##SATELLITE ORBIT ERROR  (J)@(T0=2025/07/15 00:00:00)
#!   TIME,   SAT,      R(m),      A(m),      C(m)
      300,   J02,   -0.2796,   -0.4220,   -0.0216
      300,   J03,   -0.2192,   -0.0190,    0.0371
      300,   J04,   -0.3776,    0.1183,    0.2042
      600,   J02,   -0.2719,   -0.4078,   -0.0226
      600,   J03,   -0.2163,   -0.0222,    0.0166
      600,   J04,   -0.3725,    0.1225,    0.1777
      900,   J02,   -0.2765,   -0.3661,   -0.0227
      900,   J03,   -0.2176,   -0.0312,    0.0049
      900,   J04,   -0.3697,    0.1441,    0.1604
     1200,   J02,   -0.2805,   -0.3164,   -0.0280
     1200,   J03,   -0.2173,   -0.0261,   -0.0128
     1200,   J04,   -0.3659,    0.1579,    0.1402
     1500,   J02,   -0.2842,   -0.2832,   -0.0288
     1500,   J03,   -0.2220,   -0.0137,   -0.0226
     1500,   J04,   -0.3625,    0.1641,    0.1267
     1800,   J02,   -0.2906,   -0.2519,   -0.0277
     1800,   J03,   -0.2255,   -0.0093,   -0.0237
     1800,   J04,   -0.3595,    0.1814,    0.1235
     2100,   J02,   -0.2931,   -0.2291,   -0.0205
     2100,   J03,   -0.2304,   -0.0005,   -0.0157
     2100,   J04,   -0.3616,    0.1945,    0.1257
     2400,   J02,   -0.2998,   -0.1906,   -0.0126
     2400,   J03,   -0.2346,    0.0145,   -0.0145
     2400,   J04,   -0.3669,    0.1856,    0.1183
     2700,   J02,   -0.2955,   -0.2039,   -0.0097
     2700,   J03,   -0.2369,    0.0152,   -0.0084
     2700,   J04,   -0.3756,    0.1795,    0.1190
     3000,   J02,   -0.2863,   -0.2175,   -0.0124
     3000,   J03,   -0.2350,   -0.0026,   -0.0084
     3000,   J04,   -0.3791,    0.1833,    0.1176
     3300,   J02,   -0.2872,   -0.2100,   -0.0071
     3300,   J03,   -0.2274,   -0.0173,   -0.0031
     3300,   J04,   -0.3813,    0.2160,    0.1171
