▸Orbital parameters

Orbit class	SSO
Inclination	97.6863°
Eccentricity	0.0004052
Period	96.2 min
Apogee	577 km
Perigee	572 km
Mean motion	14.97507546 rev/day
RAAN	80.0032°
Arg of perigee	119.8823°
Mean anomaly	240.2802°
B*	2.6433e-4
Rev at epoch	7,165

▸Two-line element set (TLE)

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

1 63247U 25052AP 26188.16022851 .00003024 00000-0 26433-3 0 9996

2 63247 97.6863 80.0032 0004052 119.8823 240.2802 14.97507546 71654

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EZIE-A",
  "OBJECT_ID": "2025-052AP",
  "EPOCH": "2026-07-07T03:50:43.743+00:00",
  "MEAN_MOTION": 14.97507546,
  "ECCENTRICITY": 0.0004052,
  "INCLINATION": 97.6863,
  "RA_OF_ASC_NODE": 80.0032,
  "ARG_OF_PERICENTER": 119.8823,
  "MEAN_ANOMALY": 240.2802,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63247,
  "REV_AT_EPOCH": 7165,
  "BSTAR": 0.00026433,
  "MEAN_MOTION_DOT": 0.00003024,
  "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	EZIE-A
Operator	JHU-Applied Physics Lab / Jet Propulsion LabHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree The Johns Hopkins University Applied Physics Laboratory LLCMEDIUMvia Wikidata
Country	United StatesMEDIUMvia Wikidata
Launch date	Mar 15, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/63247

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