Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-14 S/C Mass (kg) : 1629.666 Fuel Mass (kg) : 31.347 Oxidizer Mass (kg) : 47.407 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/338 06:00:00.000 Semimajor Axis (km) : 42165.91820 Eccentricity : 0.000263 Inclination (deg) : 0.210392 Right Ascension of Ascending Node (deg) : 85.486006 Argument of Perigee (deg) : 113.563222 Mean Anomaly (deg) : 215.005570 Apogee Ht (km): 35798.86299 Perigee Ht (km): 35776.69342 West Longitude (deg) : 108.524 Longitude Drift Rate (deg/day) : 0.007000 EAST Comments: GOES-14 data propagated from OATS orbit epoch 24/327 00:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/277. ============================================================= Spacecraft : GOES-16 S/C Mass (kg) : 3331.74233 Fuel Mass (kg) : 433.247159 Oxidizer Mass (kg) : 34.9351702 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/338 10:00:00.000 Semimajor Axis (km): 42165.4840 Eccentricity : 0.00009196 Inclination (deg) : 0.04425213 Right Ascension of Ascending Node (deg) : 277.717711 Argument of Perigee (deg) : 52.8921169 Mean Anomaly (deg) : 176.921496 Apogee Ht (km) : 35791.2175 Perigee Ht (km) : 35783.4624 West Longitude (deg) : 75.1926589 Longitude Drift Rate (deg/day) : 0.00074650 EAST Comments: GOES-16 data propagated from orbit epoch 24/338 10:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/338. ============================================================= Spacecraft : GOES-17 S/C Mass (kg) : 3490.05270 Fuel Mass (kg) : 568.165812 Oxidizer Mass (kg) : 29.1868927 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/338 04:00:00.000 Semimajor Axis (km): 42165.3147 Eccentricity : 0.00028486 Inclination (deg) : 0.01031368 Right Ascension of Ascending Node (deg) : 292.512534 Argument of Perigee (deg) : 317.806228 Mean Anomaly (deg) : 137.475238 Apogee Ht (km) : 35799.1820 Perigee Ht (km) : 35775.1594 West Longitude (deg) : 104.688339 Longitude Drift Rate (deg/day) : 0.00371745 EAST Comments: GOES-17 data propagated from orbit epoch 24/338 04:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/337. ============================================================= Spacecraft : GOES-18 S/C Mass (kg) : 3714.27039 Fuel Mass (kg) : 780.401533 Oxidizer Mass (kg) : 34.2688602 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/338 07:00:00.000 Semimajor Axis (km): 42166.1979 Eccentricity : 0.00003665 Inclination (deg) : 0.00705791 Right Ascension of Ascending Node (deg) : 31.1806059 Argument of Perigee (deg) : 31.0803441 Mean Anomaly (deg) : 338.344933 Apogee Ht (km) : 35789.5993 Perigee Ht (km) : 35786.5086 West Longitude (deg) : 136.999763 Longitude Drift Rate (deg/day) : 0.00262431 WEST Comments: GOES-18 data propagated from orbit epoch 24/338 07:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/337. =============================================================
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