Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-16 S/C Mass (kg) : 3260.20207 Fuel Mass (kg) : 361.706898 Oxidizer Mass (kg) : 34.9351702 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/281 06:00:00.000 Semimajor Axis (km): 42167.1147 Eccentricity : 0.00019198 Inclination (deg) : 0.60561486 Right Ascension of Ascending Node (deg) : 86.2741686 Argument of Perigee (deg) : 168.822823 Mean Anomaly (deg) : 107.085102 Apogee Ht (km) : 35797.0659 Perigee Ht (km) : 35780.8756 West Longitude (deg) : 104.707764 Longitude Drift Rate (deg/day) : 0.00293371 WEST Comments: GOES-16 data propagated from orbit epoch 26/281 06:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/280. ============================================================= Spacecraft : GOES-17 S/C Mass (kg) : 3455.87821 Fuel Mass (kg) : 533.991316 Oxidizer Mass (kg) : 29.1868927 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/281 12:00:00.000 Semimajor Axis (km): 42164.4328 Eccentricity : 0.00014608 Inclination (deg) : 1.21193259 Right Ascension of Ascending Node (deg) : 84.9050077 Argument of Perigee (deg) : 154.152068 Mean Anomaly (deg) : 228.586843 Apogee Ht (km) : 35792.4484 Perigee Ht (km) : 35780.1292 West Longitude (deg) : 89.4954670 Longitude Drift Rate (deg/day) : 0.00024472 WEST Comments: GOES-17 data propagated from orbit epoch 26/281 12:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/280. ============================================================= Spacecraft : GOES-18 S/C Mass (kg) : 3630.19362 Fuel Mass (kg) : 696.369141 Oxidizer Mass (kg) : 34.2244786 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/281 08:00:00.000 Semimajor Axis (km): 42166.8118 Eccentricity : 0.00010521 Inclination (deg) : 0.00869797 Right Ascension of Ascending Node (deg) : 210.638893 Argument of Perigee (deg) : 110.994727 Mean Anomaly (deg) : 38.3375683 Apogee Ht (km) : 35793.1044 Perigee Ht (km) : 35784.2312 West Longitude (deg) : 137.001059 Longitude Drift Rate (deg/day) : 0.00122197 EAST Comments: GOES-18 data propagated from orbit epoch 26/281 08:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/280. ============================================================= Spacecraft : GOES-19 S/C Mass (kg) : 3836.78653 Fuel Mass (kg) : 876.452028 Oxidizer Mass (kg) : 29.7345026 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/281 12:00:00.000 Semimajor Axis (km): 42165.3200 Eccentricity : 0.00009728 Inclination (deg) : 0.00910188 Right Ascension of Ascending Node (deg) : 140.382693 Argument of Perigee (deg) : 109.898627 Mean Anomaly (deg) : 231.669970 Apogee Ht (km) : 35791.2779 Perigee Ht (km) : 35783.0740 West Longitude (deg) : 75.1891728 Longitude Drift Rate (deg/day) : 0.00404484 WEST Comments: GOES-19 data propagated from orbit epoch 26/281 12:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/281. =============================================================