HALOWERKSpacewerk
satellite pass
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.
POST https://space.halowerk.com/v1/satellite-passEingaben
| Feld | Typ | Pflicht | Beschreibung |
|---|---|---|---|
| altitude_km | number | Ja | Circular altitude above a spherical Earth. |
| inclination_deg | number | Ja | |
| raan_deg | number | Ja | Right ascension of ascending node relative to Greenwich at t=0. |
| initial_phase_deg | number | Ja | Argument of latitude at t=0. |
| ground_latitude_deg | number | Ja | |
| ground_longitude_deg | number | Ja | |
| duration_seconds | integer | Ja | |
| step_seconds | integer | Ja | |
| minimum_elevation_deg | number | Ja |
Vollständiges Eingabeschema anzeigen
{
"type": "object",
"required": [
"altitude_km",
"inclination_deg",
"raan_deg",
"initial_phase_deg",
"ground_latitude_deg",
"ground_longitude_deg",
"duration_seconds",
"step_seconds",
"minimum_elevation_deg"
],
"additionalProperties": false,
"properties": {
"altitude_km": {
"type": "number",
"minimum": 100,
"maximum": 100000,
"description": "Circular altitude above a spherical Earth."
},
"inclination_deg": {
"type": "number",
"minimum": 0,
"maximum": 180
},
"raan_deg": {
"type": "number",
"minimum": -360,
"maximum": 360,
"description": "Right ascension of ascending node relative to Greenwich at t=0."
},
"initial_phase_deg": {
"type": "number",
"minimum": -360,
"maximum": 360,
"description": "Argument of latitude at t=0."
},
"ground_latitude_deg": {
"type": "number",
"minimum": -90,
"maximum": 90
},
"ground_longitude_deg": {
"type": "number",
"minimum": -180,
"maximum": 180
},
"duration_seconds": {
"type": "integer",
"minimum": 10,
"maximum": 172800
},
"step_seconds": {
"type": "integer",
"minimum": 10,
"maximum": 3600
},
"minimum_elevation_deg": {
"type": "number",
"minimum": -5,
"maximum": 90
}
}
}Veröffentlichtes Eingabebeispiel
{
"altitude_km": 550,
"inclination_deg": 53,
"raan_deg": 15,
"initial_phase_deg": 210,
"ground_latitude_deg": 52.52,
"ground_longitude_deg": 13.405,
"duration_seconds": 43200,
"step_seconds": 30,
"minimum_elevation_deg": 10
}Ergebnis & Dokumentation
Veröffentlichtes Ergebnisschema anzeigen
{
"$ref": "https://space.halowerk.com/v1/satellite-pass/schema#/outputSchema"
}Veröffentlichtes Ergebnisbeispiel öffnen
Maschinenlesbare Dokumentation dieses Hubs
Quelle dieser Seite: der veröffentlichte HALOWERK-Katalog. Stand: 2026-11-01, 15:19 UTC.
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