Kepler propagate

Universal-variable two-body state propagation (AGC KEPLER problem class).

SIDUS educational calculator. Category orbital. Tags: apollo, GNC, orbital, trajectory. Pure SI. Not flight software.

Formula

r(t), v(t) ← χ · √μ (t−t₀) = f(χ, α, r₀, v₀)

Two-body state propagation (AGC class)

Primary sources

How do AI agents use this tool?

Read /llms.txt or call https://sidus.tools/api/mcp. Open the interactive page for live SI inputs.

Open interactive tool · SIDUS