SES MPOWER-F13
Satellite information SES MPOWER-F13
| Spacetrack Directory Name | SES MPOWER-F13 |
| Follow SES MPOWER-F13 | SES MPOWER-F13 Tracker |
| Pass predictions SES MPOWER-F13 | Pass predictions SES MPOWER-F13 |
| Orbit launches |
2026-09-13 (one month ago)
|
| Days in orbit | 38 |
| Country/organisation of origin | SES |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 293 km |
| Apogee | 6649 km |
| Orbit slope (inclination) | 15.75° |
| Laps per day | 9 |
| Height SES MPOWER-F13 | 4051.1 km |
Additional information SES MPOWER-F13
SES MPOWER-F13, 100688 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.
satellite SES MPOWER-F13 Date of exalting 13.09.2026y. Average height of ISS SES MPOWER-F13 hundred 4051.1 km. Average velocity SES MPOWER-F13 is 22231.25 km/h. Inclination SES MPOWER-F13 satellite 16.45°.TLE
Average velocity SES MPOWER-F13
Average inclination SES MPOWER-F13
Mean right ascension of the ascending node (RAAN) SES MPOWER-F13
Mean argument of perigee SES MPOWER-F13
Mean semi-major axis of the orbit SES MPOWER-F13
Mean orbital eccentricity SES MPOWER-F13
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