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

S/C Mass (kg) :                               1629.470
Fuel Mass (kg) :                               31.275
Oxidizer Mass (kg) :                           47.284

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/077 06:00:00.000
Semimajor Axis (km) :                         42166.37745
Eccentricity :                                0.000071
Inclination (deg) :                           0.496416
Right Ascension of Ascending Node (deg) :     92.051747
Argument of Perigee (deg) :                   146.162513
Mean Anomaly (deg) :                          279.720176
Apogee Ht (km):                               35791.24556
Perigee Ht (km):                              35785.22933

West Longitude (deg) :                        108.130
Longitude Drift Rate (deg/day) :              0.007000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 25/073 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/044.
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Spacecraft :                                  GOES-16

S/C Mass (kg) :                               3312.97999
Fuel Mass (kg) :                              414.484817
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/077 10:00:00.000
Semimajor Axis (km):                          42167.1127
Eccentricity :                                0.00015418
Inclination (deg) :                           0.08566657
Right Ascension of Ascending Node (deg) :     269.384262
Argument of Perigee (deg) :                   108.433655
Mean Anomaly (deg) :                          233.022679
Apogee Ht (km) :                              35795.4700
Perigee Ht (km) :                             35782.4673

West Longitude (deg) :                        75.3766192
Longitude Drift Rate (deg/day) :              1895.14565 WEST

Comments:
GOES-16 data propagated from orbit epoch 25/077 10:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/076.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3475.21372
Fuel Mass (kg) :                              553.326823
Oxidizer Mass (kg) :                          29.1868927

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/077 10:00:00.000
Semimajor Axis (km):                          42166.6492
Eccentricity :                                0.00015346
Inclination (deg) :                           0.04916878
Right Ascension of Ascending Node (deg) :     267.881372
Argument of Perigee (deg) :                   190.636808
Mean Anomaly (deg) :                          123.296665
Apogee Ht (km) :                              35794.9762
Perigee Ht (km) :                             35782.0341

West Longitude (deg) :                        104.403632
Longitude Drift Rate (deg/day) :              364.981862 WEST

Comments:
GOES-17 data propagated from orbit epoch 25/077 10:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/076.
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Spacecraft :                                  GOES-18

S/C Mass (kg) :                               3701.08721
Fuel Mass (kg) :                              767.218345
Oxidizer Mass (kg) :                          34.2688602

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/077 00:00:00.000
Semimajor Axis (km):                          42166.5780
Eccentricity :                                0.00010326
Inclination (deg) :                           0.00400980
Right Ascension of Ascending Node (deg) :     241.523431
Argument of Perigee (deg) :                   165.008678
Mean Anomaly (deg) :                          352.271414
Apogee Ht (km) :                              35792.7880
Perigee Ht (km) :                             35784.0800

West Longitude (deg) :                        137.004206
Longitude Drift Rate (deg/day) :              390.537129 WEST

Comments:
GOES-18 data propagated from orbit epoch 25/077 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/076.
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Spacecraft :                                  GOES-19

S/C Mass (kg) :                               3924.84807
Fuel Mass (kg) :                              961.235069
Oxidizer Mass (kg) :                          33.0130000

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/077 13:00:00.000
Semimajor Axis (km):                          42164.7766
Eccentricity :                                0.00018245
Inclination (deg) :                           0.01053469
Right Ascension of Ascending Node (deg) :     260.945407
Argument of Perigee (deg) :                   109.139349
Mean Anomaly (deg) :                          271.793575
Apogee Ht (km) :                              35794.3256
Perigee Ht (km) :                             35778.9396

West Longitude (deg) :                        89.4634464
Longitude Drift Rate (deg/day) :              265.166991 WEST

Comments:
GOES-19 data propagated from orbit epoch 25/077 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/077.
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