{ "$schema": "https://json-schema.org/draft/2020-12/schema", "$id": "https://raw.githubusercontent.com/api-evangelist/us-space-comman/main/json-schema/us-space-command-gp-schema.json", "title": "USSPACECOM General Perturbations (GP) Orbital Element Set", "description": "JSON Schema for a space object's orbital element set from Space-Track.org.", "type": "object", "properties": { "NORAD_CAT_ID": { "type": "integer", "description": "NORAD catalog number uniquely identifying the space object" }, "OBJECT_NAME": { "type": "string", "description": "Common name of the space object" }, "OBJECT_ID": { "type": "string", "description": "International designator (YYYY-NNNPPP format)" }, "OBJECT_TYPE": { "type": "string", "enum": ["PAYLOAD", "ROCKET BODY", "DEBRIS", "UNKNOWN", "TBA - TO BE ASSIGNED"], "description": "Classification of the space object" }, "CLASSIFICATION_TYPE": { "type": "string", "enum": ["U"], "description": "Data classification (U = Unclassified)" }, "EPOCH": { "type": "string", "format": "date-time", "description": "Epoch of the orbital elements" }, "MEAN_MOTION": { "type": "number", "description": "Mean motion in revolutions per day" }, "ECCENTRICITY": { "type": "number", "minimum": 0, "maximum": 1, "description": "Orbital eccentricity" }, "INCLINATION": { "type": "number", "minimum": 0, "maximum": 180, "description": "Orbital inclination in degrees" }, "RA_OF_ASC_NODE": { "type": "number", "minimum": 0, "maximum": 360, "description": "Right ascension of the ascending node in degrees" }, "ARG_OF_PERICENTER": { "type": "number", "minimum": 0, "maximum": 360, "description": "Argument of perigee in degrees" }, "MEAN_ANOMALY": { "type": "number", "minimum": 0, "maximum": 360, "description": "Mean anomaly in degrees" }, "BSTAR": { "type": "number", "description": "BSTAR drag term (1/Earth radii)" }, "APOGEE": { "type": "number", "description": "Apogee altitude above Earth surface in km" }, "PERIGEE": { "type": "number", "description": "Perigee altitude above Earth surface in km" }, "PERIOD": { "type": "number", "description": "Orbital period in minutes" }, "COUNTRY_CODE": { "type": "string", "description": "ISO 3-letter country code of the launching entity" }, "LAUNCH_DATE": { "type": ["string", "null"], "format": "date", "description": "Launch date" }, "DECAY_DATE": { "type": ["string", "null"], "format": "date", "description": "Reentry/decay date (null if still in orbit)" } }, "required": ["NORAD_CAT_ID", "OBJECT_NAME", "EPOCH", "INCLINATION", "ECCENTRICITY"] }