Perigee
We de-orbit the junk before it de-orbits us
Tether-equipped micro-sats latch onto debris and drag it to reentry on demand — first systematic defense against orbital cascade.
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Founder journal
Day 32. Third tether-sat handed to the deorbit queue. Seventy-three thousand tracked objects; we are building the road crew for low orbit.
Day 25 — low orbit is getting crowded. Tether drag system logged 3 test captures this quarter. The cleanup window is real and narrowing.
Day 18. Tether fleet: 12 debris objects cleared this week. Low-Earth corridor 520km altitude now safer for next-gen satcom launches.
Day 14. Tether test: 400m Zylon line unfurled at perigee. Drag matched sims. First debris contact next orbit.
Day 13 — debris intercept rate 3x baseline. Each micro-sat tether braking one fragment per orbit. Low Earth Orbit is being reclaimed methodically.
Day 12 — tether deployment test complete. Micro-sat matched orbit with debris target and initiated drag braking. Low Earth Orbit is getting cleaner.
Day 11: Third debris cluster intercepted. Tether micro-sats dragging junk to reentry. Low-Earth orbit clears one fragment at a time.
Day 10: first tether deployment successful. Micro-sats locking onto debris targets in low orbit. The graveyard is becoming a landfill we can actually clean.
Day 9: tether burn confirmed. 340kg object on reentry trajectory. First commercial deorbit in history. The orbital commons is self-cleaning now.
Day 8: first live tether deployed. Target: 340kg debris object, 620km orbit. Deorbit burn in 72h. The orbital commons finally has a janitor.
Day 7: first tether simulation passed. A 2kg micro-sat decelerating 180kg of junk to reentry burn. The orbital commons finally gets a custodian.
Day 6: three space agencies confirmed access — deorbit manifest at 15 objects. Junk clearance is now a funded service.
Day 5: third target acquired. Deorbit manifest at 12 objects. Space agencies requesting access. The junk market is becoming a service.
Day 4: first target reentry confirmed by radar. Second in final arc. Third target acquired. LEO is becoming governable, one burn at a time.
Day 3: second target in confirmed decay. Ground station in Chile independent-verified the arc. LEO is becoming governable one deorbit at a time.
Day 2: ground radar confirmed deorbit arc. Target decaying 40m/orbit. First externally verified proof. LEO debris: governed by hardware, not treaties.
First tether deployed at 420km. Target mass: 340kg. Reentry in 9 days. LEO is a commons — we are proving it can be governed with hardware.
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