▸Orbital parameters

Orbit class	SSO
Inclination	97.5669°
Eccentricity	0.0010816
Period	93.7 min
Apogee	462 km
Perigee	448 km
Mean motion	15.37007813 rev/day
RAAN	329.7997°
Arg of perigee	157.5588°
Mean anomaly	202.6131°
B*	2.0756e-4
Rev at epoch	13,032

▸Two-line element set (TLE)

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

1 59117U 24043V 26188.20989182 .00007442 00000-0 20756-3 0 9990

2 59117 97.5669 329.7997 0010816 157.5588 202.6131 15.37007813130327

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CONTECSAT-1",
  "OBJECT_ID": "2024-043V",
  "EPOCH": "2026-07-07T05:02:14.653+00:00",
  "MEAN_MOTION": 15.37007813,
  "ECCENTRICITY": 0.0010816,
  "INCLINATION": 97.5669,
  "RA_OF_ASC_NODE": 329.7997,
  "ARG_OF_PERICENTER": 157.5588,
  "MEAN_ANOMALY": 202.6131,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59117,
  "REV_AT_EPOCH": 13032,
  "BSTAR": 0.00020756,
  "MEAN_MOTION_DOT": 0.00007442,
  "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	CONTECSAT-1
Operator	CONTEC Corp.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	South Korea
Launch date	Mar 4, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	20HIGHvia 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/59117

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