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 2026-10-23 10:20 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
Türksat
Country
Turkey
Manufacturer
Mitsubishi Electric
Launched
Oct 16, 2015
Mass
—
Apogee
35,803 km
Perigee
35,784 km
Inclination
0.01°
Period
23.93 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 148 days of archived orbital elements (150 element sets, one per day).
Trend
Decaying
Change
-1.1 km
Rate
-0.01 km/day
Now
35785 × 35803 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.
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