ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 16466.6302 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 69.1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1.708 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 ------------------------------------------------------------------------ 023/14:19:41.994 1.2 1.8 1.8 N/A -0.9 0.0 229.5 000/00:09:23.988 -0.9 -0.0 221.9 023/17:25:20.976 0.6 0.9 0.9 N/A -0.5 -0.0 229.6 000/00:04:41.953 -0.4 -0.0 222.4 024/09:05:00.000 0.0 0.0 0.0 N/A 0.0 0.0 229.8 000/00:00:00.000 0.0 0.0 222.5 031/14:35:00.000 0.0 0.0 0.0 N/A 0.0 0.0 228.7 000/00:00:00.000 0.0 0.0 223.5 031/19:42:00.000 0.0 0.0 0.0 N/A 0.0 0.0 228.8 000/00:00:00.000 0.0 0.0 223.4 035/03:40:00.000 0.0 0.0 0.0 N/A 0.0 0.0 228.3 000/00:00:00.000 0.0 0.0 223.8 037/05:49:00.000 0.0 0.0 0.0 N/A 0.0 0.0 227.8 000/00:00:00.000 0.0 0.0 224.2 Coasting Arc #1 (Orbit 926) --------------------------------------- Vector Time (GMT): 2020/022/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 936369.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4703983.85 A = 6795473.57 meter Y = -2732871.00 meter E = .0008954 Z = -4078549.10 I = 51.59691 XDOT = 5483.868307 Wp = 100.82609 YDOT = -3686.897726 meter/sec RA = 353.69449 deg ZDOT = -3863.233649 TA = 129.12039 MA = 129.04075 Ha = 229.208 n.mi Hp = 220.931 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -15433017.89 X = -4653263.63 Y = -8966112.20 feet Y = -2785190.27 meter Z = -13381066.59 Z = -4101275.84 XDOT = 17991.693921 XDOT = 5543.453707 YDOT = -12096.121149 feet/sec YDOT = -3625.239681 meter/sec ZDOT = -12674.651080 ZDOT = -3836.451347 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -34301.97 X = -10455.24 Y = -17770238.59 feet Y = -5416368.72 meter Z = -13484791.29 Z = -4110164.39 XDOT = 18288.106346 XDOT = 5574.214814 YDOT = 9467.563818 feet/sec YDOT = 2885.713452 meter/sec ZDOT = -12551.739042 ZDOT = -3825.770060 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 20022.52325217 .00016717 00000-0 10270-3 0 9000 2 25544 51.6411 354.1460 0004516 156.9070 203.2284 15.49577808 9270 Satellite: ISS Catalog Number: 25544 Epoch time: 20022.52325217 = yrday.fracday Element set: 900 Inclination: 51.6411 deg RA of node: 354.1460 deg Eccentricity: .0004516 Arg of perigee: 156.9070 deg Mean anomaly: 203.2284 deg Mean motion: 15.49577808 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 927 Checksum: 284 Coasting Arc #2 (Orbit 942) --------------------------------------- Vector Time (GMT): 2020/023/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 936369.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4757795.86 A = 6794961.09 meter Y = 2441193.88 meter E = .0013123 Z = 4187324.95 I = 51.56336 XDOT = -5347.844040 Wp = 121.82260 YDOT = 4055.939436 meter/sec RA = 348.74031 deg ZDOT = 3696.514312 TA = 290.09109 MA = 290.23227 Ha = 228.999 n.mi Hp = 221.089 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 15609566.47 X = 4709804.98 Y = 8009166.27 feet Y = 2494130.20 meter Z = 13737942.75 Z = 4210319.57 XDOT = -17545.420080 XDOT = -5410.756397 YDOT = 13306.887913 feet/sec YDOT = 3995.783948 meter/sec ZDOT = 12127.671627 ZDOT = 3670.384789 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 1247465.39 X = 380227.45 Y = 17417053.49 feet Y = 5308717.90 meter Z = 13842920.88 Z = 4219322.28 XDOT = -19272.741108 XDOT = -5874.331490 YDOT = -8202.872560 feet/sec YDOT = -2500.235556 meter/sec ZDOT = 12007.717474 ZDOT = 3659.952286 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 20023.55510441 .00016717 00000-0 10270-3 0 9010 2 25544 51.6420 349.0382 0004510 162.9638 197.1665 15.49618959 9432 Satellite: ISS Catalog Number: 25544 Epoch time: 20023.55510441 = yrday.fracday Element set: 901 Inclination: 51.6420 deg RA of node: 349.0382 deg Eccentricity: .0004510 Arg of perigee: 162.9638 deg Mean anomaly: 197.1665 deg Mean motion: 15.49618959 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 943 Checksum: 306 Coasting Arc #3 (Orbit 943) --------------------------------------- Vector Time (GMT): 2020/023/14:24:23.988 Vector Time (MET): N/A Weight (LBS) : 936187.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2890793.86 A = 6792675.05 meter Y = -3503158.75 meter E = .0013180 Z = -5061744.86 I = 51.55019 XDOT = 6815.099155 Wp = 97.56650 YDOT = -2934.143108 meter/sec RA = 348.23319 deg ZDOT = -1867.349090 TA = 154.30850 MA = 154.24296 Ha = 229.479 n.mi Hp = 221.907 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -9484231.83 X = -2826819.22 Y = -11493302.99 feet Y = -3535127.49 meter Z = -16606774.46 Z = -5075631.80 XDOT = 22359.249196 XDOT = 6856.473384 YDOT = -9626.453765 feet/sec YDOT = -2857.700334 meter/sec ZDOT = -6126.473393 ZDOT = -1834.144604 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -4284220.24 X = -1305830.33 Y = -14198203.54 feet Y = -4327612.44 meter Z = -16669975.96 Z = -5081008.67 XDOT = 23343.203462 XDOT = 7115.008415 YDOT = -51.916417 feet/sec YDOT = -15.824124 meter/sec ZDOT = -5974.256585 ZDOT = -1820.953407 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 20023.61959959 .00016717 00000-0 10270-3 0 9029 2 25544 51.6434 348.7186 0004945 176.5909 183.5275 15.49255423 9449 Satellite: ISS Catalog Number: 25544 Epoch time: 20023.61959959 = yrday.fracday Element set: 902 Inclination: 51.6434 deg RA of node: 348.7186 deg Eccentricity: .0004945 Arg of perigee: 176.5909 deg Mean anomaly: 183.5275 deg Mean motion: 15.49255423 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 944 Checksum: 342 Coasting Arc #4 (Orbit 945) --------------------------------------- Vector Time (GMT): 2020/023/17:27:41.953 Vector Time (MET): N/A Weight (LBS) : 936097.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3890844.39 A = 6794556.59 meter Y = -2978034.12 meter E = .0009974 Z = -4715057.43 I = 51.55218 XDOT = 6140.752164 Wp = 99.73074 YDOT = -3616.717484 meter/sec RA = 347.60988 deg ZDOT = -2789.696791 TA = 142.56602 MA = 142.49650 Ha = 229.607 n.mi Hp = 222.415 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12765237.49 X = -3834351.49 Y = -9770453.16 feet Y = -3021228.00 meter Z = -15469348.52 Z = -4733820.22 XDOT = 20146.824686 XDOT = 6194.289378 YDOT = -11865.871012 feet/sec YDOT = -3547.747648 meter/sec ZDOT = -9152.548526 ZDOT = -2759.738469 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -15509846.52 X = -4727401.22 Y = -3899126.12 feet Y = -1188453.64 meter Z = -15554911.23 Z = -4741136.94 XDOT = 13499.636674 XDOT = 4114.689258 YDOT = -17821.378550 feet/sec YDOT = -5431.956182 meter/sec ZDOT = -9015.119802 ZDOT = -2747.808516 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 20023.74860950 .00016717 00000-0 10270-3 0 9036 2 25544 51.6449 348.0816 0005356 185.6375 174.4715 15.49089858 9460 Satellite: ISS Catalog Number: 25544 Epoch time: 20023.74860950 = yrday.fracday Element set: 903 Inclination: 51.6449 deg RA of node: 348.0816 deg Eccentricity: .0005356 Arg of perigee: 185.6375 deg Mean anomaly: 174.4715 deg Mean motion: 15.49089858 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 946 Checksum: 340 Coasting Arc #5 (Orbit 955) --------------------------------------- Vector Time (GMT): 2020/024/09:05:00.000 Vector Time (MET): N/A Weight (LBS) : 936097.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -617868.42 A = 6792258.06 meter Y = -4208551.60 meter E = .0015614 Z = -5308173.62 I = 51.51992 XDOT = 7444.327363 Wp = 114.37769 YDOT = -1694.631494 meter/sec RA = 344.35982 deg ZDOT = 471.863014 TA = 160.17231 MA = 160.11155 Ha = 229.772 n.mi Hp = 222.495 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -2027127.38 X = -544977.88 Y = -13807583.98 feet Y = -4215053.05 meter Z = -17415267.79 Z = -5310998.21 XDOT = 24423.646203 XDOT = 7460.431979 YDOT = -5559.814613 feet/sec YDOT = -1611.293745 meter/sec ZDOT = 1548.107002 ZDOT = 508.062632 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13912271.07 X = 4240460.22 Y = 878127.46 feet Y = 267653.25 meter Z = -17427787.55 Z = -5311989.64 XDOT = 652.463245 XDOT = 198.870797 YDOT = 24016.261436 feet/sec YDOT = 7320.156486 meter/sec ZDOT = 1713.901822 ZDOT = 522.397275 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 20024.39372918 .00016717 00000-0 10270-3 0 9041 2 25544 51.6420 344.8891 0005543 185.0551 175.0544 15.49056594 9563 Satellite: ISS Catalog Number: 25544 Epoch time: 20024.39372918 = yrday.fracday Element set: 904 Inclination: 51.6420 deg RA of node: 344.8891 deg Eccentricity: .0005543 Arg of perigee: 185.0551 deg Mean anomaly: 175.0544 deg Mean motion: 15.49056594 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 956 Checksum: 318 Coasting Arc #6 (Orbit 971) --------------------------------------- Vector Time (GMT): 2020/025/09:05:00.000 Vector Time (MET): N/A Weight (LBS) : 936097.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 948843.55 A = 6792200.04 meter Y = 4144823.74 meter E = .0004654 Z = 5294813.62 I = 51.48670 XDOT = -7288.476504 Wp = 158.48324 YDOT = 2309.077790 meter/sec RA = 339.40473 deg ZDOT = -505.550876 TA = 296.32998 MA = 296.37777 Ha = 229.551 n.mi Hp = 222.693 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 3113003.76 X = 876705.98 Y = 13598503.09 feet Y = 4155030.72 meter Z = 17371435.77 Z = 5299247.65 XDOT = -23912.324487 XDOT = -7311.299996 YDOT = 7575.714534 feet/sec YDOT = 2227.445299 meter/sec ZDOT = -1658.631483 ZDOT = -541.009685 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13917614.72 X = -4242088.97 Y = 467369.32 feet Y = 142454.17 meter Z = 17391331.92 Z = 5300877.97 XDOT = -3060.270447 XDOT = -932.770432 YDOT = -23865.835154 feet/sec YDOT = -7274.306555 meter/sec ZDOT = -1821.085059 ZDOT = -555.066726 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 20025.42591973 .00016717 00000-0 10270-3 0 9051 2 25544 51.6407 339.7829 0005520 189.9921 170.1120 15.49075404 9726 Satellite: ISS Catalog Number: 25544 Epoch time: 20025.42591973 = yrday.fracday Element set: 905 Inclination: 51.6407 deg RA of node: 339.7829 deg Eccentricity: .0005520 Arg of perigee: 189.9921 deg Mean anomaly: 170.1120 deg Mean motion: 15.49075404 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 972 Checksum: 311 Coasting Arc #7 (Orbit 986) --------------------------------------- Vector Time (GMT): 2020/026/09:05:00.000 Vector Time (MET): N/A Weight (LBS) : 936097.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1252718.08 A = 6792274.35 meter Y = -4078667.34 meter E = .0014875 Z = -5297073.24 I = 51.45633 XDOT = 7061.513082 Wp = 115.56527 YDOT = -2890.167181 meter/sec RA = 334.44738 deg ZDOT = 550.324465 TA = 159.74167 MA = 159.68259 Ha = 229.527 n.mi Hp = 222.757 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4109967.44 X = -1181286.75 Y = -13381454.53 feet Y = -4092276.52 meter Z = -17378849.22 Z = -5302984.94 XDOT = 23167.693837 XDOT = 7090.633878 YDOT = -9482.175790 feet/sec YDOT = -2811.037535 meter/sec ZDOT = 1805.526459 ZDOT = 584.696105 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13858183.39 X = 4223974.30 Y = -1725749.55 feet Y = -526008.46 meter Z = -17405519.22 Z = -5305202.26 XDOT = 5399.486940 XDOT = 1645.763619 YDOT = 23392.944850 feet/sec YDOT = 7130.169590 meter/sec ZDOT = 1963.046954 ZDOT = 598.336712 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 20026.39359684 .00016717 00000-0 10270-3 0 9060 2 25544 51.6412 334.9961 0005477 193.0075 167.0935 15.49060609 9879 Satellite: ISS Catalog Number: 25544 Epoch time: 20026.39359684 = yrday.fracday Element set: 906 Inclination: 51.6412 deg RA of node: 334.9961 deg Eccentricity: .0005477 Arg of perigee: 193.0075 deg Mean anomaly: 167.0935 deg Mean motion: 15.49060609 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 987 Checksum: 333 Coasting Arc #8 (Orbit 1002) --------------------------------------- Vector Time (GMT): 2020/027/09:05:00.000 Vector Time (MET): N/A Weight (LBS) : 936097.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1567283.75 A = 6792210.61 meter Y = 3967839.50 meter E = .0004053 Z = 5283990.59 I = 51.42671 XDOT = -6807.016421 Wp = 164.57242 YDOT = 3467.078072 meter/sec RA = 329.48793 deg ZDOT = -588.185030 TA = 291.04110 MA = 291.08444 Ha = 229.276 n.mi Hp = 222.964 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5142007.06 X = 1497131.88 Y = 13017846.11 feet Y = 3984973.63 meter Z = 17335927.14 Z = 5291433.31 XDOT = -22332.731041 XDOT = -6842.423417 YDOT = 11374.928058 feet/sec YDOT = 3390.759228 meter/sec ZDOT = -1929.740912 ZDOT = -621.335807 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13619901.52 X = -4151345.98 Y = 3038677.64 feet Y = 926188.94 meter Z = 17369618.44 Z = 5294259.70 XDOT = -7718.444360 XDOT = -2352.581841 YDOT = -22765.739173 feet/sec YDOT = -6938.997300 meter/sec ZDOT = -2081.712682 ZDOT = -634.506025 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 20027.42578189 .00016717 00000-0 10270-3 0 9079 2 25544 51.6413 329.8898 0005412 197.6504 162.4458 15.49082565 10032 Satellite: ISS Catalog Number: 25544 Epoch time: 20027.42578189 = yrday.fracday Element set: 907 Inclination: 51.6413 deg RA of node: 329.8898 deg Eccentricity: .0005412 Arg of perigee: 197.6504 deg Mean anomaly: 162.4458 deg Mean motion: 15.49082565 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1003 Checksum: 325 Coasting Arc #9 (Orbit 1017) --------------------------------------- Vector Time (GMT): 2020/028/09:05:00.000 Vector Time (MET): N/A Weight (LBS) : 936097.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1856244.79 A = 6792280.94 meter Y = -3857890.37 meter E = .0014110 Z = -5284745.17 I = 51.39818 XDOT = 6489.802470 Wp = 116.12055 YDOT = -4000.810845 meter/sec RA = 324.52642 deg ZDOT = 636.341793 TA = 160.01684 MA = 159.96153 Ha = 229.237 n.mi Hp = 223.012 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6090041.95 X = -1787297.20 Y = -12657120.64 feet Y = -3878262.69 meter Z = -17338402.77 Z = -5293594.38 XDOT = 21292.002854 XDOT = 6530.967480 YDOT = -13126.019833 feet/sec YDOT = -3928.007107 meter/sec ZDOT = 2087.735540 ZDOT = 667.965824 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13332410.69 X = 4063718.78 Y = -4259641.78 feet Y = -1298338.81 meter Z = -17378544.29 Z = -5296980.30 XDOT = 9909.571342 XDOT = 3020.437345 YDOT = 21843.634303 feet/sec YDOT = 6657.939736 meter/sec ZDOT = 2232.752675 ZDOT = 680.543015 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 20028.39345345 .00016717 00000-0 10270-3 0 9083 2 25544 51.6409 325.1030 0005312 201.0402 159.0530 15.49070131 10185 Satellite: ISS Catalog Number: 25544 Epoch time: 20028.39345345 = yrday.fracday Element set: 908 Inclination: 51.6409 deg RA of node: 325.1030 deg Eccentricity: .0005312 Arg of perigee: 201.0402 deg Mean anomaly: 159.0530 deg Mean motion: 15.49070131 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1018 Checksum: 252 Coasting Arc #10 (Orbit 1033) --------------------------------------- Vector Time (GMT): 2020/029/09:05:00.000 Vector Time (MET): N/A Weight (LBS) : 936097.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2149267.12 A = 6792252.98 meter Y = 3703434.72 meter E = .0003437 Z = 5271811.81 I = 51.37102 XDOT = -6144.698694 Wp = 172.02931 YDOT = 4525.346720 meter/sec RA = 319.56325 deg ZDOT = -677.194978 TA = 284.44847 MA = 284.48661 Ha = 229.002 n.mi Hp = 223.256 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 7051401.32 X = 2082087.67 Y = 12150376.39 feet Y = 3727093.78 meter Z = 17295970.52 Z = 5282088.67 XDOT = -20159.772619 XDOT = -6191.556420 YDOT = 14846.938058 feet/sec YDOT = 4456.370339 meter/sec ZDOT = -2221.768302 ZDOT = -707.156644 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -12863504.70 X = -3920796.23 Y = 5501531.86 feet Y = 1676866.91 meter Z = 17342661.19 Z = 5286043.13 XDOT = -12048.975483 XDOT = -3672.527727 YDOT = -20769.398130 feet/sec YDOT = -6330.512550 meter/sec ZDOT = -2359.208166 ZDOT = -719.086649 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 20029.42563530 .00016717 00000-0 10270-3 0 9097 2 25544 51.6403 319.9970 0005333 205.6654 154.4232 15.49081311 10343 Satellite: ISS Catalog Number: 25544 Epoch time: 20029.42563530 = yrday.fracday Element set: 909 Inclination: 51.6403 deg RA of node: 319.9970 deg Eccentricity: .0005333 Arg of perigee: 205.6654 deg Mean anomaly: 154.4232 deg Mean motion: 15.49081311 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1034 Checksum: 284 Coasting Arc #11 (Orbit 1048) --------------------------------------- Vector Time (GMT): 2020/030/09:05:00.000 Vector Time (MET): N/A Weight (LBS) : 936097.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2418448.41 A = 6792284.71 meter Y = -3551929.81 meter E = .0013317 Z = -5271197.16 I = 51.34680 XDOT = 5746.280800 Wp = 117.06765 YDOT = -4998.870699 meter/sec RA = 314.59752 deg ZDOT = 727.495122 TA = 159.95206 MA = 159.89970 Ha = 228.950 n.mi Hp = 223.278 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -7934542.02 X = -2352946.01 Y = -11653313.01 feet Y = -3578608.44 meter Z = -17293953.93 Z = -5282785.65 XDOT = 18852.627296 XDOT = 5798.218884 YDOT = -16400.494420 feet/sec YDOT = -4934.321299 meter/sec ZDOT = 2386.795021 ZDOT = 755.533943 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12357957.12 X = 3766705.33 Y = -6649191.15 feet Y = -2026673.46 meter Z = -17346661.26 Z = -5287262.35 XDOT = 14010.020111 XDOT = 4270.254130 YDOT = 19437.606380 feet/sec YDOT = 5924.582425 meter/sec ZDOT = 2515.461535 ZDOT = 766.712676 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 20030.39330295 .00016717 00000-0 10270-3 0 9107 2 25544 51.6408 315.2097 0005323 209.6041 150.4808 15.49082812 10498 Satellite: ISS Catalog Number: 25544 Epoch time: 20030.39330295 = yrday.fracday Element set: 910 Inclination: 51.6408 deg RA of node: 315.2097 deg Eccentricity: .0005323 Arg of perigee: 209.6041 deg Mean anomaly: 150.4808 deg Mean motion: 15.49082812 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1049 Checksum: 279 Coasting Arc #12 (Orbit 1064) --------------------------------------- Vector Time (GMT): 2020/031/09:05:00.000 Vector Time (MET): N/A Weight (LBS) : 936097.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2683120.50 A = 6792267.85 meter Y = 3359031.86 meter E = .0002777 Z = 5258326.53 I = 51.32482 XDOT = -5321.721985 Wp = 181.43260 YDOT = 5456.197159 meter/sec RA = 309.63054 deg ZDOT = -772.696240 TA = 275.97473 MA = 276.00638 Ha = 228.685 n.mi Hp = 223.528 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 8802888.77 X = 2619817.90 Y = 11020445.73 feet Y = 3388682.53 meter Z = 17251727.45 Z = 5271206.06 XDOT = -17459.717798 XDOT = -5378.586012 YDOT = 17900.909313 feet/sec YDOT = 5396.367934 meter/sec ZDOT = -2535.092652 ZDOT = -798.684815 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -11680323.28 X = -3560162.54 Y = 7777190.04 feet Y = 2370487.52 meter Z = 17310359.26 Z = 5276197.50 XDOT = -15882.476013 XDOT = -4840.978689 YDOT = -17965.161437 feet/sec YDOT = -5475.781206 meter/sec ZDOT = -2654.402526 ZDOT = -809.061890 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 20031.42547902 .00016717 00000-0 10270-3 0 9118 2 25544 51.6414 310.1034 0005240 214.0776 146.0039 15.49091845 10654 Satellite: ISS Catalog Number: 25544 Epoch time: 20031.42547902 = yrday.fracday Element set: 911 Inclination: 51.6414 deg RA of node: 310.1034 deg Eccentricity: .0005240 Arg of perigee: 214.0776 deg Mean anomaly: 146.0039 deg Mean motion: 15.49091845 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1065 Checksum: 266 Coasting Arc #13 (Orbit 1067) --------------------------------------- Vector Time (GMT): 2020/031/14:35:00.000 Vector Time (MET): N/A Weight (LBS) : 920821.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1104300.53 A = 6794391.10 meter Y = -4731634.24 meter E = .0010709 Z = -4759078.36 I = 51.32989 XDOT = 5926.859939 Wp = 136.38143 YDOT = -4050.716795 meter/sec RA = 308.47949 deg ZDOT = 2648.065403 TA = 159.95154 MA = 159.90944 Ha = 228.675 n.mi Hp = 223.522 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3623033.24 X = -1028191.43 Y = -15523734.39 feet Y = -4743557.81 meter Z = -15613774.14 Z = -4764257.63 XDOT = 19445.078540 XDOT = 5958.853173 YDOT = -13289.753263 feet/sec YDOT = -3984.259530 meter/sec ZDOT = 8687.878620 ZDOT = 2676.933044 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -251997.37 X = -76808.80 Y = -15916060.05 feet Y = -4851215.10 meter Z = -15637076.84 Z = -4766181.02 XDOT = 20542.180187 XDOT = 6261.256521 YDOT = -9003.809639 feet/sec YDOT = -2744.361178 meter/sec ZDOT = 8820.238053 ZDOT = 2688.408559 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 20031.61901044 .00016717 00000-0 10270-3 0 9121 2 25544 51.6441 309.1472 0005272 216.6802 143.3988 15.49114788 10689 Satellite: ISS Catalog Number: 25544 Epoch time: 20031.61901044 = yrday.fracday Element set: 912 Inclination: 51.6441 deg RA of node: 309.1472 deg Eccentricity: .0005272 Arg of perigee: 216.6802 deg Mean anomaly: 143.3988 deg Mean motion: 15.49114788 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1068 Checksum: 294 Coasting Arc #14 (Orbit 1071) --------------------------------------- Vector Time (GMT): 2020/031/19:42:00.000 Vector Time (MET): N/A Weight (LBS) : 920821.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5296967.66 A = 6797684.32 meter Y = -1895718.87 meter E = .0010300 Z = 3813433.29 I = 51.33279 XDOT = -712.074435 Wp = 127.16120 YDOT = 6394.725464 meter/sec RA = 307.46088 deg ZDOT = 4154.119124 TA = 278.77829 MA = 278.89493 Ha = 228.794 n.mi Hp = 223.436 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17378502.82 X = 5299249.28 Y = -6219550.10 feet Y = -1836471.63 meter Z = 12511264.07 Z = 3839169.04 XDOT = -2336.202214 XDOT = -803.707225 YDOT = 20980.070420 feet/sec YDOT = 6386.250230 meter/sec ZDOT = 13628.999751 ZDOT = 4150.437586 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 1639632.89 X = 499760.11 Y = -18304200.92 feet Y = -5579120.44 meter Z = 12629122.09 Z = 3849356.41 XDOT = 16673.735958 XDOT = 5082.154720 YDOT = 10916.193335 feet/sec YDOT = 3327.255728 meter/sec ZDOT = 13611.643628 ZDOT = 4148.828978 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 20031.87705412 .00016717 00000-0 10270-3 0 9131 2 25544 51.6403 307.8651 0005603 213.1744 146.9055 15.49121225 10729 Satellite: ISS Catalog Number: 25544 Epoch time: 20031.87705412 = yrday.fracday Element set: 913 Inclination: 51.6403 deg RA of node: 307.8651 deg Eccentricity: .0005603 Arg of perigee: 213.1744 deg Mean anomaly: 146.9055 deg Mean motion: 15.49121225 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1072 Checksum: 274 Coasting Arc #15 (Orbit 1086) --------------------------------------- Vector Time (GMT): 2020/032/19:42:00.000 Vector Time (MET): N/A Weight (LBS) : 920821.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5113034.46 A = 6797576.89 meter Y = 2281838.60 meter E = .0004002 Z = -3854838.31 I = 51.31305 XDOT = 211.837156 Wp = 132.48314 YDOT = -6457.984394 meter/sec RA = 302.49255 deg ZDOT = -4109.118461 TA = 94.10933 MA = 94.06358 Ha = 228.618 n.mi Hp = 223.494 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16775047.45 X = -5119446.29 Y = 7486347.11 feet Y = 2224625.18 meter Z = -12647107.31 Z = -3879690.66 XDOT = 695.003793 XDOT = 303.995968 YDOT = -21187.612840 feet/sec YDOT = -6455.100181 meter/sec ZDOT = -13481.359780 ZDOT = -4107.865631 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 78494.84 X = 23925.23 Y = 18290680.07 feet Y = 5574999.28 meter Z = -12760948.02 Z = -3889536.96 XDOT = -17717.233537 XDOT = -5400.212782 YDOT = -9312.989701 feet/sec YDOT = -2838.599261 meter/sec ZDOT = -13475.118326 ZDOT = -4107.216066 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 20032.84471721 .00016717 00000-0 10270-3 0 9143 2 25544 51.6404 303.0786 0005468 216.2211 143.8569 15.49111671 10875 Satellite: ISS Catalog Number: 25544 Epoch time: 20032.84471721 = yrday.fracday Element set: 914 Inclination: 51.6404 deg RA of node: 303.0786 deg Eccentricity: .0005468 Arg of perigee: 216.2211 deg Mean anomaly: 143.8569 deg Mean motion: 15.49111671 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1087 Checksum: 292 Coasting Arc #16 (Orbit 1102) --------------------------------------- Vector Time (GMT): 2020/033/19:42:00.000 Vector Time (MET): N/A Weight (LBS) : 920821.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4898018.86 A = 6797472.55 meter Y = -2680927.16 meter E = .0009544 Z = 3875046.40 I = 51.29615 XDOT = 309.173844 Wp = 129.37356 YDOT = 6475.959649 meter/sec RA = 297.52168 deg ZDOT = 4076.853242 TA = 277.56231 MA = 277.67071 Ha = 228.545 n.mi Hp = 223.711 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 16069615.68 X = 4908811.22 Y = -8795692.80 feet Y = -2626093.77 meter Z = 12713406.82 Z = 3898864.92 XDOT = 1014.349882 XDOT = 216.932012 YDOT = 21246.586775 feet/sec YDOT = 6478.901221 meter/sec ZDOT = 13375.502762 ZDOT = 4078.131148 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -1873988.69 X = -571191.75 Y = -18146569.94 feet Y = -5531074.52 meter Z = 12822544.15 Z = 3908311.46 XDOT = 18605.473800 XDOT = 5670.948414 YDOT = 7562.865292 feet/sec YDOT = 2305.161341 meter/sec ZDOT = 13380.845486 ZDOT = 4078.481704 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 20033.87688844 .00016717 00000-0 10270-3 0 9154 2 25544 51.6407 297.9716 0005669 220.5350 139.5378 15.49127696 11030 Satellite: ISS Catalog Number: 25544 Epoch time: 20033.87688844 = yrday.fracday Element set: 915 Inclination: 51.6407 deg RA of node: 297.9716 deg Eccentricity: .0005669 Arg of perigee: 220.5350 deg Mean anomaly: 139.5378 deg Mean motion: 15.49127696 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1103 Checksum: 338 Coasting Arc #17 (Orbit 1117) --------------------------------------- Vector Time (GMT): 2020/034/19:42:00.000 Vector Time (MET): N/A Weight (LBS) : 920821.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4657520.64 A = 6797383.64 meter Y = 3029520.64 meter E = .0003247 Z = -3916407.36 I = 51.28223 XDOT = -816.198911 Wp = 129.30751 YDOT = -6459.493248 meter/sec RA = 292.55015 deg ZDOT = -4030.334043 TA = 98.28893 MA = 98.25211 Ha = 228.339 n.mi Hp = 223.793 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -15280579.52 X = -4672028.06 Y = 9939372.18 feet Y = 2977355.96 meter Z = -12849105.51 Z = -3939066.60 XDOT = -2677.817949 XDOT = -724.329505 YDOT = -21192.563149 feet/sec YDOT = -6468.106746 meter/sec ZDOT = -13222.880719 ZDOT = -4034.075863 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 3541853.22 X = 1079556.86 Y = 17806256.75 feet Y = 5427347.06 meter Z = -12952962.54 Z = -3948062.98 XDOT = -19326.890033 XDOT = -5890.836082 YDOT = -5776.496440 feet/sec YDOT = -1760.676115 meter/sec ZDOT = -13239.505086 ZDOT = -4035.401150 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 20034.84454796 .00016717 00000-0 10270-3 0 9160 2 25544 51.6417 293.1843 0005533 224.4137 135.6570 15.49111817 11181 Satellite: ISS Catalog Number: 25544 Epoch time: 20034.84454796 = yrday.fracday Element set: 916 Inclination: 51.6417 deg RA of node: 293.1843 deg Eccentricity: .0005533 Arg of perigee: 224.4137 deg Mean anomaly: 135.6570 deg Mean motion: 15.49111817 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1118 Checksum: 305 Coasting Arc #18 (Orbit 1122) --------------------------------------- Vector Time (GMT): 2020/035/03:40:00.000 Vector Time (MET): N/A Weight (LBS) : 920821.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3494610.20 A = 6792418.95 meter Y = -2596504.49 meter E = .0011620 Z = -5223466.49 I = 51.26303 XDOT = 3460.292154 Wp = 118.40887 YDOT = -6746.085994 meter/sec RA = 290.86945 deg ZDOT = 1034.707305 TA = 161.59497 MA = 161.55289 Ha = 228.293 n.mi Hp = 223.820 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -11465256.57 X = -3439943.35 Y = -8518715.53 feet Y = -2635277.83 meter Z = -17137357.24 Z = -5240309.03 XDOT = 11352.664546 XDOT = 3530.445747 YDOT = -22132.828064 feet/sec YDOT = -6706.998343 meter/sec ZDOT = 3394.709007 ZDOT = 1051.685927 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12410458.49 X = 3782707.75 Y = 6881993.29 feet Y = 2097631.56 meter Z = -17214189.62 Z = -5246884.99 XDOT = -7683.646278 XDOT = -2341.975386 YDOT = 22572.794062 feet/sec YDOT = 6880.187630 meter/sec ZDOT = 3472.863495 ZDOT = 1058.528793 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 20035.16709933 .00016717 00000-0 10270-3 0 9173 2 25544 51.6435 291.5926 0005270 227.8266 132.2437 15.49096583 11236 Satellite: ISS Catalog Number: 25544 Epoch time: 20035.16709933 = yrday.fracday Element set: 917 Inclination: 51.6435 deg RA of node: 291.5926 deg Eccentricity: .0005270 Arg of perigee: 227.8266 deg Mean anomaly: 132.2437 deg Mean motion: 15.49096583 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1123 Checksum: 313 Coasting Arc #19 (Orbit 1138) --------------------------------------- Vector Time (GMT): 2020/036/03:40:00.000 Vector Time (MET): N/A Weight (LBS) : 920821.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3682423.82 A = 6792380.37 meter Y = 2333449.73 meter E = .0001347 Z = 5209205.43 I = 51.25064 XDOT = -2902.416055 Wp = 212.33061 YDOT = 7005.078493 meter/sec RA = 285.89653 deg ZDOT = -1087.416495 TA = 248.14982 MA = 248.16415 Ha = 228.027 n.mi Hp = 223.980 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12081442.97 X = 3630753.91 Y = 7655674.96 feet Y = 2374340.02 meter Z = 17090569.00 Z = 5226967.53 XDOT = -9522.362386 XDOT = -2975.251230 YDOT = 22982.540986 feet/sec YDOT = 6972.214430 meter/sec ZDOT = -3567.639420 ZDOT = -1101.691579 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13003005.30 X = -3963316.01 Y = -5719704.02 feet Y = -1743365.79 meter Z = 17171633.91 Z = 5233914.02 XDOT = 5422.773759 XDOT = 1652.861442 YDOT = -23223.996339 feet/sec YDOT = -7078.674084 meter/sec ZDOT = -3633.435935 ZDOT = -1107.471273 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 20036.19926591 .00016717 00000-0 10270-3 0 9189 2 25544 51.6419 286.4861 0005086 230.7257 129.3443 15.49118417 11399 Satellite: ISS Catalog Number: 25544 Epoch time: 20036.19926591 = yrday.fracday Element set: 918 Inclination: 51.6419 deg RA of node: 286.4861 deg Eccentricity: .0005086 Arg of perigee: 230.7257 deg Mean anomaly: 129.3443 deg Mean motion: 15.49118417 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1139 Checksum: 322 Coasting Arc #20 (Orbit 1153) --------------------------------------- Vector Time (GMT): 2020/037/03:40:00.000 Vector Time (MET): N/A Weight (LBS) : 920821.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3854584.96 A = 6792496.70 meter Y = -2073218.85 meter E = .0010945 Z = -5203717.28 I = 51.24202 XDOT = 2324.711672 Wp = 117.86873 YDOT = -7200.524474 meter/sec RA = 280.92353 deg ZDOT = 1143.602720 TA = 163.19813 MA = 163.16184 Ha = 228.004 n.mi Hp = 224.008 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12646276.10 X = -3805839.00 Y = -6801899.12 feet Y = -2116050.69 meter Z = -17072563.24 Z = -5222322.67 XDOT = 7627.006797 XDOT = 2399.502426 YDOT = -23623.767959 feet/sec YDOT = -7174.109785 meter/sec ZDOT = 3751.977429 ZDOT = 1155.076247 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13509896.87 X = 4117816.57 Y = 4557299.70 feet Y = 1389064.95 meter Z = -17157513.00 Z = -5229609.96 XDOT = -3112.540817 XDOT = -948.702441 YDOT = 23590.972857 feet/sec YDOT = 7190.528527 meter/sec ZDOT = 3804.959800 ZDOT = 1159.751747 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 20037.16692164 .00016717 00000-0 10270-3 0 9194 2 25544 51.6411 281.6997 0005209 235.6004 124.4654 15.49095508 11541 Satellite: ISS Catalog Number: 25544 Epoch time: 20037.16692164 = yrday.fracday Element set: 919 Inclination: 51.6411 deg RA of node: 281.6997 deg Eccentricity: .0005209 Arg of perigee: 235.6004 deg Mean anomaly: 124.4654 deg Mean motion: 15.49095508 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1154 Checksum: 309 Coasting Arc #21 (Orbit 1155) --------------------------------------- Vector Time (GMT): 2020/037/05:49:00.000 Vector Time (MET): N/A Weight (LBS) : 905713.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4256826.10 A = 6794735.40 meter Y = -2571982.70 meter E = .0007012 Z = 4630045.13 I = 51.24780 XDOT = 1068.916495 Wp = 154.96616 YDOT = 7006.797992 meter/sec RA = 280.50940 deg ZDOT = 2901.650260 TA = 265.92818 MA = 266.00833 Ha = 227.826 n.mi Hp = 224.171 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13965964.88 X = 4262780.78 Y = -8438263.46 feet Y = -2524346.83 meter Z = 15190436.78 Z = 4650736.98 XDOT = 3506.943880 XDOT = 976.390734 YDOT = 22988.182388 feet/sec YDOT = 7018.233861 meter/sec ZDOT = 9519.849936 ZDOT = 2906.618208 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -4603104.24 X = -1403026.17 Y = 15561948.02 feet Y = 4743281.76 meter Z = 15285255.64 Z = 4658945.92 XDOT = -16856.216524 XDOT = -5137.774797 YDOT = -14383.538494 feet/sec YDOT = -4384.102533 meter/sec ZDOT = 9542.081213 ZDOT = 2908.426354 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 20037.29594227 .00016717 00000-0 10270-3 0 9201 2 25544 51.6396 281.0613 0005286 237.6362 122.4277 15.49136037 11560 Satellite: ISS Catalog Number: 25544 Epoch time: 20037.29594227 = yrday.fracday Element set: 920 Inclination: 51.6396 deg RA of node: 281.0613 deg Eccentricity: .0005286 Arg of perigee: 237.6362 deg Mean anomaly: 122.4277 deg Mean motion: 15.49136037 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1156 Checksum: 305