Date: May 7th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 22604 21 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 1674)
---------------------------------------

Vector Time (GMT): 2010/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1807474
56                 A    =         6731139
32  meter
 Y    =        6107857
17  meter          E    =           
0008472
 Z    =       -2159306
81                 I    =           51
99332
 XDOT =      -4267
815037                 Wp   =          317
36960
 YDOT =       3224
166075  meter/sec      RA   =           88
87719  deg
 ZDOT =       5541
038969                 TA   =           18
58519
                                          MA   =           18
55426
                                          Ha   =            188
917  n
mi
                                          Hp   =            187
445

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5930034
65                 X    =         1749530
61
 Y    =       20038901
48  feet           Y    =         6127745
55  meter
 Z    =       -7084339
93                 Z    =        -2150666
54
 XDOT =     -14002
017839                 XDOT =       -4330
468464
 YDOT =      10577
972688  feet/sec       YDOT =        3176
090254  meter/sec
 ZDOT =      18179
261708                 ZDOT =        5520
153848

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17936521
53                 X    =         5467051
76
 Y    =       10746711
27  feet           Y    =         3275597
60  meter
 Z    =       -7049833
19                 Z    =        -2148789
16
 XDOT =      -2478
590929                 XDOT =        -755
474515
 YDOT =      16021
877999  feet/sec       YDOT =        4883
468414  meter/sec
 ZDOT =      18096
139567                 ZDOT =        5515
703340


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   10125
50424338  
00016717  00000-0  10270-3 0  9005
2 25544  51
6421  89
6439 0010040 278
8281  81
1745 15
73658583 16757


Satellite: ISS
Catalog Number: 25544
Epoch time:      10125
50424338   =   yrday
fracday
Element set:     900
Inclination:       51
6421  deg
RA of node:        89
6439  deg
Eccentricity:     
0010040     
Arg of perigee:   278
8281  deg
Mean anomaly:      81
1745  deg
Mean motion:   15
73658583  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1675
Checksum:              306


Coasting Arc #2 (Orbit 1690)
---------------------------------------

Vector Time (GMT): 2010/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3425676
01                 A    =         6723073
66  meter
 Y    =       -3234119
87  meter          E    =           
0005976
 Z    =       -4799699
43                 I    =           51
96563
 XDOT =       2745
417416                 Wp   =           11
55505
 YDOT =       6718
789377  meter/sec      RA   =           83
80698  deg
 ZDOT =      -2562
579684                 TA   =          233
41313
                                          MA   =          233
46813
                                          Ha   =            189
144  n
mi
                                          Hp   =            187
330

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11239094
52                 X    =         3484902
06
 Y    =      -10610629
50  feet           Y    =        -3195480
62  meter
 Z    =      -15747045
36                 Z    =        -4782913
69
 XDOT =       9007
274988                 XDOT =        2682
531243
 YDOT =      22043
272233  feet/sec       YDOT =        6749
138735  meter/sec
 ZDOT =      -8407
413661                 ZDOT =       -2549
394943

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         925515
35                 X    =          282097
08
 Y    =      -15496629
29  feet           Y    =        -4723372
61  meter
 Z    =      -15680243
74                 Z    =        -4779338
29
 XDOT =      20606
585822                 XDOT =        6280
887359
 YDOT =       9701
756153  feet/sec       YDOT =        2957
095275  meter/sec
 ZDOT =      -8354
803281                 ZDOT =       -2546
544040


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   10126
52027681  
00016717  00000-0  10270-3 0  9019
2 25544  51
6428  84
4287 0010125 282
7728  77
2303 15
73710167 16913


Satellite: ISS
Catalog Number: 25544
Epoch time:      10126
52027681   =   yrday
fracday
Element set:     901
Inclination:       51
6428  deg
RA of node:        84
4287  deg
Eccentricity:     
0010125     
Arg of perigee:   282
7728  deg
Mean anomaly:      77
2303  deg
Mean motion:   15
73710167  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1691
Checksum:              296


Coasting Arc #3 (Orbit 1706)
---------------------------------------

Vector Time (GMT): 2010/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2957512
27                 A    =         6730603
46  meter
 Y    =       -5587615
77  meter          E    =           
0003831
 Z    =        2303892
84                 I    =           51
98723
 XDOT =       3527
261195                 Wp   =          109
76226
 YDOT =      -4121
335300  meter/sec      RA   =           78
65761  deg
 ZDOT =      -5461
460111                 TA   =           44
47911
                                          MA   =           44
44836
                                          Ha   =            189
403  n
mi
                                          Hp   =            187
232

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9703124
24                 X    =        -2906002
69
 Y    =      -18332072
73  feet           Y    =        -5620400
48  meter
 Z    =        7558703
54                 Z    =         2289650
17
 XDOT =      11572
379249                 XDOT =        3599
615480
 YDOT =     -13521
441272  feet/sec       YDOT =       -4081
486696  meter/sec
 ZDOT =     -17918
176217                 ZDOT =       -5444
148922

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19795789
98                 X    =        -6033756
78
 Y    =       -6260805
37  feet           Y    =        -1908293
48  meter
 Z    =        7501901
45                 Z    =         2286579
56
 XDOT =      -1589
072509                 XDOT =        -484
349301
 YDOT =     -16387
076769  feet/sec       YDOT =       -4994
780999  meter/sec
 ZDOT =     -17849
290024                 ZDOT =       -5440
463599


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   10127
53628187  
00016717  00000-0  10270-3 0  9020
2 25544  51
6431  79
2136 0010165 286
8397  73
1651 15
73754181 17076


Satellite: ISS
Catalog Number: 25544
Epoch time:      10127
53628187   =   yrday
fracday
Element set:     902
Inclination:       51
6431  deg
RA of node:        79
2136  deg
Eccentricity:     
0010165     
Arg of perigee:   286
8397  deg
Mean anomaly:      73
1651  deg
Mean motion:   15
73754181  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1707
Checksum:              310


Coasting Arc #4 (Orbit 1722)
---------------------------------------

Vector Time (GMT): 2010/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2718574
62                 A    =         6722931
27  meter
 Y    =        3913206
38  meter          E    =           
0002994
 Z    =        4745416
16                 I    =           51
95570
 XDOT =      -3969
582351                 Wp   =          266
16567
 YDOT =      -6020
927335  meter/sec      RA   =           73
58828  deg
 ZDOT =       2692
169370                 TA   =          157
47628
                                          MA   =          157
46313
                                          Ha   =            189
593  n
mi
                                          Hp   =            186
951

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8919208
07                 X    =        -2785183
32
 Y    =       12838603
59  feet           Y    =         3882433
15  meter
 Z    =       15568950
64                 Z    =         4732047
47
 XDOT =     -13023
564144                 XDOT =       -3915
038415
 YDOT =     -19753
698607  feet/sec       YDOT =       -6065
012639  meter/sec
 ZDOT =       8832
576673                 ZDOT =        2673
017366

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2824018
38                 X    =          860760
80
 Y    =       15429205
95  feet           Y    =         4702821
97  meter
 Z    =       15515758
53                 Z    =         4729203
20
 XDOT =     -22123
514774                 XDOT =       -6743
247303
 YDOT =      -4751
917081  feet/sec       YDOT =       -1448
384326  meter/sec
 ZDOT =       8756
223043                 ZDOT =        2668
896783


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   10128
55225661  
00016717  00000-0  10270-3 0  9034
2 25544  51
6438  73
9984 0010280 289
7981  70
2074 15
73832234 17235


Satellite: ISS
Catalog Number: 25544
Epoch time:      10128
55225661   =   yrday
fracday
Element set:     903
Inclination:       51
6438  deg
RA of node:        73
9984  deg
Eccentricity:     
0010280     
Arg of perigee:   289
7981  deg
Mean anomaly:      70
2074  deg
Mean motion:   15
73832234  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1723
Checksum:              313


Coasting Arc #5 (Orbit 1737)
---------------------------------------

Vector Time (GMT): 2010/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3944978
21                 A    =         6730227
52  meter
 Y    =        4891007
98  meter          E    =           
0009741
 Z    =       -2392383
62                 I    =           51
97019
 XDOT =      -2658
154370                 Wp   =          326
71266
 YDOT =       4792
943199  meter/sec      RA   =           68
43526  deg
 ZDOT =       5413
142904                 TA   =            6
43346
                                          MA   =            6
42096
                                          Ha   =            189
902  n
mi
                                          Hp   =            186
706

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12942841
89                 X    =         3901614
79
 Y    =       16046614
10  feet           Y    =         4934880
65  meter
 Z    =       -7849027
64                 Z    =        -2373323
93
 XDOT =      -8720
978903                 XDOT =       -2737
848768
 YDOT =      15724
879261  feet/sec       YDOT =        4762
772455  meter/sec
 ZDOT =      17759
655198                 ZDOT =        5400
035919

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20578307
85                 X    =         6272268
23
 Y    =        1652556
66  feet           Y    =          503699
27  meter
 Z    =       -7773063
59                 Z    =        -2369229
78
 XDOT =       5428
157821                 XDOT =        1654
502504
 YDOT =      15733
255385  feet/sec       YDOT =        4795
496241  meter/sec
 ZDOT =      17707
510495                 ZDOT =        5397
249199


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   10129
50470949  
00016717  00000-0  10270-3 0  9042
2 25544  51
6435  69
1084 0010293 294
3181  65
6907 15
73826306 17380


Satellite: ISS
Catalog Number: 25544
Epoch time:      10129
50470949   =   yrday
fracday
Element set:     904
Inclination:       51
6435  deg
RA of node:        69
1084  deg
Eccentricity:     
0010293     
Arg of perigee:   294
3181  deg
Mean anomaly:      65
6907  deg
Mean motion:   15
73826306  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1738
Checksum:              316


Coasting Arc #6 (Orbit 1753)
---------------------------------------

Vector Time (GMT): 2010/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1918118
31                 A    =         6722870
74  meter
 Y    =       -4402578
42  meter          E    =           
0008598
 Z    =       -4709770
26                 I    =           51
93502
 XDOT =       5006
246386                 Wp   =            9
86092
 YDOT =       5148
951338  meter/sec      RA   =           63
36468  deg
 ZDOT =      -2766
707308                 TA   =          232
93090
                                          MA   =          233
00955
                                          Ha   =            189
942  n
mi
                                          Hp   =            186
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6293039
06                 X    =         1990085
77
 Y    =      -14444154
91  feet           Y    =        -4380726
38  meter
 Z    =      -15452002
16                 Z    =        -4700277
17
 XDOT =      16424
692867                 XDOT =        4961
738197
 YDOT =      16892
884967  feet/sec       YDOT =        5204
685371  meter/sec
 ZDOT =      -9077
123713                 ZDOT =       -2742
494547

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6312858
72                 X    =        -1924159
34
 Y    =      -14475820
16  feet           Y    =        -4412229
98  meter
 Z    =      -15414239
13                 Z    =        -4698260
09
 XDOT =      22532
452644                 XDOT =        6867
891566
 YDOT =       -237
079861  feet/sec       YDOT =         -72
261942  meter/sec
 ZDOT =      -8980
643504                 ZDOT =       -2737
300140


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   10130
52063007  
00016717  00000-0  10270-3 0  9050
2 25544  51
6445  63
8925 0010230 298
2461  61
7669 15
73899863 17549


Satellite: ISS
Catalog Number: 25544
Epoch time:      10130
52063007   =   yrday
fracday
Element set:     905
Inclination:       51
6445  deg
RA of node:        63
8925  deg
Eccentricity:     
0010230     
Arg of perigee:   298
2461  deg
Mean anomaly:      61
7669  deg
Mean motion:   15
73899863  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1754
Checksum:              313


Coasting Arc #7 (Orbit 1769)
---------------------------------------

Vector Time (GMT): 2010/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4766064
95                 A    =         6729866
52  meter
 Y    =       -4084484
29  meter          E    =           
0004912
 Z    =        2426160
29                 I    =           51
94474
 XDOT =       1725
902531                 Wp   =           71
07396
 YDOT =      -5219
601619  meter/sec      RA   =           58
20952  deg
 ZDOT =      -5386
472105                 TA   =           81
67648
                                          MA   =           81
62078
                                          Ha   =            190
090  n
mi
                                          Hp   =            186
264

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15636696
02                 X    =        -4731823
37
 Y    =      -13400539
01  feet           Y    =        -4137589
90  meter
 Z    =        7959843
48                 Z    =         2403089
30
 XDOT =       5662
409880                 XDOT =        1810
307822
 YDOT =     -17124
677227  feet/sec       YDOT =       -5199
829408  meter/sec
 ZDOT =     -17672
152575                 ZDOT =       -5377
882675

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20433743
08                 X    =        -6228204
89
 Y    =        2828010
39  feet           Y    =          861977
57  meter
 Z    =        7867929
68                 Z    =         2398144
97
 XDOT =      -8769
038892                 XDOT =       -2672
803054
 YDOT =     -14193
332040  feet/sec       YDOT =       -4326
127606  meter/sec
 ZDOT =     -17637
987161                 ZDOT =       -5376
058487


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   10131
53652190  
00016717  00000-0  10270-3 0  9060
2 25544  51
6451  58
6769 0010269 301
8519  58
1644 15
73933400 17708


Satellite: ISS
Catalog Number: 25544
Epoch time:      10131
53652190   =   yrday
fracday
Element set:     906
Inclination:       51
6451  deg
RA of node:        58
6769  deg
Eccentricity:     
0010269     
Arg of perigee:   301
8519  deg
Mean anomaly:      58
1644  deg
Mean motion:   15
73933400  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1770
Checksum:              302


Coasting Arc #8 (Orbit 1785)
---------------------------------------

Vector Time (GMT): 2010/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1106684
91                 A    =         6722605
78  meter
 Y    =        4672733
12  meter          E    =           
0002710
 Z    =        4705023
74                 I    =           51
90429
 XDOT =      -5846
481334                 Wp   =          325
71961
 YDOT =      -4173
617558  meter/sec      RA   =           53
13657  deg
 ZDOT =       2772
761874                 TA   =           97
06505
                                          MA   =           97
03423
                                          Ha   =            190
233  n
mi
                                          Hp   =            185
903

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3630855
99                 X    =        -1181710
67
 Y    =       15330489
25  feet           Y    =         4659937
74  meter
 Z    =       15436429
61                 Z    =         4699465
39
 XDOT =     -19181
369206                 XDOT =       -5812
846541
 YDOT =     -13692
970990  feet/sec       YDOT =       -4238
808498  meter/sec
 ZDOT =       9096
987776                 ZDOT =        2744
440476

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9213121
73                 X    =         2808159
50
 Y    =       12806539
24  feet           Y    =         3903433
16  meter
 Z    =       15414321
77                 Z    =         4698285
27
 XDOT =     -21982
334072                 XDOT =       -6700
215425
 YDOT =       5012
349723  feet/sec       YDOT =        1527
764196  meter/sec
 ZDOT =       8984
172287                 ZDOT =        2738
375713


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   10132
55238422  
00016717  00000-0  10270-3 0  9072
2 25544  51
6454  53
4608 0010268 305
1805  54
8396 15
73988320 17865


Satellite: ISS
Catalog Number: 25544
Epoch time:      10132
55238422   =   yrday
fracday
Element set:     907
Inclination:       51
6454  deg
RA of node:        53
4608  deg
Eccentricity:     
0010268     
Arg of perigee:   305
1805  deg
Mean anomaly:      54
8396  deg
Mean motion:   15
73988320  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1786
Checksum:              311


Coasting Arc #9 (Orbit 1800)
---------------------------------------

Vector Time (GMT): 2010/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5409480
60                 A    =         6729655
51  meter
 Y    =        3179826
89  meter          E    =           
0011120
 Z    =       -2411295
30                 I    =           51
90962
 XDOT =       -792
978441                 Wp   =          338
75902
 YDOT =       5440
323422  meter/sec      RA   =           47
97831  deg
 ZDOT =       5397
751206                 TA   =          354
12673
                                          MA   =          354
13976
                                          Ha   =            190
447  n
mi
                                          Hp   =            185
613

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17747639
77                 X    =         5385235
06
 Y    =       10432502
91  feet           Y    =         3240183
56  meter
 Z    =       -7911073
83                 Z    =        -2385074
07
 XDOT =      -2601
635305                 XDOT =        -879
976075
 YDOT =      17848
830124  feet/sec       YDOT =        5430
968970  meter/sec
 ZDOT =      17709
157500                 ZDOT =        5393
687976

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19385129
94                 X    =         5908587
61
 Y    =       -7047987
36  feet           Y    =        -2148226
55  meter
 Z    =       -7806634
04                 Z    =        -2379462
06
 XDOT =      11505
527978                 XDOT =        3506
884928
 YDOT =      12056
884214  feet/sec       YDOT =        3674
938308  meter/sec
 ZDOT =      17692
997130                 ZDOT =        5392
825525


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   10133
50473005  
00016717  00000-0  10270-3 0  9087
2 25544  51
6459  48
5707 0010333 309
0085  51
0158 15
74019378 18013


Satellite: ISS
Catalog Number: 25544
Epoch time:      10133
50473005   =   yrday
fracday
Element set:     908
Inclination:       51
6459  deg
RA of node:        48
5707  deg
Eccentricity:     
0010333     
Arg of perigee:   309
0085  deg
Mean anomaly:      51
0158  deg
Mean motion:   15
74019378  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1801
Checksum:              284


Coasting Arc #10 (Orbit 1816)
---------------------------------------

Vector Time (GMT): 2010/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         300868
53                 A    =         6722260
93  meter
 Y    =       -4781742
53  meter          E    =           
0011150
 Z    =       -4722459
87                 I    =           51
86518
 XDOT =       6489
149254                 Wp   =           15
97319
 YDOT =       3109
167006  meter/sec      RA   =           42
90228  deg
 ZDOT =      -2725
796843                 TA   =          227
21183
                                          MA   =          227
30565
                                          Ha   =            190
463  n
mi
                                          Hp   =            185
303

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         987101
49                 X    =          377257
81
 Y    =      -15688131
67  feet           Y    =        -4777950
40  meter
 Z    =      -15493634
75                 Z    =        -4720813
20
 XDOT =      21289
859757                 XDOT =        6467
141399
 YDOT =      10200
679153  feet/sec       YDOT =        3181
609785  meter/sec
 ZDOT =      -8942
903027                 ZDOT =       -2694
325007

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11578507
70                 X    =        -3529129
15
 Y    =      -10641093
91  feet           Y    =        -3243405
42  meter
 Z    =      -15487086
32                 Z    =        -4720463
91
 XDOT =      20520
187923                 XDOT =        6254
553279
 YDOT =      -9451
907085  feet/sec       YDOT =       -2880
941280  meter/sec
 ZDOT =      -8817
555985                 ZDOT =       -2687
591064


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   10134
52053694  
00016717  00000-0  10270-3 0  9099
2 25544  51
6468  43
3547 0010329 313
2097  46
8202 15
74083513 18174


Satellite: ISS
Catalog Number: 25544
Epoch time:      10134
52053694   =   yrday
fracday
Element set:     909
Inclination:       51
6468  deg
RA of node:        43
3547  deg
Eccentricity:     
0010329     
Arg of perigee:   313
2097  deg
Mean anomaly:      46
8202  deg
Mean motion:   15
74083513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1817
Checksum:              297


Coasting Arc #11 (Orbit 1832)
---------------------------------------

Vector Time (GMT): 2010/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5898076
72                 A    =         6729618
04  meter
 Y    =       -2247513
18  meter          E    =           
0007054
 Z    =        2334771
62                 I    =           51
86651
 XDOT =        -78
424157                 Wp   =           61
97230
 YDOT =      -5452
235800  meter/sec      RA   =           37
74128  deg
 ZDOT =      -5430
941386                 TA   =           91
85572
                                          MA   =           91
77493
                                          Ha   =            190
611  n
mi
                                          Hp   =            185
164

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19350645
41                 X    =        -5883848
35
 Y    =       -7373730
90  feet           Y    =        -2313389
73  meter
 Z    =        7660011
88                 Z    =         2306152
54
 XDOT =       -257
297104                 XDOT =           8
932532
 YDOT =     -17887
912731  feet/sec       YDOT =       -5452
623641  meter/sec
 ZDOT =     -17818
049168                 ZDOT =       -5431
110895

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17688575
42                 X    =        -5391477
79
 Y    =       10847438
97  feet           Y    =         3306299
40  meter
 Z    =        7546027
74                 Z    =         2300029
26
 XDOT =     -13462
208744                 XDOT =       -4103
281225
 YDOT =      -9520
555236  feet/sec       YDOT =       -2901
865236  meter/sec
 ZDOT =     -17818
726050                 ZDOT =       -5431
147700


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   10135
53631591  
00016717  00000-0  10270-3 0  9101
2 25544  51
6464  38
1383 0010298 316
5090  43
5260 15
74091106 18337


Satellite: ISS
Catalog Number: 25544
Epoch time:      10135
53631591   =   yrday
fracday
Element set:     910
Inclination:       51
6464  deg
RA of node:        38
1383  deg
Eccentricity:     
0010298     
Arg of perigee:   316
5090  deg
Mean anomaly:      43
5260  deg
Mean motion:   15
74091106  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1833
Checksum:              282


Coasting Arc #12 (Orbit 1848)
---------------------------------------

Vector Time (GMT): 2010/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         412800
05                 A    =         6721842
29  meter
 Y    =        4718541
96  meter          E    =           
0004357
 Z    =        4767959
93                 I    =           51
81684
 XDOT =      -6958
375843                 Wp   =          356
36709
 YDOT =      -2023
097478  meter/sec      RA   =           32
65936  deg
 ZDOT =       2608
959081                 TA   =           68
12813
                                          MA   =           68
08181
                                          Ha   =            190
743  n
mi
                                          Hp   =            184
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1354330
88                 X    =          336843
62
 Y    =       15480780
70  feet           Y    =         4722732
77  meter
 Z    =       15642913
15                 Z    =         4769781
50
 XDOT =     -22829
317071                 XDOT =       -6947
910038
 YDOT =      -6637
458918  feet/sec       YDOT =       -2100
852025  meter/sec
 ZDOT =       8559
577038                 ZDOT =        2575
180020

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13169511
07                 X    =         4014066
98
 Y    =        8235645
57  feet           Y    =         2510224
77  meter
 Z    =       15650164
06                 Z    =         4770170
01
 XDOT =     -18389
458287                 XDOT =       -5605
106886
 YDOT =      13423
618461  feet/sec       YDOT =        4091
518907  meter/sec
 ZDOT =       8425
038576                 ZDOT =        2567
951758


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   10136
55206490  
00016717  00000-0  10270-3 0  9111
2 25544  51
6468  32
9211 0010387 320
4447  39
5957 15
74149716 18498


Satellite: ISS
Catalog Number: 25544
Epoch time:      10136
55206490   =   yrday
fracday
Element set:     911
Inclination:       51
6468  deg
RA of node:        32
9211  deg
Eccentricity:     
0010387     
Arg of perigee:   320
4447  deg
Mean anomaly:      39
5957  deg
Mean motion:   15
74149716  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1849
Checksum:              313


Coasting Arc #13 (Orbit 1863)
---------------------------------------

Vector Time (GMT): 2010/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6216579
71                 A    =         6729524
49  meter
 Y    =        1271010
01  meter          E    =           
0013209
 Z    =       -2215831
71                 I    =           51
81721
 XDOT =        868
087163                 Wp   =          350
63051
 YDOT =       5327
622870  meter/sec      RA   =           27
49543  deg
 ZDOT =       5499
592722                 TA   =          344
57087
                                          MA   =          344
61110
                                          Ha   =            190
908  n
mi
                                          Hp   =            184
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20395602
71                 X    =         6212669
19
 Y    =        4169980
35  feet           Y    =         1340505
95  meter
 Z    =       -7269789
09                 Z    =        -2185640
69
 XDOT =       2848
054998                 XDOT =         781
732003
 YDOT =      17479
077659  feet/sec       YDOT =        5336
846738  meter/sec
 ZDOT =      18043
283210                 ZDOT =        5503
600899

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15311473
34                 X    =         4666937
07
 Y    =      -14165524
59  feet           Y    =        -4317651
90  meter
 Z    =       -7149536
81                 Z    =        -2179178
82
 XDOT =      14762
471753                 XDOT =        4499
601390
 YDOT =       6855
775155  feet/sec       YDOT =        2089
640267  meter/sec
 ZDOT =      18059
239270                 ZDOT =        5504
456129


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   10137
50430360  
00016717  00000-0  10270-3 0  9123
2 25544  51
6471  28
0301 0010502 323
6531  36
3918 15
74204889 18648


Satellite: ISS
Catalog Number: 25544
Epoch time:      10137
50430360   =   yrday
fracday
Element set:     912
Inclination:       51
6471  deg
RA of node:        28
0301  deg
Eccentricity:     
0010502     
Arg of perigee:   323
6531  deg
Mean anomaly:      36
3918  deg
Mean motion:   15
74204889  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1864
Checksum:              275


Coasting Arc #14 (Orbit 1879)
---------------------------------------

Vector Time (GMT): 2010/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1062458
95                 A    =         6721273
37  meter
 Y    =       -4557979
34  meter          E    =           
0013776
 Z    =       -4833643
88                 I    =           51
76255
 XDOT =       7240
009688                 Wp   =           24
24279
 YDOT =        907
716074  meter/sec      RA   =           22
40778  deg
 ZDOT =      -2437
474315                 TA   =          221
91435
                                          MA   =          222
01989
                                          Ha   =            190
923  n
mi
                                          Hp   =            184
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3485757
72                 X    =         -987930
82
 Y    =      -14954000
44  feet           Y    =        -4569443
07  meter
 Z    =      -15858411
68                 Z    =        -4838624
86
 XDOT =      23753
312625                 XDOT =        7241
162185
 YDOT =       2978
071110  feet/sec       YDOT =         988
684921  meter/sec
 ZDOT =      -7996
962975                 ZDOT =       -2402
299343

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14224885
48                 X    =        -4335745
10
 Y    =       -5726769
13  feet           Y    =        -1745519
23  meter
 Z    =      -15878243
15                 Z    =        -4839688
51
 XDOT =      15582
457926                 XDOT =        4749
533176
 YDOT =     -16831
898832  feet/sec       YDOT =       -5130
362764  meter/sec
 ZDOT =      -7856
854266                 ZDOT =       -2394
769180


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   10138
51999716  
00016717  00000-0  10270-3 0  9131
2 25544  51
6469  22
8129 0010628 327
2919  32
7585 15
74257897 18809


Satellite: ISS
Catalog Number: 25544
Epoch time:      10138
51999716   =   yrday
fracday
Element set:     913
Inclination:       51
6469  deg
RA of node:        22
8129  deg
Eccentricity:     
0010628     
Arg of perigee:   327
2919  deg
Mean anomaly:      32
7585  deg
Mean motion:   15
74257897  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1880
Checksum:              344


Coasting Arc #15 (Orbit 1895)
---------------------------------------

Vector Time (GMT): 2010/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6410385
37                 A    =         6729705
66  meter
 Y    =        -318850
49  meter          E    =           
0008946
 Z    =        2024836
05                 I    =           51
76238
 XDOT =      -1517
728753                 Wp   =           63
37259
 YDOT =      -5076
069722  meter/sec      RA   =           17
24176  deg
 ZDOT =      -5581
446919                 TA   =           94
10511
                                          MA   =           94
00286
                                          Ha   =            191
065  n
mi
                                          Hp   =            183
965

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21031448
06                 X    =        -6416179
78
 Y    =       -1046097
40  feet           Y    =         -390567
84  meter
 Z    =        6643162
88                 Z    =         1993680
27
 XDOT =      -4979
425042                 XDOT =       -1433
740758
 YDOT =     -16653
772053  feet/sec       YDOT =       -5092
571687  meter/sec
 ZDOT =     -18311
833725                 ZDOT =       -5588
616569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12567926
85                 X    =        -3830704
11
 Y    =       16943931
10  feet           Y    =         5164510
20  meter
 Z    =        6519060
81                 Z    =         1987009
74
 XDOT =     -15320
737342                 XDOT =       -4669
760742
 YDOT =      -4278
248298  feet/sec       YDOT =       -1304
010081  meter/sec
 ZDOT =     -18340
382566                 ZDOT =       -5590
148606


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   10139
53566399  
00016717  00000-0  10270-3 0  9142
2 25544  51
6468  17
5953 0010497 331
2061  28
8522 15
74264973 18968


Satellite: ISS
Catalog Number: 25544
Epoch time:      10139
53566399   =   yrday
fracday
Element set:     914
Inclination:       51
6468  deg
RA of node:        17
5953  deg
Eccentricity:     
0010497     
Arg of perigee:   331
2061  deg
Mean anomaly:      28
8522  deg
Mean motion:   15
74264973  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1896
Checksum:              334

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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