Date: May 28th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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


156/03:21:57 281 -1 7 13 1 13 1
N/A -11 0 -0 0 191 1
000/00:03:54 562 -7 0 0 1 187 2

158/23:59:56 236 -0 7 2 6 2 6
N/A -2 2 0 0 191 3
000/00:09:52 473 -1 3 0 2 188 3

159/01:30:56 147 -0 8 2 7 2 7
N/A -2 2 -0 0 191 3
000/00:09:52 294 -1 3 0 2 189 6

Coasting Arc #1 (Orbit 2007)
---------------------------------------

Vector Time (GMT): 2010/146/14:12:41
884
Vector Time (MET): N/A
Weight (LBS)     : 816195
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4872490
23                 A    =         6721869
78  meter
 Y    =        1866051
61  meter          E    =           
0009424
 Z    =        4227895
31                 I    =           51
52828
 XDOT =      -4921
882656                 Wp   =           53
20445
 YDOT =       4724
140101  meter/sec      RA   =          340
87238  deg
 ZDOT =       3587
271921                 TA   =             
32233
                                          MA   =             
32172
                                          Ha   =            190
185  n
mi
                                          Hp   =            182
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15985860
35                 X    =         4830722
84
 Y    =        6122216
56  feet           Y    =         1920304
58  meter
 Z    =       13871047
61                 Z    =         4251465
11
 XDOT =     -16147
908976                 XDOT =       -4991
769671
 YDOT =      15499
147312  feet/sec       YDOT =        4668
709428  meter/sec
 ZDOT =      11769
264832                 ZDOT =        3563
191860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4299992
07                 X    =         1310637
58
 Y    =      -16490199
07  feet           Y    =        -5026212
68  meter
 Z    =       13964907
13                 Z    =         4256503
69
 XDOT =      16018
347440                 XDOT =        4882
392300
 YDOT =      14062
469218  feet/sec       YDOT =        4286
240618  meter/sec
 ZDOT =      11673
339437                 ZDOT =        3558
033860


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   10146
64612078  
00016717  00000-0  10270-3 0  9003
2 25544  51
6443 341
0903 0008781 347
9131  12
1821 15
74844372 20087


Satellite: ISS
Catalog Number: 25544
Epoch time:      10146
64612078   =   yrday
fracday
Element set:     900
Inclination:       51
6443  deg
RA of node:       341
0903  deg
Eccentricity:     
0008781     
Arg of perigee:   347
9131  deg
Mean anomaly:      12
1821  deg
Mean motion:   15
74844372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2008
Checksum:              284


Coasting Arc #2 (Orbit 2022)
---------------------------------------

Vector Time (GMT): 2010/147/14:12:41
884
Vector Time (MET): N/A
Weight (LBS)     : 816195
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4168506
99                 A    =         6726170
90  meter
 Y    =       -4408110
09  meter          E    =           
0011113
 Z    =       -2892573
64                 I    =           51
51542
 XDOT =       5505
042471                 Wp   =           15
26977
 YDOT =       1908
446005  meter/sec      RA   =          335
67367  deg
 ZDOT =       5039
911457                 TA   =          311
37747
                                          MA   =          311
47297
                                          Ha   =            190
466  n
mi
                                          Hp   =            182
094

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13676204
04                 X    =         4231541
28
 Y    =      -14462303
44  feet           Y    =        -4361142
47  meter
 Z    =       -9490071
01                 Z    =        -2872170
30
 XDOT =      18061
162961                 XDOT =        5458
809374
 YDOT =       6261
305791  feet/sec       YDOT =        1969
747372  meter/sec
 ZDOT =      16535
142575                 ZDOT =        5066
543373

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16116154
86                 X    =        -4912204
00
 Y    =      -11747447
68  feet           Y    =        -3580622
05  meter
 Z    =       -9408785
86                 Z    =        -2867797
93
 XDOT =       3030
874689                 XDOT =         923
810605
 YDOT =     -17446
775330  feet/sec       YDOT =       -5317
777121  meter/sec
 ZDOT =      16641
197763                 ZDOT =        5072
237078


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   10147
59795867  
00016717  00000-0  10270-3 0  9017
2 25544  51
6454 336
1967 0008748 352
4715   7
6316 15
74849896 20237


Satellite: ISS
Catalog Number: 25544
Epoch time:      10147
59795867   =   yrday
fracday
Element set:     901
Inclination:       51
6454  deg
RA of node:       336
1967  deg
Eccentricity:     
0008748     
Arg of perigee:   352
4715  deg
Mean anomaly:       7
6316  deg
Mean motion:   15
74849896  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2023
Checksum:              348


Coasting Arc #3 (Orbit 2038)
---------------------------------------

Vector Time (GMT): 2010/148/14:12:41
884
Vector Time (MET): N/A
Weight (LBS)     : 816195
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4709778
35                 A    =         6720503
74  meter
 Y    =       -1514328
93  meter          E    =           
0015488
 Z    =       -4562683
92                 I    =           51
47006
 XDOT =       4633
581009                 Wp   =           36
33116
 YDOT =      -5355
645864  meter/sec      RA   =          330
56820  deg
 ZDOT =      -2998
369799                 TA   =          203
73956
                                          MA   =          203
81108
                                          Ha   =            190
517  n
mi
                                          Hp   =            181
659

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15452028
69                 X    =        -4670329
86
 Y    =       -4968270
76  feet           Y    =        -1566775
13  meter
 Z    =      -14969435
43                 Z    =        -4585468
73
 XDOT =      15202
037432                 XDOT =        4707
690131
 YDOT =     -17571
016613  feet/sec       YDOT =       -5303
415525  meter/sec
 ZDOT =      -9837
171257                 ZDOT =       -2975
680499

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2667776
49                 X    =         -813138
27
 Y    =       15925044
39  feet           Y    =         4853953
53  meter
 Z    =      -15060173
70                 Z    =        -4590340
94
 XDOT =     -18453
360773                 XDOT =       -5624
584364
 YDOT =     -12330
601305  feet/sec       YDOT =       -3758
367278  meter/sec
 ZDOT =      -9746
772080                 ZDOT =       -2970
816130


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   10148
61323404  
00016717  00000-0  10270-3 0  9026
2 25544  51
6457 330
9771 0008861 356
5270   3
5830 15
74888389 20395


Satellite: ISS
Catalog Number: 25544
Epoch time:      10148
61323404   =   yrday
fracday
Element set:     902
Inclination:       51
6457  deg
RA of node:       330
9771  deg
Eccentricity:     
0008861     
Arg of perigee:   356
5270  deg
Mean anomaly:       3
5830  deg
Mean motion:   15
74888389  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2039
Checksum:              315


Coasting Arc #4 (Orbit 2054)
---------------------------------------

Vector Time (GMT): 2010/149/14:12:41
884
Vector Time (MET): N/A
Weight (LBS)     : 816195
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3908741
81                 A    =         6727320
11  meter
 Y    =        4953701
21  meter          E    =           
0014099
 Z    =        2329045
95                 I    =           51
46660
 XDOT =      -5254
338397                 Wp   =           70
38039
 YDOT =      -1594
131102  meter/sec      RA   =          325
36967  deg
 ZDOT =      -5396
415229                 TA   =           83
34624
                                          MA   =           83
18579
                                          Ha   =            190
613  n
mi
                                          Hp   =            181
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12823956
06                 X    =        -3975158
64
 Y    =       16252300
57  feet           Y    =         4909619
57  meter
 Z    =        7641226
87                 Z    =         2309896
69
 XDOT =     -17238
643036                 XDOT =       -5209
907033
 YDOT =      -5230
088917  feet/sec       YDOT =       -1652
638864  meter/sec
 ZDOT =     -17704
774374                 ZDOT =       -5421
833342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18135685
86                 X    =         5527757
05
 Y    =       10042322
72  feet           Y    =         3060899
96  meter
 Z    =        7564927
21                 Z    =         2305789
82
 XDOT =      -1630
459047                 XDOT =        -496
963917
 YDOT =      16435
544844  feet/sec       YDOT =        5009
554069  meter/sec
 ZDOT =     -17806
004258                 ZDOT =       -5427
270098


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   10149
62849197  
00016717  00000-0  10270-3 0  9031
2 25544  51
6452 325
7557 0008806 359
7879    
3279 15
74894962 20557


Satellite: ISS
Catalog Number: 25544
Epoch time:      10149
62849197   =   yrday
fracday
Element set:     903
Inclination:       51
6452  deg
RA of node:       325
7557  deg
Eccentricity:     
0008806     
Arg of perigee:   359
7879  deg
Mean anomaly:        
3279  deg
Mean motion:   15
74894962  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2055
Checksum:              352


Coasting Arc #5 (Orbit 2070)
---------------------------------------

Vector Time (GMT): 2010/150/14:12:41
884
Vector Time (MET): N/A
Weight (LBS)     : 816195
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4469286
82                 A    =         6719108
28  meter
 Y    =        1303173
30  meter          E    =           
0008075
 Z    =        4837819
84                 I    =           51
41680
 XDOT =      -4269
940049                 Wp   =           48
71132
 YDOT =       5976
456860  meter/sec      RA   =          320
25246  deg
 ZDOT =       2337
511842                 TA   =           18
47687
                                          MA   =           18
44756
                                          Ha   =            190
485  n
mi
                                          Hp   =            181
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14663014
51                 X    =         4430881
02
 Y    =        4275502
96  feet           Y    =         1352935
96  meter
 Z    =       15872112
33                 Z    =         4859438
63
 XDOT =     -14008
989661                 XDOT =       -4347
807753
 YDOT =      19607
798098  feet/sec       YDOT =        5928
272065  meter/sec
 ZDOT =       7669
002106                 ZDOT =        2316
580302

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1580186
25                 X    =          481640
77
 Y    =      -15101199
79  feet           Y    =        -4602845
70  meter
 Z    =       15958215
63                 Z    =         4864064
12
 XDOT =      20718
702844                 XDOT =        6315
060627
 YDOT =      10174
659876  feet/sec       YDOT =        3101
236330  meter/sec
 ZDOT =       7585
597795                 ZDOT =        2312
090208


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   10150
64373081  
00016717  00000-0  10270-3 0  9040
2 25544  51
6465 320
5354 0008852   2
9057 357
2156 15
74962959 20713


Satellite: ISS
Catalog Number: 25544
Epoch time:      10150
64373081   =   yrday
fracday
Element set:     904
Inclination:       51
6465  deg
RA of node:       320
5354  deg
Eccentricity:     
0008852     
Arg of perigee:     2
9057  deg
Mean anomaly:     357
2156  deg
Mean motion:   15
74962959  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2071
Checksum:              307


Coasting Arc #6 (Orbit 2085)
---------------------------------------

Vector Time (GMT): 2010/151/14:12:41
884
Vector Time (MET): N/A
Weight (LBS)     : 816195
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3509140
83                 A    =         6728177
75  meter
 Y    =       -5460812
76  meter          E    =           
0016030
 Z    =       -1738691
52                 I    =           51
42547
 XDOT =       5004
099873                 Wp   =           20
93274
 YDOT =       1414
631455  meter/sec      RA   =          315
06029  deg
 ZDOT =       5687
400814                 TA   =          319
74080
                                          MA   =          319
85940
                                          Ha   =            190
781  n
mi
                                          Hp   =            181
148

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11512929
25                 X    =         3578390
06
 Y    =      -17916052
35  feet           Y    =        -5421183
98  meter
 Z    =       -5704368
51                 Z    =        -1721476
79
 XDOT =      16417
650502                 XDOT =        4960
280946
 YDOT =       4641
179313  feet/sec       YDOT =        1470
344362  meter/sec
 ZDOT =      18659
451491                 ZDOT =        5711
604513

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19840751
83                 X    =        -6047461
16
 Y    =       -7788126
18  feet           Y    =        -2373820
86  meter
 Z    =       -5635774
07                 Z    =        -1717783
94
 XDOT =        768
229286                 XDOT =         234
156286
 YDOT =     -15455
483550  feet/sec       YDOT =       -4710
831386  meter/sec
 ZDOT =      18755
854757                 ZDOT =        5716
784530


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   10151
59550313  
00016717  00000-0  10270-3 0  9051
2 25544  51
6474 315
6421 0008960   7
1847 352
9443 15
74953001 20862


Satellite: ISS
Catalog Number: 25544
Epoch time:      10151
59550313   =   yrday
fracday
Element set:     905
Inclination:       51
6474  deg
RA of node:       315
6421  deg
Eccentricity:     
0008960     
Arg of perigee:     7
1847  deg
Mean anomaly:     352
9443  deg
Mean motion:   15
74953001  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2086
Checksum:              297


Coasting Arc #7 (Orbit 2101)
---------------------------------------

Vector Time (GMT): 2010/152/14:12:41
884
Vector Time (MET): N/A
Weight (LBS)     : 816195
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4259117
72                 A    =         6718116
65  meter
 Y    =       -1219009
83  meter          E    =           
0019115
 Z    =       -5066199
32                 I    =           51
37153
 XDOT =       3775
435492                 Wp   =           51
86517
 YDOT =      -6504
210452  meter/sec      RA   =          309
93071  deg
 ZDOT =      -1601
436863                 TA   =          202
63048
                                          MA   =          202
71488
                                          Ha   =            190
809  n
mi
                                          Hp   =            180
780

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13973483
33                 X    =        -4220559
36
 Y    =       -3999376
08  feet           Y    =        -1266421
50  meter
 Z    =      -16621388
85                 Z    =        -5086796
59
 XDOT =      12386
599383                 XDOT =        3855
665621
 YDOT =     -21339
273137  feet/sec       YDOT =       -6461
542464  meter/sec
 ZDOT =      -5254
057948                 ZDOT =       -1582
901889

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -938572
04                 X    =         -286076
76
 Y    =       14409659
19  feet           Y    =         4392064
12  meter
 Z    =      -16703431
31                 Z    =        -5091205
86
 XDOT =     -22451
305326                 XDOT =       -6843
157863
 YDOT =      -7495
652494  feet/sec       YDOT =       -2284
674880  meter/sec
 ZDOT =      -5180
205652                 ZDOT =       -1578
926683


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   10152
61070836  
00016717  00000-0  10270-3 0  9063
2 25544  51
6476 310
4225 0009021  10
5546 349
5805 15
74989203 21028


Satellite: ISS
Catalog Number: 25544
Epoch time:      10152
61070836   =   yrday
fracday
Element set:     906
Inclination:       51
6476  deg
RA of node:       310
4225  deg
Eccentricity:     
0009021     
Arg of perigee:    10
5546  deg
Mean anomaly:     349
5805  deg
Mean motion:   15
74989203  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2102
Checksum:              285


Coasting Arc #8 (Orbit 2117)
---------------------------------------

Vector Time (GMT): 2010/153/14:12:41
884
Vector Time (MET): N/A
Weight (LBS)     : 816195
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3075406
08                 A    =         6728838
34  meter
 Y    =        5892425
02  meter          E    =           
0013678
 Z    =        1040891
41                 I    =           51
38937
 XDOT =      -4742
431896                 Wp   =           85
46578
 YDOT =      -1422
013440  meter/sec      RA   =          304
74551  deg
 ZDOT =      -5894
448890                 TA   =           83
11430
                                          MA   =           82
95871
                                          Ha   =            190
885  n
mi
                                          Hp   =            180
730

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10089914
97                 X    =        -3146124
12
 Y    =       19332103
08  feet           Y    =         5857638
46  meter
 Z    =        3414998
05                 Z    =         1025780
08
 XDOT =     -15559
159764                 XDOT =       -4697
544111
 YDOT =      -4665
398425  feet/sec       YDOT =       -1474
794415  meter/sec
 ZDOT =     -19338
743079                 ZDOT =       -5917
378726

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21143234
21                 X    =         6444457
79
 Y    =        5376599
67  feet           Y    =         1638787
58  meter
 Z    =        3354791
85                 Z    =         1022540
56
 XDOT =       -584
478541                 XDOT =        -178
149059
 YDOT =      14562
829683  feet/sec       YDOT =        4438
750487  meter/sec
 ZDOT =     -19430
079610                 ZDOT =       -5922
288265


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   10153
62589586  
00016717  00000-0  10270-3 0  9073
2 25544  51
6476 305
2016 0008995  14
4978 345
6442 15
75013043 21181


Satellite: ISS
Catalog Number: 25544
Epoch time:      10153
62589586   =   yrday
fracday
Element set:     907
Inclination:       51
6476  deg
RA of node:       305
2016  deg
Eccentricity:     
0008995     
Arg of perigee:    14
4978  deg
Mean anomaly:     345
6442  deg
Mean motion:   15
75013043  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2118
Checksum:              318


Coasting Arc #9 (Orbit 2133)
---------------------------------------

Vector Time (GMT): 2010/154/14:12:41
884
Vector Time (MET): N/A
Weight (LBS)     : 816195
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4049373
52                 A    =         6717203
16  meter
 Y    =        1289573
15  meter          E    =           
0009007
 Z    =        5196453
96                 I    =           51
33529
 XDOT =      -3223
383855                 Wp   =           37
24662
 YDOT =       6956
907944  meter/sec      RA   =          299
59941  deg
 ZDOT =        791
753373                 TA   =           45
23082
                                          MA   =           45
15758
                                          Ha   =            190
776  n
mi
                                          Hp   =            180
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13285346
20                 X    =         4009408
90
 Y    =        4230883
04  feet           Y    =         1334631
63  meter
 Z    =       17048733
45                 Z    =         5216028
87
 XDOT =     -10575
406350                 XDOT =       -3304
783880
 YDOT =      22824
501129  feet/sec       YDOT =        6920
406926  meter/sec
 ZDOT =       2597
616053                 ZDOT =         775
897234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         837568
48                 X    =          255290
87
 Y    =      -13821520
93  feet           Y    =        -4212799
58  meter
 Z    =       17126708
55                 Z    =         5220220
76
 XDOT =      23727
417790                 XDOT =        7232
116942
 YDOT =       4552
623858  feet/sec       YDOT =        1387
639752  meter/sec
 ZDOT =       2534
449184                 ZDOT =         772
500111


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   10154
64106381  
00016717  00000-0  10270-3 0  9085
2 25544  51
6483 299
9812 0009098  17
6170 342
5308 15
75080213 21344


Satellite: ISS
Catalog Number: 25544
Epoch time:      10154
64106381   =   yrday
fracday
Element set:     908
Inclination:       51
6483  deg
RA of node:       299
9812  deg
Eccentricity:     
0009098     
Arg of perigee:    17
6170  deg
Mean anomaly:     342
5308  deg
Mean motion:   15
75080213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2134
Checksum:              303


Coasting Arc #10 (Orbit 2148)
---------------------------------------

Vector Time (GMT): 2010/155/14:12:41
884
Vector Time (MET): N/A
Weight (LBS)     : 816195
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2527402
99                 A    =         6729137
21  meter
 Y    =       -6215404
91  meter          E    =           
0020531
 Z    =        -336476
02                 I    =           51
36138
 XDOT =       4574
619133                 Wp   =           33
04616
 YDOT =       1545
075944  meter/sec      RA   =          294
42590  deg
 ZDOT =       6009
666338                 TA   =          323
27742
                                          MA   =          323
41793
                                          Ha   =            191
062  n
mi
                                          Hp   =            180
265

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8292004
57                 X    =         2598351
47
 Y    =      -20391748
40  feet           Y    =        -6186745
26  meter
 Z    =       -1103923
94                 Z    =         -324026
16
 XDOT =      15008
592955                 XDOT =        4527
807879
 YDOT =       5069
146799  feet/sec       YDOT =        1595
969713  meter/sec
 ZDOT =      19716
753079                 ZDOT =        6031
776344

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21859275
55                 X    =        -6662707
19
 Y    =       -2619130
41  feet           Y    =         -798310
95  meter
 Z    =       -1054333
45                 Z    =         -321360
83
 XDOT =        766
418220                 XDOT =         233
604273
 YDOT =     -14108
117545  feet/sec       YDOT =       -4300
154228  meter/sec
 ZDOT =      19804
828365                 ZDOT =        6036
511686


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   10155
59276972  
00016717  00000-0  10270-3 0  9095
2 25544  51
6484 295
0875 0009286  21
5345 338
6208 15
75054065 21495


Satellite: ISS
Catalog Number: 25544
Epoch time:      10155
59276972   =   yrday
fracday
Element set:     909
Inclination:       51
6484  deg
RA of node:       295
0875  deg
Eccentricity:     
0009286     
Arg of perigee:    21
5345  deg
Mean anomaly:     338
6208  deg
Mean motion:   15
75054065  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2149
Checksum:              334


Coasting Arc #11 (Orbit 2157)
---------------------------------------

Vector Time (GMT): 2010/156/03:23:54
562
Vector Time (MET): N/A
Weight (LBS)     : 815047
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4622558
76                 A    =         6728103
37  meter
 Y    =        2411476
41  meter          E    =           
0006484
 Z    =       -4259259
56                 I    =           51
32804
 XDOT =       -321
020737                 Wp   =           41
00816
 YDOT =      -6832
820039  meter/sec      RA   =          291
61937  deg
 ZDOT =      -3518
362793                 TA   =          193
12021
                                          MA   =          193
13708
                                          Ha   =            191
087  n
mi
                                          Hp   =            187
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15165875
20                 X    =        -4628489
97
 Y    =        7911668
00  feet           Y    =         2359751
46  meter
 Z    =      -13973948
69                 Z    =        -4281730
21
 XDOT =      -1053
217642                 XDOT =        -227
499409
 YDOT =     -22417
388578  feet/sec       YDOT =       -6835
886628  meter/sec
 ZDOT =     -11543
185015                 ZDOT =       -3519
695833

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14944251
12                 X    =        -4555007
74
 Y    =       -8170558
62  feet           Y    =        -2490386
27  meter
 Z    =      -14063457
37                 Z    =        -4286541
81
 XDOT =      17518
434664                 XDOT =        5339
618886
 YDOT =     -12154
116633  feet/sec       YDOT =       -3704
574750  meter/sec
 ZDOT =     -11548
502391                 ZDOT =       -3519
983529


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   10156
16380696  
00016717  00000-0  10270-3 0  9100
2 25544  51
6483 292
1546 0004230 296
0086  64
0641 15
72632503 21589


Satellite: ISS
Catalog Number: 25544
Epoch time:      10156
16380696   =   yrday
fracday
Element set:     910
Inclination:       51
6483  deg
RA of node:       292
1546  deg
Eccentricity:     
0004230     
Arg of perigee:   296
0086  deg
Mean anomaly:      64
0641  deg
Mean motion:   15
72632503  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2158
Checksum:              293


Coasting Arc #12 (Orbit 2173)
---------------------------------------

Vector Time (GMT): 2010/157/03:23:54
562
Vector Time (MET): N/A
Weight (LBS)     : 815047
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1172400
76                 A    =         6731008
45  meter
 Y    =        5679701
10  meter          E    =           
0009106
 Z    =        3411233
76                 I    =           51
32703
 XDOT =      -4921
228832                 Wp   =           75
66519
 YDOT =       3766
483775  meter/sec      RA   =          286
42191  deg
 ZDOT =      -4567
418851                 TA   =           63
83894
                                          MA   =           63
74531
                                          Ha   =            191
190  n
mi
                                          Hp   =            187
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3846459
19                 X    =         1092230
90
 Y    =       18634189
95  feet           Y    =         5692362
99  meter
 Z    =       11191711
79                 Z    =         3416735
16
 XDOT =     -16145
763884                 XDOT =       -4940
792709
 YDOT =      12357
230233  feet/sec       YDOT =        3711
342730  meter/sec
 ZDOT =     -14984
969985                 ZDOT =       -4591
373515

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13182270
01                 X    =        -4017955
90
 Y    =       13702729
32  feet           Y    =         4176591
90  meter
 Z    =       11213637
37                 Z    =         3417916
67
 XDOT =     -18294
426733                 XDOT =       -5576
141268
 YDOT =      -5225
280760  feet/sec       YDOT =       -1592
665576  meter/sec
 ZDOT =     -15080
385715                 ZDOT =       -4596
501566


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   10157
18052817  
00016717  00000-0  10270-3 0  9115
2 25544  51
6477 286
9446 0004209 300
1233  59
9512 15
72629752 21749


Satellite: ISS
Catalog Number: 25544
Epoch time:      10157
18052817   =   yrday
fracday
Element set:     911
Inclination:       51
6477  deg
RA of node:       286
9446  deg
Eccentricity:     
0004209     
Arg of perigee:   300
1233  deg
Mean anomaly:      59
9512  deg
Mean motion:   15
72629752  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2174
Checksum:              308


Coasting Arc #13 (Orbit 2189)
---------------------------------------

Vector Time (GMT): 2010/158/03:23:54
562
Vector Time (MET): N/A
Weight (LBS)     : 815047
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3841285
40                 A    =         6729996
01  meter
 Y    =       -4098146
32  meter          E    =           
0008194
 Z    =        3699073
85                 I    =           51
31706
 XDOT =       2281
413619                 Wp   =           81
61533
 YDOT =       5993
300261  meter/sec      RA   =          281
32516  deg
 ZDOT =       4263
889621                 TA   =          323
17967
                                          MA   =          323
23592
                                          Ha   =            191
188  n
mi
                                          Hp   =            187
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12602642
38                 X    =         3868856
48
 Y    =      -13445361
95  feet           Y    =        -4055037
02  meter
 Z    =       12136069
05                 Z    =         3717801
55
 XDOT =       7484
952817                 XDOT =        2193
512453
 YDOT =      19663
058599  feet/sec       YDOT =        6018
320448  meter/sec
 ZDOT =      13989
139177                 ZDOT =        4274
759985

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18227690
67                 X    =         5555800
12
 Y    =        2353630
56  feet           Y    =          717386
60  meter
 Z    =       12210660
96                 Z    =         3721809
46
 XDOT =     -11499
570798                 XDOT =       -3505
069179
 YDOT =      16141
638908  feet/sec       YDOT =        4919
971539  meter/sec
 ZDOT =      14032
456379                 ZDOT =        4277
092704


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   10158
19723303  
00016717  00000-0  10270-3 0  9123
2 25544  51
6482 281
7338 0004319 305
0780  54
9977 15
72652794 21901


Satellite: ISS
Catalog Number: 25544
Epoch time:      10158
19723303   =   yrday
fracday
Element set:     912
Inclination:       51
6482  deg
RA of node:       281
7338  deg
Eccentricity:     
0004319     
Arg of perigee:   305
0780  deg
Mean anomaly:      54
9977  deg
Mean motion:   15
72652794  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2190
Checksum:              318


Coasting Arc #14 (Orbit 2202)
---------------------------------------

Vector Time (GMT): 2010/159/00:04:52
473
Vector Time (MET): N/A
Weight (LBS)     : 814792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4165577
07                 A    =         6727080
54  meter
 Y    =        2123736
46  meter          E    =           
0008239
 Z    =       -4843938
48                 I    =           51
29673
 XDOT =       -998
831138                 Wp   =           53
32297
 YDOT =      -7263
727748  meter/sec      RA   =          276
87996  deg
 ZDOT =      -2323
581213                 TA   =          193
89085
                                          MA   =          193
91353
                                          Ha   =            191
286  n
mi
                                          Hp   =            188
315

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13666591
45                 X    =        -4165484
18
 Y    =        6967639
32  feet           Y    =         2077155
60  meter
 Z    =      -15892186
61                 Z    =        -4864174
65
 XDOT =      -3277
005045                 XDOT =        -906
244893
 YDOT =     -23831
127783  feet/sec       YDOT =       -7274
379317  meter/sec
 ZDOT =      -7623
297943                 ZDOT =       -2328
209579

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3662434
12                 X    =        -1116309
92
 Y    =      -14810191
39  feet           Y    =        -4514146
34  meter
 Z    =      -15972793
18                 Z    =        -4868507
36
 XDOT =      22856
431480                 XDOT =        6966
640315
 YDOT =       2596
884187  feet/sec       YDOT =         791
530300  meter/sec
 ZDOT =      -7641
755866                 ZDOT =       -2329
207188


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   10159
02329867  
00016717  00000-0  10270-3 0  9134
2 25544  51
6465 277
4997 0005242 285
1503  74
9079 15
72182968 22033


Satellite: ISS
Catalog Number: 25544
Epoch time:      10159
02329867   =   yrday
fracday
Element set:     913
Inclination:       51
6465  deg
RA of node:       277
4997  deg
Eccentricity:     
0005242     
Arg of perigee:   285
1503  deg
Mean anomaly:      74
9079  deg
Mean motion:   15
72182968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2203
Checksum:              331


Coasting Arc #15 (Orbit 2203)
---------------------------------------

Vector Time (GMT): 2010/159/01:35:52
294
Vector Time (MET): N/A
Weight (LBS)     : 814537
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4117367
11                 A    =         6728870
44  meter
 Y    =        2378144
90  meter          E    =           
0005734
 Z    =       -4766543
60                 I    =           51
29880
 XDOT =      -1212
974494                 Wp   =           51
72069
 YDOT =      -7164
066401  meter/sec      RA   =          276
55670  deg
 ZDOT =      -2525
108944                 TA   =          193
39749
                                          MA   =          193
41272
                                          Ha   =            191
280  n
mi
                                          Hp   =            189
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13508422
28                 X    =        -4120498
62
 Y    =        7802312
66  feet           Y    =         2332085
12  meter
 Z    =      -15638266
41                 Z    =        -4786553
37
 XDOT =      -3979
575113                 XDOT =       -1120
507765
 YDOT =     -23504
154858  feet/sec       YDOT =       -7177
113289  meter/sec
 ZDOT =      -8284
478164                 ZDOT =       -2530
777920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9915134
34                 X    =        -3022132
95
 Y    =      -11939197
94  feet           Y    =        -3639067
53  meter
 Z    =      -15717970
46                 Z    =        -4790837
40
 XDOT =      21658
774898                 XDOT =        6601
594589
 YDOT =      -7044
451144  feet/sec       YDOT =       -2147
148709  meter/sec
 ZDOT =      -8307
081323                 ZDOT =       -2531
998387


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   10159
08686648  
00016717  00000-0  10270-3 0  9144
2 25544  51
6477 277
1749 0006609 269
4422  90
5983 15
71669703 22046


Satellite: ISS
Catalog Number: 25544
Epoch time:      10159
08686648   =   yrday
fracday
Element set:     914
Inclination:       51
6477  deg
RA of node:       277
1749  deg
Eccentricity:     
0006609     
Arg of perigee:   269
4422  deg
Mean anomaly:      90
5983  deg
Mean motion:   15
71669703  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2204
Checksum:              344


Coasting Arc #16 (Orbit 2219)
---------------------------------------

Vector Time (GMT): 2010/160/01:35:52
294
Vector Time (MET): N/A
Weight (LBS)     : 814537
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2156957
55                 A    =         6735261
14  meter
 Y    =        5697822
73  meter          E    =           
0006845
 Z    =        2863673
11                 I    =           51
31767
 XDOT =      -4131
637071                 Wp   =          104
03394
 YDOT =       4099
497491  meter/sec      RA   =          271
37220  deg
 ZDOT =      -5036
291260                 TA   =           42
94579
                                          MA   =           42
89236
                                          Ha   =            191
325  n
mi
                                          Hp   =            189
800

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7076632
39                 X    =         2079171
74
 Y    =       18693644
12  feet           Y    =         5721507
78  meter
 Z    =        9395252
97                 Z    =         2873963
63
 XDOT =     -13555
239735                 XDOT =       -4152
705553
 YDOT =      13449
794918  feet/sec       YDOT =        4053
177980  meter/sec
 ZDOT =     -16523
265289                 ZDOT =       -5056
413657

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17098787
99                 X    =        -5211710
58
 Y    =       10314561
92  feet           Y    =         3143878
47  meter
 Z    =        9436264
99                 Z    =         2876173
57
 XDOT =     -14927
096467                 XDOT =       -4549
779003
 YDOT =      -9530
318190  feet/sec       YDOT =       -2904
840984  meter/sec
 ZDOT =     -16603
415342                 ZDOT =       -5060
720996


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   10160
10421245  
00016717  00000-0  10270-3 0  9150
2 25544  51
6474 271
9692 0006637 273
1395  86
9008 15
71658825 22202


Satellite: ISS
Catalog Number: 25544
Epoch time:      10160
10421245   =   yrday
fracday
Element set:     915
Inclination:       51
6474  deg
RA of node:       271
9692  deg
Eccentricity:     
0006637     
Arg of perigee:   273
1395  deg
Mean anomaly:      86
9008  deg
Mean motion:   15
71658825  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2220
Checksum:              306


Coasting Arc #17 (Orbit 2235)
---------------------------------------

Vector Time (GMT): 2010/161/01:35:52
294
Vector Time (MET): N/A
Weight (LBS)     : 814537
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2873346
56                 A    =         6731925
78  meter
 Y    =       -4626220
17  meter          E    =           
0004336
 Z    =        3954701
09                 I    =           51
30775
 XDOT =       3535
038620                 Wp   =          106
32436
 YDOT =       5578
476412  meter/sec      RA   =          266
28012  deg
 ZDOT =       3952
494466                 TA   =          302
51138
                                          MA   =          302
55327
                                          Ha   =            191
401  n
mi
                                          Hp   =            189
812

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9426990
03                 X    =         2905652
73
 Y    =      -15177887
71  feet           Y    =        -4593908
73  meter
 Z    =       12974741
12                 Z    =         3968737
72
 XDOT =      11597
895736                 XDOT =        3453
195567
 YDOT =      18302
087967  feet/sec       YDOT =        5617
549051  meter/sec
 ZDOT =      12967
501530                 ZDOT =        3969
470075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16736944
43                 X    =         5101420
66
 Y    =        6136547
67  feet           Y    =         1870419
73  meter
 Z    =       13030648
38                 Z    =         3971741
63
 XDOT =     -15190
574715                 XDOT =       -4630
087173
 YDOT =      13718
388199  feet/sec       YDOT =        4181
364723  meter/sec
 ZDOT =      13035
149405                 ZDOT =        3973
113539


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   10161
12154348  
00016717  00000-0  10270-3 0  9161
2 25544  51
6480 266
7629 0006667 278
1364  81
9042 15
71687200 22364


Satellite: ISS
Catalog Number: 25544
Epoch time:      10161
12154348   =   yrday
fracday
Element set:     916
Inclination:       51
6480  deg
RA of node:       266
7629  deg
Eccentricity:     
0006667     
Arg of perigee:   278
1364  deg
Mean anomaly:      81
9042  deg
Mean motion:   15
71687200  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2236
Checksum:              309

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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