Names | Ofek-9 |
---|---|
Mission type | Optical reconnaissance |
Operator | Israeli Ministry of Defence / Tsahal |
COSPAR ID | 2010-031A |
SATCAT no. | 36608 |
Mission duration | 5 years (planned) [1] 14 years and 27 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-10 →
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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.
It was launched on 22 June 2010, at 19:00 UTC, from Palmachim Air BaiseinIsrael. 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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