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Nodong · Iranian Space Agency

Safir

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
2008-08-16
Total launches
5
Success / Fail
4 / 1

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.

Payloads it launched · 4

FAJR
LEO
NAVID
LEO
RASAD 1
LEO
OMID
LEO