Encyclopedia Astronautica
ISA


Israeli agency overseeing development of spacecraft. Israeli Space Agency, Israel.

More... - Chronology...


Associated Countries
Associated Spacecraft
  • Ofeq 1-2 Israeli technology satellite. 2 launches, 1988.09.19 (Ofeq-1) to 1990.04.03 (Ofeq-2). Ofeq, meaning 'Horizon', was a technology demonstration satellite developed by IAI (Israel Aircraft Industries) for ISA (Israel Space Agency). More...
  • Ofeq 5 Israeli military surveillance satellite. Operational, first launch 2002.05.28. Ofeq-5 was said to be about 33% heavier than its predecessors. More...

See also
  • Agency Agencies or institutions overseeing design, development, construction, or operation of space-related systems. More...

Associated Programs
  • Offeq Israeli indigenous satellite series. Launching organization: Israel Aircraft Industries, Ltd (IAI) and Israeli Space Agency (ISA). Function of first Offeqs: 1) Experimentation in generation of solar power; 2) Experimentation in transmission reception from space; 3) Verification of system's ability to withstand vacuum and weightless conditions; 4) Data collection on space environment conditions and Earth's magnetic field. Later models provided military optical and electronic reconnaissance services. More...

ISA Chronology


1988 September 19 - . 09:32 GMT - . Launch Site: Palmachim. LV Family: Shavit. Launch Vehicle: Shavit. LV Configuration: Shaviyt 1.
  • Ofeq-1 - . Mass: 155 kg (341 lb). Nation: Israel. Agency: ISA. Program: Offeq. Class: Technology. Type: Navigation technology satellite. Spacecraft: Ofeq 1-2. Decay Date: 1989-01-14 . USAF Sat Cat: 19519 . COSPAR: 1988-087A. Apogee: 1,149 km (713 mi). Perigee: 250 km (150 mi). Inclination: 142.9000 deg. Period: 98.80 min. First Israeli launch; possibly experimental surveillance mission. Experimental satellite 'Offeq-1'. Launch time 0934 GMT. Location: site on the coast south of Tel-Aviv. Launching organization: Israel Aircraft Industries, Ltd (IAI) and Israeli Space Agency (ISA). Function: 1) Experimentation in generation of solar power; 2) Experimentation in transmission reception from space; 3) Verification of system's ability to withstand vacuum and weightless conditions; 4) Data collection on space environment conditions and Earth's magnetic field.

1990 April 3 - . 12:02 GMT - . Launch Site: Palmachim. LV Family: Shavit. Launch Vehicle: Shavit. LV Configuration: Shaviyt 2.
  • Ofeq-2 - . Mass: 160 kg (350 lb). Nation: Israel. Agency: ISA. Program: Offeq. Class: Technology. Type: Navigation technology satellite. Spacecraft: Ofeq 1-2. Decay Date: 1990-07-09 . USAF Sat Cat: 20540 . COSPAR: 1990-027A. Apogee: 251 km (155 mi). Perigee: 149 km (92 mi). Inclination: 143.2000 deg. Period: 88.50 min. Summary: Communication experiments. .

1994 September 15 - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Jericho 2. LV Configuration: Jericho II 3?. FAILURE: Failure.
  • 'Ofeq? - . Nation: Israel. Agency: ISA. Apogee: 300 km (180 mi).

1995 April 5 - . 11:16 GMT - . Launch Site: Palmachim. LV Family: Shavit. Launch Vehicle: Shavit 1. LV Configuration: Shaviyt 1 3.
  • Ofeq-3 - . Mass: 189 kg (416 lb). Nation: Israel. Agency: ISA. Program: Offeq. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Ofeq 3. Decay Date: 2000-10-24 . USAF Sat Cat: 23549 . COSPAR: 1995-018A. Apogee: 694 km (431 mi). Perigee: 366 km (227 mi). Inclination: 143.4000 deg. Period: 94.50 min.

1998 January 22 - . 12:56 GMT - . Launch Site: Palmachim. LV Family: Shavit. Launch Vehicle: Shavit 1. LV Configuration: Shaviyt 1 4. FAILURE: Launch vehicle failed during second stage burn.. Failed Stage: 2.
  • Ofeq-4 - . Nation: Israel. Agency: ISA. Manufacturer: IAI. Program: Offeq. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Ofeq 3. COSPAR: F980122A. Summary: Fell in Mediterranean Sea..

2010 June 22 - . 19:00 GMT - . Launch Site: Palmachim. LV Family: Shavit. Launch Vehicle: Shavit 1.
  • Ofeq 9 - . Mass: 189 kg (416 lb). Nation: Israel. Agency: ISA. Program: Offeq. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Ofeq 5. USAF Sat Cat: 36608 . COSPAR: 2010-031A. Apogee: 586 km (364 mi). Perigee: 400 km (240 mi). Inclination: 141.8000 deg. Period: 94.50 min. Summary: Israeli optical surveillance satellite..

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