Date: May 25th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


146/06:34:54 275 1 4 -2 4 2 4
N/A -1 5 0 0 190 6
000/00:09:48 549 -1 3 0 1 182 4

Coasting Arc #1 (Orbit 1962)
---------------------------------------

Vector Time (GMT): 2010/143/17:47:10
694
Vector Time (MET): N/A
Weight (LBS)     : 816526
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1022699
64                 A    =         6719464
79  meter
 Y    =        4083118
63  meter          E    =           
0008756
 Z    =        5237144
51                 I    =           51
60192
 XDOT =      -7597
015721                 Wp   =          358
14120
 YDOT =       1100
455643  meter/sec      RA   =          355
51207  deg
 ZDOT =        634
195155                 TA   =           85
87824
                                          MA   =           85
77816
                                          Ha   =            191
537  n
mi
                                          Hp   =            183
137

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3355313
78                 X    =          951523
99
 Y    =       13396058
48  feet           Y    =         4094156
74  meter
 Z    =       17182232
64                 Z    =         5241940
25
 XDOT =     -24924
592259                 XDOT =       -7611
837432
 YDOT =       3610
418776  feet/sec       YDOT =        1015
418372  meter/sec
 ZDOT =       2080
692767                 ZDOT =         597
252389

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4510360
81                 X    =         1374757
98
 Y    =      -13027386
01  feet           Y    =        -3970747
26  meter
 Z    =       17201322
36                 Z    =         5242963
05
 XDOT =      21975
847822                 XDOT =        6698
238416
 YDOT =      10124
225990  feet/sec       YDOT =        3085
864082  meter/sec
 ZDOT =       1933
554688                 ZDOT =         589
347469


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   10143
78971739  
00016717  00000-0  10270-3 0  9007
2 25544  51
6473 355
7639 0010323 344
3768  15
7076 15
74259033 19634


Satellite: ISS
Catalog Number: 25544
Epoch time:      10143
78971739   =   yrday
fracday
Element set:     900
Inclination:       51
6473  deg
RA of node:       355
7639  deg
Eccentricity:     
0010323     
Arg of perigee:   344
3768  deg
Mean anomaly:      15
7076  deg
Mean motion:   15
74259033  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1963
Checksum:              325


Coasting Arc #2 (Orbit 1977)
---------------------------------------

Vector Time (GMT): 2010/144/17:47:10
694
Vector Time (MET): N/A
Weight (LBS)     : 816526
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6537213
49                 A    =         6731397
71  meter
 Y    =       -1482422
14  meter          E    =           
0019425
 Z    =        -463510
98                 I    =           51
61227
 XDOT =       1461
897133                 Wp   =           16
04157
 YDOT =       4588
950381  meter/sec      RA   =          350
36365  deg
 ZDOT =       6019
519398                 TA   =          338
90940
                                          MA   =          338
98939
                                          Ha   =            191
739  n
mi
                                          Hp   =            182
894

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21447550
84                 X    =         6555556
03
 Y    =       -4863589
70  feet           Y    =        -1409216
53  meter
 Z    =       -1520705
30                 Z    =         -431708
20
 XDOT =       4796
250435                 XDOT =        1381
231749
 YDOT =      15055
611487  feet/sec       YDOT =        4604
846617  meter/sec
 ZDOT =      19749
079391                 ZDOT =        6026
425898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20802887
06                 X    =        -6340719
98
 Y    =       -7159680
63  feet           Y    =        -2182270
66  meter
 Z    =       -1394040
64                 Z    =         -424903
59
 XDOT =       3424
944432                 XDOT =        1043
923063
 YDOT =     -13747
687566  feet/sec       YDOT =       -4190
295170  meter/sec
 ZDOT =      19776
569704                 ZDOT =        6027
898446


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   10144
74191293  
00016717  00000-0  10270-3 0  9014
2 25544  51
6478 350
8734 0010371 348
6008  11
4919 15
74247881 19781


Satellite: ISS
Catalog Number: 25544
Epoch time:      10144
74191293   =   yrday
fracday
Element set:     901
Inclination:       51
6478  deg
RA of node:       350
8734  deg
Eccentricity:     
0010371     
Arg of perigee:   348
6008  deg
Mean anomaly:      11
4919  deg
Mean motion:   15
74247881  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1978
Checksum:              319


Coasting Arc #3 (Orbit 1993)
---------------------------------------

Vector Time (GMT): 2010/145/17:47:10
694
Vector Time (MET): N/A
Weight (LBS)     : 816526
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1503029
19                 A    =         6719305
20  meter
 Y    =       -3921794
76  meter          E    =           
0017473
 Z    =       -5257140
00                 I    =           51
54230
 XDOT =       7339
667842                 Wp   =           50
37537
 YDOT =      -2263
459834  meter/sec      RA   =          345
23048  deg
 ZDOT =       -399
835473                 TA   =          215
75948
                                          MA   =          215
87661
                                          Ha   =            191
766  n
mi
                                          Hp   =            182
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4931198
14                 X    =        -1433524
54
 Y    =      -12866780
70  feet           Y    =        -3938213
29  meter
 Z    =      -17247834
64                 Z    =        -5264273
48
 XDOT =      24080
275073                 XDOT =        7366
375118
 YDOT =      -7426
049323  feet/sec       YDOT =       -2181
233923  meter/sec
 ZDOT =      -1311
796172                 ZDOT =        -364
114068

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2435180
61                 X    =         -742243
05
 Y    =       13526286
58  feet           Y    =         4122812
15  meter
 Z    =      -17276227
23                 Z    =        -5265794
06
 XDOT =     -23508
678474                 XDOT =       -7165
445199
 YDOT =      -5768
207662  feet/sec       YDOT =       -1758
149695  meter/sec
 ZDOT =      -1169
522455                 ZDOT =        -356
470444


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   10145
75757077  
00016717  00000-0  10270-3 0  9025
2 25544  51
6477 345
6570 0010411 352
1265   7
9733 15
74294257 19941


Satellite: ISS
Catalog Number: 25544
Epoch time:      10145
75757077   =   yrday
fracday
Element set:     902
Inclination:       51
6477  deg
RA of node:       345
6570  deg
Eccentricity:     
0010411     
Arg of perigee:   352
1265  deg
Mean anomaly:       7
9733  deg
Mean motion:   15
74294257  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1994
Checksum:              320


Coasting Arc #4 (Orbit 2002)
---------------------------------------

Vector Time (GMT): 2010/146/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3444934
42                 A    =         6719315
69  meter
 Y    =        3009975
50  meter          E    =           
0006673
 Z    =        4917316
90                 I    =           51
53080
 XDOT =      -6358
831121                 Wp   =           22
99124
 YDOT =       3789
620739  meter/sec      RA   =          342
48747  deg
 ZDOT =       2140
197383                 TA   =           46
25852
                                          MA   =           46
20330
                                          Ha   =            190
563  n
mi
                                          Hp   =            182
353

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11302278
27                 X    =         3387132
40
 Y    =        9875247
70  feet           Y    =         3048174
98  meter
 Z    =       16132929
45                 Z    =         4933912
69
 XDOT =     -20862
306827                 XDOT =       -6411
131624
 YDOT =      12433
138909  feet/sec       YDOT =        3718
219799  meter/sec
 ZDOT =       7021
644958                 ZDOT =        2109
179045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7809528
82                 X    =         2380344
38
 Y    =       12733294
45  feet           Y    =         3881108
15  meter
 Z    =       16199009
10                 Z    =         4937457
98
 XDOT =     -22705
810884                 XDOT =       -6920
731157
 YDOT =       5171
312268  feet/sec       YDOT =        1576
215979  meter/sec
 ZDOT =       6898
093212                 ZDOT =        2102
538811


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10146
32885173  
00016717  00000-0  10270-3 0  9039
2 25544  51
6470 342
7250 0009854 345
5820  14
5062 15
74782757 20037


Satellite: ISS
Catalog Number: 25544
Epoch time:      10146
32885173   =   yrday
fracday
Element set:     903
Inclination:       51
6470  deg
RA of node:       342
7250  deg
Eccentricity:     
0009854     
Arg of perigee:   345
5820  deg
Mean anomaly:      14
5062  deg
Mean motion:   15
74782757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2003
Checksum:              300


Coasting Arc #5 (Orbit 2017)
---------------------------------------

Vector Time (GMT): 2010/147/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5404056
78                 A    =         6728846
81  meter
 Y    =       -3651183
76  meter          E    =           
0016519
 Z    =       -1615696
63                 I    =           51
53451
 XDOT =       3939
490639                 Wp   =           10
20300
 YDOT =       3299
610004  meter/sec      RA   =          337
30625  deg
 ZDOT =       5744
872534                 TA   =          331
91156
                                          MA   =          332
00060
                                          Ha   =            190
835  n
mi
                                          Hp   =            182
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17729845
07                 X    =         5452332
22
 Y    =      -11978949
35  feet           Y    =        -3590482
21  meter
 Z    =       -5300841
95                 Z    =        -1589326
57
 XDOT =      12924
838056                 XDOT =        3874
392997
 YDOT =      10825
492139  feet/sec       YDOT =        3343
298883  meter/sec
 ZDOT =      18848
007000                 ZDOT =        5763
853276

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20386867
36                 X    =         6213917
17
 Y    =       -6581859
20  feet           Y    =        -2006150
68  meter
 Z    =       -5195799
06                 Z    =        -1583679
55
 XDOT =       8827
267084                 XDOT =        2690
551007
 YDOT =      12469
143242  feet/sec       YDOT =        3800
594860  meter/sec
 ZDOT =      18923
582038                 ZDOT =        5767
907805


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10147
28072647  
00016717  00000-0  10270-3 0  9040
2 25544  51
6473 337
8315 0009990 349
2649  10
8300 15
74786320 20188


Satellite: ISS
Catalog Number: 25544
Epoch time:      10147
28072647   =   yrday
fracday
Element set:     904
Inclination:       51
6473  deg
RA of node:       337
8315  deg
Eccentricity:     
0009990     
Arg of perigee:   349
2649  deg
Mean anomaly:      10
8300  deg
Mean motion:   15
74786320  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2018
Checksum:              312


Coasting Arc #6 (Orbit 2033)
---------------------------------------

Vector Time (GMT): 2010/148/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3405670
86                 A    =         6718459
41  meter
 Y    =       -2785889
51  meter          E    =           
0017795
 Z    =       -5090708
99                 I    =           51
47322
 XDOT =       6013
004956                 Wp   =           44
03285
 YDOT =      -4545
934225  meter/sec      RA   =          332
18279  deg
 ZDOT =      -1525
530821                 TA   =          211
22650
                                          MA   =          211
33234
                                          Ha   =            190
854  n
mi
                                          Hp   =            181
698

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11173460
84                 X    =        -3349535
37
 Y    =       -9140057
44  feet           Y    =        -2823659
02  meter
 Z    =      -16701801
15                 Z    =        -5107118
07
 XDOT =      19727
706547                 XDOT =        6070
802356
 YDOT =     -14914
482365  feet/sec       YDOT =       -4478
369807  meter/sec
 ZDOT =      -5005
022380                 ZDOT =       -1496
179629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8307057
54                 X    =        -2531991
14
 Y    =      -11712938
18  feet           Y    =        -3570103
56  meter
 Z    =      -16767137
89                 Z    =        -5110623
63
 XDOT =      22109
213389                 XDOT =        6738
888241
 YDOT =      -8639
034400  feet/sec       YDOT =       -2633
177685  meter/sec
 ZDOT =      -4888
096577                 ZDOT =       -1489
891837


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10148
29604149  
00016717  00000-0  10270-3 0  9051
2 25544  51
6479 332
6116 0010040 353
3892   6
7138 15
74836680 20346


Satellite: ISS
Catalog Number: 25544
Epoch time:      10148
29604149   =   yrday
fracday
Element set:     905
Inclination:       51
6479  deg
RA of node:       332
6116  deg
Eccentricity:     
0010040     
Arg of perigee:   353
3892  deg
Mean anomaly:       6
7138  deg
Mean motion:   15
74836680  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2034
Checksum:              301


Coasting Arc #7 (Orbit 2049)
---------------------------------------

Vector Time (GMT): 2010/149/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5088258
21                 A    =         6729397
62  meter
 Y    =        4281701
09  meter          E    =           
0011023
 Z    =        1030840
18                 I    =           51
48354
 XDOT =      -3829
491849                 Wp   =           77
97233
 YDOT =      -3116
143727  meter/sec      RA   =          327
00676  deg
 ZDOT =      -5903
883522                 TA   =           90
73748
                                          MA   =           90
61117
                                          Ha   =            191
001  n
mi
                                          Hp   =            181
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16693760
54                 X    =        -5140766
47
 Y    =       14047575
76  feet           Y    =         4224507
39  meter
 Z    =        3382021
59                 Z    =         1005994
42
 XDOT =     -12563
949637                 XDOT =       -3765
681716
 YDOT =     -10223
568657  feet/sec       YDOT =       -3158
609569  meter/sec
 ZDOT =     -19369
696596                 ZDOT =       -5922
332902

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19637878
80                 X    =        -5985625
46
 Y    =        9540936
80  feet           Y    =         2908077
54  meter
 Z    =        3283037
77                 Z    =         1000669
91
 XDOT =      -8880
051212                 XDOT =       -2706
639609
 YDOT =     -11522
795229  feet/sec       YDOT =       -3512
147986  meter/sec
 ZDOT =     -19443
160165                 ZDOT =       -5926
275218


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10149
31133983  
00016717  00000-0  10270-3 0  9069
2 25544  51
6478 327
3915 0009973 356
9200   3
1900 15
74822548 20502


Satellite: ISS
Catalog Number: 25544
Epoch time:      10149
31133983   =   yrday
fracday
Element set:     906
Inclination:       51
6478  deg
RA of node:       327
3915  deg
Eccentricity:     
0009973     
Arg of perigee:   356
9200  deg
Mean anomaly:       3
1900  deg
Mean motion:   15
74822548  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2050
Checksum:              305


Coasting Arc #8 (Orbit 2065)
---------------------------------------

Vector Time (GMT): 2010/150/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3293218
26                 A    =         6717763
25  meter
 Y    =        2687040
61  meter          E    =           
0008956
 Z    =        5198810
21                 I    =           51
42072
 XDOT =      -5588
335538                 Wp   =           17
83582
 YDOT =       5238
914284  meter/sec      RA   =          321
86815  deg
 ZDOT =        840
218842                 TA   =           64
19282
                                          MA   =           64
10045
                                          Ha   =            190
964  n
mi
                                          Hp   =            181
335

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10804521
84                 X    =         3237671
55
 Y    =        8815750
03  feet           Y    =         2723555
85  meter
 Z    =       17056463
93                 Z    =         5214674
27
 XDOT =     -18334
434181                 XDOT =       -5650
584330
 YDOT =      17188
038988  feet/sec       YDOT =        5176
073991  meter/sec
 ZDOT =       2756
623496                 ZDOT =         812
920306

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8417496
33                 X    =         2565652
88
 Y    =       11020067
77  feet           Y    =         3358916
66  meter
 Z    =       17119636
81                 Z    =         5218065
30
 XDOT =     -20975
702014                 XDOT =       -6393
393974
 YDOT =      11949
232822  feet/sec       YDOT =        3642
126164  meter/sec
 ZDOT =       2647
862767                 ZDOT =         807
068571


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10150
32661842  
00016717  00000-0  10270-3 0  9073
2 25544  51
6482 322
1713 0010103    
2141 359
9025 15
74890314 20669


Satellite: ISS
Catalog Number: 25544
Epoch time:      10150
32661842   =   yrday
fracday
Element set:     907
Inclination:       51
6482  deg
RA of node:       322
1713  deg
Eccentricity:     
0010103     
Arg of perigee:      
2141  deg
Mean anomaly:     359
9025  deg
Mean motion:   15
74890314  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2066
Checksum:              266


Coasting Arc #9 (Orbit 2080)
---------------------------------------

Vector Time (GMT): 2010/151/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4634435
02                 A    =         6729526
86  meter
 Y    =       -4843238
03  meter          E    =           
0020404
 Z    =        -434479
47                 I    =           51
43774
 XDOT =       3743
907696                 Wp   =           23
44641
 YDOT =       3053
769768  meter/sec      RA   =          316
69979  deg
 ZDOT =       6008
558373                 TA   =          331
80880
                                          MA   =          331
91910
                                          Ha   =            191
135  n
mi
                                          Hp   =            181
105

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15204839
31                 X    =         4690359
17
 Y    =      -15889888
55  feet           Y    =        -4791100
26  meter
 Z    =       -1425457
59                 Z    =         -411830
33
 XDOT =      12283
161733                 XDOT =        3680
293140
 YDOT =      10018
929685  feet/sec       YDOT =        3095
279695  meter/sec
 ZDOT =      19713
118023                 ZDOT =        6026
592269

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18219483
56                 X    =         5553298
59
 Y    =      -12327823
67  feet           Y    =        -3757520
65  meter
 Z    =       -1335218
56                 Z    =         -406974
62
 XDOT =       8883
412133                 XDOT =        2707
664018
 YDOT =      11029
550699  feet/sec       YDOT =        3361
807053  meter/sec
 ZDOT =      19784
936537                 ZDOT =        6030
448656


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10151
27842767  
00016717  00000-0  10270-3 0  9086
2 25544  51
6486 317
2775 0010213   3
4474 356
6758 15
74907857 20817


Satellite: ISS
Catalog Number: 25544
Epoch time:      10151
27842767   =   yrday
fracday
Element set:     908
Inclination:       51
6486  deg
RA of node:       317
2775  deg
Eccentricity:     
0010213     
Arg of perigee:     3
4474  deg
Mean anomaly:     356
6758  deg
Mean motion:   15
74907857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2081
Checksum:              327


Coasting Arc #10 (Orbit 2096)
---------------------------------------

Vector Time (GMT): 2010/152/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3236679
36                 A    =         6717406
99  meter
 Y    =       -2678774
46  meter          E    =           
0019336
 Z    =       -5255490
69                 I    =           51
37588
 XDOT =       5027
413738                 Wp   =           57
12475
 YDOT =      -5818
435670  meter/sec      RA   =          311
54596  deg
 ZDOT =       -120
489917                 TA   =          211
66790
                                          MA   =          211
78437
                                          Ha   =            191
181  n
mi
                                          Hp   =            180
751

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10619026
76                 X    =        -3180954
09
 Y    =       -8788630
12  feet           Y    =        -2714656
58  meter
 Z    =      -17242423
53                 Z    =        -5271079
50
 XDOT =      16494
139562                 XDOT =        5092
688204
 YDOT =     -19089
355874  feet/sec       YDOT =       -5761
851149  meter/sec
 ZDOT =       -395
308126                 ZDOT =         -95
909099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8613771
02                 X    =        -2625477
41
 Y    =      -10661229
95  feet           Y    =        -3249542
89  meter
 Z    =      -17304509
32                 Z    =        -5274414
44
 XDOT =      19106
385980                 XDOT =        5823
626447
 YDOT =     -14901
261532  feet/sec       YDOT =       -4541
904515  meter/sec
 ZDOT =       -297
373743                 ZDOT =         -90
639517


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10152
29367279  
00016717  00000-0  10270-3 0  9090
2 25544  51
6484 312
0573 0010293   6
9199 353
2105 15
74946739 20972


Satellite: ISS
Catalog Number: 25544
Epoch time:      10152
29367279   =   yrday
fracday
Element set:     909
Inclination:       51
6484  deg
RA of node:       312
0573  deg
Eccentricity:     
0010293     
Arg of perigee:     6
9199  deg
Mean anomaly:     353
2105  deg
Mean motion:   15
74946739  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2097
Checksum:              326


Coasting Arc #11 (Orbit 2112)
---------------------------------------

Vector Time (GMT): 2010/153/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4145642
89                 A    =         6729527
97  meter
 Y    =        5296954
38  meter          E    =           
0009944
 Z    =        -244229
08                 I    =           51
39730
 XDOT =      -3653
338474                 Wp   =           81
60892
 YDOT =      -3126
702923  meter/sec      RA   =          306
38726  deg
 ZDOT =      -6007
159929                 TA   =          101
05233
                                          MA   =          100
94047
                                          Ha   =            191
315  n
mi
                                          Hp   =            180
758

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13601190
59                 X    =        -4203379
86
 Y    =       17378459
25  feet           Y    =         5250272
54  meter
 Z    =        -801276
52                 Z    =         -264508
12
 XDOT =     -11986
018614                 XDOT =       -3588
921965
 YDOT =     -10258
211691  feet/sec       YDOT =       -3167
195769  meter/sec
 ZDOT =     -19708
529952                 ZDOT =       -6024
751753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16456798
65                 X    =        -5016032
23
 Y    =       14698333
52  feet           Y    =         4480052
06  meter
 Z    =        -882068
59                 Z    =         -268854
51
 XDOT =      -8795
075559                 XDOT =       -2680
739030
 YDOT =     -10997
211045  feet/sec       YDOT =       -3351
949927  meter/sec
 ZDOT =     -19778
598041                 ZDOT =       -6028
516683


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10153
30890151  
00016717  00000-0  10270-3 0  9105
2 25544  51
6484 306
8374 0010140  10
6957 349
4420 15
74917254 21133


Satellite: ISS
Catalog Number: 25544
Epoch time:      10153
30890151   =   yrday
fracday
Element set:     910
Inclination:       51
6484  deg
RA of node:       306
8374  deg
Eccentricity:     
0010140     
Arg of perigee:    10
6957  deg
Mean anomaly:     349
4420  deg
Mean motion:   15
74917254  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2113
Checksum:              282


Coasting Arc #12 (Orbit 2128)
---------------------------------------

Vector Time (GMT): 2010/154/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3175783
55                 A    =         6717406
08  meter
 Y    =        2802527
50  meter          E    =           
0012533
 Z    =        5210519
38                 I    =           51
33995
 XDOT =      -4424
789730                 Wp   =           23
99295
 YDOT =       6273
883879  meter/sec      RA   =          301
21634  deg
 ZDOT =       -665
721722                 TA   =           72
42726
                                          MA   =           72
29039
                                          Ha   =            191
268  n
mi
                                          Hp   =            180
419

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10419237
36                 X    =         3118897
42
 Y    =        9194644
04  feet           Y    =         2837722
34  meter
 Z    =       17094879
84                 Z    =         5225809
46
 XDOT =     -14517
026674                 XDOT =       -4491
382620
 YDOT =      20583
608528  feet/sec       YDOT =        6224
030981  meter/sec
 ZDOT =      -2184
126383                 ZDOT =        -687
378358

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8714072
28                 X    =         2656049
23
 Y    =       10727577
22  feet           Y    =         3269765
54  meter
 Z    =       17155784
28                 Z    =         5229083
05
 XDOT =     -16828
031908                 XDOT =       -5129
184126
 YDOT =      17362
394478  feet/sec       YDOT =        5292
057837  meter/sec
 ZDOT =      -2270
401152                 ZDOT =        -692
018271


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10154
32410969  
00016717  00000-0  10270-3 0  9114
2 25544  51
6482 301
6167 0010336  13
9105 346
2342 15
74998389 21295


Satellite: ISS
Catalog Number: 25544
Epoch time:      10154
32410969   =   yrday
fracday
Element set:     911
Inclination:       51
6482  deg
RA of node:       301
6167  deg
Eccentricity:     
0010336     
Arg of perigee:    13
9105  deg
Mean anomaly:     346
2342  deg
Mean motion:   15
74998389  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2129
Checksum:              303


Coasting Arc #13 (Orbit 2144)
---------------------------------------

Vector Time (GMT): 2010/155/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3560881
59                 A    =         6728883
97  meter
 Y    =       -5620072
54  meter          E    =           
0022752
 Z    =         912068
21                 I    =           51
36337
 XDOT =       3665
831708                 Wp   =           38
55568
 YDOT =       3295
214733  meter/sec      RA   =          296
06734  deg
 ZDOT =       5931
096354                 TA   =          331
45747
                                          MA   =          331
58185
                                          Ha   =            191
338  n
mi
                                          Hp   =            180
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11682682
39                 X    =         3619030
94
 Y    =      -18438558
19  feet           Y    =        -5579927
60  meter
 Z    =        2992349
78                 Z    =          929507
66
 XDOT =      12027
006917                 XDOT =        3599
899338
 YDOT =      10811
071960  feet/sec       YDOT =        3335
838982  meter/sec
 ZDOT =      19458
977540                 ZDOT =        5948
745184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14181489
22                 X    =         4322517
91
 Y    =      -16581021
83  feet           Y    =        -5053895
45  meter
 Z    =        3061818
41                 Z    =          933242
25
 XDOT =       9034
467120                 XDOT =        2753
705578
 YDOT =      11369
752966  feet/sec       YDOT =        3465
500704  meter/sec
 ZDOT =      19529
281570                 ZDOT =        5952
525023


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10155
33930103  
00016717  00000-0  10270-3 0  9124
2 25544  51
6473 296
3957 0010354  17
3005 342
8510 15
75028766 21450


Satellite: ISS
Catalog Number: 25544
Epoch time:      10155
33930103   =   yrday
fracday
Element set:     912
Inclination:       51
6473  deg
RA of node:       296
3957  deg
Eccentricity:     
0010354     
Arg of perigee:    17
3005  deg
Mean anomaly:     342
8510  deg
Mean motion:   15
75028766  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2145
Checksum:              288


Coasting Arc #14 (Orbit 2159)
---------------------------------------

Vector Time (GMT): 2010/156/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3236152
49                 A    =         6717828
54  meter
 Y    =       -2968558
98  meter          E    =           
0018721
 Z    =       -5097115
44                 I    =           51
31292
 XDOT =       3746
424951                 Wp   =           67
76150
 YDOT =      -6558
298845  meter/sec      RA   =          290
88042  deg
 ZDOT =       1452
185627                 TA   =          216
17298
                                          MA   =          216
29974
                                          Ha   =            191
421  n
mi
                                          Hp   =            179
910

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10617298
19                 X    =        -3177956
03
 Y    =       -9739366
73  feet           Y    =        -3004421
67  meter
 Z    =      -16722819
68                 Z    =        -5112695
68
 XDOT =      12291
420443                 XDOT =        3812
428103
 YDOT =     -21516
728493  feet/sec       YDOT =       -6516
035189  meter/sec
 ZDOT =       4764
388541                 ZDOT =        1470
545519

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9207966
70                 X    =        -2806588
25
 Y    =      -10987079
26  feet           Y    =        -3348861
76  meter
 Z    =      -16784886
71                 Z    =        -5116033
47
 XDOT =      14074
164388                 XDOT =        4289
805306
 YDOT =     -19129
308807  feet/sec       YDOT =       -5830
613324  meter/sec
 ZDOT =       4837
516827                 ZDOT =        1474
475129


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10156
29102748  
00016717  00000-0  10270-3 0  9137
2 25544  51
6462 291
5005 0010413  20
7082 339
4501 15
75047427 21602


Satellite: ISS
Catalog Number: 25544
Epoch time:      10156
29102748   =   yrday
fracday
Element set:     913
Inclination:       51
6462  deg
RA of node:       291
5005  deg
Eccentricity:     
0010413     
Arg of perigee:    20
7082  deg
Mean anomaly:     339
4501  deg
Mean motion:   15
75047427  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2160
Checksum:              273


Coasting Arc #15 (Orbit 2175)
---------------------------------------

Vector Time (GMT): 2010/157/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3000196
39                 A    =         6727992
90  meter
 Y    =        5798185
47  meter          E    =           
0009584
 Z    =       -1642932
05                 I    =           51
33719
 XDOT =      -3744
056168                 Wp   =           70
14093
 YDOT =      -3547
695754  meter/sec      RA   =          285
74288  deg
 ZDOT =      -5707
107940                 TA   =          128
07197
                                          MA   =          127
98547
                                          Ha   =            191
529  n
mi
                                          Hp   =            179
851

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9843164
00                 X    =        -3056828
63
 Y    =       19022918
20  feet           Y    =         5764319
00  meter
 Z    =       -5390197
03                 Z    =        -1657644
11
 XDOT =     -12283
648844                 XDOT =       -3676
382597
 YDOT =     -11639
421764  feet/sec       YDOT =       -3589
185064  meter/sec
 ZDOT =     -18724
107415                 ZDOT =       -5725
132694

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11823734
08                 X    =        -3603874
15
 Y    =       17841623
01  feet           Y    =         5438126
69  meter
 Z    =       -5448790
64                 Z    =        -1660791
39
 XDOT =      -9532
387929                 XDOT =       -2905
471841
 YDOT =     -12033
804317  feet/sec       YDOT =       -3667
903556  meter/sec
 ZDOT =     -18795
915794                 ZDOT =       -5728
995134


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10157
30618477  
00016717  00000-0  10270-3 0  9142
2 25544  51
6458 286
2801 0010364  24
2864 335
8786 15
75045990 21769


Satellite: ISS
Catalog Number: 25544
Epoch time:      10157
30618477   =   yrday
fracday
Element set:     914
Inclination:       51
6458  deg
RA of node:       286
2801  deg
Eccentricity:     
0010364     
Arg of perigee:    24
2864  deg
Mean anomaly:     335
8786  deg
Mean motion:   15
75045990  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2176
Checksum:              325


Coasting Arc #16 (Orbit 2191)
---------------------------------------

Vector Time (GMT): 2010/158/06:39:48
549
Vector Time (MET): N/A
Weight (LBS)     : 816271
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3347420
70                 A    =         6718735
06  meter
 Y    =        3228138
32  meter          E    =           
0016515
 Z    =        4844748
18                 I    =           51
29918
 XDOT =      -3103
808960                 Wp   =           39
38241
 YDOT =       6673
047121  meter/sec      RA   =          280
54113  deg
 ZDOT =      -2284
960111                 TA   =           73
03796
                                          MA   =           72
85701
                                          Ha   =            191
466  n
mi
                                          Hp   =            179
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10982351
37                 X    =         3287539
10
 Y    =       10591005
00  feet           Y    =         3265235
83  meter
 Z    =       15894843
12                 Z    =         4860865
04
 XDOT =     -10183
100263                 XDOT =       -3167
097444
 YDOT =      21893
199217  feet/sec       YDOT =        6637
984865  meter/sec
 ZDOT =      -7496
588292                 ZDOT =       -2300
191596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9870681
32                 X    =         3008583
67
 Y    =       11545810
20  feet           Y    =         3519162
95  meter
 Z    =       15959053
34                 Z    =         4864319
46
 XDOT =     -11262
601655                 XDOT =       -3432
840984
 YDOT =      20150
647205  feet/sec       YDOT =        6141
917268  meter/sec
 ZDOT =      -7557
246117                 ZDOT =       -2303
448616


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10158
32132300  
00016717  00000-0  10270-3 0  9152
2 25544  51
6456 281
0580 0010389  27
7488 332
4228 15
75097492 21927


Satellite: ISS
Catalog Number: 25544
Epoch time:      10158
32132300   =   yrday
fracday
Element set:     915
Inclination:       51
6456  deg
RA of node:       281
0580  deg
Eccentricity:     
0010389     
Arg of perigee:    27
7488  deg
Mean anomaly:     332
4228  deg
Mean motion:   15
75097492  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2192
Checksum:              303

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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