ELEKTRON / RB
Satellite information ELEKTRON / RB
| Spacetrack Directory Name | ELEKTRON / RB |
| Orbit launches |
2026-09-26 |
| Deorbitation |
|
| Country/organisation of origin | Japonia (JPN) |
| Starting point | RLLC |
| Perigee | 172 km |
| Apogee | 538 km |
| Height ELEKTRON / RB | 213.5 km |
Additional information ELEKTRON / RB
ELEKTRON / RB, 100830 is a Japanese payload satellite in LEO that was launched on Sat, 26 Sep 2026 UTC launched from the Rocket Lab Launch Complex (RLLC). 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 ELEKTRON / RB Date of exalting 26.09.2026y. Average height of ISS ELEKTRON / RB hundred 213.5 km. Average velocity ELEKTRON / RB is 28016.15 km/h. Inclination ELEKTRON / RB satellite 37.87°.Average velocity ELEKTRON / RB
Average inclination ELEKTRON / RB
Mean right ascension of the ascending node (RAAN) ELEKTRON / RB
Mean argument of perigee ELEKTRON / RB
Mean semi-major axis of the orbit ELEKTRON / RB
Mean orbital eccentricity ELEKTRON / RB
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