FALCON HEAVY R/B
Satellite information FALCON HEAVY R/B
| Spacetrack Directory Name | FALCON HEAVY R/B |
| Follow FALCON HEAVY R/B | FALCON HEAVY R/B Tracker |
| Pass predictions FALCON HEAVY R/B | Pass predictions FALCON HEAVY R/B |
| Orbit launches |
2026-04-29 (3 months ago)
|
| Days in orbit | 113 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 22983 km |
| Apogee | 33152 km |
| Orbit slope (inclination) | 2.5° |
| Laps per day | 1 |
| Height FALCON HEAVY R/B | 28457.74 km |
Additional information FALCON HEAVY R/B
FALCON HEAVY R/B, 68894 is space debris originally from an American launch on Wed, 29 Apr 2026 UTC launched from the Air Force Eastern Test Range (AFETR). 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 FALCON HEAVY R/B Date of exalting 29.04.2026y. Average height of ISS FALCON HEAVY R/B hundred 28457.74 km. Average velocity FALCON HEAVY R/B is 12171.34 km/h. Inclination FALCON HEAVY R/B satellite 2.51°.TLE
Average velocity FALCON HEAVY R/B
Average inclination FALCON HEAVY R/B
Mean right ascension of the ascending node (RAAN) FALCON HEAVY R/B
Mean argument of perigee FALCON HEAVY R/B
Mean semi-major axis of the orbit FALCON HEAVY R/B
Mean orbital eccentricity FALCON HEAVY R/B
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