Ofeq-9, also known as Ofek 9 ("Horizon in Hebrew), is part of the Ofeq family of reconnaissance satellites designed and built by Israel Aerospace Industries (IAI) for the Israeli Ministry of Defense.
Names | Ofek-9 |
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Mission type | Optical reconnaissance |
Operator | Israeli Ministry of Defence / Tsahal |
COSPAR ID | 2010-031A ![]() |
SATCAT no. | 36608 |
Mission duration | 5 years (planned) [1] 12 years, 2 months and 28 days (in progress) |
Spacecraft properties | |
Spacecraft | Ofeq-9 |
Bus | OPSAT-2000[2] |
Manufacturer | Israel Aerospace Industries |
Launch mass | 297 kg (655 lb) |
Dimensions | 2.3 m in height 1.2 m in diameter Span: 3.6 m on orbit [3] |
Power | 400 watts |
Start of mission | |
Launch date | 22 June 2010, 19:00 UTC[4] |
Rocket | Shavit 2 (No.8) |
Launch site | Palmachim Air Base |
Contractor | Israel Aerospace Industries |
Entered service | 25 June 2010 [3] |
Orbital parameters | |
Reference system | Geocentric orbit[5] |
Regime | Low Earth orbit (Retrograde orbit) |
Perigee altitude | 466 km (290 mi) |
Apogee altitude | 567 km (352 mi) |
Inclination | 141.74° |
Period | 94.81 minutes |
Ofeq series ← TecSAR-1 (Ofeq-8) |
It was launched on 22 June 2010, at 19:00 UTC, from Palmachim Air Baise in Israel. It was delivered using an improved version of the Shavit launcher.
The payload is believed to be the multi-spectral "Jupiter" space camera produced by El-Op.[6][7][8][9] While precise imaging capabilities remain classified, sources say that like the still operating Ofeq-5 and Ofeq-7, Ofeq-9 offers a resolution "much better than" a half-meter.[7] The satellite was also said to be able to detect objects being carried by people.[10] The satellite operates in a retrograde low Earth orbit.[11]
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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Cubesats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses). |
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