▸Orbital parameters

Orbit class	GEO
Inclination	0.0218°
Eccentricity	0.0002286
Period	1436.1 min
Apogee	35,797 km
Perigee	35,778 km
Mean motion	1.00269109 rev/day
RAAN	15.2338°
Arg of perigee	100.4611°
Mean anomaly	194.1442°
B*	0.0000e+0
Rev at epoch	6,080

▸Two-line element set (TLE)

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

1 36097U 09064A 26188.19350479 .00000000 00000-0 00000-0 0 9997

2 36097 0.0218 15.2338 0002286 100.4611 194.1442 1.00269109 60808

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 14 (IS-14)",
  "OBJECT_ID": "2009-064A",
  "EPOCH": "2026-07-07T04:38:38.814+00:00",
  "MEAN_MOTION": 1.00269109,
  "ECCENTRICITY": 0.0002286,
  "INCLINATION": 0.0218,
  "RA_OF_ASC_NODE": 15.2338,
  "ARG_OF_PERICENTER": 100.4611,
  "MEAN_ANOMALY": 194.1442,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 36097,
  "REV_AT_EPOCH": 6080,
  "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 14 (IS-14)
Operator	Intelsat Ltd, US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	United States
Launch date	Nov 23, 2009HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5663HIGHvia 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/36097

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