plot_altitude
Propagates satellite orbit and plots geodetic altitude over time. Visualize orbital decay, eccentricity effects, and maneuver impacts.
Instructions
Plot satellite altitude (above WGS84 ellipsoid) versus time.
Propagates the orbit and converts each ECEF position to geodetic altitude. Useful for visualizing orbital decay, altitude variations due to eccentricity, and maneuver effects.
Args: satellite: Satellite spec dict (same format as compute_access). Must include "source" key ("tle", "gp_record", or "state"). start_epoch: Start epoch (ISO string). end_epoch: End epoch (ISO string). step_seconds: Propagation step size in seconds (default 60). title: Optional plot title.
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| title | No | ||
| end_epoch | Yes | ||
| satellite | Yes | ||
| start_epoch | Yes | ||
| step_seconds | No |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
| result | Yes |