Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-14 S/C Mass (kg) : 1629.774 Fuel Mass (kg) : 31.387 Oxidizer Mass (kg) : 47.475 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/268 06:00:00.000 Semimajor Axis (km) : 42164.85967 Eccentricity : 0.000371 Inclination (deg) : 0.051135 Right Ascension of Ascending Node (deg) : 125.716817 Argument of Perigee (deg) : 48.468485 Mean Anomaly (deg) : 170.953837 Apogee Ht (km): 35802.35495 Perigee Ht (km): 35771.08439 West Longitude (deg) : 108.421 Longitude Drift Rate (deg/day) : 0.010000 EAST Comments: GOES-14 data propagated from OATS orbit epoch 24/264 18:56:27.804 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/267. ============================================================= Spacecraft : GOES-16 S/C Mass (kg) : 3341.65834 Fuel Mass (kg) : 443.163169 Oxidizer Mass (kg) : 34.9351702 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/268 08:00:00.000 Semimajor Axis (km): 42165.9608 Eccentricity : 0.00004543 Inclination (deg) : 0.08065145 Right Ascension of Ascending Node (deg) : 271.521772 Argument of Perigee (deg) : 5.65070859 Mean Anomaly (deg) : 131.279939 Apogee Ht (km) : 35789.7326 Perigee Ht (km) : 35785.9010 West Longitude (deg) : 75.1972445 Longitude Drift Rate (deg/day) : 0.00141808 EAST Comments: GOES-16 data propagated from orbit epoch 24/268 08:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/267. ============================================================= Spacecraft : GOES-17 S/C Mass (kg) : 3496.89084 Fuel Mass (kg) : 575.003944 Oxidizer Mass (kg) : 29.1868927 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/268 11:30:00.000 Semimajor Axis (km): 42166.2390 Eccentricity : 0.00022914 Inclination (deg) : 0.00259433 Right Ascension of Ascending Node (deg) : 18.1432172 Argument of Perigee (deg) : 195.519840 Mean Anomaly (deg) : 217.928436 Apogee Ht (km) : 35797.7568 Perigee Ht (km) : 35778.4332 West Longitude (deg) : 104.701368 Longitude Drift Rate (deg/day) : 0.00074242 EAST Comments: GOES-17 data propagated from orbit epoch 24/268 11:30:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/267. ============================================================= Spacecraft : GOES-18 S/C Mass (kg) : 3722.51293 Fuel Mass (kg) : 788.612119 Oxidizer Mass (kg) : 34.3008065 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/268 10:00:00.000 Semimajor Axis (km): 42165.8373 Eccentricity : 0.00004218 Inclination (deg) : 0.00269637 Right Ascension of Ascending Node (deg) : 34.8916853 Argument of Perigee (deg) : 243.576430 Mean Anomaly (deg) : 98.2698137 Apogee Ht (km) : 35789.4720 Perigee Ht (km) : 35785.9146 West Longitude (deg) : 136.993540 Longitude Drift Rate (deg/day) : 0.00251954 WEST Comments: GOES-18 data propagated from orbit epoch 24/268 10:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/267. ============================================================= Fuel and oxidizer remaining are estimates after the last maneuver on 24/253. =============================================================