Orbital Safety System of Record

FinisImpact

End impacts. From orbit to Earth.

Real-time orbital risk scoring for satellites and near-Earth objects. API-first. Decision-ready. Autonomy-ready.

NEO Surveyor spacecraft in infrared starfield. NASA/JPL-Caltech, public domain. Goldstone radar observations of asteroid 99942 Apophis. NASA/JPL-Caltech, public domain. Electro-mechanical actuators for thrust vector control. NASA, public domain.

Detect. Decide. Deflect.

Three layers of orbital protection. From conjunction screening to autonomous maneuver planning to planetary defense.

01

Detect

Ingest global SSA catalogs (18th SDS), TLEs, operator ephemerides, and NEO feeds from NASA CNEOS. Continuous screening at scale, millions of conjunction checks per day.

02

Decide

Probabilistic collision risk (Pc), covariance propagation, ranked conjunctions. Fuel-aware maneuver options with delta-v, cost, and miss distance. Cut noise by 90%+.

03

Deflect

Actionable burn plans today. Mission design for kinetic impactor deflection tomorrow. From satellite avoidance to asteroid redirection, the same physics, the same platform.

Numbers, not adjectives

10M+
Conjunction checks per day across active catalog
90%
Noise reduction: top-N actionable alerts only
Δv
Fuel-optimized maneuvers that extend satellite life
Reg-ready
Compliance reporting for regulators and insurers
"You monetize collision avoidance for satellites today. You earn the right to do asteroid deflection tomorrow."
Core Thesis

Three phases to planetary scale

Each phase unlocks revenue and credibility for the next. Sell orbit safety now, earn the right to defend Earth later.

V1: Now

Orbit Safety

Ingest SSA catalogs (18th SDS), TLEs, operator ephemerides. Compute conjunction assessment (Pc), covariance propagation, screening. Output ranked alerts with recommended maneuvers, delta-v, fuel cost, and miss distance. Deliver via API, dashboard, email/webhooks.

V2: Expand

Autonomous Maneuvers

Integrate with flight software and ops consoles. One-click burn plans with closed-loop verification post-maneuver. Debris avoidance and traffic management layer for constellation operators.

V3: Defend

Planetary Defense

NEO ingestion from NASA CNEOS. Impact probability pipelines, scenario simulation. Deflection playbooks (kinetic impactor, targeting windows, mission design partners). The DART mission proved it works. We build the operational layer.

Request early access

We're onboarding satellite operators and constellation teams for V1. Tell us about your operations.

What you get

API access to conjunction assessment, ranked alerts, and maneuver recommendations. Dashboard for ops teams. Webhook integration for automated workflows.

Real-time conjunction screening against full public catalog
Probability of collision (Pc) with covariance propagation
Delta-v optimized maneuver recommendations
Compliance-ready reporting (FCC, ITU, insurers)

Tell us about your mission

Early access program. We respond within 24 hours.