Cost-Efficient LEO Navigation Augmentation Constellation Design under a Constrained Deployment Approach

Table 2

Maximum orbit radius estimations of the piggyback launches that are inclined at angles of approximately 74°.

Mission index	Orbit radius (km)	Inclination (deg)	Maximum orbit radius (km)
13	7802.489484	73.98400001	9462.087485
92	7818.911117	74.00040001	9484.031118
44	7845.741149	74.00220002	9519.899150
98	7822.795266	74.00620001	9489.222267
10	7864.360174	74.00670003	9544.800175
53	7859.111068	74.00869999	9537.779069
33	7850.459563	74.01220002	9526.208564
61	7861.005309	74.01260000	9540.313310
75	7828.742114	74.01509999	9497.172115
48	7831.935530	74.01590001	9501.440531
30	7824.724115	74.01900000	9491.801116
8	7850.098940	74.02849998	9525.725941
47	7818.776592	74.02909998	9483.851593
82	7822.145265	74.03459998	9488.354266
3	7157.951397	74.03909999	8606.443398
32	7159.343825	74.03909999	8608.279826
6	7762.008920	74.04399998	9408.024921