SDA-NG-T1TL-318
Satellite information SDA-NG-T1TL-318
| Spacetrack Directory Name | SDA-NG-T1TL-318 |
| Follow SDA-NG-T1TL-318 | SDA-NG-T1TL-318 Tracker |
| Pass predictions SDA-NG-T1TL-318 | Pass predictions SDA-NG-T1TL-318 |
| Orbit launches |
2026-10-10 (26 days ago)
|
| Days in orbit | 26 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 935 km |
| Apogee | 948 km |
| Orbit slope (inclination) | 81.5° |
| Laps per day | 14 |
| Height SDA-NG-T1TL-318 | 953.77 km |
Additional information SDA-NG-T1TL-318
SDA-NG-T1TL-318, 101000 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-318 Date of exalting 10.10.2026y. Average height of ISS SDA-NG-T1TL-318 hundred 953.77 km. Average velocity SDA-NG-T1TL-318 is 26555.1 km/h. Inclination SDA-NG-T1TL-318 satellite 81.5°.TLE
Average velocity SDA-NG-T1TL-318
Average inclination SDA-NG-T1TL-318
Mean right ascension of the ascending node (RAAN) SDA-NG-T1TL-318
Mean argument of perigee SDA-NG-T1TL-318
Mean semi-major axis of the orbit SDA-NG-T1TL-318
Mean orbital eccentricity SDA-NG-T1TL-318
ISS
Buy us a coffee!
