Small electric loitering munition derived from the Orbiter 2 mini-UAS, designed for soft-target attack with a video tracker and abort/re-attack capability; reusable via parachute if not detonated.
| Country | Israel |
|---|---|
| Subcategory | Loitering munitions |
| Subtype | Loitering munition |
| Role | Loitering munition / strike |
| Class | Class I (Mini) |
| Classification | Class 1 / mini-UAS loitering munition |
| Mission | ISR, Strike |
| Datalink | Digital RF (~100 km module) |
| MTOW (kg) | 40 |
| Operators | Greece |
| Frame type | Fixed-wing |
| Propulsion | Electric |
| Range (km) | 200 |
| Wingspan (m) | 2.9 |
| Combat-proven | Yes |
| Export status | Exported |
| Launch method | Catapult |
| Autonomy level | Operator-in-the-loop with abort |
| Endurance (min) | 180 |
| Recovery method | Parachute/airbag (if not expended) |
| Max payload (kg) | 5.5 |
| Max speed (km/h) | 130 |
| Standard sensors | Day/night EO camera, Video tracker |
| Production status | Active |
| Service ceiling (m) | 3962 |
| Airframe / lift type | Fixed-wing |
| Control / autonomy level | Semi-autonomous (human-on-the-loop) |
| Domain | Aerial (UAV/UAS) |
| Mission / use case – military | ISR, Loitering munition (one-way attack) |
| Origin / supply chain | Military-grade |
| Propulsion | Electric (LiPo / Li-ion) |
| Range / endurance | Short range (50–150 km) |
| Signature / detectability | RCS – small, RF-emitting |
| Speed regime | Medium (50–150 km/h) |
| Strike depth / operational role | Middle strike (20–150 km, operational rear: logistics, artillery, EW, C2) |
| Threat vector | Kinetic – loitering munition, Surveillance / reconnaissance |
| Weight / class | Class I – Small (20–150 kg), FAA >25 kg (Part 137 / waiver) |