▸Orbital parameters

Orbit class	GEO
Inclination	0.0456°
Eccentricity	0.0004590
Period	1436.1 min
Apogee	35,806 km
Perigee	35,767 km
Mean motion	1.00271767 rev/day
RAAN	3.2755°
Arg of perigee	72.4137°
Mean anomaly	295.2984°
B*	0.0000e+0
Rev at epoch	4,216

▸Two-line element set (TLE)

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

1 40364U 14089A 26188.16017221 .00000165 00000-0 00000-0 0 9996

2 40364 0.0456 3.2755 0004590 72.4137 295.2984 1.00271767 42161

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASTRA 2G",
  "OBJECT_ID": "2014-089A",
  "EPOCH": "2026-07-07T03:50:38.879+00:00",
  "MEAN_MOTION": 1.00271767,
  "ECCENTRICITY": 0.000459,
  "INCLINATION": 0.0456,
  "RA_OF_ASC_NODE": 3.2755,
  "ARG_OF_PERICENTER": 72.4137,
  "MEAN_ANOMALY": 295.2984,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40364,
  "REV_AT_EPOCH": 4216,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000165,
  "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	ASTRA 2G
Operator	SES S.A.HIGHvia GCAT — Jonathan McDowell's General Catalog SES S.A.MEDIUMvia Wikidata
Country	Luxembourg
Launch date	Dec 27, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	6002HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/40364

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