▸Orbital parameters

Orbit class	GEO
Inclination	4.2653°
Eccentricity	0.0005964
Period	1436.1 min
Apogee	35,812 km
Perigee	35,762 km
Mean motion	1.00269637 rev/day
RAAN	76.2858°
Arg of perigee	31.3683°
Mean anomaly	313.1565°
B*	0.0000e+0
Rev at epoch	5,252

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 28924U 05052A 26187.89433683 .00000021 00000-0 00000-0 0 9998

2 28924 4.2653 76.2858 0005964 31.3683 313.1565 1.00269637 52523

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EUTELSAT 174A",
  "OBJECT_ID": "2005-052A",
  "EPOCH": "2026-07-06T21:27:50.702+00:00",
  "MEAN_MOTION": 1.00269637,
  "ECCENTRICITY": 0.0005964,
  "INCLINATION": 4.2653,
  "RA_OF_ASC_NODE": 76.2858,
  "ARG_OF_PERICENTER": 31.3683,
  "MEAN_ANOMALY": 313.1565,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 28924,
  "REV_AT_EPOCH": 5252,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 2.1e-7,
  "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	EUTELSAT 174A
Operator	SES AmericomHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree EutelsatMEDIUMvia Wikidata
Country	United StatesMEDIUMvia Wikidata
Launch date	Dec 29, 2005HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5035HIGH

▸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/28924

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