SES MPOWER-F12, 100687
Orbit data source: Space-Track
SES MPOWER-F12, 100687 is a Luxembourger payload satellite that was launched on Sun, 13 Sep 2026 UTC launched 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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100687 intel report (Beta)
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Identifier
Orbit
Country
LU / SESRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SES MPOWER-F12
1 A0687U 26208B 26257.08540483 .00005222 00000-0 34456-3 0 9999
2 A0687 16.8931 115.7107 3226571 181.3693 177.5154 8.86991821 35Epoch: 2026-09-14T02:02Z
TLE epoch observation values (Epoch: 2026-09-14T02:02:58.977Z)
Latitude
-0.00001°
Longitude
91.89415°
Altitude
6,655.969 km
Speed
4.555 km/s
True Right ascension
07h 42m 50s
True Declination
0° 00' 00"
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
02:08:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
6,666.711 km
Perigee altitude
302.23 km
Semi-major axis
9,862.608 km
Eccentricity
0.32266
Inclination
16.8931°
RAAN
115.7107°
Arg. of periapsis
181.3693°
True anomaly
178.6556°
Mean anomaly
177.5154°
Eccentric anomaly
178.12143°
Mean motion
2.21593 °/min
Orbital period
162.46 mins
BSTAR
0.00034456
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Other satellites on launch #208 in the year 2026 (2026-09-13 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 MPOWER-F12 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. |
|---|---|---|---|---|---|---|---|
| 39 mins | 2026-09-15 12:46:17.369Z | 174.109° S | 2026-09-15 13:05:17.369Z | 146.257° SSE | 15.625° | 2026-09-15 13:25:17.369Z | 120.691° SE |
| 61 mins | 2026-09-15 15:39:17.369Z | 213.71° SW | 2026-09-15 16:15:17.369Z | 163.532° S | 32.715° | 2026-09-15 16:40:17.369Z | 112.534° SE |
| 48 mins | 2026-09-15 18:48:17.369Z | 238.107° WSW | 2026-09-15 19:21:17.369Z | 185.008° SSW | 37.27° | 2026-09-15 19:36:17.369Z | 125.755° SE |
| 21 mins | 2026-09-15 22:05:17.369Z | 247.048° WSW | 2026-09-15 22:18:17.369Z | 210.669° SW | 22.4° | 2026-09-15 22:26:17.369Z | 160.846° S |
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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