AE2A
Satellite information AE2A - 2025-135BR
| Spacetrack Directory Name | AE2A |
| Alternative name | 2025-135BR |
| Follow AE2A | AE2A Tracker |
| Pass predictions AE2A | Pass predictions AE2A |
| Orbit launches |
2025-06-23 (one year ago)
|
| Days in orbit | 471 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 587 km |
| Apogee | 595 km |
| Orbit slope (inclination) | 97.78° |
| Laps per day | 15 |
| Height AE2A | 591.39 km |
Additional information AE2A
TBA - TO BE ASSIGNED named objects are likely recently launched satellites that are being tracked but not necessarily identified.
satellite AE2A Date of exalting 23.06.2025y. Average height of ISS AE2A hundred 591.39 km. Average velocity AE2A is 27236.91 km/h. Inclination AE2A satellite 97.77°.TLE
Average velocity AE2A
Average inclination AE2A
Mean right ascension of the ascending node (RAAN) AE2A
Mean argument of perigee AE2A
Mean semi-major axis of the orbit AE2A
Mean orbital eccentricity AE2A
Frequency AE2A
In the table below we show the frequencies AE2A.
ISS
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