ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 9687.52 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 72.1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2.19 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 ------------------------------------------------------------------------ 014/18:07:09.671 6.8 9.8 9.8 N/A 5.3 0.0 193.6 000/00:02:19.341 4.8 -0.1 192.9 Coasting Arc #1 (Orbit 2036) --------------------------------------- Vector Time (GMT): 2009/005/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 640263.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3780238.25 A = 6725736.74 meter Y = 1742971.67 meter E = .0007039 Z = 5278836.74 I = 51.90428 XDOT = -3676.405083 Wp = 143.45136 YDOT = -6755.525633 meter/sec RA = 59.06444 deg ZDOT = -407.428840 TA = 310.37219 MA = 310.43362 Ha = 194.826 n.mi Hp = 185.801 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12402356.46 X = -3825091.20 Y = 5718411.01 feet Y = 1700447.62 meter Z = 17319018.18 Z = 5260363.49 XDOT = -12061.696467 XDOT = -3598.611224 YDOT = -22163.798007 feet/sec YDOT = -6796.202321 meter/sec ZDOT = -1336.708793 ZDOT = -425.100496 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8658397.52 X = -2639079.56 Y = -10678575.95 feet Y = -3254829.95 meter Z = 17247238.30 Z = 5256958.23 XDOT = 17674.467477 XDOT = 5387.177687 YDOT = -16573.546440 feet/sec YDOT = -5051.616955 meter/sec ZDOT = -1405.908579 ZDOT = -428.520935 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 09005.54697578 .00010596 00000-0 82463-4 0 9005 2 25544 51.6411 59.4499 0006743 165.7805 194.3548 15.72041805 20371 Satellite: ISS Catalog Number: 25544 Epoch time: 09005.54697578 = yrday.fracday Element set: 900 Inclination: 51.6411 deg RA of node: 59.4499 deg Eccentricity: .0006743 Arg of perigee: 165.7805 deg Mean anomaly: 194.3548 deg Mean motion: 15.72041805 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2037 Checksum: 326 Coasting Arc #2 (Orbit 2051) --------------------------------------- Vector Time (GMT): 2009/006/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 640263.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4140150.03 A = 6737818.46 meter Y = 5306447.35 meter E = .0009657 Z = -288736.19 I = 51.92843 XDOT = -3588.406476 Wp = 76.68168 YDOT = 3119.488623 meter/sec RA = 53.96394 deg ZDOT = 6047.410719 TA = 280.19737 MA = 280.30626 Ha = 194.662 n.mi Hp = 185.977 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13583169.40 X = 4081907.39 Y = 17409604.17 feet Y = 5352419.29 meter Z = -947297.21 Z = -268764.14 XDOT = -11772.987126 XDOT = -3652.399751 YDOT = 10234.542727 feet/sec YDOT = 3079.002508 meter/sec ZDOT = 19840.586350 ZDOT = 6029.823077 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13163285.06 X = -4012169.29 Y = 17733203.94 feet Y = 5405080.56 meter Z = -869243.80 Z = -264945.51 XDOT = -11737.128828 XDOT = -3577.476867 YDOT = -7773.116898 feet/sec YDOT = -2369.246031 meter/sec ZDOT = 19772.333134 ZDOT = 6026.607139 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 09006.50051127 .00010596 00000-0 82463-4 0 9017 2 25544 51.6411 54.5672 0006516 167.4178 192.7148 15.72006144 20522 Satellite: ISS Catalog Number: 25544 Epoch time: 09006.50051127 = yrday.fracday Element set: 901 Inclination: 51.6411 deg RA of node: 54.5672 deg Eccentricity: .0006516 Arg of perigee: 167.4178 deg Mean anomaly: 192.7148 deg Mean motion: 15.72006144 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2052 Checksum: 279 Coasting Arc #3 (Orbit 2067) --------------------------------------- Vector Time (GMT): 2009/007/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 640263.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2338146.48 A = 6725991.25 meter Y = -3554100.54 meter E = .0016074 Z = -5222149.11 I = 51.87161 XDOT = 5589.852268 Wp = 106.54740 YDOT = 5176.009699 meter/sec RA = 48.87243 deg ZDOT = -1026.986047 TA = 153.71517 MA = 153.63352 Ha = 194.563 n.mi Hp = 186.074 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 7671084.26 X = 2403083.55 Y = -11660434.83 feet Y = -3527590.22 meter Z = -17133035.13 Z = -5210633.13 XDOT = 18339.410327 XDOT = 5536.546747 YDOT = 16981.659116 feet/sec YDOT = 5238.220761 meter/sec ZDOT = -3369.376794 ZDOT = -999.959246 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13381844.60 X = 4078786.23 Y = 4154992.18 feet Y = 1266441.62 meter Z = -17088430.07 Z = -5208553.48 XDOT = -10793.871547 XDOT = -3289.972047 YDOT = 21435.566884 feet/sec YDOT = 6533.560786 meter/sec ZDOT = -3263.879832 ZDOT = -994.830573 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 09007.51760095 .00010596 00000-0 82463-4 0 9021 2 25544 51.6420 49.3588 0006660 171.5255 188.6021 15.72049935 20688 Satellite: ISS Catalog Number: 25544 Epoch time: 09007.51760095 = yrday.fracday Element set: 902 Inclination: 51.6420 deg RA of node: 49.3588 deg Eccentricity: .0006660 Arg of perigee: 171.5255 deg Mean anomaly: 188.6021 deg Mean motion: 15.72049935 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2068 Checksum: 309 Coasting Arc #4 (Orbit 2083) --------------------------------------- Vector Time (GMT): 2009/008/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 640263.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5473118.95 A = 6736656.07 meter Y = -3609494.84 meter E = .0018548 Z = 1500312.96 I = 51.88706 XDOT = 1569.723267 Wp = 135.17940 YDOT = -4808.517146 meter/sec RA = 43.74626 deg ZDOT = -5811.766332 TA = 28.35014 MA = 28.24933 Ha = 194.410 n.mi Hp = 186.073 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -17956427.00 X = -5439638.44 Y = -11842174.66 feet Y = -3670511.47 meter Z = 4922286.61 Z = 1473805.35 XDOT = 5150.010718 XDOT = 1651.608657 YDOT = -15775.974889 feet/sec YDOT = -4790.504800 meter/sec ZDOT = -19067.474841 ZDOT = -5803.942520 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 5917649.76 X = 1803699.65 Y = -20704078.73 feet Y = -6310603.20 meter Z = 4818902.56 Z = 1468801.50 XDOT = 15117.468661 XDOT = 4607.804448 YDOT = -133.766921 feet/sec YDOT = -40.772157 meter/sec ZDOT = -19037.306139 ZDOT = -5802.570911 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 09008.53467539 .00010596 00000-0 82463-4 0 9032 2 25544 51.6415 44.1507 0006550 174.1537 185.9703 15.72100997 20847 Satellite: ISS Catalog Number: 25544 Epoch time: 09008.53467539 = yrday.fracday Element set: 903 Inclination: 51.6415 deg RA of node: 44.1507 deg Eccentricity: .0006550 Arg of perigee: 174.1537 deg Mean anomaly: 185.9703 deg Mean motion: 15.72100997 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2084 Checksum: 309 Coasting Arc #5 (Orbit 2099) --------------------------------------- Vector Time (GMT): 2009/009/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 640263.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -305426.32 A = 6727324.48 meter Y = 4644158.64 meter E = .0011831 Z = 4855866.04 I = 51.83308 XDOT = -6696.122498 Wp = 148.16408 YDOT = -2952.871306 meter/sec RA = 38.67324 deg ZDOT = 2390.479518 TA = 278.50729 MA = 278.64135 Ha = 194.277 n.mi Hp = 186.155 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -1002054.87 X = -380924.05 Y = 15236740.94 feet Y = 4640320.21 meter Z = 15931319.03 Z = 4854199.72 XDOT = -21968.905834 XDOT = -6674.217734 YDOT = -9687.897985 feet/sec YDOT = -3027.629164 meter/sec ZDOT = 7842.780571 ZDOT = 2358.002772 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14803350.68 X = -4512061.29 Y = 3771106.59 feet Y = 1149433.29 meter Z = 15925102.14 Z = 4853971.13 XDOT = 2519.738550 XDOT = 768.016310 YDOT = -22866.688415 feet/sec YDOT = -6969.766629 meter/sec ZDOT = 7716.194739 ZDOT = 2351.896156 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 09009.55173605 .00010596 00000-0 82463-4 0 9044 2 25544 51.6408 38.9423 0006538 176.9908 183.1294 15.72111907 21002 Satellite: ISS Catalog Number: 25544 Epoch time: 09009.55173605 = yrday.fracday Element set: 904 Inclination: 51.6408 deg RA of node: 38.9423 deg Eccentricity: .0006538 Arg of perigee: 176.9908 deg Mean anomaly: 183.1294 deg Mean motion: 15.72111907 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2100 Checksum: 306 Coasting Arc #6 (Orbit 2114) --------------------------------------- Vector Time (GMT): 2009/010/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 640263.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6016704.60 A = 6734460.48 meter Y = 1502578.44 meter E = .0005285 Z = -2634322.74 I = 51.83471 XDOT = 909.664467 Wp = 130.58980 YDOT = 5548.287042 meter/sec RA = 33.52510 deg ZDOT = 5245.790396 TA = 199.59010 MA = 199.61042 Ha = 194.097 n.mi Hp = 186.279 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 19739844.49 X = 6012252.18 Y = 4929719.30 feet Y = 1569836.26 meter Z = -8642791.16 Z = -2605104.68 XDOT = 2984.463476 XDOT = 822.072361 YDOT = 18203.041478 feet/sec YDOT = 5557.968817 meter/sec ZDOT = 17210.598411 ZDOT = 5249.997627 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 1917711.64 X = 584518.51 Y = 20303708.24 feet Y = 6188570.27 meter Z = -8528965.09 Z = -2599628.56 XDOT = -14733.278697 XDOT = -4490.703347 YDOT = 8623.366227 feet/sec YDOT = 2628.402026 meter/sec ZDOT = 17227.296436 ZDOT = 5250.879954 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 09010.50521679 .00010596 00000-0 82463-4 0 9050 2 25544 51.6419 34.0596 0006546 180.3274 179.7885 15.72168112 21159 Satellite: ISS Catalog Number: 25544 Epoch time: 09010.50521679 = yrday.fracday Element set: 905 Inclination: 51.6419 deg RA of node: 34.0596 deg Eccentricity: .0006546 Arg of perigee: 180.3274 deg Mean anomaly: 179.7885 deg Mean motion: 15.72168112 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2115 Checksum: 309 Coasting Arc #7 (Orbit 2130) --------------------------------------- Vector Time (GMT): 2009/011/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 640263.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1890376.19 A = 6729474.40 meter Y = -4848693.54 meter E = .0008223 Z = -4270777.75 I = 51.79198 XDOT = 6796.811383 Wp = 113.95515 YDOT = 487.518319 meter/sec RA = 28.46203 deg ZDOT = -3570.614565 TA = 119.88099 MA = 119.79926 Ha = 193.941 n.mi Hp = 186.379 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6202021.64 X = -1815270.64 Y = -15907787.20 feet Y = -4869412.28 meter Z = -14011738.01 Z = -4279779.23 XDOT = 22299.249945 XDOT = 6808.199703 YDOT = 1599.469551 feet/sec YDOT = 563.588379 meter/sec ZDOT = -11714.614716 ZDOT = -3537.568714 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12782617.62 X = 3896141.85 Y = -11275473.06 feet Y = -3436764.19 meter Z = -14047062.40 Z = -4281544.62 XDOT = 5463.492759 XDOT = 1665.272593 YDOT = 20592.348820 feet/sec YDOT = 6276.547920 meter/sec ZDOT = -11585.938135 ZDOT = -3531.393943 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 09011.52224865 .00010596 00000-0 82463-4 0 9061 2 25544 51.6411 28.8504 0006430 185.0211 175.0888 15.72157029 21311 Satellite: ISS Catalog Number: 25544 Epoch time: 09011.52224865 = yrday.fracday Element set: 906 Inclination: 51.6411 deg RA of node: 28.8504 deg Eccentricity: .0006430 Arg of perigee: 185.0211 deg Mean anomaly: 175.0888 deg Mean motion: 15.72157029 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2131 Checksum: 282 Coasting Arc #8 (Orbit 2146) --------------------------------------- Vector Time (GMT): 2009/012/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 640263.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5657657.29 A = 6731833.64 meter Y = 632199.41 meter E = .0012507 Z = 3578155.72 I = 51.77266 XDOT = -3408.981389 Wp = 116.12859 YDOT = -5284.560255 meter/sec RA = 23.29993 deg ZDOT = -4449.923553 TA = 21.22975 MA = 21.17790 Ha = 193.847 n.mi Hp = 186.524 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18561867.75 X = -5681687.73 Y = 2074145.04 feet Y = 568797.46 meter Z = 11739356.05 Z = 3550613.25 XDOT = -11184.322142 XDOT = -3328.018859 YDOT = -17337.796111 feet/sec YDOT = -5322.228303 meter/sec ZDOT = -14599.486723 ZDOT = -4466.287854 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8715560.28 X = -2656502.77 Y = -16594855.36 feet Y = -5058111.91 meter Z = 11632165.63 Z = 3545484.08 XDOT = 10895.484613 XDOT = 3320.943710 YDOT = -16015.856014 feet/sec YDOT = -4881.632913 meter/sec ZDOT = -14663.505871 ZDOT = -4469.436589 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 09012.53926556 .00010596 00000-0 82463-4 0 9070 2 25544 51.6402 23.6412 0006288 188.9483 171.1568 15.72202349 21471 Satellite: ISS Catalog Number: 25544 Epoch time: 09012.53926556 = yrday.fracday Element set: 907 Inclination: 51.6402 deg RA of node: 23.6412 deg Eccentricity: .0006288 Arg of perigee: 188.9483 deg Mean anomaly: 171.1568 deg Mean motion: 15.72202349 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2147 Checksum: 311 Coasting Arc #9 (Orbit 2162) --------------------------------------- Vector Time (GMT): 2009/013/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 640263.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3978854.00 A = 6732029.56 meter Y = 4183173.85 meter E = .0012699 Z = 3459662.37 I = 51.74576 XDOT = -5918.106514 Wp = 120.58079 YDOT = 1838.842461 meter/sec RA = 18.23796 deg ZDOT = 4564.137724 TA = 280.30756 MA = 280.45071 Ha = 193.584 n.mi Hp = 186.659 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13053982.93 X = 3914975.36 Y = 13724323.65 feet Y = 4227310.28 meter Z = 11350598.32 Z = 3478836.30 XDOT = -19416.359954 XDOT = -5960.400096 YDOT = 6032.947706 feet/sec YDOT = 1772.425950 meter/sec ZDOT = 14974.205132 ZDOT = 4535.285704 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7757316.57 X = -2364430.09 Y = 17230255.86 feet Y = 5251781.99 meter Z = 11425494.95 Z = 3482490.86 XDOT = -11736.847915 XDOT = -3577.391245 YDOT = -15179.607687 feet/sec YDOT = -4626.744423 meter/sec ZDOT = 14861.987457 ZDOT = 4529.933777 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 09013.55626847 .00010596 00000-0 82463-4 0 9084 2 25544 51.6399 18.4323 0006325 193.3536 166.7459 15.72205919 21633 Satellite: ISS Catalog Number: 25544 Epoch time: 09013.55626847 = yrday.fracday Element set: 908 Inclination: 51.6399 deg RA of node: 18.4323 deg Eccentricity: .0006325 Arg of perigee: 193.3536 deg Mean anomaly: 166.7459 deg Mean motion: 15.72205919 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2163 Checksum: 327 Coasting Arc #10 (Orbit 2177) --------------------------------------- Vector Time (GMT): 2009/014/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 640263.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4519819.13 A = 6729243.45 meter Y = -2469549.55 meter E = .0011073 Z = -4341639.37 I = 51.70790 XDOT = 5536.920297 Wp = 144.32173 YDOT = 4075.271544 meter/sec RA = 13.07232 deg ZDOT = 3441.696681 TA = 160.47461 MA = 160.43217 Ha = 193.485 n.mi Hp = 186.956 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14828802.93 X = 4568188.55 Y = -8102196.68 feet Y = -2418735.64 meter Z = -14244223.66 Z = -4319565.21 XDOT = 18165.749007 XDOT = 5474.219655 YDOT = 13370.313465 feet/sec YDOT = 4136.837847 meter/sec ZDOT = 11291.655778 ZDOT = 3468.442355 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13344187.46 X = 4067308.34 Y = 10483716.53 feet Y = 3195436.80 meter Z = -14158433.66 Z = -4315490.58 XDOT = -4346.050000 XDOT = -1324.676040 YDOT = 20942.086932 feet/sec YDOT = 6383.148097 meter/sec ZDOT = 11396.025061 ZDOT = 3473.508439 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 09014.50969510 .00010596 00000-0 82463-4 0 9098 2 25544 51.6401 13.5488 0006222 196.9691 163.1264 15.72198796 21787 Satellite: ISS Catalog Number: 25544 Epoch time: 09014.50969510 = yrday.fracday Element set: 909 Inclination: 51.6401 deg RA of node: 13.5488 deg Eccentricity: .0006222 Arg of perigee: 196.9691 deg Mean anomaly: 163.1264 deg Mean motion: 15.72198796 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2178 Checksum: 325 Coasting Arc #11 (Orbit 2181) --------------------------------------- Vector Time (GMT): 2009/014/18:08:19.341 Vector Time (MET): N/A Weight (LBS) : 639553.5 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5154193.65 A = 6736175.94 meter Y = -2021418.96 meter E = .0003158 Z = -3837494.83 I = 51.70926 XDOT = 4799.309335 Wp = 219.14886 YDOT = 4347.402374 meter/sec RA = 11.76228 deg ZDOT = 4151.753425 TA = 94.31490 MA = 94.27882 Ha = 193.591 n.mi Hp = 192.896 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 16910084.15 X = 5195055.88 Y = -6631951.98 feet Y = -1963553.13 meter Z = -12590206.12 Z = -3812357.12 XDOT = 15745.765536 XDOT = 4730.171228 YDOT = 14263.131147 feet/sec YDOT = 4400.684270 meter/sec ZDOT = 13621.238272 ZDOT = 4174.900251 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12435955.77 X = 3790479.32 Y = -13331631.22 feet Y = -4063481.20 meter Z = -12492463.19 Z = -3807702.78 XDOT = 19326.047025 XDOT = 5890.579133 YDOT = 5165.941388 feet/sec YDOT = 1574.578935 meter/sec ZDOT = 13711.612829 ZDOT = 4179.299590 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 09014.76393920 .00010596 00000-0 82463-4 0 9104 2 25544 51.6428 12.2470 0008092 263.8810 96.1430 15.70395973 21826 Satellite: ISS Catalog Number: 25544 Epoch time: 09014.76393920 = yrday.fracday Element set: 910 Inclination: 51.6428 deg RA of node: 12.2470 deg Eccentricity: .0008092 Arg of perigee: 263.8810 deg Mean anomaly: 96.1430 deg Mean motion: 15.70395973 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2182 Checksum: 300 Coasting Arc #12 (Orbit 2197) --------------------------------------- Vector Time (GMT): 2009/015/18:08:19.341 Vector Time (MET): N/A Weight (LBS) : 639553.5 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5504685.60 A = 6739234.76 meter Y = -2792694.73 meter E = .0005092 Z = -2697059.60 I = 51.69130 XDOT = 4379.537220 Wp = 234.06958 YDOT = -3614.755932 meter/sec RA = 6.70705 deg ZDOT = -5191.799936 TA = 336.61139 MA = 336.63454 Ha = 192.923 n.mi Hp = 192.486 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18059992.14 X = -5459946.50 Y = -9162384.27 feet Y = -2854001.06 meter Z = -8848620.74 Z = -2723692.36 XDOT = 14368.560432 XDOT = 4444.852929 YDOT = -11859.435473 feet/sec YDOT = -3565.416004 meter/sec ZDOT = -17033.464357 ZDOT = -5170.365987 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -20205224.25 X = -6158552.35 Y = -113464.59 feet Y = -34584.01 meter Z = -8952470.59 Z = -2728713.04 XDOT = 7603.524133 XDOT = 2317.554156 YDOT = -15614.343297 feet/sec YDOT = -4759.251837 meter/sec ZDOT = -16950.239172 ZDOT = -5166.432900 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 09015.78210326 .00010596 00000-0 82463-4 0 9116 2 25544 51.6434 7.0465 0008214 267.4945 92.5276 15.70393589 21980 Satellite: ISS Catalog Number: 25544 Epoch time: 09015.78210326 = yrday.fracday Element set: 911 Inclination: 51.6434 deg RA of node: 7.0465 deg Eccentricity: .0008214 Arg of perigee: 267.4945 deg Mean anomaly: 92.5276 deg Mean motion: 15.70393589 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2198 Checksum: 316 Coasting Arc #13 (Orbit 2213) --------------------------------------- Vector Time (GMT): 2009/016/18:08:19.341 Vector Time (MET): N/A Weight (LBS) : 639553.5 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2189632.56 A = 6731378.18 meter Y = 3916718.03 meter E = .0004999 Z = 5021638.11 I = 51.63598 XDOT = -7272.475747 Wp = 314.45425 YDOT = -1673.827963 meter/sec RA = 1.56257 deg ZDOT = -1863.256531 TA = 153.55446 MA = 153.52894 Ha = 192.906 n.mi Hp = 192.445 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -7183833.87 X = -2257661.11 Y = 12850124.76 feet Y = 3891851.70 meter Z = 16475190.64 Z = 5010835.93 XDOT = -23859.828566 XDOT = -7244.166972 YDOT = -5491.561559 feet/sec YDOT = -1754.994644 meter/sec ZDOT = -6113.046361 ZDOT = -1898.517085 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -489170.47 X = -149099.16 Y = 14760420.53 feet Y = 4498976.18 meter Z = 16433373.97 Z = 5008892.39 XDOT = -22577.757987 XDOT = -6881.700635 YDOT = 6219.008841 feet/sec YDOT = 1895.553895 meter/sec ZDOT = -6250.412687 ZDOT = -1905.125787 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 09016.80025213 .00010596 00000-0 82463-4 0 9120 2 25544 51.6433 1.8456 0008231 272.2756 87.7463 15.70471274 22145 Satellite: ISS Catalog Number: 25544 Epoch time: 09016.80025213 = yrday.fracday Element set: 912 Inclination: 51.6433 deg RA of node: 1.8456 deg Eccentricity: .0008231 Arg of perigee: 272.2756 deg Mean anomaly: 87.7463 deg Mean motion: 15.70471274 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 2214 Checksum: 285