▸Orbital parameters

Orbit class	GEO
Inclination	0.0640°
Eccentricity	0.0003936
Period	1436.1 min
Apogee	35,803 km
Perigee	35,770 km
Mean motion	1.00273561 rev/day
RAAN	340.8709°
Arg of perigee	128.4539°
Mean anomaly	231.3329°
B*	0.0000e+0
Rev at epoch	4,426

▸Two-line element set (TLE)

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

1 39773U 14030A 26188.14566787 .00000035 00000-0 00000-0 0 9994

2 39773 0.0640 340.8709 0003936 128.4539 231.3329 1.00273561 44269

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EUTELSAT 3B",
  "OBJECT_ID": "2014-030A",
  "EPOCH": "2026-07-07T03:29:45.704+00:00",
  "MEAN_MOTION": 1.00273561,
  "ECCENTRICITY": 0.0003936,
  "INCLINATION": 0.064,
  "RA_OF_ASC_NODE": 340.8709,
  "ARG_OF_PERICENTER": 128.4539,
  "MEAN_ANOMALY": 231.3329,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39773,
  "REV_AT_EPOCH": 4426,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 3.5e-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 3B
Operator	Eutelsat SAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	France
Launch date	May 26, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5967HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/39773

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