Table 1. Coefficients of Earth orbit elements
a
0
a
1
a
2
a
3
L
100.466449
+36000.7698231
+0.00030368
+0.000000021
a
1.000001018
e
0.01670862
-0.000042037
-0.0000001236
+0.00000000004
i
0
Ω
0
ω
102.937348
+1.7195269
+0.00045962
+0.000000499