Date: July 6th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12378 5 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 2588)
---------------------------------------

Vector Time (GMT): 2010/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6062241
52                 A    =         6737233
36  meter
 Y    =        2864903
84  meter          E    =           
0022593
 Z    =         517799
26                 I    =           51
82447
 XDOT =      -1610
672023                 Wp   =           42
65293
 YDOT =      -4522
244671  meter/sec      RA   =          151
22451  deg
 ZDOT =       6027
678262                 TA   =          322
96782
                                          MA   =          323
12354
                                          Ha   =            195
885  n
mi
                                          Hp   =            184
138

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19889243
82                 X    =        -6096342
19
 Y    =        9399290
80  feet           Y    =         2796921
51  meter
 Z    =        1698816
45                 Z    =          488266
62
 XDOT =      -5284
357030                 XDOT =       -1589
264879
 YDOT =     -14836
760731  feet/sec       YDOT =       -4540
137152  meter/sec
 ZDOT =      19775
847316                 ZDOT =        6019
905169

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12599792
73                 X    =         3840416
82
 Y    =       18043298
20  feet           Y    =         5499597
29  meter
 Z    =        1580910
45                 Z    =          481861
50
 XDOT =     -12406
006844                 XDOT =       -3781
350886
 YDOT =       6891
246096  feet/sec       YDOT =        2100
451810  meter/sec
 ZDOT =      19744
747805                 ZDOT =        6018
199131


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   10183
56264152  
00016717  00000-0  10270-3 0  9001
2 25544  51
6437 151
9092 0009789  32
0679 328
1077 15
72193407 25896


Satellite: ISS
Catalog Number: 25544
Epoch time:      10183
56264152   =   yrday
fracday
Element set:     900
Inclination:       51
6437  deg
RA of node:       151
9092  deg
Eccentricity:     
0009789     
Arg of perigee:    32
0679  deg
Mean anomaly:     328
1077  deg
Mean motion:   15
72193407  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2589
Checksum:              321


Coasting Arc #2 (Orbit 2603)
---------------------------------------

Vector Time (GMT): 2010/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2390492
02                 A    =         6725325
20  meter
 Y    =        3413304
14  meter          E    =           
0022289
 Z    =       -5296529
38                 I    =           51
81072
 XDOT =      -6347
318492                 Wp   =           68
26798
 YDOT =       4327
763212  meter/sec      RA   =          146
11129  deg
 ZDOT =        -67
916250                 TA   =          201
04163
                                          MA   =          201
13347
                                          Ha   =            196
019  n
mi
                                          Hp   =            184
070

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7842821
59                 X    =         2377875
62
 Y    =       11198504
40  feet           Y    =         3439966
09  meter
 Z    =      -17377064
89                 Z    =        -5284946
69
 XDOT =     -20824
535735                 XDOT =       -6394
910655
 YDOT =      14198
698202  feet/sec       YDOT =        4256
517615  meter/sec
 ZDOT =       -222
822343                 ZDOT =         -98
866507

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9540345
95                 X    =         2907897
45
 Y    =       -9874470
04  feet           Y    =        -3009738
47  meter
 Z    =      -17330763
86                 Z    =        -5282416
82
 XDOT =      17075
652750                 XDOT =        5204
658958
 YDOT =      17151
062339  feet/sec       YDOT =        5227
643801  meter/sec
 ZDOT =       -346
382927                 ZDOT =        -105
577516


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   10184
51609218  
00016717  00000-0  10270-3 0  9014
2 25544  51
6442 147
0262 0009909  34
6243 325
5563 15
72172655 26047


Satellite: ISS
Catalog Number: 25544
Epoch time:      10184
51609218   =   yrday
fracday
Element set:     901
Inclination:       51
6442  deg
RA of node:       147
0262  deg
Eccentricity:     
0009909     
Arg of perigee:    34
6243  deg
Mean anomaly:     325
5563  deg
Mean motion:   15
72172655  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2604
Checksum:              295


Coasting Arc #3 (Orbit 2619)
---------------------------------------

Vector Time (GMT): 2010/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4892055
27                 A    =         6737099
53  meter
 Y    =       -4588001
69  meter          E    =           
0016589
 Z    =         619972
49                 I    =           51
87555
 XDOT =       3677
604358                 Wp   =           91
65743
 YDOT =       3090
704291  meter/sec      RA   =          140
99718  deg
 ZDOT =      -6009
718588                 TA   =           81
62316
                                          MA   =           81
43513
                                          Ha   =            196
033  n
mi
                                          Hp   =            183
829

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16050050
10                 X    =         4939983
84
 Y    =      -15052499
00  feet           Y    =        -4533027
90  meter
 Z    =        2034030
49                 Z    =          643853
96
 XDOT =      12065
631096                 XDOT =        3671
964299
 YDOT =      10140
105942  feet/sec       YDOT =        3131
798609  meter/sec
 ZDOT =     -19716
924501                 ZDOT =       -5991
866153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17972981
04                 X    =        -5478164
62
 Y    =      -12678992
99  feet           Y    =        -3864557
06  meter
 Z    =        2129366
95                 Z    =          649031
05
 XDOT =       6554
796508                 XDOT =        1997
901976
 YDOT =     -12663
238686  feet/sec       YDOT =       -3859
755152  meter/sec
 ZDOT =     -19645
584204                 ZDOT =       -5987
974065


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   10185
53309212  
00016717  00000-0  10270-3 0  9029
2 25544  51
6446 141
8178 0009947  38
0471 322
1392 15
72206787 26207


Satellite: ISS
Catalog Number: 25544
Epoch time:      10185
53309212   =   yrday
fracday
Element set:     902
Inclination:       51
6446  deg
RA of node:       141
8178  deg
Eccentricity:     
0009947     
Arg of perigee:    38
0471  deg
Mean anomaly:     322
1392  deg
Mean motion:   15
72206787  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2620
Checksum:              300


Coasting Arc #4 (Orbit 2635)
---------------------------------------

Vector Time (GMT): 2010/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3905226
51                 A    =         6725708
09  meter
 Y    =       -1843317
87  meter          E    =           
0011175
 Z    =        5146620
78                 I    =           51
86075
 XDOT =       4639
974353                 Wp   =           64
86518
 YDOT =      -5997
933192  meter/sec      RA   =          135
91014  deg
 ZDOT =       1374
903660                 TA   =           12
03790
                                          MA   =           12
01122
                                          Ha   =            196
083  n
mi
                                          Hp   =            183
697

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12812422
94                 X    =        -3909325
34
 Y    =       -6047630
80  feet           Y    =        -1887012
00  meter
 Z    =       16885238
79                 Z    =         5127638
98
 XDOT =      15223
012969                 XDOT =        4700
020435
 YDOT =     -19678
258505  feet/sec       YDOT =       -5945
710667  meter/sec
 ZDOT =       4510
838778                 ZDOT =        1397
589791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3084806
64                 X    =         -940249
06
 Y    =       13920180
12  feet           Y    =         4242870
90  meter
 Z    =       16809398
04                 Z    =         5123504
52
 XDOT =     -21504
019084                 XDOT =       -6554
425017
 YDOT =     -10312
563769  feet/sec       YDOT =       -3143
269437  meter/sec
 ZDOT =       4601
399512                 ZDOT =        1402
506571


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   10186
55007762  
00016717  00000-0  10270-3 0  9038
2 25544  51
6449 136
6103 0009818  41
2951 318
8952 15
72256337 26363


Satellite: ISS
Catalog Number: 25544
Epoch time:      10186
55007762   =   yrday
fracday
Element set:     903
Inclination:       51
6449  deg
RA of node:       136
6103  deg
Eccentricity:     
0009818     
Arg of perigee:    41
2951  deg
Mean anomaly:     318
8952  deg
Mean motion:   15
72256337  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2636
Checksum:              315


Coasting Arc #5 (Orbit 2650)
---------------------------------------

Vector Time (GMT): 2010/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3095527
74                 A    =         6735815
46  meter
 Y    =        5708993
66  meter          E    =           
0017348
 Z    =       -1766832
54                 I    =           51
91523
 XDOT =      -5061
891358                 Wp   =           42
29950
 YDOT =       -989
541382  meter/sec      RA   =          130
77779  deg
 ZDOT =       5715
925015                 TA   =          298
21741
                                          MA   =          298
39247
                                          Ha   =            196
079  n
mi
                                          Hp   =            183
562

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10155930
91                 X    =        -3150553
70
 Y    =       18730294
15  feet           Y    =         5674070
20  meter
 Z    =       -5796694
68                 Z    =        -1782003
50
 XDOT =     -16607
255112                 XDOT =       -5078
216918
 YDOT =      -3246
526844  feet/sec       YDOT =       -1046
238565  meter/sec
 ZDOT =      18753
034826                 ZDOT =        5691
294479

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20583538
04                 X    =         6273862
39
 Y    =        5438664
73  feet           Y    =         1657705
01  meter
 Z    =       -5857252
66                 Z    =        -1785290
61
 XDOT =       1168
451736                 XDOT =         356
144089
 YDOT =      15511
553064  feet/sec       YDOT =        4727
921374  meter/sec
 ZDOT =      18654
631813                 ZDOT =        5685
931777


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   10187
50349131  
00016717  00000-0  10270-3 0  9044
2 25544  51
6446 131
7272 0009940  44
9169 315
2796 15
72234851 26511


Satellite: ISS
Catalog Number: 25544
Epoch time:      10187
50349131   =   yrday
fracday
Element set:     904
Inclination:       51
6446  deg
RA of node:       131
7272  deg
Eccentricity:     
0009940     
Arg of perigee:    44
9169  deg
Mean anomaly:     315
2796  deg
Mean motion:   15
72234851  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2651
Checksum:              309


Coasting Arc #6 (Orbit 2666)
---------------------------------------

Vector Time (GMT): 2010/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4737696
83                 A    =         6727280
26  meter
 Y    =        -152858
44  meter          E    =           
0021001
 Z    =       -4793443
69                 I    =           51
90649
 XDOT =      -2402
220344                 Wp   =           61
19821
 YDOT =       6820
738801  meter/sec      RA   =          125
71078  deg
 ZDOT =      -2590
433011                 TA   =          183
42186
                                          MA   =          183
43625
                                          Ha   =            196
089  n
mi
                                          Hp   =            183
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15543624
76                 X    =         4762339
73
 Y    =        -501504
07  feet           Y    =          -99740
12  meter
 Z    =      -15726521
28                 Z    =        -4770368
06
 XDOT =      -7881
300342                 XDOT =       -2465
728663
 YDOT =      22377
751973  feet/sec       YDOT =        6793
521068  meter/sec
 ZDOT =      -8498
795967                 ZDOT =       -2602
256180

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4419683
79                 X    =        -1347119
62
 Y    =      -15007110
25  feet           Y    =        -4574167
20  meter
 Z    =      -15634330
36                 Z    =        -4765343
89
 XDOT =      22533
499261                 XDOT =        6868
210575
 YDOT =       2271
579844  feet/sec       YDOT =         692
377536  meter/sec
 ZDOT =      -8545
986575                 ZDOT =       -2604
816708


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   10188
52045182  
00016717  00000-0  10270-3 0  9057
2 25544  51
6455 126
5182 0009943  48
7593 311
4424 15
72275047 26674


Satellite: ISS
Catalog Number: 25544
Epoch time:      10188
52045182   =   yrday
fracday
Element set:     905
Inclination:       51
6455  deg
RA of node:       126
5182  deg
Eccentricity:     
0009943     
Arg of perigee:    48
7593  deg
Mean anomaly:     311
4424  deg
Mean motion:   15
72275047  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2667
Checksum:              315


Coasting Arc #7 (Orbit 2682)
---------------------------------------

Vector Time (GMT): 2010/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1077408
78                 A    =         6733758
48  meter
 Y    =       -6048190
83  meter          E    =           
0021502
 Z    =        2743972
96                 I    =           51
94589
 XDOT =       5526
389072                 Wp   =           80
59010
 YDOT =      -1382
881373  meter/sec      RA   =          120
56610  deg
 ZDOT =      -5180
352641                 TA   =           68
21734
                                          MA   =           67
98867
                                          Ha   =            196
102  n
mi
                                          Hp   =            183
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3534805
72                 X    =         1131630
96
 Y    =      -19843145
78  feet           Y    =        -6035839
93  meter
 Z    =        9002535
95                 Z    =         2749337
61
 XDOT =      18131
197744                 XDOT =        5566
607178
 YDOT =      -4537
012378  feet/sec       YDOT =       -1320
856177  meter/sec
 ZDOT =     -16995
907614                 ZDOT =       -5153
408003

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20049625
79                 X    =        -6111125
94
 Y    =        1967723
77  feet           Y    =          599762
20  meter
 Z    =        9023940
84                 Z    =         2750497
17
 XDOT =      -9117
365067                 XDOT =       -2778
972872
 YDOT =     -14884
492363  feet/sec       YDOT =       -4536
793272  meter/sec
 ZDOT =     -16888
253234                 ZDOT =       -5147
539586


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   10189
53739880  
00016717  00000-0  10270-3 0  9065
2 25544  51
6460 121
3098 0009932  52
3105 307
8957 15
72294006 26831


Satellite: ISS
Catalog Number: 25544
Epoch time:      10189
53739880   =   yrday
fracday
Element set:     906
Inclination:       51
6460  deg
RA of node:       121
3098  deg
Eccentricity:     
0009932     
Arg of perigee:    52
3105  deg
Mean anomaly:     307
8957  deg
Mean motion:   15
72294006  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2683
Checksum:              320


Coasting Arc #8 (Orbit 2698)
---------------------------------------

Vector Time (GMT): 2010/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4726836
39                 A    =         6729393
87  meter
 Y    =        2268395
98  meter          E    =           
0018272
 Z    =        4201364
74                 I    =           51
94600
 XDOT =         35
437215                 Wp   =           81
59127
 YDOT =      -6770
849931  meter/sec      RA   =          115
51342  deg
 ZDOT =       3684
670170                 TA   =          330
98286
                                          MA   =          331
08431
                                          Ha   =            196
227  n
mi
                                          Hp   =            183
178

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15507993
40                 X    =        -4772260
07
 Y    =        7442244
03  feet           Y    =         2215282
87  meter
 Z    =       13784005
04                 Z    =         4178291
98
 XDOT =        116
263828                 XDOT =          93
248079
 YDOT =     -22214
074578  feet/sec       YDOT =       -6770
131137  meter/sec
 ZDOT =      12088
812895                 ZDOT =        3684
981417

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11573267
91                 X    =         3527532
06
 Y    =       12824875
06  feet           Y    =         3909021
92  meter
 Z    =       13691811
43                 Z    =         4173264
12
 XDOT =     -20371
783118                 XDOT =       -6209
319494
 YDOT =       5437
895886  feet/sec       YDOT =        1657
470666  meter/sec
 ZDOT =      12090
032410                 ZDOT =        3685
041879


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   10190
55433211  
00016717  00000-0  10270-3 0  9079
2 25544  51
6464 116
1016 0009875  56
4211 303
7893 15
72315209 26996


Satellite: ISS
Catalog Number: 25544
Epoch time:      10190
55433211   =   yrday
fracday
Element set:     907
Inclination:       51
6464  deg
RA of node:       116
1016  deg
Eccentricity:     
0009875     
Arg of perigee:    56
4211  deg
Mean anomaly:     303
7893  deg
Mean motion:   15
72315209  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2699
Checksum:              299


Coasting Arc #9 (Orbit 2713)
---------------------------------------

Vector Time (GMT): 2010/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         969856
55                 A    =         6731176
17  meter
 Y    =        5580786
41  meter          E    =           
0014614
 Z    =       -3644701
26                 I    =           51
96496
 XDOT =      -5067
636051                 Wp   =           74
05752
 YDOT =       3746
604763  meter/sec      RA   =          110
36263  deg
 ZDOT =       4406
764369                 TA   =          242
54963
                                          MA   =          242
69831
                                          Ha   =            196
126  n
mi
                                          Hp   =            183
080

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3181944
06                 X    =          925084
21
 Y    =       18309666
72  feet           Y    =         5591382
32  meter
 Z    =      -11957681
30                 Z    =        -3640097
39
 XDOT =     -16626
102529                 XDOT =       -5130
561665
 YDOT =      12292
010378  feet/sec       YDOT =        3689
582724  meter/sec
 ZDOT =      14457
888351                 ZDOT =        4381
993943

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16479582
01                 X    =         5022976
60
 Y    =       -8615803
68  feet           Y    =        -2626096
96  meter
 Z    =      -11939267
53                 Z    =        -3639088
74
 XDOT =      16126
438919                 XDOT =        4915
338582
 YDOT =      11031
561574  feet/sec       YDOT =        3362
419968  meter/sec
 ZDOT =      14358
899275                 ZDOT =        4376
592499


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   10191
50769539  
00016717  00000-0  10270-3 0  9081
2 25544  51
6470 111
2186 0009897  59
5828 300
6311 15
72333874 27146


Satellite: ISS
Catalog Number: 25544
Epoch time:      10191
50769539   =   yrday
fracday
Element set:     908
Inclination:       51
6470  deg
RA of node:       111
2186  deg
Eccentricity:     
0009897     
Arg of perigee:    59
5828  deg
Mean anomaly:     300
6311  deg
Mean motion:   15
72333874  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2714
Checksum:              321


Coasting Arc #10 (Orbit 2729)
---------------------------------------

Vector Time (GMT): 2010/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3973331
19                 A    =         6731644
50  meter
 Y    =       -4179452
70  meter          E    =           
0014687
 Z    =       -3489292
46                 I    =           51
97711
 XDOT =       2110
950058                 Wp   =           71
07605
 YDOT =       5809
963087  meter/sec      RA   =          105
31445  deg
 ZDOT =      -4566
267345                 TA   =          150
00721
                                          MA   =          149
92299
                                          Ha   =            196
119  n
mi
                                          Hp   =            183
027

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13035863
48                 X    =         4036721
35
 Y    =      -13712115
15  feet           Y    =        -4134665
45  meter
 Z    =      -11447809
89                 Z    =        -3469837
13
 XDOT =       6925
689167                 XDOT =        2068
006839
 YDOT =      19061
558686  feet/sec       YDOT =        5833
329734  meter/sec
 ZDOT =     -14981
192076                 ZDOT =       -4556
115738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17163544
02                 X    =        -5231448
22
 Y    =       -8071112
67  feet           Y    =        -2460075
14  meter
 Z    =      -11370052
18                 Z    =        -3465591
90
 XDOT =      15258
865484                 XDOT =        4650
902199
 YDOT =     -11452
032586  feet/sec       YDOT =       -3490
579532  meter/sec
 ZDOT =     -14940
604595                 ZDOT =       -4553
896280


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   10192
52460270  
00016717  00000-0  10270-3 0  9095
2 25544  51
6480 106
0099 0009915  63
1408 297
0767 15
72360052 27308


Satellite: ISS
Catalog Number: 25544
Epoch time:      10192
52460270   =   yrday
fracday
Element set:     909
Inclination:       51
6480  deg
RA of node:       106
0099  deg
Eccentricity:     
0009915     
Arg of perigee:    63
1408  deg
Mean anomaly:     297
0767  deg
Mean motion:   15
72360052  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2730
Checksum:              297


Coasting Arc #11 (Orbit 2745)
---------------------------------------

Vector Time (GMT): 2010/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2634191
23                 A    =         6728771
04  meter
 Y    =       -4429153
38  meter          E    =           
0019621
 Z    =        4315213
84                 I    =           51
97394
 XDOT =       3810
572854                 Wp   =           69
17296
 YDOT =      -5703
963333  meter/sec      RA   =          100
16588  deg
 ZDOT =      -3508
879335                 TA   =           56
23853
                                          MA   =           56
05176
                                          Ha   =            196
181  n
mi
                                          Hp   =            182
885

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8642359
68                 X    =        -2605429
94
 Y    =      -14531343
11  feet           Y    =        -4458450
37  meter
 Z    =       14157525
71                 Z    =         4302486
34
 XDOT =      12501
879441                 XDOT =        3891
117547
 YDOT =     -18713
790461  feet/sec       YDOT =       -5660
900313  meter/sec
 ZDOT =     -11512
071309                 ZDOT =       -3490
173240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10784815
17                 X    =        -3287211
66
 Y    =       13075790
27  feet           Y    =         3985500
88  meter
 Z    =       14106640
92                 Z    =         4299704
15
 XDOT =     -20883
039520                 XDOT =       -6365
150446
 YDOT =      -4815
731374  feet/sec       YDOT =       -1467
834923  meter/sec
 ZDOT =     -11437
301264                 ZDOT =       -3486
089425


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   10193
54149693  
00016717  00000-0  10270-3 0  9103
2 25544  51
6475 100
8015 0009898  66
7693 293
4510 15
72373151 27464


Satellite: ISS
Catalog Number: 25544
Epoch time:      10193
54149693   =   yrday
fracday
Element set:     910
Inclination:       51
6475  deg
RA of node:       100
8015  deg
Eccentricity:     
0009898     
Arg of perigee:    66
7693  deg
Mean anomaly:     293
4510  deg
Mean motion:   15
72373151  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2746
Checksum:              321


Coasting Arc #12 (Orbit 2761)
---------------------------------------

Vector Time (GMT): 2010/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2546998
69                 A    =         6733894
79  meter
 Y    =        5651146
65  meter          E    =           
0023614
 Z    =        2601985
38                 I    =           51
99584
 XDOT =      -3774
536514                 Wp   =           74
11727
 YDOT =      -4149
588999  meter/sec      RA   =           95
11333  deg
 ZDOT =       5284
538091                 TA   =          315
30248
                                          MA   =          315
49256
                                          Ha   =            196
176  n
mi
                                          Hp   =            182
822

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8356294
93                 X    =        -2622641
24
 Y    =       18540507
37  feet           Y    =         5622241
30  meter
 Z    =        8536697
46                 Z    =         2589429
36
 XDOT =     -12383
649981                 XDOT =       -3753
525285
 YDOT =     -13614
137137  feet/sec       YDOT =       -4191
681343  meter/sec
 ZDOT =      17337
723397                 ZDOT =        5266
252277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20310341
12                 X    =         6190591
97
 Y    =        1386548
41  feet           Y    =          422619
96  meter
 Z    =        8486507
47                 Z    =         2586687
48
 XDOT =      -8282
030432                 XDOT =       -2524
362876
 YDOT =      14979
573225  feet/sec       YDOT =        4565
773919  meter/sec
 ZDOT =      17264
614584                 ZDOT =        5262
254525


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   10194
55837774  
00016717  00000-0  10270-3 0  9110
2 25544  51
6480  95
5925 0009897  70
3330 289
8899 15
72378954 27621


Satellite: ISS
Catalog Number: 25544
Epoch time:      10194
55837774   =   yrday
fracday
Element set:     911
Inclination:       51
6480  deg
RA of node:        95
5925  deg
Eccentricity:     
0009897     
Arg of perigee:    70
3330  deg
Mean anomaly:     289
8899  deg
Mean motion:   15
72378954  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2762
Checksum:              365


Coasting Arc #13 (Orbit 2776)
---------------------------------------

Vector Time (GMT): 2010/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3796937
09                 A    =         6726603
72  meter
 Y    =        2729070
33  meter          E    =           
0020743
 Z    =       -4853585
49                 I    =           51
97345
 XDOT =      -1917
800818                 Wp   =           92
30486
 YDOT =       7022
589527  meter/sec      RA   =           89
97319  deg
 ZDOT =       2456
531532                 TA   =          201
59854
                                          MA   =          201
68616
                                          Ha   =            196
061  n
mi
                                          Hp   =            182
854

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12457142
69                 X    =         3789715
29
 Y    =        8953642
83  feet           Y    =         2771490
09  meter
 Z    =      -15923836
89                 Z    =        -4835157
59
 XDOT =      -6291
997433                 XDOT =       -2008
119299
 YDOT =      23039
991885  feet/sec       YDOT =        7000
638275  meter/sec
 ZDOT =       8059
486653                 ZDOT =        2446
996408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3737873
20                 X    =         1139303
75
 Y    =      -14957187
80  feet           Y    =        -4558950
84  meter
 Z    =      -15850159
07                 Z    =        -4831128
48
 XDOT =      22671
132452                 XDOT =        6910
161171
 YDOT =      -2806
128746  feet/sec       YDOT =        -855
308042  meter/sec
 ZDOT =       8021
371591                 ZDOT =        2444
914061


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   10195
51169001  
00016717  00000-0  10270-3 0  9129
2 25544  51
6483  90
7090 0009762  73
5764 286
6470 15
72413283 27772


Satellite: ISS
Catalog Number: 25544
Epoch time:      10195
51169001   =   yrday
fracday
Element set:     912
Inclination:       51
6483  deg
RA of node:        90
7090  deg
Eccentricity:     
0009762     
Arg of perigee:    73
5764  deg
Mean anomaly:     286
6470  deg
Mean motion:   15
72413283  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2777
Checksum:              315


Coasting Arc #14 (Orbit 2792)
---------------------------------------

Vector Time (GMT): 2010/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         756685
33                 A    =         6735474
55  meter
 Y    =       -6473731
79  meter          E    =           
0014724
 Z    =       -1700176
34                 I    =           52
00204
 XDOT =       4688
383721                 Wp   =          106
12634
 YDOT =       2045
099572  meter/sec      RA   =           84
90845  deg
 ZDOT =      -5745
294667                 TA   =           92
55460
                                          MA   =           92
38604
                                          Ha   =            196
046  n
mi
                                          Hp   =            182
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2482563
42                 X    =          837278
55
 Y    =      -21239277
53  feet           Y    =        -6464819
32  meter
 Z    =       -5578006
38                 Z    =        -1696305
24
 XDOT =      15381
836354                 XDOT =        4693
075736
 YDOT =       6709
644265  feet/sec       YDOT =        2097
554617  meter/sec
 ZDOT =     -18849
391953                 ZDOT =       -5722
507296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20589799
25                 X    =        -6275770
81
 Y    =        5788142
65  feet           Y    =         1764225
88  meter
 Z    =       -5562531
60                 Z    =        -1695459
63
 XDOT =        704
437489                 XDOT =         214
712547
 YDOT =     -15379
528847  feet/sec       YDOT =       -4687
680393  meter/sec
 ZDOT =     -18758
284335                 ZDOT =       -5717
525065


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   10196
52854459  
00016717  00000-0  10270-3 0  9130
2 25544  51
6482  85
4994 0009628  78
0490 282
1751 15
72401553 27930


Satellite: ISS
Catalog Number: 25544
Epoch time:      10196
52854459   =   yrday
fracday
Element set:     913
Inclination:       51
6482  deg
RA of node:        85
4994  deg
Eccentricity:     
0009628     
Arg of perigee:    78
0490  deg
Mean anomaly:     282
1751  deg
Mean motion:   15
72401553  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2793
Checksum:              334


Coasting Arc #15 (Orbit 2808)
---------------------------------------

Vector Time (GMT): 2010/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4237377
00                 A    =         6725008
36  meter
 Y    =        -786956
27  meter          E    =           
0013692
 Z    =        5152160
74                 I    =           51
96373
 XDOT =       -273
051149                 Wp   =           72
29301
 YDOT =      -7579
263189  meter/sec      RA   =           79
78173  deg
 ZDOT =      -1375
204093                 TA   =           30
83975
                                          MA   =           30
75939
                                          Ha   =            196
033  n
mi
                                          Hp   =            182
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13902155
51                 X    =        -4253290
15
 Y    =       -2581877
52  feet           Y    =         -834430
55  meter
 Z    =       16903414
49                 Z    =         5131537
08
 XDOT =       -895
837102                 XDOT =        -181
597740
 YDOT =     -24866
349046  feet/sec       YDOT =       -7581
805154  meter/sec
 ZDOT =      -4511
824452                 ZDOT =       -1376
309045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3201877
64                 X    =          975932
30
 Y    =       13873167
83  feet           Y    =         4228541
55  meter
 Z    =       16820958
21                 Z    =         5127028
06
 XDOT =     -21456
763515                 XDOT =       -6540
021519
 YDOT =      10456
160399  feet/sec       YDOT =        3187
037690  meter/sec
 ZDOT =      -4516
237454                 ZDOT =       -1376
549176


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   10197
54538350  
00016717  00000-0  10270-3 0  9143
2 25544  51
6482  80
2899 0009583  80
6405 279
5840 15
72494578 28098


Satellite: ISS
Catalog Number: 25544
Epoch time:      10197
54538350   =   yrday
fracday
Element set:     914
Inclination:       51
6482  deg
RA of node:        80
2899  deg
Eccentricity:     
0009583     
Arg of perigee:    80
6405  deg
Mean anomaly:     279
5840  deg
Mean motion:   15
72494578  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2809
Checksum:              345

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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