Date: May 13th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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 17)
---------------------------------------

Vector Time (GMT): 2009/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3741851
40                 A    =         6724235
76  meter
 Y    =        2028675
38  meter          E    =           
0016944
 Z    =       -5218191
52                 I    =           51
85497
 XDOT =      -4696
886661                 Wp   =           49
01553
 YDOT =       5999
264976  meter/sec      RA   =          134
13450  deg
 ZDOT =      -1026
992200                 TA   =          211
15479
                                          MA   =          211
25535
                                          Ha   =            193
878  n
mi
                                          Hp   =            185
521

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12276415
36                 X    =         3744237
73
 Y    =        6655759
12  feet           Y    =         2070532
91  meter
 Z    =      -17120050
93                 Z    =        -5200007
29
 XDOT =     -15409
733141                 XDOT =       -4758
633348
 YDOT =      19682
627874  feet/sec       YDOT =        5946
396528  meter/sec
 ZDOT =      -3369
396981                 ZDOT =       -1049
959299

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13172712
44                 X    =         4015042
75
 Y    =       -4891355
23  feet           Y    =        -1490885
07  meter
 Z    =      -17048751
81                 Z    =        -5196459
55
 XDOT =       4248
183970                 XDOT =        1294
846474
 YDOT =      23596
505036  feet/sec       YDOT =        7192
214735  meter/sec
 ZDOT =      -3458
879371                 ZDOT =       -1054
266432


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   09131
51767387  
00010596  00000-0  82463-4 0  9008
2 25544  51
6367 134
9785 0009266 350
2895   9
8087 15
72682441   183


Satellite: ISS
Catalog Number: 25544
Epoch time:      09131
51767387   =   yrday
fracday
Element set:     900
Inclination:       51
6367  deg
RA of node:       134
9785  deg
Eccentricity:     
0009266     
Arg of perigee:   350
2895  deg
Mean anomaly:       9
8087  deg
Mean motion:   15
72682441  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:              18
Checksum:              331


Coasting Arc #2 (Orbit 33)
---------------------------------------

Vector Time (GMT): 2009/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3324981
04                 A    =         6735047
83  meter
 Y    =       -5712673
73  meter          E    =           
0011338
 Z    =        1290663
99                 I    =           51
91133
 XDOT =       4760
394137                 Wp   =           78
58152
 YDOT =       1433
951287  meter/sec      RA   =          129
00431  deg
 ZDOT =      -5871
276754                 TA   =           87
32558
                                          MA   =           87
19580
                                          Ha   =            193
965  n
mi
                                          Hp   =            185
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10908730
43                 X    =         3382344
11
 Y    =      -18742367
87  feet           Y    =        -5675171
28  meter
 Z    =        4234461
92                 Z    =         1306955
57
 XDOT =      15618
091002                 XDOT =        4772
527578
 YDOT =       4704
564591  feet/sec       YDOT =        1487
253366  meter/sec
 ZDOT =     -19262
719009                 ZDOT =       -5848
120835

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7228937
69                 X    =        -2203380
21
 Y    =      -20432286
72  feet           Y    =        -6227760
99  meter
 Z    =        4297852
97                 Z    =         1309985
58
 XDOT =      12282
676273                 XDOT =        3743
759728
 YDOT =      -8409
275436  feet/sec       YDOT =       -2563
147153  meter/sec
 ZDOT =     -19171
993963                 ZDOT =       -5843
623760


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   09132
53434476  
00010596  00000-0  82463-4 0  9012
2 25544  51
6363 129
7664 0009436 354
5741   5
5317 15
72729357   348


Satellite: ISS
Catalog Number: 25544
Epoch time:      09132
53434476   =   yrday
fracday
Element set:     901
Inclination:       51
6363  deg
RA of node:       129
7664  deg
Eccentricity:     
0009436     
Arg of perigee:   354
5741  deg
Mean anomaly:       5
5317  deg
Mean motion:   15
72729357  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:              34
Checksum:              310


Coasting Arc #3 (Orbit 49)
---------------------------------------

Vector Time (GMT): 2009/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4456400
45                 A    =         6724988
19  meter
 Y    =        -419315
00  meter          E    =           
0007551
 Z    =        5013462
91                 I    =           51
89467
 XDOT =       2817
956929                 Wp   =           35
54374
 YDOT =      -6904
408840  meter/sec      RA   =          123
92485  deg
 ZDOT =       1931
943944                 TA   =           35
89656
                                          MA   =           35
84586
                                          Ha   =            194
201  n
mi
                                          Hp   =            184
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14620736
38                 X    =        -4475735
08
 Y    =       -1375705
39  feet           Y    =         -469257
79  meter
 Z    =       16448369
13                 Z    =         4991766
52
 XDOT =       9245
265516                 XDOT =        2885
568644
 YDOT =     -22652
259975  feet/sec       YDOT =       -6872
519001  meter/sec
 ZDOT =       6338
398768                 ZDOT =        1945
797080

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10400868
21                 X    =        -3170184
63
 Y    =       10500855
49  feet           Y    =         3200660
75  meter
 Z    =       16363414
04                 Z    =         4987568
60
 XDOT =     -10898
737702                 XDOT =       -3321
935251
 YDOT =     -20732
374075  feet/sec       YDOT =       -6319
227618  meter/sec
 ZDOT =       6392
180646                 ZDOT =        1948
336661


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   09133
55100475  
00010596  00000-0  82463-4 0  9025
2 25544  51
6360 124
5548 0009440 357
7379   2
3739 15
72721760   507


Satellite: ISS
Catalog Number: 25544
Epoch time:      09133
55100475   =   yrday
fracday
Element set:     902
Inclination:       51
6360  deg
RA of node:       124
5548  deg
Eccentricity:     
0009440     
Arg of perigee:   357
7379  deg
Mean anomaly:       2
3739  deg
Mean motion:   15
72721760  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:              50
Checksum:              292


Coasting Arc #4 (Orbit 64)
---------------------------------------

Vector Time (GMT): 2009/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1553059
04                 A    =         6733850
47  meter
 Y    =        6205751
90  meter          E    =           
0015056
 Z    =       -2078086
50                 I    =           51
94054
 XDOT =      -5281
476391                 Wp   =           17
97943
 YDOT =        538
770858  meter/sec      RA   =          118
78488  deg
 ZDOT =       5580
674035                 TA   =          318
91749
                                          MA   =          319
03077
                                          Ha   =            194
185  n
mi
                                          Hp   =            184
668

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5095338
05                 X    =        -1612242
35
 Y    =       20360078
40  feet           Y    =         6188054
01  meter
 Z    =       -6817869
11                 Z    =        -2085774
36
 XDOT =     -17327
678449                 XDOT =       -5314
218540
 YDOT =       1767
620924  feet/sec       YDOT =         479
526605  meter/sec
 ZDOT =      18309
298016                 ZDOT =        5554
937006

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12815482
69                 X    =         3906159
12
 Y    =       16608816
41  feet           Y    =         5062367
24  meter
 Z    =       -6847570
55                 Z    =        -2087139
50
 XDOT =      -8232
257021                 XDOT =       -2509
191940
 YDOT =      13826
015207  feet/sec       YDOT =        4214
169435  meter/sec
 ZDOT =      18208
577412                 ZDOT =        5549
974395


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   09134
50411220  
00010596  00000-0  82463-4 0  9035
2 25544  51
6362 119
6697 0009443   2
1768 357
9434 15
72746265   659


Satellite: ISS
Catalog Number: 25544
Epoch time:      09134
50411220   =   yrday
fracday
Element set:     903
Inclination:       51
6362  deg
RA of node:       119
6697  deg
Eccentricity:     
0009443     
Arg of perigee:     2
1768  deg
Mean anomaly:     357
9434  deg
Mean motion:   15
72746265  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:              65
Checksum:              304


Coasting Arc #5 (Orbit 80)
---------------------------------------

Vector Time (GMT): 2009/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4622909
68                 A    =         6726225
66  meter
 Y    =       -1345776
13  meter          E    =           
0017255
 Z    =       -4712197
36                 I    =           51
92816
 XDOT =       -758
946856                 Wp   =           40
93650
 YDOT =       7127
734445  meter/sec      RA   =          113
71849  deg
 ZDOT =      -2773
169262                 TA   =          201
74710
                                          MA   =          201
82045
                                          Ha   =            194
288  n
mi
                                          Hp   =            184
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15167026
51                 X    =         4660505
89
 Y    =       -4415276
02  feet           Y    =        -1293869
37  meter
 Z    =      -15459965
08                 Z    =        -4689647
98
 XDOT =      -2489
983123                 XDOT =        -825
122366
 YDOT =      23384
955528  feet/sec       YDOT =        7118
877728  meter/sec
 ZDOT =      -9098
324350                 ZDOT =       -2777
016272

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5762430
46                 X    =         1756388
81
 Y    =      -14800238
82  feet           Y    =        -4511112
79  meter
 Z    =      -15371766
39                 Z    =        -4685314
39
 XDOT =      16013
503059                 XDOT =        4880
915733
 YDOT =      15723
768709  feet/sec       YDOT =        4792
604703  meter/sec
 ZDOT =      -9112
936935                 ZDOT =       -2777
623178


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   09135
52074918  
00010596  00000-0  82463-4 0  9048
2 25544  51
6363 114
4573 0009486   5
4780 354
6485 15
72754108   816


Satellite: ISS
Catalog Number: 25544
Epoch time:      09135
52074918   =   yrday
fracday
Element set:     904
Inclination:       51
6363  deg
RA of node:       114
4573  deg
Eccentricity:     
0009486     
Arg of perigee:     5
4780  deg
Mean anomaly:     354
6485  deg
Mean motion:   15
72754108  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:              81
Checksum:              314


Coasting Arc #6 (Orbit 96)
---------------------------------------

Vector Time (GMT): 2009/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -212403
75                 A    =         6732319
55  meter
 Y    =       -6137640
86  meter          E    =           
0016338
 Z    =        2755500
91                 I    =           51
95997
 XDOT =       5113
940680                 Wp   =           64
63287
 YDOT =      -2513
090637  meter/sec      RA   =          108
56979  deg
 ZDOT =      -5172
947577                 TA   =           84
04995
                                          MA   =           83
86376
                                          Ha   =            194
345  n
mi
                                          Hp   =            184
281

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -696862
70                 X    =         -157141
61
 Y    =      -20136616
98  feet           Y    =        -6139707
33  meter
 Z    =        9040357
31                 Z    =         2754602
76
 XDOT =      16778
020604                 XDOT =        5166
791754
 YDOT =      -8245
048021  feet/sec       YDOT =       -2455
607621  meter/sec
 ZDOT =     -16971
612786                 ZDOT =       -5147
975781

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16646552
61                 X    =        -5073869
24
 Y    =      -11354811
07  feet           Y    =        -3460946
41  meter
 Z    =        9036457
99                 Z    =         2754312
40
 XDOT =       2559
414758                 XDOT =         780
109618
 YDOT =     -17260
748188  feet/sec       YDOT =       -5261
076048  meter/sec
 ZDOT =     -16873
995191                 ZDOT =       -5143
193734


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   09136
53737313  
00010596  00000-0  82463-4 0  9056
2 25544  51
6364 109
2457 0009621   8
4468 351
6855 15
72794897   971


Satellite: ISS
Catalog Number: 25544
Epoch time:      09136
53737313   =   yrday
fracday
Element set:     905
Inclination:       51
6364  deg
RA of node:       109
2457  deg
Eccentricity:     
0009621     
Arg of perigee:     8
4468  deg
Mean anomaly:     351
6855  deg
Mean motion:   15
72794897  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:              97
Checksum:              337


Coasting Arc #7 (Orbit 112)
---------------------------------------

Vector Time (GMT): 2009/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4187093
02                 A    =         6727523
37  meter
 Y    =        3019707
04  meter          E    =           
0012875
 Z    =        4300410
03                 I    =           51
95300
 XDOT =      -1226
314685                 Wp   =           61
10511
 YDOT =      -6737
804924  meter/sec      RA   =          103
51366  deg
 ZDOT =       3535
404470                 TA   =          353
26034
                                          MA   =          353
27764
                                          Ha   =            194
439  n
mi
                                          Hp   =            184
077

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13737181
83                 X    =        -4241439
44
 Y    =        9907175
34  feet           Y    =         2972580
35  meter
 Z    =       14108956
78                 Z    =         4279937
21
 XDOT =      -4023
342143                 XDOT =       -1168
054730
 YDOT =     -22105
659198  feet/sec       YDOT =       -6751
192795  meter/sec
 ZDOT =      11599
096029                 ZDOT =        3529
588028

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          57921
56                 X    =           17654
49
 Y    =       17003214
94  feet           Y    =         5182579
91  meter
 Z    =       14028979
87                 Z    =         4276033
06
 XDOT =     -19141
233441                 XDOT =       -5834
247953
 YDOT =      -9490
768307  feet/sec       YDOT =       -2892
786180  meter/sec
 ZDOT =      11575
905776                 ZDOT =        3528
336081


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   09137
55398433  
00010596  00000-0  82463-4 0  9066
2 25544  51
6369 104
0345 0009459  11
8099 348
3284 15
72837246  1136


Satellite: ISS
Catalog Number: 25544
Epoch time:      09137
55398433   =   yrday
fracday
Element set:     906
Inclination:       51
6369  deg
RA of node:       104
0345  deg
Eccentricity:     
0009459     
Arg of perigee:    11
8099  deg
Mean anomaly:     348
3284  deg
Mean motion:   15
72837246  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             113
Checksum:              322


Coasting Arc #8 (Orbit 127)
---------------------------------------

Vector Time (GMT): 2009/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1879277
89                 A    =         6730599
63  meter
 Y    =        5495290
24  meter          E    =           
0011945
 Z    =       -3398559
78                 I    =           51
96864
 XDOT =      -4320
510445                 Wp   =           39
06930
 YDOT =       4346
686008  meter/sec      RA   =           98
35957  deg
 ZDOT =       4657
139913                 TA   =          281
04919
                                          MA   =          281
18350
                                          Ha   =            194
587  n
mi
                                          Hp   =            183
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6165609
86                 X    =         1834198
69
 Y    =       18029167
46  feet           Y    =         5516053
58  meter
 Z    =      -11150130
52                 Z    =        -3389539
33
 XDOT =     -14174
903035                 XDOT =       -4391
418457
 YDOT =      14260
780865  feet/sec       YDOT =        4297
974781  meter/sec
 ZDOT =      15279
330423                 ZDOT =        4635
978714

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18390671
47                 X    =         5605476
66
 Y    =        5063860
66  feet           Y    =         1543464
73  meter
 Z    =      -11114474
93                 Z    =        -3387691
96
 XDOT =       4057
896347                 XDOT =        1236
846806
 YDOT =      18488
428539  feet/sec       YDOT =        5635
273019  meter/sec
 ZDOT =      15196
733055                 ZDOT =        4631
964235


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   09138
50704813  
00010596  00000-0  82463-4 0  9076
2 25544  51
6368  99
1481 0009660  15
8261 344
3202 15
72801017  1288


Satellite: ISS
Catalog Number: 25544
Epoch time:      09138
50704813   =   yrday
fracday
Element set:     907
Inclination:       51
6368  deg
RA of node:        99
1481  deg
Eccentricity:     
0009660     
Arg of perigee:    15
8261  deg
Mean anomaly:     344
3202  deg
Mean motion:   15
72801017  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             128
Checksum:              294


Coasting Arc #9 (Orbit 143)
---------------------------------------

Vector Time (GMT): 2009/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3263417
23                 A    =         6729141
80  meter
 Y    =       -4477942
89  meter          E    =           
0014181
 Z    =       -3835027
68                 I    =           51
96802
 XDOT =       2947
336826                 Wp   =           40
89982
 YDOT =       5733
272285  meter/sec      RA   =           93
30660  deg
 ZDOT =      -4184
585498                 TA   =          185
36360
                                          MA   =          185
37881
                                          Ha   =            194
560  n
mi
                                          Hp   =            183
737

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10706749
43                 X    =         3331877
91
 Y    =      -14691413
69  feet           Y    =        -4441066
45  meter
 Z    =      -12582111
82                 Z    =        -3819007
76
 XDOT =       9669
740244                 XDOT =        2903
335580
 YDOT =      18809
948442  feet/sec       YDOT =        5765
985347  meter/sec
 ZDOT =     -13728
955046                 ZDOT =       -4170
373692

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6309758
66                 X    =        -1923214
44
 Y    =      -17094649
03  feet           Y    =        -5210449
03  meter
 Z    =      -12519647
66                 Z    =        -3815988
61
 XDOT =      19820
613473                 XDOT =        6041
322987
 YDOT =       2702
096160  feet/sec       YDOT =         823
598910  meter/sec
 ZDOT =     -13672
962456                 ZDOT =       -4167
518957


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   09139
52363583  
00010596  00000-0  82463-4 0  9085
2 25544  51
6375  93
9357 0009679  19
5448 340
6083 15
72851395  1446


Satellite: ISS
Catalog Number: 25544
Epoch time:      09139
52363583   =   yrday
fracday
Element set:     908
Inclination:       51
6375  deg
RA of node:        93
9357  deg
Eccentricity:     
0009679     
Arg of perigee:    19
5448  deg
Mean anomaly:     340
6083  deg
Mean motion:   15
72851395  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             144
Checksum:              341


Coasting Arc #10 (Orbit 159)
---------------------------------------

Vector Time (GMT): 2009/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3200834
04                 A    =         6728828
29  meter
 Y    =       -4442439
00  meter          E    =           
0018326
 Z    =        3906827
91                 I    =           51
96794
 XDOT =       3012
740846                 Wp   =           53
93773
 YDOT =      -5787
067061  meter/sec      RA   =           88
15152  deg
 ZDOT =      -4088
335492                 TA   =           78
55202
                                          MA   =           78
34625
                                          Ha   =            194
647  n
mi
                                          Hp   =            183
519

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10501424
02                 X    =        -3169899
04
 Y    =      -14574931
09  feet           Y    =        -4478059
88  meter
 Z    =       12817676
86                 Z    =         3891352
84
 XDOT =       9884
320360                 XDOT =        3097
089635
 YDOT =     -18986
440490  feet/sec       YDOT =       -5752
904954  meter/sec
 ZDOT =     -13413
174186                 ZDOT =       -4073
494821

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17974188
50                 X    =        -5478532
65
 Y    =        1092449
79  feet           Y    =          332978
69  meter
 Z    =       12756820
30                 Z    =         3888278
83
 XDOT =     -10585
282339                 XDOT =       -3226
394057
 YDOT =     -17290
115955  feet/sec       YDOT =       -5270
027343  meter/sec
 ZDOT =     -13355
395965                 ZDOT =       -4070
724690


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   09140
54021077  
00010596  00000-0  82463-4 0  9099
2 25544  51
6379  88
7238 0009669  22
8658 337
2934 15
72870914  1602


Satellite: ISS
Catalog Number: 25544
Epoch time:      09140
54021077   =   yrday
fracday
Element set:     909
Inclination:       51
6379  deg
RA of node:        88
7238  deg
Eccentricity:     
0009669     
Arg of perigee:    22
8658  deg
Mean anomaly:     337
2934  deg
Mean motion:   15
72870914  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             160
Checksum:              331


Coasting Arc #11 (Orbit 175)
---------------------------------------

Vector Time (GMT): 2009/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1917100
80                 A    =         6730678
97  meter
 Y    =        5538786
90  meter          E    =           
0019293
 Z    =        3284626
77                 I    =           51
97272
 XDOT =      -4270
050275                 Wp   =           62
17578
 YDOT =      -4307
250857  meter/sec      RA   =           83
09867  deg
 ZDOT =       4758
698945                 TA   =          336
18547
                                          MA   =          336
27462
                                          Ha   =            194
702  n
mi
                                          Hp   =            183
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6289700
79                 X    =        -1994850
44
 Y    =       18171873
04  feet           Y    =         5516913
78  meter
 Z    =       10776334
54                 Z    =         3275124
88
 XDOT =     -14009
351296                 XDOT =       -4244
685907
 YDOT =     -14131
400451  feet/sec       YDOT =       -4354
859614  meter/sec
 ZDOT =      15612
529346                 ZDOT =        4738
015855

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12174968
68                 X    =         3710930
46
 Y    =       14911114
18  feet           Y    =         4544907
60  meter
 Z    =       10739436
84                 Z    =         3273380
35
 XDOT =     -18328
577348                 XDOT =       -5586
550376
 YDOT =       3750
153356  feet/sec       YDOT =        1143
046743  meter/sec
 ZDOT =      15531
293229                 ZDOT =        4733
938176


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   09141
55677291  
00010596  00000-0  82463-4 0  9108
2 25544  51
6384  83
5119 0009596  26
9166 333
2493 15
72888925  1761


Satellite: ISS
Catalog Number: 25544
Epoch time:      09141
55677291   =   yrday
fracday
Element set:     910
Inclination:       51
6384  deg
RA of node:        83
5119  deg
Eccentricity:     
0009596     
Arg of perigee:    26
9166  deg
Mean anomaly:     333
2493  deg
Mean motion:   15
72888925  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             176
Checksum:              339


Coasting Arc #12 (Orbit 190)
---------------------------------------

Vector Time (GMT): 2009/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4140998
45                 A    =         6727115
17  meter
 Y    =        3011237
64  meter          E    =           
0014199
 Z    =       -4371542
81                 I    =           51
95637
 XDOT =      -1304
187628                 Wp   =           68
44280
 YDOT =       6757
871055  meter/sec      RA   =           77
94510  deg
 ZDOT =       3433
555384                 TA   =          236
01980
                                          MA   =          236
15480
                                          Ha   =            194
767  n
mi
                                          Hp   =            183
233

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13585952
94                 X    =         4128255
19
 Y    =        9879388
59  feet           Y    =         3057473
92  meter
 Z    =      -14342332
05                 Z    =        -4351455
98
 XDOT =      -4278
830800                 XDOT =       -1396
338346
 YDOT =      22171
492961  feet/sec       YDOT =        6742
771261  meter/sec
 ZDOT =      11264
945487                 ZDOT =        3426
996365

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15451479
40                 X    =         4709610
92
 Y    =       -6759219
37  feet           Y    =        -2060210
07  meter
 Z    =      -14263508
08                 Z    =        -4347517
26
 XDOT =      16402
023639                 XDOT =        4999
336805
 YDOT =      13873
767404  feet/sec       YDOT =        4228
724305  meter/sec
 ZDOT =      11239
624932                 ZDOT =        3425
837679


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   09142
50978875  
00010596  00000-0  82463-4 0  9117
2 25544  51
6388  78
6255 0009658  29
9961 330
1753 15
72897038  1913


Satellite: ISS
Catalog Number: 25544
Epoch time:      09142
50978875   =   yrday
fracday
Element set:     911
Inclination:       51
6388  deg
RA of node:        78
6255  deg
Eccentricity:     
0009658     
Arg of perigee:    29
9961  deg
Mean anomaly:     330
1753  deg
Mean motion:   15
72897038  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             191
Checksum:              350

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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