▸Orbital parameters

Orbit class	GEO
Inclination	0.0605°
Eccentricity	0.0004059
Period	1436.1 min
Apogee	35,804 km
Perigee	35,770 km
Mean motion	1.00269551 rev/day
RAAN	12.3708°
Arg of perigee	125.7834°
Mean anomaly	183.0638°
B*	0.0000e+0
Rev at epoch	4,420

▸Two-line element set (TLE)

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

1 37258U 10069A 26188.07552382 .00000076 00000-0 00000-0 0 9991

2 37258 0.0605 12.3708 0004059 125.7834 183.0638 1.00269551 44205

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EUTELSAT KA-SAT 9A",
  "OBJECT_ID": "2010-069A",
  "EPOCH": "2026-07-07T01:48:45.258+00:00",
  "MEAN_MOTION": 1.00269551,
  "ECCENTRICITY": 0.0004059,
  "INCLINATION": 0.0605,
  "RA_OF_ASC_NODE": 12.3708,
  "ARG_OF_PERICENTER": 125.7834,
  "MEAN_ANOMALY": 183.0638,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 37258,
  "REV_AT_EPOCH": 4420,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 7.6e-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 KA-SAT 9A
Operator	Eutelsat SAHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree EutelsatMEDIUMvia Wikidata
Country	France
Launch date	Dec 26, 2010HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5800HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/37258

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