TURKSAT 4A, 39522
Orbit data source: Space-Track
TURKSAT 4A, 39522 is a payload satellite owned by Turksat (TR) in GEO that was launched on Fri, 14 Feb 2014 UTC via a PROTON-M/BRIZ-M launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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39522 intel report (Beta)
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Identifier
Orbit
Country
TR / TURKRelated business
Manufacturer
MELCO
Mission
Operational Civil Communications
Bus & Motor
DS-2000, R-4D-11-164
Mass
4,850 kg wet, ~2,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 15.8 m
Radar Cross Section
59.064 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 TURKSAT 4A
1 39522U 14007A 26171.18649036 .00000141 00000-0 00000+0 0 9992
2 39522 0.0668 288.2837 0001004 16.0389 73.2267 1.00267919 44991Epoch: 2026-06-20T04:28Z
TLE epoch observation values (Epoch: 2026-06-20T04:28:32.767Z)
Latitude
0.07064°
Longitude
42.03142°
Altitude
35,785.954 km
Speed
3.075 km/s
True Right ascension
01h 10m 17s
True Declination
0° 04' 14"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:09:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,792.983 km
Perigee altitude
35,784.516 km
Semi-major axis
42,166.886 km
Eccentricity
0.0001
Inclination
0.0668°
RAAN
288.2837°
Arg. of periapsis
16.0389°
True anomaly
73.23772°
Mean anomaly
73.2267°
Eccentric anomaly
73.23221°
Mean motion
0.25066 °/min
Orbital period
1,436.21 mins
BSTAR
0
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Other satellites on launch #7 in the year 2014 (2014-02-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.TURKSAT 4A Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| TURKSAT 4A is likely not visible in the next few days. |
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39522 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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