| Spacecraft | CUTE-I (Cubical Tokyo Tech Engineering Satellite-I) |
|---|---|
| Spacecraft type | CubeSat |
| Units or mass | 1U |
| Status | Operational (CW beacon still received, but unsure about data contents. Last SatNOGS report 2023-06-06 last checked on 2023-06-06) |
| Launched | 2003-03-30 |
| NORAD ID | 27844 |
| Deployer | P-POD (Poly-Picosatellite Orbital Deployer) |
| Launcher | Rokot |
| Entity name | Tokyo Institute of Technology |
| Institution | University |
| Entity | Academic / Education |
| Country | Japan |
| Launch brokerer | Space Flight Laboratory (UTIAS-SFL) |
| Partners | SRTL (Space Robotics and Teleoperations Laboratory) of Tokyo |
| Oneliner |
Communication and solar panel deployment. |
| Description |
Communication, sensing and deployment mechanism missions. CW-transmitter and FM-transmitter. FM-telemetry by two different protocol (Ax.25 and TITech original. Broadcasting service of CW-telemetry data and FM-telemetry data on WWW. Deploy the solar battery paddle by command uplink. |
| Sources | [1] [2] [3] |
| Photo sources | [1] [2] [3] |
| Keywords | First CubeSat of country |
| On the same launch |
Last modified: 2023-06-06
