QPS-SAR-7 TSUKUYOMI-II
Satellite information QPS-SAR-7 TSUKUYOMI-II - 2024-066F
| Spacetrack Directory Name | QPS-SAR-7 TSUKUYOMI-II |
| Alternative name | 2024-066F |
| Follow QPS-SAR-7 TSUKUYOMI-II | QPS-SAR-7 TSUKUYOMI-II Tracker |
| Pass predictions QPS-SAR-7 TSUKUYOMI-II | Pass predictions QPS-SAR-7 TSUKUYOMI-II |
| Orbit launches |
2024-04-07 (2 years ago)
|
| Days in orbit | 813 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 590 km |
| Apogee | 595 km |
| Orbit slope (inclination) | 45.6° |
| Laps per day | 15 |
| Height QPS-SAR-7 TSUKUYOMI-II | 551.65 km |
Additional information QPS-SAR-7 TSUKUYOMI-II
QPS-SAR-7 TSUKUYOMI-II, 59447 is a payload satellite owned by QPS Labs (JP) in LEO that was launched on Sun, 07 Apr 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite QPS-SAR-7 TSUKUYOMI-II Date of exalting 07.04.2024y. Average height of ISS QPS-SAR-7 TSUKUYOMI-II hundred 551.65 km. Average velocity QPS-SAR-7 TSUKUYOMI-II is 27240.24 km/h. Inclination QPS-SAR-7 TSUKUYOMI-II satellite 45.48°.TLE
Average orbit height QPS-SAR-7 TSUKUYOMI-II
Average velocity QPS-SAR-7 TSUKUYOMI-II
Average inclination QPS-SAR-7 TSUKUYOMI-II
ISS
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