# The Symmetry of GPS Orbit Ascending Nodes
## 4 Conclusions
\begin{table}
\begin{tabular}{c c c c c c c} \hline \hline
**SVN** & **PRN** & **OP** & **SVA** & \begin{tabular}{c} \(a\) \\ [\({}^{\circ}\)**/Year]** \\ \end{tabular} & **\
\begin{tabular}{c} **MD** \\ **[Year]** \\ \end{tabular}** & **n** &
\begin{tabular}{c} **d\(\Omega\)** [\({}^{\circ}\)**]** \\ \end{tabular} \\ \hline
13 & 2 & B & NO & \(-0.39\) & \(8.12\) & \(1241\) & - \\
20 & 20 & B & NO & \(-0.13\) & \(0.69\) & \(33\) & - \\
22 & 22 & B & NO & \(-0.4\) & \(7.35\) & \(1054\) & - \\
30 & 30 & B & NO & \(-0.22\) & \(14.8\) & \(3689\) & - \\
35 & \(05,30\) & B & NO & \(-0.35\) & \(17.09\) & \(3492\) & - \\
44 & 28 & B & **YES** & \(0.25\) & \(20.06\) & \(6615\) & \(4.6\) \\
49 & 1 & B & NO & \(-0.06\) & \(1.14\) & \(414\) & - \\
56 & 16 & B & **YES** & \(0.29\) & \(17.61\) & \(6101\) & \(4.53\) \\
58 & 12 & B & **YES** & \(0.34\) & \(13.81\) & \(5002\) & \(3.72\) \\
62 & 25 & B & **YES** & \(0.2\) & \(10.32\) & \(3745\) & \(0.14\) \\
71 & 26 & B & **YES** & \(-0.23\) & \(5.47\) & \(1991\) & \(-2.03\) \\ \hline \hline \end{tabular}
\end{table} 
Table 14: Descriptive parameters of the OP B satellites. \begin{table}
\begin{tabular}{c c c c c c c c} \hline \hline
**SVN** & **PRN** & **OP** & **SVA** & \begin{tabular}{c} \(a\) \\ [\({}^{\circ}\)**/Year**] \\ \end{tabular} & \
\begin{tabular}{c} **MD** \\ **[Year]** \\ \end{tabular} & **n** &
\begin{tabular}{c} **d\(\Omega\)** [\({}^{\circ}\)**]** \\ \end{tabular} \\ \hline
14 & 14 & E & NO & 0.22 & 4.04 & 402 & - \\
16 & 16 & E & NO & 0.18 & 4.51 & 427 & - \\
21 & 21 & E & NO & 0.18 & 6.83 & 928 & - \\
23 & 23, 32 & E & NO & 0.06 & 19.83 & 4277 & - \\
40 & 10 & E & NO & \(-0.05\) & 18.93 & 5136 & - \\
47 & 22 & E & YES & \(-0.57\) & 16.72 & 5888 & \(-5.08\) \\
50 & 5 & E & YES & \(-0.1\) & 11.07 & 4017 & \(-1.88\) \\
51 & 20 & E & YES & \(-0.47\) & 20.29 & 6627 & \(-7.55\) \\
54 & 18 & E & NO & \(-0.46\) & 17.05 & 5647 & - \\
69 & 3 & E & YES & 0.18 & 5.87 & 2136 & 0.04 \\
73 & 10 & E & YES & 0.11 & 4.86 & 1770 & \(-0.26\) \\
76 & 23 & E & YES & \(-0.02\) & 0.18 & 67 & \(-1.64\) \\ \hline \hline \end{tabular}
\end{table} 
Table 4: Descriptive parameters of the OP E satellites. Figure A4: Separation of satellite ANs from the hex-LS-estimated position of the OP E AN with satellite dot(\(\Omega\)) values. Figure A5: Separation of satellite ANs from the hex-LS-estimated position of the OP F AN with satellite dot(\(\Omega\)) values. \begin{table}
\begin{tabular}{c c c c c c c} \hline \hline
**SVN** & **PRN** & **OP** & **SVA** & \(\mathbf{a}\) & **MD** & **n** & **d\(\Omega\)**[\({}^{\circ}\)]** \\  & & & & & [\({}^{\circ}\)/**Year**]** & **[Year]** & **n** & **d\(\Omega\)**[\({}^{\circ}\)]** \\ \hline
18 & 18 & F & NO & \(-0.15\) & 4.38 & 420 & - \\
26 & 26 & F & NO & 0.28 & 18.77 & 4966 & - \\
29 & 29 & F & NO & 0.14 & 11.57 & 2363 & - \\
32 & 1 & F & NO & 0.17 & 11.97 & 2502 & - \\
41 & 14 & F & NO & 0.25 & 19.55 & 6532 & - \\
43 & 13 & F & **YES** & 0.37 & 23.11 & 6908 & 7.24 \\
55 & 15 & F & **YES** & \(-0.44\) & 12.89 & 4671 & \(-6.14\) \\
60 & 23 & F & NO & \(-0.11\) & 15.7 & 5576 & - \\
68 & 9 & F & **YES** & 0.05 & 6.12 & 2224 & \(-0.97\) \\
70 & 32 & F & **YES** & 0.06 & 4.6 & 1675 & \(-0.62\) \\
74 & 4 & F & **YES** & \(-0.07\) & 0.93 & 337 & 1.49 \\ \hline \hline \end{tabular}
\end{table} 
Table 5: Descriptive parameters of the OP F satellites.