CE-SAT-IE
Satellite information CE-SAT-IE - 2024-032A
| Spacetrack Directory Name | CE-SAT-IE |
| Alternative name | 2024-032A |
| Follow CE-SAT-IE | CE-SAT-IE Tracker |
| Pass predictions CE-SAT-IE | Pass predictions CE-SAT-IE |
| Orbit launches |
2024-02-17 (2 years ago)
|
| Days in orbit | 814 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 671 km |
| Apogee | 673 km |
| Orbit slope (inclination) | 98° |
| Laps per day | 15 |
| Height CE-SAT-IE | 677.56 km |
Additional information CE-SAT-IE
CE-SAT-IE, 58987 is a payload satellite owned by Canon STL (JP) in SSO that was launched on Sat, 17 Feb 2024 UTC via a H3-22S launch vehicle from the Tanegashima Space Center (TNSTA). 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 CE-SAT-IE Date of exalting 17.02.2024y. Average height of ISS CE-SAT-IE hundred 677.56 km. Average velocity CE-SAT-IE is 26992.31 km/h. Inclination CE-SAT-IE satellite 97.76°.TLE
Average orbit height CE-SAT-IE
Average velocity CE-SAT-IE
Average inclination CE-SAT-IE
ISS
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