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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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: 2 days ago
TLE from 2 days ago
0 SES 10
1 42432U 17017A 26171.37872375 -.00000277 00000-0 00000+0 0 9996
2 42432 0.0216 40.5012 0002727 55.6577 241.8767 1.00272149 33783Epoch: 2026-06-20T09:05Z
TLE epoch observation values (Epoch: 2026-06-20T09:05:21.731Z)
Latitude
-0.02761°
Longitude
-66.91452°
Altitude
35,791.418 km
Speed
3.074 km/s
True Right ascension
22h 32m 04s
True Declination
0° 01' 39"
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
21:37:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,799.062 km
Perigee altitude
35,776.065 km
Semi-major axis
42,165.7 km
Eccentricity
0.00027
Inclination
0.0216°
RAAN
40.5012°
Arg. of periapsis
55.6577°
True anomaly
241.84914°
Mean anomaly
241.8767°
Eccentric anomaly
241.86292°
Mean motion
0.25067 °/min
Orbital period
1,436.15 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 | 2026-06-22 10:35:05.131Z | 129.194° SE | 2026-06-22 16:33:05.131Z | 129.128° SE | 26.234° | 2026-06-23 10:35:05.131Z | 129.198° 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
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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