Random Error Estimation and Propagation Analysis for Satellites’ Initial Positions

Table 1

Satellite’s expected initial six orbital elements.

	(km)		(°)	(°)	(°)	(°)
	6904.14	0	97.5	0	0	60
	26553.4	0.740969	63.4	240.377	270.0	0
	42167.2	0.002100	54.8	211.400	167.1	201.3
Standard deviation	2	0.0002	0.05	0.03	0.03	0.03