▸Orbital parameters

Orbit class	GEO
Inclination	0.0094°
Eccentricity	0.0002215
Period	1436.1 min
Apogee	35,796 km
Perigee	35,778 km
Mean motion	1.00270153 rev/day
RAAN	10.1998°
Arg of perigee	332.1572°
Mean anomaly	68.3588°
B*	0.0000e+0
Rev at epoch	3,615

▸Two-line element set (TLE)

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

1 41747U 16053A 26188.15858126 -.00000009 00000-0 00000-0 0 9999

2 41747 0.0094 10.1998 0002215 332.1572 68.3588 1.00270153 36151

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 36 (IS-36)",
  "OBJECT_ID": "2016-053A",
  "EPOCH": "2026-07-07T03:48:21.421+00:00",
  "MEAN_MOTION": 1.00270153,
  "ECCENTRICITY": 0.0002215,
  "INCLINATION": 0.0094,
  "RA_OF_ASC_NODE": 10.1998,
  "ARG_OF_PERICENTER": 332.1572,
  "MEAN_ANOMALY": 68.3588,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41747,
  "REV_AT_EPOCH": 3615,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -9e-8,
  "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 36 (IS-36)
Operator	Intelsat S.A., US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	United States
Launch date	Aug 24, 2016HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3253HIGHvia 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/41747

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