high machines

Impossible. But doable.

Orbital data centres for AI inference. European sovereign. Architecture-lock phase.

Closer to the data

Why orbital compute wins: round-trip latency scales with altitude. LEO is a hundred times faster than GEO. The Moon is 2,500× slower. The Sun–Earth Lagrange points are minutes away.

LEO Low Earth Orbit
Distance: 550 km
Round-trip latency: 4 ms (geometric: 3.7 ms)
MEO Medium Earth Orbit
Distance: 5,500 km
Round-trip latency: 50 ms (geometric: 36.7 ms)
GEO Geostationary Orbit
Distance: 35,786 km
Round-trip latency: 600 ms (geometric: 238.6 ms)
Lunar surface Moon surface (near side)
Distance: 384,400 km
Round-trip latency: 2.56 s (geometric: 2.56 s)
Lunar orbit Satellite orbiting the Moon
Distance: 384,400 km
Round-trip latency: 2.56 s (geometric: 2.56 s)
L1 Sun–Earth Lagrange 1 (between Earth and Sun)
Distance: 1,500,000 km
Round-trip latency: 10 s (geometric: 10.00 s)
L4 Sun–Earth Lagrange 4 (60° ahead of Earth)
Distance: 149,600,000 km
Round-trip latency: 16.7 min (geometric: 16.6 min)
L5 Sun–Earth Lagrange 5 (60° behind Earth)
Distance: 149,600,000 km
Round-trip latency: 16.7 min (geometric: 16.6 min)

The Three Whys

The full story lives on /story. Here's the 30-second version.

Why this

The orbital compute thesis.

AI inference is bottlenecked by terrestrial power, cooling, and grid constraints. Orbital data centres eliminate all three: continuous solar, radiative cooling into deep space, no permitting on the ground.

Why now

The 18-month architecture window.

Launch costs crossed the LEO economic threshold in 2024. AI inference demand scaled 10× in 2025. Whoever locks the architecture by mid-2027 sets the standards the primes have to comply with. We are racing for the standard, not the compute market.

Why us

6 AI4CE papers + a PhD in mission-architecture design.

JP (the founder) has spent 4 years building the AI4CE methodology — agent-based deep-RL for CubeSat system generation. 6 peer-reviewed papers, 1 ESA CDF collaboration, the only open-stack agent framework for concurrent engineering in space.

Read the full Three Whys on /story

120 satellites 600 km LEO 100 TFLOPS/sat 5 EU ground stations
Seed stage Raising €2–5M Architecture lock phase ~24 months to Series A

Who are you?

The site has a different pitch for each audience. Pick the one that fits.

Investors

VCs, angels, family offices, strategic investors. The Three Whys + the ask.

Customers

Data centres, European-AI companies. The SLA, the workload fit, the timeline.

Partners

Satellite builders, ground-station operators, integrators. Reciprocal, network-effects.

Regulators

EU, ESA, national space agencies. Sovereign, policy-aligned, evidence-led.