▸Orbital parameters

Orbit class	GEO
Inclination	0.0098°
Eccentricity	0.0001622
Period	1436.1 min
Apogee	35,794 km
Perigee	35,780 km
Mean motion	1.00270818 rev/day
RAAN	22.5735°
Arg of perigee	26.6946°
Mean anomaly	164.8256°
B*	0.0000e+0
Rev at epoch	1,334

▸Two-line element set (TLE)

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

1 54244U 22153B 26188.05572243 -.00000159 00000-0 00000-0 0 9991

2 54244 0.0098 22.5735 0001622 26.6946 164.8256 1.00270818 13346

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GALAXY 32 (G-32)",
  "OBJECT_ID": "2022-153B",
  "EPOCH": "2026-07-07T01:20:14.418+00:00",
  "MEAN_MOTION": 1.00270818,
  "ECCENTRICITY": 0.0001622,
  "INCLINATION": 0.0098,
  "RA_OF_ASC_NODE": 22.5735,
  "ARG_OF_PERICENTER": 26.6946,
  "MEAN_ANOMALY": 164.8256,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54244,
  "REV_AT_EPOCH": 1334,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000159,
  "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	GALAXY 32 (G-32)
Operator	Intelsat S.A., US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	United States
Launch date	Nov 12, 2022HIGHvia 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/54244

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