▸Orbital parameters

Orbit class	GEO
Inclination	0.0176°
Eccentricity	0.0002278
Period	1436.1 min
Apogee	35,796 km
Perigee	35,777 km
Mean motion	1.00271377 rev/day
RAAN	24.3334°
Arg of perigee	86.4837°
Mean anomaly	317.7435°
B*	0.0000e+0
Rev at epoch	4,142

▸Two-line element set (TLE)

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

1 36106U 09067A 26188.16187463 -.00000170 00000-0 00000-0 0 9998

2 36106 0.0176 24.3334 0002278 86.4837 317.7435 1.00271377 41425

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 15 (IS-15)",
  "OBJECT_ID": "2009-067A",
  "EPOCH": "2026-07-07T03:53:05.968+00:00",
  "MEAN_MOTION": 1.00271377,
  "ECCENTRICITY": 0.0002278,
  "INCLINATION": 0.0176,
  "RA_OF_ASC_NODE": 24.3334,
  "ARG_OF_PERICENTER": 86.4837,
  "MEAN_ANOMALY": 317.7435,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 36106,
  "REV_AT_EPOCH": 4142,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.0000017,
  "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 15 (IS-15)
Operator	Intelsat Ltd, US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	United StatesMEDIUMvia Wikidata
Launch date	Nov 30, 2009HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2484HIGH

▸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/36106

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