FIREFLY ALPHA R/B
Satellite information FIREFLY ALPHA R/B
| Spacetrack Directory Name | FIREFLY ALPHA R/B |
| Follow FIREFLY ALPHA R/B | FIREFLY ALPHA R/B Tracker |
| Pass predictions FIREFLY ALPHA R/B | Pass predictions FIREFLY ALPHA R/B |
| Orbit launches |
2026-03-12 (6 months ago)
|
| Days in orbit | 195 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 382 km |
| Apogee | 406 km |
| Orbit slope (inclination) | 123.09° |
| Laps per day | 16 |
| Height FIREFLY ALPHA R/B | 363.54 km |
Additional information FIREFLY ALPHA R/B
FIREFLY ALPHA R/B, 68128 is space debris in LEO originally from a launch on Thu, 12 Mar 2026 UTC launched from the Air Force Western Test Range (AFWTR). 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 FIREFLY ALPHA R/B Date of exalting 12.03.2026y. Average height of ISS FIREFLY ALPHA R/B hundred 363.54 km. Average velocity FIREFLY ALPHA R/B is 27695.76 km/h. Inclination FIREFLY ALPHA R/B satellite 123.09°.TLE
Average velocity FIREFLY ALPHA R/B
Average inclination FIREFLY ALPHA R/B
Mean right ascension of the ascending node (RAAN) FIREFLY ALPHA R/B
Mean argument of perigee FIREFLY ALPHA R/B
Mean semi-major axis of the orbit FIREFLY ALPHA R/B
Mean orbital eccentricity FIREFLY ALPHA R/B
ISS
Buy us a coffee!
