Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-16 S/C Mass (kg) : 3260.67963 Fuel Mass (kg) : 362.184455 Oxidizer Mass (kg) : 34.9351702 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/222 09:00:00.000 Semimajor Axis (km): 42165.7171 Eccentricity : 0.00014446 Inclination (deg) : 0.49037673 Right Ascension of Ascending Node (deg) : 85.1159054 Argument of Perigee (deg) : 137.229717 Mean Anomaly (deg) : 126.792111 Apogee Ht (km) : 35793.6643 Perigee Ht (km) : 35781.4818 West Longitude (deg) : 104.720481 Longitude Drift Rate (deg/day) : 0.00079182 WEST Comments: GOES-16 data propagated from orbit epoch 26/222 09:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/221. ============================================================= Spacecraft : GOES-17 S/C Mass (kg) : 3456.15128 Fuel Mass (kg) : 534.264385 Oxidizer Mass (kg) : 29.1868927 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/222 12:00:00.000 Semimajor Axis (km): 42164.6570 Eccentricity : 0.00011344 Inclination (deg) : 1.09520971 Right Ascension of Ascending Node (deg) : 84.8683499 Argument of Perigee (deg) : 103.590261 Mean Anomaly (deg) : 221.043245 Apogee Ht (km) : 35791.2961 Perigee Ht (km) : 35781.7298 West Longitude (deg) : 89.4844495 Longitude Drift Rate (deg/day) : 0.00218146 EAST Comments: GOES-17 data propagated from orbit epoch 26/222 12:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/221. ============================================================= Spacecraft : GOES-18 S/C Mass (kg) : 3636.59468 Fuel Mass (kg) : 702.755382 Oxidizer Mass (kg) : 34.2392986 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/222 08:00:00.000 Semimajor Axis (km): 42167.1240 Eccentricity : 0.00010760 Inclination (deg) : 0.00724595 Right Ascension of Ascending Node (deg) : 39.3963470 Argument of Perigee (deg) : 221.147833 Mean Anomaly (deg) : 41.2745105 Apogee Ht (km) : 35793.5171 Perigee Ht (km) : 35784.4428 West Longitude (deg) : 137.000825 Longitude Drift Rate (deg/day) : 0.00179556 WEST Comments: GOES-18 data propagated from orbit epoch 26/222 08:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/221. ============================================================= Spacecraft : GOES-19 S/C Mass (kg) : 3843.26133 Fuel Mass (kg) : 882.926828 Oxidizer Mass (kg) : 29.7345026 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/222 10:00:00.000 Semimajor Axis (km): 42164.2944 Eccentricity : 0.00008468 Inclination (deg) : 0.01285569 Right Ascension of Ascending Node (deg) : 58.4822405 Argument of Perigee (deg) : 166.952149 Mean Anomaly (deg) : 168.279742 Apogee Ht (km) : 35789.7209 Perigee Ht (km) : 35782.5800 West Longitude (deg) : 75.1885868 Longitude Drift Rate (deg/day) : 0.00431704 EAST Comments: GOES-19 data propagated from orbit epoch 26/222 10:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/222. =========================================================================