ELECTRON R/B
Satellite information ELECTRON R/B
| Spacetrack Directory Name | ELECTRON R/B |
| Orbit launches |
2026-09-19 |
| Deorbitation |
|
| Country/organisation of origin | USA (US) |
| Starting point | RLLC |
| Perigee | 172 km |
| Apogee | 545 km |
| Height ELECTRON R/B | 213.33 km |
Additional information ELECTRON R/B
ELECTRON R/B, 100747 is space debris in LEO originally from a launch on Sat, 19 Sep 2026 UTC launched from the Rocket Lab Launch Complex (RLLC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite ELECTRON R/B Date of exalting 19.09.2026y. Average height of ISS ELECTRON R/B hundred 213.33 km. Average velocity ELECTRON R/B is 28015.41 km/h. Inclination ELECTRON R/B satellite 38.15°.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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