| Name | CICERO-2 |
|---|---|
| Type | CubeSat |
| Units or mass | 6U |
| Organisation | GeoOptics |
| Institution | Company |
| Entity | Commercial |
| Nation | US |
| Manufacturer | AIVT by Terran Orbital |
| Launch brokerer | Tyvak, ? |
| Partners | Tyvak |
| Oneliner |
Demonstration of GPS radio occultation sensor that allows the measurement of global weather pattern with high accuracy. |
| Sources | [1] |
| Photo sources | [1] |
| COTS subsystems |
|
| Space photos | 
|
Related Spacecraft
| Name | Status | Launch | Orbit |
|---|---|---|---|
| CICERO-2 1 (VEH 1, Vehicle 1, Community Initiative for Continuous Earth Remote Observation, OP1, TYVAK-0820) | Operational? (News on 2022-05-26 as of 2022-12-21) | 2022-05-25 | 530 km, 97.5 deg, SSO |
| CICERO-2 2 (VEH 2, Vehicle 2, Community Initiative for Continuous Earth Remote Observation, OP2, TYVAK-0821) | Operational? (News on 2022-05-26 as of 2022-12-21) | 2022-05-25 | 530 km, 97.5 deg, SSO |
Last modified: 2023-06-08
Detailed CICERO-2 entry in the Database
Full Nanosats Database (much more data)
