Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-14 S/C Mass (kg) : 1651.851 Fuel Mass (kg) : 39.673 Oxidizer Mass (kg) : 61.267 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/075 06:00:00.000 Semimajor Axis (km) : 42165.55870 Eccentricity : 0.000201 Inclination (deg) : 0.132297 Right Ascension of Ascending Node (deg) : 131.431098 Argument of Perigee (deg) : 260.241112 Mean Anomaly (deg) : 123.219158 Apogee Ht (km): 35795.90359 Perigee Ht (km): 35778.93380 West Longitude (deg) : 108.425 Longitude Drift Rate (deg/day) : 0.002000 WEST Comments: GOES-14 data propagated from OATS orbit epoch 24/074 00:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/074. ============================================================= Spacecraft : GOES-16 S/C Mass (kg) : 3369.88305 Fuel Mass (kg) : 464.537888 Oxidizer Mass (kg) : 34.9351702 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/074 08:00:00.000 Semimajor Axis (km): 42166.7846 Eccentricity : 4.1195e-05 Inclination (deg) : 0.06445084 Right Ascension of Ascending Node (deg) : 257.458569 Argument of Perigee (deg) : 50.1836539 Mean Anomaly (deg) : 269.585984 Apogee Ht (km) : 35790.3847 Perigee Ht (km) : 35786.9106 West Longitude (deg) : 75.2099317 Longitude Drift Rate (deg/day) : 0.00014320 WEST Comments: GOES-16 data propagated from orbit epoch 24/074 08:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/074. ============================================================= Spacecraft : GOES-17 S/C Mass (kg) : 3513.10423 Fuel Mass (kg) : 591.217343 Oxidizer Mass (kg) : 29.1868926 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/074 11:30:00.000 Semimajor Axis (km): 42166.1509 Eccentricity : 0.00014862 Inclination (deg) : 0.00428638 Right Ascension of Ascending Node (deg) : 310.562413 Argument of Perigee (deg) : 341.482298 Mean Anomaly (deg) : 308.334710 Apogee Ht (km) : 35794.2810 Perigee Ht (km) : 35781.7468 West Longitude (deg) : 104.711116 Longitude Drift Rate (deg/day) : 0.00247467 EAST Comments: GOES-17 data propagated from orbit epoch 24/074 11:30:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/070. ============================================================= Spacecraft : GOES-18 S/C Mass (kg) : 3740.73039 Fuel Mass (kg) : 806.829587 Oxidizer Mass (kg) : 34.3008065 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/074 10:00:00.000 Semimajor Axis (km): 42166.1740 Eccentricity : 9.7476e-05 Inclination (deg) : 0.00092354 Right Ascension of Ascending Node (deg) : 166.753535 Argument of Perigee (deg) : 89.9481092 Mean Anomaly (deg) : 288.804468 Apogee Ht (km) : 35792.1472 Perigee Ht (km) : 35783.9268 West Longitude (deg) : 137.020035 Longitude Drift Rate (deg/day) : 0.00349768 EAST Comments: GOES-18 data propagated from orbit epoch 24/074 10:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/074. =============================================================