TLE-Based Orbital Propagation Validation
Methodology and results for validating orbital propagation accuracy against public two-line element data from Space-Track and CelesTrak.
Coming soonResources
Technical research and analysis documents from the KNOWN engineering team. Whitepapers will be published as the platform approaches institutional release.
Methodology and results for validating orbital propagation accuracy against public two-line element data from Space-Track and CelesTrak.
Coming soonA framework for integrating orbital simulation into mission planning workflows for Low Earth Orbit operations.
Coming soonEngineering decisions behind the KNOWN physics engine: propagation models, validation-first development, and the implementation sequence.
Coming soonMethods for determining satellite visibility windows, ground contact periods, and coverage zone analysis in LEO.
Coming soon