▸Orbital parameters

Orbit class	GEO
Inclination	0.0154°
Eccentricity	0.0001704
Period	1436.1 min
Apogee	35,794 km
Perigee	35,779 km
Mean motion	1.00271699 rev/day
RAAN	11.3752°
Arg of perigee	93.1241°
Mean anomaly	213.8363°
B*	0.0000e+0
Rev at epoch	3,301

▸Two-line element set (TLE)

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

1 42818U 17041A 26188.18794692 -.00000223 00000-0 00000-0 0 9995

2 42818 0.0154 11.3752 0001704 93.1241 213.8363 1.00271699 33014

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 35E (IS-35E)",
  "OBJECT_ID": "2017-041A",
  "EPOCH": "2026-07-07T04:30:38.614+00:00",
  "MEAN_MOTION": 1.00271699,
  "ECCENTRICITY": 0.0001704,
  "INCLINATION": 0.0154,
  "RA_OF_ASC_NODE": 11.3752,
  "ARG_OF_PERICENTER": 93.1241,
  "MEAN_ANOMALY": 213.8363,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 42818,
  "REV_AT_EPOCH": 3301,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000223,
  "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 35E (IS-35E)
Operator	Intelsat S.A., US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	United StatesMEDIUMvia Wikidata
Launch date	Jul 5, 2017HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	6761HIGH

▸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/42818

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