Ofec 3 / 1995 - 018A
Spacecraft propulsion supplied by ArianeGroup
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Ofec 3 / 1995 - 018A
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Category | Reconnaissance |
| Operator | Israel Space Agency | |
| Orbit | LEO | |
| Sat position | 368 km x 729 km | |
| Launch date | 5.4.1995 | |
| Launch mass | 225 kg | |
| Design life | - | |
| Launcher | Shavit | |
| Satellite / Bus | - | |
| Manufacturer | Israel Aircraft Industry (IAI) | |
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Orbital Propulsion Centre Contribution
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2 x 20 N hydrazine thruster, CHT 20
