▸Orbital parameters

Orbit class	GEO
Inclination	2.9984°
Eccentricity	0.0002433
Period	1436.1 min
Apogee	35,796 km
Perigee	35,776 km
Mean motion	1.00274018 rev/day
RAAN	1.1586°
Arg of perigee	126.5430°
Mean anomaly	210.5787°
B*	0.0000e+0
Rev at epoch	4,421

▸Two-line element set (TLE)

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

1 39215U 13038A 26188.07873050 .00000147 00000-0 00000-0 0 9992

2 39215 2.9984 1.1586 0002433 126.5430 210.5787 1.00274018 44212

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ALPHASAT",
  "OBJECT_ID": "2013-038A",
  "EPOCH": "2026-07-07T01:53:22.315+00:00",
  "MEAN_MOTION": 1.00274018,
  "ECCENTRICITY": 0.0002433,
  "INCLINATION": 2.9984,
  "RA_OF_ASC_NODE": 1.1586,
  "ARG_OF_PERICENTER": 126.543,
  "MEAN_ANOMALY": 210.5787,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39215,
  "REV_AT_EPOCH": 4421,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000147,
  "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	ALPHASAT
Operator	International Maritime Satellite Organization Ltd, / European Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree European Space AgencyMEDIUMvia Wikidata
Country	United Kingdom
Launch date	Jul 25, 2013HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	6650HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/39215

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