

Very-low Earth orbit is now accessible. Where others can't fly, NEO-1 thrives — delivering next-level imaging, global connectivity, real-time data, and redefining what's possible in orbit.
Aplatformforvery-lowEarthorbit.
NEO-1 is a product of years of relentless engineering. It’s a first and only spacecraft capable of operating at altitudes between 200 and 300 km for five years. Its control design, breakthrough propulsion system, and advanced materials—everything is crafted to make the ride in very-low Earth orbit as smooth as possible.
Discover the precision, performance, and groundbreaking capabilities of NEO-1, the world's first, and only satellite engineered for sustained operations in very-Low Earth Orbit.
km
• Target Orbit
200-300 km
• Payload Type
EO, Telco, GNSS, RF
• Payload Mass
50 kg
• Telecom
S-band & X-band
• Slew rate
1 deg/s
• Power
200 W OAP (modifiable)
• Lifetime
5 years


Atmospheric Drag
The closer to Earth, the thicker the atmosphere, the faster orbital decay. While conventional satellites stay in space for decades, very-low Earth orbit satellites re-enter the atmosphere within weeks, requiring constant orbit correction using propulsion. Until now, the propellant needed to correct the orbit made operations at these altitudes impossible.

Atomic Oxygen
Not all materials can survive in very-low Earth orbit. Atomic oxygen reacts with surfaces and electronics, quickly degrading them, damaging payloads, and shortening the satellite’s lifespan.

Aerodynamic Torques
In very-low Earth orbits, even minor asymmetries generate unwanted torque, making precise, controlled flight an engineering challenge.
HowNEO-1staysclose.
Each challenge above has an answer engineered into NEO-1: AURA for drag, atomic-oxygen-tolerant materials for oxidisation, and aerodynamic symmetry for torques.
Built for efficient, sustained operation in very-low Earth orbit, AURA is our breakthrough xenon-driven propulsion system. It delivers four times higher specific impulse than typical alternatives, achieving the same capabilities with four times less propellant.

At VLEO altitudes, atomic oxygen aggressively degrades exposed surfaces and electronics. NEO-1's structural alloys and exterior architecture are selected and laid out to resist this degradation — protecting the platform, the payload and the five-year mission life.

In VLEO, even minor geometric asymmetries generate unwanted torque. NEO-1's symmetrical geometry, forward centre of mass, and precision ADCS neutralise aerodynamic torque — giving hosted payloads the pointing stability they need.

AURA is our in-house electric propulsion system, in development since 2021 and now in its seventh generation. It uses a radio-frequency thruster and a proprietary cathode to deliver four times the specific impulse of conventional electric propulsion. That difference is what makes a five-year mission at 200–300 km possible.

Meet AURA-X, our breakthrough propulsion system, driving unmatched efficiency and sustained operation at very-low Earth orbit. It delivers four times higher specific impulse than typical alternatives, requiring four times less propellant.
(s) Specific impulse
• Propellant
Xenon
• Total Power
100-750 W
• Thrust level
4-20 mN
• Specific impulse
up to 4500s