▸Orbital parameters

Orbit class	SSO
Inclination	97.5095°
Eccentricity	0.0014828
Period	95.4 min
Apogee	549 km
Perigee	528 km
Mean motion	15.09203469 rev/day
RAAN	336.8890°
Arg of perigee	16.0736°
Mean anomaly	344.0960°
B*	4.8604e-4
Rev at epoch	1,127

▸Two-line element set (TLE)

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

1 68795U 26088D 26187.92340545 .00007686 00000-0 48604-3 0 9997

2 68795 97.5095 336.8890 0014828 16.0736 344.0960 15.09203469 11271

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ORIGAMISAT-2",
  "OBJECT_ID": "2026-088D",
  "EPOCH": "2026-07-06T22:09:42.231+00:00",
  "MEAN_MOTION": 15.09203469,
  "ECCENTRICITY": 0.0014828,
  "INCLINATION": 97.5095,
  "RA_OF_ASC_NODE": 336.889,
  "ARG_OF_PERICENTER": 16.0736,
  "MEAN_ANOMALY": 344.096,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68795,
  "REV_AT_EPOCH": 1127,
  "BSTAR": 0.00048604,
  "MEAN_MOTION_DOT": 0.00007686,
  "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	ORIGAMISAT-2
Operator	Science TokyoHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Tokyo Institute of TechnologyMEDIUMvia Wikidata
Country	JapanMEDIUMvia Wikidata
Launch date	Apr 23, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4HIGH

▸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/68795

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