America to Türkiye (Turkey). The Skynet and NATO satellites were placed into a svnchronous orbit and had a stationkeeping capability. The satellites featured a solid rocket motor for apogee maneuver and hydrazine propulsion for on-orbit use.

The satellites were all launched on Delta-M rockets from Cape Canaveral.

NATO 2A was launched on 20 March 1970 and operated for 26 months.

NATO 2B was launched on 3 February 1971. It operated until August 1976.

Satellite COSPAR Date LS Launch Vehicle Remarks
NATO 2A 1970-021A 1970-03-20 AFETR Delta-M
NATO 2B 1971-009A 1971-02-03 AFETR Delta-M