▸Orbital parameters

Orbit class	SSO
Inclination	97.5097°
Eccentricity	0.0015378
Period	95.6 min
Apogee	556 km
Perigee	535 km
Mean motion	15.07001793 rev/day
RAAN	336.6436°
Arg of perigee	45.5872°
Mean anomaly	314.6612°
B*	2.2417e-4
Rev at epoch	1,125

▸Two-line element set (TLE)

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

1 68792U 26088A 26187.87454259 .00003303 00000-0 22417-3 0 9992

2 68792 97.5097 336.6436 0015378 45.5872 314.6612 15.07001793 11252

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FSI-SAT2",
  "OBJECT_ID": "2026-088A",
  "EPOCH": "2026-07-06T20:59:20.48+00:00",
  "MEAN_MOTION": 15.07001793,
  "ECCENTRICITY": 0.0015378,
  "INCLINATION": 97.5097,
  "RA_OF_ASC_NODE": 336.6436,
  "ARG_OF_PERICENTER": 45.5872,
  "MEAN_ANOMALY": 314.6612,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68792,
  "REV_AT_EPOCH": 1125,
  "BSTAR": 0.00022417,
  "MEAN_MOTION_DOT": 0.00003303,
  "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	FSI-SAT2
Operator	Future Science Institute / Happy Science UniversityHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	JapanMEDIUMvia Wikidata
Launch date	Apr 23, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1.4HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/68792

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