ISA (original) (raw)

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

ISA

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

Country: Israel. Spacecraft: Ofeq 1-2, Ofeq 5. Projects: Ofeq.

1988 September 19 - . 09:32 GMT - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Shaviyt.

Ofeq-1 - . Mass: 155 kg (341 lb). Nation: Israel. Agency: ISA. Program: Ofeq. 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: 142.90 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: Jericho. Launch Vehicle: Shaviyt.

Ofeq-2 - . Mass: 160 kg (350 lb). Nation: Israel. Agency: ISA. Program: Ofeq. 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: 143.20 deg. Period: 88.50 min. Communication experiments. .

1994 September 15 - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Jericho II. FAILURE: Failure.

'Ofeq? - . Nation: Israel. Agency: ISA. Apogee: 300 km (180 mi).

1995 April 5 - . 11:16 GMT - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Shaviyt 1.

Ofeq-3 - . Mass: 189 kg (416 lb). Nation: Israel. Agency: ISA. Program: Ofeq. 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: 143.40 deg. Period: 94.50 min.

1998 January 22 - . 12:56 GMT - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Shaviyt 1. FAILURE: Launch vehicle failed during second stage burn.. Failed Stage: 2.

Ofeq-4 - . Mass: 189 kg (416 lb). Nation: Israel. Agency: ISA. Manufacturer: IAI. Program: Ofeq. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Ofeq 3. Fell in Mediterranean Sea..

2010 June 22 - . 19:00 GMT - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Shaviyt 1.

Ofeq 9 - . Mass: 189 kg (416 lb). Nation: Israel. Agency: ISA. Program: Ofeq. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Ofeq 5. USAF Sat Cat: 36608 . COSPAR: 2010-031A. Apogee: 586 km (364 mi). Perigee: 400 km (240 mi). Inclination: 141.80 deg. Period: 94.50 min. Israeli optical surveillance satellite..

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z