TURKSAT 3A, 33056
Orbit data source: Space-Track
TURKSAT 3A, 33056 is a payload satellite owned by Turksat (TR) in GEO that was launched on Thu, 12 Jun 2008 UTC via an ARIANE 5ECA launch vehicle from the French Guiana (FRGUI). 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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33056 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / TURKRelated business
Manufacturer
Thales Alenia
Mission
Operational Civil Communications
Bus & Motor
SPACEBUS 4000B2, S400
Mass
3,010 kg wet, ~1,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 15.0 m
Radar Cross Section
28.939 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 TURKSAT 3A
1 33056U 08030B 25243.53385854 .00000150 00000-0 00000-0 0 9991
2 33056 0.0382 84.5862 0004891 63.9214 65.6200 1.00273795 49457Epoch: 2025-08-31T12:48Z
TLE epoch observation values (Epoch: 2025-08-31T12:48:45.377Z)
Latitude
0.04478°
Longitude
42.03244°
Altitude
35,776.958 km
Speed
3.075 km/s
True Right ascension
14h 16m 41s
True Declination
0° 02' 41"
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
13:00:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,807.725 km
Perigee altitude
35,766.479 km
Semi-major axis
42,165.239 km
Eccentricity
0.00049
Inclination
0.0382°
RAAN
84.5862°
Arg. of periapsis
63.9214°
True anomaly
65.67106°
Mean anomaly
65.62°
Eccentric anomaly
65.64553°
Mean motion
0.25068 °/min
Orbital period
1,436.12 mins
BSTAR
0
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Other satellites on launch #30 in the year 2008 (2008-06-12 UTC)
TURKSAT 3A Visibility
Observer location: undefined°, undefined°
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. |
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33056 neighbors
Authenticating...
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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