1 | Semi-major axis (SMA) | [3474, 17370] km |
2 | Number of satellites (T) | {8, 9, …, 30} |
3 | Number of planes (P) | {1, …, T} |
4 | Phasing (F) | {0, …, P-1} |
5 | Eccentricity (e) | [0 – 0.7] |
6 | Inclination (i) | [0 – 180] deg |
7 | Argument of periapsis (ω) | {90, 270} deg |
| Design decisions (constellation 2) | Value range |
8 | Semi-major axis (SMA2) | [3474,17370] km |
9 | Number of satellites (T2) | {0, 1, …, 10} |
10 | Number of planes (P2) | {1, …, T2} |
11 | Phasing (F2) | {0, …, P2-1} |
12 | Eccentricity (e2) | [0 – 0.7] |
13 | Inclination (i2) | [0 – 180] deg |
14 | Argument of periapsis (ω2) | {90, 270} deg |