▸Orbital parameters

Orbit class	MEO
Inclination	55.1299°
Eccentricity	0.0001025
Period	844.7 min
Apogee	23,225 km
Perigee	23,219 km
Mean motion	1.70473925 rev/day
RAAN	100.5421°
Arg of perigee	304.6843°
Mean anomaly	233.1982°
B*	0.0000e+0
Rev at epoch	1,364

▸Two-line element set (TLE)

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

1 59598U 24079A 26187.46658044 -.00000001 00000-0 00000-0 0 9991

2 59598 55.1299 100.5421 0001025 304.6843 233.1982 1.70473925 13648

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GSAT0225 (GALILEO 29)",
  "OBJECT_ID": "2024-079A",
  "EPOCH": "2026-07-06T11:11:52.55+00:00",
  "MEAN_MOTION": 1.70473925,
  "ECCENTRICITY": 0.00010247,
  "INCLINATION": 55.1299,
  "RA_OF_ASC_NODE": 100.5421,
  "ARG_OF_PERICENTER": 304.6843,
  "MEAN_ANOMALY": 233.1982,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59598,
  "REV_AT_EPOCH": 1364,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -1e-8,
  "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	GSAT0225 (GALILEO 29)
Operator	EU Agency for the Space ProgrammeHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree European Union Agency for the Space ProgrammeMEDIUMvia Wikidata
Country	European Union
Launch date	Apr 28, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	733HIGHvia GCAT — Jonathan McDowell's General Catalog

▸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/59598

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