TURKSAT 4B
Launch
Launched on Oct 16, 2015 from 200/39 (200L), Kazakhstan aboard a Proton-M Briz-M.
Proton-M/Briz-M | Türksat 4B →
Live · TLE epoch 2026-09-08 10:55 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
Türksat
Country
Turkey
Manufacturer
Mitsubishi Electric
Launched
Oct 16, 2015
Mass
—
Apogee
35,804 km
Perigee
35,785 km
Inclination
0.04°
Period
23.94 h
Summary from Wikipedia (CC-BY-SA 4.0)
Türksat 4B is a Turkish communications satellite, operated by Türksat.
Full article on Wikipedia →Altitude history
Apogee and perigee for TURKSAT 4B across 103 days of archived orbital elements (105 element sets, one per day).
Trend
Stable
Change
-0.4 km
Rate
-0.00 km/day
Now
35785 × 35804 km
Apogee Perigee
Derived from our own archive of CelesTrak orbital elements, sampled every 3 hours. Short windows show drag and station-keeping; they are not a reentry prediction.
Related satellites
Sources & further reading
Embed this satellite on your site
Free for editorial use. Attribution back to LowEarth is required.
<iframe src="https://lowearth.app/embed/40984" width="640" height="400" frameborder="0" allow="fullscreen"></iframe>