▸Orbital parameters

Orbit class	GEO
Inclination	0.0166°
Eccentricity	0.0002353
Period	1436.1 min
Apogee	35,797 km
Perigee	35,778 km
Mean motion	1.00268892 rev/day
RAAN	47.5554°
Arg of perigee	96.4042°
Mean anomaly	70.1284°
B*	0.0000e+0
Rev at epoch	1,202

▸Two-line element set (TLE)

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

1 56174U 23052A 26188.05572243 .00000000 00000-0 00000-0 0 9998

2 56174 0.0166 47.5554 0002353 96.4042 70.1284 1.00268892 12029

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 40E (IS-40E)",
  "OBJECT_ID": "2023-052A",
  "EPOCH": "2026-07-07T01:20:14.418+00:00",
  "MEAN_MOTION": 1.00268892,
  "ECCENTRICITY": 0.0002353,
  "INCLINATION": 0.0166,
  "RA_OF_ASC_NODE": 47.5554,
  "ARG_OF_PERICENTER": 96.4042,
  "MEAN_ANOMALY": 70.1284,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 56174,
  "REV_AT_EPOCH": 1202,
  "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 40E (IS-40E)
Operator	Intelsat S.A., US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	United States
Launch date	Apr 7, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	6013HIGHvia 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/56174

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