▸Orbital parameters

Orbit class	GEO
Inclination	0.0223°
Eccentricity	0.0003124
Period	1436.1 min
Apogee	35,800 km
Perigee	35,774 km
Mean motion	1.00270321 rev/day
RAAN	21.2636°
Arg of perigee	98.7240°
Mean anomaly	292.1864°
B*	0.0000e+0
Rev at epoch	5,064

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 38356U 12030A 26187.89251683 .00000000 00000-0 00000-0 0 9997

2 38356 0.0223 21.2636 0003124 98.7240 292.1864 1.00270321 50647

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 19 (IS-19)",
  "OBJECT_ID": "2012-030A",
  "EPOCH": "2026-07-06T21:25:13.454+00:00",
  "MEAN_MOTION": 1.00270321,
  "ECCENTRICITY": 0.0003124,
  "INCLINATION": 0.0223,
  "RA_OF_ASC_NODE": 21.2636,
  "ARG_OF_PERICENTER": 98.724,
  "MEAN_ANOMALY": 292.1864,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 38356,
  "REV_AT_EPOCH": 5064,
  "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 19 (IS-19)
Operator	Intelsat S.A., US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	United States
Launch date	Jun 1, 2012HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5600HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/38356

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