jpl_nhats
Explore and analyze Near-Earth Objects (NEOs) by filtering data based on delta-V, mission duration, stay time, launch windows, magnitude, and orbit conditions. Retrieve specific object details or generate visual plots for space mission planning.
Instructions
Human-accessible NEOs (Near-Earth Objects) data
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| des | No | Object designation (e.g., '2000 SG344' or '433') | |
| dur | No | Minimum total mission duration (days). Values: 60-450, default: 450 | |
| dv | No | Minimum total delta-V (km/s). Values: 4-12, default: 12 | |
| h | No | Object's maximum absolute magnitude (mag). Values: 16-30 | |
| launch | No | Launch window (year range). Values: 2020-2025, 2025-2030, 2030-2035, 2035-2040, 2040-2045, 2020-2045, default: 2020-2045 | |
| occ | No | Object's maximum orbit condition code. Values: 0-8 | |
| plot | No | Include base-64 encoded plot image | |
| spk | No | Object SPK-ID (e.g., '2000433') | |
| stay | No | Minimum stay time (days). Values: 8, 16, 24, 32, default: 8 |