LEO Express

Host or deploy your payload in any orbit with flexible maneuverability and smarter constellation deployment.


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Hardware

Meet Mira

Fast and precise on-demand maneuvering with best-in-class propulsion

Mira Hardware
Saiph 5-lbf thruster

Saiph 5-lbf thruster

Mira orbital maneuvering vehicle

Mira orbital maneuvering vehicle

In-house composite overwrapped propellant tanks

In-house composite overwrapped propellant tanks

Services

A Flexible Ride to Any Orbit

Reliable and affordable ride to space for Smallsats
Reliable and affordable ride to space for Smallsats
Competitive pricing
Quality-controlled in-house subsystems
Interoperable with all major launch providers
Last mile delivery to any orbit in LEO
Last mile delivery to any orbit in LEO
Don’t be restricted by your launch drop-off orbit
Choose your altitude, inclination, and plane
Trusted maneuvers with best-in-class propulsion systems
Precision Earth re-entry injection service
Precision Earth re-entry injection service
Up to two 150 kg re-entry capsules at once
High delta-V maneuver for a precision re-entry ellipse
Enabled by high-thrust chemical propulsion
Smarter constellation deployment
Smarter constellation deployment
Fastest method of constellation deployment
Deploy into multiple planes (RAAN) with a single launch
Custom phasing with precise orbit insertion
Mobile payload hosting
Mobile payload hosting
Maneuver on-demand for flexible mission operations
3-axis control for accurate pointing
Common interfaces for easy integration
Test your space system on-orbit
Test your space system on-orbit
An easy and affordable way to get flight heritage for your space technology
Dedicated mission design and operations support
Customize your on-orbit demo with us

Specifications

Deploy or Host your Payload

Specification
Payload Capacity
Up to 300 kg
Payload Volume
50 x 73 x 50 cm (x2)
Payload Interface
15-in ring, 24-in ring, or custom interface
Delta-V
600 m/s for 300 kg payload
Mira Wet Mass (no payload)
250 kg
Propulsion
8x 5 lbf Saiph thrusters
Propellant
Ethane and nitrous oxide
Reaction Control System
16x cold gas thrusters
Orbital Insertion Accuracy
± 2 km semi-major axis, ±0.001 eccentricity, ±0.01° inclination, ±1° mean anomaly
Deployer Provided
Optional
Contact Us for CAD file of Payload Envelope

Book your Mission

Upcoming Missions

MissionDateLaunch VehicleDrop-off OrbitMass AvailableVolume AvailableAvailability
LEO Express-1Oct 2023SpaceX F9500-600 km SSOUp to 300 kgUp to 50x73x50 cmReservations Closed
LEO Express-2Jun 2024SpaceX F9500-600 km SSOUp to 300 kgUp to 50x73x50 cmAsk Us
LEO Express-3Oct 2024SpaceX F9500-600 km SSOUp to 300 kgUp to 50x73x50 cmSpace Available
Custom MissionChoose your timelineAny launch vehicleLEO, MEO, GEO, cislunarUp to 500 kgCustomAsk Us
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