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 |
2026-10-23 (5 days ago)
|
| Days in orbit | 5 |
| Country/organisation of origin | USA (US) |
| Starting point | RLLC |
| Perigee | 167 km |
| Apogee | 495 km |
| Orbit slope (inclination) | 97.41° |
| Laps per day | 16 |
| Height ELECTRON R/B | 313.63 km |
Additional information ELECTRON R/B
ELECTRON R/B, 101147 is space debris in SSO originally from a launch on Fri, 23 Oct 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 23.10.2026y. Average height of ISS ELECTRON R/B hundred 313.63 km. Average velocity ELECTRON R/B is 27798.15 km/h. Inclination ELECTRON R/B satellite 97.42°.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
Buy us a coffee!
