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Date:
July 29th 2010
<B> ISS TRAJECTORY DATA</B>
Lift off time (UTC) : N/A
Area (sq ft) : 8880.23
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 2996)
Vector Time (GMT): 2010/209/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6516113.77 A = 6739113.74 meter
Y = 1075697.33 meter E = .0008112
Z = -1348545.43 I = 51.76930
XDOT = 379.902553 Wp = 90.86388
YDOT = 4984.838824 meter/sec RA = 18.63083 deg
ZDOT = 5841.971976 TA = 254.38104
MA = 254.47058
Ha = 196.328 n.mi
Hp = 186.522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21378326.01 X = 6510151.69
Y = 3529190.72 feet Y = 1148531.16 meter
Z = -4424361.65 Z = -1316905.21
XDOT = 1246.399451 XDOT = 295.754282
YDOT = 16354.458084 feet/sec YDOT = 4988.616247 meter/sec
ZDOT = 19166.574723 ZDOT = 5843.613434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9477785.26 X = -2888828.95
Y = -19513152.93 feet Y = -5947609.01 meter
Z = -4297840.79 Z = -1309981.87
XDOT = 11276.028065 XDOT = 3436.933354
YDOT = -9677.510145 feet/sec YDOT = -2949.705092 meter/sec
ZDOT = 19173.089367 ZDOT = 5843.957639
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 10209.50254265 .00016717 00000-0 10270-3 0 9008
2 25544 51.6420 19.1528 0007751 159.6876 200.4595 15.71301570 29970
Satellite: ISS
Catalog Number: 25544
Epoch time: 10209.50254265 = yrday.fracday
Element set: 900
Inclination: 51.6420 deg
RA of node: 19.1528 deg
Eccentricity: .0007751
Arg of perigee: 159.6876 deg
Mean anomaly: 200.4595 deg
Mean motion: 15.71301570 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 302
Coasting Arc #2 (Orbit 3012)
Vector Time (GMT): 2010/210/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1774311.45 A = 6729662.15 meter
Y = -4349633.23 meter E = .0014282
Z = -4829241.59 I = 51.70945
XDOT = 7278.280118 Wp = 104.82108
YDOT = -245.294757 meter/sec RA = 13.55506 deg
ZDOT = -2462.799354 TA = 141.14064
MA = 141.03787
Ha = 196.197 n.mi
Hp = 186.505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5821231.80 X = -1702082.01
Y = -14270450.24 feet Y = -4369070.55 meter
Z = -15843968.46 Z = -4837685.82
XDOT = 23878.871778 XDOT = 7292.445737
YDOT = -804.772825 feet/sec YDOT = -163.825349 meter/sec
ZDOT = -8080.050375 ZDOT = -2427.407688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8121069.96 X = -2475302.12
Y = 13057981.64 feet Y = 3980072.80 meter
Z = -15877693.94 Z = -4839521.11
XDOT = -13846.353559 XDOT = -4220.368565
YDOT = -18225.826072 feet/sec YDOT = -5555.231787 meter/sec
ZDOT = -7938.519472 ZDOT = -2419.660735
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 10210.52011815 .00016717 00000-0 10270-3 0 9015
2 25544 51.6427 13.9486 0007709 162.3543 197.7888 15.71326345 30137
Satellite: ISS
Catalog Number: 25544
Epoch time: 10210.52011815 = yrday.fracday
Element set: 901
Inclination: 51.6427 deg
RA of node: 13.9486 deg
Eccentricity: .0007709
Arg of perigee: 162.3543 deg
Mean anomaly: 197.7888 deg
Mean motion: 15.71326345 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 296
Coasting Arc #3 (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 = -5881744.62 A = 6736240.36 meter
Y = 1459490.95 meter E = .0017719
Z = 2916437.15 I = 51.70098
XDOT = -3635.167120 Wp = 121.99076
YDOT = -4558.045636 meter/sec RA = 8.40128 deg
ZDOT = -5037.219711 TA = 24.46598
MA = 24.38199
Ha = 196.200 n.mi
Hp = 186.794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19297062.39 X = -5911795.10
Y = 4788356.13 feet Y = 1393549.62 meter
Z = 9568363.34 Z = 2887791.09
XDOT = -11926.401311 XDOT = -3559.458478
YDOT = -14954.217967 feet/sec YDOT = -4598.272726 meter/sec
ZDOT = -16526.311388 ZDOT = -5054.695412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15524118.05 X = 4731751.18
Y = 12509434.54 feet Y = 3812875.65 meter
Z = 9453801.07 Z = 2881518.56
XDOT = -3835.340678 XDOT = -1169.011839
YDOT = 17334.564542 feet/sec YDOT = 5283.575272 meter/sec
ZDOT = -16596.148045 ZDOT = -5058.505924
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 10211.53768462 .00016717 00000-0 10270-3 0 9025
2 25544 51.6422 8.7430 0007710 167.4197 192.7159 15.71310320 30295
Satellite: ISS
Catalog Number: 25544
Epoch time: 10211.53768462 = yrday.fracday
Element set: 902
Inclination: 51.6422 deg
RA of node: 8.7430 deg
Eccentricity: .0007710
Arg of perigee: 167.4197 deg
Mean anomaly: 192.7159 deg
Mean motion: 15.71310320 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3029
Checksum: 284
Coasting Arc #4 (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 = 4419500.56 A = 6733190.74 meter
Y = 3308687.31 meter E = .0015535
Z = 3851289.51 I = 51.66224
XDOT = -5802.149592 Wp = 127.10210
YDOT = 2927.361394 meter/sec RA = 3.33869 deg
ZDOT = 4122.665932 TA = 279.73611
MA = 279.91153
Ha = 195.907 n.mi
Hp = 186.827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14499673.74 X = 4363465.06
Y = 10855273.34 feet Y = 3357795.34 meter
Z = 12635464.26 Z = 3872623.26
XDOT = -19035.923857 XDOT = -5854.479622
YDOT = 9604.204047 feet/sec YDOT = 2862.185523 meter/sec
ZDOT = 13525.806862 ZDOT = 4094.352376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -397417.09 X = -121132.73
Y = -18048750.29 feet Y = -5501259.09 meter
Z = 12720736.13 Z = 3877280.37
XDOT = 18057.107948 XDOT = 5503.806503
YDOT = 9102.850259 feet/sec YDOT = 2774.548759 meter/sec
ZDOT = 13412.564880 ZDOT = 4088.149775
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 10212.55524169 .00016717 00000-0 10270-3 0 9033
2 25544 51.6430 3.5383 0007738 171.3522 188.7775 15.71359169 30451
Satellite: ISS
Catalog Number: 25544
Epoch time: 10212.55524169 = yrday.fracday
Element set: 903
Inclination: 51.6430 deg
RA of node: 3.5383 deg
Eccentricity: .0007738
Arg of perigee: 171.3522 deg
Mean anomaly: 188.7775 deg
Mean motion: 15.71359169 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3045
Checksum: 308
Coasting Arc #5 (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 = 4010554.86 A = 6732257.00 meter
Y = -3442258.01 meter E = .0013189
Z = -4184015.30 I = 51.62949
XDOT = 6175.097768 Wp = 141.00469
YDOT = 2717.752384 meter/sec RA = 358.17383 deg
ZDOT = 3679.377107 TA = 166.65207
MA = 166.61715
Ha = 195.878 n.mi
Hp = 187.094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13157988.39 X = 4069073.80
Y = -11293497.41 feet Y = -3397082.19 meter
Z = -13727084.32 Z = -4164390.17
XDOT = 20259.507112 XDOT = 6126.374782
YDOT = 8916.510446 feet/sec YDOT = 2786.533419 meter/sec
ZDOT = 12071.447202 ZDOT = 3709.257324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17120247.58 X = -5218251.46
Y = -3118003.69 feet Y = -950367.52 meter
Z = -13648580.95 Z = -4160087.47
XDOT = -6080.709696 XDOT = -1853.400315
YDOT = -20030.485295 feet/sec YDOT = -6105.291918 meter/sec
ZDOT = 12190.892595 ZDOT = 3715.784063
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 10213.50919489 .00016717 00000-0 10270-3 0 9043
2 25544 51.6441 358.6595 0007670 174.1104 186.0150 15.71346623 30600
Satellite: ISS
Catalog Number: 25544
Epoch time: 10213.50919489 = yrday.fracday
Element set: 904
Inclination: 51.6441 deg
RA of node: 358.6595 deg
Eccentricity: .0007670
Arg of perigee: 174.1104 deg
Mean anomaly: 186.0150 deg
Mean motion: 15.71346623 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3060
Checksum: 297
Coasting Arc #6 (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 = -6114171.14 A = 6736845.84 meter
Y = -1267695.63 meter E = .0011658
Z = -2515463.39 I = 51.61507
XDOT = 3132.189428 Wp = 157.99540
YDOT = -4613.299231 meter/sec RA = 353.10384 deg
ZDOT = -5306.794511 TA = 50.47485
MA = 50.37187
Ha = 195.629 n.mi
Hp = 187.123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20059616.60 X = -6087321.50
Y = -4159106.41 feet Y = -1335917.68 meter
Z = -8252832.65 Z = -2545100.77
XDOT = 10276.212035 XDOT = 3209.322730
YDOT = -15135.496166 feet/sec YDOT = -4577.841622 meter/sec
ZDOT = -17410.743147 ZDOT = -5291.391319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9738019.52 X = 2968148.35
Y = 17969074.85 feet Y = 5476974.01 meter
Z = -8371317.45 Z = -2551577.56
XDOT = -16949.907476 XDOT = -5166.331799
YDOT = 1131.101307 feet/sec YDOT = 344.759678 meter/sec
ZDOT = -17349.109246 ZDOT = -5288.008498
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 10214.52673505 .00016717 00000-0 10270-3 0 9053
2 25544 51.6439 353.4544 0007593 178.1416 181.9766 15.71369601 30763
Satellite: ISS
Catalog Number: 25544
Epoch time: 10214.52673505 = yrday.fracday
Element set: 905
Inclination: 51.6439 deg
RA of node: 353.4544 deg
Eccentricity: .0007593
Arg of perigee: 178.1416 deg
Mean anomaly: 181.9766 deg
Mean motion: 15.71369601 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 320
Coasting Arc #7 (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 = -1322709.43 A = 6729012.82 meter
Y = 4323254.72 meter E = .0006416
Z = 4978522.94 I = 51.55880
XDOT = -7444.497362 Wp = 131.13838
YDOT = -10.479641 meter/sec RA = 347.94741 deg
ZDOT = -1971.283858 TA = 337.92325
MA = 337.95087
Ha = 195.679 n.mi
Hp = 187.339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4339597.86 X = -1395139.22
Y = 14183906.55 feet Y = 4308058.03 meter
Z = 16333736.67 Z = 4971921.64
XDOT = -24424.203942 XDOT = -7434.250777
YDOT = -34.382024 feet/sec YDOT = -93.671020 meter/sec
ZDOT = -6467.466727 ZDOT = -2007.424212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13596498.05 X = 4144212.61
Y = -6001131.00 feet Y = -1829144.73 meter
Z = 16307297.02 Z = 4970464.13
XDOT = 15593.251658 XDOT = 4752.823105
YDOT = 17384.177102 feet/sec YDOT = 5298.697181 meter/sec
ZDOT = -6611.962626 ZDOT = -2015.326208
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 10215.54426839 .00016717 00000-0 10270-3 0 9063
2 25544 51.6444 348.2500 0007585 181.1250 178.9896 15.71343549 30925
Satellite: ISS
Catalog Number: 25544
Epoch time: 10215.54426839 = yrday.fracday
Element set: 906
Inclination: 51.6444 deg
RA of node: 348.2500 deg
Eccentricity: .0007585
Arg of perigee: 181.1250 deg
Mean anomaly: 178.9896 deg
Mean motion: 15.71343549 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3092
Checksum: 322
Coasting Arc #8 (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 = 6554450.82 A = 6739193.01 meter
Y = -1276112.99 meter E = .0010474
Z = 898718.08 I = 51.56537
XDOT = 129.990087 Wp = 87.88706
YDOT = 4890.130543 meter/sec RA = 342.85144 deg
ZDOT = 5936.504210 TA = 281.91723
MA = 282.03464
Ha = 195.430 n.mi
Hp = 187.413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21504103.73 X = 6563867.62
Y = -4186722.40 feet Y = -1202764.63 meter
Z = 2948550.15 Z = 930582.21
XDOT = 426.476662 XDOT = 46.459769
YDOT = 16043.735376 feet/sec YDOT = 4891.116576 meter/sec
ZDOT = 19476.719850 ZDOT = 5936.933259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17526971.96 X = -5342221.05
Y = -13114601.60 feet Y = -3997330.57 meter
Z = 3075963.04 Z = 937553.54
XDOT = 10726.507000 XDOT = 3269.439334
YDOT = -9723.270816 feet/sec YDOT = -2963.652945 meter/sec
ZDOT = 19478.381513 ZDOT = 5937.010685
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 10216.56178918 .00016717 00000-0 10270-3 0 9079
2 25544 51.6453 343.0452 0007540 185.6751 174.4326 15.71404114 31083
Satellite: ISS
Catalog Number: 25544
Epoch time: 10216.56178918 = yrday.fracday
Element set: 907
Inclination: 51.6453 deg
RA of node: 343.0452 deg
Eccentricity: .0007540
Arg of perigee: 185.6751 deg
Mean anomaly: 174.4326 deg
Mean motion: 15.71404114 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 296
Coasting Arc #9 (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 = -1496796.08 A = 6727457.31 meter
Y = -3918621.57 meter E = .0015736
Z = -5271540.75 I = 51.49749
XDOT = 7137.823361 Wp = 118.29976
YDOT = -2851.102041 meter/sec RA = 337.71922 deg
ZDOT = 85.537640 TA = 152.55661
MA = 152.47341
Ha = 195.219 n.mi
Hp = 187.552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4910748.30 X = -1427258.10
Y = -12856369.98 feet Y = -3934970.27 meter
Z = -17295081.20 Z = -5278643.64
XDOT = 23418.055646 XDOT = 7168.758882
YDOT = -9354.009320 feet/sec YDOT = -2771.109672 meter/sec
ZDOT = 280.635302 ZDOT = 120.287756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6090738.55 X = -1856457.11
Y = 12301339.34 feet Y = 3749448.23 meter
Z = -17323437.47 Z = -5280183.74
XDOT = -21942.487771 XDOT = -6688.070273
YDOT = -10240.519835 feet/sec YDOT = -3121.310446 meter/sec
ZDOT = 419.606633 ZDOT = 127.896102
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 10217.51570882 .00016717 00000-0 10270-3 0 9082
2 25544 51.6454 338.1665 0007393 189.5722 170.5300 15.71425065 31236
Satellite: ISS
Catalog Number: 25544
Epoch time: 10217.51570882 = yrday.fracday
Element set: 908
Inclination: 51.6454 deg
RA of node: 338.1665 deg
Eccentricity: .0007393
Arg of perigee: 189.5722 deg
Mean anomaly: 170.5300 deg
Mean motion: 15.71425065 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 302
Coasting Arc #10 (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 = -5634666.80 A = 6739330.60 meter
Y = 3598580.54 meter E = .0017768
Z = 754981.09 I = 51.50999
XDOT = -3169.172308 Wp = 149.53391
YDOT = -3700.840956 meter/sec RA = 332.58728 deg
ZDOT = -5966.615392 TA = 22.22373
MA = 22.14681
Ha = 195.121 n.mi
Hp = 187.839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18486439.62 X = -5678155.52
Y = 11806366.61 feet Y = 3535327.09 meter
Z = 2476972.09 Z = 727502.99
XDOT = -10397.546942 XDOT = -3098.568909
YDOT = -12141.866655 feet/sec YDOT = -3735.885099 meter/sec
ZDOT = -19575.509815 ZDOT = -5981.839966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21356937.60 X = 6509594.58
Y = 5054933.03 feet Y = 1540743.59 meter
Z = 2367065.97 Z = 721481.71
XDOT = -1185.350720 XDOT = -361.294899
YDOT = 14277.199512 feet/sec YDOT = 4351.690411 meter/sec
ZDOT = -19636.344463 ZDOT = -5985.157792
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 10218.53321460 .00016717 00000-0 10270-3 0 9092
2 25544 51.6456 332.9611 0007446 193.6726 166.4235 15.71412878 31396
Satellite: ISS
Catalog Number: 25544
Epoch time: 10218.53321460 = yrday.fracday
Element set: 909
Inclination: 51.6456 deg
RA of node: 332.9611 deg
Eccentricity: .0007446
Arg of perigee: 193.6726 deg
Mean anomaly: 166.4235 deg
Mean motion: 15.71412878 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 312
Coasting Arc #11 (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 = 3852425.73 A = 6728364.79 meter
Y = 2288407.10 meter E = .0010291
Z = 5020088.82 I = 51.44828
XDOT = -5421.943077 Wp = 167.77085
YDOT = 5157.095545 meter/sec RA = 327.48205 deg
ZDOT = 1799.375050 TA = 264.77519
MA = 264.89263
Ha = 194.794 n.mi
Hp = 187.945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12639192.01 X = 3802163.77
Y = 7507897.32 feet Y = 2331205.67 meter
Z = 16470107.69 Z = 5038681.74
XDOT = -17788.527156 XDOT = -5487.948576
YDOT = 16919.604806 feet/sec YDOT = 5096.094888 meter/sec
ZDOT = 5903.461449 ZDOT = 1772.875937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3589803.16 X = -1094172.00
Y = -14169590.19 feet Y = -4318891.09 meter
Z = 16544430.22 Z = 5042742.33
XDOT = 23535.064409 XDOT = 7173.487632
YDOT = 846.928604 feet/sec YDOT = 258.143838 meter/sec
ZDOT = 5797.453857 ZDOT = 1767.063936
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 10219.55070986 .00016717 00000-0 10270-3 0 9101
2 25544 51.6465 327.7563 0007346 198.1419 161.9482 15.71467617 31555
Satellite: ISS
Catalog Number: 25544
Epoch time: 10219.55070986 = yrday.fracday
Element set: 910
Inclination: 51.6465 deg
RA of node: 327.7563 deg
Eccentricity: .0007346
Arg of perigee: 198.1419 deg
Mean anomaly: 161.9482 deg
Mean motion: 15.71467617 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 330
Coasting Arc #12 (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 = 3639647.56 A = 6737196.89 meter
Y = -5166686.31 meter E = .0002833
Z = -2339622.53 I = 51.45268
XDOT = 5326.149311 Wp = 150.86546
YDOT = 1311.796888 meter/sec RA = 322.31817 deg
ZDOT = 5389.064192 TA = 182.78157
MA = 182.78315
Ha = 194.744 n.mi
Hp = 188.283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11941100.90 X = 3708517.09
Y = -16951070.57 feet Y = -5125600.32 meter
Z = -7675926.94 Z = -2321774.69
XDOT = 17474.243146 XDOT = 5284.906197
YDOT = 4303.795564 feet/sec YDOT = 1371.126005 meter/sec
ZDOT = 17680.656799 ZDOT = 5414.837984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20390127.25 X = -6214910.79
Y = 3906734.97 feet Y = 1190772.82 meter
Z = -7604516.49 Z = -2317856.63
XDOT = -9248.690870 XDOT = -2819.000977
YDOT = -13656.713544 feet/sec YDOT = -4162.566288 meter/sec
ZDOT = 17783.707220 ZDOT = 5420.473961
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 10220.50460613 .00016717 00000-0 10270-3 0 9119
2 25544 51.6466 322.8773 0007135 202.3950 157.6901 15.71419937 31706
Satellite: ISS
Catalog Number: 25544
Epoch time: 10220.50460613 = yrday.fracday
Element set: 911
Inclination: 51.6466 deg
RA of node: 322.8773 deg
Eccentricity: .0007135
Arg of perigee: 202.3950 deg
Mean anomaly: 157.6901 deg
Mean motion: 15.71419937 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 289
Coasting Arc #13 (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 = -5178556.93 A = 6731316.08 meter
Y = 114342.49 meter E = .0006174
Z = -4301250.23 I = 51.41004
XDOT = 2735.329701 Wp = 123.11274
YDOT = -6299.404364 meter/sec RA = 317.23280 deg
ZDOT = -3467.612429 TA = 111.70513
MA = 111.63939
Ha = 194.517 n.mi
Hp = 188.270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16990016.16 X = -5158556.47
Y = 375139.40 feet Y = 56544.84 meter
Z = -14111713.37 Z = -4326358.45
XDOT = 8974.178808 XDOT = 2822.412108
YDOT = -20667.337152 feet/sec YDOT = -6268.329171 meter/sec
ZDOT = -11376.681196 ZDOT = -3454.113368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12638795.32 X = 3852304.81
Y = 11234697.99 feet Y = 3424335.95 meter
Z = -14212116.20 Z = -4331853.02
XDOT = -19873.487666 XDOT = -6057.439041
YDOT = 8062.331633 feet/sec YDOT = 2457.398682 meter/sec
ZDOT = -11322.660776 ZDOT = -3451.147004
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 10221.52208609 .00016717 00000-0 10270-3 0 9128
2 25544 51.6465 317.6729 0007254 205.8198 154.2602 15.71447118 31862
Satellite: ISS
Catalog Number: 25544
Epoch time: 10221.52208609 = yrday.fracday
Element set: 912
Inclination: 51.6465 deg
RA of node: 317.6729 deg
Eccentricity: .0007254
Arg of perigee: 205.8198 deg
Mean anomaly: 154.2602 deg
Mean motion: 15.71447118 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 304
Coasting Arc #14 (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 = -1062265.70 A = 6733589.46 meter
Y = 5542441.95 meter E = .0009896
Z = 3661620.69 I = 51.39600
XDOT = -6153.257976 Wp = 120.96690
YDOT = 1675.330307 meter/sec RA = 312.05045 deg
ZDOT = -4317.393796 TA = 14.88559
MA = 14.85648
Ha = 194.405 n.mi
Hp = 188.494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3485123.70 X = -1141950.41
Y = 18183864.67 feet Y = 5530117.43 meter
Z = 12013191.26 Z = 3656266.92
XDOT = -20187.854253 XDOT = -6150.561900
YDOT = 5496.490509 feet/sec YDOT = 1606.536074 meter/sec
ZDOT = -14164.677810 ZDOT = -4347.279001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14794491.51 X = 4509361.01
Y = -11155113.70 feet Y = -3400078.65 meter
Z = 11991757.39 Z = 3655087.65
XDOT = 17817.378026 XDOT = 5430.736822
YDOT = 8262.119505 feet/sec YDOT = 2518.294025 meter/sec
ZDOT = -14284.189939 ZDOT = -4353.821094
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 10222.53955771 .00016717 00000-0 10270-3 0 9130
2 25544 51.6463 312.4685 0007040 208.9289 151.1483 15.71468869 32020
Satellite: ISS
Catalog Number: 25544
Epoch time: 10222.53955771 = yrday.fracday
Element set: 913
Inclination: 51.6463 deg
RA of node: 312.4685 deg
Eccentricity: .0007040
Arg of perigee: 208.9289 deg
Mean anomaly: 151.1483 deg
Mean motion: 15.71468869 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3202
Checksum: 314
Coasting Arc #15 (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 = 5254637.81 A = 6734882.87 meter
Y = -2783503.44 meter E = .0010370
Z = 3160246.31 I = 51.38122
XDOT = 282.273681 Wp = 119.41242
YDOT = 6004.650423 meter/sec RA = 306.96700 deg
ZDOT = 4802.618807 TA = 277.50424
MA = 277.62204
Ha = 194.183 n.mi
Hp = 188.600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17239625.35 X = 5270021.33
Y = -9132229.12 feet Y = -2724656.92 meter
Z = 10368262.18 Z = 3185810.18
XDOT = 926.094754 XDOT = 191.777833
YDOT = 19700.296665 feet/sec YDOT = 6007.300989 meter/sec
ZDOT = 15756.623382 ZDOT = 4803.770252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18960539.28 X = -5779172.37
Y = -4355442.62 feet Y = -1327538.91 meter
Z = 10470492.89 Z = 3191406.23
XDOT = 11960.626866 XDOT = 3645.599069
YDOT = -14046.562501 feet/sec YDOT = -4281.392250 meter/sec
ZDOT = 15761.210708 ZDOT = 4804.017024
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 10223.55701894 .00016717 00000-0 10270-3 0 9149
2 25544 51.6460 307.2632 0007070 213.6446 146.4268 15.71502866 32183
Satellite: ISS
Catalog Number: 25544
Epoch time: 10223.55701894 = yrday.fracday
Element set: 914
Inclination: 51.6460 deg
RA of node: 307.2632 deg
Eccentricity: .0007070
Arg of perigee: 213.6446 deg
Mean anomaly: 146.4268 deg
Mean motion: 15.71502866 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 296
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics
DOD C-Band Radar Network
Goddard Space Flight Center (GSFC)
NASA Johnson Space Center (JSC)
DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command.
David Cottle
Director Of Engineering
IDB Communications
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