Below are the weekly GOES element sets:
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Spacecraft :                                  GOES-14

S/C Mass (kg) :                               1814.361
Fuel Mass (kg) :                              100.206
Oxidizer Mass (kg) :                          163.245

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             20/184 06:00:00.000
Semimajor Axis (km) :                         42167.17047
Eccentricity :                                0.000923
Inclination (deg) :                           0.357677
Right Ascension of Ascending Node (deg) :     94.206517
Argument of Perigee (deg) :                   121.050647
Mean Anomaly (deg) :                          51.151537
Apogee Ht (km):                               35827.95796
Perigee Ht (km):                              35750.10297

West Longitude (deg) :                        104.245
Longitude Drift Rate (deg/day) :              0.002000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 20/177 15:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 20/063.
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Spacecraft :                                  GOES-15

S/C Mass (kg) :                               1850.047
Fuel Mass (kg) :                              108.076
Oxidizer Mass (kg) :                          182.789

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             20/184 06:00:00.000
Semimajor Axis (km) :                         42168.89325
Eccentricity :                                0.000238
Inclination (deg) :                           0.081071
Right Ascension of Ascending Node (deg) :     282.083830
Argument of Perigee (deg) :                   150.051375
Mean Anomaly (deg) :                          170.448813
Apogee Ht (km):                               35800.77453
Perigee Ht (km):                              35780.73197

West Longitude (deg) :                        128.148
Longitude Drift Rate (deg/day) :              0.022000 WEST

Comments:
GOES-15 data propagated from OATS orbit epoch 20/177 15:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 20/168.
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Spacecraft :                                  GOES-16

S/C Mass (kg) :                               3604.33612
Fuel Mass (kg) :                              698.990953
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             20/184 10:00:00.000
Semimajor Axis (km):                          42164.9616
Eccentricity :                                0.00012685
Inclination (deg) :                           0.01055794
Right Ascension of Ascending Node (deg) :     248.796490
Argument of Perigee (deg) :                   234.027489
Mean Anomaly (deg) :                          232.886274
Apogee Ht (km) :                              35792.1734
Perigee Ht (km) :                             35781.4758

West Longitude (deg) :                        75.2073126
Longitude Drift Rate (deg/day) :              0.00211802 WEST

Comments:
GOES-16 data propagated from orbit epoch 20/184 10:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 20/183.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3701.12910
Fuel Mass (kg) :                              779.242207
Oxidizer Mass (kg) :                          29.1868926

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             20/184 09:00:00.000
Semimajor Axis (km):                          42166.3763
Eccentricity :                                4.1636e-05
Inclination (deg) :                           0.03414827
Right Ascension of Ascending Node (deg) :     274.593313
Argument of Perigee (deg) :                   274.546442
Mean Anomaly (deg) :                          89.5256509
Apogee Ht (km) :                              35789.9950
Perigee Ht (km) :                             35786.4837

West Longitude (deg) :                        137.194729
Longitude Drift Rate (deg/day) :              0.00203674 EAST

Comments:
GOES-17 data propagated from orbit epoch 20/184 09:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 20/183.
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