VLEO-1 provides an IOD/IOV mission integration platform that validates space hardware in orbit and converts successful tests into reusable, cataloged capabilities for future missions.
Funding
Funding not disclosed
Founders
Product
Problem
Space hardware developers must spend $5‑15 M and months building dedicated satellites or securing limited hosted slots to obtain the in‑orbit demonstration needed for market adoption. This custom, one‑off approach creates high risk, long timelines, and prevents reusable, cataloged capabilities from emerging.
Solution
Satelyx’s VLEO‑1 mission acts as an IOD/IOV integration platform that provides a dedicated ~8 kg, 50 W payload slot on a 400 km sun‑synchronous orbit launching in Q3/Q4 2027. Technology providers submit their hardware, which Satelyx integrates, operates, and validates in orbit, delivering flight data, performance evidence, and standardized interface documentation. Each successful validation is added to a growing catalog of flight‑proven components that can be redeployed on future missions, reducing cost and risk for subsequent customers. The platform includes full mission services—power, thermal management, high‑speed X‑band downlink, orbit maintenance, and 48‑hour response to inquiries—so developers focus solely on their payload. By turning one‑off demonstrations into reusable infrastructure, Satelyx compresses development timelines from years to months and creates a shared supply chain for space technology.
Target Audience
Primary customers are technology developers and hardware manufacturers in propulsion, sensors, communications, AI edge compute, and related domains that require in‑orbit demonstration and a reusable deployment pathway.
Features
- ~8 kg payload capacity with 50 W (24.5‑29.2 V) dedicated power and 450 Mbps X‑band downlink
- Standardized mechanical, electrical, and data interfaces plus integration “recipes” for rapid payload insertion
- Full mission operations support: thermal control, orbit maintenance (N2O propulsion), and 0.1° pointing accuracy
- Flight‑heritage catalog entry that includes flight data, interface specs, operational constraints, and reuse path
- Agile Prime model that compounds validation evidence across missions, lowering integration risk over time
- 48‑hour response time for payload inquiries and mission design feedback