▸Orbital parameters

Orbit class	GEO
Inclination	0.0332°
Eccentricity	0.0001929
Period	1436.1 min
Apogee	35,795 km
Perigee	35,779 km
Mean motion	1.00269770 rev/day
RAAN	294.0570°
Arg of perigee	189.9889°
Mean anomaly	284.5290°
B*	0.0000e+0
Rev at epoch	514

▸Two-line element set (TLE)

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

1 62876U 25023A 26188.09164389 -.00000218 00000-0 00000-0 0 9998

2 62876 0.0332 294.0570 0001929 189.9889 284.5290 1.00269770 5141

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QZS-6 (MICHIBIKI-6)",
  "OBJECT_ID": "2025-023A",
  "EPOCH": "2026-07-07T02:11:58.032+00:00",
  "MEAN_MOTION": 1.0026977,
  "ECCENTRICITY": 0.0001929,
  "INCLINATION": 0.0332,
  "RA_OF_ASC_NODE": 294.057,
  "ARG_OF_PERICENTER": 189.9889,
  "MEAN_ANOMALY": 284.529,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62876,
  "REV_AT_EPOCH": 514,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000218,
  "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	QZS-6 (MICHIBIKI-6)
Operator	Cabinet Space Strategy Office / Japan Aerospace Exploration AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Japan Aerospace Exploration AgencyMEDIUMvia Wikidata
Country	JapanMEDIUMvia Wikidata
Launch date	Feb 2, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4900

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/62876

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