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Our high-quality small satellite systems benefit lives here on Earth.

40

ACTIVE PROGRAMS

10

YEARS on orbit

100

%

mission success

Hover on one of our mission opportunities to learn more →

MISSILE WARNING / MISSILE DEFENSE

COMMUNICATIONS

ADVANCED SPACE

INTELLIGENCE, SURVEILLANCE, & RECONNAISSANCE

MISSILE WARNING / MISSILE DEFENSE

COMMUNICATIONS

ADVANCED SPACE

INTELLIGENCE, SURVEILLANCE, & RecoNNAISSANCE

Earth
Moon

Solutions Across Orbits

We are focused on affordability, performance and flexibility to deliver autonomous, dynamic spacecraft for our customers’ missions. We offer highly agile and maneuverable small satellites that are flexible to host different payloads across orbits. And the onboard processing we’ve developed has proven to be orders of magnitude better than heritage systems. 

LEO

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ISR

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ADV. SPACE*

Icon - Communications

COMMS*

MEO

Icon - MW/MD

MW/MD

Icon - Communications

COMMS*

GEO

Icon - MW/WD

MW/MD

ADV. SPACE*

Icon - Communications

COMMS*

V-LEO

200-300 km

Future small satellite opportunities are in V-LEO, or very-low Earth orbit, approximately 150 km above Earth. V-LEO utility includes quick missions for tactical support. These systems operate much closer to the ground and have very short mission lives, resulting in lower all-around costs. Tactically relevant capabilities tailored for theater operations for specific time periods is a new market opportunity.

LEO

300-1200 km

We can design to any requirements in low Earth orbit. We can provide one-to-three-year lifetimes or three-to-seven-year lifetimes with selective-redundancy approaches. Our systems offer green, monopropellant and bipropellant propulsion.

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10kg - 1,000kg Class

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Up to 500 w

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12u to ESPA Grande typical

MEO

1200-35000 km

We can design to any requirements in medium Earth orbit. We can provide one-to-three-year lifetimes or three-to-seven-year lifetimes with selective-redundancy approaches. Our systems are rated to MEO radiation environments and offer electric, monopropellant and bipropellant propulsion.

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50kg - 3,000kg Class

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Up to 4,000 w

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1/2 ESPA to launch-vehicle limited

GEO

35000-37000 km

We can design to any requirements in medium Earth orbit. We can provide one-to-three-year lifetimes or three-to-seven-year lifetimes with selective-redundancy approaches. Our systems are rated to MEO radiation environments and offer electric, monopropellant and bipropellant propulsion.

Icon.- ISR

50kg - 3,000kg Class

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Up to 4,000 w

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1/2 ESPA to launch-vehicle limited

Cis-lunar

≤ 400,000 km

With lower cost launch and manned-missions to the moon, the econosphere in cis-lunar space will grow. The need to service and protect this new space operations domain will grow over time. The orbit agnostic capabilities we’ve developed are easily transitioned to cis-lunar.

GEO

35000-37000 km

We can design to any requirements in geosynchronous orbit. We can provide small satellites with three-to-five-year lifetimes with single-string avionics or five-to-seven-year lifetimes with selective-redundancy approaches. Our systems are rated to GEO radiation environments and offer electric, monopropellant and bipropellant propulsion.

Icon.- ISR

50kg - 3,000kg Class

Icon.- ISR

Up to 4,000 w

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1/2 ESPA to launch-vehicle limited

WFOV Space Program, Set for 2022 Launch

MEO

1200-35000 km

We can design to any requirements in medium Earth orbit. We can provide one-to-three-year lifetimes or three-to-seven-year lifetimes with selective-redundancy approaches. Our systems are rated to MEO radiation environments and offer electric, monopropellant and bipropellant propulsion.

Icon.- ISR

50kg - 3,000kg Class

Icon.- ISR

Up to 4,000 w

Icon.- ISR

1/2 ESPA to launch-vehicle limited

WFOV Space Program, Set for 2022 Launch

LEO

300-1200 km

We can design to any requirements in low Earth orbit. We can provide one-to-three-year lifetimes or three-to-seven-year lifetimes with selective-redundancy approaches. Our systems offer green, monopropellant and bipropellant propulsion.

Icon.- ISR

10kg - 1,000kg Class

Icon.- ISR

Up to 500 w

Icon.- ISR

12u to ESPA Grande typical

WFOV Space Program, Set for 2022 Launch

V-LEO

200-300 km

Future small satellite opportunities are in V-LEO, or very-low Earth orbit, approximately 150 km above Earth. V-LEO utility includes quick missions for tactical support. These systems operate much closer to the ground and have very short mission lives, resulting in lower all-around costs. Tactically relevant capabilities tailored for theater operations for specific time periods is a new market opportunity.

Cis-lunar

≤400,000 km

With lower cost launch and manned-missions to the moon, the econosphere in cis-lunar space will grow. The need to service and protect this new space operations domain will grow over time. The orbit agnostic capabilities we’ve developed are easily transitioned to cis-lunar.

Scalable Missions to Meet Your Needs

Single
Satellites

We develop single small satellites to support development programs and to prototype phenomenologies and/or mission payloads.

Prototype
‍Constellations

We develop prototype collaborative small satellites and operations, with a minimum of three small satellites.

Large
Constellations

We develop large constellations based on our single satellites and prototype constellation designs.