SES 14, 43175
Orbit data source: Space-Track
SES 14, 43175 is a payload satellite owned by SES (LU) in GEO that was launched on Thu, 25 Jan 2018 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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43175 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
LU / SESRelated business
Manufacturer
Airbus/Toulouse
Mission
Operational Commercial Communications
Bus & Motor
EUROSTAR 3000E, EOR
Mass
4,423 kg wet, ~2,800 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 19.6 m
Radar Cross Section
49.877 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 SES 14
1 43175U 18012B 25306.38598117 -.00000266 00000-0 00000+0 0 9994
2 43175 0.0227 358.8800 0001179 217.0347 277.4866 1.00273694 4755Epoch: 2025-11-02T09:15Z
TLE epoch observation values (Epoch: 2025-11-02T09:15:48.773Z)
Latitude
-0.00753°
Longitude
-47.5068°
Altitude
35,784.905 km
Speed
3.075 km/s
True Right ascension
08h 53m 23s
True Declination
0° 00' 27"
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
21:04:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,792.101 km
Perigee altitude
35,782.159 km
Semi-major axis
42,165.267 km
Eccentricity
0.00012
Inclination
0.0227°
RAAN
358.88°
Arg. of periapsis
217.0347°
True anomaly
277.4732°
Mean anomaly
277.4866°
Eccentric anomaly
277.4799°
Mean motion
0.25067 °/min
Orbital period
1,436.12 mins
BSTAR
0
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Other satellites on launch #12 in the year 2018 (2018-01-25 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.SES 14 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-11-04 01:10:41.920Z | 112.1° ESE | 2025-11-04 05:16:41.920Z | 112.115° ESE | 15.318° | 2025-11-05 01:10:41.920Z | 112.094° ESE |
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43175 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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