ELECTRON SECOND STAGE
Satellite information ELECTRON SECOND STAGE
| Spacetrack Directory Name | ELECTRON SECOND STAGE |
| Orbit launches |
2026-09-02 |
| Deorbitation |
|
| Country/organisation of origin | Japonia (JPN) |
| Starting point | RLLC |
| Perigee | 219 km |
| Apogee | 581 km |
| Height ELECTRON SECOND STAGE | 322.1 km |
Additional information ELECTRON SECOND STAGE
ELECTRON SECOND STAGE, 100562 is a payload satellite owned by Rocket Lab (JP) in LEO that was launched on Wed, 02 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 SECOND STAGE Date of exalting 02.09.2026y. Average height of ISS ELECTRON SECOND STAGE hundred 322.1 km. Average velocity ELECTRON SECOND STAGE is 27786.12 km/h. Inclination ELECTRON SECOND STAGE satellite 38.04°.Average velocity ELECTRON SECOND STAGE
Average inclination ELECTRON SECOND STAGE
Mean right ascension of the ascending node (RAAN) ELECTRON SECOND STAGE
Mean argument of perigee ELECTRON SECOND STAGE
Mean semi-major axis of the orbit ELECTRON SECOND STAGE
Mean orbital eccentricity ELECTRON SECOND STAGE
ISS
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