A MATLAB-based tool designed to simulate satellite orbits, analyze perturbation effects, and predict collision risks using real-world TLE data. This project is perfect for students, researchers, and professionals in aerospace engineering.
- 📊 TLE Data Integration: Processes Two-Line Element (TLE) data to extract orbital parameters.
- 🌌 3D Orbit Visualization: Simulates and visualizes satellite trajectories in 3D.
- 📈 Perturbation Analysis: Models long-term effects of J2 perturbation, atmospheric drag, and solar radiation pressure.
⚠️ Collision Risk Prediction: Calculates proximity between satellites and predicts collision risks.- 🛰️ Multi-Satellite Simulation: Simulates constellations like Starlink for advanced analysis.
- Load TLE Data: Start with real TLE data, such as the provided
last-30-days.txt. - Process Orbital Parameters: Extract inclination, eccentricity, RAAN, and more.
- Visualize Orbits: Generate 3D plots of satellite orbits.
- Analyze Perturbations: Observe long-term changes in orbital parameters.
- Predict Risks: Identify potential satellite collisions.
- MATLAB: Version R2021a or later
- TLE Data File: Example provided in the repository (
last-30-days.txt)
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