Date: May 28th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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 269)
---------------------------------------

Vector Time (GMT): 2009/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2749647
18                 A    =         6733337
74  meter
 Y    =       -5882697
39  meter          E    =           
0011573
 Z    =       -1791928
04                 I    =           51
92199
 XDOT =       5119
888226                 Wp   =           87
37188
 YDOT =       -666
281893  meter/sec      RA   =           52
46184  deg
 ZDOT =      -5699
901882                 TA   =          112
37907
                                          MA   =          112
25640
                                          Ha   =            194
624  n
mi
                                          Hp   =            182
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9021152
17                 X    =        -2674956
63
 Y    =      -19300188
29  feet           Y    =        -5913027
61  meter
 Z    =       -5879029
01                 Z    =        -1805105
50
 XDOT =      16797
533551                 XDOT =        5154
647313
 YDOT =      -2185
964215  feet/sec       YDOT =        -608
832932  meter/sec
 ZDOT =     -18700
465492                 ZDOT =       -5674
945112

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21288792
96                 X    =        -6488824
09
 Y    =        -230035
56  feet           Y    =          -70114
84  meter
 Z    =       -5930920
22                 Z    =        -1807744
48
 XDOT =       5312
744239                 XDOT =        1619
324444
 YDOT =     -14639
498756  feet/sec       YDOT =       -4462
119221  meter/sec
 ZDOT =     -18602
728858                 ZDOT =       -5670
111756


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   09147
52829137  
00010596  00000-0  82463-4 0  9008
2 25544  51
6427  52
9019 0009397  48
2766 311
9199 15
73090892  2700


Satellite: ISS
Catalog Number: 25544
Epoch time:      09147
52829137   =   yrday
fracday
Element set:     900
Inclination:       51
6427  deg
RA of node:        52
9019  deg
Eccentricity:     
0009397     
Arg of perigee:    48
2766  deg
Mean anomaly:     311
9199  deg
Mean motion:   15
73090892  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             270
Checksum:              328


Coasting Arc #2 (Orbit 285)
---------------------------------------

Vector Time (GMT): 2009/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4233013
49                 A    =         6723484
83  meter
 Y    =        1268244
01  meter          E    =           
0014745
 Z    =        5059782
06                 I    =           51
86998
 XDOT =      -3999
247871                 Wp   =           51
99472
 YDOT =      -6353
003547  meter/sec      RA   =           47
32019  deg
 ZDOT =      -1741
066278                 TA   =           54
76576
                                          MA   =           54
62783
                                          Ha   =            194
669  n
mi
                                          Hp   =            182
150

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13887839
53                 X    =        -4271460
05
 Y    =        4160905
55  feet           Y    =         1220692
21  meter
 Z    =       16600334
83                 Z    =         5039124
93
 XDOT =     -13120
891966                 XDOT =       -3919
452512
 YDOT =     -20843
187490  feet/sec       YDOT =       -6397
279034  meter/sec
 ZDOT =      -5712
159706                 ZDOT =       -1760
301778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2038197
67                 X    =         -621242
65
 Y    =       14446777
42  feet           Y    =         4403377
76  meter
 Z    =       16519464
61                 Z    =         5035132
81
 XDOT =     -23346
189128                 XDOT =       -7115
918446
 YDOT =       3370
846151  feet/sec       YDOT =        1027
433907  meter/sec
 ZDOT =      -5787
806721                 ZDOT =       -1764
123489


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   09148
54469169  
00010596  00000-0  82463-4 0  9017
2 25544  51
6423  47
6891 0009409  51
0088 309
1911 15
73172882  2866


Satellite: ISS
Catalog Number: 25544
Epoch time:      09148
54469169   =   yrday
fracday
Element set:     901
Inclination:       51
6423  deg
RA of node:        47
6891  deg
Eccentricity:     
0009409     
Arg of perigee:    51
0088  deg
Mean anomaly:     309
1911  deg
Mean motion:   15
73172882  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             286
Checksum:              323


Coasting Arc #3 (Orbit 301)
---------------------------------------

Vector Time (GMT): 2009/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4183447
22                 A    =         6733922
50  meter
 Y    =        5113529
23  meter          E    =           
0023398
 Z    =        1241684
58                 I    =           51
88427
 XDOT =      -4455
437008                 Wp   =           56
88348
 YDOT =       2198
175665  meter/sec      RA   =           42
23387  deg
 ZDOT =       5891
711364                 TA   =          316
69447
                                          MA   =          316
87813
                                          Ha   =            194
655  n
mi
                                          Hp   =            182
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13725220
54                 X    =         4119924
09
 Y    =       16776670
69  feet           Y    =         5159955
63  meter
 Z    =        4073768
30                 Z    =         1261854
10
 XDOT =     -14617
575487                 XDOT =       -4508
307027
 YDOT =       7211
862417  feet/sec       YDOT =        2148
055969  meter/sec
 ZDOT =      19329
761692                 ZDOT =        5869
938780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20860562
01                 X    =         6358299
30
 Y    =       -5832951
68  feet           Y    =        -1777883
67  meter
 Z    =        4153019
84                 Z    =         1265840
45
 XDOT =        282
059126                 XDOT =          85
971622
 YDOT =      14863
896685  feet/sec       YDOT =        4530
515710  meter/sec
 ZDOT =      19244
560915                 ZDOT =        5865
742167


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   09149
56107861  
00010596  00000-0  82463-4 0  9029
2 25544  51
6427  42
4758 0009477  54
8824 305
3226 15
73145740  3028


Satellite: ISS
Catalog Number: 25544
Epoch time:      09149
56107861   =   yrday
fracday
Element set:     902
Inclination:       51
6427  deg
RA of node:        42
4758  deg
Eccentricity:     
0009477     
Arg of perigee:    54
8824  deg
Mean anomaly:     305
3226  deg
Mean motion:   15
73145740  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             302
Checksum:              307


Coasting Arc #4 (Orbit 316)
---------------------------------------

Vector Time (GMT): 2009/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3479900
76                 A    =         6722858
08  meter
 Y    =       -2495280
63  meter          E    =           
0022260
 Z    =       -5201156
86                 I    =           51
82487
 XDOT =       5475
688892                 Wp   =           82
70683
 YDOT =       5267
824827  meter/sec      RA   =           37
09786  deg
 ZDOT =       1143
235839                 TA   =          198
16323
                                          MA   =          198
24287
                                          Ha   =            194
582  n
mi
                                          Hp   =            182
042

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11416997
26                 X    =         3532811
03
 Y    =       -8186616
25  feet           Y    =        -2456069
93  meter
 Z    =      -17064162
93                 Z    =        -5184123
27
 XDOT =      17964
858568                 XDOT =        5410
822591
 YDOT =      17282
889851  feet/sec       YDOT =        5328
694364  meter/sec
 ZDOT =       3750
773750                 ZDOT =        1169
679738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3125392
79                 X    =         -952619
72
 Y    =      -13779320
52  feet           Y    =        -4199936
89  meter
 Z    =      -16997541
42                 Z    =        -5180850
62
 XDOT =      21851
634444                 XDOT =        6660
378178
 YDOT =      -9683
092197  feet/sec       YDOT =       -2951
406502  meter/sec
 ZDOT =       3854
613367                 ZDOT =        1174
886154


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   09150
51392399  
00010596  00000-0  82463-4 0  9039
2 25544  51
6430  37
5884 0009354  58
1839 302
0233 15
73194254  3176


Satellite: ISS
Catalog Number: 25544
Epoch time:      09150
51392399   =   yrday
fracday
Element set:     903
Inclination:       51
6430  deg
RA of node:        37
5884  deg
Eccentricity:     
0009354     
Arg of perigee:    58
1839  deg
Mean anomaly:     302
0233  deg
Mean motion:   15
73194254  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             317
Checksum:              305


Coasting Arc #5 (Orbit 332)
---------------------------------------

Vector Time (GMT): 2009/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5324936
28                 A    =         6734244
59  meter
 Y    =       -4046990
57  meter          E    =           
0015213
 Z    =        -776693
48                 I    =           51
83889
 XDOT =       3440
228893                 Wp   =          104
05549
 YDOT =      -3397
124500  meter/sec      RA   =           31
99924  deg
 ZDOT =      -5986
015675                 TA   =           84
38066
                                          MA   =           84
20718
                                          Ha   =            194
587  n
mi
                                          Hp   =            181
963

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17470263
39                 X    =        -5275513
34
 Y    =      -13277528
12  feet           Y    =        -4106260
71  meter
 Z    =       -2548206
95                 Z    =         -802442
44
 XDOT =      11286
840199                 XDOT =        3507
039486
 YDOT =     -11145
421587  feet/sec       YDOT =       -3358
279708  meter/sec
 ZDOT =     -19639
159038                 ZDOT =       -5969
141044

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18779766
57                 X    =        -5724072
85
 Y    =       11326869
54  feet           Y    =         3452429
84  meter
 Z    =       -2649265
65                 Z    =         -807496
17
 XDOT =      -5328
691573                 XDOT =       -1624
185191
 YDOT =     -13338
369650  feet/sec       YDOT =       -4065
535069  meter/sec
 ZDOT =     -19573
200639                 ZDOT =       -5965
911555


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   09151
53027853  
00010596  00000-0  82463-4 0  9043
2 25544  51
6432  32
3751 0009207  62
6792 297
5307 15
73171715  3334


Satellite: ISS
Catalog Number: 25544
Epoch time:      09151
53027853   =   yrday
fracday
Element set:     904
Inclination:       51
6432  deg
RA of node:        32
3751  deg
Eccentricity:     
0009207     
Arg of perigee:    62
6792  deg
Mean anomaly:     297
5307  deg
Mean motion:   15
73171715  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             333
Checksum:              297


Coasting Arc #6 (Orbit 348)
---------------------------------------

Vector Time (GMT): 2009/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2464817
81                 A    =         6722338
00  meter
 Y    =        3386198
33  meter          E    =           
0012154
 Z    =        5249214
67                 I    =           51
77386
 XDOT =      -6629
288347                 Wp   =           64
47302
 YDOT =      -3887
442714  meter/sec      RA   =           26
86835  deg
 ZDOT =       -598
897600                 TA   =           31
23900
                                          MA   =           31
16683
                                          Ha   =            194
587  n
mi
                                          Hp   =            181
773

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8086672
61                 X    =        -2527999
58
 Y    =       11109574
57  feet           Y    =         3358281
53  meter
 Z    =       17221832
89                 Z    =         5237087
35
 XDOT =     -21749
633683                 XDOT =       -6582
416242
 YDOT =     -12754
077145  feet/sec       YDOT =       -3961
313156  meter/sec
 ZDOT =      -1964
887140                 ZDOT =        -630
989439

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7507151
55                 X    =         2288179
79
 Y    =       11579665
22  feet           Y    =         3529481
96  meter
 Z    =       17174471
70                 Z    =         5234778
97
 XDOT =     -18758
932684                 XDOT =       -5717
722682
 YDOT =      15292
762677  feet/sec       YDOT =        4661
234064  meter/sec
 ZDOT =      -2090
782424                 ZDOT =        -637
270483


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   09152
54661458  
00010596  00000-0  82463-4 0  9051
2 25544  51
6434  27
1616 0009222  65
2502 294
9620 15
73257301  3495


Satellite: ISS
Catalog Number: 25544
Epoch time:      09152
54661458   =   yrday
fracday
Element set:     905
Inclination:       51
6434  deg
RA of node:        27
1616  deg
Eccentricity:     
0009222     
Arg of perigee:    65
2502  deg
Mean anomaly:     294
9620  deg
Mean motion:   15
73257301  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             349
Checksum:              296


Coasting Arc #7 (Orbit 364)
---------------------------------------

Vector Time (GMT): 2009/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6159511
54                 A    =         6734205
67  meter
 Y    =        2686961
01  meter          E    =           
0021661
 Z    =         269862
90                 I    =           51
78664
 XDOT =      -2141
654421                 Wp   =           56
31885
 YDOT =       4268
928235  meter/sec      RA   =           21
75648  deg
 ZDOT =       6044
293917                 TA   =          306
60845
                                          MA   =          306
80751
                                          Ha   =            194
491  n
mi
                                          Hp   =            181
691

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20208371
18                 X    =         6127696
73
 Y    =        8815488
87  feet           Y    =         2755662
35  meter
 Z    =         885376
97                 Z    =          299709
16
 XDOT =      -7026
425265                 XDOT =       -2218
593548
 YDOT =      14005
670061  feet/sec       YDOT =        4244
548181  meter/sec
 ZDOT =      19830
360619                 ZDOT =        6033
703199

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15102502
36                 X    =         4603242
72
 Y    =      -16055671
48  feet           Y    =        -4893768
67  meter
 Z    =        1002416
22                 Z    =          305536
47
 XDOT =       9613
353117                 XDOT =        2930
150030
 YDOT =      10338
464811  feet/sec       YDOT =        3151
164074  meter/sec
 ZDOT =      19789
055030                 ZDOT =        6031
703973


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   09153
56293618  
00010596  00000-0  82463-4 0  9064
2 25544  51
6431  21
9481 0009177  68
7918 291
4225 15
73275271  3659


Satellite: ISS
Catalog Number: 25544
Epoch time:      09153
56293618   =   yrday
fracday
Element set:     906
Inclination:       51
6431  deg
RA of node:        21
9481  deg
Eccentricity:     
0009177     
Arg of perigee:    68
7918  deg
Mean anomaly:     291
4225  deg
Mean motion:   15
73275271  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             365
Checksum:              323


Coasting Arc #8 (Orbit 379)
---------------------------------------

Vector Time (GMT): 2009/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1268644
69                 A    =         6722123
59  meter
 Y    =       -3977518
43  meter          E    =           
0023863
 Z    =       -5288756
21                 I    =           51
71724
 XDOT =       7344
365122                 Wp   =           83
26629
 YDOT =       2252
137798  meter/sec      RA   =           16
63023  deg
 ZDOT =         70
980119                 TA   =          187
39051
                                          MA   =          187
42574
                                          Ha   =            194
450  n
mi
                                          Hp   =            181
668

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4162220
12                 X    =         1338719
88
 Y    =      -13049601
14  feet           Y    =        -3962939
24  meter
 Z    =      -17351562
37                 Z    =        -5282423
32
 XDOT =      24095
686097                 XDOT =        7318
290670
 YDOT =       7388
903538  feet/sec       YDOT =        2334
120980  meter/sec
 ZDOT =        232
874407                 ZDOT =         106
596507

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10995972
18                 X    =        -3351572
32
 Y    =       -8219447
23  feet           Y    =        -2505287
52  meter
 Z    =      -17326920
27                 Z    =        -5281245
30
 XDOT =      14120
094410                 XDOT =        4303
804776
 YDOT =     -19654
230666  feet/sec       YDOT =       -5990
609507  meter/sec
 ZDOT =        372
494112                 ZDOT =         113
536205


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   09154
51572373  
00010596  00000-0  82463-4 0  9079
2 25544  51
6423  17
0599 0009137  71
8262 288
3895 15
73295042  3802


Satellite: ISS
Catalog Number: 25544
Epoch time:      09154
51572373   =   yrday
fracday
Element set:     907
Inclination:       51
6423  deg
RA of node:        17
0599  deg
Eccentricity:     
0009137     
Arg of perigee:    71
8262  deg
Mean anomaly:     288
3895  deg
Mean motion:   15
73295042  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             380
Checksum:              321


Coasting Arc #9 (Orbit 395)
---------------------------------------

Vector Time (GMT): 2009/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6613309
23                 A    =         6734227
44  meter
 Y    =       -1238771
38  meter          E    =           
0018946
 Z    =         133503
43                 I    =           51
72915
 XDOT =        746
881259                 Wp   =          109
45875
 YDOT =      -4712
426728  meter/sec      RA   =           11
50635  deg
 ZDOT =      -6042
012653                 TA   =           69
09332
                                          MA   =           68
89062
                                          Ha   =            194
476  n
mi
                                          Hp   =            181
665

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21697208
75                 X    =        -6599614
10
 Y    =       -4064210
56  feet           Y    =        -1312648
71  meter
 Z    =         438003
38                 Z    =          101408
55
 XDOT =       2450
397833                 XDOT =         828
872363
 YDOT =     -15460
717613  feet/sec       YDOT =       -4703
615358  meter/sec
 ZDOT =     -19822
876158                 ZDOT =       -6038
185767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10470020
35                 X    =        -3191262
20
 Y    =       19436041
57  feet           Y    =         5924105
47  meter
 Z    =         312224
02                 Z    =           95165
88
 XDOT =     -12531
576217                 XDOT =       -3819
624431
 YDOT =      -6381
699111  feet/sec       YDOT =       -1945
141889  meter/sec
 ZDOT =     -19808
076173                 ZDOT =       -6037
501618


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   09155
53201566  
00010596  00000-0  82463-4 0  9086
2 25544  51
6424  11
8469 0009094  76
3297 283
8878 15
73277845  3960


Satellite: ISS
Catalog Number: 25544
Epoch time:      09155
53201566   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:        11
8469  deg
Eccentricity:     
0009094     
Arg of perigee:    76
3297  deg
Mean anomaly:     283
8878  deg
Mean motion:   15
73277845  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             396
Checksum:              346


Coasting Arc #10 (Orbit 411)
---------------------------------------

Vector Time (GMT): 2009/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          -8819
08                 A    =         6722087
67  meter
 Y    =        4180589
84  meter          E    =           
0011407
 Z    =        5254146
14                 I    =           51
65856
 XDOT =      -7679
873190                 Wp   =           84
82005
 YDOT =       -532
250551  meter/sec      RA   =            6
38381  deg
 ZDOT =        410
859270                 TA   =            1
28522
                                          MA   =            1
28230
                                          Ha   =            194
451  n
mi
                                          Hp   =            181
572

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -28934
00                 X    =          -81090
56
 Y    =       13715845
92  feet           Y    =         4180086
25  meter
 Z    =       17238012
29                 Z    =         5253928
44
 XDOT =     -25196
434349                 XDOT =       -7675
346594
 YDOT =      -1746
228843  feet/sec       YDOT =        -618
106136  meter/sec
 ZDOT =       1347
963485                 ZDOT =         373
560788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13099372
20                 X    =         3992688
65
 Y    =        4068835
76  feet           Y    =         1240181
14  meter
 Z    =       17237324
55                 Z    =         5253936
52
 XDOT =      -8625
442928                 XDOT =       -2629
035004
 YDOT =      22681
138932  feet/sec       YDOT =        6913
211147  meter/sec
 ZDOT =       1201
827871                 ZDOT =         366
317135


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   09156
54829043  
00010596  00000-0  82463-4 0  9095
2 25544  51
6417   6
6325 0009069  79
4497 280
7687 15
73312701  4127


Satellite: ISS
Catalog Number: 25544
Epoch time:      09156
54829043   =   yrday
fracday
Element set:     909
Inclination:       51
6417  deg
RA of node:         6
6325  deg
Eccentricity:     
0009069     
Arg of perigee:    79
4497  deg
Mean anomaly:     280
7687  deg
Mean motion:   15
73312701  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             412
Checksum:              322


Coasting Arc #11 (Orbit 426)
---------------------------------------

Vector Time (GMT): 2009/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6696804
39                 A    =         6733927
51  meter
 Y    =        -309685
51  meter          E    =           
0018742
 Z    =        -575681
39                 I    =           51
66777
 XDOT =        723
388267                 Wp   =           59
03243
 YDOT =       4764
775286  meter/sec      RA   =            1
24546  deg
 ZDOT =       6004
970366                 TA   =          294
70590
                                          MA   =          294
90089
                                          Ha   =            194
388  n
mi
                                          Hp   =            181
546

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21971143
01                 X    =         6702566
21
 Y    =       -1016028
57  feet           Y    =         -234765
61  meter
 Z    =       -1888718
48                 Z    =         -543133
96
 XDOT =       2373
321087                 XDOT =         640
882555
 YDOT =      15632
464848  feet/sec       YDOT =        4772
402220  meter/sec
 ZDOT =      19701
346345                 ZDOT =        6008
285097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4981848
35                 X    =         1518467
38
 Y    =      -21433851
02  feet           Y    =        -6533037
79  meter
 Z    =       -1761225
28                 Z    =         -536821
46
 XDOT =      14096
746409                 XDOT =        4296
688305
 YDOT =       1700
809651  feet/sec       YDOT =         518
406782  meter/sec
 ZDOT =      19714
515405                 ZDOT =        6008
984295


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   09157
50103331  
00010596  00000-0  82463-4 0  9109
2 25544  51
6405   1
7437 0008957  82
5174 277
7006 15
73339588  4275


Satellite: ISS
Catalog Number: 25544
Epoch time:      09157
50103331   =   yrday
fracday
Element set:     910
Inclination:       51
6405  deg
RA of node:         1
7437  deg
Eccentricity:     
0008957     
Arg of perigee:    82
5174  deg
Mean anomaly:     277
7006  deg
Mean motion:   15
73339588  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             427
Checksum:              304


Coasting Arc #12 (Orbit 442)
---------------------------------------

Vector Time (GMT): 2009/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1229012
04                 A    =         6722111
21  meter
 Y    =       -4069877
23  meter          E    =           
0023673
 Z    =       -5227465
15                 I    =           51
59746
 XDOT =       7542
277929                 Wp   =           84
43744
 YDOT =      -1186
493652  meter/sec      RA   =          356
12585  deg
 ZDOT =       -850
534325                 TA   =          177
44686
                                          MA   =          177
43476
                                          Ha   =            194
322  n
mi
                                          Hp   =            181
419

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4032191
74                 X    =        -1158016
33
 Y    =      -13352615
58  feet           Y    =        -4083222
78  meter
 Z    =      -17150476
22                 Z    =        -5233264
09
 XDOT =      24745
006329                 XDOT =        7559
116719
 YDOT =      -3892
695710  feet/sec       YDOT =       -1102
057181  meter/sec
 ZDOT =      -2790
466947                 ZDOT =        -813
852923

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13914104
80                 X    =        -4241019
14
 Y    =         404392
39  feet           Y    =          123258
80  meter
 Z    =      -17173348
60                 Z    =        -5234436
65
 XDOT =       2567
322527                 XDOT =         782
519906
 YDOT =     -23921
464451  feet/sec       YDOT =       -7291
262365  meter/sec
 ZDOT =      -2646
807572                 ZDOT =        -806
746948


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   09158
51727777  
00010596  00000-0  82463-4 0  9118
2 25544  51
6394 356
5286 0008976  86
7408 273
4782 15
73373814  4434


Satellite: ISS
Catalog Number: 25544
Epoch time:      09158
51727777   =   yrday
fracday
Element set:     911
Inclination:       51
6394  deg
RA of node:       356
5286  deg
Eccentricity:     
0008976     
Arg of perigee:    86
7408  deg
Mean anomaly:     273
4782  deg
Mean motion:   15
73373814  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             443
Checksum:              352

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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