▸Orbital parameters

Orbit class	SSO
Inclination	97.3483°
Eccentricity	0.0006870
Period	93.6 min
Apogee	454 km
Perigee	444 km
Mean motion	15.39084664 rev/day
RAAN	272.2401°
Arg of perigee	327.5753°
Mean anomaly	32.5070°
B*	2.7706e-4
Rev at epoch	12,280

▸Two-line element set (TLE)

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

1 59587U 24077A 26188.17148661 .00010655 00000-0 27706-3 0 9995

2 59587 97.3483 272.2401 0006870 327.5753 32.5070 15.39084664122807

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NEONSAT-1",
  "OBJECT_ID": "2024-077A",
  "EPOCH": "2026-07-07T04:06:56.443+00:00",
  "MEAN_MOTION": 15.39084664,
  "ECCENTRICITY": 0.000687,
  "INCLINATION": 97.3483,
  "RA_OF_ASC_NODE": 272.2401,
  "ARG_OF_PERICENTER": 327.5753,
  "MEAN_ANOMALY": 32.507,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59587,
  "REV_AT_EPOCH": 12280,
  "BSTAR": 0.00027706,
  "MEAN_MOTION_DOT": 0.00010655,
  "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-1
Operator	Korea Advanced Institute for Space TechnologyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree KAISTMEDIUMvia Wikidata
Country	South KoreaMEDIUMvia Wikidata
Launch date	Apr 23, 2024HIGHvia 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/59587

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