##SATELLITE ORBIT ERROR  (R)@(T0=2026/04/28 00:00:00)
#!   TIME,   SAT,   CLK(ns)
      900,   R02,   -1.8638
      900,   R03,    0.9762
      900,   R04,    0.6112
      900,   R05,    0.5932
      900,   R07,    1.1052
      900,   R08,    1.4152
      900,   R09,   -2.0418
      900,   R12,    1.2042
      900,   R14,   -2.4118
      900,   R21,    0.0822
      900,   R24,    0.3302
     1800,   R02,   -1.9685
     1800,   R03,    0.8635
     1800,   R07,    0.9245
     1800,   R08,    1.2965
     1800,   R12,    1.1635
     1800,   R14,   -2.5555
     1800,   R21,    0.0165
     1800,   R24,    0.2595
     2700,   R02,   -2.0718
     2700,   R03,    0.4672
     2700,   R04,    0.4642
     2700,   R05,    0.4842
     2700,   R07,    0.9912
     2700,   R08,    1.3802
     2700,   R09,   -2.2068
     2700,   R12,    1.0892
     2700,   R15,    0.8242
     2700,   R16,   -0.5678
     2700,   R18,   -0.9728
     2700,   R21,   -0.1228
     2700,   R24,    0.2412
     3600,   R02,   -2.0117
     3600,   R03,    0.6053
     3600,   R07,    0.9103
     3600,   R08,    1.3263
     3600,   R09,   -2.1947
     3600,   R12,    1.0443
     3600,   R18,   -0.9997
     3600,   R24,    0.3913
     6300,   R02,   -1.7425
     6300,   R03,    0.7945
     6300,   R08,    1.6105
     6300,   R09,   -1.9595
     6300,   R12,    1.1405
     6300,   R14,   -2.2065
     6300,   R21,    0.0205
     7200,   R02,   -1.0062
     7200,   R03,    1.4728
     7200,   R09,   -1.2092
     7200,   R21,    0.7428
     8100,   R03,    0.5902
     8100,   R04,    0.3422
     8100,   R05,    0.3272
     8100,   R07,    0.7302
     8100,   R08,    1.5402
     8100,   R09,   -2.1298
     8100,   R12,    0.8582
     8100,   R14,   -2.2098
     8100,   R15,    0.8942
     8100,   R16,   -0.3258
     8100,   R18,   -0.9338
     8100,   R21,   -0.1338
     8100,   R24,    0.4502
     9000,   R03,    0.7521
     9000,   R04,    0.4161
     9000,   R05,    0.4621
     9000,   R08,    1.5501
     9000,   R09,   -1.9069
     9000,   R12,    0.8651
     9000,   R14,   -2.0799
     9000,   R15,    1.0631
     9000,   R16,   -0.2439
     9000,   R18,   -0.8179
     9000,   R21,   -0.0599
     9900,   R02,   -1.5628
     9900,   R03,    0.6572
     9900,   R04,    0.6012
     9900,   R05,    0.6302
     9900,   R07,    1.0072
     9900,   R08,    1.7472
     9900,   R09,   -1.6708
     9900,   R14,   -2.0268
     9900,   R15,    1.2642
     9900,   R18,   -0.6258
    10800,   R02,   -2.0476
    10800,   R03,    0.2354
    10800,   R04,   -0.0346
    10800,   R08,    1.1324
    10800,   R15,    0.7144
    13500,   R05,    0.4017
    13500,   R07,    0.6527
    13500,   R09,   -1.6723
    13500,   R12,    0.6927
    13500,   R16,   -0.0243
    13500,   R21,   -0.0503
    14400,   R05,    0.2898
    14400,   R07,    0.7608
    14400,   R09,   -1.7132
    14400,   R12,    0.6798
    14400,   R16,    0.0518
    14400,   R21,   -0.0692
    15300,   R02,   -0.9957
    15300,   R09,   -1.3067
    15300,   R12,    1.0833
    15300,   R14,   -1.7567
    15300,   R15,    1.5063
    15300,   R16,    0.4263
    15300,   R18,   -0.2457
    15300,   R21,    0.3723
    15300,   R24,    0.9163
    16200,   R02,   -0.9180
    16200,   R09,   -1.1360
    16200,   R16,    0.6050
    16200,   R21,    0.3940
    16200,   R24,    1.0550
    17100,   R03,    0.7309
    17100,   R04,    0.3669
    17100,   R05,    0.2569
    17100,   R08,    1.3239
    17100,   R09,   -1.6931
    17100,   R14,   -2.4071
    17100,   R15,    0.8789
    17100,   R16,    0.0939
    17100,   R24,    0.4489
    18000,   R03,    0.5736
    18000,   R04,    0.1556
    18000,   R08,    1.0066
    18000,   R09,   -1.9534
    18000,   R24,    0.2176
    18900,   R02,   -1.2662
    18900,   R04,    0.6527
    18900,   R05,    0.4107
    18900,   R07,    0.9858
    18900,   R08,    1.4578
    18900,   R12,    0.7818
    18900,   R14,   -2.3643
    18900,   R15,    0.9627
    18900,   R16,    0.1787
    18900,   R18,   -0.3933
    18900,   R21,    0.0628
