FGN-TUG-S01
Satellite information FGN-TUG-S01
| Spacetrack Directory Name | FGN-TUG-S01 |
| Follow FGN-TUG-S01 | FGN-TUG-S01 Tracker |
| Pass predictions FGN-TUG-S01 | Pass predictions FGN-TUG-S01 |
| Orbit launches |
2025-11-28 (9 months ago)
|
| Days in orbit | 301 |
| Country/organisation of origin | Turcja (TURK) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 532 km |
| Apogee | 1213 km |
| Orbit slope (inclination) | 97.38° |
| Laps per day | 14 |
| Height FGN-TUG-S01 | 892.45 km |
Additional information FGN-TUG-S01
FGN-TUG-S01, 100399 is a Turkish payload satellite in SSO that was launched on Fri, 28 Nov 2025 UTC launched from the Air Force Western Test Range (AFWTR). 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 FGN-TUG-S01 Date of exalting 28.11.2025y. Average height of ISS FGN-TUG-S01 hundred 892.45 km. Average velocity FGN-TUG-S01 is 26666.38 km/h. Inclination FGN-TUG-S01 satellite 97.38°.TLE
Average velocity FGN-TUG-S01
Average inclination FGN-TUG-S01
Mean right ascension of the ascending node (RAAN) FGN-TUG-S01
Mean argument of perigee FGN-TUG-S01
Mean semi-major axis of the orbit FGN-TUG-S01
Mean orbital eccentricity FGN-TUG-S01
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