| Spacecraft | CICERO-2 (Community Initiative for Continuous Earth Remote Observation) |
|---|---|
| Spacecraft type | CubeSat |
| Units or mass | 6U |
| Organisation | GeoOptics |
| Institution | Company |
| Entity type | 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 | Launcher | Date | Orbit |
|---|---|---|---|---|
| CICERO-2 1 (VEH 1, Vehicle 1, Community Initiative for Continuous Earth Remote Observation, OP1, OP15 FLT1, TYVAK-0820) | Reentry 2024-09-18. Was operational? (News on 2022-05-26 as of 2022-12-21) | Falcon 9, (Transporter-5) | 2022-05-25 | 530 km, 97.5 deg |
| CICERO-2 2 (VEH 2, Vehicle 2, Community Initiative for Continuous Earth Remote Observation, OP2, OP15 FLT2, TYVAK-0821) | Reentry 2024-09-09. Was operational? (News on 2022-05-26 as of 2022-12-21) | Falcon 9, (Transporter-5) | 2022-05-25 | 530 km, 97.5 deg |
Last modified: 2024-09-29
