▸Orbital parameters

Orbit class	GEO
Inclination	0.0433°
Eccentricity	0.0002774
Period	1436.1 min
Apogee	35,798 km
Perigee	35,775 km
Mean motion	1.00272390 rev/day
RAAN	192.7518°
Arg of perigee	324.9283°
Mean anomaly	225.1023°
B*	0.0000e+0
Rev at epoch	721

▸Two-line element set (TLE)

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

1 60233U 24127A 26188.15461182 .00000161 00000-0 00000-0 0 9991

2 60233 0.0433 192.7518 0002774 324.9283 225.1023 1.00272390 7219

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TURKSAT 6A",
  "OBJECT_ID": "2024-127A",
  "EPOCH": "2026-07-07T03:42:38.461+00:00",
  "MEAN_MOTION": 1.0027239,
  "ECCENTRICITY": 0.0002774,
  "INCLINATION": 0.0433,
  "RA_OF_ASC_NODE": 192.7518,
  "ARG_OF_PERICENTER": 324.9283,
  "MEAN_ANOMALY": 225.1023,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60233,
  "REV_AT_EPOCH": 721,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000161,
  "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	TURKSAT 6A
Operator	Turksat Satellite Comm. and Cable TV Operation ASHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree TürksatMEDIUMvia Wikidata
Country	TurkeyMEDIUMvia Wikidata
Launch date	Jul 8, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4250HIGH

▸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/60233

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