Date: August 17th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 1513)
---------------------------------------

Vector Time (GMT): 2009/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -770577
05                 A    =         6721591
31  meter
 Y    =       -4223596
84  meter          E    =           
0013899
 Z    =       -5182229
90                 I    =           51
66183
 XDOT =       7606
143377                 Wp   =           48
58163
 YDOT =         22
972771  meter/sec      RA   =            6
99634  deg
 ZDOT =      -1142
680586                 TA   =          210
45980
                                          MA   =          210
54061
                                          Ha   =            191
342  n
mi
                                          Hp   =            185
123

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2528139
91                 X    =         -698116
50
 Y    =      -13856945
01  feet           Y    =        -4231808
35  meter
 Z    =      -17002066
60                 Z    =        -5185797
67
 XDOT =      24954
538639                 XDOT =        7610
872110
 YDOT =         75
369985  feet/sec       YDOT =         108
055654  meter/sec
 ZDOT =      -3748
952055                 ZDOT =       -1105
718522

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6557354
67                 X    =        -1998681
70
 Y    =       12446865
44  feet           Y    =         3793804
58  meter
 Z    =      -17016266
50                 Z    =        -5186558
03
 XDOT =     -18801
406867                 XDOT =       -5730
668813
 YDOT =     -14863
179935  feet/sec       YDOT =       -4530
297244  meter/sec
 ZDOT =      -3603
579970                 ZDOT =       -1098
371175


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   09226
51773491  
00010596  00000-0  82463-4 0  9006
2 25544  51
6400   7
3976 0007945 331
7541  28
3190 15
73618790 15140


Satellite: ISS
Catalog Number: 25544
Epoch time:      09226
51773491   =   yrday
fracday
Element set:     900
Inclination:       51
6400  deg
RA of node:         7
3976  deg
Eccentricity:     
0007945     
Arg of perigee:   331
7541  deg
Mean anomaly:      28
3190  deg
Mean motion:   15
73618790  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1514
Checksum:              306


Coasting Arc #2 (Orbit 1529)
---------------------------------------

Vector Time (GMT): 2009/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6608976
56                 A    =         6732779
64  meter
 Y    =         655261
96  meter          E    =           
0008080
 Z    =        1097422
51                 I    =           51
66920
 XDOT =      -1454
231130                 Wp   =           92
22353
 YDOT =      -4717
248823  meter/sec      RA   =            1
84454  deg
 ZDOT =      -5904
179403                 TA   =           75
78136
                                          MA   =           75
69163
                                          Ha   =            191
500  n
mi
                                          Hp   =            185
027

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21682993
96                 X    =        -6621143
67
 Y    =        2149809
59  feet           Y    =          581288
38  meter
 Z    =        3600467
57                 Z    =         1065286
80
 XDOT =      -4771
099509                 XDOT =       -1372
692699
 YDOT =     -15476
538133  feet/sec       YDOT =       -4733
054454  meter/sec
 ZDOT =     -19370
667332                 ZDOT =       -5911
046383

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18678665
55                 X    =         5693257
26
 Y    =       11259456
15  feet           Y    =         3431882
24  meter
 Z    =        3474100
68                 Z    =         1058905
89
 XDOT =      -4703
677608                 XDOT =       -1433
680935
 YDOT =      13827
061765  feet/sec       YDOT =        4214
488426  meter/sec
 ZDOT =     -19397
861105                 ZDOT =       -5912
468065


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   09227
53382142  
00010596  00000-0  82463-4 0  9019
2 25544  51
6396   2
1811 0008006 334
9357  25
1416 15
73615920 15300


Satellite: ISS
Catalog Number: 25544
Epoch time:      09227
53382142   =   yrday
fracday
Element set:     901
Inclination:       51
6396  deg
RA of node:         2
1811  deg
Eccentricity:     
0008006     
Arg of perigee:   334
9357  deg
Mean anomaly:      25
1416  deg
Mean motion:   15
73615920  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1530
Checksum:              279


Coasting Arc #3 (Orbit 1545)
---------------------------------------

Vector Time (GMT): 2009/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1759204
80                 A    =         6721665
54  meter
 Y    =        3970726
81  meter          E    =           
0005057
 Z    =        5128806
47                 I    =           51
60359
 XDOT =      -7424
474343                 Wp   =            5
52677
 YDOT =       1516
867579  meter/sec      RA   =          356
73337  deg
 ZDOT =       1377
102827                 TA   =           71
31319
                                          MA   =           71
25831
                                          Ha   =            191
572  n
mi
                                          Hp   =            184
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5771669
30                 X    =         1689758
18
 Y    =       13027318
92  feet           Y    =         3990010
50  meter
 Z    =       16826792
87                 Z    =         5137184
27
 XDOT =     -24358
511625                 XDOT =       -7447
574054
 YDOT =       4976
599670  feet/sec       YDOT =        1433
713468  meter/sec
 ZDOT =       4518
053895                 ZDOT =        1340
979167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3007549
96                 X    =          916701
23
 Y    =      -13887496
00  feet           Y    =        -4232908
78  meter
 Z    =       16859900
98                 Z    =         5138897
82
 XDOT =      21684
166361                 XDOT =        6609
333907
 YDOT =       9989
476921  feet/sec       YDOT =        3044
792565  meter/sec
 ZDOT =       4376
030527                 ZDOT =        1333
814105


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   09228
54990000  
00010596  00000-0  82463-4 0  9020
2 25544  51
6409 356
9658 0008099 338
4738  21
6083 15
73653353 15468


Satellite: ISS
Catalog Number: 25544
Epoch time:      09228
54990000   =   yrday
fracday
Element set:     902
Inclination:       51
6409  deg
RA of node:       356
9658  deg
Eccentricity:     
0008099     
Arg of perigee:   338
4738  deg
Mean anomaly:      21
6083  deg
Mean motion:   15
73653353  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1546
Checksum:              328


Coasting Arc #4 (Orbit 1560)
---------------------------------------

Vector Time (GMT): 2009/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6289122
96                 A    =         6732534
51  meter
 Y    =       -1982059
87  meter          E    =           
0015294
 Z    =       -1311693
94                 I    =           51
61074
 XDOT =       2571
378374                 Wp   =           11
32286
 YDOT =       4304
780676  meter/sec      RA   =          351
57512  deg
 ZDOT =       5850
250472                 TA   =          334
26412
                                          MA   =          334
34015
                                          Ha   =            191
857  n
mi
                                          Hp   =            184
519

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20633605
51                 X    =         6317191
14
 Y    =       -6502821
11  feet           Y    =        -1911574
17  meter
 Z    =       -4303457
82                 Z    =        -1281073
88
 XDOT =       8436
280756                 XDOT =        2494
631493
 YDOT =      14123
296180  feet/sec       YDOT =        4333
105755  meter/sec
 ZDOT =      19193
735145                 ZDOT =        5862
555946

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20678532
25                 X    =        -6302816
63
 Y    =       -6438331
91  feet           Y    =        -1962403
57  meter
 Z    =       -4183096
24                 Z    =        -1275007
73
 XDOT =        746
185025                 XDOT =         227
437196
 YDOT =     -14841
209645  feet/sec       YDOT =       -4523
600700  meter/sec
 ZDOT =      19242
309257                 ZDOT =        5865
055862


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   09229
50246863  
00010596  00000-0  82463-4 0  9039
2 25544  51
6415 352
0771 0008151 343
0902  16
9989 15
73625909 15617


Satellite: ISS
Catalog Number: 25544
Epoch time:      09229
50246863   =   yrday
fracday
Element set:     903
Inclination:       51
6415  deg
RA of node:       352
0771  deg
Eccentricity:     
0008151     
Arg of perigee:   343
0902  deg
Mean anomaly:      16
9989  deg
Mean motion:   15
73625909  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1561
Checksum:              316


Coasting Arc #5 (Orbit 1576)
---------------------------------------

Vector Time (GMT): 2009/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2688880
34                 A    =         6721928
11  meter
 Y    =       -3502554
60  meter          E    =           
0015824
 Z    =       -5080610
99                 I    =           51
54626
 XDOT =       6909
594795                 Wp   =           46
50498
 YDOT =      -2971
115031  meter/sec      RA   =          346
46421  deg
 ZDOT =      -1600
994533                 TA   =          208
03435
                                          MA   =          208
11967
                                          Ha   =            191
897  n
mi
                                          Hp   =            184
230

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8821785
89                 X    =        -2624834
17
 Y    =      -11491320
85  feet           Y    =        -3532264
86  meter
 Z    =      -16668671
24                 Z    =        -5093517
92
 XDOT =      22669
274261                 XDOT =        6950
081955
 YDOT =      -9747
752725  feet/sec       YDOT =       -2893
621425  meter/sec
 ZDOT =      -5252
606734                 ZDOT =       -1567
330253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         861842
73                 X    =          262689
66
 Y    =       14402488
89  feet           Y    =         4389878
61  meter
 Z    =      -16719584
41                 Z    =        -5096129
33
 XDOT =     -23236
800467                 XDOT =       -7082
576782
 YDOT =      -4582
398599  feet/sec       YDOT =       -1396
715093  meter/sec
 ZDOT =      -5120
310138                 ZDOT =       -1560
670530


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   09230
51853376  
00010596  00000-0  82463-4 0  9046
2 25544  51
6419 346
8625 0008204 346
5569  13
5374 15
73644606 15779


Satellite: ISS
Catalog Number: 25544
Epoch time:      09230
51853376   =   yrday
fracday
Element set:     904
Inclination:       51
6419  deg
RA of node:       346
8625  deg
Eccentricity:     
0008204     
Arg of perigee:   346
5569  deg
Mean anomaly:      13
5374  deg
Mean motion:   15
73644606  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1577
Checksum:              325


Coasting Arc #6 (Orbit 1592)
---------------------------------------

Vector Time (GMT): 2009/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5743264
77                 A    =         6732262
54  meter
 Y    =        3183626
25  meter          E    =           
0011051
 Z    =        1478658
67                 I    =           51
55246
 XDOT =      -3524
689292                 Wp   =           83
04867
 YDOT =      -3654
590501  meter/sec      RA   =          341
29797  deg
 ZDOT =      -5783
549352                 TA   =           80
66159
                                          MA   =           80
53665
                                          Ha   =            192
040  n
mi
                                          Hp   =            184
137

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18842732
17                 X    =        -5785620
66
 Y    =       10444968
02  feet           Y    =         3119164
84  meter
 Z    =        4851242
35                 Z    =         1450655
71
 XDOT =     -11563
941247                 XDOT =       -3455
466273
 YDOT =     -11990
126317  feet/sec       YDOT =       -3693
618481  meter/sec
 ZDOT =     -18974
899450                 ZDOT =       -5800
503840

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21520322
68                 X    =         6559394
35
 Y    =        1441160
28  feet           Y    =          439265
65  meter
 Z    =        4741227
03                 Z    =         1445126
00
 XDOT =       3238
082099                 XDOT =         986
967424
 YDOT =      14713
556151  feet/sec       YDOT =        4484
691915  meter/sec
 ZDOT =     -19041
745481                 ZDOT =       -5803
924023


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   09231
53459203  
00010596  00000-0  82463-4 0  9051
2 25544  51
6420 341
6473 0008145 350
8800   9
2214 15
73650525 15935


Satellite: ISS
Catalog Number: 25544
Epoch time:      09231
53459203   =   yrday
fracday
Element set:     905
Inclination:       51
6420  deg
RA of node:       341
6473  deg
Eccentricity:     
0008145     
Arg of perigee:   350
8800  deg
Mean anomaly:       9
2214  deg
Mean motion:   15
73650525  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1593
Checksum:              286


Coasting Arc #7 (Orbit 1608)
---------------------------------------

Vector Time (GMT): 2009/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3442261
15                 A    =         6721955
86  meter
 Y    =        2846034
46  meter          E    =           
0006241
 Z    =        5019117
48                 I    =           51
49128
 XDOT =      -6150
678136                 Wp   =           34
06967
 YDOT =       4277
464413  meter/sec      RA   =          336
18514  deg
 ZDOT =       1796
845958                 TA   =           38
61225
                                          MA   =           38
56763
                                          Ha   =            192
025  n
mi
                                          Hp   =            183
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11293507
71                 X    =         3385799
01
 Y    =        9337383
39  feet           Y    =         2884212
20  meter
 Z    =       16466920
87                 Z    =         5035702
47
 XDOT =     -20179
390210                 XDOT =       -6206
780920
 YDOT =      14033
675895  feet/sec       YDOT =        4208
370249  meter/sec
 ZDOT =       5895
163903                 ZDOT =        1766
830267

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4593529
79                 X    =        -1400107
88
 Y    =      -13837364
56  feet           Y    =        -4217628
72  meter
 Z    =       16532282
18                 Z    =         5039039
61
 XDOT =      23565
583218                 XDOT =        7182
789765
 YDOT =       -936
189609  feet/sec       YDOT =        -285
350593  meter/sec
 ZDOT =       5777
285998                 ZDOT =        1760
916772


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   09232
55064117  
00010596  00000-0  82463-4 0  9061
2 25544  51
6428 336
4320 0008260 354
5520   5
5552 15
73703742 16096


Satellite: ISS
Catalog Number: 25544
Epoch time:      09232
55064117   =   yrday
fracday
Element set:     906
Inclination:       51
6428  deg
RA of node:       336
4320  deg
Eccentricity:     
0008260     
Arg of perigee:   354
5520  deg
Mean anomaly:       5
5552  deg
Mean motion:   15
73703742  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1609
Checksum:              287


Coasting Arc #8 (Orbit 1623)
---------------------------------------

Vector Time (GMT): 2009/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4938972
77                 A    =         6732013
16  meter
 Y    =       -4248270
07  meter          E    =           
0015486
 Z    =       -1662560
44                 I    =           51
49766
 XDOT =       4329
755328                 Wp   =           16
81930
 YDOT =       2805
193784  meter/sec      RA   =          331
01268  deg
 ZDOT =       5722
228110                 TA   =          324
76104
                                          MA   =          324
86333
                                          Ha   =            192
410  n
mi
                                          Hp   =            183
667

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16203978
90                 X    =         4994186
87
 Y    =      -13937893
94  feet           Y    =        -4192730
91  meter
 Z    =       -5454594
63                 Z    =        -1638433
05
 XDOT =      14205
234017                 XDOT =        4270
268263
 YDOT =       9203
391680  feet/sec       YDOT =        2853
279220  meter/sec
 ZDOT =      18773
714273                 ZDOT =        5743
117148

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21084052
26                 X    =        -6426419
13
 Y    =        3649765
89  feet           Y    =         1112448
64  meter
 Z    =       -5359885
39                 Z    =        -1633693
07
 XDOT =      -7122
194292                 XDOT =       -2170
844820
 YDOT =     -13588
894147  feet/sec       YDOT =       -4141
894936  meter/sec
 ZDOT =      18856
003974                 ZDOT =        5747
310011


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   09233
50318309  
00010596  00000-0  82463-4 0  9073
2 25544  51
6428 331
5438 0008514 358
3799   1
7335 15
73648932 16247


Satellite: ISS
Catalog Number: 25544
Epoch time:      09233
50318309   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:       331
5438  deg
Eccentricity:     
0008514     
Arg of perigee:   358
3799  deg
Mean anomaly:       1
7335  deg
Mean motion:   15
73648932  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1624
Checksum:              320


Coasting Arc #9 (Orbit 1639)
---------------------------------------

Vector Time (GMT): 2009/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4060005
33                 A    =         6722295
55  meter
 Y    =       -2036079
99  meter          E    =           
0017387
 Z    =       -4970363
00                 I    =           51
43929
 XDOT =       5127
154669                 Wp   =           47
55062
 YDOT =      -5376
201488  meter/sec      RA   =          325
89956  deg
 ZDOT =      -1978
606886                 TA   =          203
19421
                                          MA   =          203
27277
                                          Ha   =            192
386  n
mi
                                          Hp   =            183
356

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13320227
45                 X    =        -4012790
90
 Y    =       -6680052
45  feet           Y    =        -2081217
55  meter
 Z    =      -16306965
21                 Z    =        -4989971
54
 XDOT =      16821
373585                 XDOT =        5196
502835
 YDOT =     -17638
456326  feet/sec       YDOT =       -5318
478962  meter/sec
 ZDOT =      -6491
492407                 ZDOT =       -1953
530769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8147792
87                 X    =         2483447
27
 Y    =       12375004
07  feet           Y    =         3771901
24  meter
 Z    =      -16384182
01                 Z    =        -4993898
68
 XDOT =     -22497
815509                 XDOT =       -6857
334167
 YDOT =       6317
531305  feet/sec       YDOT =        1925
583542  meter/sec
 ZDOT =      -6393
111191                 ZDOT =       -1948
620291


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   09234
51921956  
00010596  00000-0  82463-4 0  9084
2 25544  51
6423 326
3291 0008381   1
9038 358
2156 15
73674849 16405


Satellite: ISS
Catalog Number: 25544
Epoch time:      09234
51921956   =   yrday
fracday
Element set:     908
Inclination:       51
6423  deg
RA of node:       326
3291  deg
Eccentricity:     
0008381     
Arg of perigee:     1
9038  deg
Mean anomaly:     358
2156  deg
Mean motion:   15
73674849  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1640
Checksum:              319


Coasting Arc #10 (Orbit 1655)
---------------------------------------

Vector Time (GMT): 2009/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3995388
74                 A    =         6731683
55  meter
 Y    =        5111331
11  meter          E    =           
0014062
 Z    =        1790496
93                 I    =           51
44622
 XDOT =      -4889
016652                 Wp   =           79
44709
 YDOT =      -1825
844808  meter/sec      RA   =          320
72010  deg
 ZDOT =      -5657
179497                 TA   =           80
66406
                                          MA   =           80
50508
                                          Ha   =            192
547  n
mi
                                          Hp   =            183
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13108230
76                 X    =        -4060945
44
 Y    =       16769459
02  feet           Y    =         5066285
84  meter
 Z    =        5874333
76                 Z    =         1770928
02
 XDOT =     -16040
080880                 XDOT =       -4840
754955
 YDOT =      -5990
304487  feet/sec       YDOT =       -1880
247006  meter/sec
 ZDOT =     -18560
300186                 ZDOT =       -5680
812935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19603233
18                 X    =         5975065
47
 Y    =       -8345614
09  feet           Y    =        -2543743
17  meter
 Z    =        5797606
50                 Z    =         1767110
46
 XDOT =      10454
378709                 XDOT =        3186
494631
 YDOT =      11505
613535  feet/sec       YDOT =        3506
911006  meter/sec
 ZDOT =     -18653
334811                 ZDOT =       -5685
536451


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   09235
53524910  
00010596  00000-0  82463-4 0  9097
2 25544  51
6415 321
1140 0008465   7
0180 353
1100 15
73696724 16566


Satellite: ISS
Catalog Number: 25544
Epoch time:      09235
53524910   =   yrday
fracday
Element set:     909
Inclination:       51
6415  deg
RA of node:       321
1140  deg
Eccentricity:     
0008465     
Arg of perigee:     7
0180  deg
Mean anomaly:     353
1100  deg
Mean motion:   15
73696724  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1656
Checksum:              283


Coasting Arc #11 (Orbit 1671)
---------------------------------------

Vector Time (GMT): 2009/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4444849
02                 A    =         6722315
61  meter
 Y    =        1131723
51  meter          E    =           
0008277
 Z    =        4907167
55                 I    =           51
39311
 XDOT =      -3952
603679                 Wp   =           52
84967
 YDOT =       6260
313008  meter/sec      RA   =          315
60426  deg
 ZDOT =       2138
879806                 TA   =           16
35997
                                          MA   =           16
33327
                                          Ha   =            192
451  n
mi
                                          Hp   =            182
996

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14582837
98                 X    =         4408025
44
 Y    =        3713003
65  feet           Y    =         1181222
63  meter
 Z    =       16099631
08                 Z    =         4928671
13
 XDOT =     -12967
859840                 XDOT =       -4032
704085
 YDOT =      20539
084672  feet/sec       YDOT =        6215
664849  meter/sec
 ZDOT =       7017
322199                 ZDOT =        2119
483399

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11072775
40                 X    =        -3374981
94
 Y    =      -10055208
71  feet           Y    =        -3064827
62  meter
 Z    =       16184254
79                 Z    =         4932960
86
 XDOT =      20367
404986                 XDOT =        6207
985040
 YDOT =     -11269
109183  feet/sec       YDOT =       -3434
824479  meter/sec
 ZDOT =       6941
329914                 ZDOT =        2115
717358


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   09236
55126937  
00010596  00000-0  82463-4 0  9109
2 25544  51
6418 315
8980 0008505  10
0138 350
1193 15
73736790 16728


Satellite: ISS
Catalog Number: 25544
Epoch time:      09236
55126937   =   yrday
fracday
Element set:     910
Inclination:       51
6418  deg
RA of node:       315
8980  deg
Eccentricity:     
0008505     
Arg of perigee:    10
0138  deg
Mean anomaly:     350
1193  deg
Mean motion:   15
73736790  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1672
Checksum:              307


Coasting Arc #12 (Orbit 1686)
---------------------------------------

Vector Time (GMT): 2009/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2867542
08                 A    =         6731432
04  meter
 Y    =       -5762550
55  meter          E    =           
0015329
 Z    =       -1945787
12                 I    =           51
40211
 XDOT =       5244
310031                 Wp   =           24
41468
 YDOT =        730
350445  meter/sec      RA   =          310
41930  deg
 ZDOT =       5595
059245                 TA   =          313
85420
                                          MA   =          313
98076
                                          Ha   =            192
805  n
mi
                                          Hp   =            182
864

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9407946
46                 X    =         2941219
07
 Y    =      -18906005
75  feet           Y    =        -5730072
07  meter
 Z    =       -6383816
00                 Z    =        -1931677
62
 XDOT =      17205
741573                 XDOT =        5208
573571
 YDOT =       2396
162877  feet/sec       YDOT =         788
795604  meter/sec
 ZDOT =      18356
493586                 ZDOT =        5620
449296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16972916
10                 X    =        -5173344
83
 Y    =       12592403
57  feet           Y    =         3838164
61  meter
 Z    =       -6328594
46                 Z    =        -1928955
59
 XDOT =     -13248
947205                 XDOT =       -4038
279108
 YDOT =      -8631
073347  feet/sec       YDOT =       -2630
751156  meter/sec
 ZDOT =      18456
382740                 ZDOT =        5625
505459


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   09237
50378394  
00010596  00000-0  82463-4 0  9112
2 25544  51
6411 311
0092 0008745  13
2224 346
9167 15
73691578 16874


Satellite: ISS
Catalog Number: 25544
Epoch time:      09237
50378394   =   yrday
fracday
Element set:     911
Inclination:       51
6411  deg
RA of node:       311
0092  deg
Eccentricity:     
0008745     
Arg of perigee:    13
2224  deg
Mean anomaly:     346
9167  deg
Mean motion:   15
73691578  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1687
Checksum:              316


Coasting Arc #13 (Orbit 1702)
---------------------------------------

Vector Time (GMT): 2009/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4654642
10                 A    =         6722620
53  meter
 Y    =        -157715
07  meter          E    =           
0018663
 Z    =       -4864609
95                 I    =           51
35354
 XDOT =       2621
284027                 Wp   =           50
56803
 YDOT =      -6856
511257  meter/sec      RA   =          305
30302  deg
 ZDOT =      -2280
005758                 TA   =          197
07937
                                          MA   =          197
14227
                                          Ha   =            192
840  n
mi
                                          Hp   =            182
502

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15271135
51                 X    =        -4628901
18
 Y    =        -517437
91  feet           Y    =         -209622
03  meter
 Z    =      -15960006
41                 Z    =        -4887159
67
 XDOT =       8600
013212                 XDOT =        2708
835745
 YDOT =     -22495
115671  feet/sec       YDOT =       -6826
708961  meter/sec
 ZDOT =      -7480
333852                 ZDOT =       -2267
058995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13427658
30                 X    =         4092750
25
 Y    =        7094672
10  feet           Y    =         2162456
06  meter
 Z    =      -16048699
22                 Z    =        -4891643
52
 XDOT =     -17082
961174                 XDOT =       -5206
886566
 YDOT =      15482
122980  feet/sec       YDOT =        4718
951084  meter/sec
 ZDOT =      -7429
736983                 ZDOT =       -2264
583832


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   09238
51979201  
00010596  00000-0  82463-4 0  9129
2 25544  51
6403 305
7933 0008678  17
6905 342
4559 15
73716295 17037


Satellite: ISS
Catalog Number: 25544
Epoch time:      09238
51979201   =   yrday
fracday
Element set:     912
Inclination:       51
6403  deg
RA of node:       305
7933  deg
Eccentricity:     
0008678     
Arg of perigee:    17
6905  deg
Mean anomaly:     342
4559  deg
Mean motion:   15
73716295  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1703
Checksum:              326


Coasting Arc #14 (Orbit 1718)
---------------------------------------

Vector Time (GMT): 2009/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1703259
04                 A    =         6731031
81  meter
 Y    =        6182571
76  meter          E    =           
0016709
 Z    =        2037420
20                 I    =           51
36659
 XDOT =      -5332
624682                 Wp   =           78
69355
 YDOT =        370
057785  meter/sec      RA   =          300
11245  deg
 ZDOT =      -5539
342234                 TA   =           78
49993
                                          MA   =           78
31235
                                          Ha   =            192
936  n
mi
                                          Hp   =            182
347

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5588120
21                 X    =        -1782164
42
 Y    =       20284028
08  feet           Y    =         6163083
68  meter
 Z    =        6684449
47                 Z    =         2028954
29
 XDOT =     -17495
487801                 XDOT =       -5309
457340
 YDOT =       1214
100346  feet/sec       YDOT =         310
554924  meter/sec
 ZDOT =     -18173
694992                 ZDOT =       -5565
191779

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13647380
47                 X    =         4159721
57
 Y    =      -16026790
98  feet           Y    =        -4884965
89  meter
 Z    =        6651445
30                 Z    =         2027360
53
 XDOT =      15114
012817                 XDOT =        4606
751107
 YDOT =       5228
535660  feet/sec       YDOT =        1593
657669  meter/sec
 ZDOT =     -18275
343352                 ZDOT =       -5570
324654


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   09239
53579154  
00010596  00000-0  82463-4 0  9136
2 25544  51
6407 300
5774 0008930  21
4905 338
6627 15
73775493 17196


Satellite: ISS
Catalog Number: 25544
Epoch time:      09239
53579154   =   yrday
fracday
Element set:     913
Inclination:       51
6407  deg
RA of node:       300
5774  deg
Eccentricity:     
0008930     
Arg of perigee:    21
4905  deg
Mean anomaly:     338
6627  deg
Mean motion:   15
73775493  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1719
Checksum:              332


Coasting Arc #15 (Orbit 1734)
---------------------------------------

Vector Time (GMT): 2009/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4621246
28                 A    =         6722641
66  meter
 Y    =        -810618
54  meter          E    =           
0010677
 Z    =        4804628
04                 I    =           51
32418
 XDOT =      -1237
720758                 Wp   =           65
39272
 YDOT =       7217
131153  meter/sec      RA   =          294
99540  deg
 ZDOT =       2408
330785                 TA   =            1
01794
                                          MA   =            1
01577
                                          Ha   =            192
863  n
mi
                                          Hp   =            182
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15161569
15                 X    =         4606627
40
 Y    =       -2659509
64  feet           Y    =         -759022
94  meter
 Z    =       15763215
34                 Z    =         4827042
39
 XDOT =      -4060
763643                 XDOT =       -1330
031142
 YDOT =      23678
251813  feet/sec       YDOT =        7202
774019  meter/sec
 ZDOT =       7901
347720                 ZDOT =        2402
093985

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14853048
47                 X    =        -4527209
17
 Y    =       -3680658
92  feet           Y    =        -1121864
84  meter
 Z    =       15851335
27                 Z    =         4831486
99
 XDOT =      13088
205643                 XDOT =        3989
285080
 YDOT =     -18895
190412  feet/sec       YDOT =       -5759
254038  meter/sec
 ZDOT =       7877
163489                 ZDOT =        2400
959432


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   09240
55178450  
00010596  00000-0  82463-4 0  9145
2 25544  51
6404 295
3617 0008855  25
5891 334
5709 15
73772077 17354


Satellite: ISS
Catalog Number: 25544
Epoch time:      09240
55178450   =   yrday
fracday
Element set:     914
Inclination:       51
6404  deg
RA of node:       295
3617  deg
Eccentricity:     
0008855     
Arg of perigee:    25
5891  deg
Mean anomaly:     334
5709  deg
Mean motion:   15
73772077  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1735
Checksum:              329

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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