SES MPOWER-F12, 100687
Orbit data source: Space-Track
SES MPOWER-F12, 100687 is a payload satellite owned by O3B SES (LU) 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
Manufacturer
Boeing/ES
Mission
Operational spacecraft
Bus & Motor
702X, PPS5000
Mass
1,700 kg wet, 1,700 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
BOX + 2 PAN, 13.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 SES MPOWER-F12
1 A0687U 26208B 26259.44619590 .00021346 00000-0 14928-2 0 9993
2 A0687 16.8865 109.4909 3225044 192.9008 156.3972 8.87096376 241Epoch: 2026-09-16T10:42Z
TLE epoch observation values (Epoch: 2026-09-16T10:42:31.325Z)
Latitude
-0.00001°
Longitude
-46.53733°
Altitude
6,500.921 km
Speed
4.634 km/s
True Right ascension
07h 17m 57s
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
02:03:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
6,664.181 km
Perigee altitude
303.212 km
Semi-major axis
9,861.833 km
Eccentricity
0.3225
Inclination
16.8865°
RAAN
109.4909°
Arg. of periapsis
192.9008°
True anomaly
167.12435°
Mean anomaly
156.3972°
Eccentric anomaly
162.08208°
Mean motion
2.21619 °/min
Orbital period
162.44 mins
BSTAR
0.0014928
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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. |
|---|---|---|---|---|---|---|---|
| 54 mins | 2026-09-17 13:24:58.173Z | 190.209° SSW | 2026-09-17 13:50:58.173Z | 150.139° SSE | 22.94° | 2026-09-17 14:18:58.173Z | 111.468° ESE |
| 62 mins | 2026-09-17 16:22:58.173Z | 223.472° SW | 2026-09-17 17:00:58.173Z | 169.781° S | 38.076° | 2026-09-17 17:24:58.173Z | 113.759° SE |
| 44 mins | 2026-09-17 19:34:58.173Z | 245.03° WSW | 2026-09-17 20:05:58.173Z | 191.381° SSW | 37.077° | 2026-09-17 20:18:58.173Z | 134.236° SE |
| 14 mins | 2026-09-17 22:52:58.173Z | 244.581° WSW | 2026-09-17 23:01:58.173Z | 214.228° SW | 16.597° | 2026-09-17 23:06:58.173Z | 184.53° SSW |
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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