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Nodong · Iranian Space Agency

Safir 1B

active
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Specifications

Status
active
Height
22 m
Diameter
1.25 m
Mass
26,000 kg
Stages
2
Payload to LEO
0
Payload to GTO
0
First flight
2012-05-23
Total launches
3
Success / Fail
0 / 3

The Safir was the first Iranian expendable launch vehicle able to place a satellite in orbit. The first successful orbital launch using the Safir launch system took place on 2 February 2009 when a Safir carrier rocket placed the Omid satellite into an orbit with a 245.2 km (152.4 mi) apogee. This made Iran the ninth nation capable of producing and launching a satellite.