Palmachim

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Palmachim

Palmachim
Credit: © Mark Wade

Israeli Air Force Test Range. Israeli coastal missile test site from which the Shavit satellite launch vehicle is also launched. A due-west launch over the Mediterranean is required to avoid overflying Arab countries, resulting in unique orbital inclinations and directions.

First Launch: 1987-05-01. Last Launch: 2014-04-09. Number: 54 . Location: Palmachim Beach. Longitude: 34.68 deg. Latitude: 31.88 deg.

Minimum Inclination: 142.0 degrees. Maximum Inclination: 144.0 degrees.

Subtopics

Palmachim IAFTR Arrow launch complex. Sea Launch Area, Palmachim Beach

Palmachim SH Shavit pad, Palmachim Beach

Family: Orbital Launch Site. Country: Israel. Spacecraft: Ofeq 1-2, Ofeq 3, Ofeq 5. Launch Vehicles: Jericho II, Shaviyt, Arrow 1, Shaviyt 1, Arrow 2. Projects: Ofeq. Launch Sites: Palmdale Omni DZ, Palmachim IAFTR, Palmachim SH. Bibliography: 2.

Photo Gallery

Palmachim
Location of Palmachim
Credit: © Mark Wade

1987 May 1 - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Jericho II.

Test mission - . Nation: Israel. Agency: IDF. Apogee: 300 km (180 mi).

1988 January 1 - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Jericho II.

Nation: Israel. Agency: IDF. Apogee: 300 km (180 mi).

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.

1989 September 14 - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Jericho II.

Test mission - . Nation: Israel. Agency: IDF. Apogee: 300 km (180 mi).

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. .

1990 August 9 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1. FAILURE: Failure.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 0 km (0 mi).

1991 March 25 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1. FAILURE: Failure.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 20 km (12 mi).

1991 October 30 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1. FAILURE: Failure.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 20 km (12 mi).

1992 September 23 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 20 km (12 mi).

1993 February 28 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 20 km (12 mi).

1993 February 28 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 20 km (12 mi).

1993 July 14 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 20 km (12 mi).

1993 October 14 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 20 km (12 mi).

1993 October 14 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 20 km (12 mi).

1994 March 1 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 20 km (12 mi).

1994 June 12 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 20 km (12 mi).

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.

1995 July 30 - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 20 km (12 mi).

1996 February 20 - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

Test mission - . Nation: Israel. Agency: IAI. Apogee: 80 km (49 mi).

1996 August 20 - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

ATBM test - . Nation: Israel. Agency: IAI. Apogee: 80 km (49 mi).

1996 August 20 - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1.

Target mission - . Nation: Israel. Agency: IAI. Apogee: 80 km (49 mi).

1997 March 11 - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

ATBM test - . Nation: Israel. Agency: IAI. Apogee: 80 km (49 mi).

1997 August 19 - . 08:20 GMT - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1.

Target mission - . Nation: Israel. Agency: IAI. Apogee: 80 km (49 mi).

1997 August 19 - . 08:29 GMT - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

ATBM test - . Nation: Israel. Agency: IAI. Apogee: 80 km (49 mi).

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..

1998 September 14 - . 12:41 GMT - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

ATBM test - . Nation: Israel. Agency: IAI. Apogee: 80 km (49 mi).

1999 November 1 - . 09:42 GMT - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

ATBM test - . Nation: Israel. Agency: IAI. Apogee: 80 km (49 mi).

1999 November 1 - . 09:42 GMT - . Launch Site: Palmachim. Launch Complex: Palmachim IAFTR. Launch Platform: SHIP-ISR. LV Family: Arrow. Launch Vehicle: Arrow 1.

Target mission - . Nation: Israel. Agency: IAI. Apogee: 80 km (49 mi).

2000 September 14 - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

AST-5 Black Sparrow - . Nation: Israel. Agency: IAI. Apogee: 80 km (49 mi).

2000 September 14 - . 09:00 GMT - . Launch Site: Palmachim. Launch Platform: F-15D. Launch Vehicle: Black Sparrow.

Nation: Israel. Agency: IDF. Type: ABM Target. Apogee: 40 km (24 mi).

2001 June 27 - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Jericho II.

Operational test - . Nation: Israel. Agency: IDF. Apogee: 100 km (60 mi).

2001 August 27 - . Launch Site: Palmachim. Launch Platform: F-15D. Launch Vehicle: Black Sparrow.

Nation: Israel. Agency: IDF. Type: ABM Target. Apogee: 40 km (24 mi).

2001 August 27 - . 10:50 GMT - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

AST-6 Black Sparrow - . Nation: Israel. Agency: IAI. Apogee: 100 km (60 mi).

2002 May 28 - . 15:25 GMT - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Shaviyt 1.

Ofeq-5 - . Mass: 300 kg (660 lb). Nation: Israel. Agency: Tsahal. Manufacturer: IAI. Program: Ofeq. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Ofeq 5. USAF Sat Cat: 27434 . COSPAR: 2002-025A. Apogee: 757 km (470 mi). Perigee: 370 km (220 mi). Inclination: 143.50 deg. Period: 95.90 min.
Military Observation satellite. Return to flight of the Shavit booster following a lauanch failure. Launch delayed from third quarter 2001. The three-stage Shavit rocket took off from Palmachim Air Force Base on the Israeli coast and flew westward to put the satellite in a retrograde orbit. The AUS-51 third stage solid motor entered a 262 x 774 km x 143.5 deg orbit and separated from the Ofeq satellite. Both coasted up to apogee at around 1620 UTC when Ofeq made a burn to increase its velocity by 33 m/s, raising the orbit to 369 x 771 km x 143.5 deg.

2003 January 5 - . 14:37 GMT - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

AST-8 ATBM test - . Nation: Israel. Agency: IAI. Apogee: 30 km (18 mi).

2003 December 16 - . Launch Site: Palmachim. Launch Platform: F-15D. Launch Vehicle: Black Sparrow.

Nation: Israel. Agency: IDF. Type: ABM Target. Apogee: 40 km (24 mi).

2003 December 16 - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

AST-9 Black Sparrow - . Nation: Israel. Agency: IAI. Apogee: 30 km (18 mi).

2004 September 6 - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Shaviyt 1. FAILURE: Third stage orientation failure at 270 seconds into the flight. Failed Stage: 3.

Ofeq-6 - . Mass: 300 kg (660 lb). Nation: Israel. Agency: Tsahal. Manufacturer: IAI. Program: Ofeq. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Ofeq 5. Military observation satellite failed to reach orbit. Finanical loss estimated by Israeli press as $ 100 million..

2005 December 2 - . 08:27 GMT - . Launch Site: Palmachim. Launch Platform: F-15D. Launch Vehicle: Black Sparrow.

Nation: Israel. Agency: IDF. Type: ABM Target. Apogee: 40 km (24 mi).

2005 December 2 - . 08:28 GMT - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

AST? Black Sparrow - . Nation: Israel. Agency: IAI. Apogee: 40 km (24 mi).

2007 February 11 - . Launch Site: Palmachim. Launch Platform: F-15D. Launch Vehicle: Black Sparrow.

Nation: Israel. Agency: IDF. Type: ABM Target. Apogee: 40 km (24 mi).

2007 February 11 - . 18:18 GMT - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

AST Black Sparrow - . Nation: Israel. Agency: IAI. Apogee: 40 km (24 mi).

2007 March 26 - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

Nation: Israel. Agency: IAI. Apogee: 40 km (24 mi).

2007 June 10 - . 23:40 GMT - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Shaviyt 1.

Ofeq-7 - . Mass: 300 kg (660 lb). Nation: Israel. Agency: Tsahal. Manufacturer: IAI. Program: Ofeq. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Ofeq 5. USAF Sat Cat: 31601 . COSPAR: 2007-025A. Apogee: 576 km (357 mi). Perigee: 340 km (210 mi). Inclination: 141.80 deg. Period: 93.80 min. Israeli optical reconnaisance satellite, evidently using an improved version of the Shavit booster and probably heavier and more capable than its predecessors..

2008 January 17 - . 06:45 GMT - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Jericho III.

Nation: Israel. Agency: IDF. Apogee: 300 km (180 mi).

2008 April 15 - . Launch Site: Palmachim. Launch Platform: F-15D. Launch Vehicle: Blue Sparrow.

Nation: Israel. Agency: IDF. Type: ABM Target. Apogee: 100 km (60 mi).

2009 April 7 - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 2.

AST Black Sparrow - . Nation: Israel. Agency: IAI. Type: ABM. Apogee: 40 km (24 mi).

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..

2011 Q4? - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 3.

Canister eject test - . Nation: Israel. Agency: IDF. Type: ABM. Apogee: 0 km (0 mi).

2011 November 2 - . 07:50 GMT - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Jericho III.

Jericho III test - . Nation: Israel. Apogee: 300 km (180 mi). Test mission. Believed to be second test of an improved Jericho missile..

2013 February 25 - . 06:00 GMT - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 3.

Arrow KV - . Nation: Israel. Type: ABM. Apogee: 100 km (60 mi). ABM - exoatmospheric interceptor test..

2013 July 12 - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Jericho III.

Jericho RV - . Nation: Israel. Apogee: 300 km (180 mi). Developmental test.

2014 January 3 - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 3.

Arrow KV - . Nation: Israel. Type: ABM. Apogee: 100 km (60 mi). Missile test.

2014 April 9 - . 19:06 GMT - . Launch Site: Palmachim. Launch Pad: xxx. LV Family: Jericho. Launch Vehicle: Shaviyt 1.

Ofeq-10 - . Mass: 260 kg (570 lb). Nation: Israel. Class: Surveillance. Type: Military Radarsat. Spacecraft: Tecsar. USAF Sat Cat: 39650 . COSPAR: 2014-019A. Apogee: 598 km (371 mi). Perigee: 388 km (241 mi). Inclination: 140.94 deg. Period: 94.48 min. Reportedly carried a radar imaging (SAR) payload..

2015 December 10 - . 06:15 GMT - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 3.

Arrow 3 KV - . Nation: Israel. Type: ABM. Apogee: 150 km (90 mi). ABM Interceptor mission..

2016 September 13 - . 13:48 GMT - . Launch Site: Palmachim. LV Family: Jericho. Launch Vehicle: Shavit.

'Ofeq-11 - . Nation: Israel. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Tecsar. USAF Sat Cat: 41759 . COSPAR: 2016-056A. Apogee: 600 km (370 mi). Perigee: 250 km (150 mi). Inclination: 141.00 deg. Ofeq-11 spy satellite, thought to be ususal retrograde orbit. It was reported that Israeli mission controllers were working to correct unspecified technical problems with the payload..

2018 February 18 - . 23:30 GMT - . Launch Site: Palmachim. LV Family: Arrow. Launch Vehicle: Arrow 3.

Arrow KV - . Nation: Israel. Type: ABM. Apogee: 100 km (60 mi). Test mission. Impacted Mediterranean?..

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