Research Article
Design, Analysis, Optimization, Manufacturing, and Testing of a 2U Cubesat
| ISS orbit |
| Semimajor axis (km) | 6780 | Eccentricity (degrees) | 0 | Ascending node longitude (degrees) | ā94.354 | Inclination (degrees) | 51.64 | Mean anomaly (degrees) | 254.215 |
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