ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 10494.81 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 ------------------------------------------------------------------------ There are no maneuvers. Coasting Arc #1 (Orbit 820) --------------------------------------- Vector Time (GMT): 2009/182/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2065539.19 A = 6720761.87 meter Y = 3939609.98 meter E = .0014826 Z = -5048877.50 I = 51.35731 XDOT = -5557.731516 Wp = 109.03118 YDOT = -5047.406667 meter/sec RA = 232.51093 deg ZDOT = -1673.508725 TA = 144.84375 MA = 144.74584 Ha = 191.647 n.mi Hp = 182.666 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6776703.39 X = -2084912.46 Y = 12925229.59 feet Y = 3916404.36 meter Z = -16564558.73 Z = -5058958.38 XDOT = -18234.027282 XDOT = -5492.747866 YDOT = -16559.733158 feet/sec YDOT = -5109.192873 meter/sec ZDOT = -5490.514191 ZDOT = -1700.351193 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13803555.36 X = 4207323.67 Y = 4598150.29 feet Y = 1401516.21 meter Z = -16603877.51 Z = -5060861.86 XDOT = -13205.929689 XDOT = -4025.167369 YDOT = 19540.191309 feet/sec YDOT = 5955.850311 meter/sec ZDOT = -5596.056185 ZDOT = -1705.677925 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 09182.51880199 .00010596 00000-0 82463-4 0 9001 2 25544 51.6396 233.3229 0007827 173.9476 186.1783 15.74103705 8215 Satellite: ISS Catalog Number: 25544 Epoch time: 09182.51880199 = yrday.fracday Element set: 900 Inclination: 51.6396 deg RA of node: 233.3229 deg Eccentricity: .0007827 Arg of perigee: 173.9476 deg Mean anomaly: 186.1783 deg Mean motion: 15.74103705 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 821 Checksum: 326 Coasting Arc #2 (Orbit 836) --------------------------------------- Vector Time (GMT): 2009/183/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5210667.55 A = 6730882.05 meter Y = 4004725.39 meter E = .0019213 Z = 1399580.74 I = 51.41116 XDOT = -2010.116650 Wp = 139.05537 YDOT = 4655.298045 meter/sec RA = 227.32895 deg ZDOT = -5806.302317 TA = 25.48944 MA = 25.39482 Ha = 191.418 n.mi Hp = 182.829 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 17095365.97 X = 5158699.83 Y = 13138862.81 feet Y = 4062703.31 meter Z = 4591800.34 Z = 1424768.70 XDOT = -6594.870898 XDOT = -2033.817547 YDOT = 15273.287548 feet/sec YDOT = 4632.688219 meter/sec ZDOT = -19049.548284 ZDOT = -5816.124266 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 10010557.16 X = 3051217.82 Y = -19072256.48 feet Y = -5813223.77 meter Z = 4690806.16 Z = 1429757.72 XDOT = 14769.194673 XDOT = 4501.650536 YDOT = 3033.225115 feet/sec YDOT = 924.527015 meter/sec ZDOT = -19087.815856 ZDOT = -5817.966273 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 09183.53455379 .00010596 00000-0 82463-4 0 9013 2 25544 51.6397 228.1057 0007643 177.1499 182.9709 15.74144713 8377 Satellite: ISS Catalog Number: 25544 Epoch time: 09183.53455379 = yrday.fracday Element set: 901 Inclination: 51.6397 deg RA of node: 228.1057 deg Eccentricity: .0007643 Arg of perigee: 177.1499 deg Mean anomaly: 182.9709 deg Mean motion: 15.74144713 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 837 Checksum: 340 Coasting Arc #3 (Orbit 852) --------------------------------------- Vector Time (GMT): 2009/184/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1436047.93 A = 6720558.48 meter Y = -4165821.87 meter E = .0011262 Z = 5073454.29 I = 51.39643 XDOT = 6343.649874 Wp = 159.65439 YDOT = 4085.040393 meter/sec RA = 222.20264 deg ZDOT = 1547.218122 TA = 275.38620 MA = 275.51467 Ha = 191.401 n.mi Hp = 182.989 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 4711443.35 X = 1457878.19 Y = -13667394.59 feet Y = -4149642.03 meter Z = 16645191.23 Z = 5080482.86 XDOT = 20812.499587 XDOT = 6289.982672 YDOT = 13402.363493 feet/sec YDOT = 4155.678435 meter/sec ZDOT = 5076.174940 ZDOT = 1577.906010 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14292454.87 X = -4356340.25 Y = -1951961.36 feet Y = -594957.82 meter Z = 16672532.65 Z = 5081787.95 XDOT = 9096.356352 XDOT = 2772.569416 YDOT = -21896.634099 feet/sec YDOT = -6674.094073 meter/sec ZDOT = 5196.769200 ZDOT = 1583.975252 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 09184.55030636 .00010596 00000-0 82463-4 0 9022 2 25544 51.6389 222.8886 0007677 180.3851 179.7308 15.74131210 8539 Satellite: ISS Catalog Number: 25544 Epoch time: 09184.55030636 = yrday.fracday Element set: 902 Inclination: 51.6389 deg RA of node: 222.8886 deg Eccentricity: .0007677 Arg of perigee: 180.3851 deg Mean anomaly: 179.7308 deg Mean motion: 15.74131210 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 853 Checksum: 321 Coasting Arc #4 (Orbit 867) --------------------------------------- Vector Time (GMT): 2009/185/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5830485.37 A = 6731014.23 meter Y = -3107458.63 meter E = .0004880 Z = -1292841.83 I = 51.45519 XDOT = 1293.409790 Wp = 96.67092 YDOT = -4846.458788 meter/sec RA = 217.02526 deg ZDOT = 5834.112056 TA = 249.11556 MA = 249.16781 Ha = 191.286 n.mi Hp = 183.146 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19128889.00 X = -5789023.53 Y = -10195074.23 feet Y = -3172426.44 meter Z = -4241607.06 Z = -1321066.17 XDOT = 4243.470439 XDOT = 1319.166602 YDOT = -15900.455342 feet/sec YDOT = -4831.852265 meter/sec ZDOT = 19140.787586 ZDOT = 5840.457030 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6049160.67 X = -1843784.17 Y = 20792031.43 feet Y = 6337411.18 meter Z = -4352499.00 Z = -1326641.70 XDOT = -14893.829566 XDOT = -4539.639252 YDOT = -333.396091 feet/sec YDOT = -101.619129 meter/sec ZDOT = 19165.412375 ZDOT = 5841.617692 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 09185.50257442 .00010596 00000-0 82463-4 0 9035 2 25544 51.6393 217.9973 0007621 184.0064 176.1039 15.74136452 8683 Satellite: ISS Catalog Number: 25544 Epoch time: 09185.50257442 = yrday.fracday Element set: 903 Inclination: 51.6393 deg RA of node: 217.9973 deg Eccentricity: .0007621 Arg of perigee: 184.0064 deg Mean anomaly: 176.1039 deg Mean motion: 15.74136452 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 868 Checksum: 318 Coasting Arc #5 (Orbit 883) --------------------------------------- Vector Time (GMT): 2009/186/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -836277.55 A = 6720458.26 meter Y = 4285196.81 meter E = .0013574 Z = -5118887.64 I = 51.44383 XDOT = -6940.455480 Wp = 111.40931 YDOT = -3010.830525 meter/sec RA = 211.89943 deg ZDOT = -1394.436033 TA = 145.23220 MA = 145.14342 Ha = 191.168 n.mi Hp = 183.371 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -2743692.77 X = -859266.73 Y = 14059044.65 feet Y = 4275717.56 meter Z = -16794250.79 Z = -5123005.23 XDOT = -22770.523227 XDOT = -6899.498157 YDOT = -9878.052905 feet/sec YDOT = -3088.213471 meter/sec ZDOT = -4574.921368 ZDOT = -1428.053678 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14295111.74 X = 4357150.06 Y = -547216.54 feet Y = -166791.60 meter Z = -16810168.96 Z = -5123739.50 XDOT = -4611.906731 XDOT = -1405.709172 YDOT = 23328.543189 feet/sec YDOT = 7110.539964 meter/sec ZDOT = -4706.984011 ZDOT = -1434.688727 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 09186.51832632 .00010596 00000-0 82463-4 0 9048 2 25544 51.6393 212.7795 0007598 188.1265 171.9777 15.74111609 8846 Satellite: ISS Catalog Number: 25544 Epoch time: 09186.51832632 = yrday.fracday Element set: 904 Inclination: 51.6393 deg RA of node: 212.7795 deg Eccentricity: .0007598 Arg of perigee: 188.1265 deg Mean anomaly: 171.9777 deg Mean motion: 15.74111609 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 884 Checksum: 344 Coasting Arc #6 (Orbit 899) --------------------------------------- Vector Time (GMT): 2009/187/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6268711.38 A = 6731211.77 meter Y = 2127101.88 meter E = .0017997 Z = 1156236.83 I = 51.50483 XDOT = -586.739821 Wp = 145.20668 YDOT = 4944.187588 meter/sec RA = 206.72792 deg ZDOT = -5884.334564 TA = 22.09373 MA = 22.01626 Ha = 191.005 n.mi Hp = 183.514 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 20566638.39 X = 6238843.13 Y = 6978680.69 feet Y = 2197035.04 meter Z = 3793427.93 Z = 1186617.80 XDOT = -1924.999412 XDOT = -613.398228 YDOT = 16221.087888 feet/sec YDOT = 4937.478427 meter/sec ZDOT = -19305.559593 ZDOT = -5887.248694 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 1862854.84 X = 567798.16 Y = -21617094.46 feet Y = -6588890.39 meter Z = 3912760.29 Z = 1192609.34 XDOT = 14607.208787 XDOT = 4452.277238 YDOT = -2255.037306 feet/sec YDOT = -687.335371 meter/sec ZDOT = -19316.717977 ZDOT = -5887.735640 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 09187.53407813 .00010596 00000-0 82463-4 0 9051 2 25544 51.6379 207.5619 0007490 191.0279 169.0721 15.74123877 9002 Satellite: ISS Catalog Number: 25544 Epoch time: 09187.53407813 = yrday.fracday Element set: 905 Inclination: 51.6379 deg RA of node: 207.5619 deg Eccentricity: .0007490 Arg of perigee: 191.0279 deg Mean anomaly: 169.0721 deg Mean motion: 15.74123877 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 900 Checksum: 323 Coasting Arc #7 (Orbit 915) --------------------------------------- Vector Time (GMT): 2009/188/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 187483.00 A = 6720320.16 meter Y = -4324803.38 meter E = .0009754 Z = 5140868.97 I = 51.49453 XDOT = 7371.150935 Wp = 171.06673 YDOT = 1835.822450 meter/sec RA = 201.60339 deg ZDOT = 1265.778161 TA = 266.75295 MA = 266.86455 Ha = 190.917 n.mi Hp = 183.728 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 615101.72 X = 210856.69 Y = -14188987.46 feet Y = -4322577.11 meter Z = 16866368.00 Z = 5141835.71 XDOT = 24183.566061 XDOT = 7343.925781 YDOT = 6023.039534 feet/sec YDOT = 1918.098509 meter/sec ZDOT = 4152.815490 ZDOT = 1301.520942 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13848795.11 X = -4221112.75 Y = 3129995.87 feet Y = 954022.74 meter Z = 16869916.56 Z = 5141950.57 XDOT = -129.612819 XDOT = -39.505987 YDOT = -23886.077334 feet/sec YDOT = -7280.476372 meter/sec ZDOT = 4293.191179 ZDOT = 1308.564671 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 09188.54982962 .00010596 00000-0 82463-4 0 9067 2 25544 51.6372 202.3439 0007412 195.1590 164.9352 15.74122066 9163 Satellite: ISS Catalog Number: 25544 Epoch time: 09188.54982962 = yrday.fracday Element set: 906 Inclination: 51.6372 deg RA of node: 202.3439 deg Eccentricity: .0007412 Arg of perigee: 195.1590 deg Mean anomaly: 164.9352 deg Mean motion: 15.74122066 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 916 Checksum: 320 Coasting Arc #8 (Orbit 930) --------------------------------------- Vector Time (GMT): 2009/189/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6562815.06 A = 6731169.51 meter Y = -1070763.73 meter E = .0003535 Z = -1045943.87 I = 51.56054 XDOT = -134.631578 Wp = 82.93198 YDOT = -4928.740707 meter/sec RA = 196.43840 deg ZDOT = 5907.906198 TA = 265.62579 MA = 265.66619 Ha = 190.736 n.mi Hp = 183.810 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -21531545.48 X = -6545272.91 Y = -3513004.37 feet Y = -1144054.70 meter Z = -3431574.37 Z = -1077783.09 XDOT = -441.704652 XDOT = -108.206627 YDOT = -16170.409144 feet/sec YDOT = -4930.099510 meter/sec ZDOT = 19382.894352 ZDOT = 5907.315500 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 2479856.93 X = 755860.39 Y = 21654681.50 feet Y = 6600346.92 meter Z = -3556603.96 Z = -1084052.89 XDOT = -13828.387552 XDOT = -4214.892526 YDOT = 4757.581051 feet/sec YDOT = 1450.110704 meter/sec ZDOT = 19380.291425 ZDOT = 5907.112826 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 09189.50209644 .00010596 00000-0 82463-4 0 9074 2 25544 51.6378 197.4531 0007507 198.6194 161.4696 15.74171424 9311 Satellite: ISS Catalog Number: 25544 Epoch time: 09189.50209644 = yrday.fracday Element set: 907 Inclination: 51.6378 deg RA of node: 197.4531 deg Eccentricity: .0007507 Arg of perigee: 198.6194 deg Mean anomaly: 161.4696 deg Mean motion: 15.74171424 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 931 Checksum: 335 Coasting Arc #9 (Orbit 946) --------------------------------------- Vector Time (GMT): 2009/190/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 409758.41 A = 6720222.22 meter Y = 4274739.17 meter E = .0012104 Z = -5178020.45 I = 51.55107 XDOT = -7587.570959 Wp = 112.27098 YDOT = -615.370047 meter/sec RA = 191.31518 deg ZDOT = -1115.035849 TA = 147.10239 MA = 147.02699 Ha = 190.595 n.mi Hp = 184.184 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 1344351.74 X = 387080.55 Y = 14024734.79 feet Y = 4279195.33 meter Z = -16988256.08 Z = -5176084.30 XDOT = -24893.605510 XDOT = -7574.709314 YDOT = -2018.930601 feet/sec YDOT = -700.146619 meter/sec ZDOT = -3658.254097 ZDOT = -1151.864500 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13009350.45 X = 3965250.02 Y = -5433595.45 feet Y = -1656159.89 meter Z = -16980404.99 Z = -5175627.44 XDOT = 4857.102958 XDOT = 1480.444982 YDOT = 23445.836952 feet/sec YDOT = 7146.291103 meter/sec ZDOT = -3802.857930 ZDOT = -1159.111097 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 09190.51784799 .00010596 00000-0 82463-4 0 9087 2 25544 51.6370 192.2347 0007342 203.7648 156.3177 15.74111910 9478 Satellite: ISS Catalog Number: 25544 Epoch time: 09190.51784799 = yrday.fracday Element set: 908 Inclination: 51.6370 deg RA of node: 192.2347 deg Eccentricity: .0007342 Arg of perigee: 203.7648 deg Mean anomaly: 156.3177 deg Mean motion: 15.74111910 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 947 Checksum: 325 Coasting Arc #10 (Orbit 962) --------------------------------------- Vector Time (GMT): 2009/191/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6658745.52 A = 6731414.91 meter Y = -9307.17 meter E = .0016217 Z = 913175.88 I = 51.61828 XDOT = 826.700021 Wp = 151.26652 YDOT = 4828.867975 meter/sec RA = 186.15591 deg ZDOT = -5949.433398 TA = 18.75232 MA = 18.69265 Ha = 190.356 n.mi Hp = 184.329 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21846277.97 X = 6653918.74 Y = -30535.35 feet Y = 65127.70 meter Z = 2995983.84 Z = 945511.81 XDOT = 2712.270409 XDOT = 801.542149 YDOT = 15842.742700 feet/sec YDOT = 4837.972752 meter/sec ZDOT = -19519.138446 ZDOT = -5945.477814 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6694438.75 X = -2040464.93 Y = -20776634.04 feet Y = -6332718.05 meter Z = 3122928.21 Z = 951868.52 XDOT = 12707.857222 XDOT = 3873.354881 YDOT = -7040.104332 feet/sec YDOT = -2145.823800 meter/sec ZDOT = -19503.321590 ZDOT = -5944.612421 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 09191.53359957 .00010596 00000-0 82463-4 0 9095 2 25544 51.6367 187.0167 0007172 207.8234 152.2546 15.74131149 9632 Satellite: ISS Catalog Number: 25544 Epoch time: 09191.53359957 = yrday.fracday Element set: 909 Inclination: 51.6367 deg RA of node: 187.0167 deg Eccentricity: .0007172 Arg of perigee: 207.8234 deg Mean anomaly: 152.2546 deg Mean motion: 15.74131149 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 963 Checksum: 327 Coasting Arc #11 (Orbit 978) --------------------------------------- Vector Time (GMT): 2009/192/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1027712.97 A = 6720133.86 meter Y = -4136960.50 meter E = .0008106 Z = 5197020.78 I = 51.60941 XDOT = 7609.525550 Wp = 186.02112 YDOT = -643.118224 meter/sec RA = 181.03519 deg ZDOT = 985.066591 TA = 254.54019 MA = 254.62973 Ha = 190.286 n.mi Hp = 184.609 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3371761.72 X = -1006622.22 Y = -13572705.05 feet Y = -4148335.66 meter Z = 17050593.11 Z = 5192078.97 XDOT = 24965.635008 XDOT = 7611.366245 YDOT = -2109.967927 feet/sec YDOT = -558.013877 meter/sec ZDOT = 3231.845770 ZDOT = 1022.037539 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -11734449.55 X = -3576660.22 Y = 7652422.15 feet Y = 2332458.27 meter Z = 17030941.07 Z = 5191030.84 XDOT = -9464.711320 XDOT = -2884.844010 YDOT = -22085.989630 feet/sec YDOT = -6731.809639 meter/sec ZDOT = 3376.961131 ZDOT = 1029.297753 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 09192.54935142 .00010596 00000-0 82463-4 0 9105 2 25544 51.6364 181.7989 0007190 212.7050 147.3669 15.74111287 9792 Satellite: ISS Catalog Number: 25544 Epoch time: 09192.54935142 = yrday.fracday Element set: 910 Inclination: 51.6364 deg RA of node: 181.7989 deg Eccentricity: .0007190 Arg of perigee: 212.7050 deg Mean anomaly: 147.3669 deg Mean motion: 15.74111287 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 979 Checksum: 327 Coasting Arc #12 (Orbit 993) --------------------------------------- Vector Time (GMT): 2009/193/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6589881.67 A = 6731424.64 meter Y = 1108738.28 meter E = .0003142 Z = -800595.21 I = 51.67792 XDOT = -1500.608415 Wp = 48.82684 YDOT = -4621.614708 meter/sec RA = 175.88305 deg ZDOT = 5968.561876 TA = 302.45215 MA = 302.48253 Ha = 190.093 n.mi Hp = 184.665 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -21620346.70 X = -6597900.89 Y = 3637592.78 feet Y = 1035001.61 meter Z = -2626624.71 Z = -832627.88 XDOT = -4923.255956 XDOT = -1477.811080 YDOT = -15162.777913 feet/sec YDOT = -4638.268530 meter/sec ZDOT = 19581.895917 ZDOT = 5961.326903 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 10724389.40 X = 3268793.89 Y = 19104522.11 feet Y = 5823058.34 meter Z = -2752332.99 Z = -838911.10 XDOT = -11175.192522 XDOT = -3406.198681 YDOT = 9082.470073 feet/sec YDOT = 2768.336878 meter/sec ZDOT = 19553.206903 ZDOT = 5959.817464 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 09193.50161815 .00010596 00000-0 82463-4 0 9111 2 25544 51.6365 176.9079 0007207 214.9860 145.0830 15.74154175 9946 Satellite: ISS Catalog Number: 25544 Epoch time: 09193.50161815 = yrday.fracday Element set: 911 Inclination: 51.6365 deg RA of node: 176.9079 deg Eccentricity: .0007207 Arg of perigee: 214.9860 deg Mean anomaly: 145.0830 deg Mean motion: 15.74154175 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 994 Checksum: 317 Coasting Arc #13 (Orbit 1009) --------------------------------------- Vector Time (GMT): 2009/194/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1581524.73 A = 6720036.03 meter Y = 3928665.76 meter E = .0010595 Z = -5225641.49 I = 51.66886 XDOT = -7414.828566 Wp = 110.58845 YDOT = 1876.996095 meter/sec RA = 170.76360 deg ZDOT = -837.957795 TA = 151.46043 MA = 151.40238 Ha = 189.919 n.mi Hp = 185.040 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5188729.44 X = 1562861.23 Y = 12889323.34 feet Y = 3946247.44 meter Z = -17144493.09 Z = -5218003.45 XDOT = -24326.865374 XDOT = -7431.195750 YDOT = 6158.123670 feet/sec YDOT = 1793.987707 meter/sec ZDOT = -2749.205364 ZDOT = -874.018365 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 10181656.65 X = 3103368.95 Y = -9509318.84 feet Y = -2898440.38 meter Z = -17114261.18 Z = -5216426.81 XDOT = 13673.265110 XDOT = 4167.611205 YDOT = 19812.807606 feet/sec YDOT = 6038.943758 meter/sec ZDOT = -2890.692771 ZDOT = -881.083157 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 09194.51736999 .00010596 00000-0 82463-4 0 9125 2 25544 51.6367 171.6895 0007086 220.5975 139.4661 15.74111658 10109 Satellite: ISS Catalog Number: 25544 Epoch time: 09194.51736999 = yrday.fracday Element set: 912 Inclination: 51.6367 deg RA of node: 171.6895 deg Eccentricity: .0007086 Arg of perigee: 220.5975 deg Mean anomaly: 139.4661 deg Mean motion: 15.74111658 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 1010 Checksum: 334 Coasting Arc #14 (Orbit 1025) --------------------------------------- Vector Time (GMT): 2009/195/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6327110.85 A = 6731590.53 meter Y = -2169439.55 meter E = .0014222 Z = 671851.30 I = 51.73758 XDOT = 2128.435609 Wp = 157.18579 YDOT = 4340.085296 meter/sec RA = 165.61793 deg ZDOT = -6000.783035 TA = 15.50142 MA = 15.45791 Ha = 189.643 n.mi Hp = 185.188 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 20758237.71 X = 6347635.93 Y = -7117583.83 feet Y = -2098571.40 meter Z = 2204236.54 Z = 702637.96 XDOT = 6983.056459 XDOT = 2108.896482 YDOT = 14239.124988 feet/sec YDOT = 4363.778060 meter/sec ZDOT = -19687.608382 ZDOT = -5990.490149 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14289925.77 X = -4355569.37 Y = -16637772.02 feet Y = -5071192.91 meter Z = 2325006.40 Z = 708661.95 XDOT = 9387.698514 XDOT = 2861.370507 YDOT = -10821.182993 feet/sec YDOT = -3298.296576 meter/sec ZDOT = -19646.924933 ZDOT = -5988.382720 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 09195.53312128 .00010596 00000-0 82463-4 0 9133 2 25544 51.6369 166.4721 0007015 225.8534 134.2053 15.74130746 10266 Satellite: ISS Catalog Number: 25544 Epoch time: 09195.53312128 = yrday.fracday Element set: 913 Inclination: 51.6369 deg RA of node: 166.4721 deg Eccentricity: .0007015 Arg of perigee: 225.8534 deg Mean anomaly: 134.2053 deg Mean motion: 15.74130746 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 1026 Checksum: 289 Coasting Arc #15 (Orbit 1041) --------------------------------------- Vector Time (GMT): 2009/196/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 672678.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2124545.35 A = 6719932.26 meter Y = -3634288.70 meter E = .0006583 Z = 5240837.64 I = 51.72673 XDOT = 7021.694281 Wp = 204.30026 YDOT = -3077.730742 meter/sec RA = 160.50167 deg ZDOT = 706.632900 TA = 238.95365 MA = 239.01829 Ha = 189.548 n.mi Hp = 185.424 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6970293.14 X = -2109207.26 Y = -11923519.34 feet Y = -3657961.43 meter Z = 17194349.20 Z = 5230553.44 XDOT = 23037.054729 XDOT = 7052.155426 YDOT = -10097.541803 feet/sec YDOT = -2999.039807 meter/sec ZDOT = 2318.349408 ZDOT = 740.817954 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8269754.32 X = -2520621.12 Y = 11124802.88 feet Y = 3390839.92 meter Z = 17153742.12 Z = 5228460.60 XDOT = -17391.155308 XDOT = -5300.824138 YDOT = -16737.653461 feet/sec YDOT = -5101.636775 meter/sec ZDOT = 2452.423110 ZDOT = 747.498564 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 09196.54887292 .00010596 00000-0 82463-4 0 9145 2 25544 51.6369 161.2551 0007056 230.2861 129.7681 15.74123426 10429 Satellite: ISS Catalog Number: 25544 Epoch time: 09196.54887292 = yrday.fracday Element set: 914 Inclination: 51.6369 deg RA of node: 161.2551 deg Eccentricity: .0007056 Arg of perigee: 230.2861 deg Mean anomaly: 129.7681 deg Mean motion: 15.74123426 rev/day Decay rate: 1.05960E-04 rev/day^2 Epoch rev: 1042 Checksum: 314