▸Orbital parameters

Orbit class	GEO
Inclination	1.1576°
Eccentricity	0.0001885
Period	1436.1 min
Apogee	35,795 km
Perigee	35,779 km
Mean motion	1.00270389 rev/day
RAAN	84.0164°
Arg of perigee	17.1319°
Mean anomaly	326.1993°
B*	0.0000e+0
Rev at epoch	7,396

▸Two-line element set (TLE)

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

1 29045U 06010A 26188.02861977 -.00000313 00000-0 00000-0 0 9990

2 29045 1.1576 84.0164 0001885 17.1319 326.1993 1.00270389 73967

▸ source OMM (JSON)

{
  "OBJECT_NAME": "JCSAT-5A",
  "OBJECT_ID": "2006-010A",
  "EPOCH": "2026-07-07T00:41:12.748+00:00",
  "MEAN_MOTION": 1.00270389,
  "ECCENTRICITY": 0.0001885,
  "INCLINATION": 1.1576,
  "RA_OF_ASC_NODE": 84.0164,
  "ARG_OF_PERICENTER": 17.1319,
  "MEAN_ANOMALY": 326.1993,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 29045,
  "REV_AT_EPOCH": 7396,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000313,
  "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-5A
Operator	Japan Satellite Systems IncHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree SKY Perfect JSAT HoldingsMEDIUMvia Wikidata
Country	Japan
Launch date	Apr 12, 2006HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4401HIGHvia GCAT — Jonathan McDowell's General Catalog

▸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/29045

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