▸Orbital parameters

Orbit class	SSO
Inclination	97.6343°
Eccentricity	0.0023051
Period	95.9 min
Apogee	580 km
Perigee	548 km
Mean motion	15.00944346 rev/day
RAAN	252.1437°
Arg of perigee	259.3265°
Mean anomaly	100.5363°
B*	1.4821e-4
Rev at epoch	14,228

▸Two-line element set (TLE)

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

1 58463U 23185B 26188.18811641 .00001838 00000-0 14821-3 0 9999

2 58463 97.6343 252.1437 0023051 259.3265 100.5363 15.00944346142288

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KORSAT-7",
  "OBJECT_ID": "2023-185B",
  "EPOCH": "2026-07-07T04:30:53.258+00:00",
  "MEAN_MOTION": 15.00944346,
  "ECCENTRICITY": 0.0023051,
  "INCLINATION": 97.6343,
  "RA_OF_ASC_NODE": 252.1437,
  "ARG_OF_PERICENTER": 259.3265,
  "MEAN_ANOMALY": 100.5363,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58463,
  "REV_AT_EPOCH": 14228,
  "BSTAR": 0.00014821,
  "MEAN_MOTION_DOT": 0.00001838,
  "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	KORSAT-7
Operator	Defense Acquisition Program AdministrationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Agency for Defense DevelopmentMEDIUMvia Wikidata
Country	South Korea
Launch date	Dec 1, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	800HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/58463

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