▸Orbital parameters

Orbit class	GEO
Inclination	0.0280°
Eccentricity	0.0002201
Period	1436.1 min
Apogee	35,796 km
Perigee	35,777 km
Mean motion	1.00272739 rev/day
RAAN	82.5799°
Arg of perigee	356.1244°
Mean anomaly	328.2679°
B*	0.0000e+0
Rev at epoch	4,715

▸Two-line element set (TLE)

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

1 39237U 13045A 26188.15788794 .00000022 00000-0 00000-0 0 9995

2 39237 0.0280 82.5799 0002201 356.1244 328.2679 1.00272739 47151

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AMOS-4",
  "OBJECT_ID": "2013-045A",
  "EPOCH": "2026-07-07T03:47:21.518+00:00",
  "MEAN_MOTION": 1.00272739,
  "ECCENTRICITY": 0.0002201,
  "INCLINATION": 0.028,
  "RA_OF_ASC_NODE": 82.5799,
  "ARG_OF_PERICENTER": 356.1244,
  "MEAN_ANOMALY": 328.2679,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39237,
  "REV_AT_EPOCH": 4715,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 2.2e-7,
  "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	AMOS-4
Operator	IAI Space Communications Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree SpacecomMEDIUMvia Wikidata
Country	Israel
Launch date	Aug 31, 2013HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4260HIGHvia 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/39237

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