Mathematical Problems in Engineering / 2009 / Article / Tab 2

Research Article

The Impact on Geographic Location Accuracy due to Different Satellite Orbit Ephemerides

Table 2

Location errors for a simulated ideal case.

DPCDateTimeInternetCCS
no.Nov. 2008(UTC)TLE error (km)TLE error (km)

1092116:29:501.070.59
1092118:14:200.670.42
1092208:31:300.990.28
1092210:19:500.830.20
1092217:27:200.880.32
1092219:13:500.850.29
1092221:02:000.610.66
325902109:16:400.590.38
325902111:02:500.490.27
325902118:09:400.940.23
325902208:29:500.640.46
325902210:15:401.040.32
325902215:36:101.250.51
325902217:22:301.280.17
325902219:09:400.240.42

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