▸Orbital parameters

Orbit class	GEO
Inclination	0.0132°
Eccentricity	0.0000502
Period	1436.1 min
Apogee	35,788 km
Perigee	35,784 km
Mean motion	1.00273565 rev/day
RAAN	330.2943°
Arg of perigee	54.1290°
Mean anomaly	253.4592°
B*	0.0000e+0
Rev at epoch	3,983

▸Two-line element set (TLE)

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

1 40874U 15039A 26188.13405448 -.00000270 00000-0 00000-0 0 9995

2 40874 0.0132 330.2943 0000502 54.1290 253.4592 1.00273565 39835

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 34 (IS-34)",
  "OBJECT_ID": "2015-039A",
  "EPOCH": "2026-07-07T03:13:02.307+00:00",
  "MEAN_MOTION": 1.00273565,
  "ECCENTRICITY": 0.0000502,
  "INCLINATION": 0.0132,
  "RA_OF_ASC_NODE": 330.2943,
  "ARG_OF_PERICENTER": 54.129,
  "MEAN_ANOMALY": 253.4592,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40874,
  "REV_AT_EPOCH": 3983,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.0000027,
  "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 34 (IS-34)
Operator	Intelsat S.A., US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	United States
Launch date	Aug 20, 2015HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3300HIGHvia GCAT — Jonathan McDowell's General Catalog⚠

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/40874

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