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Collision Forecast System

Our probabilistic collision analysis tools predict potential conjunctions between space assets with high precision.

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How It Works

insights

Probabilistic Analysis

Combines TLE data, atmospheric models, and debris tracking to calculate collision risks using Monte Carlo simulations.

timeline

Risk Timeline

Visualizes potential conjunction times over a 7-day window with confidence intervals using adaptive error models.

Algorithm Overview

State Vector Estimation

Uses SGP4 and SDP4 models with covariance matrices to propagate orbital states.

Closest Approach Calculation

Numerically solves distance minimization problem using Runge-Kutta integration.

Collision Probability

Applies Gaussian distribution models to calculate PC using error ellipsoids around both objects.

CA: 300km ΔV: 0.5m/s

Technical Specifications

Parameter Value
Time Accuracy ±5s over 7-day prediction
Position Accuracy ±300m RMS (LEO)
Update Frequency 5 times/day for all cataloged objects
Debris Tracking 10+ million pieces cataloged
API Throughput 5000+ queries/second

Run a Simulation

Collision Simulation Parameters

Integration & Applications

Orbital visualizer interface showing conjunction timeline

Mission Planning

Identify potential collision risks during orbital transfers and station-keeping maneuvers.

Ground station monitoring space debris

Space Traffic Control

Monitor and coordinate with other space agencies to avoid collisions between active satellites.

Satellite maneuver planning interface

Mitigation Planning

Get detailed maneuver suggestions to avoid potential conjunctions.

Ready to integrate our collision prediction API?

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