Ofeq

While exact technical details and capabilities are classified, it is assumed that the Ofeq satellites have ultraviolet and visible imaging sensors, and an effective operational lifespan of 1–3 years. Some early reports stated the reconnaissance capabilities as such that would allow "reading license plates in Baghdad", but that can be ruled out on grounds of physical optics. Other reports more plausibly place the imaging resolution at 0.8 meters for Ofeq 5.

Most non-Israeli satellites are launched eastward to gain a boost from the Earth's rotational speed. However, Ofeq satellites are launched westward (in retrograde orbits) over the Mediterranean to avoid flying over, and dropping spent rocket stages over, populated land areas. Other Israeli satellites (such as the Amos series) are launched from locations in other countries.[1]

Ofeq's east-to-west orbit of about 141 degrees orbital inclination[2] is phased to give good daylight coverage of the Middle East. Ofeq makes a half-dozen or so daylight passes per day over Israel and the surrounding countries, whereas U.S. and Russian spysats only get one or two passes per day from their higher inclination orbits.

• Ofeq 1, launched September 19, 1988, possessed a weight of 155 kg and circled the earth on an orbit with a perigee of 249 km and an apogee of 1149 km on a course bent around 142.9 degrees. It accomplished mainly solar cell and radio transmission tests.
• Ofeq 2, was launched April 23, 1990 on a course with a perigee of 149 km and an apogee of 251 km, bent around 143.2 degrees. It also accomplished communication tests.
• The launch of Ofeq 3 series was initially postponed from September 15, 1994, to April 5, 1995.[4]
• Ofeq 3, launched April 5, 1995, was the first operational Israeli satellite with reconnaissance (photography) capabilities. It weighed 225 kg and had a perigee of 369 km and was launched on a new version of Shavit.
• Ofeq 4, launched January 22, 1998, did not achieve earth orbit due to a launcher failure and was lost.
• Ofeq 5, was launched 28 May 2002. The 300 kg Ofeq 5 orbited the earth on a course with a perigee of 262 km and an apogee of 774 km, bent around 143.5 degrees. During the course of its mission, its perigee was raised to 369 km and its apogee was lowered to 771 kilometers, in an attempt to prolong the satellite's lifespan. Some observers believe that the 300 kg weight of the satellite, combined with the additional propulsive requirements of the retrograde orbit, constitute a de facto demonstration of the Shavit's ICBM potential.
• Ofeq 6, launched September 6, 2004 encountered another launcher failure, failed to achieve low earth orbit and crashed to the sea. The launcher failure was due to the third stage of the Shavit launcher.
• Ofeq 7 was successfully launched on June 11, 2007 using the Shavit launcher.[5]
• Ofeq 8 designation is used for the TecSAR synthetic aperture radar satellite launched by an Indian rocket on 21 January 2008.[6]
• Ofeq 9 was successfully launched on June 22, 2010 from Palmachim Air Base using the upgraded Shavit launcher.[6][7]
• Ofeq 10, providing high-resolution synthetic aperture radar, was successfully launched on April 9, 2014 from Palmachim Air Base using the upgraded Shavit launcher.[2]
• Ofeq 11 was successfully launched on September 13, 2016 from Palmachim Air Base using the upgraded Shavit launcher.[8]

• IAI's space systems website
• Description of Ofeq 1,2 in Astronautix
• Description of Ofeq 5 in Astronautix
• Palmachim Air Force base in GlobalSecurity
• Speculation on Ofeq's orbit in GlobalSecurity
• Ofeq 5 description
• Ofeq 7 description