ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 14504.3693 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 68.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1.748 ET - UTC (sec) : 68.18 UT1 - UTC (sec) : 0.00 Maneuvers contained within the current ephemeris are as follows: IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP ------------------------------------------------------------------------ 201/16:28:21.000 0.0 0.0 0.0 N/A 0.0 0.0 227.5 000/00:00:00.000 0.0 0.0 218.5 201/22:50:29.000 0.0 -0.0 0.0 N/A -0.0 0.0 227.4 000/00:00:58.000 0.0 -0.0 218.6 202/23:35:13.000 0.0 0.0 0.0 N/A 0.0 0.0 227.4 000/00:00:00.000 0.0 0.0 218.7 203/20:55:00.000 0.0 0.0 0.0 N/A 0.0 0.0 227.4 000/00:00:00.000 0.0 0.0 219.0 204/11:00:00.000 0.0 0.0 0.0 N/A 0.0 0.0 227.4 000/00:00:00.000 0.0 0.0 218.9 210/10:44:30.000 0.0 0.0 0.0 N/A 0.0 0.0 226.6 000/00:00:00.000 0.0 0.0 219.8 212/15:35:00.000 0.0 0.0 0.0 N/A 0.0 0.0 226.2 000/00:00:00.000 0.0 0.0 220.2 213/11:38:30.000 0.0 0.0 0.0 N/A 0.0 0.0 226.2 000/00:00:00.000 0.0 0.0 220.3 Coasting Arc #1 (Orbit 1994) --------------------------------------- Vector Time (GMT): 2019/198/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 916459.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3081042.45 A = 6786918.67 meter Y = 3051063.12 meter E = .0019199 Z = -5237519.30 I = 51.42552 XDOT = -6142.347222 Wp = 114.63320 YDOT = -4443.464481 meter/sec RA = 209.72267 deg ZDOT = 1019.950600 TA = 165.21486 MA = 165.15864 Ha = 227.916 n.mi Hp = 218.020 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -10108406.98 X = -3089490.89 Y = 10010049.61 feet Y = 3016562.23 meter Z = -17183462.28 Z = -5252505.64 XDOT = -20152.057816 XDOT = -6097.156871 YDOT = -14578.295540 feet/sec YDOT = -4511.899984 meter/sec ZDOT = 3346.294619 ZDOT = 990.223131 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13219805.73 X = 4029396.79 Y = 5026621.87 feet Y = 1532114.35 meter Z = -17251729.48 Z = -5258327.15 XDOT = -4688.314262 XDOT = -1428.998187 YDOT = 23407.362809 feet/sec YDOT = 7134.564184 meter/sec ZDOT = 3211.651629 ZDOT = 978.911417 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19198.51445789 .00016717 00000-0 10270-3 0 9008 2 25544 51.6396 210.8143 0006832 151.2501 208.9027 15.50961524 19955 Satellite: ISS Catalog Number: 25544 Epoch time: 19198.51445789 = yrday.fracday Element set: 900 Inclination: 51.6396 deg RA of node: 210.8143 deg Eccentricity: .0006832 Arg of perigee: 151.2501 deg Mean anomaly: 208.9027 deg Mean motion: 15.50961524 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1995 Checksum: 317 Coasting Arc #2 (Orbit 2010) --------------------------------------- Vector Time (GMT): 2019/199/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 916459.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3495406.93 A = 6787466.67 meter Y = -2838196.07 meter E = .0007925 Z = 5071881.60 I = 51.45671 XDOT = 6073.501239 Wp = 113.71566 YDOT = 4340.731403 meter/sec RA = 204.74260 deg ZDOT = -1757.593205 TA = 353.31714 MA = 353.32770 Ha = 227.723 n.mi Hp = 218.183 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 11467870.50 X = 3502248.84 Y = -9311666.91 feet Y = -2799070.34 meter Z = 16640031.51 Z = 5088876.88 XDOT = 19926.185167 XDOT = 6033.047765 YDOT = 14241.244760 feet/sec YDOT = 4408.423578 meter/sec ZDOT = -5766.381905 ZDOT = -1728.188794 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13250680.96 X = -4038807.56 Y = -6329100.28 feet Y = -1929109.77 meter Z = 16717409.70 Z = 5095466.48 XDOT = 3957.026354 XDOT = 1206.101633 YDOT = -23155.537327 feet/sec YDOT = -7057.807777 meter/sec ZDOT = -5633.170378 ZDOT = -1716.990331 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19199.54537797 .00016717 00000-0 10270-3 0 9014 2 25544 51.6390 205.6987 0006804 153.9299 206.2196 15.50991253 20119 Satellite: ISS Catalog Number: 25544 Epoch time: 19199.54537797 = yrday.fracday Element set: 901 Inclination: 51.6390 deg RA of node: 205.6987 deg Eccentricity: .0006804 Arg of perigee: 153.9299 deg Mean anomaly: 206.2196 deg Mean motion: 15.50991253 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2011 Checksum: 337 Coasting Arc #3 (Orbit 2025) --------------------------------------- Vector Time (GMT): 2019/200/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 916459.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3941758.94 A = 6788552.87 meter Y = 2682629.21 meter E = .0016915 Z = -4848049.24 I = 51.49056 XDOT = -5897.057764 Wp = 125.46358 YDOT = -4203.529710 meter/sec RA = 199.76644 deg ZDOT = 2465.169015 TA = 168.87390 MA = 168.83645 Ha = 227.768 n.mi Hp = 218.234 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12932279.99 X = -3947915.31 Y = 8801276.93 feet Y = 2638515.76 meter Z = -15905673.37 Z = -4867211.09 XDOT = -19347.302374 XDOT = -5861.588564 YDOT = -13791.107971 feet/sec YDOT = -4269.276678 meter/sec ZDOT = 8087.824853 ZDOT = 2436.609676 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13545862.39 X = 4128778.86 Y = 7644214.22 feet Y = 2329956.50 meter Z = -15992885.54 Z = -4874631.51 XDOT = -3289.044987 XDOT = -1002.500912 YDOT = 22502.515400 feet/sec YDOT = 6858.766694 meter/sec ZDOT = 7958.415419 ZDOT = 2425.725020 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19200.51186468 .00016717 00000-0 10270-3 0 9020 2 25544 51.6388 200.9040 0006705 157.0745 203.0706 15.50961095 20264 Satellite: ISS Catalog Number: 25544 Epoch time: 19200.51186468 = yrday.fracday Element set: 902 Inclination: 51.6388 deg RA of node: 200.9040 deg Eccentricity: .0006705 Arg of perigee: 157.0745 deg Mean anomaly: 203.0706 deg Mean motion: 15.50961095 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2026 Checksum: 288 Coasting Arc #4 (Orbit 2041) --------------------------------------- Vector Time (GMT): 2019/201/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 916459.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4352829.87 A = 6789670.42 meter Y = -2568586.05 meter E = .0010477 Z = 4523456.71 I = 51.52530 XDOT = 5680.133638 Wp = 106.43934 YDOT = 4084.013515 meter/sec RA = 194.79321 deg ZDOT = -3143.677213 TA = 15.14693 MA = 15.11559 Ha = 227.481 n.mi Hp = 218.483 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14280937.88 X = 4359257.05 Y = -8427119.58 feet Y = -2519874.09 meter Z = 14840737.25 Z = 4544616.08 XDOT = 18635.609048 XDOT = 5649.312786 YDOT = 13398.994472 feet/sec YDOT = 4147.360691 meter/sec ZDOT = -10313.901617 ZDOT = -3116.160345 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13959756.10 X = -4254933.66 Y = -8787469.02 feet Y = -2678420.56 meter Z = 14937021.49 Z = 4552804.15 XDOT = 2769.112646 XDOT = 844.025535 YDOT = -21736.123557 feet/sec YDOT = -6625.170460 meter/sec ZDOT = -10189.195531 ZDOT = -3105.666798 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19201.54278260 .00016717 00000-0 10270-3 0 9037 2 25544 51.6376 195.7890 0006626 161.9077 198.2311 15.50996805 20421 Satellite: ISS Catalog Number: 25544 Epoch time: 19201.54278260 = yrday.fracday Element set: 903 Inclination: 51.6376 deg RA of node: 195.7890 deg Eccentricity: .0006626 Arg of perigee: 161.9077 deg Mean anomaly: 198.2311 deg Mean motion: 15.50996805 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2042 Checksum: 322 Coasting Arc #5 (Orbit 2044) --------------------------------------- Vector Time (GMT): 2019/201/16:28:21.000 Vector Time (MET): N/A Weight (LBS) : 916459.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 167044.59 A = 6786624.45 meter Y = -4271645.05 meter E = .0009124 Z = 5267859.92 I = 51.52349 XDOT = 7527.234909 Wp = 149.55835 YDOT = 1240.869243 meter/sec RA = 193.89770 deg ZDOT = 759.235183 TA = 293.12618 MA = 293.22230 Ha = 227.487 n.mi Hp = 218.529 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 548046.56 X = 189211.13 Y = -14014583.48 feet Y = -4269653.52 meter Z = 17283004.99 Z = 5268724.83 XDOT = 24695.652589 XDOT = 7509.111852 YDOT = 4071.093316 feet/sec YDOT = 1324.942675 meter/sec ZDOT = 2490.929077 ZDOT = 795.754999 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 635506.82 X = 193702.48 Y = 14005683.34 feet Y = 4268932.28 meter Z = 17287224.53 Z = 5269146.04 XDOT = -23895.227247 XDOT = -7283.265265 YDOT = -2228.481924 feet/sec YDOT = -679.241290 meter/sec ZDOT = 2656.726183 ZDOT = 809.770141 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19201.73608012 .00016717 00000-0 10270-3 0 9041 2 25544 51.6399 194.8309 0006510 163.7125 196.4236 15.51022518 20458 Satellite: ISS Catalog Number: 25544 Epoch time: 19201.73608012 = yrday.fracday Element set: 904 Inclination: 51.6399 deg RA of node: 194.8309 deg Eccentricity: .0006510 Arg of perigee: 163.7125 deg Mean anomaly: 196.4236 deg Mean motion: 15.51022518 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2045 Checksum: 293 Coasting Arc #6 (Orbit 2048) --------------------------------------- Vector Time (GMT): 2019/201/22:50:58.000 Vector Time (MET): N/A Weight (LBS) : 931973.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4747586.75 A = 6790793.02 meter Y = -2377985.01 meter E = .0011735 Z = 4221184.52 I = 51.54453 XDOT = 5322.692856 Wp = 108.03024 YDOT = 4149.190707 meter/sec RA = 192.54375 deg ZDOT = -3644.244645 TA = 19.34642 MA = 19.30191 Ha = 227.368 n.mi Hp = 218.639 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 15576072.00 X = 4753321.45 Y = -7801788.10 feet Y = -2324862.42 meter Z = 13849030.58 Z = 4244259.80 XDOT = 17462.903072 XDOT = 5293.601184 YDOT = 13612.830405 feet/sec YDOT = 4208.550416 meter/sec ZDOT = -11956.183220 ZDOT = -3618.459854 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 10438370.31 X = 3181615.27 Y = 13842096.58 feet Y = 4219071.04 meter Z = 13954008.45 Z = 4253181.78 XDOT = -9253.857582 XDOT = -2820.575791 YDOT = 18929.134581 feet/sec YDOT = 5769.600220 meter/sec ZDOT = -11839.339709 ZDOT = -3608.630743 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19201.99380842 .00016717 00000-0 10270-3 0 9058 2 25544 51.6385 193.5494 0006552 165.8952 194.2383 15.50995604 20498 Satellite: ISS Catalog Number: 25544 Epoch time: 19201.99380842 = yrday.fracday Element set: 905 Inclination: 51.6385 deg RA of node: 193.5494 deg Eccentricity: .0006552 Arg of perigee: 165.8952 deg Mean anomaly: 194.2383 deg Mean motion: 15.50995604 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2049 Checksum: 340 Coasting Arc #7 (Orbit 2063) --------------------------------------- Vector Time (GMT): 2019/202/22:50:58.000 Vector Time (MET): N/A Weight (LBS) : 931973.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5129573.31 A = 6792279.73 meter Y = 2352650.64 meter E = .0010896 Z = -3793150.22 I = 51.58204 XDOT = -4960.975310 Wp = 138.03189 YDOT = -4027.887418 meter/sec RA = 187.57536 deg ZDOT = 4209.714624 TA = 176.57103 MA = 176.56356 Ha = 227.480 n.mi Hp = 218.588 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16829308.76 X = -5137075.39 Y = 7718670.07 feet Y = 2295246.45 meter Z = -12444718.56 Z = -3818085.40 XDOT = -16276.165716 XDOT = -4936.013710 YDOT = -13214.853734 feet/sec YDOT = -4083.225231 meter/sec ZDOT = 13811.399684 ZDOT = 4185.676846 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -10840148.61 X = -3304077.30 Y = -14915041.66 feet Y = -4546104.70 meter Z = -12558153.98 Z = -3827725.33 XDOT = 8674.343170 XDOT = 2643.939798 YDOT = -17844.092696 feet/sec YDOT = -5438.879454 meter/sec ZDOT = 13702.465899 ZDOT = 4176.511606 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19202.96029324 .00016717 00000-0 10270-3 0 9062 2 25544 51.6382 188.7531 0006700 167.9369 192.1944 15.50994826 20645 Satellite: ISS Catalog Number: 25544 Epoch time: 19202.96029324 = yrday.fracday Element set: 906 Inclination: 51.6382 deg RA of node: 188.7531 deg Eccentricity: .0006700 Arg of perigee: 167.9369 deg Mean anomaly: 192.1944 deg Mean motion: 15.50994826 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2064 Checksum: 331 Coasting Arc #8 (Orbit 2064) --------------------------------------- Vector Time (GMT): 2019/202/23:35:13.000 Vector Time (MET): N/A Weight (LBS) : 931973.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4423470.98 A = 6790650.37 meter Y = -2848629.40 meter E = .0011277 Z = 4281544.20 I = 51.57724 XDOT = 5764.201266 Wp = 109.53608 YDOT = 3597.231665 meter/sec RA = 187.42356 deg ZDOT = -3557.984298 TA = 16.79042 MA = 16.75312 Ha = 227.426 n.mi Hp = 218.728 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14512700.08 X = 4434199.41 Y = -9345896.97 feet Y = -2799103.33 meter Z = 14047061.02 Z = 4303057.27 XDOT = 18911.421476 XDOT = 5740.829998 YDOT = 11801.941157 feet/sec YDOT = 3661.560564 meter/sec ZDOT = -11673.176832 ZDOT = -3530.040981 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14126789.90 X = 4305845.56 Y = 9779439.20 feet Y = 2980773.07 meter Z = 14144983.32 Z = 4311390.92 XDOT = -2977.712044 XDOT = -907.606631 YDOT = 21020.877161 feet/sec YDOT = 6407.163359 meter/sec ZDOT = -11546.471239 ZDOT = -3519.364434 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19203.02472587 .00016717 00000-0 10270-3 0 9074 2 25544 51.6381 188.4329 0006774 168.5248 191.6058 15.50972107 20659 Satellite: ISS Catalog Number: 25544 Epoch time: 19203.02472587 = yrday.fracday Element set: 907 Inclination: 51.6381 deg RA of node: 188.4329 deg Eccentricity: .0006774 Arg of perigee: 168.5248 deg Mean anomaly: 191.6058 deg Mean motion: 15.50972107 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2065 Checksum: 327 Coasting Arc #9 (Orbit 2078) --------------------------------------- Vector Time (GMT): 2019/203/20:55:00.000 Vector Time (MET): N/A Weight (LBS) : 931973.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4015156.76 A = 6791231.01 meter Y = -3532970.02 meter E = .0014077 Z = 4181932.64 I = 51.61057 XDOT = 6177.533213 Wp = 129.02004 YDOT = -2611.339509 meter/sec RA = 183.06401 deg ZDOT = 3707.992827 TA = 282.78188 MA = 282.93916 Ha = 227.387 n.mi Hp = 218.954 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -13173086.48 X = -3995664.88 Y = -11591109.00 feet Y = -3577761.58 meter Z = 13720251.44 Z = 4162475.92 XDOT = 20267.497417 XDOT = 6188.263724 YDOT = -8567.386842 feet/sec YDOT = -2542.198212 meter/sec ZDOT = 12165.330798 ZDOT = 3738.026455 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14932987.42 X = 4551574.57 Y = -9343525.96 feet Y = -2847906.71 meter Z = 13632084.37 Z = 4155059.32 XDOT = 1677.479536 XDOT = 511.295763 YDOT = 20711.634463 feet/sec YDOT = 6312.906184 meter/sec ZDOT = 12301.958007 ZDOT = 3749.636801 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19203.92677539 .00016717 00000-0 10270-3 0 9088 2 25544 51.6403 183.9605 0006305 171.3430 188.7831 15.50971563 20792 Satellite: ISS Catalog Number: 25544 Epoch time: 19203.92677539 = yrday.fracday Element set: 908 Inclination: 51.6403 deg RA of node: 183.9605 deg Eccentricity: .0006305 Arg of perigee: 171.3430 deg Mean anomaly: 188.7831 deg Mean motion: 15.50971563 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2079 Checksum: 324 Coasting Arc #10 (Orbit 2087) --------------------------------------- Vector Time (GMT): 2019/204/11:00:00.000 Vector Time (MET): N/A Weight (LBS) : 931973.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 69492.32 A = 6786505.71 meter Y = -4212544.88 meter E = .0007261 Z = 5317493.65 I = 51.61261 XDOT = 7665.907477 Wp = 153.35548 YDOT = 62.313949 meter/sec RA = 180.12743 deg ZDOT = -57.134968 TA = 297.15229 MA = 297.22631 Ha = 227.359 n.mi Hp = 218.891 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 227993.18 X = 90763.93 Y = -13820685.29 feet Y = -4211649.13 meter Z = 17445845.32 Z = 5317882.64 XDOT = 25150.615083 XDOT = 7664.918449 YDOT = 204.442089 feet/sec YDOT = 148.033984 meter/sec ZDOT = -187.450682 ZDOT = -19.899710 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13376836.27 X = -4077259.70 Y = 3471634.91 feet Y = 1058154.32 meter Z = 17447889.39 Z = 5318116.69 XDOT = -6062.158947 XDOT = -1847.746047 YDOT = -23370.938481 feet/sec YDOT = -7123.462049 meter/sec ZDOT = -18.268024 ZDOT = -5.568094 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19204.50666393 .00016717 00000-0 10270-3 0 9090 2 25544 51.6382 181.0838 0006530 172.2537 187.8716 15.50987895 20880 Satellite: ISS Catalog Number: 25544 Epoch time: 19204.50666393 = yrday.fracday Element set: 909 Inclination: 51.6382 deg RA of node: 181.0838 deg Eccentricity: .0006530 Arg of perigee: 172.2537 deg Mean anomaly: 187.8716 deg Mean motion: 15.50987895 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2088 Checksum: 344 Coasting Arc #11 (Orbit 2102) --------------------------------------- Vector Time (GMT): 2019/205/11:00:00.000 Vector Time (MET): N/A Weight (LBS) : 951979.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -580525.42 A = 6786765.49 meter Y = 4241823.64 meter E = .0016965 Z = -5279806.64 I = 51.64666 XDOT = -7607.148831 Wp = 118.64694 YDOT = -9.425452 meter/sec RA = 175.16062 deg ZDOT = 822.923967 TA = 159.27028 MA = 159.20138 Ha = 227.260 n.mi Hp = 219.033 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -1904610.97 X = -602269.43 Y = 13916744.22 feet Y = 4235210.54 meter Z = -17322200.25 Z = -5282679.14 XDOT = -24957.837373 XDOT = -7610.475329 YDOT = -30.923399 feet/sec YDOT = -94.512584 meter/sec ZDOT = 2699.881782 ZDOT = 785.963534 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13869649.65 X = 4227469.21 Y = -2115203.50 feet Y = -644714.03 meter Z = -17335531.92 Z = -5283870.13 XDOT = 6697.432117 XDOT = 2041.377309 YDOT = 23005.850274 feet/sec YDOT = 7012.183164 meter/sec ZDOT = 2531.924442 ZDOT = 771.730570 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19205.47314528 .00016717 00000-0 10270-3 0 9109 2 25544 51.6382 176.2890 0006511 175.6156 184.5053 15.50972193 21038 Satellite: ISS Catalog Number: 25544 Epoch time: 19205.47314528 = yrday.fracday Element set: 910 Inclination: 51.6382 deg RA of node: 176.2890 deg Eccentricity: .0006511 Arg of perigee: 175.6156 deg Mean anomaly: 184.5053 deg Mean motion: 15.50972193 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2103 Checksum: 301 Coasting Arc #12 (Orbit 2118) --------------------------------------- Vector Time (GMT): 2019/206/11:00:00.000 Vector Time (MET): N/A Weight (LBS) : 951979.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1049086.63 A = 6787236.11 meter Y = -4302667.64 meter E = .0005386 Z = 5139046.74 I = 51.68193 XDOT = 7504.907416 Wp = 134.45643 YDOT = -39.484114 meter/sec RA = 170.19640 deg ZDOT = -1567.783928 TA = 330.63581 MA = 330.66607 Ha = 227.097 n.mi Hp = 219.194 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 3441885.26 X = 1072159.85 Y = -14116363.66 feet Y = -4290807.39 meter Z = 16860389.56 Z = 5144198.50 XDOT = 24622.399659 XDOT = 7512.406534 YDOT = -129.541058 feet/sec YDOT = 44.483077 meter/sec ZDOT = -5143.648057 ZDOT = -1531.309924 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14471963.71 X = -4411054.54 Y = 938562.03 feet Y = 286073.71 meter Z = 16884087.21 Z = 5146269.78 XDOT = -7255.822788 XDOT = -2211.574786 YDOT = -22488.526828 feet/sec YDOT = -6854.502977 meter/sec ZDOT = -4977.877251 ZDOT = -1517.256986 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19206.50405627 .00016717 00000-0 10270-3 0 9116 2 25544 51.6384 171.1739 0006458 180.1621 179.9529 15.50997564 21196 Satellite: ISS Catalog Number: 25544 Epoch time: 19206.50405627 = yrday.fracday Element set: 911 Inclination: 51.6384 deg RA of node: 171.1739 deg Eccentricity: .0006458 Arg of perigee: 180.1621 deg Mean anomaly: 179.9529 deg Mean motion: 15.50997564 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2119 Checksum: 326 Coasting Arc #13 (Orbit 2133) --------------------------------------- Vector Time (GMT): 2019/207/11:00:00.000 Vector Time (MET): N/A Weight (LBS) : 951979.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1519689.20 A = 6788210.12 meter Y = 4425386.70 meter E = .0015001 Z = -4931263.46 I = 51.71805 XDOT = -7300.356898 Wp = 131.10595 YDOT = 53.075416 meter/sec RA = 165.23496 deg ZDOT = 2292.348222 TA = 161.35680 MA = 161.30179 Ha = 226.996 n.mi Hp = 219.322 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4985856.96 X = -1545109.00 Y = 14518985.22 feet Y = 4408250.78 meter Z = -16178685.88 Z = -4938706.83 XDOT = -23951.302158 XDOT = -7311.542718 YDOT = 174.131942 feet/sec YDOT = -28.625054 meter/sec ZDOT = 7520.827500 ZDOT = 2256.858856 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15314312.20 X = 4667802.36 Y = 161475.93 feet Y = 49217.86 meter Z = -16212814.24 Z = -4941665.78 XDOT = 7580.461610 XDOT = 2310.524699 YDOT = 21660.678120 feet/sec YDOT = 6602.174691 meter/sec ZDOT = 7359.509100 ZDOT = 2243.178374 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19207.47053344 .00016717 00000-0 10270-3 0 9129 2 25544 51.6388 166.3786 0006332 183.1470 176.9643 15.50981451 21343 Satellite: ISS Catalog Number: 25544 Epoch time: 19207.47053344 = yrday.fracday Element set: 912 Inclination: 51.6388 deg RA of node: 166.3786 deg Eccentricity: .0006332 Arg of perigee: 183.1470 deg Mean anomaly: 176.9643 deg Mean motion: 15.50981451 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2134 Checksum: 316 Coasting Arc #14 (Orbit 2149) --------------------------------------- Vector Time (GMT): 2019/208/11:00:00.000 Vector Time (MET): N/A Weight (LBS) : 951979.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1933383.14 A = 6789307.96 meter Y = -4568540.22 meter E = .0007173 Z = 4628125.57 I = 51.75335 XDOT = 7063.430430 Wp = 112.77507 YDOT = -34.061347 meter/sec RA = 160.27731 deg ZDOT = -2983.374125 TA = 6.92761 MA = 6.91770 Ha = 226.805 n.mi Hp = 219.512 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 6343120.52 X = 1961845.45 Y = -14988649.00 feet Y = -4546761.13 meter Z = 15184139.02 Z = 4637585.79 XDOT = 23173.984349 XDOT = 7077.777828 YDOT = -111.749825 feet/sec YDOT = 45.007440 meter/sec ZDOT = -9787.972850 ZDOT = -2949.027997 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -16202013.59 X = -4938373.74 Y = -1035484.75 feet Y = -315615.75 meter Z = 15227454.86 Z = 4641328.24 XDOT = -7728.550713 XDOT = -2355.662257 YDOT = -20761.849789 feet/sec YDOT = -6328.211816 meter/sec ZDOT = -9631.829464 ZDOT = -2935.781621 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19208.50144141 .00016717 00000-0 10270-3 0 9131 2 25544 51.6382 161.2639 0006290 187.8398 172.2656 15.51004598 21501 Satellite: ISS Catalog Number: 25544 Epoch time: 19208.50144141 = yrday.fracday Element set: 913 Inclination: 51.6382 deg RA of node: 161.2639 deg Eccentricity: .0006290 Arg of perigee: 187.8398 deg Mean anomaly: 172.2656 deg Mean motion: 15.51004598 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2150 Checksum: 306 Coasting Arc #15 (Orbit 2164) --------------------------------------- Vector Time (GMT): 2019/209/11:00:00.000 Vector Time (MET): N/A Weight (LBS) : 936703.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2317599.39 A = 6790756.83 meter Y = 4759542.02 meter E = .0011121 Z = -4264700.52 I = 51.78944 XDOT = -6743.406470 Wp = 144.63227 YDOT = -37.051225 meter/sec RA = 155.32277 deg ZDOT = 3619.162411 TA = 162.38851 MA = 162.34992 Ha = 226.737 n.mi Hp = 219.659 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -7603672.54 X = -2349934.35 Y = 15615295.33 feet Y = 4733444.73 meter Z = -13991799.59 Z = -4276036.39 XDOT = -22124.036976 XDOT = -6760.070695 YDOT = -121.559137 feet/sec YDOT = -112.554357 meter/sec ZDOT = 11873.892423 ZDOT = 3586.365275 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 17239120.12 X = 5254483.81 Y = 1735472.11 feet Y = 528971.90 meter Z = -14043668.12 Z = -4280510.04 XDOT = 7583.520544 XDOT = 2311.457062 YDOT = 19657.024407 feet/sec YDOT = 5991.461039 meter/sec ZDOT = 11724.772348 ZDOT = 3573.710612 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19209.46791695 .00016717 00000-0 10270-3 0 9140 2 25544 51.6386 156.4686 0006288 191.6211 168.4796 15.50986891 21659 Satellite: ISS Catalog Number: 25544 Epoch time: 19209.46791695 = yrday.fracday Element set: 914 Inclination: 51.6386 deg RA of node: 156.4686 deg Eccentricity: .0006288 Arg of perigee: 191.6211 deg Mean anomaly: 168.4796 deg Mean motion: 15.50986891 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2165 Checksum: 363 Coasting Arc #16 (Orbit 2180) --------------------------------------- Vector Time (GMT): 2019/210/10:44:30.000 Vector Time (MET): N/A Weight (LBS) : 936703.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3610317.24 A = 6787332.64 meter Y = -2592510.43 meter E = .0009306 Z = 5129720.50 I = 51.80917 XDOT = 5773.935778 Wp = 165.22306 YDOT = -4761.417413 meter/sec RA = 150.46460 deg ZDOT = 1647.910405 TA = 268.84474 MA = 268.95136 Ha = 226.624 n.mi Hp = 219.848 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -11844872.82 X = -3605975.72 Y = -8505611.64 feet Y = -2632859.93 meter Z = 16829791.67 Z = 5112193.36 XDOT = 18943.358852 XDOT = 5818.745658 YDOT = -15621.448206 feet/sec YDOT = -4696.598879 meter/sec ZDOT = 5406.530200 ZDOT = 1676.065867 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -4628146.67 X = -1410659.10 Y = 13924696.46 feet Y = 4244247.48 meter Z = 16750266.15 Z = 5105481.12 XDOT = -19459.218066 XDOT = -5931.169667 YDOT = -13163.093812 feet/sec YDOT = -4012.110994 meter/sec ZDOT = 5534.899676 ZDOT = 1687.037421 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19210.49882080 .00016717 00000-0 10270-3 0 9155 2 25544 51.6400 151.3539 0006296 196.6718 163.4227 15.51030929 21818 Satellite: ISS Catalog Number: 25544 Epoch time: 19210.49882080 = yrday.fracday Element set: 915 Inclination: 51.6400 deg RA of node: 151.3539 deg Eccentricity: .0006296 Arg of perigee: 196.6718 deg Mean anomaly: 163.4227 deg Mean motion: 15.51030929 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2181 Checksum: 307 Coasting Arc #17 (Orbit 2195) --------------------------------------- Vector Time (GMT): 2019/211/10:44:30.000 Vector Time (MET): N/A Weight (LBS) : 936703.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3174831.93 A = 6786757.00 meter Y = 2857336.49 meter E = .0012899 Z = -5284120.66 I = 51.83561 XDOT = -5844.980692 Wp = 108.66779 YDOT = 4862.586092 meter/sec RA = 145.50989 deg ZDOT = -888.209442 TA = 152.87938 MA = 152.81194 Ha = 226.482 n.mi Hp = 220.110 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 10416115.26 X = 3168311.27 Y = 9374463.55 feet Y = 2892803.91 meter Z = -17336353.86 Z = -5268714.26 XDOT = -19176.445841 XDOT = -5894.606770 YDOT = 15953.366442 feet/sec YDOT = 4796.946051 meter/sec ZDOT = -2914.072974 ZDOT = -916.721560 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 5655080.27 X = 1723668.47 Y = -12915644.72 feet Y = -3936688.51 meter Z = -17266481.33 Z = -5262823.51 XDOT = 20155.084818 XDOT = 6143.269853 YDOT = 12868.879667 feet/sec YDOT = 3922.434523 meter/sec ZDOT = -3044.096616 ZDOT = -927.840649 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19211.46529296 .00016717 00000-0 10270-3 0 9161 2 25544 51.6402 146.5578 0006179 199.3841 160.7076 15.51001971 21969 Satellite: ISS Catalog Number: 25544 Epoch time: 19211.46529296 = yrday.fracday Element set: 916 Inclination: 51.6402 deg RA of node: 146.5578 deg Eccentricity: .0006179 Arg of perigee: 199.3841 deg Mean anomaly: 160.7076 deg Mean motion: 15.51001971 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2196 Checksum: 324 Coasting Arc #18 (Orbit 2211) --------------------------------------- Vector Time (GMT): 2019/212/10:44:30.000 Vector Time (MET): N/A Weight (LBS) : 936703.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2779520.65 A = 6786420.20 meter Y = -3139091.25 meter E = .0005983 Z = 5336465.18 I = 51.86203 XDOT = 5851.428459 Wp = 180.81746 YDOT = -4947.315395 meter/sec RA = 140.55930 deg ZDOT = 131.733862 TA = 267.89600 MA = 267.96452 Ha = 226.372 n.mi Hp = 220.159 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -9119162.24 X = -2770132.83 Y = -10298855.81 feet Y = -3170121.92 meter Z = 17508087.86 Z = 5322986.07 XDOT = 19197.599930 XDOT = 5905.676000 YDOT = -16231.349720 feet/sec YDOT = -4881.577310 meter/sec ZDOT = 432.197710 ZDOT = 160.288442 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6728066.32 X = -2050714.62 Y = 12086945.82 feet Y = 3684101.09 meter Z = 17446992.74 Z = 5317843.39 XDOT = -20716.158388 XDOT = -6314.285077 YDOT = -12370.981071 feet/sec YDOT = -3770.675030 meter/sec ZDOT = 562.443509 ZDOT = 171.432781 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19212.49619494 .00016717 00000-0 10270-3 0 9176 2 25544 51.6406 141.4444 0006154 203.9168 156.1698 15.51021376 22125 Satellite: ISS Catalog Number: 25544 Epoch time: 19212.49619494 = yrday.fracday Element set: 917 Inclination: 51.6406 deg RA of node: 141.4444 deg Eccentricity: .0006154 Arg of perigee: 203.9168 deg Mean anomaly: 156.1698 deg Mean motion: 15.51021376 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2212 Checksum: 305 Coasting Arc #19 (Orbit 2214) --------------------------------------- Vector Time (GMT): 2019/212/15:35:00.000 Vector Time (MET): N/A Weight (LBS) : 936703.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1822211.27 A = 6792442.37 meter Y = -5380873.83 meter E = .0010020 Z = 3711611.75 I = 51.89004 XDOT = 6263.664058 Wp = 116.14714 YDOT = -872.802205 meter/sec RA = 139.53640 deg ZDOT = -4335.717600 TA = 19.81522 MA = 19.77632 Ha = 226.167 n.mi Hp = 220.176 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5978383.42 X = 1864217.80 Y = -17653785.52 feet Y = -5360262.11 meter Z = 12177203.92 Z = 3720564.60 XDOT = 20550.078931 XDOT = 6294.018457 YDOT = -2863.524295 feet/sec YDOT = -802.587319 meter/sec ZDOT = -14224.795277 ZDOT = -4305.218170 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -5329388.63 X = -1624397.65 Y = 17832328.93 feet Y = 5435293.86 meter Z = 12218312.83 Z = 3724141.75 XDOT = -19242.955197 XDOT = -5865.252744 YDOT = 3911.090851 feet/sec YDOT = 1192.100491 meter/sec ZDOT = -14085.985960 ZDOT = -4293.408521 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19212.68948789 .00016717 00000-0 10270-3 0 9180 2 25544 51.6430 140.4867 0006084 205.3162 154.7692 15.51044598 22154 Satellite: ISS Catalog Number: 25544 Epoch time: 19212.68948789 = yrday.fracday Element set: 918 Inclination: 51.6430 deg RA of node: 140.4867 deg Eccentricity: .0006084 Arg of perigee: 205.3162 deg Mean anomaly: 154.7692 deg Mean motion: 15.51044598 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2215 Checksum: 328 Coasting Arc #20 (Orbit 2226) --------------------------------------- Vector Time (GMT): 2019/213/11:38:30.000 Vector Time (MET): N/A Weight (LBS) : 936703.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 424367.62 A = 6790417.19 meter Y = -5198306.12 meter E = .0006714 Z = 4341335.93 I = 51.90267 XDOT = 6372.198389 Wp = 111.74636 YDOT = -2415.077676 meter/sec RA = 135.40518 deg ZDOT = -3512.766582 TA = 13.87004 MA = 13.85160 Ha = 226.187 n.mi Hp = 220.340 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 1392282.22 X = 461377.80 Y = -17054810.11 feet Y = -5193353.99 meter Z = 14243228.12 Z = 4343486.73 XDOT = 20906.162693 XDOT = 6415.793503 YDOT = -7923.483188 feet/sec YDOT = -2343.575216 meter/sec ZDOT = -11524.824744 ZDOT = -3481.707983 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14932258.99 X = -4551352.54 Y = 8339260.53 feet Y = 2541806.61 meter Z = 14253382.77 Z = 4344431.07 XDOT = -17587.926314 XDOT = -5360.799940 YDOT = -12025.792568 feet/sec YDOT = -3665.461575 meter/sec ZDOT = -11383.345556 ZDOT = -3469.643726 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19213.52709600 .00016717 00000-0 10270-3 0 9192 2 25544 51.6419 136.3302 0006191 207.9625 152.1194 15.51012802 22275 Satellite: ISS Catalog Number: 25544 Epoch time: 19213.52709600 = yrday.fracday Element set: 919 Inclination: 51.6419 deg RA of node: 136.3302 deg Eccentricity: .0006191 Arg of perigee: 207.9625 deg Mean anomaly: 152.1194 deg Mean motion: 15.51012802 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2227 Checksum: 281