Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-14 S/C Mass (kg) : 1776.816 Fuel Mass (kg) : 86.249 Oxidizer Mass (kg) : 139.655 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 20/346 06:00:00.000 Semimajor Axis (km) : 42166.50012 Eccentricity : 0.001231 Inclination (deg) : 0.183775 Right Ascension of Ascending Node (deg) : 265.638308 Argument of Perigee (deg) : 318.455047 Mean Anomaly (deg) : 202.074342 Apogee Ht (km): 35840.25508 Perigee Ht (km): 35736.46516 West Longitude (deg) : 104.296 Longitude Drift Rate (deg/day) : 0.005000 WEST Comments: GOES-14 data propagated from OATS orbit epoch 20/344 14:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 20/233. ============================================================= Spacecraft : GOES-15 S/C Mass (kg) : 1849.041 Fuel Mass (kg) : 107.699 Oxidizer Mass (kg) : 182.161 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 20/346 06:00:00.000 Semimajor Axis (km) : 42168.16983 Eccentricity : 0.000239 Inclination (deg) : 0.287120 Right Ascension of Ascending Node (deg) : 96.209399 Argument of Perigee (deg) : 331.369091 Mean Anomaly (deg) : 334.688093 Apogee Ht (km): 35800.11998 Perigee Ht (km): 35779.93967 West Longitude (deg) : 128.156 Longitude Drift Rate (deg/day) : 0.019000 WEST Comments: GOES-15 data propagated from OATS orbit epoch 20/344 14:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 20/322. ============================================================= Spacecraft : GOES-16 S/C Mass (kg) : 3579.78723 Fuel Mass (kg) : 674.442064 Oxidizer Mass (kg) : 34.9351702 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 20/344 11:00:00.000 Semimajor Axis (km): 42165.9145 Eccentricity : 0.00013795 Inclination (deg) : 0.00906269 Right Ascension of Ascending Node (deg) : 268.274585 Argument of Perigee (deg) : 8.37063809 Mean Anomaly (deg) : 251.850646 Apogee Ht (km) : 35793.5945 Perigee Ht (km) : 35781.9604 West Longitude (deg) : 75.1697748 Longitude Drift Rate (deg/day) : 0.00688195 EAST Comments: GOES-16 data propagated from orbit epoch 20/344 11:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 20/344. ============================================================= Spacecraft : GOES-17 S/C Mass (kg) : 3680.23773 Fuel Mass (kg) : 758.350846 Oxidizer Mass (kg) : 29.1868926 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 20/344 09:00:00.000 Semimajor Axis (km): 42165.4791 Eccentricity : 4.8869e-05 Inclination (deg) : 0.04740471 Right Ascension of Ascending Node (deg) : 264.950884 Argument of Perigee (deg) : 45.8761226 Mean Anomaly (deg) : 125.516412 Apogee Ht (km) : 35789.4027 Perigee Ht (km) : 35785.2815 West Longitude (deg) : 137.220505 Longitude Drift Rate (deg/day) : 0.00089860 WEST Comments: GOES-17 data propagated from orbit epoch 20/344 09:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 20/343. =============================================================