▸Orbital parameters

Orbit class	GEO
Inclination	0.0172°
Eccentricity	0.0001155
Period	1436.0 min
Apogee	35,790 km
Perigee	35,781 km
Mean motion	1.00275929 rev/day
RAAN	34.0663°
Arg of perigee	76.0069°
Mean anomaly	211.1687°
B*	0.0000e+0
Rev at epoch	3,831

▸Two-line element set (TLE)

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

1 41310U 16005A 26188.07552382 .00000077 00000-0 00000-0 0 9992

2 41310 0.0172 34.0663 0001155 76.0069 211.1687 1.00275929 38319

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EUTELSAT 9B",
  "OBJECT_ID": "2016-005A",
  "EPOCH": "2026-07-07T01:48:45.258+00:00",
  "MEAN_MOTION": 1.00275929,
  "ECCENTRICITY": 0.0001155,
  "INCLINATION": 0.0172,
  "RA_OF_ASC_NODE": 34.0663,
  "ARG_OF_PERICENTER": 76.0069,
  "MEAN_ANOMALY": 211.1687,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41310,
  "REV_AT_EPOCH": 3831,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 7.7e-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 9B
Operator	Eutelsat SAHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree EutelsatMEDIUMvia Wikidata
Country	France
Launch date	Jan 29, 2016HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5162HIGHvia 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/41310

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