plot_orbit_elements
Plots the time evolution of Keplerian orbital elements for a satellite over a defined propagation arc, showing changes in each of the six classical elements.
Instructions
Plot Keplerian orbital element evolution over a propagation arc.
Uses brahe's plot_keplerian_trajectory to show how each of the 6 classical orbital elements changes over time.
Args: satellite: Satellite spec dict (same format as compute_access). start_epoch: Start epoch (ISO string). end_epoch: End epoch (ISO string). step_seconds: Propagation step size in seconds (default 60).
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| end_epoch | Yes | ||
| satellite | Yes | ||
| start_epoch | Yes | ||
| step_seconds | No |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
| result | Yes |