Preliminary Orbit Determination of Artificial Satellites: A Vectorial Sixth-Order Approach

Table 4

Results of tundra Orbit.

Method	Iter	𝜌	𝐼̃	𝐼𝑐̃	𝜀𝑎	𝜀𝑒	𝜀𝑖	𝜀𝑤	𝜀Ω	Time (s)
N	6	2.0121	1.1041	1.1041	3.1284𝑒−16	1.6038𝑒−17	2.4321𝑒−16	6.5148𝑒−15	0	0.005069
T	5	2.9852	1.1331	1.1051	3.1284𝑒−16	1.6038𝑒−17	2.4321𝑒−16	6.5148𝑒−15	0	0.005493
J	3	3.9931	1.1409	1.0859	3.1284𝑒−16	1.6038𝑒−17	2.4321𝑒−16	6.5148𝑒−15	0	0.004457
NAJC1	3	4.9478	1.1336	1.0482	3.1284𝑒−16	1.6038𝑒−17	2.4321𝑒−16	6.5148𝑒−15	0	0.009004
NAJC2	3	5.2465	1.1337	1.0482	3.1284𝑒−16	1.6038𝑒−17	2.4321𝑒−16	6.5148𝑒−15	0	0.007704