▸Orbital parameters

Orbit class	SSO
Inclination	97.7112°
Eccentricity	0.0010534
Period	95.9 min
Apogee	571 km
Perigee	557 km
Mean motion	15.00953042 rev/day
RAAN	135.8115°
Arg of perigee	310.6718°
Mean anomaly	49.3590°
B*	3.8750e-5
Rev at epoch	3,250

▸Two-line element set (TLE)

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

1 66820U 25279A 26187.41648678 .00000434 00000-0 38750-4 0 9993

2 66820 97.7112 135.8115 0010534 310.6718 49.3590 15.00953042 32503

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KOMPSAT-7",
  "OBJECT_ID": "2025-279A",
  "EPOCH": "2026-07-06T09:59:44.458+00:00",
  "MEAN_MOTION": 15.00953042,
  "ECCENTRICITY": 0.0010534,
  "INCLINATION": 97.7112,
  "RA_OF_ASC_NODE": 135.8115,
  "ARG_OF_PERICENTER": 310.6718,
  "MEAN_ANOMALY": 49.359,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66820,
  "REV_AT_EPOCH": 3250,
  "BSTAR": 0.00003875,
  "MEAN_MOTION_DOT": 0.00000434,
  "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	KOMPSAT-7
Operator	Korea Aerospace Research InstituteHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	South Korea
Launch date	Dec 1, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1800HIGHvia 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/66820

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