Names | Ofeq-8 TechSar Polaris |
---|---|
Mission type | Imaging radar |
Operator | Israel Aerospace Industries (IAI) |
COSPAR ID | 2008-002A |
SATCAT no. | 32476 |
Mission duration | 4 years (planned) 16 years, 5 months and 12 days |
Spacecraft properties | |
Bus | TECSAR Bus |
Manufacturer | Israel Aerospace Industries (IAI) |
Launch mass | 295 kg (650 lb) [1] |
Power | 750 watts |
Start of mission | |
Launch date | 21 January 2008, 03:45 UTC |
Rocket | PSLV-CA (PSLV-C10) |
Launch site | Satish Dhawan, FLP |
Contractor | Indian Space Research Organisation |
Entered service | 1 February 2008 |
End of mission | |
Decay date | 3 July 2024 |
Orbital parameters | |
Reference system | Geocentric orbit[2] |
Regime | Low Earth orbit |
Perigee altitude | 405 km (252 mi) |
Apogee altitude | 580 km (360 mi) |
Inclination | 41.03° |
Period | 94.50 minutes |
TecSAR-1, also known as TechSAR, Polaris and Ofeq-8,[3] is an Israeli reconnaissance satellite, equipped with a synthetic-aperture radar (SAR) developed by Elta Systems. It was successfully launched at 03:45 UTC on 21 January 2008, by PSLV C-10 launch vehicle, from the Satish Dhawan Space Centre in India.[4]
The TecSAR satellite is fitted with a large dish-like antenna to transmit and receive radar signals that can penetrate darkness and thickness of clouds. Built by Israel Aerospace Industries, TecSAR ranks among the world's most advanced space systems.[5]
Elta Systems Ltd cooperates with Azerbaijan to produce a TecSAR reconnaissance satellite system for the country.[6] According to Azerbaijani military experts, this is an indispensable system for military operations in the mountainous terrains of Azerbaijan.[7]