▸Orbital parameters

Orbit class	GEO
Inclination	0.0345°
Eccentricity	0.0002570
Period	1436.1 min
Apogee	35,797 km
Perigee	35,776 km
Mean motion	1.00272422 rev/day
RAAN	283.6944°
Arg of perigee	195.4077°
Mean anomaly	303.9221°
B*	0.0000e+0
Rev at epoch	4,793

▸Two-line element set (TLE)

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

1 29272U 06033A 26188.02783977 -.00000330 00000-0 00000-0 0 9999

2 29272 0.0345 283.6944 0002570 195.4077 303.9221 1.00272422 47932

▸ source OMM (JSON)

{
  "OBJECT_NAME": "JCSAT-3A",
  "OBJECT_ID": "2006-033A",
  "EPOCH": "2026-07-07T00:40:05.356+00:00",
  "MEAN_MOTION": 1.00272422,
  "ECCENTRICITY": 0.000257,
  "INCLINATION": 0.0345,
  "RA_OF_ASC_NODE": 283.6944,
  "ARG_OF_PERICENTER": 195.4077,
  "MEAN_ANOMALY": 303.9221,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 29272,
  "REV_AT_EPOCH": 4793,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.0000033,
  "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	JCSAT-3A
Operator	Japan Satellite Systems IncHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	JapanMEDIUMvia Wikidata
Launch date	Aug 11, 2006HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4048HIGHvia 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/29272

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