Table 4
Test result of Spacecraft Ephemeris Generation by Hermite interpolation

Interpolation order	Interpolation interval (min)	Maximum distance error (m)	Mean distance error (m)	Standard deviation (m)	Data budget (byte/day)	Requirements satisfaction
6	30	140.61	47.98	35.20	7,296	no
	60	6,744.78	2,838.89	1,998.27	3,648	no
8	30	15.28	2.47	2.63	9,600	yes
	60	155.82	1.43	36.74	4,800	no
10	60	59.34	10.92	12.76	5,952	no
	90	220.33	41.40	47.69	4,464	no
12	60	84.38	6.94	11.13	7,104	no
	90	195.95	21.74	30.22	4,736	no