▸Orbital parameters

Orbit class	GEO
Inclination	0.0170°
Eccentricity	0.0001290
Period	1436.1 min
Apogee	35,793 km
Perigee	35,782 km
Mean motion	1.00269059 rev/day
RAAN	300.9294°
Arg of perigee	247.7332°
Mean anomaly	237.4945°
B*	0.0000e+0
Rev at epoch	4,174

▸Two-line element set (TLE)

EPOCH Jul 5, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 40277U 14064A 26186.24975387 .00000112 00000-0 00000-0 0 9997

2 40277 0.0170 300.9294 0001290 247.7332 237.4945 1.00269059 41749

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EUTELSAT 53A",
  "OBJECT_ID": "2014-064A",
  "EPOCH": "2026-07-05T05:59:38.734+00:00",
  "MEAN_MOTION": 1.00269059,
  "ECCENTRICITY": 0.000129,
  "INCLINATION": 0.017,
  "RA_OF_ASC_NODE": 300.9294,
  "ARG_OF_PERICENTER": 247.7332,
  "MEAN_ANOMALY": 237.4945,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40277,
  "REV_AT_EPOCH": 4174,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000112,
  "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 53A
Operator	Russian Satellite Communications Co.HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Russian Satellite Communications CompanyMEDIUMvia Wikidata
Country	RussiaMEDIUMvia Wikidata
Launch date	Oct 21, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3361

▸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/40277

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