▸Orbital parameters

Orbit class	GEO
Inclination	0.0680°
Eccentricity	0.0002542
Period	1436.1 min
Apogee	35,798 km
Perigee	35,776 km
Mean motion	1.00269844 rev/day
RAAN	322.3463°
Arg of perigee	151.8830°
Mean anomaly	257.0543°
B*	0.0000e+0
Rev at epoch	4,661

▸Two-line element set (TLE)

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

1 39285U 13056A 26188.16017221 .00000165 00000-0 00000-0 0 9999

2 39285 0.0680 322.3463 0002542 151.8830 257.0543 1.00269844 46612

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASTRA 2E",
  "OBJECT_ID": "2013-056A",
  "EPOCH": "2026-07-07T03:50:38.879+00:00",
  "MEAN_MOTION": 1.00269844,
  "ECCENTRICITY": 0.0002542,
  "INCLINATION": 0.068,
  "RA_OF_ASC_NODE": 322.3463,
  "ARG_OF_PERICENTER": 151.883,
  "MEAN_ANOMALY": 257.0543,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39285,
  "REV_AT_EPOCH": 4661,
  "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 2E
Operator	SES S.A.HIGHvia GCAT — Jonathan McDowell's General Catalog SES S.A.MEDIUMvia Wikidata
Country	Luxembourg
Launch date	Sep 29, 2013HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	6052HIGHvia 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/39285

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