TURKSAT 6A, 60233
Orbit data source: Space-Track
TURKSAT 6A, 60233 is a payload satellite owned by Turksat (TR) in GEO that was launched on Mon, 08 Jul 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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60233 intel report (Beta)
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Identifier
Orbit
Country
TR / TURKRelated business
Manufacturer
TUSAS
Mission
Operational Commercial Communications
Bus & Motor
TURKSAT 6, Unknown motor
Mass
4,250 kg wet, ~1,700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 15.0 m
Radar Cross Section
39.706 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 TURKSAT 6A
1 60233U 24127A 26275.06850512 .00000141 00000-0 00000-0 0 9995
2 60233 0.0333 219.1805 0004951 350.5693 227.7344 1.00274267 8085Epoch: 2026-10-02T01:38Z
TLE epoch observation values (Epoch: 2026-10-02T01:38:38.842Z)
Latitude
-0.03581°
Longitude
41.96139°
Altitude
35,799.455 km
Speed
3.074 km/s
True Right ascension
05h 09m 40s
True Declination
0° 02' 09"
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
21:09:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,807.846 km
Perigee altitude
35,766.094 km
Semi-major axis
42,165.107 km
Eccentricity
0.0005
Inclination
0.0333°
RAAN
219.1805°
Arg. of periapsis
350.5693°
True anomaly
227.69243°
Mean anomaly
227.7344°
Eccentric anomaly
227.71341°
Mean motion
0.25068 °/min
Orbital period
1,436.11 mins
BSTAR
0
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Other satellites on launch #127 in the year 2024 (2024-07-08 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 6A 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. |
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| TURKSAT 6A is likely not visible in the next few days. |
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60233 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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