ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 18836.84 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 763) --------------------------------------- Vector Time (GMT): 2010/067/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6234802.97 A = 6730671.74 meter Y = 1045767.73 meter E = .0013586 Z = -2295663.59 I = 51.81059 XDOT = 1106.466435 Wp = 32.18011 YDOT = 5321.865514 meter/sec RA = 26.11907 deg ZDOT = 5455.335592 TA = 302.08120 MA = 302.21303 Ha = 192.727 n.mi Hp = 182.606 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 20455390.31 X = 6233797.35 Y = 3430996.50 feet Y = 1115483.32 meter Z = -7531704.71 Z = -2265377.91 XDOT = 3630.139224 XDOT = 1020.373567 YDOT = 17460.188693 feet/sec YDOT = 5333.757445 meter/sec ZDOT = 17898.082651 ZDOT = 5460.501464 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 16820256.55 X = 5126814.20 Y = -12209495.86 feet Y = -3721454.34 meter Z = -7411375.44 Z = -2258987.23 XDOT = 14030.020551 XDOT = 4276.350264 YDOT = 8503.839446 feet/sec YDOT = 2591.970263 meter/sec ZDOT = 17918.706991 ZDOT = 5461.621891 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 10067.67113940 .00016717 00000-0 10270-3 0 9002 2 25544 51.6488 26.6488 0007819 24.1633 335.9895 15.73746945 7642 Satellite: ISS Catalog Number: 25544 Epoch time: 10067.67113940 = yrday.fracday Element set: 900 Inclination: 51.6488 deg RA of node: 26.6488 deg Eccentricity: .0007819 Arg of perigee: 24.1633 deg Mean anomaly: 335.9895 deg Mean motion: 15.73746945 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 764 Checksum: 338 Coasting Arc #2 (Orbit 779) --------------------------------------- Vector Time (GMT): 2010/068/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1443844.14 A = 6723017.77 meter Y = -4559344.27 meter E = .0017924 Z = -4741953.17 I = 51.75796 XDOT = 7188.652573 Wp = 53.22008 YDOT = 507.495855 meter/sec RA = 21.03651 deg ZDOT = -2673.210459 TA = 190.47779 MA = 190.51519 Ha = 192.674 n.mi Hp = 182.361 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4737021.46 X = -1369718.34 Y = -14958478.58 feet Y = -4575075.90 meter Z = -15557589.14 Z = -4748787.02 XDOT = 23584.818152 XDOT = 7195.429101 YDOT = 1665.012649 feet/sec YDOT = 587.921434 meter/sec ZDOT = -8770.375521 ZDOT = -2638.272246 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14043872.28 X = -4280572.27 Y = -6936637.72 feet Y = -2114287.18 meter Z = -15584824.09 Z = -4750254.38 XDOT = 16982.356658 XDOT = 5176.222309 YDOT = -14963.235532 feet/sec YDOT = -4560.794190 meter/sec ZDOT = -8631.573660 ZDOT = -2630.903652 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 10068.68713421 .00016717 00000-0 10270-3 0 9015 2 25544 51.6491 21.4339 0007864 27.3490 332.8086 15.73783857 7809 Satellite: ISS Catalog Number: 25544 Epoch time: 10068.68713421 = yrday.fracday Element set: 901 Inclination: 51.6491 deg RA of node: 21.4339 deg Eccentricity: .0007864 Arg of perigee: 27.3490 deg Mean anomaly: 332.8086 deg Mean motion: 15.73783857 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 780 Checksum: 318 Coasting Arc #3 (Orbit 795) --------------------------------------- Vector Time (GMT): 2010/069/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6292390.47 A = 6730441.09 meter Y = 155696.46 meter E = .0017698 Z = 2372968.72 I = 51.75390 XDOT = -2174.373279 Wp = 81.17621 YDOT = -5041.776060 meter/sec RA = 15.86985 deg ZDOT = -5398.225279 TA = 72.13291 MA = 71.93996 Ha = 192.794 n.mi Hp = 182.311 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20644325.69 X = -6305191.03 Y = 510815.15 feet Y = 85259.76 meter Z = 7785330.45 Z = 2342369.86 XDOT = -7133.770601 XDOT = -2091.610609 YDOT = -16541.260041 feet/sec YDOT = -5065.628714 meter/sec ZDOT = -17710.712859 ZDOT = -5408.586872 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13615335.18 X = -4149954.16 Y = 15586841.02 feet Y = 4750869.14 meter Z = 7663779.78 Z = 2335920.08 XDOT = -15802.752564 XDOT = -4816.678981 YDOT = -5015.382351 feet/sec YDOT = -1528.688541 meter/sec ZDOT = -17751.971505 ZDOT = -5410.800915 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 10069.70311080 .00016717 00000-0 10270-3 0 9025 2 25544 51.6489 16.2186 0007818 32.0999 328.0639 15.73777997 7960 Satellite: ISS Catalog Number: 25544 Epoch time: 10069.70311080 = yrday.fracday Element set: 902 Inclination: 51.6489 deg RA of node: 16.2186 deg Eccentricity: .0007818 Arg of perigee: 32.0999 deg Mean anomaly: 328.0639 deg Mean motion: 15.73777997 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 796 Checksum: 339 Coasting Arc #4 (Orbit 811) --------------------------------------- Vector Time (GMT): 2010/070/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2338546.40 A = 6723080.11 meter Y = 4208781.83 meter E = .0011717 Z = 4681242.07 I = 51.70083 XDOT = -7137.687762 Wp = 75.69427 YDOT = 873.419526 meter/sec RA = 10.78367 deg ZDOT = 2777.492044 TA = 346.96060 MA = 346.99087 Ha = 192.728 n.mi Hp = 182.088 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 7672396.34 X = 2268569.13 Y = 13808339.35 feet Y = 4234541.90 meter Z = 15358405.76 Z = 4692432.22 XDOT = -23417.610768 XDOT = -7160.416261 YDOT = 2865.549627 feet/sec YDOT = 793.474767 meter/sec ZDOT = 9112.506706 ZDOT = 2742.762672 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15361986.40 X = 4682333.46 Y = 3489315.47 feet Y = 1063543.35 meter Z = 15402940.63 Z = 4694816.30 XDOT = -13174.175798 XDOT = -4015.488783 YDOT = 18341.620608 feet/sec YDOT = 5590.525961 meter/sec ZDOT = 8974.563903 ZDOT = 2735.447078 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 10070.71906562 .00016717 00000-0 10270-3 0 9034 2 25544 51.6493 11.0031 0007861 35.0501 325.1178 15.73818058 8126 Satellite: ISS Catalog Number: 25544 Epoch time: 10070.71906562 = yrday.fracday Element set: 903 Inclination: 51.6493 deg RA of node: 11.0031 deg Eccentricity: .0007861 Arg of perigee: 35.0501 deg Mean anomaly: 325.1178 deg Mean motion: 15.73818058 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 812 Checksum: 274 Coasting Arc #5 (Orbit 826) --------------------------------------- Vector Time (GMT): 2010/071/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6109723.10 A = 6730023.22 meter Y = -1356839.95 meter E = .0013233 Z = -2465751.95 I = 51.69434 XDOT = 3158.186131 Wp = 40.91449 YDOT = 4553.317582 meter/sec RA = 5.61118 deg ZDOT = 5345.781298 TA = 291.23791 MA = 291.37920 Ha = 192.788 n.mi Hp = 182.027 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 20045023.30 X = 6136419.37 Y = -4451574.65 feet Y = -1288368.34 meter Z = -8089737.37 Z = -2436006.59 XDOT = 10361.503055 XDOT = 3081.067110 YDOT = 14938.705977 feet/sec YDOT = 4588.203554 meter/sec ZDOT = 17538.652553 ZDOT = 5360.935733 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9689492.84 X = 2953357.42 Y = -18155730.17 feet Y = -5533866.56 meter Z = -7971606.93 Z = -2429745.79 XDOT = 16695.289911 XDOT = 5088.724365 YDOT = 1220.789683 feet/sec YDOT = 372.096695 meter/sec ZDOT = 17598.942421 ZDOT = 5364.157650 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 10071.67150478 .00016717 00000-0 10270-3 0 9048 2 25544 51.6491 6.1136 0007803 37.0306 323.1395 15.73852144 8275 Satellite: ISS Catalog Number: 25544 Epoch time: 10071.67150478 = yrday.fracday Element set: 904 Inclination: 51.6491 deg RA of node: 6.1136 deg Eccentricity: .0007803 Arg of perigee: 37.0306 deg Mean anomaly: 323.1395 deg Mean motion: 15.73852144 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 827 Checksum: 287 Coasting Arc #6 (Orbit 842) --------------------------------------- Vector Time (GMT): 2010/072/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3120438.55 A = 6722985.26 meter Y = -3721617.91 meter E = .0018085 Z = -4666277.13 I = 51.64053 XDOT = 6811.628399 Wp = 57.85520 YDOT = -2171.393973 meter/sec RA = .52129 deg ZDOT = -2821.792968 TA = 184.21967 MA = 184.23494 Ha = 192.692 n.mi Hp = 181.776 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -10237659.29 X = -3055923.33 Y = -12210032.50 feet Y = -3756152.25 meter Z = -15309308.18 Z = -4681278.86 XDOT = 22347.862201 XDOT = 6849.110565 YDOT = -7123.995975 feet/sec YDOT = -2095.013004 meter/sec ZDOT = -9257.850946 ZDOT = -2788.611442 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -15876484.58 X = -4839152.50 Y = 36752.11 feet Y = 11202.04 meter Z = -15368974.10 Z = -4684463.31 XDOT = 8791.255935 XDOT = 2679.574809 YDOT = -20645.052828 feet/sec YDOT = -6292.612102 meter/sec ZDOT = -9126.094171 ZDOT = -2781.633503 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 10072.68742080 .00016717 00000-0 10270-3 0 9057 2 25544 51.6486 .8978 0007714 40.4919 319.6817 15.73889526 8434 Satellite: ISS Catalog Number: 25544 Epoch time: 10072.68742080 = yrday.fracday Element set: 905 Inclination: 51.6486 deg RA of node: .8978 deg Eccentricity: .0007714 Arg of perigee: 40.4919 deg Mean anomaly: 319.6817 deg Mean motion: 15.73889526 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 843 Checksum: 335 Coasting Arc #7 (Orbit 858) --------------------------------------- Vector Time (GMT): 2010/073/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5766808.96 A = 6729781.61 meter Y = 2427568.83 meter E = .0018960 Z = 2465135.99 I = 51.63396 XDOT = -3943.299644 Wp = 83.87323 YDOT = -3914.510462 meter/sec RA = 355.34416 deg ZDOT = -5332.916136 TA = 68.25361 MA = 68.05191 Ha = 192.745 n.mi Hp = 181.686 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18919976.90 X = -5805500.87 Y = 7964464.67 feet Y = 2362864.88 meter Z = 8087716.51 Z = 2437027.00 XDOT = -12937.334791 XDOT = -3873.327855 YDOT = -12842.882094 feet/sec YDOT = -3958.216145 meter/sec ZDOT = -17496.444016 ZDOT = -5351.902002 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -5612193.97 X = -1710596.72 Y = 19791264.60 feet Y = 6032377.45 meter Z = 7976121.00 Z = 2431121.68 XDOT = -16601.441082 XDOT = -5060.119242 YDOT = 2423.619977 feet/sec YDOT = 738.719369 meter/sec ZDOT = -17571.937071 ZDOT = -5355.926419 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 10073.70331694 .00016717 00000-0 10270-3 0 9067 2 25544 51.6491 355.6825 0007811 44.5357 315.6432 15.73940294 8597 Satellite: ISS Catalog Number: 25544 Epoch time: 10073.70331694 = yrday.fracday Element set: 906 Inclination: 51.6491 deg RA of node: 355.6825 deg Eccentricity: .0007811 Arg of perigee: 44.5357 deg Mean anomaly: 315.6432 deg Mean motion: 15.73940294 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 859 Checksum: 318 Coasting Arc #8 (Orbit 874) --------------------------------------- Vector Time (GMT): 2010/074/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3740454.70 A = 6722920.02 meter Y = 3092012.70 meter E = .0012991 Z = 4640728.30 I = 51.58007 XDOT = -6322.177728 Wp = 82.67773 YDOT = 3374.032627 meter/sec RA = 350.24947 deg ZDOT = 2842.536419 TA = 339.22194 MA = 339.27470 Ha = 192.700 n.mi Hp = 181.582 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12271833.02 X = 3683057.68 Y = 10144398.62 feet Y = 3133520.31 meter Z = 15225486.55 Z = 4658759.46 XDOT = -20742.052914 XDOT = -6373.245272 YDOT = 11069.660850 feet/sec YDOT = 3303.049078 meter/sec ZDOT = 9325.906888 ZDOT = 2811.699161 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15471886.63 X = 4715831.04 Y = -3455366.83 feet Y = -1053195.81 meter Z = 15297166.86 Z = 4662576.46 XDOT = -4180.241053 XDOT = -1274.137473 YDOT = 22101.212564 feet/sec YDOT = 6736.449589 meter/sec ZDOT = 9203.503241 ZDOT = 2805.227788 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 10074.71919381 .00016717 00000-0 10270-3 0 9075 2 25544 51.6482 350.4662 0007785 48.3978 311.7851 15.73919911 8752 Satellite: ISS Catalog Number: 25544 Epoch time: 10074.71919381 = yrday.fracday Element set: 907 Inclination: 51.6482 deg RA of node: 350.4662 deg Eccentricity: .0007785 Arg of perigee: 48.3978 deg Mean anomaly: 311.7851 deg Mean motion: 15.73919911 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 875 Checksum: 341 Coasting Arc #9 (Orbit 889) --------------------------------------- Vector Time (GMT): 2010/075/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5224968.39 A = 6729620.35 meter Y = -3433574.60 meter E = .0012995 Z = -2484530.20 I = 51.57247 XDOT = 4586.245047 Wp = 49.59766 YDOT = 3146.977679 meter/sec RA = 345.06663 deg ZDOT = 5322.273779 TA = 282.27684 MA = 282.42232 Ha = 192.703 n.mi Hp = 181.525 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17142284.74 X = 5275044.23 Y = -11265008.53 feet Y = -3374866.20 meter Z = -8151345.80 Z = -2459025.41 XDOT = 15046.735718 XDOT = 4524.859615 YDOT = 10324.729919 feet/sec YDOT = 3197.921199 meter/sec ZDOT = 17461.528145 ZDOT = 5344.404157 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 1219070.30 X = 371572.63 Y = -20516141.79 feet Y = -6253320.02 meter Z = -8050128.91 Z = -2453679.29 XDOT = 15706.940197 XDOT = 4787.475372 YDOT = -5918.269578 feet/sec YDOT = -1803.888567 meter/sec ZDOT = 17549.485273 ZDOT = 5349.083111 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 10075.67155720 .00016717 00000-0 10270-3 0 9081 2 25544 51.6472 345.5759 0007578 51.3717 308.8123 15.73975688 8907 Satellite: ISS Catalog Number: 25544 Epoch time: 10075.67155720 = yrday.fracday Element set: 908 Inclination: 51.6472 deg RA of node: 345.5759 deg Eccentricity: .0007578 Arg of perigee: 51.3717 deg Mean anomaly: 308.8123 deg Mean motion: 15.73975688 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 890 Checksum: 342 Coasting Arc #10 (Orbit 905) --------------------------------------- Vector Time (GMT): 2010/076/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4213715.23 A = 6722614.97 meter Y = -2412583.27 meter E = .0018469 Z = -4667396.76 I = 51.51933 XDOT = 5630.228963 Wp = 64.20757 YDOT = -4420.681376 meter/sec RA = 339.96740 deg ZDOT = -2798.590827 TA = 178.07694 MA = 178.06983 Ha = 192.657 n.mi Hp = 181.235 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -13824525.03 X = -4163750.77 Y = -7915299.44 feet Y = -2459424.68 meter Z = -15312981.50 Z = -4687745.34 XDOT = 18471.879800 XDOT = 5692.838392 YDOT = -14503.547823 feet/sec YDOT = -4357.371045 meter/sec ZDOT = -9181.728434 ZDOT = -2771.086653 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14437315.92 X = -4400493.89 Y = 6546021.96 feet Y = 1995227.49 meter Z = -15393841.80 Z = -4692042.98 XDOT = -509.688022 XDOT = -155.352909 YDOT = -22454.258244 feet/sec YDOT = -6844.057913 meter/sec ZDOT = -9072.597954 ZDOT = -2765.327857 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 10076.68739319 .00016717 00000-0 10270-3 0 9096 2 25544 51.6460 340.3596 0007576 55.6688 304.5191 15.74008429 9065 Satellite: ISS Catalog Number: 25544 Epoch time: 10076.68739319 = yrday.fracday Element set: 909 Inclination: 51.6460 deg RA of node: 340.3596 deg Eccentricity: .0007576 Arg of perigee: 55.6688 deg Mean anomaly: 304.5191 deg Mean motion: 15.74008429 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 906 Checksum: 335 Coasting Arc #11 (Orbit 921) --------------------------------------- Vector Time (GMT): 2010/077/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4593711.53 A = 6729459.98 meter Y = 4278889.34 meter E = .0019749 Z = 2407230.75 I = 51.51563 XDOT = -5013.036343 Wp = 89.18570 YDOT = -2346.613406 meter/sec RA = 334.78063 deg ZDOT = -5357.197410 TA = 63.59581 MA = 63.39324 Ha = 192.565 n.mi Hp = 181.233 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -15071232.05 X = -4652911.33 Y = 14038350.85 feet Y = 4227188.95 meter Z = 7897738.68 Z = 2384770.27 XDOT = -16446.969630 XDOT = -4960.399160 YDOT = -7698.862880 feet/sec YDOT = -2402.378345 meter/sec ZDOT = -17576.106989 ZDOT = -5381.422712 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 2947205.85 X = 898308.34 Y = 20418882.50 feet Y = 6223675.38 meter Z = 7808637.64 Z = 2380072.75 XDOT = -14139.732025 XDOT = -4309.790321 YDOT = 8847.447189 feet/sec YDOT = 2696.701903 meter/sec ZDOT = -17672.356237 ZDOT = -5386.534181 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 10077.70320686 .00016717 00000-0 10270-3 0 9105 2 25544 51.6466 335.1430 0007529 57.7814 302.4078 15.74090682 9223 Satellite: ISS Catalog Number: 25544 Epoch time: 10077.70320686 = yrday.fracday Element set: 910 Inclination: 51.6466 deg RA of node: 335.1430 deg Eccentricity: .0007529 Arg of perigee: 57.7814 deg Mean anomaly: 302.4078 deg Mean motion: 15.74090682 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 922 Checksum: 302 Coasting Arc #12 (Orbit 937) --------------------------------------- Vector Time (GMT): 2010/078/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4513326.48 A = 6722380.74 meter Y = 1677830.16 meter E = .0013540 Z = 4679378.09 I = 51.46338 XDOT = -4831.274276 Wp = 90.42168 YDOT = 5349.457863 meter/sec RA = 329.67553 deg ZDOT = 2734.848744 TA = 332.57396 MA = 332.64536 Ha = 192.552 n.mi Hp = 181.162 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14807501.59 X = 4471497.59 Y = 5504692.12 feet Y = 1728067.32 meter Z = 15352290.32 Z = 4701202.18 XDOT = -15850.637389 XDOT = -4904.019245 YDOT = 17550.714773 feet/sec YDOT = 5295.025141 meter/sec ZDOT = 8972.600867 ZDOT = 2711.201248 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 12742678.54 X = 3883968.42 Y = -9193387.47 feet Y = -2802144.50 meter Z = 15438987.24 Z = 4705803.31 XDOT = 5114.626118 XDOT = 1558.938041 YDOT = 22037.681922 feet/sec YDOT = 6717.085450 meter/sec ZDOT = 8878.809651 ZDOT = 2706.261182 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 10078.71900396 .00016717 00000-0 10270-3 0 9110 2 25544 51.6452 329.9257 0007570 63.0621 297.1315 15.74046819 9382 Satellite: ISS Catalog Number: 25544 Epoch time: 10078.71900396 = yrday.fracday Element set: 911 Inclination: 51.6452 deg RA of node: 329.9257 deg Eccentricity: .0007570 Arg of perigee: 63.0621 deg Mean anomaly: 297.1315 deg Mean motion: 15.74046819 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 938 Checksum: 316 Coasting Arc #13 (Orbit 952) --------------------------------------- Vector Time (GMT): 2010/079/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3810942.92 A = 6729507.54 meter Y = -5021749.77 meter E = .0012996 Z = -2352242.01 I = 51.46182 XDOT = 5286.680172 Wp = 57.68895 YDOT = 1500.867087 meter/sec RA = 324.48439 deg ZDOT = 5389.419528 TA = 275.76399 MA = 275.91215 Ha = 192.608 n.mi Hp = 181.046 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12503093.57 X = 3878240.59 Y = -16475556.98 feet Y = -4978757.38 meter Z = -7717329.43 Z = -2333564.67 XDOT = 17344.751219 XDOT = 5243.323378 YDOT = 4924.104616 feet/sec YDOT = 1559.743743 meter/sec ZDOT = 17681.822600 ZDOT = 5414.996908 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7086662.86 X = -2160014.84 Y = -19459912.12 feet Y = -5931381.22 meter Z = -7643266.96 Z = -2329667.77 XDOT = 12038.236664 XDOT = 3669.254535 YDOT = -11331.683826 feet/sec YDOT = -3453.897230 meter/sec ZDOT = 17783.418579 ZDOT = 5420.385983 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 10079.67129162 .00016717 00000-0 10270-3 0 9121 2 25544 51.6446 325.0343 0007496 68.0002 292.1957 15.74105805 9538 Satellite: ISS Catalog Number: 25544 Epoch time: 10079.67129162 = yrday.fracday Element set: 912 Inclination: 51.6446 deg RA of node: 325.0343 deg Eccentricity: .0007496 Arg of perigee: 68.0002 deg Mean anomaly: 292.1957 deg Mean motion: 15.74105805 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 953 Checksum: 303 Coasting Arc #14 (Orbit 968) --------------------------------------- Vector Time (GMT): 2010/080/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4678125.65 A = 6721888.81 meter Y = -975719.28 meter E = .0019203 Z = -4745445.55 I = 51.41266 XDOT = 3906.199790 Wp = 71.46812 YDOT = -6086.449033 meter/sec RA = 319.37477 deg ZDOT = -2601.940972 TA = 172.88130 MA = 172.85400 Ha = 192.593 n.mi Hp = 180.730 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -15348181.28 X = -4643814.76 Y = -3201178.74 feet Y = -1027841.18 meter Z = -15569047.09 Z = -4768088.53 XDOT = 12815.616108 XDOT = 3986.608999 YDOT = -19968.664806 feet/sec YDOT = -6042.318082 meter/sec ZDOT = -8536.551747 ZDOT = -2582.769121 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -10742808.90 X = -3274408.15 Y = 11295920.05 feet Y = 3442996.43 meter Z = -15658981.07 Z = -4772857.43 XDOT = -9401.484389 XDOT = -2865.572442 YDOT = -20657.816657 feet/sec YDOT = -6296.502517 meter/sec ZDOT = -8460.546498 ZDOT = -2578.774573 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 10080.68704624 .00016717 00000-0 10270-3 0 9137 2 25544 51.6444 319.8174 0007630 72.0513 288.1481 15.74146795 9698 Satellite: ISS Catalog Number: 25544 Epoch time: 10080.68704624 = yrday.fracday Element set: 913 Inclination: 51.6444 deg RA of node: 319.8174 deg Eccentricity: .0007630 Arg of perigee: 72.0513 deg Mean anomaly: 288.1481 deg Mean motion: 15.74146795 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 969 Checksum: 319 Coasting Arc #15 (Orbit 984) --------------------------------------- Vector Time (GMT): 2010/081/16:00:00.000 Vector Time (MET): N/A Weight (LBS) : 798335.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2999609.32 A = 6729569.44 meter Y = 5600697.04 meter E = .0020565 Z = 2196221.83 I = 51.41665 XDOT = -5380.595470 Wp = 97.04970 YDOT = -721.777313 meter/sec RA = 314.18140 deg ZDOT = -5467.007144 TA = 58.24537 MA = 58.04515 Ha = 192.461 n.mi Hp = 180.877 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -9841237.94 X = -3072683.19 Y = 18374990.30 feet Y = 5566745.10 meter Z = 7205452.20 Z = 2181472.15 XDOT = -17652.872278 XDOT = -5345.566881 YDOT = -2368.035805 feet/sec YDOT = -781.750603 meter/sec ZDOT = -17936.375145 ZDOT = -5493.060889 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 10746149.18 X = 3275426.27 Y = 17884336.16 feet Y = 5451145.66 meter Z = 7146997.43 Z = 2178404.82 XDOT = -9697.000545 XDOT = -2955.645766 YDOT = 13090.224175 feet/sec YDOT = 3989.900329 meter/sec ZDOT = -18039.850803 ZDOT = -5498.546525 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 10081.70277822 .00016717 00000-0 10270-3 0 9147 2 25544 51.6444 314.5995 0007381 74.7162 285.4817 15.74192747 9852 Satellite: ISS Catalog Number: 25544 Epoch time: 10081.70277822 = yrday.fracday Element set: 914 Inclination: 51.6444 deg RA of node: 314.5995 deg Eccentricity: .0007381 Arg of perigee: 74.7162 deg Mean anomaly: 285.4817 deg Mean motion: 15.74192747 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 985 Checksum: 333