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Omid
Omid
Omid
Credit: Manufacturer Image
Iranian technology satellite.ranian technology satellite. First Iranian-built, Iranian-launched satellite. Technology satellite for Iran National Space Administration (INSA), Iran. Launched 2008-2009.

Status: Operational 2008. First Launch: 2008-08-16. Last Launch: 2009-02-02. Number: 2 . Gross mass: 27 kg (59 lb).


More at: Omid.

Family: Shahab, Technology, Technology satellite. Country: Iran. Engines: Nodong. Launch Vehicles: Shahab 3, Safir. Launch Sites: Semnan. Bibliography: 6750, 12916.

2008 August 16 - . 19:32 GMT - . Launch Site: Semnan. LV Family: Nodong 1. Launch Vehicle: Safir. FAILURE: Second stage failed catastrophically..
  • Omid - . Nation: Iran. Agency: IRSA. Class: Technology. Type: Technology satellite. Spacecraft: Omid. Apogee: 152 km (94 mi).

    Iranian suborbital launch in support of development of an indigenous satellite launch capability. Western analysts claimed it was a failed satellite launch attempt, and that the second stage of the launch vehicle failed catastrophically at 152 km altitude.


2009 February 2 - . Launch Site: Semnan. LV Family: Nodong 1. Launch Vehicle: Safir.
  • Omid - . Mass: 25 kg (55 lb). Nation: Iran. Agency: IRSA. Class: Technology. Type: Technology satellite. Spacecraft: Omid. Decay Date: 2009-04-25 . USAF Sat Cat: 33506 . COSPAR: 2009-004A. Apogee: 373 km (231 mi). Perigee: 245 km (152 mi). Inclination: 55.5500 deg. Period: 90.70 min. First Iranian satellite launched by an Iranian launch vehicle..


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