▸Orbital parameters

Orbit class	LEO
Inclination	45.4112°
Eccentricity	0.0003569
Period	96.1 min
Apogee	573 km
Perigee	568 km
Mean motion	14.98823585 rev/day
RAAN	328.2565°
Arg of perigee	305.3003°
Mean anomaly	54.7541°
B*	3.4436e-4
Rev at epoch	8,444

▸Two-line element set (TLE)

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

1 62377U 24247A 26187.39189174 .00003989 00000-0 34436-3 0 9992

2 62377 45.4112 328.2565 0003569 305.3003 54.7541 14.98823585 84441

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KORSAT-2",
  "OBJECT_ID": "2024-247A",
  "EPOCH": "2026-07-06T09:24:19.446+00:00",
  "MEAN_MOTION": 14.98823585,
  "ECCENTRICITY": 0.00035686,
  "INCLINATION": 45.4112,
  "RA_OF_ASC_NODE": 328.2565,
  "ARG_OF_PERICENTER": 305.3003,
  "MEAN_ANOMALY": 54.7541,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62377,
  "REV_AT_EPOCH": 8444,
  "BSTAR": 0.00034436495,
  "MEAN_MOTION_DOT": 0.00003989,
  "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-2
Operator	Defense Acquisition Program AdministrationHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	South Korea
Launch date	Dec 21, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	800HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/62377

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