▸Orbital parameters

Orbit class	SSO
Inclination	97.9220°
Eccentricity	0.0001613
Period	97.3 min
Apogee	632 km
Perigee	630 km
Mean motion	14.79466478 rev/day
RAAN	285.1335°
Arg of perigee	97.9060°
Mean anomaly	262.2335°
B*	1.9955e-4
Rev at epoch	10,884

▸Two-line element set (TLE)

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

1 60182U 24123A 26188.24548714 .00001439 00000-0 19955-3 0 9998

2 60182 97.9220 285.1335 0001613 97.9060 262.2335 14.79466478108847

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ALOS-4 (DAICHI-4)",
  "OBJECT_ID": "2024-123A",
  "EPOCH": "2026-07-07T05:53:30.089+00:00",
  "MEAN_MOTION": 14.79466478,
  "ECCENTRICITY": 0.0001613,
  "INCLINATION": 97.922,
  "RA_OF_ASC_NODE": 285.1335,
  "ARG_OF_PERICENTER": 97.906,
  "MEAN_ANOMALY": 262.2335,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60182,
  "REV_AT_EPOCH": 10884,
  "BSTAR": 0.00019955,
  "MEAN_MOTION_DOT": 0.00001439,
  "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	ALOS-4 (DAICHI-4)
Operator	Japan Aerospace Exploration AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog Japan Aerospace Exploration AgencyMEDIUMvia Wikidata
Country	JapanMEDIUMvia Wikidata
Launch date	Jul 1, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2900HIGH

▸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/60182

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