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Ofeq 5
Ofeq-3 Credit: Manufacturer Image |
Israeli military surveillance satellite. Ofeq-5 was said to be about 33% heavier than its predecessors. Reconnaissance, optical satellite built by IAI for Tsahal, Israel. Launched 2002-2010. Used OPSAT-2000 Bus.
Status: Operational 2002. First Launch: 2002-05-28. Last Launch: 2010-06-22. Number: 4 . Gross mass: 300 kg (660 lb). Height: 2.30 m (7.50 ft).
It was built by IAI/MBT for the Israeli Space Agency and carried an imaging reconnaissance camera. The Ofeq-5 telescope/camera was produced by El-Op Electro-Optic Industries, a subsidiary of Elbit Systems. The system - which acquired images underneath and lateral to the satellite and in swaths ahead of its trajectory - was bigger than that installed on the Ofeq-3 and could produce images with 0.8 meter resolution. The Ofeq-5 had a design life of four years.
More at: Ofeq 5.
Subtopics
| EROS B Earth Observing satellite built by IAI for ImageSat International, Israel. Launched 2006. Used OPSAT-2000 Bus. |
Family:
Military surveillance sat,
Surveillance.
Country:
Israel.
Launch Vehicles:
Minuteman 3,
Shaviyt,
Shaviyt 1.
Projects:
Ofeq.
Launch Sites:
Palmachim.
Agency:
ISA,
IAI,
MBT.
Bibliography:
2,
4,
552,
554,
6747,
12903.
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.
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..
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..
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..
2015 October 21 - .
12:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Ofeq 5.
Launch Pad: LF04.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- GT216GM RV - .
Nation: USA.
Apogee: 1,300 km (800 mi). Training mission. Impacted Kwajalein..
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