Date: April 14th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 23680 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


There are no maneuvers



Coasting Arc #1 (Orbit 1316)
---------------------------------------

Vector Time (GMT): 2010/102/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1668998
74                 A    =         6721758
05  meter
 Y    =       -4739030
11  meter          E    =           
0012570
 Z    =        4461052
47                 I    =           51
48908
 XDOT =       6993
704543                 Wp   =          129
06153
 YDOT =        547
110388  meter/sec      RA   =          205
64500  deg
 ZDOT =       3183
947180                 TA   =          288
98787
                                          MA   =          289
12403
                                          Ha   =            190
196  n
mi
                                          Hp   =            182
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5475717
65                 X    =        -1637553
19
 Y    =      -15547999
05  feet           Y    =        -4757517
68  meter
 Z    =       14635998
93                 Z    =         4453021
16
 XDOT =      22945
224879                 XDOT =        6971
599690
 YDOT =       1794
981587  feet/sec       YDOT =         625
194810  meter/sec
 ZDOT =      10446
020933                 ZDOT =        3217
869151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14242317
87                 X    =        -4341058
49
 Y    =        8355768
05  feet           Y    =         2546838
10  meter
 Z    =       14603894
85                 Z    =         4451267
15
 XDOT =      -1881
760896                 XDOT =        -573
560721
 YDOT =     -21779
506765  feet/sec       YDOT =       -6638
393662  meter/sec
 ZDOT =      10580
867498                 ZDOT =        3225
048413


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   10102
77743184  
00016717  00000-0  10270-3 0  9002
2 25544  51
6458 206
3604 0004677 162
8688 197
2634 15
74628882 13170


Satellite: ISS
Catalog Number: 25544
Epoch time:      10102
77743184   =   yrday
fracday
Element set:     900
Inclination:       51
6458  deg
RA of node:       206
3604  deg
Eccentricity:     
0004677     
Arg of perigee:   162
8688  deg
Mean anomaly:     197
2634  deg
Mean motion:   15
74628882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1317
Checksum:              326


Coasting Arc #2 (Orbit 1331)
---------------------------------------

Vector Time (GMT): 2010/103/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6215372
56                 A    =         6727164
31  meter
 Y    =        -132978
53  meter          E    =           
0005319
 Z    =       -2576953
82                 I    =           51
53734
 XDOT =      -2064
478293                 Wp   =          106
49146
 YDOT =      -5226
335858  meter/sec      RA   =          200
45069  deg
 ZDOT =       5256
482767                 TA   =          224
23137
                                          MA   =          224
27390
                                          Ha   =            189
932  n
mi
                                          Hp   =            182
048

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20391642
27                 X    =        -6200905
09
 Y    =        -436281
25  feet           Y    =         -202401
80  meter
 Z    =       -8454572
90                 Z    =        -2607113
34
 XDOT =      -6773
222745                 XDOT =       -2031
418408
 YDOT =     -17146
771188  feet/sec       YDOT =       -5249
236878  meter/sec
 ZDOT =      17245
678368                 ZDOT =        5246
534061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3698190
30                 X    =         1127208
40
 Y    =       20007281
48  feet           Y    =         6098219
40  meter
 Z    =       -8574455
94                 Z    =        -2613494
17
 XDOT =     -13936
736668                 XDOT =       -4247
917337
 YDOT =       9939
647609  feet/sec       YDOT =        3029
604591  meter/sec
 ZDOT =      17205
933426                 ZDOT =        5244
368508


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   10103
72937367  
00016717  00000-0  10270-3 0  9017
2 25544  51
6469 201
4683 0004627 166
5201 193
6087 15
74715780 13325


Satellite: ISS
Catalog Number: 25544
Epoch time:      10103
72937367   =   yrday
fracday
Element set:     901
Inclination:       51
6469  deg
RA of node:       201
4683  deg
Eccentricity:     
0004627     
Arg of perigee:   166
5201  deg
Mean anomaly:     193
6087  deg
Mean motion:   15
74715780  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1332
Checksum:              306


Coasting Arc #3 (Orbit 1347)
---------------------------------------

Vector Time (GMT): 2010/104/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1885438
80                 A    =         6720445
87  meter
 Y    =        4405616
85  meter          E    =           
0011295
 Z    =       -4721002
22                 I    =           51
54230
 XDOT =      -7210
131181                 Wp   =           94
29199
 YDOT =        225
094401  meter/sec      RA   =          195
34585  deg
 ZDOT =      -2675
786099                 TA   =          149
37371
                                          MA   =          149
30772
                                          Ha   =            189
776  n
mi
                                          Hp   =            182
274

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6185822
82                 X    =         1858968
42
 Y    =       14454123
52  feet           Y    =         4426552
71  meter
 Z    =      -15488852
42                 Z    =        -4711907
13
 XDOT =     -23655
286027                 XDOT =       -7199
113651
 YDOT =        738
498691  feet/sec       YDOT =         144
527892  meter/sec
 ZDOT =      -8778
825783                 ZDOT =       -2710
786733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12722216
46                 X    =         3877731
58
 Y    =       -9298123
49  feet           Y    =        -2834068
04  meter
 Z    =      -15452532
10                 Z    =        -4709931
78
 XDOT =       5226
215936                 XDOT =        1592
950617
 YDOT =      21937
010178  feet/sec       YDOT =        6686
400702  meter/sec
 ZDOT =      -8917
946818                 ZDOT =       -2718
190190


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   10104
74474687  
00016717  00000-0  10270-3 0  9022
2 25544  51
6459 196
2488 0004461 171
4304 188
6937 15
74734244 13484


Satellite: ISS
Catalog Number: 25544
Epoch time:      10104
74474687   =   yrday
fracday
Element set:     902
Inclination:       51
6459  deg
RA of node:       196
2488  deg
Eccentricity:     
0004461     
Arg of perigee:   171
4304  deg
Mean anomaly:     188
6937  deg
Mean motion:   15
74734244  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1348
Checksum:              330


Coasting Arc #4 (Orbit 1363)
---------------------------------------

Vector Time (GMT): 2010/105/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6363125
49                 A    =         6727932
35  meter
 Y    =        -540946
86  meter          E    =           
0016362
 Z    =        2087722
09                 I    =           51
59679
 XDOT =       2239
430793                 Wp   =          123
84104
 YDOT =       4865
122589  meter/sec      RA   =          190
15995  deg
 ZDOT =      -5542
964920                 TA   =           32
79832
                                          MA   =           32
69686
                                          Ha   =            189
489  n
mi
                                          Hp   =            182
216

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20876395
96                 X    =         6358559
57
 Y    =       -1774760
04  feet           Y    =         -469816
08  meter
 Z    =        6849481
92                 Z    =         2118623
63
 XDOT =       7347
213888                 XDOT =        2211
788885
 YDOT =      15961
688284  feet/sec       YDOT =        4890
010533  meter/sec
 ZDOT =     -18185
580445                 ZDOT =       -5532
152845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6649437
69                 X    =        -2026748
61
 Y    =      -19825765
86  feet           Y    =        -6042893
43  meter
 Z    =        6972307
42                 Z    =         2125159
30
 XDOT =      12301
168671                 XDOT =        3749
396211
 YDOT =     -10530
929654  feet/sec       YDOT =       -3209
827359  meter/sec
 ZDOT =     -18142
418027                 ZDOT =       -5529
809015


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   10105
76008726  
00016717  00000-0  10270-3 0  9033
2 25544  51
6448 191
0291 0004258 174
5338 185
5873 15
74802139 13644


Satellite: ISS
Catalog Number: 25544
Epoch time:      10105
76008726   =   yrday
fracday
Element set:     903
Inclination:       51
6448  deg
RA of node:       191
0291  deg
Eccentricity:     
0004258     
Arg of perigee:   174
5338  deg
Mean anomaly:     185
5873  deg
Mean motion:   15
74802139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1364
Checksum:              311


Coasting Arc #5 (Orbit 1379)
---------------------------------------

Vector Time (GMT): 2010/106/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1986254
85                 A    =         6719266
18  meter
 Y    =       -4102567
32  meter          E    =           
0009291
 Z    =        4934767
11                 I    =           51
59656
 XDOT =       7342
198699                 Wp   =          145
63222
 YDOT =      -1020
211436  meter/sec      RA   =          185
05176  deg
 ZDOT =       2097
635979                 TA   =          283
98441
                                          MA   =          284
08770
                                          Ha   =            189
452  n
mi
                                          Hp   =            182
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6516584
16                 X    =        -1964204
21
 Y    =      -13459866
53  feet           Y    =        -4124655
50  meter
 Z    =       16190180
81                 Z    =         4925171
29
 XDOT =      24088
578409                 XDOT =        7342
871076
 YDOT =      -3347
150379  feet/sec       YDOT =        -938
102837  meter/sec
 ZDOT =       6882
007804                 ZDOT =        2133
306645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11348186
35                 X    =        -3458927
20
 Y    =        9802612
35  feet           Y    =         2987836
24  meter
 Z    =       16151881
89                 Z    =         4923093
60
 XDOT =      -8608
680968                 XDOT =       -2623
925959
 YDOT =     -21590
412067  feet/sec       YDOT =       -6580
757598  meter/sec
 ZDOT =       7023
789826                 ZDOT =        2140
851139


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   10106
77539567  
00016717  00000-0  10270-3 0  9048
2 25544  51
6438 185
8092 0004188 179
5775 180
5393 15
74825358 13803


Satellite: ISS
Catalog Number: 25544
Epoch time:      10106
77539567   =   yrday
fracday
Element set:     904
Inclination:       51
6438  deg
RA of node:       185
8092  deg
Eccentricity:     
0004188     
Arg of perigee:   179
5775  deg
Mean anomaly:     180
5393  deg
Mean motion:   15
74825358  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1380
Checksum:              345


Coasting Arc #6 (Orbit 1394)
---------------------------------------

Vector Time (GMT): 2010/107/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6429989
93                 A    =         6728495
32  meter
 Y    =        1236900
02  meter          E    =           
0005287
 Z    =       -1546550
47                 I    =           51
65858
 XDOT =      -2261
743487                 Wp   =           65
61956
 YDOT =      -4561
258974  meter/sec      RA   =          179
87802  deg
 ZDOT =       5773
053509                 TA   =          277
33834
                                          MA   =          277
39842
                                          Ha   =            189
221  n
mi
                                          Hp   =            182
250

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21095767
48                 X    =        -6435830
29
 Y    =        4058070
94  feet           Y    =         1164963
42  meter
 Z    =       -5073984
47                 Z    =        -1577802
00
 XDOT =      -7420
418264                 XDOT =       -2238
615453
 YDOT =     -14964
760415  feet/sec       YDOT =       -4586
421931  meter/sec
 ZDOT =      18940
464269                 ZDOT =        5762
121881

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9588199
67                 X    =         2922483
26
 Y    =       19190876
88  feet           Y    =         5849379
27  meter
 Z    =       -5198205
01                 Z    =        -1584412
89
 XDOT =     -10979
445890                 XDOT =       -3346
535107
 YDOT =      10588
911112  feet/sec       YDOT =        3227
500107  meter/sec
 ZDOT =      18896
836982                 ZDOT =        5759
755912


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   10107
72721705  
00016717  00000-0  10270-3 0  9052
2 25544  51
6435 180
9162 0004208 181
4164 178
6989 15
74907583 13957


Satellite: ISS
Catalog Number: 25544
Epoch time:      10107
72721705   =   yrday
fracday
Element set:     905
Inclination:       51
6435  deg
RA of node:       180
9162  deg
Eccentricity:     
0004208     
Arg of perigee:   181
4164  deg
Mean anomaly:     178
6989  deg
Mean motion:   15
74907583  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1395
Checksum:              323


Coasting Arc #7 (Orbit 1410)
---------------------------------------

Vector Time (GMT): 2010/108/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1924114
69                 A    =         6718167
35  meter
 Y    =        3900160
94  meter          E    =           
0013299
 Z    =       -5131615
94                 I    =           51
65324
 XDOT =      -7350
034282                 Wp   =           96
13019
 YDOT =       1787
407919  meter/sec      RA   =          174
76278  deg
 ZDOT =      -1401
932123                 TA   =          160
45926
                                          MA   =          160
40824
                                          Ha   =            189
054  n
mi
                                          Hp   =            182
456

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6312712
23                 X    =         1905288
13
 Y    =       12795803
61  feet           Y    =         3921572
44  meter
 Z    =      -16836010
29                 Z    =        -5122314
08
 XDOT =     -24114
285702                 XDOT =       -7362
664712
 YDOT =       5864
199208  feet/sec       YDOT =        1705
144891  meter/sec
 ZDOT =      -4599
514838                 ZDOT =       -1437
669616

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10425226
03                 X    =         3177608
89
 Y    =       -9805421
94  feet           Y    =        -2988692
61  meter
 Z    =      -16798884
82                 Z    =        -5120300
09
 XDOT =      11797
107040                 XDOT =        3595
758226
 YDOT =      20640
884138  feet/sec       YDOT =        6291
341485  meter/sec
 ZDOT =      -4741
573376                 ZDOT =       -1445
231565


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   10108
74246273  
00016717  00000-0  10270-3 0  9068
2 25544  51
6428 175
6948 0004018 187
0100 173
1008 15
74920123 14119


Satellite: ISS
Catalog Number: 25544
Epoch time:      10108
74246273   =   yrday
fracday
Element set:     906
Inclination:       51
6428  deg
RA of node:       175
6948  deg
Eccentricity:     
0004018     
Arg of perigee:   187
0100  deg
Mean anomaly:     173
1008  deg
Mean motion:   15
74920123  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1411
Checksum:              281


Coasting Arc #8 (Orbit 1426)
---------------------------------------

Vector Time (GMT): 2010/109/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6388122
72                 A    =         6728980
88  meter
 Y    =       -1886442
56  meter          E    =           
0015554
 Z    =         890303
98                 I    =           51
72055
 XDOT =       2134
549810                 Wp   =          138
53982
 YDOT =       4392
036204  meter/sec      RA   =          169
60284  deg
 ZDOT =      -5962
140088                 TA   =           31
74387
                                          MA   =           31
65019
                                          Ha   =            188
772  n
mi
                                          Hp   =            182
408

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20958407
89                 X    =         6404417
52
 Y    =       -6189116
03  feet           Y    =        -1814915
70  meter
 Z    =        2920944
80                 Z    =          921377
19
 XDOT =       7003
116173                 XDOT =        2114
241817
 YDOT =      14409
567597  feet/sec       YDOT =        4415
792689  meter/sec
 ZDOT =     -19560
827060                 ZDOT =       -5951
819537

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12236083
78                 X    =        -3729558
34
 Y    =      -18085944
78  feet           Y    =        -5512595
97  meter
 Z    =        3044469
11                 Z    =          927954
18
 XDOT =      10260
403778                 XDOT =        3127
371072
 YDOT =     -10252
693825  feet/sec       YDOT =       -3125
021078  meter/sec
 ZDOT =     -19519
630027                 ZDOT =       -5949
583232


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   10109
75767588  
00016717  00000-0  10270-3 0  9078
2 25544  51
6428 170
4741 0003809 192
2389 167
8683 15
74993561 14279


Satellite: ISS
Catalog Number: 25544
Epoch time:      10109
75767588   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:       170
4741  deg
Eccentricity:     
0003809     
Arg of perigee:   192
2389  deg
Mean anomaly:     167
8683  deg
Mean motion:   15
74993561  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1427
Checksum:              351


Coasting Arc #9 (Orbit 1442)
---------------------------------------

Vector Time (GMT): 2010/110/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1785531
19                 A    =         6717332
85  meter
 Y    =       -3799727
31  meter          E    =           
0005227
 Z    =        5242854
72                 I    =           51
71089
 XDOT =       7249
423425                 Wp   =          163
03295
 YDOT =      -2529
688922  meter/sec      RA   =          164
48018  deg
 ZDOT =        630
456623                 TA   =          280
95294
                                          MA   =          281
01174
                                          Ha   =            188
695  n
mi
                                          Hp   =            182
509

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5858041
95                 X    =        -1768378
14
 Y    =      -12466296
95  feet           Y    =        -3819598
43  meter
 Z    =       17200966
92                 Z    =         5234222
14
 XDOT =      23784
197589                 XDOT =        7274
109414
 YDOT =      -8299
504338  feet/sec       YDOT =       -2448
483550  meter/sec
 ZDOT =       2068
427242                 ZDOT =         665
734284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9913805
28                 X    =        -3021727
85
 Y    =        9624251
92  feet           Y    =         2933471
98  meter
 Z    =       17166499
88                 Z    =         5232349
16
 XDOT =     -14746
678212                 XDOT =       -4494
787519
 YDOT =     -19159
582622  feet/sec       YDOT =       -5839
840783  meter/sec
 ZDOT =       2208
671590                 ZDOT =         673
203101


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   10110
77285817  
00016717  00000-0  10270-3 0  9083
2 25544  51
6427 165
2535 0003802 197
1513 162
9523 15
75021754 14431


Satellite: ISS
Catalog Number: 25544
Epoch time:      10110
77285817   =   yrday
fracday
Element set:     908
Inclination:       51
6427  deg
RA of node:       165
2535  deg
Eccentricity:     
0003802     
Arg of perigee:   197
1513  deg
Mean anomaly:     162
9523  deg
Mean motion:   15
75021754  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1443
Checksum:              298


Coasting Arc #10 (Orbit 1457)
---------------------------------------

Vector Time (GMT): 2010/111/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6237294
45                 A    =         6729027
68  meter
 Y    =        2509749
79  meter          E    =           
0008455
 Z    =        -187090
33                 I    =           51
77999
 XDOT =      -1930
045869                 Wp   =           54
62555
 YDOT =      -4360
477632  meter/sec      RA   =          159
33689  deg
 ZDOT =       6045
849666                 TA   =          303
34541
                                          MA   =          303
42632
                                          Ha   =            188
466  n
mi
                                          Hp   =            182
463

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20463564
46                 X    =        -6263986
50
 Y    =        8234087
23  feet           Y    =         2439851
41  meter
 Z    =        -613813
41                 Z    =         -217455
88
 XDOT =      -6332
171486                 XDOT =       -1910
512403
 YDOT =     -14306
028977  feet/sec       YDOT =       -4381
951411  meter/sec
 ZDOT =      19835
464784                 ZDOT =        6036
520903

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14616322
33                 X    =         4455055
05
 Y    =       16515387
12  feet           Y    =         5033890
00  meter
 Z    =        -734533
54                 Z    =         -223885
82
 XDOT =     -10111
536437                 XDOT =       -3081
996306
 YDOT =       9805
544054  feet/sec       YDOT =        2988
729828  meter/sec
 ZDOT =      19798
205039                 ZDOT =        6034
492896


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   10111
72456202  
00016717  00000-0  10270-3 0  9098
2 25544  51
6427 160
3589 0003849 198
9121 161
1900 15
75097567 14582


Satellite: ISS
Catalog Number: 25544
Epoch time:      10111
72456202   =   yrday
fracday
Element set:     909
Inclination:       51
6427  deg
RA of node:       160
3589  deg
Eccentricity:     
0003849     
Arg of perigee:   198
9121  deg
Mean anomaly:     161
1900  deg
Mean motion:   15
75097567  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1458
Checksum:              314


Coasting Arc #11 (Orbit 1473)
---------------------------------------

Vector Time (GMT): 2010/112/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1569846
44                 A    =         6716936
32  meter
 Y    =        3860700
26  meter          E    =           
0013978
 Z    =       -5279247
69                 I    =           51
76811
 XDOT =      -7002
392544                 Wp   =          105
90470
 YDOT =       3176
736094  meter/sec      RA   =          154
20259  deg
 ZDOT =        237
661894                 TA   =          166
36817
                                          MA   =          166
33038
                                          Ha   =            188
277  n
mi
                                          Hp   =            182
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5150414
81                 X    =         1552204
32
 Y    =       12666339
44  feet           Y    =         3878156
52  meter
 Z    =      -17320366
45                 Z    =        -5271664
28
 XDOT =     -22973
728818                 XDOT =       -7038
549459
 YDOT =      10422
362512  feet/sec       YDOT =        3098
229011  meter/sec
 ZDOT =        779
730623                 ZDOT =         203
556454

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10012569
95                 X    =         3051831
32
 Y    =       -9368038
73  feet           Y    =        -2855378
20  meter
 Z    =      -17290064
05                 Z    =        -5270011
52
 XDOT =      17148
792044                 XDOT =        5226
951815
 YDOT =      17120
181120  feet/sec       YDOT =        5218
231205  meter/sec
 ZDOT =        644
140594                 ZDOT =         196
334053


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   10112
73968273  
00016717  00000-0  10270-3 0  9108
2 25544  51
6436 155
1373 0003690 205
3174 154
7809 15
75115245 14748


Satellite: ISS
Catalog Number: 25544
Epoch time:      10112
73968273   =   yrday
fracday
Element set:     910
Inclination:       51
6436  deg
RA of node:       155
1373  deg
Eccentricity:     
0003690     
Arg of perigee:   205
3174  deg
Mean anomaly:     154
7809  deg
Mean motion:   15
75115245  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1474
Checksum:              300


Coasting Arc #12 (Orbit 1489)
---------------------------------------

Vector Time (GMT): 2010/113/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5974944
86                 A    =         6728698
72  meter
 Y    =       -3016753
91  meter          E    =           
0012644
 Z    =        -613754
89                 I    =           51
83560
 XDOT =       1666
830466                 Wp   =          155
47143
 YDOT =       4514
317020  meter/sec      RA   =          149
07811  deg
 ZDOT =      -6017
461019                 TA   =           31
19790
                                          MA   =           31
12291
                                          Ha   =            188
113  n
mi
                                          Hp   =            182
573

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19602837
45                 X    =         6011216
18
 Y    =       -9897486
60  feet           Y    =        -2949735
74  meter
 Z    =       -2013631
52                 Z    =         -584640
38
 XDOT =       5468
603891                 XDOT =        1645
458448
 YDOT =      14810
751377  feet/sec       YDOT =        4532
836822  meter/sec
 ZDOT =     -19742
326178                 ZDOT =       -6009
415605

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16412290
43                 X    =        -5002466
12
 Y    =      -14605510
88  feet           Y    =        -4451759
72  meter
 Z    =       -1897884
03                 Z    =         -578475
05
 XDOT =      10657
085216                 XDOT =        3248
279574
 YDOT =      -9439
196483  feet/sec       YDOT =       -2877
067088  meter/sec
 ZDOT =     -19710
161606                 ZDOT =       -6007
657258


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   10113
75477191  
00016717  00000-0  10270-3 0  9116
2 25544  51
6442 149
9161 0003632 210
2546 149
8408 15
75172244 14905


Satellite: ISS
Catalog Number: 25544
Epoch time:      10113
75477191   =   yrday
fracday
Element set:     911
Inclination:       51
6442  deg
RA of node:       149
9161  deg
Eccentricity:     
0003632     
Arg of perigee:   210
2546  deg
Mean anomaly:     149
8408  deg
Mean motion:   15
75172244  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1490
Checksum:              295


Coasting Arc #13 (Orbit 1505)
---------------------------------------

Vector Time (GMT): 2010/114/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1353262
90                 A    =         6717037
30  meter
 Y    =       -4053973
03  meter          E    =           
0001416
 Z    =        5180818
15                 I    =           51
82228
 XDOT =       6650
922912                 Wp   =          124
83814
 YDOT =      -3709
765155  meter/sec      RA   =          143
93247  deg
 ZDOT =      -1166
184504                 TA   =          336
26052
                                          MA   =          336
26705
                                          Ha   =            187
961  n
mi
                                          Hp   =            182
586

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4439838
92                 X    =        -1332997
69
 Y    =      -13300436
46  feet           Y    =        -4068992
49  meter
 Z    =       16997434
86                 Z    =         5174293
36
 XDOT =      21820
613229                 XDOT =        6697
577003
 YDOT =     -12171
145523  feet/sec       YDOT =       -3635
129769  meter/sec
 ZDOT =      -3826
064646                 ZDOT =       -1133
760664

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10543207
68                 X    =        -3213569
70
 Y    =        9291989
21  feet           Y    =         2832198
31  meter
 Z    =       16971337
01                 Z    =         5172863
52
 XDOT =     -18937
822036                 XDOT =       -5772
248157
 YDOT =     -14738
646584  feet/sec       YDOT =       -4492
339479  meter/sec
 ZDOT =      -3697
162489                 ZDOT =       -1126
895127


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   10114
76982975  
00016717  00000-0  10270-3 0  9120
2 25544  51
6443 144
6953 0003594 214
5464 145
5467 15
75219357 15063


Satellite: ISS
Catalog Number: 25544
Epoch time:      10114
76982975   =   yrday
fracday
Element set:     912
Inclination:       51
6443  deg
RA of node:       144
6953  deg
Eccentricity:     
0003594     
Arg of perigee:   214
5464  deg
Mean anomaly:     145
5467  deg
Mean motion:   15
75219357  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1506
Checksum:              327


Coasting Arc #14 (Orbit 1521)
---------------------------------------

Vector Time (GMT): 2010/115/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5611752
95                 A    =         6727699
20  meter
 Y    =        3414033
13  meter          E    =           
0010763
 Z    =        1433525
66                 I    =           51
88200
 XDOT =      -1436
299905                 Wp   =           68
08391
 YDOT =      -4822
430056  meter/sec      RA   =          138
82548  deg
 ZDOT =       5831
545729                 TA   =          307
64075
                                          MA   =          307
73836
                                          Ha   =            187
719  n
mi
                                          Hp   =            182
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18411262
97                 X    =        -5656476
09
 Y    =       11200896
11  feet           Y    =         3351029
17  meter
 Z    =        4703168
16                 Z    =         1406154
69
 XDOT =      -4712
270028                 XDOT =       -1410
596784
 YDOT =     -15821
620918  feet/sec       YDOT =       -4838
347663  meter/sec
 ZDOT =      19132
367878                 ZDOT =        5824
630740

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17630715
74                 X    =         5373842
16
 Y    =       12433995
33  feet           Y    =         3789881
78  meter
 Z    =        4594354
31                 Z    =         1400359
19
 XDOT =     -11672
848935                 XDOT =       -3557
884355
 YDOT =       9454
096817  feet/sec       YDOT =        2881
608710  meter/sec
 ZDOT =      19104
695450                 ZDOT =        5823
111173


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   10115
78485524  
00016717  00000-0  10270-3 0  9132
2 25544  51
6440 139
4731 0003611 218
8956 141
1949 15
75275425 15222


Satellite: ISS
Catalog Number: 25544
Epoch time:      10115
78485524   =   yrday
fracday
Element set:     913
Inclination:       51
6440  deg
RA of node:       139
4731  deg
Eccentricity:     
0003611     
Arg of perigee:   218
8956  deg
Mean anomaly:     141
1949  deg
Mean motion:   15
75275425  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1522
Checksum:              308


Coasting Arc #15 (Orbit 1536)
---------------------------------------

Vector Time (GMT): 2010/116/17:22:44
831
Vector Time (MET): N/A
Weight (LBS)     : 797575
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1169382
16                 A    =         6717811
28  meter
 Y    =        4401070
79  meter          E    =           
0011521
 Z    =       -4949167
51                 I    =           51
87128
 XDOT =      -6183
759122                 Wp   =          121
61996
 YDOT =       4048
987239  meter/sec      RA   =          133
66631  deg
 ZDOT =       2137
205075                 TA   =          169
07044
                                          MA   =          169
04539
                                          Ha   =            187
525  n
mi
                                          Hp   =            182
648

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3836555
65                 X    =         1144124
24
 Y    =       14439208
62  feet           Y    =         4414006
16  meter
 Z    =      -16237426
23                 Z    =        -4943548
04
 XDOT =     -20287
923629                 XDOT =       -6238
958355
 YDOT =      13284
078869  feet/sec       YDOT =        3979
528186  meter/sec
 ZDOT =       7011
827674                 ZDOT =        2107
029696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11505647
82                 X    =         3506921
46
 Y    =       -9568702
91  feet           Y    =        -2916540
65  meter
 Z    =      -16214928
56                 Z    =        -4942310
23
 XDOT =      19823
983184                 XDOT =        6042
350075
 YDOT =      12145
315706  feet/sec       YDOT =        3701
892227  meter/sec
 ZDOT =       6891
861858                 ZDOT =        2100
639494


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   10116
73641318  
00016717  00000-0  10270-3 0  9144
2 25544  51
6441 134
5772 0003554 223
5724 136
5159 15
75316899 15374


Satellite: ISS
Catalog Number: 25544
Epoch time:      10116
73641318   =   yrday
fracday
Element set:     914
Inclination:       51
6441  deg
RA of node:       134
5772  deg
Eccentricity:     
0003554     
Arg of perigee:   223
5724  deg
Mean anomaly:     136
5159  deg
Mean motion:   15
75316899  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1537
Checksum:              312

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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