# atging/two-body-orbit-generator

> Takes position and velocity vectors and central body information as inputs. Determines type of orbit, Keplerian elements, and whether the spacecraft is on an impactor trajectory. Computes the position and velocity vectors at a user input specified time.

- **Canonical URL**: https://githubrepo.cloud/repo/atging/two-body-orbit-generator
- **GitHub Repository**: https://github.com/atging/two-body-orbit-generator
- **Maintainer / Creator**: https://github.com/atging
- **Discovered On**: Sep 29, 2026

---
*Indexed by GitHubRepo (https://githubrepo.cloud). Real-time open-source discovery & telemetry.*