ELECTRON R/B
Satellite information ELECTRON R/B
| Spacetrack Directory Name | ELECTRON R/B |
| Follow ELECTRON R/B | ELECTRON R/B Tracker |
| Pass predictions ELECTRON R/B | Pass predictions ELECTRON R/B |
| Orbit launches |
2026-09-11 (one month ago)
|
| Days in orbit | 42 |
| Country/organisation of origin | USA (US) |
| Starting point | RLLC |
| Perigee | 192 km |
| Apogee | 477 km |
| Orbit slope (inclination) | 36.06° |
| Laps per day | 16 |
| Height ELECTRON R/B | 249.03 km |
Additional information ELECTRON R/B
ELECTRON R/B, 100683 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 R/B Date of exalting 11.09.2026y. Average height of ISS ELECTRON R/B hundred 249.03 km. Average velocity ELECTRON R/B is 27938.47 km/h. Inclination ELECTRON R/B satellite 36.07°.TLE
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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