VECTORDEFENCE DRONE
INTELLIGENCE
INDEPENDENT PERSPECTIVE
THE EVOLVING FIELD GUIDE
Editor

DEFENCE DRONES / THE LIBRARY

Compare the evidence.

Choose up to three systems. Specifications retain their source and configuration; missing information is left undisclosed.

Orbiter 2 LM

Current electric loitering-munition entry in the Orbiter family, separated from the reusable ISR aircraft.

Country / region
Israel
Programme status
Supplier-reported status
Sources reviewed
21 Sept 2026
Supplier-reported statusSupplier-reported status
Primary domain
Air
System type
Loitering munition
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.

Role & capabilities

  • Loitering munition programme

Specifications in context

Airframe
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
Electric

Current supplier configuration; maxima are not necessarily simultaneous.

Source
Dimensions
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Mass
13 kg maximum take-off

Current supplier configuration; maxima are not necessarily simultaneous.

Source
Endurance
Not established: current headline omits the unit

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
Not established: current maximum lacks a flight-condition definition

Current supplier configuration; maxima are not necessarily simultaneous.

Source
Altitude
16,000 ft maximum advertised

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
Stabilised dual EO/IR

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