▸Orbital parameters

Orbit class	SSO
Inclination	97.5461°
Eccentricity	0.0022129
Period	96.8 min
Apogee	619 km
Perigee	588 km
Mean motion	14.88179325 rev/day
RAAN	11.9983°
Arg of perigee	237.7306°
Mean anomaly	122.1768°
B*	2.3043e-4
Rev at epoch	65,177

▸Two-line element set (TLE)

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

1 40011U 14033B 26188.13857683 .00002081 00000-0 23043-3 0 9999

2 40011 97.5461 11.9983 0022129 237.7306 122.1768 14.88179325651776

▸ source OMM (JSON)

{
  "OBJECT_NAME": "HODOYOSHI-4",
  "OBJECT_ID": "2014-033B",
  "EPOCH": "2026-07-07T03:19:33.038+00:00",
  "MEAN_MOTION": 14.88179325,
  "ECCENTRICITY": 0.0022129,
  "INCLINATION": 97.5461,
  "RA_OF_ASC_NODE": 11.9983,
  "ARG_OF_PERICENTER": 237.7306,
  "MEAN_ANOMALY": 122.1768,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40011,
  "REV_AT_EPOCH": 65177,
  "BSTAR": 0.00023043,
  "MEAN_MOTION_DOT": 0.00002081,
  "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	HODOYOSHI-4
Operator	Tokyo UniversityHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Japan
Launch date	Jun 19, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	64HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/40011

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