▸Orbital parameters

Orbit class	SSO
Inclination	97.6438°
Eccentricity	0.0031380
Period	96.9 min
Apogee	634 km
Perigee	590 km
Mean motion	14.85426379 rev/day
RAAN	350.1708°
Arg of perigee	290.5000°
Mean anomaly	69.2849°
B*	9.9451e-5
Rev at epoch	65,055

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 40015U 14033F 26187.92234713 .00000811 00000-0 99451-4 0 9998

2 40015 97.6438 350.1708 0031380 290.5000 69.2849 14.85426379650552

▸ source OMM (JSON)

{
  "OBJECT_NAME": "HODOYOSHI-3",
  "OBJECT_ID": "2014-033F",
  "EPOCH": "2026-07-06T22:08:10.792+00:00",
  "MEAN_MOTION": 14.85426379,
  "ECCENTRICITY": 0.003138,
  "INCLINATION": 97.6438,
  "RA_OF_ASC_NODE": 350.1708,
  "ARG_OF_PERICENTER": 290.5,
  "MEAN_ANOMALY": 69.2849,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40015,
  "REV_AT_EPOCH": 65055,
  "BSTAR": 0.000099451,
  "MEAN_MOTION_DOT": 0.00000811,
  "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-3
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)	58HIGHvia 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/40015

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