▸Orbital parameters

Orbit class	GEO
Inclination	0.0267°
Eccentricity	0.0001781
Period	1436.1 min
Apogee	35,795 km
Perigee	35,780 km
Mean motion	1.00269463 rev/day
RAAN	55.0939°
Arg of perigee	67.5931°
Mean anomaly	266.1382°
B*	0.0000e+0
Rev at epoch	738

▸Two-line element set (TLE)

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

1 38098U 12011A 26188.08800389 .00000000 00000-0 00000-0 0 9994

2 38098 0.0267 55.0939 0001781 67.5931 266.1382 1.00269463 7381

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 22 (IS-22)",
  "OBJECT_ID": "2012-011A",
  "EPOCH": "2026-07-07T02:06:43.536+00:00",
  "MEAN_MOTION": 1.00269463,
  "ECCENTRICITY": 0.0001781,
  "INCLINATION": 0.0267,
  "RA_OF_ASC_NODE": 55.0939,
  "ARG_OF_PERICENTER": 67.5931,
  "MEAN_ANOMALY": 266.1382,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 38098,
  "REV_AT_EPOCH": 738,
  "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 22 (IS-22)
Operator	Intelsat S.A., US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	United States
Launch date	Mar 25, 2012HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	6249HIGHvia 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/38098

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