Propagates a circular two-body orbit from altitude, inclination, RAAN, and initi...
https://space.halowerk.com/v1/satellite-passOverview
Propagates a circular two-body orbit from altitude, inclination, RAAN, and initial orbital phase; rotates Earth at a fixed sidereal rate; and samples ground-station elevation. It ignores eccentricity, perturbations, epoch-dependent Greenwich angle, refraction, ellipsoid shape, terrain, and antenna masks, so it is a planning estimate rather than operational ephemeris.
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| Time | Status | HTTP | Latency | Error |
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| 2026-10-31 07:11:00 | healthy | 402 | 634ms | |
| 2026-10-31 06:08:32 | healthy | 402 | 402ms | |
| 2026-10-31 05:10:02 | healthy | 402 | 489ms | |
| 2026-10-31 04:06:52 | healthy | 402 | 85ms | |
| 2026-10-31 03:19:00 | healthy | 402 | 435ms |