▸Orbital parameters

Orbit class	GEO
Inclination	0.0599°
Eccentricity	0.0002101
Period	1436.2 min
Apogee	35,797 km
Perigee	35,779 km
Mean motion	1.00266757 rev/day
RAAN	96.1578°
Arg of perigee	21.8031°
Mean anomaly	220.0480°
B*	0.0000e+0
Rev at epoch	1,322

▸Two-line element set (TLE)

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

1 54259U 22157A 26188.11919594 .00000083 00000-0 00000-0 0 9997

2 54259 0.0599 96.1578 0002101 21.8031 220.0480 1.00266757 13223

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EUTELSAT 10B",
  "OBJECT_ID": "2022-157A",
  "EPOCH": "2026-07-07T02:51:38.529+00:00",
  "MEAN_MOTION": 1.00266757,
  "ECCENTRICITY": 0.0002101,
  "INCLINATION": 0.0599,
  "RA_OF_ASC_NODE": 96.1578,
  "ARG_OF_PERICENTER": 21.8031,
  "MEAN_ANOMALY": 220.048,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54259,
  "REV_AT_EPOCH": 1322,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 8.3e-7,
  "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	EUTELSAT 10B
Operator	Eutelsat SAHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree EutelsatMEDIUMvia Wikidata
Country	France
Launch date	Nov 23, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4500HIGHvia 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/54259

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