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ORBITAL MECHANICS CALCULATOR
Keplerian propagation · J2 perturbations · Transfer ΔV · Sweep analysis · Universal tool /calc/orbital
SI Units
Universal Tool — W1–W6 callable
Plotly Visualisation
JetBrains Mono · Inter
Configuration
Central Body
Nodal precession from equatorial oblateness (J2 = 0.001083 Earth default)
Orbital Presets
Initial State
Propagation
86400 s = 1 day
Transfer Analysis
Run calculation to see orbital summary.
Run calculation to see trajectory data.
State Vectors at Key Points
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Run calculation to see transfer analysis.
Burn Sequence
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Multi-orbit comparison. Add configurations via the left panel.
| # | Label | a (km) | e | i (°) | Period (min) | vᵀ (m/s) | ΔV→GEO (m/s) | |
|---|---|---|---|---|---|---|---|---|
| No orbits added yet | ||||||||
Parameter sweep — vary one variable across a range and map system-wide response. Results route to active workspace dataspace.
Sweep Statistics
Run sweep to see statistical summary.
All exports include full state manifest. GMAT scripts are ready for /data/w5 integration. Workspace sends route to localStorage (Achilles-compatible — no duplicate data layers).
File Exports
→ Send to Workspace Dataspace
Routes results to Achilles localStorage layer. Single record per workspace — no duplicate data sets.
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Export Preview
Select format above to preview export content.
Ready — configure parameters and run calculation
Universal Calculator | Callable by all workspaces:
W5 DATASPACE
W4 DATASPACE
ACHILLES DASH
● initialising beacon...