Content-Length: 5943 | pFad | https://noaasis.noaa.gov/cemscs/navsum.txt

Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-14 S/C Mass (kg) : 1629.275 Fuel Mass (kg) : 31.202 Oxidizer Mass (kg) : 47.161 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 25/259 06:00:00.000 Semimajor Axis (km) : 42166.62625 Eccentricity : 0.000368 Inclination (deg) : 0.974446 Right Ascension of Ascending Node (deg) : 87.725033 Argument of Perigee (deg) : 113.703982 Mean Anomaly (deg) : 135.683277 Apogee Ht (km): 35804.01096 Perigee Ht (km): 35772.96154 West Longitude (deg) : 108.305 Longitude Drift Rate (deg/day) : 0.006000 WEST Comments: GOES-14 data propagated from OATS orbit epoch 25/246 00:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 25/212. ============================================================= Spacecraft : GOES-16 S/C Mass (kg) : 3289.45544 Fuel Mass (kg) : 390.960271 Oxidizer Mass (kg) : 34.9351702 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 25/259 10:00:00.000 Semimajor Axis (km): 42165.2003 Eccentricity : 0.00024724 Inclination (deg) : 0.12225376 Right Ascension of Ascending Node (deg) : 95.8019283 Argument of Perigee (deg) : 118.909850 Mean Anomaly (deg) : 186.235940 Apogee Ht (km) : 35797.4812 Perigee Ht (km) : 35776.6313 West Longitude (deg) : 104.661051 Longitude Drift Rate (deg/day) : 0.00086420 WEST Comments: GOES-16 data propagated from orbit epoch 25/259 10:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 25/258. ============================================================= Spacecraft : GOES-17 S/C Mass (kg) : 3458.46450 Fuel Mass (kg) : 536.577611 Oxidizer Mass (kg) : 29.1868927 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 25/259 12:00:00.000 Semimajor Axis (km): 42165.7983 Eccentricity : 0.00025179 Inclination (deg) : 0.23838090 Right Ascension of Ascending Node (deg) : 96.9478089 Argument of Perigee (deg) : 137.760914 Mean Anomaly (deg) : 211.489927 Apogee Ht (km) : 35798.2714 Perigee Ht (km) : 35777.0373 West Longitude (deg) : 89.4940236 Longitude Drift Rate (deg/day) : 0.00179088 EAST Comments: GOES-17 data propagated from orbit epoch 25/259 12:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 25/258. ============================================================= Spacecraft : GOES-18 S/C Mass (kg) : 3679.47518 Fuel Mass (kg) : 745.621154 Oxidizer Mass (kg) : 34.2540284 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 25/259 10:00:00.000 Semimajor Axis (km): 42165.7424 Eccentricity : 0.00009104 Inclination (deg) : 0.02334322 Right Ascension of Ascending Node (deg) : 90.1473358 Argument of Perigee (deg) : 175.912142 Mean Anomaly (deg) : 102.549437 Apogee Ht (km) : 35791.4373 Perigee Ht (km) : 35783.7596 West Longitude (deg) : 136.998207 Longitude Drift Rate (deg/day) : 0.00237976 WEST Comments: GOES-18 data propagated from orbit epoch 25/259 10:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 25/258. ============================================================= Spacecraft : GOES-19 S/C Mass (kg) : 3887.85415 Fuel Mass (kg) : 927.755155 Oxidizer Mass (kg) : 29.4989954 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 25/259 13:00:00.000 Semimajor Axis (km): 42166.3982 Eccentricity : 0.00005983 Inclination (deg) : 0.00448327 Right Ascension of Ascending Node (deg) : 308.278048 Argument of Perigee (deg) : 269.608811 Mean Anomaly (deg) : 257.650345 Apogee Ht (km) : 35790.7772 Perigee Ht (km) : 35785.7312 West Longitude (deg) : 75.1954283 Longitude Drift Rate (deg/day) : 0.00226788 EAST Comments: GOES-19 data propagated from orbit epoch 25/259 13:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 25/259. =============================================================

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