ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 21814.1409 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 70.5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2.049 ET - UTC (sec) : 68.18 UT1 - UTC (sec) : 0.00 Maneuvers contained within the current ephemeris are as follows: IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP ------------------------------------------------------------------------ 320/18:14:08.000 0.0 0.0 0.0 N/A 0.0 0.0 222.7 000/00:00:00.000 0.0 0.0 213.3 321/09:01:23.000 0.0 0.0 0.0 N/A 0.0 0.0 222.9 000/00:00:00.000 0.0 0.0 213.4 322/19:30:01.000 0.0 0.0 0.0 N/A 0.0 0.0 222.9 000/00:00:00.000 0.0 0.0 213.2 323/10:20:00.000 0.0 0.0 0.0 N/A 0.0 0.0 223.0 000/00:00:00.000 0.0 0.0 213.0 325/21:45:00.000 0.0 0.0 0.0 N/A 0.0 0.0 222.9 000/00:00:00.000 0.0 0.0 213.1 331/13:15:00.000 0.0 0.0 0.0 N/A 0.0 0.0 223.0 000/00:00:00.000 0.0 0.0 212.9 Coasting Arc #1 (Orbit 2219) --------------------------------------- Vector Time (GMT): 2018/320/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 902349.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5220617.29 A = 6782696.72 meter Y = 1466331.39 meter E = .0014568 Z = 4061078.25 I = 51.50341 XDOT = -4403.639115 Wp = 86.56746 YDOT = 4962.754681 meter/sec RA = 339.13043 deg ZDOT = 3857.986311 TA = 323.42134 MA = 323.52074 Ha = 222.910 n.mi Hp = 213.274 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17128009.50 X = 5184105.53 Y = 4810798.53 feet Y = 1524507.76 meter Z = 13323747.54 Z = 4086349.87 XDOT = -14447.634893 XDOT = -4477.547043 YDOT = 16282.003546 feet/sec YDOT = 4913.096829 meter/sec ZDOT = 12657.435405 ZDOT = 3836.415238 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13786524.65 X = -4202132.71 Y = 11108967.60 feet Y = 3386013.32 meter Z = 13437161.81 Z = 4095646.92 XDOT = -4056.225372 XDOT = -1236.337493 YDOT = -20269.551380 feet/sec YDOT = -6178.159261 meter/sec ZDOT = 12559.737385 ZDOT = 3828.207955 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 18320.55531318 .00016717 00000-0 10270-3 0 9002 2 25544 51.6400 339.4281 0005316 53.7842 306.3801 15.53958858 22206 Satellite: ISS Catalog Number: 25544 Epoch time: 18320.55531318 = yrday.fracday Element set: 900 Inclination: 51.6400 deg RA of node: 339.4281 deg Eccentricity: .0005316 Arg of perigee: 53.7842 deg Mean anomaly: 306.3801 deg Mean motion: 15.53958858 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2220 Checksum: 292 Coasting Arc #2 (Orbit 2223) --------------------------------------- Vector Time (GMT): 2018/320/18:14:08.000 Vector Time (MET): N/A Weight (LBS) : 902349.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4139764.85 A = 6779871.33 meter Y = 2423058.29 meter E = .0010290 Z = 4782653.39 I = 51.48654 XDOT = -5638.209489 Wp = 91.80997 YDOT = 4519.429364 meter/sec RA = 337.82909 deg ZDOT = 2585.484296 TA = 332.66053 MA = 332.71464 Ha = 222.736 n.mi Hp = 213.344 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13581905.69 X = 4089129.94 Y = 7949666.30 feet Y = 2469068.85 meter Z = 15691120.05 Z = 4802640.24 XDOT = -18498.062627 XDOT = -5700.887053 YDOT = 14827.524159 feet/sec YDOT = 4456.028508 meter/sec ZDOT = 8482.560027 ZDOT = 2557.943275 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 7317625.64 X = 2230412.30 Y = 13831142.71 feet Y = 4215732.30 meter Z = 15780635.32 Z = 4809937.64 XDOT = -22563.179008 XDOT = -6877.256962 YDOT = 2382.215588 feet/sec YDOT = 726.099311 meter/sec ZDOT = 8358.087339 ZDOT = 2547.545021 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 18320.81254693 .00016717 00000-0 10270-3 0 9010 2 25544 51.6403 338.1474 0005053 51.4587 308.7017 15.53998777 22241 Satellite: ISS Catalog Number: 25544 Epoch time: 18320.81254693 = yrday.fracday Element set: 901 Inclination: 51.6403 deg RA of node: 338.1474 deg Eccentricity: .0005053 Arg of perigee: 51.4587 deg Mean anomaly: 308.7017 deg Mean motion: 15.53998777 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2224 Checksum: 315 Coasting Arc #3 (Orbit 2232) --------------------------------------- Vector Time (GMT): 2018/321/09:01:23.000 Vector Time (MET): N/A Weight (LBS) : 902349.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1408804.65 A = 6777934.02 meter Y = -4003915.03 meter E = .0018841 Z = -5300469.24 I = 51.46057 XDOT = 7038.653260 Wp = 83.70600 YDOT = -2983.154240 meter/sec RA = 334.72739 deg ZDOT = 385.851926 TA = 189.97035 MA = 190.00779 Ha = 222.891 n.mi Hp = 213.352 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4622062.48 X = -1338179.78 Y = -13136204.15 feet Y = -4019274.35 meter Z = -17389990.95 Z = -5307141.30 XDOT = 23092.694421 XDOT = 7069.614302 YDOT = -9787.251442 feet/sec YDOT = -2904.270015 meter/sec ZDOT = 1265.918392 ZDOT = 420.118952 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 6896515.08 X = 2102057.80 Y = 12055582.91 feet Y = 3674541.67 meter Z = -17419417.52 Z = -5309438.46 XDOT = -19952.050383 XDOT = -6081.384957 YDOT = 13450.976250 feet/sec YDOT = 4099.857561 meter/sec ZDOT = 1420.403180 ZDOT = 432.938889 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 18321.39132369 .00016717 00000-0 10270-3 0 9020 2 25544 51.6403 335.2616 0004867 55.1622 304.9987 15.53952654 22338 Satellite: ISS Catalog Number: 25544 Epoch time: 18321.39132369 = yrday.fracday Element set: 902 Inclination: 51.6403 deg RA of node: 335.2616 deg Eccentricity: .0004867 Arg of perigee: 55.1622 deg Mean anomaly: 304.9987 deg Mean motion: 15.53952654 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2233 Checksum: 312 Coasting Arc #4 (Orbit 2248) --------------------------------------- Vector Time (GMT): 2018/322/09:01:23.000 Vector Time (MET): N/A Weight (LBS) : 902349.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -202286.21 A = 6779412.58 meter Y = 4656938.63 meter E = .0011488 Z = 4916363.03 I = 51.43705 XDOT = -7047.835518 Wp = 57.65248 YDOT = 2057.602623 meter/sec RA = 329.71721 deg ZDOT = -2229.167869 TA = 54.21191 MA = 54.10517 Ha = 222.848 n.mi Hp = 213.283 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -663668.68 X = -278227.88 Y = 15278670.04 feet Y = 4654251.92 meter Z = 16129799.97 Z = 4915195.91 XDOT = -23122.819940 XDOT = -7059.492083 YDOT = 6750.664775 feet/sec YDOT = 1978.723646 meter/sec ZDOT = -7313.542877 ZDOT = -2263.432724 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -2376703.19 X = -724419.13 Y = -15113568.31 feet Y = -4606615.62 meter Z = 16123895.20 Z = 4914563.26 XDOT = 20098.416408 XDOT = 6125.997321 YDOT = -11162.172755 feet/sec YDOT = -3402.230256 meter/sec ZDOT = -7467.873051 ZDOT = -2276.207706 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 18322.42025504 .00016717 00000-0 10270-3 0 9038 2 25544 51.6408 330.1334 0004892 57.9857 302.1770 15.54009723 22490 Satellite: ISS Catalog Number: 25544 Epoch time: 18322.42025504 = yrday.fracday Element set: 903 Inclination: 51.6408 deg RA of node: 330.1334 deg Eccentricity: .0004892 Arg of perigee: 57.9857 deg Mean anomaly: 302.1770 deg Mean motion: 15.54009723 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2249 Checksum: 292 Coasting Arc #5 (Orbit 2255) --------------------------------------- Vector Time (GMT): 2018/322/19:30:01.000 Vector Time (MET): N/A Weight (LBS) : 917475.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5971982.69 A = 6785659.31 meter Y = -887673.84 meter E = .0017775 Z = 3077270.40 I = 51.44656 XDOT = -1681.974727 Wp = 76.79027 YDOT = 5677.561412 meter/sec RA = 327.57923 deg ZDOT = 4882.126459 TA = 318.70773 MA = 318.84201 Ha = 222.918 n.mi Hp = 213.199 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 19593119.06 X = 5966517.01 Y = -2912315.75 feet Y = -820921.53 meter Z = 10096031.48 Z = 3106267.49 XDOT = -5518.289786 XDOT = -1769.053039 YDOT = 18627.169987 feet/sec YDOT = 5658.265533 meter/sec ZDOT = 16017.475260 ZDOT = 4873.744334 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 19728019.92 X = 6013100.47 Y = 724886.53 feet Y = 220945.41 meter Z = 10226510.58 Z = 3117040.42 XDOT = -8898.354801 XDOT = -2712.218543 YDOT = 15839.430623 feet/sec YDOT = 4827.858454 meter/sec ZDOT = 15978.994488 ZDOT = 4870.397520 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 18322.87041443 .00016717 00000-0 10270-3 0 9048 2 25544 51.6421 327.8914 0005242 57.7622 302.4039 15.53973547 22562 Satellite: ISS Catalog Number: 25544 Epoch time: 18322.87041443 = yrday.fracday Element set: 904 Inclination: 51.6421 deg RA of node: 327.8914 deg Eccentricity: .0005242 Arg of perigee: 57.7622 deg Mean anomaly: 302.4039 deg Mean motion: 15.53973547 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2256 Checksum: 304 Coasting Arc #6 (Orbit 2264) --------------------------------------- Vector Time (GMT): 2018/323/10:20:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3768550.76 A = 6778514.29 meter Y = -2348682.92 meter E = .0018772 Z = -5138344.35 I = 51.40472 XDOT = 5335.228533 Wp = 74.06383 YDOT = -5279.243869 meter/sec RA = 324.47692 deg ZDOT = -1499.391687 TA = 181.41781 MA = 181.42314 Ha = 223.026 n.mi Hp = 213.039 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12364011.69 X = -3717047.15 Y = -7705652.64 feet Y = -2390537.51 meter Z = -16858085.14 Z = -5156525.95 XDOT = 17504.030621 XDOT = 5401.149393 YDOT = -17320.353901 feet/sec YDOT = -5219.213050 meter/sec ZDOT = -4919.264066 ZDOT = -1473.314338 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14473666.28 X = 4411573.48 Y = -87675.26 feet Y = -26723.42 meter Z = -16939486.40 Z = -5163155.45 XDOT = -5481.893202 XDOT = -1670.881048 YDOT = 22976.861116 feet/sec YDOT = 7003.347268 meter/sec ZDOT = -4801.300182 ZDOT = -1463.436295 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 18323.44918568 .00016717 00000-0 10270-3 0 9054 2 25544 51.6413 325.0058 0005164 62.7428 297.4250 15.53976215 22658 Satellite: ISS Catalog Number: 25544 Epoch time: 18323.44918568 = yrday.fracday Element set: 905 Inclination: 51.6413 deg RA of node: 325.0058 deg Eccentricity: .0005164 Arg of perigee: 62.7428 deg Mean anomaly: 297.4250 deg Mean motion: 15.53976215 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2265 Checksum: 316 Coasting Arc #7 (Orbit 2280) --------------------------------------- Vector Time (GMT): 2018/324/10:20:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2418591.54 A = 6777786.06 meter Y = 3483706.46 meter E = .0007966 Z = 5280779.68 I = 51.37415 XDOT = -6015.631068 Wp = 67.93357 YDOT = 4750.343846 meter/sec RA = 319.46131 deg ZDOT = -375.232837 TA = 25.67447 MA = 25.63494 Ha = 223.001 n.mi Hp = 213.051 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 7935011.60 X = 2353804.14 Y = 11429483.13 feet Y = 3510390.51 meter Z = 17325392.66 Z = 5292371.33 XDOT = -19736.322403 XDOT = -6066.480916 YDOT = 15585.117604 feet/sec YDOT = 4682.788564 meter/sec ZDOT = -1231.078860 ZDOT = -404.578844 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -12830047.06 X = -3910598.34 Y = -5214987.19 feet Y = -1589528.10 meter Z = 17377011.41 Z = 5296513.08 XDOT = 7466.310681 XDOT = 2275.731496 YDOT = -22949.670907 feet/sec YDOT = -6995.059693 meter/sec ZDOT = -1363.649654 ZDOT = -415.640414 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 18324.47811211 .00016717 00000-0 10270-3 0 9066 2 25544 51.6394 319.8776 0005321 66.7869 293.3843 15.53995769 22818 Satellite: ISS Catalog Number: 25544 Epoch time: 18324.47811211 = yrday.fracday Element set: 906 Inclination: 51.6394 deg RA of node: 319.8776 deg Eccentricity: .0005321 Arg of perigee: 66.7869 deg Mean anomaly: 293.3843 deg Mean motion: 15.53995769 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2281 Checksum: 348 Coasting Arc #8 (Orbit 2295) --------------------------------------- Vector Time (GMT): 2018/325/10:20:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1062395.20 A = 6779474.27 meter Y = -4546469.20 meter E = .0016624 Z = -4930388.05 I = 51.35632 XDOT = 6241.650958 Wp = 95.00174 YDOT = -3845.084882 meter/sec RA = 314.44542 deg ZDOT = 2205.752088 TA = 196.61839 MA = 196.67294 Ha = 223.059 n.mi Hp = 213.067 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3485548.56 X = -987526.49 Y = -14916237.54 feet Y = -4557930.86 meter Z = -16175813.80 Z = -4935367.24 XDOT = 20477.857475 XDOT = 6273.469209 YDOT = -12615.107881 feet/sec YDOT = -3775.108572 meter/sec ZDOT = 7236.719448 ZDOT = 2236.149829 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 11231314.70 X = 3423304.72 Y = 10382515.33 feet Y = 3164590.67 meter Z = -16197564.29 Z = -4937017.59 XDOT = -8937.759254 XDOT = -2724.229021 YDOT = 21146.635750 feet/sec YDOT = 6445.494576 meter/sec ZDOT = 7373.882162 ZDOT = 2247.559283 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 18325.44272689 .00016717 00000-0 10270-3 0 9075 2 25544 51.6407 315.0702 0005164 68.3634 291.8069 15.53975063 22967 Satellite: ISS Catalog Number: 25544 Epoch time: 18325.44272689 = yrday.fracday Element set: 907 Inclination: 51.6407 deg RA of node: 315.0702 deg Eccentricity: .0005164 Arg of perigee: 68.3634 deg Mean anomaly: 291.8069 deg Mean motion: 15.53975063 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2296 Checksum: 326 Coasting Arc #9 (Orbit 2303) --------------------------------------- Vector Time (GMT): 2018/325/21:45:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4228379.35 A = 6778605.88 meter Y = 1406422.16 meter E = .0008735 Z = 5100700.14 I = 51.34123 XDOT = -4022.451591 Wp = 95.22654 YDOT = 6341.401731 meter/sec RA = 312.09520 deg ZDOT = 1582.886820 TA = 339.44087 MA = 339.47600 Ha = 222.917 n.mi Hp = 213.147 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13872635.66 X = 4187560.89 Y = 4614245.94 feet Y = 1453478.38 meter Z = 16734580.51 Z = 5121141.62 XDOT = -13197.019657 XDOT = -4100.752998 YDOT = 20805.123791 feet/sec YDOT = 6295.982001 meter/sec ZDOT = 5193.198228 ZDOT = 1563.156710 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14384502.22 X = 4384396.28 Y = -1936595.96 feet Y = -590274.45 meter Z = 16826264.07 Z = 5128645.29 XDOT = -2823.315994 XDOT = -860.546715 YDOT = 23461.124874 feet/sec YDOT = 7150.950862 meter/sec ZDOT = 5103.641593 ZDOT = 1555.589958 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 18325.95718742 .00016717 00000-0 10270-3 0 9087 2 25544 51.6394 312.5051 0005124 68.0257 292.1439 15.53969947 23044 Satellite: ISS Catalog Number: 25544 Epoch time: 18325.95718742 = yrday.fracday Element set: 908 Inclination: 51.6394 deg RA of node: 312.5051 deg Eccentricity: .0005124 Arg of perigee: 68.0257 deg Mean anomaly: 292.1439 deg Mean motion: 15.53969947 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2304 Checksum: 325 Coasting Arc #10 (Orbit 2318) --------------------------------------- Vector Time (GMT): 2018/326/21:45:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3181407.38 A = 6777748.75 meter Y = -2821937.07 meter E = .0019708 Z = -5294670.60 I = 51.31534 XDOT = 4796.676634 Wp = 87.09931 YDOT = -5956.933310 meter/sec RA = 307.07410 deg ZDOT = 294.660745 TA = 185.71638 MA = 185.73891 Ha = 223.019 n.mi Hp = 212.910 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -10437688.25 X = -3123895.82 Y = -9258323.73 feet Y = -2857191.84 meter Z = -17370966.54 Z = -5309985.71 XDOT = 15737.128063 XDOT = 4861.500879 YDOT = -19543.744457 feet/sec YDOT = -5902.931106 meter/sec ZDOT = 966.734728 ZDOT = 318.119007 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13412590.47 X = -4088157.57 Y = -3518753.40 feet Y = -1072516.04 meter Z = -17439414.10 Z = -5315533.42 XDOT = 4802.961392 XDOT = 1463.942632 YDOT = -23594.267254 feet/sec YDOT = -7191.532659 meter/sec ZDOT = 1072.988694 ZDOT = 327.046954 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 18326.92179673 .00016717 00000-0 10270-3 0 9090 2 25544 51.6376 307.6962 0005126 72.4574 287.7138 15.54007852 23194 Satellite: ISS Catalog Number: 25544 Epoch time: 18326.92179673 = yrday.fracday Element set: 909 Inclination: 51.6376 deg RA of node: 307.6962 deg Eccentricity: .0005126 Arg of perigee: 72.4574 deg Mean anomaly: 287.7138 deg Mean motion: 15.54007852 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2319 Checksum: 338 Coasting Arc #11 (Orbit 2334) --------------------------------------- Vector Time (GMT): 2018/327/21:45:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2055963.12 A = 6779311.67 meter Y = 4162598.89 meter E = .0011178 Z = 4932848.23 I = 51.30191 XDOT = -5260.988515 Wp = 65.43934 YDOT = 5156.348329 meter/sec RA = 302.05378 deg ZDOT = -2150.055259 TA = 45.64489 MA = 45.55335 Ha = 222.926 n.mi Hp = 213.093 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 6745285.83 X = 1985301.20 Y = 13656820.52 feet Y = 4185194.55 meter Z = 16183885.27 Z = 4942664.39 XDOT = -17260.461006 XDOT = -5307.813139 YDOT = 16917.153309 feet/sec YDOT = 5097.254686 meter/sec ZDOT = -7053.987071 ZDOT = -2175.725211 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12300622.62 X = 3749229.78 Y = 8904534.48 feet Y = 2714102.11 meter Z = 16227437.22 Z = 4946122.86 XDOT = -6534.421627 XDOT = -1991.691712 YDOT = 22143.340894 feet/sec YDOT = 6749.290304 meter/sec ZDOT = -7170.067610 ZDOT = -2185.436608 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 18327.95071146 .00016717 00000-0 10270-3 0 9102 2 25544 51.6381 302.5679 0004959 76.3374 283.8330 15.53997690 23359 Satellite: ISS Catalog Number: 25544 Epoch time: 18327.95071146 = yrday.fracday Element set: 910 Inclination: 51.6381 deg RA of node: 302.5679 deg Eccentricity: .0004959 Arg of perigee: 76.3374 deg Mean anomaly: 283.8330 deg Mean motion: 15.53997690 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2335 Checksum: 335 Coasting Arc #12 (Orbit 2349) --------------------------------------- Vector Time (GMT): 2018/328/21:45:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -988084.66 A = 6782477.10 meter Y = -5311719.06 meter E = .0012202 Z = -4111797.28 I = 51.29579 XDOT = 5392.310428 Wp = 97.42900 YDOT = -3916.800935 meter/sec RA = 297.03755 deg ZDOT = 3772.129478 TA = 211.67157 MA = 211.74504 Ha = 223.015 n.mi Hp = 212.955 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3241747.59 X = -908640.75 Y = -17426899.82 feet Y = -5322323.87 meter Z = -13490148.55 Z = -4116404.76 XDOT = 17691.307178 XDOT = 5417.385034 YDOT = -12850.396770 feet/sec YDOT = -3856.360581 meter/sec ZDOT = 12375.752882 ZDOT = 3798.384471 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -11245620.58 X = -3427665.15 Y = -13682178.58 feet Y = -4170328.03 meter Z = -13510139.88 Z = -4117890.64 XDOT = 8116.008865 XDOT = 2473.759502 YDOT = -18981.646037 feet/sec YDOT = -5785.605712 meter/sec ZDOT = 12494.292133 ZDOT = 3808.260242 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 18328.91531563 .00016717 00000-0 10270-3 0 9114 2 25544 51.6380 297.7589 0005089 80.8042 279.3686 15.54016938 23509 Satellite: ISS Catalog Number: 25544 Epoch time: 18328.91531563 = yrday.fracday Element set: 911 Inclination: 51.6380 deg RA of node: 297.7589 deg Eccentricity: .0005089 Arg of perigee: 80.8042 deg Mean anomaly: 279.3686 deg Mean motion: 15.54016938 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2350 Checksum: 337 Coasting Arc #13 (Orbit 2365) --------------------------------------- Vector Time (GMT): 2018/329/21:45:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -38052.15 A = 6786183.03 meter Y = 6156013.25 meter E = .0018176 Z = 2837722.89 I = 51.29422 XDOT = -5297.308824 Wp = 94.89035 YDOT = 2306.553981 meter/sec RA = 292.03118 deg ZDOT = -5048.296383 TA = 52.66769 MA = 52.50221 Ha = 222.939 n.mi Hp = 212.997 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -124843.02 X = -120671.95 Y = 20196893.88 feet Y = 6155125.45 meter Z = 9310114.48 Z = 2837338.07 XDOT = -17379.622127 XDOT = -5298.185326 YDOT = 7567.434320 feet/sec YDOT = 2247.311467 meter/sec ZDOT = -16562.652176 ZDOT = -5074.031124 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9983563.98 X = 3042990.30 Y = 17558646.40 feet Y = 5351875.42 meter Z = 9307562.88 Z = 2836945.17 XDOT = -9851.499112 XDOT = -3002.736929 YDOT = 14488.516189 feet/sec YDOT = 4416.099734 meter/sec ZDOT = -16678.636333 ZDOT = -5083.648354 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 18329.94422111 .00016717 00000-0 10270-3 0 9127 2 25544 51.6380 292.6304 0004963 83.2201 276.9516 15.54037670 23660 Satellite: ISS Catalog Number: 25544 Epoch time: 18329.94422111 = yrday.fracday Element set: 912 Inclination: 51.6380 deg RA of node: 292.6304 deg Eccentricity: .0004963 Arg of perigee: 83.2201 deg Mean anomaly: 276.9516 deg Mean motion: 15.54037670 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2366 Checksum: 301 Coasting Arc #14 (Orbit 2380) --------------------------------------- Vector Time (GMT): 2018/330/21:45:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 907769.58 A = 6788899.44 meter Y = -6592884.29 meter E = .0012718 Z = -1326728.43 I = 51.29102 XDOT = 4998.745631 Wp = 56.23903 YDOT = -467.979016 meter/sec RA = 287.03299 deg ZDOT = 5792.802128 TA = 289.25120 MA = 289.38875 Ha = 223.065 n.mi Hp = 212.924 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 2978246.67 X = 987870.20 Y = -21630197.82 feet Y = -6582284.97 meter Z = -4352783.57 Z = -1322124.92 XDOT = 16400.084090 XDOT = 4975.468545 YDOT = -1535.364225 feet/sec YDOT = -412.210346 meter/sec ZDOT = 19005.256324 ZDOT = 5817.027945 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8611090.89 X = -2624660.50 Y = -20069174.05 feet Y = -6117084.25 meter Z = -4331224.13 Z = -1320157.12 XDOT = 11671.948313 XDOT = 3557.609846 YDOT = -9099.732995 feet/sec YDOT = -2773.598617 meter/sec ZDOT = 19114.216864 ZDOT = 5826.013300 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 18330.90882021 .00016717 00000-0 10270-3 0 9136 2 25544 51.6372 287.8228 0005192 89.3802 270.7945 15.54020217 23815 Satellite: ISS Catalog Number: 25544 Epoch time: 18330.90882021 = yrday.fracday Element set: 913 Inclination: 51.6372 deg RA of node: 287.8228 deg Eccentricity: .0005192 Arg of perigee: 89.3802 deg Mean anomaly: 270.7945 deg Mean motion: 15.54020217 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2381 Checksum: 305 Coasting Arc #15 (Orbit 2391) --------------------------------------- Vector Time (GMT): 2018/331/13:15:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1692243.84 A = 6789613.05 meter Y = -6568413.34 meter E = .0016514 Z = 93406.15 I = 51.28961 XDOT = 4621.590895 Wp = 58.31880 YDOT = 1286.757244 meter/sec RA = 283.81478 deg ZDOT = 5983.111187 TA = 302.69230 MA = 302.85145 Ha = 223.027 n.mi Hp = 212.923 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5551981.10 X = 1765114.18 Y = -21549912.52 feet Y = -6549082.06 meter Z = 306450.62 Z = 101802.88 XDOT = 15162.699786 XDOT = 4577.795540 YDOT = 4221.644502 feet/sec YDOT = 1338.193618 meter/sec ZDOT = 19629.629878 ZDOT = 6005.455179 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 20888661.81 X = 6366864.12 Y = 7672149.96 feet Y = 2338471.31 meter Z = 345048.60 Z = 105170.81 XDOT = -5142.282281 XDOT = -1567.367639 YDOT = 13012.008969 feet/sec YDOT = 3966.060334 meter/sec ZDOT = 19729.906078 ZDOT = 6013.675373 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 18331.61619003 .00016717 00000-0 10270-3 0 9144 2 25544 51.6393 284.3009 0005140 88.2842 271.8899 15.54029935 23920 Satellite: ISS Catalog Number: 25544 Epoch time: 18331.61619003 = yrday.fracday Element set: 914 Inclination: 51.6393 deg RA of node: 284.3009 deg Eccentricity: .0005140 Arg of perigee: 88.2842 deg Mean anomaly: 271.8899 deg Mean motion: 15.54029935 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2392 Checksum: 318 Coasting Arc #16 (Orbit 2406) --------------------------------------- Vector Time (GMT): 2018/332/13:15:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2386304.36 A = 6788236.44 meter Y = 6100522.15 meter E = .0011363 Z = -1774563.02 I = 51.27916 XDOT = -4072.873339 Wp = 120.67351 YDOT = -3223.183521 meter/sec RA = 278.81942 deg ZDOT = -5636.305484 TA = 78.90735 MA = 78.77959 Ha = 223.014 n.mi Hp = 212.895 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -7829082.55 X = -2445724.82 Y = 20014836.44 feet Y = 6073504.73 meter Z = -5822057.17 Z = -1786298.76 XDOT = -13362.445337 XDOT = -4009.149785 YDOT = -10574.749086 feet/sec YDOT = -3268.372479 meter/sec ZDOT = -18491.815891 ZDOT = -5655.935651 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -19302168.73 X = -5883301.03 Y = -9417445.79 feet Y = -2870437.48 meter Z = -5875590.03 Z = -1790879.84 XDOT = 10947.286883 XDOT = 3336.733042 YDOT = -10912.106562 feet/sec YDOT = -3326.010080 meter/sec ZDOT = -18579.654053 ZDOT = -5663.078555 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 18332.58078083 .00016717 00000-0 10270-3 0 9159 2 25544 51.6402 279.4927 0005166 90.3970 269.7774 15.54034865 24072 Satellite: ISS Catalog Number: 25544 Epoch time: 18332.58078083 = yrday.fracday Element set: 915 Inclination: 51.6402 deg RA of node: 279.4927 deg Eccentricity: .0005166 Arg of perigee: 90.3970 deg Mean anomaly: 269.7774 deg Mean motion: 15.54034865 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2407 Checksum: 335 Coasting Arc #17 (Orbit 2422) --------------------------------------- Vector Time (GMT): 2018/333/13:15:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2938903.88 A = 6785133.60 meter Y = -5186291.73 meter E = .0017919 Z = 3224975.25 I = 51.26388 XDOT = 3479.771514 Wp = 89.10727 YDOT = 4931.904640 meter/sec RA = 273.81808 deg ZDOT = 4737.622903 TA = 308.48313 MA = 308.64373 Ha = 222.990 n.mi Hp = 212.887 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 9642073.11 X = 2981014.73 Y = -17015392.81 feet Y = -5153191.59 meter Z = 10580627.45 Z = 3239353.47 XDOT = 11416.573209 XDOT = 3401.349989 YDOT = 16180.789500 feet/sec YDOT = 4970.379115 meter/sec ZDOT = 15543.382227 ZDOT = 4754.336298 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 16351302.50 X = 4983877.00 Y = 10665004.55 feet Y = 3250693.39 meter Z = 10645911.33 Z = 3244873.77 XDOT = -16110.326395 XDOT = -4910.427485 YDOT = 9036.437056 feet/sec YDOT = 2754.306015 meter/sec ZDOT = 15617.907534 ZDOT = 4760.338216 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 18333.60967415 .00016717 00000-0 10270-3 0 9160 2 25544 51.6393 274.3651 0005205 94.2230 265.9517 15.54036057 24231 Satellite: ISS Catalog Number: 25544 Epoch time: 18333.60967415 = yrday.fracday Element set: 916 Inclination: 51.6393 deg RA of node: 274.3651 deg Eccentricity: .0005205 Arg of perigee: 94.2230 deg Mean anomaly: 265.9517 deg Mean motion: 15.54036057 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2423 Checksum: 305 Coasting Arc #18 (Orbit 2437) --------------------------------------- Vector Time (GMT): 2018/334/13:15:00.000 Vector Time (MET): N/A Weight (LBS) : 932630.3 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3448583.02 A = 6781264.30 meter Y = 3857910.72 meter E = .0013873 Z = -4396195.84 I = 51.25080 XDOT = -2805.799510 Wp = 79.46457 YDOT = -6297.362498 meter/sec RA = 268.80608 deg ZDOT = -3331.800800 TA = 156.65389 MA = 156.59083 Ha = 222.974 n.mi Hp = 212.779 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -11314248.77 X = -3470112.42 Y = 12657187.39 feet Y = 3819226.06 meter Z = -14423214.70 Z = -4413000.11 XDOT = -9205.378970 XDOT = -2718.987880 YDOT = -20660.638117 feet/sec YDOT = -6328.253375 meter/sec ZDOT = -10931.104988 ZDOT = -3345.219878 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -12099389.35 X = -3687893.88 Y = -11816208.51 feet Y = -3601580.35 meter Z = -14499232.18 Z = -4419365.97 XDOT = 20216.866835 XDOT = 6162.101011 YDOT = -7241.200289 feet/sec YDOT = -2207.117848 meter/sec ZDOT = -10990.669198 ZDOT = -3349.955971 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 18334.57425848 .00016717 00000-0 10270-3 0 9177 2 25544 51.6401 269.5572 0005175 97.3424 262.8317 15.54061210 24383 Satellite: ISS Catalog Number: 25544 Epoch time: 18334.57425848 = yrday.fracday Element set: 917 Inclination: 51.6401 deg RA of node: 269.5572 deg Eccentricity: .0005175 Arg of perigee: 97.3424 deg Mean anomaly: 262.8317 deg Mean motion: 15.54061210 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2438 Checksum: 314