▸Orbital parameters

Orbit class	GEO
Inclination	0.0159°
Eccentricity	0.0000038
Period	1436.1 min
Apogee	35,787 km
Perigee	35,786 km
Mean motion	1.00272756 rev/day
RAAN	64.4321°
Arg of perigee	187.9219°
Mean anomaly	132.7279°
B*	0.0000e+0
Rev at epoch	437

▸Two-line element set (TLE)

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

1 62483U 25001A 26188.15461182 .00000154 00000-0 00000-0 0 9994

2 62483 0.0159 64.4321 0000038 187.9219 132.7279 1.00272756 4373

▸ source OMM (JSON)

{
  "OBJECT_NAME": "THURAYA-4",
  "OBJECT_ID": "2025-001A",
  "EPOCH": "2026-07-07T03:42:38.461+00:00",
  "MEAN_MOTION": 1.00272756,
  "ECCENTRICITY": 0.0000038,
  "INCLINATION": 0.0159,
  "RA_OF_ASC_NODE": 64.4321,
  "ARG_OF_PERICENTER": 187.9219,
  "MEAN_ANOMALY": 132.7279,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62483,
  "REV_AT_EPOCH": 437,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000154,
  "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-4
Operator	Space42 Plc / Thuraya SatelliteHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Space42MEDIUMvia Wikidata
Country	United Arab EmiratesMEDIUMvia Wikidata
Launch date	Jan 4, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5000HIGH

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/62483

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