Role & capabilities
- Reconnaissance
- Primary domain
- Air
- System type
- Reconnaissance aircraft
- Developer / manufacturer
- Aeronautics
- Origin / production countries
- Israel
- Other names
- No additional names recorded
- Variants / configurations
- Not distinguished in reviewed sources
- Operators / programme customers
- Not identified in reviewed sources
Evidence & current status
Supplier information is attributed; performance and operational acceptance require configuration-specific evidence.
Orbiter 5 extends the Aeronautics tactical surveillance family into a larger airframe and longer-duration offering. The current product page identifies a seventy-five-kilogram maximum take-off configuration and a modular multisensor architecture. Its reconnaissance role is distinct from the family’s expendable products.
The manufacturer describes runway independence and autonomous flight/recovery functions. These broad architecture statements do not establish that every launch method used elsewhere in the Orbiter family applies to this model. Detailed equipment and customer acceptance need model-specific evidence.
The displayed duration, speed and ceiling are supplier maxima. They should not be treated as one simultaneously achievable operating point. A current product listing supports inclusion in the reference catalogue but is not a complete military inventory. The record leaves named operators and any undisclosed dimensional or propulsion details open, providing a clear baseline for later contract and flight-test updates.
Sourced specifications
Figures apply to the named configuration. Maximum values are not guaranteed operating performance.
| Specification | Reported value | Context & source |
|---|---|---|
| Airframe | Runway-independent fixed wing | Current supplier configuration; maxima are not necessarily simultaneous. Source |
| Launch / recovery | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Propulsion | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Dimensions | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Mass | 75 kg maximum take-off | Current supplier configuration; maxima are not necessarily simultaneous. Source |
| Endurance | Up to 25 hours | Current supplier configuration; maxima are not necessarily simultaneous. Source |
| Range | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Speed | 70 knots maximum | Current supplier configuration; maxima are not necessarily simultaneous. Source |
| Altitude | 18,000 ft maximum | Current supplier configuration; maxima are not necessarily simultaneous. Source |
| Payload | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Sensors | Multiple modular imaging, radar and intelligence payload options | Current supplier configuration; maxima are not necessarily simultaneous. Source |
| Communications / navigation | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
Publication history
- — Published reference update.
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Follow the evidence
Source types identify who makes the claim. Programme milestones and supplier statements should be read in context.