▸Orbital parameters

Orbit class	SSO
Inclination	97.3926°
Eccentricity	0.0007687
Period	94.5 min
Apogee	499 km
Perigee	488 km
Mean motion	15.24197275 rev/day
RAAN	80.4359°
Arg of perigee	84.1723°
Mean anomaly	276.0390°
B*	2.2260e-4
Rev at epoch	7,284

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 63232U 25052Y 26187.70004060 .00005356 00000-0 22260-3 0 9995

2 63232 97.3926 80.4359 0007687 84.1723 276.0390 15.24197275 72847

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SPHINX/FRAZIER",
  "OBJECT_ID": "2025-052Y",
  "EPOCH": "2026-07-06T16:48:03.508+00:00",
  "MEAN_MOTION": 15.24197275,
  "ECCENTRICITY": 0.0007687,
  "INCLINATION": 97.3926,
  "RA_OF_ASC_NODE": 80.4359,
  "ARG_OF_PERICENTER": 84.1723,
  "MEAN_ANOMALY": 276.039,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63232,
  "REV_AT_EPOCH": 7284,
  "BSTAR": 0.0002226,
  "MEAN_MOTION_DOT": 0.00005356,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	SPHINX/FRAZIER
Operator	Vestigo Aerospace / Astro DigitalHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Mar 15, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	32HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/63232

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.