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 |
2026-05-22 (2 months ago)
|
| Days in orbit | 89 |
| Country/organisation of origin | USA (US) |
| Starting point | RLLC |
| Perigee | 540 km |
| Apogee | 579 km |
| Orbit slope (inclination) | 44.91° |
| Laps per day | 15 |
| Height ELECTRON KICK STAGE R/B | 563.42 km |
Additional information ELECTRON KICK STAGE R/B
ELECTRON KICK STAGE R/B, 69178 is space debris in LEO originally from an American launch on Fri, 22 May 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 22.05.2026y. Average height of ISS ELECTRON KICK STAGE R/B hundred 563.42 km. Average velocity ELECTRON KICK STAGE R/B is 27295.13 km/h. Inclination ELECTRON KICK STAGE R/B satellite 44.91°.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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