ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 9149.32 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 3028) --------------------------------------- Vector Time (GMT): 2010/211/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5886772.53 A = 6736192.33 meter Y = 1453024.09 meter E = .0017697 Z = 2909467.41 I = 51.70110 XDOT = -3624.406982 Wp = 121.91121 YDOT = -4560.767225 meter/sec RA = 8.40280 deg ZDOT = -5042.500272 TA = 24.63621 MA = 24.55178 Ha = 196.145 n.mi Hp = 186.771 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19313558.18 X = -5916716.47 Y = 4767139.42 feet Y = 1387027.14 meter Z = 9545496.75 Z = 2880797.19 XDOT = -11891.099021 XDOT = -3548.643054 YDOT = -14963.147063 feet/sec YDOT = -4600.873679 meter/sec ZDOT = -16543.636064 ZDOT = -5059.923567 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15517127.17 X = 4729620.36 Y = 12535298.83 feet Y = 3820759.08 meter Z = 9430837.90 Z = 2874519.39 XDOT = -3861.988708 XDOT = -1177.134158 YDOT = 17312.292654 feet/sec YDOT = 5276.786801 meter/sec ZDOT = -16613.263137 ZDOT = -5063.722604 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 10211.53766810 .00016717 00000-0 10270-3 0 9008 2 25544 51.6422 8.7446 0007649 167.4000 192.7355 15.71333273 30296 Satellite: ISS Catalog Number: 25544 Epoch time: 10211.53766810 = yrday.fracday Element set: 900 Inclination: 51.6422 deg RA of node: 8.7446 deg Eccentricity: .0007649 Arg of perigee: 167.4000 deg Mean anomaly: 192.7355 deg Mean motion: 15.71333273 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3029 Checksum: 288 Coasting Arc #2 (Orbit 3044) --------------------------------------- Vector Time (GMT): 2010/212/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4403939.30 A = 6733087.50 meter Y = 3316504.31 meter E = .0015483 Z = 3862163.07 I = 51.66218 XDOT = -5817.533868 Wp = 127.13796 YDOT = 2915.774610 meter/sec RA = 3.33999 deg ZDOT = 4109.325400 TA = 279.87419 MA = 280.04895 Ha = 195.851 n.mi Hp = 186.803 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14448619.76 X = 4347764.73 Y = 10880919.65 feet Y = 3365437.54 meter Z = 12671138.68 Z = 3883420.89 XDOT = -19086.397205 XDOT = -5869.668385 YDOT = 9566.189665 feet/sec YDOT = 2850.427797 meter/sec ZDOT = 13482.038713 ZDOT = 4080.937582 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -345548.62 X = -105323.22 Y = -18024347.84 feet Y = -5493821.22 meter Z = 12756106.85 Z = 3888061.37 XDOT = 18060.093134 XDOT = 5504.716387 YDOT = 9162.037204 feet/sec YDOT = 2792.588940 meter/sec ZDOT = 13368.499903 ZDOT = 4074.718770 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 10212.55521023 .00016717 00000-0 10270-3 0 9017 2 25544 51.6431 3.5398 0007677 171.3351 188.7945 15.71382511 30456 Satellite: ISS Catalog Number: 25544 Epoch time: 10212.55521023 = yrday.fracday Element set: 901 Inclination: 51.6431 deg RA of node: 3.5398 deg Eccentricity: .0007677 Arg of perigee: 171.3351 deg Mean anomaly: 188.7945 deg Mean motion: 15.71382511 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3045 Checksum: 287 Coasting Arc #3 (Orbit 3059) --------------------------------------- Vector Time (GMT): 2010/213/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4034796.50 A = 6732241.50 meter Y = -3431398.38 meter E = .0013066 Z = -4169465.53 I = 51.62973 XDOT = 6154.530716 Wp = 140.96198 YDOT = 2735.484062 meter/sec RA = 358.17491 deg ZDOT = 3700.820262 TA = 166.95153 MA = 166.91770 Ha = 195.823 n.mi Hp = 187.068 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13237521.32 X = 4093121.53 Y = -11257868.70 feet Y = -3385952.56 meter Z = -13679348.84 Z = -4149723.10 XDOT = 20192.029908 XDOT = 6105.506814 YDOT = 8974.685243 feet/sec YDOT = 2804.033420 meter/sec ZDOT = 12141.798759 ZDOT = 3730.599834 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17142740.47 X = -5225107.29 Y = -3201932.10 feet Y = -975948.90 meter Z = -13600376.58 Z = -4145394.78 XDOT = -5998.832653 XDOT = -1828.444193 YDOT = -20013.019266 feet/sec YDOT = -6099.968272 meter/sec ZDOT = 12260.841561 ZDOT = 3737.104508 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 10213.50914917 .00016717 00000-0 10270-3 0 9022 2 25544 51.6442 358.6609 0007609 174.0799 186.0454 15.71370390 30603 Satellite: ISS Catalog Number: 25544 Epoch time: 10213.50914917 = yrday.fracday Element set: 902 Inclination: 51.6442 deg RA of node: 358.6609 deg Eccentricity: .0007609 Arg of perigee: 174.0799 deg Mean anomaly: 186.0454 deg Mean motion: 15.71370390 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3060 Checksum: 309 Coasting Arc #4 (Orbit 3075) --------------------------------------- Vector Time (GMT): 2010/214/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6097573.56 A = 6736715.92 meter Y = -1291998.91 meter E = .0011505 Z = -2543244.12 I = 51.61493 XDOT = 3174.176473 Wp = 157.68464 YDOT = -4604.441598 meter/sec RA = 353.10498 deg ZDOT = -5289.396247 TA = 51.12935 MA = 51.02676 Ha = 195.573 n.mi Hp = 187.096 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20005162.59 X = -6070318.44 Y = -4238841.58 feet Y = -1360033.08 meter Z = -8343976.77 Z = -2572799.88 XDOT = 10413.964808 XDOT = 3251.123090 YDOT = -15106.435690 feet/sec YDOT = -4568.515509 meter/sec ZDOT = -17353.662229 ZDOT = -5273.789536 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9641619.94 X = 2938765.76 Y = 17978534.22 feet Y = 5479857.23 meter Z = -8462135.01 Z = -2579258.75 XDOT = -17015.707449 XDOT = -5186.387631 YDOT = 1014.413853 feet/sec YDOT = 309.193342 meter/sec ZDOT = -17291.214696 ZDOT = -5270.362239 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 10214.52667404 .00016717 00000-0 10270-3 0 9032 2 25544 51.6440 353.4557 0007532 178.1212 181.9980 15.71393501 30760 Satellite: ISS Catalog Number: 25544 Epoch time: 10214.52667404 = yrday.fracday Element set: 903 Inclination: 51.6440 deg RA of node: 353.4557 deg Eccentricity: .0007532 Arg of perigee: 178.1212 deg Mean anomaly: 181.9980 deg Mean motion: 15.71393501 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3076 Checksum: 296 Coasting Arc #5 (Orbit 3091) --------------------------------------- Vector Time (GMT): 2010/215/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1371872.07 A = 6729001.25 meter Y = 4322991.60 meter E = .0006436 Z = 4965333.78 I = 51.55905 XDOT = -7432.911066 Wp = 129.85057 YDOT = -47.895012 meter/sec RA = 347.94790 deg ZDOT = -2014.273460 TA = 339.64444 MA = 339.67008 Ha = 195.625 n.mi Hp = 187.310 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4500892.63 X = -1444231.20 Y = 14183043.29 feet Y = 4307245.54 meter Z = 16290465.16 Z = 4958493.82 XDOT = -24386.191162 XDOT = -7422.038122 YDOT = -157.135866 feet/sec YDOT = -130.953320 meter/sec ZDOT = -6608.508727 ZDOT = -2050.356009 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13701883.08 X = 4176333.96 Y = -5879363.79 feet Y = -1792030.08 meter Z = 16263071.30 Z = 4956984.13 XDOT = 15484.161929 XDOT = 4719.572556 YDOT = 17428.087009 feet/sec YDOT = 5312.080920 meter/sec ZDOT = -6752.773111 ZDOT = -2058.245244 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 10215.54419145 .00016717 00000-0 10270-3 0 9043 2 25544 51.6444 348.2512 0007526 181.0944 179.0203 15.71367854 30921 Satellite: ISS Catalog Number: 25544 Epoch time: 10215.54419145 = yrday.fracday Element set: 904 Inclination: 51.6444 deg RA of node: 348.2512 deg Eccentricity: .0007526 Arg of perigee: 181.0944 deg Mean anomaly: 179.0203 deg Mean motion: 15.71367854 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3092 Checksum: 298 Coasting Arc #6 (Orbit 3107) --------------------------------------- Vector Time (GMT): 2010/216/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6555126.59 A = 6739080.95 meter Y = -1237044.90 meter E = .0010593 Z = 945855.02 I = 51.56530 XDOT = 61.906571 Wp = 88.01616 YDOT = 4903.216536 meter/sec RA = 342.85250 deg ZDOT = 5926.981240 TA = 282.30813 MA = 282.42671 Ha = 195.373 n.mi Hp = 187.380 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21506320.83 X = 6563877.49 Y = -4058546.25 feet Y = -1163692.71 meter Z = 3103198.89 Z = 977720.82 XDOT = 203.105548 XDOT = -21.718756 YDOT = 16086.668426 feet/sec YDOT = 4903.440688 meter/sec ZDOT = 19445.476510 ZDOT = 5927.079311 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17432840.66 X = -5313529.83 Y = -13201615.44 feet Y = -4023852.39 meter Z = 3230618.03 Z = 984692.37 XDOT = 10901.806470 XDOT = 3322.870612 YDOT = -9593.538187 feet/sec YDOT = -2924.110439 meter/sec ZDOT = 19445.814717 ZDOT = 5927.084326 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 10216.56169618 .00016717 00000-0 10270-3 0 9054 2 25544 51.6454 343.0463 0007480 185.6533 174.4545 15.71429694 31080 Satellite: ISS Catalog Number: 25544 Epoch time: 10216.56169618 = yrday.fracday Element set: 905 Inclination: 51.6454 deg RA of node: 343.0463 deg Eccentricity: .0007480 Arg of perigee: 185.6533 deg Mean anomaly: 174.4545 deg Mean motion: 15.71429694 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3108 Checksum: 318 Coasting Arc #7 (Orbit 3122) --------------------------------------- Vector Time (GMT): 2010/217/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1430093.20 A = 6727390.25 meter Y = -3944958.80 meter E = .0015772 Z = -5270397.92 I = 51.49756 XDOT = 7155.643262 Wp = 118.52036 YDOT = -2803.326845 meter/sec RA = 337.71910 deg ZDOT = 149.623062 TA = 152.94608 MA = 152.86379 Ha = 195.163 n.mi Hp = 187.519 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4691906.82 X = -1360271.22 Y = -12942778.21 feet Y = -3960560.00 meter Z = -17291331.76 Z = -5277176.08 XDOT = 23476.519890 XDOT = 7185.731915 YDOT = -9197.266551 feet/sec YDOT = -2723.139946 meter/sec ZDOT = 490.889312 ZDOT = 184.457695 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6303435.90 X = -1921287.26 Y = 12200808.82 feet Y = 3718806.53 meter Z = -17318389.39 Z = -5278645.09 XDOT = -21874.601567 XDOT = -6667.378558 YDOT = -10373.961954 feet/sec YDOT = -3161.983604 meter/sec ZDOT = 630.198039 ZDOT = 192.084362 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 10217.51560057 .00016717 00000-0 10270-3 0 9063 2 25544 51.6455 338.1675 0007331 189.5309 170.5715 15.71451001 31230 Satellite: ISS Catalog Number: 25544 Epoch time: 10217.51560057 = yrday.fracday Element set: 906 Inclination: 51.6455 deg RA of node: 338.1675 deg Eccentricity: .0007331 Arg of perigee: 189.5309 deg Mean anomaly: 170.5715 deg Mean motion: 15.71451001 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3123 Checksum: 287 Coasting Arc #8 (Orbit 3138) --------------------------------------- Vector Time (GMT): 2010/218/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5668315.21 A = 6739293.94 meter Y = 3558442.54 meter E = .0017708 Z = 690817.10 I = 51.51017 XDOT = -3089.554469 Wp = 149.97622 YDOT = -3751.257183 meter/sec RA = 332.58813 deg ZDOT = -5976.821625 TA = 22.48622 MA = 22.40871 Ha = 195.060 n.mi Hp = 187.805 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18596834.68 X = -5711040.91 Y = 11674680.26 feet Y = 3494817.08 meter Z = 2266460.30 Z = 663177.38 XDOT = -10136.333561 XDOT = -3018.343645 YDOT = -12307.274222 feet/sec YDOT = -3785.407593 meter/sec ZDOT = -19608.994833 ZDOT = -5991.657951 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21338438.78 X = 6503956.14 Y = 5224973.79 feet Y = 1592572.01 meter Z = 2155908.42 Z = 657120.89 XDOT = -1473.701921 XDOT = -449.184346 YDOT = 14206.142288 feet/sec YDOT = 4330.032169 meter/sec ZDOT = -19668.276580 ZDOT = -5994.890702 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 10218.53308976 .00016717 00000-0 10270-3 0 9077 2 25544 51.6457 332.9620 0007380 193.6676 166.4287 15.71439190 31391 Satellite: ISS Catalog Number: 25544 Epoch time: 10218.53308976 = yrday.fracday Element set: 907 Inclination: 51.6457 deg RA of node: 332.9620 deg Eccentricity: .0007380 Arg of perigee: 193.6676 deg Mean anomaly: 166.4287 deg Mean motion: 15.71439190 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3139 Checksum: 332 Coasting Arc #9 (Orbit 3154) --------------------------------------- Vector Time (GMT): 2010/219/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3785930.69 A = 6728196.49 meter Y = 2351004.55 meter E = .0010105 Z = 5041444.49 I = 51.44802 XDOT = -5482.734137 Wp = 168.43646 YDOT = 5120.218712 meter/sec RA = 327.48149 deg ZDOT = 1719.241985 TA = 264.90851 MA = 265.02386 Ha = 194.735 n.mi Hp = 187.911 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12421032.46 X = 3734869.96 Y = 7713269.53 feet Y = 2393055.06 meter Z = 16540172.23 Z = 5059712.45 XDOT = -17987.972890 XDOT = -5547.933489 YDOT = 16798.617821 feet/sec YDOT = 5058.542769 meter/sec ZDOT = 5640.557693 ZDOT = 1692.449509 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -3290009.02 X = -1002794.75 Y = -14160913.50 feet Y = -4316246.43 meter Z = 16613194.79 Z = 5063701.77 XDOT = 23590.558399 XDOT = 7190.402200 YDOT = 1050.430793 feet/sec YDOT = 320.171306 meter/sec ZDOT = 5533.377431 ZDOT = 1686.573441 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 10219.55056819 .00016717 00000-0 10270-3 0 9087 2 25544 51.6466 327.7571 0007280 198.1513 161.9390 15.71494074 31552 Satellite: ISS Catalog Number: 25544 Epoch time: 10219.55056819 = yrday.fracday Element set: 908 Inclination: 51.6466 deg RA of node: 327.7571 deg Eccentricity: .0007280 Arg of perigee: 198.1513 deg Mean anomaly: 161.9390 deg Mean motion: 15.71494074 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3155 Checksum: 323 Coasting Arc #10 (Orbit 3169) --------------------------------------- Vector Time (GMT): 2010/220/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3711722.68 A = 6737266.64 meter Y = -5148078.37 meter E = .0002595 Z = -2265936.53 I = 51.45323 XDOT = 5260.943075 Wp = 146.10152 YDOT = 1403.406083 meter/sec RA = 322.31852 deg ZDOT = 5430.112501 TA = 188.43582 MA = 188.44018 Ha = 194.686 n.mi Hp = 188.243 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12177567.86 X = 3780020.84 Y = -16890020.90 feet Y = -5106189.59 meter Z = -7434174.98 Z = -2247739.94 XDOT = 17260.311926 XDOT = 5218.481016 YDOT = 4604.350667 feet/sec YDOT = 1461.999206 meter/sec ZDOT = 17815.329729 ZDOT = 5455.566575 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -20517180.26 X = -6253636.54 Y = 3699792.73 feet Y = 1127696.83 meter Z = -7361370.16 Z = -2243745.62 XDOT = -8900.665088 XDOT = -2712.922719 YDOT = -13715.194095 feet/sec YDOT = -4180.391160 meter/sec ZDOT = 17917.100945 ZDOT = 5461.132368 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 10220.50444842 .00016717 00000-0 10270-3 0 9092 2 25544 51.6467 322.8780 0007067 202.3646 157.7209 15.71446669 31705 Satellite: ISS Catalog Number: 25544 Epoch time: 10220.50444842 = yrday.fracday Element set: 909 Inclination: 51.6467 deg RA of node: 322.8780 deg Eccentricity: .0007067 Arg of perigee: 202.3646 deg Mean anomaly: 157.7209 deg Mean motion: 15.71446669 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3170 Checksum: 311 Coasting Arc #11 (Orbit 3185) --------------------------------------- Vector Time (GMT): 2010/221/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5136470.09 A = 6731045.96 meter Y = 19200.35 meter E = .0006339 Z = -4352924.83 I = 51.40944 XDOT = 2836.922562 Wp = 120.34210 YDOT = -6300.690623 meter/sec RA = 317.23213 deg ZDOT = -3382.184244 TA = 115.46472 MA = 115.39913 Ha = 194.460 n.mi Hp = 188.229 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -16851935.99 X = -5115157.85 Y = 62993.27 feet Y = -38119.32 meter Z = -14281249.43 Z = -4377825.41 XDOT = 9307.488719 XDOT = 2923.596817 YDOT = -20671.557161 feet/sec YDOT = -6268.481645 meter/sec ZDOT = -11096.405000 ZDOT = -3368.192649 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12324415.10 X = 3756481.72 Y = 11368666.12 feet Y = 3465169.43 meter Z = -14380821.37 Z = -4383274.35 XDOT = -20109.514053 XDOT = -6129.379883 YDOT = 7862.568548 feet/sec YDOT = 2396.510893 meter/sec ZDOT = -11040.415039 ZDOT = -3365.118504 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 10221.52191099 .00016717 00000-0 10270-3 0 9100 2 25544 51.6466 317.6735 0007190 205.8403 154.2401 15.71473815 31868 Satellite: ISS Catalog Number: 25544 Epoch time: 10221.52191099 = yrday.fracday Element set: 910 Inclination: 51.6466 deg RA of node: 317.6735 deg Eccentricity: .0007190 Arg of perigee: 205.8403 deg Mean anomaly: 154.2401 deg Mean motion: 15.71473815 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3186 Checksum: 292 Coasting Arc #12 (Orbit 3201) --------------------------------------- Vector Time (GMT): 2010/222/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1164305.44 A = 6733743.18 meter Y = 5569201.58 meter E = .0010216 Z = 3589218.91 I = 51.39680 XDOT = -6129.108029 Wp = 121.32462 YDOT = 1554.579537 meter/sec RA = 312.04998 deg ZDOT = -4396.411965 TA = 15.61791 MA = 15.58642 Ha = 194.351 n.mi Hp = 188.451 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3819899.73 X = -1243930.08 Y = 18271658.73 feet Y = 5555736.33 meter Z = 11775652.59 Z = 3583369.59 XDOT = -20108.622144 XDOT = -6124.679645 YDOT = 5100.326564 feet/sec YDOT = 1486.065050 meter/sec ZDOT = -14423.923771 ZDOT = -4426.175647 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15101194.47 X = 4602844.08 Y = -10997726.66 feet Y = -3352107.09 meter Z = 11752237.00 Z = 3582081.84 XDOT = 17504.086811 XDOT = 5335.245660 YDOT = 8480.588989 feet/sec YDOT = 2584.883524 meter/sec ZDOT = -14542.949406 ZDOT = -4432.690979 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 10222.53936499 .00016717 00000-0 10270-3 0 9114 2 25544 51.6463 312.4690 0006979 208.8906 151.1870 15.71495421 32025 Satellite: ISS Catalog Number: 25544 Epoch time: 10222.53936499 = yrday.fracday Element set: 911 Inclination: 51.6463 deg RA of node: 312.4690 deg Eccentricity: .0006979 Arg of perigee: 208.8906 deg Mean anomaly: 151.1870 deg Mean motion: 15.71495421 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3202 Checksum: 313 Coasting Arc #13 (Orbit 3217) --------------------------------------- Vector Time (GMT): 2010/223/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5258542.94 A = 6734559.54 meter Y = -2674023.07 meter E = .0010418 Z = 3246535.46 I = 51.38045 XDOT = 157.914461 Wp = 121.09529 YDOT = 6069.261879 meter/sec RA = 306.96651 deg ZDOT = 4726.693877 TA = 277.00825 MA = 277.12673 Ha = 194.122 n.mi Hp = 188.556 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17252437.46 X = 5272282.77 Y = -8773041.57 feet Y = -2615142.07 meter Z = 10651363.05 Z = 3272114.30 XDOT = 518.092064 XDOT = 67.074181 YDOT = 19912.276505 feet/sec YDOT = 6070.519859 meter/sec ZDOT = 15507.525842 ZDOT = 4727.240360 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -18733617.04 X = -5710006.47 Y = -4634104.42 feet Y = -1412475.03 meter Z = 10753653.35 Z = 3277713.54 XDOT = 12386.302565 XDOT = 3775.345022 YDOT = -13956.911682 feet/sec YDOT = -4254.066681 meter/sec ZDOT = 15509.693915 ZDOT = 4727.354705 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 10223.55680824 .00016717 00000-0 10270-3 0 9126 2 25544 51.6461 307.2636 0007007 213.6571 146.4147 15.71531311 32180 Satellite: ISS Catalog Number: 25544 Epoch time: 10223.55680824 = yrday.fracday Element set: 912 Inclination: 51.6461 deg RA of node: 307.2636 deg Eccentricity: .0007007 Arg of perigee: 213.6571 deg Mean anomaly: 146.4147 deg Mean motion: 15.71531311 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3218 Checksum: 280 Coasting Arc #14 (Orbit 3232) --------------------------------------- Vector Time (GMT): 2010/224/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1361085.73 A = 6730051.23 meter Y = -4752248.11 meter E = .0010606 Z = -4576215.72 I = 51.34718 XDOT = 5535.616561 Wp = 147.89623 YDOT = -4440.417348 meter/sec RA = 301.78372 deg ZDOT = 2959.085518 TA = 151.65831 MA = 151.60058 Ha = 193.927 n.mi Hp = 188.677 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4465504.37 X = -1285613.98 Y = -15591365.17 feet Y = -4767046.65 meter Z = -15013831.09 Z = -4582644.40 XDOT = 18161.471658 XDOT = 5570.484220 YDOT = -14568.298385 feet/sec YDOT = -4378.319781 meter/sec ZDOT = 9708.285819 ZDOT = 2986.061870 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6655967.34 X = -2028738.84 Y = 14763372.02 feet Y = 4499875.79 meter Z = -15039530.14 Z = -4584048.79 XDOT = -22156.188064 XDOT = -6753.206122 YDOT = 29.840209 feet/sec YDOT = 9.095296 meter/sec ZDOT = 9816.160431 ZDOT = 2991.965699 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 10224.51065509 .00016717 00000-0 10270-3 0 9131 2 25544 51.6452 302.3844 0006843 217.1411 142.9279 15.71554390 32332 Satellite: ISS Catalog Number: 25544 Epoch time: 10224.51065509 = yrday.fracday Element set: 913 Inclination: 51.6452 deg RA of node: 302.3844 deg Eccentricity: .0006843 Arg of perigee: 217.1411 deg Mean anomaly: 142.9279 deg Mean motion: 15.71554390 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3233 Checksum: 287 Coasting Arc #15 (Orbit 3248) --------------------------------------- Vector Time (GMT): 2010/225/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 828730.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4165371.74 A = 6737637.36 meter Y = 4942250.42 meter E = .0010604 Z = -1878727.23 I = 51.35679 XDOT = -2778.228543 Wp = 180.16326 YDOT = -4472.865737 meter/sec RA = 296.68621 deg ZDOT = -5617.175003 TA = 20.77501 MA = 20.73194 Ha = 193.709 n.mi Hp = 188.952 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -13665917.80 X = -4211200.89 Y = 16214732.35 feet Y = 4895414.48 meter Z = -6163803.25 Z = -1899073.76 XDOT = -9114.923042 XDOT = -2700.718710 YDOT = -14674.756356 feet/sec YDOT = -4503.500214 meter/sec ZDOT = -18429.051846 ZDOT = -5630.483197 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 20793261.04 X = 6337785.97 Y = -4038016.06 feet Y = -1230787.30 meter Z = -6245161.86 Z = -1903525.33 XDOT = -2519.739768 XDOT = -768.016681 YDOT = 15557.522047 feet/sec YDOT = 4741.932720 meter/sec ZDOT = -18482.262817 ZDOT = -5633.393706 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 10225.52808320 .00016717 00000-0 10270-3 0 9140 2 25544 51.6443 297.1789 0006813 221.4446 138.6200 15.71532026 32499 Satellite: ISS Catalog Number: 25544 Epoch time: 10225.52808320 = yrday.fracday Element set: 914 Inclination: 51.6443 deg RA of node: 297.1789 deg Eccentricity: .0006813 Arg of perigee: 221.4446 deg Mean anomaly: 138.6200 deg Mean motion: 15.71532026 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3249 Checksum: 293