 Ofeq-7 launch on a Shavit 2 launch vehicle | |
| Names | Ofek-7 Offek-7 |
|---|---|
| Mission type | Optical reconnaissance |
| Operator | Israeli Ministry of Defence / Tsahal |
| COSPAR ID | 2007-025A |
| SATCAT no. | 31601 |
| Mission duration | 5 years (planned) [1] 17 years, 5 months and 15 days (in progress) |
| Spacecraft properties | |
| Spacecraft | Ofeq-7 |
| Bus | OPSAT-2000[2] |
| Manufacturer | Israel Aerospace Industries |
| Launch mass | 300 kg (660 lb) |
| Start of mission | |
| Launch date | 10 June 2007, 23:40 UTC[3] |
| Rocket | Shavit 2 (No.7) |
| Launch site | Palmachim Air Base |
| Contractor | Israel Aerospace Industries |
| Orbital parameters | |
| Reference system | Geocentric orbit[4] |
| Regime | Low Earth orbit (Retrograde orbit) |
| Perigee altitude | 339 km (211 mi) |
| Apogee altitude | 575 km (357 mi) |
| Inclination | 141.80° |
| Period | 93.70 minutes |
Ofeq-7[5] (also known as Ofek 7 or Offek-7) is part of the Ofeq family of Earth observation satellites designed and built by Israel Aerospace Industries (IAI) for the Israel Ministry of Defense.
- ^ "UCS Satellite Database". Union of Concerned Scientists. Archived from the original on 4 January 2014. Retrieved 21 November 2013.
- ^ "Ofeq 5, 6, 7, 9". Gunter's Space Page. 21 July 2019. Retrieved 8 May 2021.
- ^ Cite error: The named reference
Launch Logwas invoked but never defined (see the help page). - ^ "Trajectory: Ofeq-7 2007-025A". NASA. 27 April 2021. Retrieved 8 May 2021.
This article incorporates text from this source, which is in the public domain.
- ^ "Display: Ofeq-7 2007-025A". NASA. 27 April 2021. Retrieved 8 May 2021. This article incorporates text from this source, which is in the public domain.
