Estimation and Analysis of Powered Phase’s Orbit of the Spacecraft Based on Multiple-Point Intersection Algorithm

Table 5

Estimations of spacecraft 0.

Time (s)	Estimation position (m)			Estimation velocity (m/s)
	x	y	z	x	y	z
50	−1.1053335 E + 06	6.2034360 E + 06	1.1350124 E + 06	−7.6829756 E + 02	7.7969235 E + 03	9.7559569 E + 02
60	−1.1135553 E + 06	6.2111612 E + 06	1.1454274 E + 06	−8.8420484 E + 02	7.6487188 E + 03	1.1173389 E + 03
70	−1.1230364 E + 06	6.2187452 E + 06	1.1573817 E + 06	−1.0130099 E + 03	7.5255725 E + 03	1.2747035 E + 03
80	−1.1338359 E + 06	6.2262251 E + 06	1.1709458 E + 06	−1.1479464 E + 03	7.4408492 E + 03	1.4393986 E + 03
90	−1.1460175 E + 06	6.2336408 E + 06	1.1861961 E + 06	−1.2895491 E + 03	7.3978234 E + 03	1.6120649 E + 03
100	−1.1596510 E + 06	6.2410358 E + 06	1.2032160 E + 06	−1.4384300 E + 03	7.4002235 E + 03	1.7934354 E + 03
110	−1.1748126 E + 06	6.2484577 E + 06	1.2220966 E + 06	−1.5952926 E + 03	7.4523179 E + 03	1.9843530 E + 03
120	−1.1915861 E + 06	6.2559586 E + 06	1.2429380 E + 06	−1.7609510 E + 03	7.5590229 E + 03	2.1857932 E + 03
130	−1.2100640 E + 06	6.2635958 E + 06	1.2658512 E + 06	−1.9363541 E + 03	7.7260386 E + 03	2.3988928 E + 03
140	−1.2303493 E + 06	6.2714329 E + 06	1.2909590 E + 06	−2.1226160 E + 03	7.9600243 E + 03	2.6249870 E + 03
150	−1.2525568 E + 06	6.2795407 E + 06	1.3183993 E + 06	−2.3210565 E + 03	8.2688256 E + 03	2.8656573 E + 03
160	−1.2768161 E + 06	6.2879985 E + 06	1.3483269 E + 06	−2.5332536 E + 03	8.6617746 E + 03	3.1227952 E + 03
170	−1.3032739 E + 06	6.2968959 E + 06	1.3809175 E + 06	−2.7469620 E + 03	9.1178683 E + 03	3.3815571 E + 03