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

Table 4

Observation of spacecraft 0.

Time (s)	Observation position (m)			Observation velocity (m/s)
	x	y	z	x	y	z
50	−1.1045785 E + 06	6.2026543 E + 06	1.1340530 E + 06	−7.4903883 E + 02	7.8251039 E + 02	9.5203116 E + 02
60	−1.1131004 E + 06	6.2103568 E + 06	1.1442698 E + 06	−9.3028087 E + 02	7.8195722 E + 02	1.1023444 E + 03
70	−1.1233125 E + 06	6.2184561 E + 06	1.1564104 E + 06	−1.0912921 E + 03	8.3312097 E + 02	1.3019919 E + 03
80	−1.1352505 E + 06	6.2270647 E + 06	1.1706173 E + 06	−1.2918543 E + 03	8.7182984 E + 02	1.5207654 E + 03
90	−1.1490173 E + 06	6.2361108 E + 06	1.1870506 E + 06	−1.4794826 E + 03	9.3487786 E + 02	1.7629851 E + 03
100	−1.1646975 E + 06	6.2455991 E + 06	1.2058790 E + 06	−1.6627190 E + 03	9.6992430 E + 02	1.9973859 E + 03
110	−1.1824947 E + 06	6.2554542 E + 06	1.2271690 E + 06	−1.8905454 E + 03	1.0071563 E + 03	2.2702085 E + 03
120	−1.2025020 E + 06	6.2656861 E + 06	1.2511673 E + 06	−2.1194352 E + 03	1.0520625 E + 03	2.5351808 E + 03
130	−1.2248703 E + 06	6.2762167 E + 06	1.2780546 E + 06	−2.3455157 E + 03	1.0697871 E + 03	2.8286792 E + 03
140	−1.2497717 E + 06	6.2871388 E + 06	1.3080340 E + 06	−2.6280271 E + 03	1.1075056 E + 03	3.1616176 E + 03
150	−1.2773908 E + 06	6.2983536 E + 06	1.3413011 E + 06	−2.8949518 E + 03	1.1338597 E + 03	3.4867523 E + 03
160	−1.3079042 E + 06	6.3099141 E + 06	1.3781158 E + 06	−3.2136372 E + 03	1.1845338 E + 03	3.8839258 E + 03
170	−1.3416105 E + 06	6.3218029 E + 06	1.4187374 E + 06	−3.5230289 E + 03	1.1994513 E + 03	4.2283819 E + 03