▸Orbital parameters

Orbit class	GEO
Inclination	6.0210°
Eccentricity	0.0002096
Period	1436.2 min
Apogee	35,797 km
Perigee	35,779 km
Mean motion	1.00266478 rev/day
RAAN	35.8077°
Arg of perigee	76.0926°
Mean anomaly	267.9525°
B*	0.0000e+0
Rev at epoch	6,768

▸Two-line element set (TLE)

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

1 32404U 08001A 26188.08635720 .00000022 00000-0 00000-0 0 9992

2 32404 6.0210 35.8077 0002096 76.0926 267.9525 1.00266478 67688

▸ source OMM (JSON)

{
  "OBJECT_NAME": "THURAYA-3",
  "OBJECT_ID": "2008-001A",
  "EPOCH": "2026-07-07T02:04:21.262+00:00",
  "MEAN_MOTION": 1.00266478,
  "ECCENTRICITY": 0.0002096,
  "INCLINATION": 6.021,
  "RA_OF_ASC_NODE": 35.8077,
  "ARG_OF_PERICENTER": 76.0926,
  "MEAN_ANOMALY": 267.9525,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 32404,
  "REV_AT_EPOCH": 6768,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 2.2e-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	THURAYA-3
Operator	Thuraya SatelliteHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Arab Emirates
Launch date	Jan 15, 2008HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5180HIGHvia 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/32404

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