▸Orbital parameters

Orbit class	GEO
Inclination	0.0197°
Eccentricity	0.0000902
Period	1436.1 min
Apogee	35,791 km
Perigee	35,784 km
Mean motion	1.00268632 rev/day
RAAN	19.9142°
Arg of perigee	303.4172°
Mean anomaly	80.3703°
B*	0.0000e+0
Rev at epoch	2,532

▸Two-line element set (TLE)

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

1 44476U 19049B 26188.15728126 .00000000 00000-0 00000-0 0 9995

2 44476 0.0197 19.9142 0000902 303.4172 80.3703 1.00268632 25322

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 39 (IS-39)",
  "OBJECT_ID": "2019-049B",
  "EPOCH": "2026-07-07T03:46:29.101+00:00",
  "MEAN_MOTION": 1.00268632,
  "ECCENTRICITY": 0.0000902,
  "INCLINATION": 0.0197,
  "RA_OF_ASC_NODE": 19.9142,
  "ARG_OF_PERICENTER": 303.4172,
  "MEAN_ANOMALY": 80.3703,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 44476,
  "REV_AT_EPOCH": 2532,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0,
  "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	INTELSAT 39 (IS-39)
Operator	Intelsat S.A., US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	United States
Launch date	Aug 6, 2019HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	6600HIGHvia 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/44476

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