GOKTURK 1A is a payload in SSO orbit, operated by Turkish Ministry of National Defense, launched 2016.
| Orbit class | SSO |
| Inclination | 98.1220° |
| Eccentricity | 0.0001414 |
| Period | 98.4 min |
| Apogee | 685 km |
| Perigee | 683 km |
| Mean motion | 14.62791004 rev/day |
| RAAN | 82.5104° |
| Arg of perigee | 78.1321° |
| Mean anomaly | 282.0039° |
| B* | 1.4083e-4 |
| Rev at epoch | 51,174 |
1 41875U 16073A 26188.15120551 .00000672 00000-0 14083-3 0 99912 41875 98.1220 82.5104 0001414 78.1321 282.0039 14.62791004511747{
"OBJECT_NAME": "GOKTURK 1A",
"OBJECT_ID": "2016-073A",
"EPOCH": "2026-07-07T03:37:44.156+00:00",
"MEAN_MOTION": 14.62791004,
"ECCENTRICITY": 0.0001414,
"INCLINATION": 98.122,
"RA_OF_ASC_NODE": 82.5104,
"ARG_OF_PERICENTER": 78.1321,
"MEAN_ANOMALY": 282.0039,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 41875,
"REV_AT_EPOCH": 51174,
"BSTAR": 0.00014083,
"MEAN_MOTION_DOT": 0.00000672,
"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.
| Name | GOKTURK 1A |
| Operator | Turkish Ministry of National DefenseHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | |
| Launch date | |
| Launch mass (kg) | 1060HIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |