ELECTRON R/B
Satellite information ELECTRON R/B - ELEKTRON / RB
| Spacetrack Directory Name | ELECTRON R/B |
| Alternative name | ELEKTRON / RB |
| Follow ELECTRON R/B | ELECTRON R/B Tracker |
| Pass predictions ELECTRON R/B | Pass predictions ELECTRON R/B |
| Orbit launches |
2026-09-26 (one month ago)
|
| Days in orbit | 44 |
| Country/organisation of origin | USA (US) |
| Starting point | RLLC |
| Perigee | 172 km |
| Apogee | 538 km |
| Orbit slope (inclination) | 37.87° |
| Laps per day | 16 |
| Height ELECTRON R/B | 213.5 km |
Additional information ELECTRON R/B
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 ELECTRON R/B Date of exalting 26.09.2026y. Average height of ISS ELECTRON R/B hundred 213.5 km. Average velocity ELECTRON R/B is 28016.15 km/h. Inclination ELECTRON R/B satellite 37.87°.TLE
Average velocity ELECTRON R/B
Average inclination ELECTRON R/B
Mean right ascension of the ascending node (RAAN) ELECTRON R/B
Mean argument of perigee ELECTRON R/B
Mean semi-major axis of the orbit ELECTRON R/B
Mean orbital eccentricity ELECTRON R/B
ISS
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