ELECTRON SECOND STAGE
Satellite information ELECTRON SECOND STAGE
| Spacetrack Directory Name | ELECTRON SECOND STAGE |
| Follow ELECTRON SECOND STAGE | ELECTRON SECOND STAGE Tracker |
| Pass predictions ELECTRON SECOND STAGE | Pass predictions ELECTRON SECOND STAGE |
| Orbit launches |
2026-09-02 (23 days ago)
|
| Days in orbit | 23 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | RLLC |
| Perigee | 219 km |
| Apogee | 581 km |
| Orbit slope (inclination) | 38.04° |
| Laps per day | 16 |
| Height ELECTRON SECOND STAGE | 377.34 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 377.34 km. Average velocity ELECTRON SECOND STAGE is 27670.63 km/h. Inclination ELECTRON SECOND STAGE satellite 38.04°.TLE
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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