iss-orbit-calculation

TLE propagation calculates ISS orbital positions by parsing Two-Line Element data and using SGP4 algorithms via satellite.js to compute real-time coordinates. This Skill automates TLE validation, propagation, and position calculation to track satellite location accurately over time.

ECI to geodetic conversion transforms Earth-Centered Inertial coordinates into usable geographic coordinates. This Skill performs coordinate conversion and distance validation, enabling you to translate orbital calculations into ground-based positions for tracking and verification.

Yes. TLE format validation checks Two-Line Element structure and syntax before propagation starts. This Skill implements robust validation and error handling to catch malformed TLE data early, preventing downstream propagation failures.

Path generation computes ISS positions at multiple time intervals to forecast orbital passes and trajectories. This Skill generates predicted paths by propagating TLE data and computing positions across a time range, supporting pass prediction and accuracy debugging workflows.

TLE propagation estimates orbital position from published element sets using mathematical models, while GPS provides direct measured location. TLE propagation is lower-cost and works for any tracked satellite; this Skill automates that calculation and validation for ISS tracking.

Yes. This Skill integrates satellite.js for SGP4 orbital propagation, TLE parsing, and coordinate conversion. satellite.js provides the core algorithms; this Skill wraps validation, error handling, and geodetic conversion for ISS-specific workflows.