ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 10979.19 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 119.7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2.152 ET - UTC (sec) : 66.18 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 ------------------------------------------------------------------------ There are no maneuvers. Coasting Arc #1 (Orbit 3701) --------------------------------------- Vector Time (GMT): 2012/034/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3667057.92 A = 6764650.21 meter Y = 2247285.80 meter E = .0018467 Z = 5214974.97 I = 51.96161 XDOT = -2635.417598 Wp = 11.62583 YDOT = -7110.375691 meter/sec RA = 76.94051 deg ZDOT = 1227.785041 TA = 66.76277 MA = 66.56842 Ha = 219.888 n.mi Hp = 203.505 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12031029.93 X = -3717247.70 Y = 7372984.89 feet Y = 2205997.67 meter Z = 17109497.92 Z = 5197039.06 XDOT = -8646.383194 XDOT = -2561.676280 YDOT = -23328.004235 feet/sec YDOT = -7139.434290 meter/sec ZDOT = 4028.166145 ZDOT = 1215.161362 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13619608.08 X = -4151256.54 Y = -4016221.84 feet Y = -1224144.42 meter Z = 17035778.37 Z = 5192505.25 XDOT = 11131.879492 XDOT = 3392.996869 YDOT = -21116.585630 feet/sec YDOT = -6436.335300 meter/sec ZDOT = 3976.966266 ZDOT = 1212.179318 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 12034.55019472 .00016717 00000-0 10270-3 0 9000 2 25544 51.6407 77.4144 0020358 1.3772 358.7436 15.58661152 37028 Satellite: ISS Catalog Number: 25544 Epoch time: 12034.55019472 = yrday.fracday Element set: 900 Inclination: 51.6407 deg RA of node: 77.4144 deg Eccentricity: .0020358 Arg of perigee: 1.3772 deg Mean anomaly: 358.7436 deg Mean motion: 15.58661152 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3702 Checksum: 292 Coasting Arc #2 (Orbit 3716) --------------------------------------- Vector Time (GMT): 2012/035/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4470246.89 A = 6766011.83 meter Y = 1302198.87 meter E = .0021464 Z = -4914404.46 I = 51.95903 XDOT = 441.595210 Wp = 38.06095 YDOT = 7287.467865 meter/sec RA = 71.91611 deg ZDOT = 2354.583594 TA = 254.75811 MA = 254.99552 Ha = 220.038 n.mi Hp = 203.303 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14666164.35 X = 4479225.76 Y = 4272306.00 feet Y = 1352238.30 meter Z = -16123374.20 Z = -4892666.81 XDOT = 1448.803182 XDOT = 348.634676 YDOT = 23909.015304 feet/sec YDOT = 7291.886198 meter/sec ZDOT = 7725.011792 ZDOT = 2356.503266 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 7009313.80 X = 2136438.85 Y = 13677775.36 feet Y = 4168985.93 meter Z = -16034342.90 Z = -4887267.72 XDOT = -15451.097658 XDOT = -4709.494566 YDOT = 16897.902741 feet/sec YDOT = 5150.480755 meter/sec ZDOT = 7732.301048 ZDOT = 2356.805359 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 12035.51191994 .00016717 00000-0 10270-3 0 9018 2 25544 51.6416 72.5874 0020468 4.9178 355.2174 15.58656749 37178 Satellite: ISS Catalog Number: 25544 Epoch time: 12035.51191994 = yrday.fracday Element set: 901 Inclination: 51.6416 deg RA of node: 72.5874 deg Eccentricity: .0020468 Arg of perigee: 4.9178 deg Mean anomaly: 355.2174 deg Mean motion: 15.58656749 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3717 Checksum: 330 Coasting Arc #3 (Orbit 3732) --------------------------------------- Vector Time (GMT): 2012/036/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4279558.50 A = 6772736.16 meter Y = -4443199.80 meter E = .0024256 Z = 2805988.85 I = 51.97057 XDOT = 2104.812043 Wp = 42.44820 YDOT = -5294.300381 meter/sec RA = 66.91394 deg ZDOT = -5129.971998 TA = 105.84124 MA = 105.57371 Ha = 220.044 n.mi Hp = 202.953 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -14040546.26 X = -4243186.20 Y = -14577427.16 feet Y = -4490853.15 meter Z = 9206000.16 Z = 2785287.71 XDOT = 6905.551323 XDOT = 2188.777150 YDOT = -17369.751907 feet/sec YDOT = -5270.293483 meter/sec ZDOT = -16830.616791 ZDOT = -5119.543354 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 603545.30 X = 183960.61 Y = -20268776.27 feet Y = -6177923.01 meter Z = 9121469.31 Z = 2780223.84 XDOT = 15853.820029 XDOT = 4832.244345 YDOT = -7147.121373 feet/sec YDOT = -2178.442595 meter/sec ZDOT = -16787.425129 ZDOT = -5116.807179 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 12036.53774461 .00016717 00000-0 10270-3 0 9028 2 25544 51.6405 67.4376 0020524 9.0384 351.1137 15.58717680 37338 Satellite: ISS Catalog Number: 25544 Epoch time: 12036.53774461 = yrday.fracday Element set: 902 Inclination: 51.6405 deg RA of node: 67.4376 deg Eccentricity: .0020524 Arg of perigee: 9.0384 deg Mean anomaly: 351.1137 deg Mean motion: 15.58717680 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3733 Checksum: 300 Coasting Arc #4 (Orbit 3748) --------------------------------------- Vector Time (GMT): 2012/037/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2984581.37 A = 6776036.27 meter Y = 6055034.40 meter E = .0031771 Z = 274009.07 I = 51.96900 XDOT = -4367.040814 Wp = 25.89243 YDOT = 1868.149002 meter/sec RA = 61.94157 deg ZDOT = 6050.572517 TA = 337.05897 MA = 337.20057 Ha = 220.203 n.mi Hp = 202.625 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 9791933.63 X = 2915319.90 Y = 19865598.44 feet Y = 6088022.57 meter Z = 898979.90 Z = 288339.41 XDOT = -14327.561725 XDOT = -4416.997755 YDOT = 6129.097775 feet/sec YDOT = 1819.034726 meter/sec ZDOT = 19850.959703 ZDOT = 6029.236887 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7039064.84 X = -2145506.96 Y = 20996841.63 feet Y = 6399837.33 meter Z = 957255.42 Z = 291771.45 XDOT = -13044.271274 XDOT = -3975.893884 YDOT = -5306.928413 feet/sec YDOT = -1617.551780 meter/sec ZDOT = 19763.314324 ZDOT = 6023.858206 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 12037.56355610 .00016717 00000-0 10270-3 0 9034 2 25544 51.6409 62.2885 0020593 12.9097 347.2581 15.58706756 37498 Satellite: ISS Catalog Number: 25544 Epoch time: 12037.56355610 = yrday.fracday Element set: 903 Inclination: 51.6409 deg RA of node: 62.2885 deg Eccentricity: .0020593 Arg of perigee: 12.9097 deg Mean anomaly: 347.2581 deg Mean motion: 15.58706756 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3749 Checksum: 326 Coasting Arc #5 (Orbit 3763) --------------------------------------- Vector Time (GMT): 2012/038/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -738219.26 A = 6771300.47 meter Y = -5881009.26 meter E = .0021949 Z = -3304200.45 I = 51.93799 XDOT = 5690.939333 Wp = 28.28723 YDOT = 1949.568289 meter/sec RA = 56.96365 deg ZDOT = -4735.461607 TA = 189.91449 MA = 189.95786 Ha = 220.230 n.mi Hp = 202.404 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -2421979.20 X = -656351.17 Y = -19294649.80 feet Y = -5888806.81 meter Z = -10840552.65 Z = -3307587.59 XDOT = 18671.060804 XDOT = 5691.719050 YDOT = 6396.221419 feet/sec YDOT = 2013.212125 meter/sec ZDOT = -15536.291362 ZDOT = -4707.814231 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 11647380.47 X = 3550121.57 Y = -15562681.37 feet Y = -4743505.28 meter Z = -10853964.84 Z = -3308288.48 XDOT = 7990.530972 XDOT = 2435.513840 YDOT = 16750.456193 feet/sec YDOT = 5105.539047 meter/sec ZDOT = -15423.070906 ZDOT = -4700.952012 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 12038.52523870 .00016717 00000-0 10270-3 0 9047 2 25544 51.6405 57.4601 0020526 16.5619 343.6203 15.58742510 37648 Satellite: ISS Catalog Number: 25544 Epoch time: 12038.52523870 = yrday.fracday Element set: 904 Inclination: 51.6405 deg RA of node: 57.4601 deg Eccentricity: .0020526 Arg of perigee: 16.5619 deg Mean anomaly: 343.6203 deg Mean motion: 15.58742510 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3764 Checksum: 289 Coasting Arc #6 (Orbit 3779) --------------------------------------- Vector Time (GMT): 2012/039/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1972743.38 A = 6764806.53 meter Y = 3966493.71 meter E = .0019893 Z = 5098688.28 I = 51.89781 XDOT = -5603.399780 Wp = 34.42564 YDOT = -4976.179932 meter/sec RA = 51.95088 deg ZDOT = 1715.943704 TA = 39.16875 MA = 39.02494 Ha = 220.429 n.mi Hp = 202.104 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6472255.18 X = -2041718.49 Y = 13013430.82 feet Y = 3944047.87 meter Z = 16727979.94 Z = 5088937.32 XDOT = -18383.857545 XDOT = -5555.674123 YDOT = -16326.049647 feet/sec YDOT = -5038.573670 meter/sec ZDOT = 5629.736563 ZDOT = 1688.839548 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13664724.56 X = -4165008.05 Y = 5085447.50 feet Y = 1550044.40 meter Z = 16687669.34 Z = 5086401.61 XDOT = -2055.444418 XDOT = -626.499459 YDOT = -23495.468350 feet/sec YDOT = -7161.418753 meter/sec ZDOT = 5518.991714 ZDOT = 1682.188674 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 12039.55101961 .00016717 00000-0 10270-3 0 9055 2 25544 51.6393 52.3093 0020581 20.5198 339.6779 15.58760295 37802 Satellite: ISS Catalog Number: 25544 Epoch time: 12039.55101961 = yrday.fracday Element set: 905 Inclination: 51.6393 deg RA of node: 52.3093 deg Eccentricity: .0020581 Arg of perigee: 20.5198 deg Mean anomaly: 339.6779 deg Mean motion: 15.58760295 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3780 Checksum: 321 Coasting Arc #7 (Orbit 3794) --------------------------------------- Vector Time (GMT): 2012/040/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4363911.42 A = 6765133.12 meter Y = -1140952.82 meter E = .0026031 Z = -5055252.10 I = 51.87976 XDOT = 3859.268835 Wp = 52.80560 YDOT = 6336.730021 meter/sec RA = 46.92031 deg ZDOT = 1923.424079 TA = 235.67220 MA = 235.91882 Ha = 220.478 n.mi Hp = 202.006 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14317294.69 X = 4400902.14 Y = -3743283.51 feet Y = -1091946.37 meter Z = -16585472.77 Z = -5033963.00 XDOT = 12661.643161 XDOT = 3778.780083 YDOT = 20789.796658 feet/sec YDOT = 6379.436834 meter/sec ZDOT = 6310.446454 ZDOT = 1941.975866 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13243361.16 X = 4036576.48 Y = 6819223.53 feet Y = 2078499.33 meter Z = -16498078.11 Z = -5028614.21 XDOT = -3950.878946 XDOT = -1204.227903 YDOT = 22946.358401 feet/sec YDOT = 6994.050041 meter/sec ZDOT = 6386.004121 ZDOT = 1946.454056 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 12040.51267474 .00016717 00000-0 10270-3 0 9066 2 25544 51.6399 47.4821 0020592 23.6966 336.5132 15.58762003 37955 Satellite: ISS Catalog Number: 25544 Epoch time: 12040.51267474 = yrday.fracday Element set: 906 Inclination: 51.6399 deg RA of node: 47.4821 deg Eccentricity: .0020592 Arg of perigee: 23.6966 deg Mean anomaly: 336.5132 deg Mean motion: 15.58762003 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3795 Checksum: 315 Coasting Arc #8 (Orbit 3810) --------------------------------------- Vector Time (GMT): 2012/041/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5723915.45 A = 6771680.01 meter Y = -1869057.54 meter E = .0028254 Z = 3099534.06 I = 51.88004 XDOT = -767.083063 Wp = 52.48478 YDOT = -5853.543066 meter/sec RA = 41.90659 deg ZDOT = -4898.997722 TA = 91.94099 MA = 91.61740 Ha = 220.490 n.mi Hp = 201.636 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18779250.17 X = -5717646.41 Y = -6132078.54 feet Y = -1933030.61 meter Z = 10169075.00 Z = 3071743.44 XDOT = -2516.676717 XDOT = -677.772791 YDOT = -19204.537618 feet/sec YDOT = -5861.622061 meter/sec ZDOT = -16072.827171 ZDOT = -4902.506745 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -10250779.35 X = -3124437.54 Y = -16955404.83 feet Y = -5168007.39 meter Z = 10055271.27 Z = 3064846.68 XDOT = 9486.338769 XDOT = 2891.436057 YDOT = -15368.437887 feet/sec YDOT = -4684.299868 meter/sec ZDOT = -16086.733649 ZDOT = -4903.236416 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 12041.53842440 .00016717 00000-0 10270-3 0 9072 2 25544 51.6392 42.3307 0020707 27.4356 332.7888 15.58837787 38111 Satellite: ISS Catalog Number: 25544 Epoch time: 12041.53842440 = yrday.fracday Element set: 907 Inclination: 51.6392 deg RA of node: 42.3307 deg Eccentricity: .0020707 Arg of perigee: 27.4356 deg Mean anomaly: 332.7888 deg Mean motion: 15.58837787 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3811 Checksum: 317 Coasting Arc #9 (Orbit 3825) --------------------------------------- Vector Time (GMT): 2012/042/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5429526.21 A = 6775580.33 meter Y = 4023369.71 meter E = .0032395 Z = -58136.44 I = 51.87047 XDOT = -2797.148948 Wp = 36.28916 YDOT = 3837.079506 meter/sec RA = 36.92597 deg ZDOT = 6048.781924 TA = 323.08423 MA = 323.30677 Ha = 220.433 n.mi Hp = 201.327 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17813406.20 X = 5384414.96 Y = 13200031.85 feet Y = 4083833.78 meter Z = -190736.35 Z = -31870.29 XDOT = -9176.997860 XDOT = -2869.231236 YDOT = 12588.843522 feet/sec YDOT = 3805.397449 meter/sec ZDOT = 19845.085052 ZDOT = 6035.018351 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 5225139.35 X = 1592622.47 Y = 21547288.22 feet Y = 6567613.45 meter Z = -83369.90 Z = -25411.15 XDOT = -13632.654146 XDOT = -4155.232984 YDOT = 3332.049656 feet/sec YDOT = 1015.608735 meter/sec ZDOT = 19788.329066 ZDOT = 6031.482699 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 12042.50005166 .00016717 00000-0 10270-3 0 9087 2 25544 51.6395 37.5037 0020510 31.5497 328.6883 15.58874755 38265 Satellite: ISS Catalog Number: 25544 Epoch time: 12042.50005166 = yrday.fracday Element set: 908 Inclination: 51.6395 deg RA of node: 37.5037 deg Eccentricity: .0020510 Arg of perigee: 31.5497 deg Mean anomaly: 328.6883 deg Mean motion: 15.58874755 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3826 Checksum: 316 Coasting Arc #10 (Orbit 3841) --------------------------------------- Vector Time (GMT): 2012/043/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3424833.98 A = 6771549.30 meter Y = -4985810.32 meter E = .0022618 Z = -3077403.01 I = 51.83167 XDOT = 5789.768862 Wp = 45.47633 YDOT = -945.740271 meter/sec RA = 31.94211 deg ZDOT = -4918.003162 TA = 169.74697 MA = 169.70076 Ha = 220.603 n.mi Hp = 201.110 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -11236331.95 X = -3353877.95 Y = -16357645.41 feet Y = -5023712.36 meter Z = -10096466.56 Z = -3093867.88 XDOT = 18995.304665 XDOT = 5823.804288 YDOT = -3102.822412 feet/sec YDOT = -880.805478 meter/sec ZDOT = -16135.180977 ZDOT = -4889.794327 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 1556886.46 X = 474538.99 Y = -19749546.99 feet Y = -6019661.92 meter Z = -10163555.21 Z = -3097851.63 XDOT = 15376.819657 XDOT = 4686.854631 YDOT = 9444.711383 feet/sec YDOT = 2878.748029 meter/sec ZDOT = -16019.438162 ZDOT = -4882.724752 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 12043.52577132 .00016717 00000-0 10270-3 0 9098 2 25544 51.6391 32.3523 0020718 35.0986 325.1530 15.58852682 38420 Satellite: ISS Catalog Number: 25544 Epoch time: 12043.52577132 = yrday.fracday Element set: 909 Inclination: 51.6391 deg RA of node: 32.3523 deg Eccentricity: .0020718 Arg of perigee: 35.0986 deg Mean anomaly: 325.1530 deg Mean motion: 15.58852682 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3842 Checksum: 302 Coasting Arc #11 (Orbit 3857) --------------------------------------- Vector Time (GMT): 2012/044/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 182833.19 A = 6764759.23 meter Y = 4518953.07 meter E = .0021817 Z = 5011759.93 I = 51.78272 XDOT = -7185.675265 Wp = 53.00818 YDOT = -1899.339844 meter/sec RA = 26.92482 deg ZDOT = 1981.646021 TA = 17.88879 MA = 17.81212 Ha = 220.638 n.mi Hp = 200.947 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 599846.44 X = 107942.02 Y = 14825961.51 feet Y = 4520579.06 meter Z = 16442781.91 Z = 5012466.05 XDOT = -23575.050083 XDOT = -7173.528701 YDOT = -6231.429935 feet/sec YDOT = -1979.626510 meter/sec ZDOT = 6501.463322 ZDOT = 1946.768262 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8704989.08 X = -2653280.67 Y = 12012894.75 feet Y = 3661530.32 meter Z = 16445289.67 Z = 5012524.29 XDOT = -13943.359574 XDOT = -4249.935998 YDOT = -18777.522348 feet/sec YDOT = -5723.388812 meter/sec ZDOT = 6358.623188 ZDOT = 1938.108348 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 12044.55147375 .00016717 00000-0 10270-3 0 9106 2 25544 51.6391 27.2023 0020657 38.4048 321.8573 15.58882279 38588 Satellite: ISS Catalog Number: 25544 Epoch time: 12044.55147375 = yrday.fracday Element set: 910 Inclination: 51.6391 deg RA of node: 27.2023 deg Eccentricity: .0020657 Arg of perigee: 38.4048 deg Mean anomaly: 321.8573 deg Mean motion: 15.58882279 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3858 Checksum: 318 Coasting Arc #12 (Orbit 3872) --------------------------------------- Vector Time (GMT): 2012/045/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3268371.49 A = 6764547.95 meter Y = -3027747.60 meter E = .0029586 Z = -5110038.34 I = 51.75438 XDOT = 6317.531843 Wp = 64.88478 YDOT = 3982.466969 meter/sec RA = 21.88432 deg ZDOT = 1700.969135 TA = 221.42856 MA = 221.65327 Ha = 220.715 n.mi Hp = 200.837 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 10723003.59 X = 3326808.59 Y = -9933555.12 feet Y = -2990871.98 meter Z = -16765217.66 Z = -5094018.94 XDOT = 20726.810507 XDOT = 6264.266734 YDOT = 13065.836514 feet/sec YDOT = 4052.815705 meter/sec ZDOT = 5580.607398 ZDOT = 1731.529637 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14620454.44 X = 4456314.51 Y = -1451690.96 feet Y = -442475.41 meter Z = -16699273.98 Z = -5089938.71 XDOT = 8606.663786 XDOT = 2623.311122 YDOT = 21803.019077 feet/sec YDOT = 6645.560215 meter/sec ZDOT = 5705.561298 ZDOT = 1739.055084 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 12045.51305516 .00016717 00000-0 10270-3 0 9117 2 25544 51.6393 22.3742 0020708 42.0817 318.1924 15.58880110 38734 Satellite: ISS Catalog Number: 25544 Epoch time: 12045.51305516 = yrday.fracday Element set: 911 Inclination: 51.6393 deg RA of node: 22.3742 deg Eccentricity: .0020708 Arg of perigee: 42.0817 deg Mean anomaly: 318.1924 deg Mean motion: 15.58880110 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3873 Checksum: 285 Coasting Arc #13 (Orbit 3888) --------------------------------------- Vector Time (GMT): 2012/046/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5888745.64 A = 6771065.80 meter Y = 867580.96 meter E = .0030820 Z = 3219463.07 I = 51.74800 XDOT = -3374.399094 Wp = 63.22076 YDOT = -4964.813347 meter/sec RA = 16.85974 deg ZDOT = -4785.351025 TA = 79.49157 MA = 79.14447 Ha = 220.729 n.mi Hp = 200.581 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19320031.63 X = -5913648.63 Y = 2846394.23 feet Y = 801590.13 meter Z = 10562542.89 Z = 3190795.75 XDOT = -11070.863170 XDOT = -3295.384950 YDOT = -16288.757700 feet/sec YDOT = -5002.106157 meter/sec ZDOT = -15699.970555 ZDOT = -4801.551549 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17372821.86 X = -5295236.10 Y = -9056567.54 feet Y = -2760441.79 meter Z = 10444928.90 Z = 3183614.33 XDOT = -2.937906 XDOT = -.895474 YDOT = -18364.226430 feet/sec YDOT = -5597.416216 meter/sec ZDOT = -15765.957821 ZDOT = -4805.463944 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 12046.53872478 .00016717 00000-0 10270-3 0 9127 2 25544 51.6392 17.2231 0020720 45.5902 314.6945 15.58939476 38897 Satellite: ISS Catalog Number: 25544 Epoch time: 12046.53872478 = yrday.fracday Element set: 912 Inclination: 51.6392 deg RA of node: 17.2231 deg Eccentricity: .0020720 Arg of perigee: 45.5902 deg Mean anomaly: 314.6945 deg Mean motion: 15.58939476 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3889 Checksum: 328 Coasting Arc #14 (Orbit 3903) --------------------------------------- Vector Time (GMT): 2012/047/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6641971.55 A = 6775300.56 meter Y = 1249150.33 meter E = .0032526 Z = -181959.10 I = 51.73323 XDOT = -739.153778 Wp = 47.24701 YDOT = 4706.634740 meter/sec RA = 11.86806 deg ZDOT = 6031.909672 TA = 310.78857 MA = 311.07031 Ha = 220.695 n.mi Hp = 200.305 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21791245.24 X = 6628393.55 Y = 4098262.24 feet Y = 1323349.03 meter Z = -596978.67 Z = -149726.30 XDOT = -2425.045205 XDOT = -821.030465 YDOT = 15441.715027 feet/sec YDOT = 4697.911236 meter/sec ZDOT = 19789.729896 ZDOT = 6028.120120 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15529083.17 X = 4733264.55 Y = 15831674.60 feet Y = 4825494.42 meter Z = -464931.39 Z = -141711.09 XDOT = -9769.108347 XDOT = -2977.624224 YDOT = 10076.264569 feet/sec YDOT = 3071.245441 meter/sec ZDOT = 19773.776939 ZDOT = 6027.047211 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 12047.50027498 .00016717 00000-0 10270-3 0 9130 2 25544 51.6393 12.3952 0020688 49.6279 310.6678 15.58967174 39042 Satellite: ISS Catalog Number: 25544 Epoch time: 12047.50027498 = yrday.fracday Element set: 913 Inclination: 51.6393 deg RA of node: 12.3952 deg Eccentricity: .0020688 Arg of perigee: 49.6279 deg Mean anomaly: 310.6678 deg Mean motion: 15.58967174 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3904 Checksum: 336 Coasting Arc #15 (Orbit 3919) --------------------------------------- Vector Time (GMT): 2012/048/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 886586.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5267528.82 A = 6771276.02 meter Y = -3034183.04 meter E = .0023598 Z = -3014955.08 I = 51.69113 XDOT = 4766.095186 Wp = 61.49256 YDOT = -3368.547531 meter/sec RA = 6.87498 deg ZDOT = -4955.475633 TA = 152.99637 MA = 152.87339 Ha = 220.699 n.mi Hp = 200.087 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -17281918.69 X = -5218562.86 Y = -9954668.75 feet Y = -3092814.01 meter Z = -9891584.91 Z = -3040424.94 XDOT = 15636.795229 XDOT = 4827.480738 YDOT = -11051.665127 feet/sec YDOT = -3314.906902 meter/sec ZDOT = -16258.122155 ZDOT = -4932.173607 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8736118.03 X = -2662768.78 Y = -17870894.86 feet Y = -5447048.75 meter Z = -9995746.81 Z = -3046703.63 XDOT = 17921.880551 XDOT = 5462.589192 YDOT = 245.426637 feet/sec YDOT = 74.806039 meter/sec ZDOT = -16162.283633 ZDOT = -4926.264051 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 12048.52591123 .00016717 00000-0 10270-3 0 9145 2 25544 51.6402 7.2436 0020738 52.9742 307.3307 15.58991853 39202 Satellite: ISS Catalog Number: 25544 Epoch time: 12048.52591123 = yrday.fracday Element set: 914 Inclination: 51.6402 deg RA of node: 7.2436 deg Eccentricity: .0020738 Arg of perigee: 52.9742 deg Mean anomaly: 307.3307 deg Mean motion: 15.58991853 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3920 Checksum: 301