▸Orbital parameters

Orbit class	GEO
Inclination	0.0610°
Eccentricity	0.0002667
Period	1436.1 min
Apogee	35,797 km
Perigee	35,775 km
Mean motion	1.00273956 rev/day
RAAN	249.5756°
Arg of perigee	290.7794°
Mean anomaly	190.6585°
B*	0.0000e+0
Rev at epoch	4,133

▸Two-line element set (TLE)

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

1 38778U 12051A 26188.16017221 .00000165 00000-0 00000-0 0 9999

2 38778 0.0610 249.5756 0002667 290.7794 190.6585 1.00273956 41337

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASTRA 2F",
  "OBJECT_ID": "2012-051A",
  "EPOCH": "2026-07-07T03:50:38.879+00:00",
  "MEAN_MOTION": 1.00273956,
  "ECCENTRICITY": 0.0002667,
  "INCLINATION": 0.061,
  "RA_OF_ASC_NODE": 249.5756,
  "ARG_OF_PERICENTER": 290.7794,
  "MEAN_ANOMALY": 190.6585,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 38778,
  "REV_AT_EPOCH": 4133,
  "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 2F
Operator	SES S.A.HIGHvia GCAT — Jonathan McDowell's General Catalog SES S.A.MEDIUMvia Wikidata
Country	Luxembourg
Launch date	Sep 28, 2012HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5968HIGHvia 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/38778

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