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// MISSION_MANIFEST

Mission Manifest

Our scheduled missions and payload slots. Join the next wave of space validation.

IN DEVELOPMENT
Sun-synchronous VLEO

VLEO-1

Codename: UKS2

100kg-class sun-synchronous platform at 400km with ~8kg available for customer payloads. High-speed X-band data downlink (450 Mbps), N2O propulsion for orbit maintenance, and precision three-axis attitude control. Payload interfaces via CAN bus and RS422.

PAYLOAD CAPACITY
~8 kg
PAYLOAD POWER
~50W
ALTITUDE
400 km
DURATION
2 years
LAUNCH
Q2/Q3 2027
DOWNLINK
Up to 450 Mbps
POINTING
0.1° (0.005°/s)
INTERFACES
CAN bus, RS422
TARGET PAYLOADS:
Earth observation Data communication systems (D2D) Sensor demonstration
COMPLETE
LEO

Mission 0

Our first orbital mission. Validated core capabilities including Earth observation, AI edge compute, and communications on a partner satellite platform. Three catalog entries confirmed.

ALTITUDE
500 km
DURATION
Ongoing
LAUNCH
Q4 2024
ORBIT
LEO
TARGET PAYLOADS:
Earth observation AI edge compute Communications
// JOIN_A_MISSION

How It Works

From first contact to flight heritage in five steps.

1

Submit Requirements

Share your payload specs and mission goals through our contact form.

2

Technical Review

Our team assesses payload compatibility, interfaces, and mission fit.

3

Integration Planning

We work with you on timelines, interfaces, and testing milestones.

4

Validation Flight

Your hardware launches and operates on orbit. We manage the mission.

5

Catalog Entry

Successful hardware earns flight heritage and joins our catalog for re-flights.