SDA-NG-T1TL-408
Satellite information SDA-NG-T1TL-408 - SDA-NG-T1TL-308
| Spacetrack Directory Name | SDA-NG-T1TL-408 |
| Alternative name | SDA-NG-T1TL-308 |
| Follow SDA-NG-T1TL-408 | SDA-NG-T1TL-408 Tracker |
| Pass predictions SDA-NG-T1TL-408 | Pass predictions SDA-NG-T1TL-408 |
| Orbit launches |
2026-10-10 (one month ago)
|
| Days in orbit | 33 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 938 km |
| Apogee | 951 km |
| Orbit slope (inclination) | 81.5° |
| Laps per day | 14 |
| Height SDA-NG-T1TL-408 | 956.03 km |
Additional information SDA-NG-T1TL-408
SDA-NG-T1TL-308, 100990 is an American payload satellite in LEO that was launched on Sat, 10 Oct 2026 UTC via an FALCON 9 launch vehicle 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 SDA-NG-T1TL-408 Date of exalting 10.10.2026y. Average height of ISS SDA-NG-T1TL-408 hundred 956.03 km. Average velocity SDA-NG-T1TL-408 is 26551.02 km/h. Inclination SDA-NG-T1TL-408 satellite 81.5°.TLE
Average velocity SDA-NG-T1TL-408
Average inclination SDA-NG-T1TL-408
Mean right ascension of the ascending node (RAAN) SDA-NG-T1TL-408
Mean argument of perigee SDA-NG-T1TL-408
Mean semi-major axis of the orbit SDA-NG-T1TL-408
Mean orbital eccentricity SDA-NG-T1TL-408
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