ELECTRON KICK STAGE R/B
Satellite information ELECTRON KICK STAGE R/B
| Spacetrack Directory Name | ELECTRON KICK STAGE R/B |
| Follow ELECTRON KICK STAGE R/B | ELECTRON KICK STAGE R/B Tracker |
| Pass predictions ELECTRON KICK STAGE R/B | Pass predictions ELECTRON KICK STAGE R/B |
| Orbit launches |
2026-09-11 (one month ago)
|
| Days in orbit | 36 |
| Country/organisation of origin | USA (US) |
| Starting point | RLLC |
| Perigee | 248 km |
| Apogee | 508 km |
| Orbit slope (inclination) | 36° |
| Laps per day | 16 |
| Height ELECTRON KICK STAGE R/B | 339.66 km |
Additional information ELECTRON KICK STAGE R/B
ELECTRON KICK STAGE R/B, 100684 is space debris in LEO originally from an American launch on Fri, 11 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 KICK STAGE R/B Date of exalting 11.09.2026y. Average height of ISS ELECTRON KICK STAGE R/B hundred 339.66 km. Average velocity ELECTRON KICK STAGE R/B is 27747.87 km/h. Inclination ELECTRON KICK STAGE R/B satellite 36.01°.TLE
Average orbit height ELECTRON KICK STAGE R/B
Average velocity ELECTRON KICK STAGE R/B
Average inclination ELECTRON KICK STAGE R/B
Mean right ascension of the ascending node (RAAN) ELECTRON KICK STAGE R/B
Mean argument of perigee ELECTRON KICK STAGE R/B
Mean semi-major axis of the orbit ELECTRON KICK STAGE R/B
Mean orbital eccentricity ELECTRON KICK STAGE R/B
ISS
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