SES 10, 42432
Orbit data source: Space-Track
SES 10, 42432 is a payload satellite owned by SES Sat. Leasing (LU) in GEO that was launched on Thu, 30 Mar 2017 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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42432 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
LU / SESRelated business
Manufacturer
ADS/Bremen
Mission
Operational Commercial Communications
Bus & Motor
EUROSTAR 3000, R-4D-15
Mass
5,300 kg wet, ~3,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.5 m
Radar Cross Section
56.564 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SES 10
1 42432U 17017A 25260.99778654 -.00000293 00000-0 00000-0 0 9996
2 42432 0.0076 200.8270 0002705 346.2157 102.4243 1.00269068 31014Epoch: 2025-09-17T23:56Z
TLE epoch observation values (Epoch: 2025-09-17T23:56:48.757Z)
Latitude
0.02369°
Longitude
-66.86964°
Altitude
35,789.343 km
Speed
3.075 km/s
True Right ascension
19h 17m 59s
True Declination
0° 01' 25"
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
22:05:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,799.833 km
Perigee altitude
35,777.021 km
Semi-major axis
42,166.564 km
Eccentricity
0.00027
Inclination
0.0076°
RAAN
200.827°
Arg. of periapsis
346.2157°
True anomaly
102.45457°
Mean anomaly
102.4243°
Eccentric anomaly
102.43943°
Mean motion
0.25066 °/min
Orbital period
1,436.19 mins
BSTAR
0
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Other satellites on launch #17 in the year 2017 (2017-03-30 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 10 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 | 2025-09-19 05:12:23.984Z | 129.18° SE | 2025-09-20 03:58:23.984Z | 129.177° SE | 26.231° | 2025-09-20 05:12:23.984Z | 129.194° SE |
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42432 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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