ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 10763.91 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74 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 3578) --------------------------------------- Vector Time (GMT): 2010/246/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2412178.69 A = 6728243.65 meter Y = 3703164.02 meter E = .0009910 Z = -5079835.80 I = 51.57106 XDOT = -7118.735458 Wp = 64.42788 YDOT = -2415.220978 meter/sec RA = 188.85700 deg ZDOT = 1626.337450 TA = 221.19453 MA = 221.26936 Ha = 194.687 n.mi Hp = 188.591 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -7913972.07 X = -2428732.12 Y = 12149488.26 feet Y = 3676097.10 meter Z = -16666127.96 Z = -5091594.24 XDOT = -23355.431294 XDOT = -7099.099329 YDOT = -7923.953339 feet/sec YDOT = -2494.717173 meter/sec ZDOT = 5335.752789 ZDOT = 1591.802544 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 11228658.28 X = 3422495.04 Y = -9087850.28 feet Y = -2769976.77 meter Z = -16713140.06 Z = -5094165.09 XDOT = 19062.676079 XDOT = 5810.303669 YDOT = 14034.871434 feet/sec YDOT = 4277.828813 meter/sec ZDOT = 5197.440502 ZDOT = 1584.179865 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 10246.51321039 .00016717 00000-0 10270-3 0 9004 2 25544 51.6434 189.8456 0008498 327.8779 32.1864 15.71435228 35794 Satellite: ISS Catalog Number: 25544 Epoch time: 10246.51321039 = yrday.fracday Element set: 900 Inclination: 51.6434 deg RA of node: 189.8456 deg Eccentricity: .0008498 Arg of perigee: 327.8779 deg Mean anomaly: 32.1864 deg Mean motion: 15.71435228 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3579 Checksum: 332 Coasting Arc #2 (Orbit 3594) --------------------------------------- Vector Time (GMT): 2010/247/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6644970.72 A = 6739270.33 meter Y = 931698.27 meter E = .0003196 Z = -624373.43 I = 51.63922 XDOT = -1215.059472 Wp = 105.13680 YDOT = 4670.266058 meter/sec RA = 183.75792 deg ZDOT = -5988.631873 TA = 81.64911 MA = 81.61288 Ha = 194.839 n.mi Hp = 188.433 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21801085.03 X = 6637091.49 Y = 3056752.86 feet Y = 1005962.26 meter Z = -2048469.25 Z = -592111.66 XDOT = -3986.415591 XDOT = -1238.101574 YDOT = 15322.395205 feet/sec YDOT = 4656.549704 meter/sec ZDOT = -19647.742367 ZDOT = -5994.590531 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -19920715.22 X = -6071834.00 Y = -9397275.85 feet Y = -2864289.68 meter Z = -1919266.66 Z = -584992.48 XDOT = 7560.602875 XDOT = 2304.471756 YDOT = -12028.391921 feet/sec YDOT = -3666.253857 meter/sec ZDOT = -19671.516588 ZDOT = -5995.878256 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 10247.53069351 .00016717 00000-0 10270-3 0 9014 2 25544 51.6442 184.6406 0008500 331.7975 28.2726 15.71456516 35951 Satellite: ISS Catalog Number: 25544 Epoch time: 10247.53069351 = yrday.fracday Element set: 901 Inclination: 51.6442 deg RA of node: 184.6406 deg Eccentricity: .0008500 Arg of perigee: 331.7975 deg Mean anomaly: 28.2726 deg Mean motion: 15.71456516 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3595 Checksum: 309 Coasting Arc #3 (Orbit 3610) --------------------------------------- Vector Time (GMT): 2010/248/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -341744.14 A = 6727225.23 meter Y = -4166575.94 meter E = .0007320 Z = 5271308.84 I = 51.62983 XDOT = 7685.259167 Wp = 350.71117 YDOT = -358.511398 meter/sec RA = 178.63822 deg ZDOT = 222.000812 TA = 97.22211 MA = 97.13889 Ha = 194.880 n.mi Hp = 188.176 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -1121207.80 X = -320734.02 Y = -13669868.56 feet Y = -4170279.93 meter Z = 17294320.35 Z = 5269699.80 XDOT = 25214.104878 XDOT = 7687.618497 YDOT = -1176.218496 feet/sec YDOT = -272.557025 meter/sec ZDOT = 728.349121 ZDOT = 259.341009 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -2660135.07 X = -810809.17 Y = 13463718.15 feet Y = 4103741.29 meter Z = 17287796.42 Z = 5269320.35 XDOT = -23545.201780 XDOT = -7176.577503 YDOT = -5749.173405 feet/sec YDOT = -1752.348054 meter/sec ZDOT = 877.881552 ZDOT = 267.578297 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 10248.54816256 .00016717 00000-0 10270-3 0 9021 2 25544 51.6446 179.4358 0008573 334.9290 25.1455 15.71509450 36118 Satellite: ISS Catalog Number: 25544 Epoch time: 10248.54816256 = yrday.fracday Element set: 902 Inclination: 51.6446 deg RA of node: 179.4358 deg Eccentricity: .0008573 Arg of perigee: 334.9290 deg Mean anomaly: 25.1455 deg Mean motion: 15.71509450 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3611 Checksum: 313 Coasting Arc #4 (Orbit 3625) --------------------------------------- Vector Time (GMT): 2010/249/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6471227.90 A = 6738868.87 meter Y = 1541161.83 meter E = .0015950 Z = -1012982.24 I = 51.69928 XDOT = -1993.068550 Wp = 10.93744 YDOT = -4489.193334 meter/sec RA = 173.51158 deg ZDOT = 5932.921539 TA = 338.00297 MA = 338.07135 Ha = 195.064 n.mi Hp = 187.954 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -21231062.65 X = -6483059.68 Y = 5056305.20 feet Y = 1468730.47 meter Z = -3323432.53 Z = -1044447.81 XDOT = -6538.938813 XDOT = -1971.542072 YDOT = -14728.324586 feet/sec YDOT = -4511.360348 meter/sec ZDOT = 19464.965680 ZDOT = 5923.291880 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21793322.03 X = 6642604.56 Y = 722504.36 feet Y = 220219.33 meter Z = -3449427.40 Z = -1051385.47 XDOT = 2583.016419 XDOT = 787.303404 YDOT = 14372.703922 feet/sec YDOT = 4380.800155 meter/sec ZDOT = 19426.306711 ZDOT = 5921.138285 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 10249.50203035 .00016717 00000-0 10270-3 0 9034 2 25544 51.6447 174.5557 0008626 339.1935 20.8874 15.71483811 36263 Satellite: ISS Catalog Number: 25544 Epoch time: 10249.50203035 = yrday.fracday Element set: 903 Inclination: 51.6447 deg RA of node: 174.5557 deg Eccentricity: .0008626 Arg of perigee: 339.1935 deg Mean anomaly: 20.8874 deg Mean motion: 15.71483811 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3626 Checksum: 311 Coasting Arc #5 (Orbit 3641) --------------------------------------- Vector Time (GMT): 2010/250/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3025918.33 A = 6728580.63 meter Y = 3390660.81 meter E = .0015234 Z = -4974051.97 I = 51.69610 XDOT = -6762.843939 Wp = 40.74406 YDOT = 3030.304647 meter/sec RA = 168.42593 deg ZDOT = -2040.640185 TA = 209.43915 MA = 209.52503 Ha = 195.196 n.mi Hp = 187.724 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 9927553.58 X = 3011941.19 Y = 11124215.24 feet Y = 3424419.89 meter Z = -16319068.13 Z = -4959386.46 XDOT = -22187.808199 XDOT = -6786.313793 YDOT = 9941.944380 feet/sec YDOT = 2954.547077 meter/sec ZDOT = -6695.013731 ZDOT = -2073.550925 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6961169.00 X = -2121764.31 Y = -13257552.99 feet Y = -4040902.15 meter Z = -16260254.75 Z = -4956125.65 XDOT = 22951.848283 XDOT = 6995.723357 YDOT = -3646.875589 feet/sec YDOT = -1111.567679 meter/sec ZDOT = -6826.775460 ZDOT = -2080.801160 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 10250.51947577 .00016717 00000-0 10270-3 0 9044 2 25544 51.6459 169.3504 0008580 343.5311 16.5571 15.71534605 36428 Satellite: ISS Catalog Number: 25544 Epoch time: 10250.51947577 = yrday.fracday Element set: 904 Inclination: 51.6459 deg RA of node: 169.3504 deg Eccentricity: .0008580 Arg of perigee: 343.5311 deg Mean anomaly: 16.5571 deg Mean motion: 15.71534605 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3642 Checksum: 306 Coasting Arc #6 (Orbit 3657) --------------------------------------- Vector Time (GMT): 2010/251/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5109752.63 A = 6736414.76 meter Y = -3600494.76 meter E = .0012499 Z = 2509224.36 I = 51.75210 XDOT = 4708.553402 Wp = 66.63976 YDOT = 2960.178167 meter/sec RA = 163.27749 deg ZDOT = -5315.154969 TA = 85.04307 MA = 84.90038 Ha = 195.276 n.mi Hp = 187.447 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 16764280.28 X = 5137444.98 Y = -11812646.86 feet Y = -3543199.36 meter Z = 8232363.39 Z = 2534114.97 XDOT = 15448.009849 XDOT = 4700.922076 YDOT = 9711.870627 feet/sec YDOT = 3012.788850 meter/sec ZDOT = -17438.172471 ZDOT = -5292.299807 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -18988998.40 X = -5787846.71 Y = 7638543.30 feet Y = 2328228.00 meter Z = 8331993.89 Z = 2539591.74 XDOT = -12334.910380 XDOT = -3759.680684 YDOT = -11651.656600 feet/sec YDOT = -3551.424932 meter/sec ZDOT = -17346.557822 ZDOT = -5287.230824 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 10251.53690841 .00016717 00000-0 10270-3 0 9057 2 25544 51.6458 164.1453 0008570 346.9373 13.1565 15.71532889 36582 Satellite: ISS Catalog Number: 25544 Epoch time: 10251.53690841 = yrday.fracday Element set: 905 Inclination: 51.6458 deg RA of node: 164.1453 deg Eccentricity: .0008570 Arg of perigee: 346.9373 deg Mean anomaly: 13.1565 deg Mean motion: 15.71532889 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3658 Checksum: 323 Coasting Arc #7 (Orbit 3673) --------------------------------------- Vector Time (GMT): 2010/252/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4995197.48 A = 6731532.79 meter Y = -1580648.63 meter E = .0010182 Z = 4215567.43 I = 51.76445 XDOT = 4642.903746 Wp = 56.22065 YDOT = -4948.695891 meter/sec RA = 158.21560 deg ZDOT = 3645.313324 TA = 356.72756 MA = 356.73421 Ha = 195.515 n.mi Hp = 187.249 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16388443.17 X = -4997629.57 Y = -5185855.07 feet Y = -1636521.11 meter Z = 13830601.81 Z = 4191295.03 XDOT = 15232.623840 XDOT = 4680.187642 YDOT = -16235.878908 feet/sec YDOT = -4896.567332 meter/sec ZDOT = 11959.689382 ZDOT = 3667.959576 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14980006.70 X = 4565906.04 Y = 8588051.51 feet Y = 2617638.10 meter Z = 13733334.60 Z = 4185920.39 XDOT = -17656.773088 XDOT = -5381.784437 YDOT = 11524.767536 feet/sec YDOT = 3512.749145 meter/sec ZDOT = 12050.307764 ZDOT = 3672.933806 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 10252.55432765 .00016717 00000-0 10270-3 0 9060 2 25544 51.6460 158.9398 0008617 350.9089 9.1916 15.71554027 36746 Satellite: ISS Catalog Number: 25544 Epoch time: 10252.55432765 = yrday.fracday Element set: 906 Inclination: 51.6460 deg RA of node: 158.9398 deg Eccentricity: .0008617 Arg of perigee: 350.9089 deg Mean anomaly: 9.1916 deg Mean motion: 15.71554027 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3674 Checksum: 330 Coasting Arc #8 (Orbit 3688) --------------------------------------- Vector Time (GMT): 2010/253/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2836936.95 A = 6732770.61 meter Y = 4786884.75 meter E = .0008732 Z = -3789047.72 I = 51.79718 XDOT = -6415.453952 Wp = 36.43293 YDOT = -468.173026 meter/sec RA = 153.05835 deg ZDOT = 4223.740992 TA = 277.82175 MA = 277.92087 Ha = 195.450 n.mi Hp = 186.978 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -9307535.94 X = -2871847.34 Y = 15705002.45 feet Y = 4754964.90 meter Z = -12431258.93 Z = -3802914.82 XDOT = -21048.077271 XDOT = -6430.260204 YDOT = -1536.000740 feet/sec YDOT = -539.996910 meter/sec ZDOT = 13857.417954 ZDOT = 4192.538659 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12147113.43 X = 3702440.17 Y = -13577297.35 feet Y = -4138360.23 meter Z = -12486719.25 Z = -3805952.03 XDOT = 19422.980185 XDOT = 5920.124360 YDOT = 4783.187228 feet/sec YDOT = 1457.915467 meter/sec ZDOT = 13732.406020 ZDOT = 4185.637355 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 10253.50814568 .00016717 00000-0 10270-3 0 9072 2 25544 51.6462 154.0598 0008680 354.0627 6.0431 15.71585218 36890 Satellite: ISS Catalog Number: 25544 Epoch time: 10253.50814568 = yrday.fracday Element set: 907 Inclination: 51.6462 deg RA of node: 154.0598 deg Eccentricity: .0008680 Arg of perigee: 354.0627 deg Mean anomaly: 6.0431 deg Mean motion: 15.71585218 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3689 Checksum: 316 Coasting Arc #9 (Orbit 3704) --------------------------------------- Vector Time (GMT): 2010/254/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5924899.51 A = 6734956.54 meter Y = -821755.49 meter E = .0008358 Z = -3107258.12 I = 51.83077 XDOT = -1784.259139 Wp = 27.97906 YDOT = 5651.701999 meter/sec RA = 148.00377 deg ZDOT = -4894.959236 TA = 187.91930 MA = 187.93250 Ha = 195.558 n.mi Hp = 186.977 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 19438646.68 X = 5948742.78 Y = -2696048.21 feet Y = -755366.59 meter Z = -10194416.41 Z = -3078416.79 XDOT = -5853.868566 XDOT = -1823.545899 YDOT = 18542.329394 feet/sec YDOT = 5631.529370 meter/sec ZDOT = -16059.577545 ZDOT = -4903.723014 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -19665492.51 X = -5994042.12 Y = -860451.39 feet Y = -262265.58 meter Z = -10078879.61 Z = -3072042.50 XDOT = 8941.878392 XDOT = 2725.484534 YDOT = -15767.040662 feet/sec YDOT = -4805.793994 meter/sec ZDOT = -16094.586012 ZDOT = -4905.629816 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 10254.52553890 .00016717 00000-0 10270-3 0 9084 2 25544 51.6462 148.8542 0008668 357.0094 3.1015 15.71590288 37055 Satellite: ISS Catalog Number: 25544 Epoch time: 10254.52553890 = yrday.fracday Element set: 908 Inclination: 51.6462 deg RA of node: 148.8542 deg Eccentricity: .0008668 Arg of perigee: 357.0094 deg Mean anomaly: 3.1015 deg Mean motion: 15.71590288 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3705 Checksum: 313 Coasting Arc #10 (Orbit 3720) --------------------------------------- Vector Time (GMT): 2010/255/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 261959.44 A = 6729310.87 meter Y = -4820174.04 meter E = .0014307 Z = 4687802.36 I = 51.83722 XDOT = 6767.797613 Wp = 29.94008 YDOT = -2368.515349 meter/sec RA = 142.85462 deg ZDOT = -2797.795368 TA = 87.67861 MA = 87.51480 Ha = 195.601 n.mi Hp = 186.566 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 859446.97 X = 293067.37 Y = -15814219.28 feet Y = -4817070.52 meter Z = 15379929.02 Z = 4689150.73 XDOT = 22204.060409 XDOT = 6807.371073 YDOT = -7770.719649 feet/sec YDOT = -2292.612626 meter/sec ZDOT = -9179.118663 ZDOT = -2764.820941 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -3338777.68 X = -1017659.44 Y = 15476337.07 feet Y = 4717187.54 meter Z = 15385251.10 Z = 4689424.54 XDOT = -22099.379697 XDOT = -6735.890932 YDOT = 4277.684900 feet/sec YDOT = 1303.838358 meter/sec ZDOT = -9047.036322 ZDOT = -2757.536671 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 10255.54291781 .00016717 00000-0 10270-3 0 9096 2 25544 51.6458 143.6481 0008818 .7257 359.3917 15.71658650 37218 Satellite: ISS Catalog Number: 25544 Epoch time: 10255.54291781 = yrday.fracday Element set: 909 Inclination: 51.6458 deg RA of node: 143.6481 deg Eccentricity: .0008818 Arg of perigee: .7257 deg Mean anomaly: 359.3917 deg Mean motion: 15.71658650 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3721 Checksum: 328 Coasting Arc #11 (Orbit 3736) --------------------------------------- Vector Time (GMT): 2010/256/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5618744.69 A = 6737690.36 meter Y = 3267260.24 meter E = .0020055 Z = 1727385.71 I = 51.88845 XDOT = -1152.020585 Wp = 42.19852 YDOT = -5022.652023 meter/sec RA = 137.78936 deg ZDOT = 5729.250648 TA = 336.85462 MA = 336.94482 Ha = 195.834 n.mi Hp = 186.420 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18434201.74 X = -5663253.57 Y = 10719357.74 feet Y = 3204179.25 meter Z = 5667275.95 Z = 1699981.50 XDOT = -3779.595096 XDOT = -1123.602568 YDOT = -16478.517135 feet/sec YDOT = -5035.375570 meter/sec ZDOT = 18796.754096 ZDOT = 5723.723255 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 19836318.91 X = 6046110.01 Y = -7904236.50 feet Y = -2409211.29 meter Z = 5557511.85 Z = 1693929.61 XDOT = 863.593801 XDOT = 263.223390 YDOT = 15423.260079 feet/sec YDOT = 4701.009672 meter/sec ZDOT = 18774.528354 ZDOT = 5722.476242 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 10256.56028550 .00016717 00000-0 10270-3 0 9103 2 25544 51.6458 138.4418 0008853 4.6678 355.4565 15.71631193 37375 Satellite: ISS Catalog Number: 25544 Epoch time: 10256.56028550 = yrday.fracday Element set: 910 Inclination: 51.6458 deg RA of node: 138.4418 deg Eccentricity: .0008853 Arg of perigee: 4.6678 deg Mean anomaly: 355.4565 deg Mean motion: 15.71631193 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3737 Checksum: 322 Coasting Arc #12 (Orbit 3751) --------------------------------------- Vector Time (GMT): 2010/257/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2153804.44 A = 6727124.12 meter Y = 3692389.17 meter E = .0016775 Z = -5206521.52 I = 51.87506 XDOT = -5770.758476 Wp = 67.01305 YDOT = 4950.085406 meter/sec RA = 132.66362 deg ZDOT = 1132.590320 TA = 213.72866 MA = 213.83551 Ha = 195.806 n.mi Hp = 186.246 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 7066287.54 X = 2137647.80 Y = 12114137.70 feet Y = 3716383.88 meter Z = -17081763.52 Z = -5196097.62 XDOT = -18932.934634 XDOT = -5831.184279 YDOT = 16240.437683 feet/sec YDOT = 4885.215483 meter/sec ZDOT = 3715.847507 ZDOT = 1104.409047 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -5542711.07 X = -1689418.33 Y = -12937939.73 feet Y = -3943484.03 meter Z = -17039937.39 Z = -5193772.92 XDOT = 19950.194002 XDOT = 6080.819132 YDOT = -13251.937659 feet/sec YDOT = -4039.190598 meter/sec ZDOT = 3602.976838 ZDOT = 1098.187340 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 10257.51405340 .00016717 00000-0 10270-3 0 9116 2 25544 51.6458 133.5611 0008815 7.5497 352.5797 15.71677439 37520 Satellite: ISS Catalog Number: 25544 Epoch time: 10257.51405340 = yrday.fracday Element set: 911 Inclination: 51.6458 deg RA of node: 133.5611 deg Eccentricity: .0008815 Arg of perigee: 7.5497 deg Mean anomaly: 352.5797 deg Mean motion: 15.71677439 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3752 Checksum: 320 Coasting Arc #13 (Orbit 3767) --------------------------------------- Vector Time (GMT): 2010/258/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4263806.64 A = 6738856.89 meter Y = -5212452.84 meter E = .0009781 Z = -256117.41 I = 51.93403 XDOT = 3532.037955 Wp = 90.70106 YDOT = 3176.676584 meter/sec RA = 127.57651 deg ZDOT = -6048.054943 TA = 92.06581 MA = 91.95379 Ha = 195.879 n.mi Hp = 186.132 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13988866.91 X = 4323020.52 Y = -17101223.22 feet Y = -5164441.31 meter Z = -840280.22 Z = -235259.95 XDOT = 11588.051032 XDOT = 3525.633594 YDOT = 10422.167271 feet/sec YDOT = 3216.138048 meter/sec ZDOT = -19842.699945 ZDOT = -6030.911925 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -15822358.56 X = -4822654.89 Y = 15424869.63 feet Y = 4701500.26 meter Z = -756749.84 Z = -230657.35 XDOT = -9338.776532 XDOT = -2846.459087 YDOT = -10514.194588 feet/sec YDOT = -3204.726510 meter/sec ZDOT = -19773.949574 ZDOT = -6027.099830 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 10258.53139485 .00016717 00000-0 10270-3 0 9124 2 25544 51.6459 128.3554 0008650 11.4718 348.6642 15.71644975 37687 Satellite: ISS Catalog Number: 25544 Epoch time: 10258.53139485 = yrday.fracday Element set: 912 Inclination: 51.6459 deg RA of node: 128.3554 deg Eccentricity: .0008650 Arg of perigee: 11.4718 deg Mean anomaly: 348.6642 deg Mean motion: 15.71644975 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3768 Checksum: 335 Coasting Arc #14 (Orbit 3783) --------------------------------------- Vector Time (GMT): 2010/259/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3822440.54 A = 6726766.33 meter Y = -1684175.67 meter E = .0008815 Z = 5267972.31 I = 51.91134 XDOT = 3738.053904 Wp = 33.71769 YDOT = -6709.650822 meter/sec RA = 122.48069 deg ZDOT = 573.969600 TA = 50.88837 MA = 50.81002 Ha = 196.050 n.mi Hp = 185.839 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12540815.43 X = -3828914.44 Y = -5525510.72 feet Y = -1726956.57 meter Z = 17283373.71 Z = 5249387.29 XDOT = 12263.956377 XDOT = 3810.016405 YDOT = -22013.290097 feet/sec YDOT = -6667.447284 meter/sec ZDOT = 1883.102361 ZDOT = 592.303932 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12061165.47 X = 3676243.24 Y = 6700884.41 feet Y = 2042429.57 meter Z = 17208857.11 Z = 5245259.65 XDOT = -13799.452528 XDOT = -4206.073130 YDOT = 19870.382710 feet/sec YDOT = 6056.492650 meter/sec ZDOT = 1956.513515 ZDOT = 596.345319 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 10259.54872080 .00016717 00000-0 10270-3 0 9132 2 25544 51.6458 123.1488 0008837 15.0041 345.1381 15.71700532 37843 Satellite: ISS Catalog Number: 25544 Epoch time: 10259.54872080 = yrday.fracday Element set: 913 Inclination: 51.6458 deg RA of node: 123.1488 deg Eccentricity: .0008837 Arg of perigee: 15.0041 deg Mean anomaly: 345.1381 deg Mean motion: 15.71700532 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3784 Checksum: 299 Coasting Arc #15 (Orbit 3798) --------------------------------------- Vector Time (GMT): 2010/260/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 826788.6 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2134642.04 A = 6737994.49 meter Y = 6257180.48 meter E = .0017694 Z = -1253409.05 I = 51.96387 XDOT = -4929.165015 Wp = 27.73611 YDOT = -510.302259 meter/sec RA = 117.36634 deg ZDOT = 5895.545223 TA = 318.58414 MA = 318.71814 Ha = 196.008 n.mi Hp = 185.678 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -7003418.78 X = -2198363.54 Y = 20528807.34 feet Y = 6232953.30 meter Z = -4112234.41 Z = -1263934.07 XDOT = -16171.801229 XDOT = -4951.731675 YDOT = -1674.220009 feet/sec YDOT = -565.549107 meter/sec ZDOT = 19342.339970 ZDOT = 5871.544706 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 8555816.25 X = 2607812.79 Y = -19923092.50 feet Y = -6072558.59 meter Z = -4154355.64 Z = -1266247.60 XDOT = 14653.731237 XDOT = 4466.457281 YDOT = 2312.466105 feet/sec YDOT = 704.839669 meter/sec ZDOT = 19246.121965 ZDOT = 5866.217975 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 10260.50245200 .00016717 00000-0 10270-3 0 9149 2 25544 51.6451 118.2675 0008915 17.4602 342.6865 15.71713637 37990 Satellite: ISS Catalog Number: 25544 Epoch time: 10260.50245200 = yrday.fracday Element set: 914 Inclination: 51.6451 deg RA of node: 118.2675 deg Eccentricity: .0008915 Arg of perigee: 17.4602 deg Mean anomaly: 342.6865 deg Mean motion: 15.71713637 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3799 Checksum: 303