▸Orbital parameters

Orbit class	SSO
Inclination	97.6815°
Eccentricity	0.0000936
Period	97.6 min
Apogee	644 km
Perigee	643 km
Mean motion	14.75562757 rev/day
RAAN	24.5829°
Arg of perigee	71.5727°
Mean anomaly	288.5584°
B*	3.3015e-5
Rev at epoch	72,745

▸Two-line element set (TLE)

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

1 39030U 12073A 26188.15331618 .00000178 00000-0 33015-4 0 9993

2 39030 97.6815 24.5829 0000936 71.5727 288.5584 14.75562757727454

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GOKTURK 2",
  "OBJECT_ID": "2012-073A",
  "EPOCH": "2026-07-07T03:40:46.518+00:00",
  "MEAN_MOTION": 14.75562757,
  "ECCENTRICITY": 0.0000936,
  "INCLINATION": 97.6815,
  "RA_OF_ASC_NODE": 24.5829,
  "ARG_OF_PERICENTER": 71.5727,
  "MEAN_ANOMALY": 288.5584,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39030,
  "REV_AT_EPOCH": 72745,
  "BSTAR": 0.000033015,
  "MEAN_MOTION_DOT": 0.00000178,
  "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	GOKTURK 2
Operator	Turkish Ministry of National DefenseHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Ministry of National DefenseMEDIUMvia Wikidata
Country	TurkeyMEDIUMvia Wikidata
Launch date	Dec 18, 2012HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	450HIGH

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/39030

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