▸Orbital parameters

Orbit class	SSO
Inclination	97.4289°
Eccentricity	0.0014492
Period	95.5 min
Apogee	551 km
Perigee	531 km
Mean motion	15.08546522 rev/day
RAAN	307.3946°
Arg of perigee	122.1344°
Mean anomaly	238.1293°
B*	1.7813e-4
Rev at epoch	2,378

▸Two-line element set (TLE)

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

1 67614U 26019A 26187.87113059 .00002726 00000-0 17813-3 0 9990

2 67614 97.4289 307.3946 0014492 122.1344 238.1293 15.08546522 23780

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NEONSAT-1A",
  "OBJECT_ID": "2026-019A",
  "EPOCH": "2026-07-06T20:54:25.683+00:00",
  "MEAN_MOTION": 15.08546522,
  "ECCENTRICITY": 0.0014492,
  "INCLINATION": 97.4289,
  "RA_OF_ASC_NODE": 307.3946,
  "ARG_OF_PERICENTER": 122.1344,
  "MEAN_ANOMALY": 238.1293,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67614,
  "REV_AT_EPOCH": 2378,
  "BSTAR": 0.00017813,
  "MEAN_MOTION_DOT": 0.00002726,
  "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	NEONSAT-1A
Operator	Korea Advanced Institute for Space TechnologyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree KAISTMEDIUMvia Wikidata
Country	South KoreaMEDIUMvia Wikidata
Launch date	Jan 30, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	100HIGH

▸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/67614

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