▸Orbital parameters

Orbit class	GEO
Inclination	0.0686°
Eccentricity	0.0001931
Period	1436.1 min
Apogee	35,795 km
Perigee	35,779 km
Mean motion	1.00270689 rev/day
RAAN	307.9755°
Arg of perigee	160.4725°
Mean anomaly	259.8469°
B*	0.0000e+0
Rev at epoch	4,486

▸Two-line element set (TLE)

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

1 39617U 14011B 26188.16572669 .00000152 00000-0 00000-0 0 9998

2 39617 0.0686 307.9755 0001931 160.4725 259.8469 1.00270689 44861

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASTRA 5B",
  "OBJECT_ID": "2014-011B",
  "EPOCH": "2026-07-07T03:58:38.786+00:00",
  "MEAN_MOTION": 1.00270689,
  "ECCENTRICITY": 0.0001931,
  "INCLINATION": 0.0686,
  "RA_OF_ASC_NODE": 307.9755,
  "ARG_OF_PERICENTER": 160.4725,
  "MEAN_ANOMALY": 259.8469,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39617,
  "REV_AT_EPOCH": 4486,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000152,
  "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 5B
Operator	SES S.A.HIGHvia GCAT — Jonathan McDowell's General Catalog SES S.A.MEDIUMvia Wikidata
Country	Luxembourg
Launch date	Mar 22, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5724HIGHvia 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/39617

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