##SATELLITE ORBIT ERROR  (J)@(T0=2025/07/15 00:00:00)
#!   TIME,   SAT,      R(m),      A(m),      C(m)
      300,   J02,   -0.2653,   -0.4021,   -0.0129
      300,   J03,   -0.3465,    0.0236,    0.0084
      300,   J04,   -0.5237,    0.1381,    0.1602
      600,   J02,   -0.2575,   -0.3901,   -0.0155
      600,   J03,   -0.3408,    0.0238,   -0.0126
      600,   J04,   -0.5256,    0.1347,    0.1335
      900,   J02,   -0.2622,   -0.3463,   -0.0136
      900,   J03,   -0.3384,    0.0210,   -0.0242
      900,   J04,   -0.5296,    0.1527,    0.1146
     1200,   J02,   -0.2669,   -0.2973,   -0.0191
     1200,   J03,   -0.3341,    0.0295,   -0.0432
     1200,   J04,   -0.5335,    0.1630,    0.0940
     1500,   J02,   -0.2706,   -0.2635,   -0.0206
     1500,   J03,   -0.3346,    0.0460,   -0.0530
     1500,   J04,   -0.5370,    0.1646,    0.0801
     1800,   J02,   -0.2777,   -0.2300,   -0.0188
     1800,   J03,   -0.3346,    0.0559,   -0.0549
     1800,   J04,   -0.5417,    0.1785,    0.0745
     2100,   J02,   -0.2796,   -0.2085,   -0.0110
     2100,   J03,   -0.3365,    0.0667,   -0.0470
     2100,   J04,   -0.5518,    0.1860,    0.0763
     2400,   J02,   -0.2869,   -0.1699,   -0.0043
     2400,   J03,   -0.3364,    0.0823,   -0.0445
     2400,   J04,   -0.5652,    0.1722,    0.0694
     2700,   J02,   -0.2825,   -0.1833,   -0.0012
     2700,   J03,   -0.3357,    0.0850,   -0.0386
     2700,   J04,   -0.5819,    0.1618,    0.0693
     3000,   J02,   -0.2741,   -0.1963,   -0.0035
     3000,   J03,   -0.3307,    0.0698,   -0.0374
     3000,   J04,   -0.5942,    0.1620,    0.0666
     3300,   J02,   -0.2741,   -0.1889,    0.0009
     3300,   J03,   -0.3195,    0.0564,   -0.0326
     3300,   J04,   -0.6047,    0.1911,    0.0665
