Date: June 10th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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


159/00:14:50 537 0 8 2 5 2 5
N/A -2 2 -0 1 192 1
000/00:09:41 074 0 8 0 2 189 2

159/01:48:37 850 0 8 1 9 1 9
N/A -1 6 -0 0 193 0
000/00:07:15 699 0 8 0 1 189 9

Coasting Arc #1 (Orbit 2194)
---------------------------------------

Vector Time (GMT): 2010/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3998810
59                 A    =         6724339
28  meter
 Y    =       -1443190
00  meter          E    =           
0009928
 Z    =       -5218402
74                 I    =           51
29473
 XDOT =       1796
285367                 Wp   =           85
87200
 YDOT =      -7447
539352  meter/sec      RA   =          279
45156  deg
 ZDOT =        685
024958                 TA   =          190
67066
                                          MA   =          190
69174
                                          Ha   =            190
945  n
mi
                                          Hp   =            187
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13119457
33                 X    =        -3957025
01
 Y    =       -4734875
33  feet           Y    =        -1487672
86  meter
 Z    =      -17120743
91                 Z    =        -5237727
87
 XDOT =       5893
324694                 XDOT =        1876
103825
 YDOT =     -24434
184226  feet/sec       YDOT =       -7427
006007  meter/sec
 ZDOT =       2247
457210                 ZDOT =         693
944468

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7942871
47                 X    =        -2420987
22
 Y    =       11349358
86  feet           Y    =         3459284
58  meter
 Z    =      -17197730
18                 Z    =        -5241868
16
 XDOT =     -21252
659617                 XDOT =       -6477
810651
 YDOT =     -11423
359751  feet/sec       YDOT =       -3481
840052  meter/sec
 ZDOT =       2282
968694                 ZDOT =         695
848858


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
51472515  
00016717  00000-0  10270-3 0  9002
2 25544  51
6480 280
1107 0005261 293
4449  66
6160 15
72568775 21959


Satellite: ISS
Catalog Number: 25544
Epoch time:      10158
51472515   =   yrday
fracday
Element set:     900
Inclination:       51
6480  deg
RA of node:       280
1107  deg
Eccentricity:     
0005261     
Arg of perigee:   293
4449  deg
Mean anomaly:      66
6160  deg
Mean motion:   15
72568775  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2195
Checksum:              305


Coasting Arc #2 (Orbit 2202)
---------------------------------------

Vector Time (GMT): 2010/159/00:19:41
074
Vector Time (MET): N/A
Weight (LBS)     : 799097
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2885820
81                 A    =         6729859
70  meter
 Y    =       -4374017
39  meter          E    =           
0001298
 Z    =       -4223293
64                 I    =           51
30571
 XDOT =       3572
770112                 Wp   =           62
67814
 YDOT =      -5804
890663  meter/sec      RA   =          276
79117  deg
 ZDOT =       3572
176498                 TA   =          243
80888
                                          MA   =          243
82222
                                          Ha   =            192
092  n
mi
                                          Hp   =            189
177

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9467916
03                 X    =        -2816178
99
 Y    =      -14350450
75  feet           Y    =        -4405898
46  meter
 Z    =      -13855950
28                 Z    =        -4237144
52
 XDOT =      11721
686720                 XDOT =        3620
062686
 YDOT =     -19044
916874  feet/sec       YDOT =       -5764
673822  meter/sec
 ZDOT =      11719
739167                 ZDOT =        3589
647434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15711593
16                 X    =         4788893
59
 Y    =       -6869518
68  feet           Y    =        -2093829
29  meter
 Z    =      -13911138
78                 Z    =        -4240115
10
 XDOT =      16341
387584                 XDOT =        4980
854936
 YDOT =      13510
596779  feet/sec       YDOT =        4118
029898  meter/sec
 ZDOT =      11789
319766                 ZDOT =        3593
384665


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   10159
02311036  
00016717  00000-0  10270-3 0  9010
2 25544  51
6474 277
5086 0007560 297
7172  62
3223 15
72074301 22032


Satellite: ISS
Catalog Number: 25544
Epoch time:      10159
02311036   =   yrday
fracday
Element set:     901
Inclination:       51
6474  deg
RA of node:       277
5086  deg
Eccentricity:     
0007560     
Arg of perigee:   297
7172  deg
Mean anomaly:      62
3223  deg
Mean motion:   15
72074301  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2203
Checksum:              276


Coasting Arc #3 (Orbit 2203)
---------------------------------------

Vector Time (GMT): 2010/159/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2682362
84                 A    =         6731706
02  meter
 Y    =       -4709924
82  meter          E    =           
0002321
 Z    =       -3989679
02                 I    =           51
30962
 XDOT =       3767
904036                 Wp   =          329
75086
 YDOT =      -5455
777168  meter/sec      RA   =          276
45991  deg
 ZDOT =       3908
424926                 TA   =          340
83089
                                          MA   =          340
83963
                                          Ha   =            192
976  n
mi
                                          Hp   =            189
902

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8800403
03                 X    =        -2610114
84
 Y    =      -15452509
25  feet           Y    =        -4739516
15  meter
 Z    =      -13089498
09                 Z    =        -4002535
20
 XDOT =      12361
889882                 XDOT =        3809
644798
 YDOT =     -17899
531391  feet/sec       YDOT =       -5413
409309  meter/sec
 ZDOT =      12822
916423                 ZDOT =        3926
830388

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12960505
09                 X    =         3950361
95
 Y    =      -12120591
70  feet           Y    =        -3694356
35  meter
 Z    =      -13140725
26                 Z    =        -4005293
06
 XDOT =      19407
453012                 XDOT =        5915
391678
 YDOT =       6774
188911  feet/sec       YDOT =        2064
772780  meter/sec
 ZDOT =      12896
220806                 ZDOT =        3930
768102


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   10159
08667749  
00016717  00000-0  10270-3 0  9022
2 25544  51
6487 277
1834 0009022 298
1274  61
8975 15
71721542 22040


Satellite: ISS
Catalog Number: 25544
Epoch time:      10159
08667749   =   yrday
fracday
Element set:     902
Inclination:       51
6487  deg
RA of node:       277
1834  deg
Eccentricity:     
0009022     
Arg of perigee:   298
1274  deg
Mean anomaly:      61
8975  deg
Mean motion:   15
71721542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2204
Checksum:              326


Coasting Arc #4 (Orbit 2219)
---------------------------------------

Vector Time (GMT): 2010/160/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2405344
69                 A    =         6735113
61  meter
 Y    =        5615622
21  meter          E    =           
0004519
 Z    =       -2836144
04                 I    =           51
31957
 XDOT =      -3946
922518                 Wp   =          306
66068
 YDOT =      -4247
896939  meter/sec      RA   =          271
36803  deg
 ZDOT =      -5055
286196                 TA   =          265
98261
                                          MA   =          266
03427
                                          Ha   =            193
253  n
mi
                                          Hp   =            189
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7891550
83                 X    =        -2454183
14
 Y    =       18423957
39  feet           Y    =         5588451
55  meter
 Z    =       -9304934
51                 Z    =        -2847947
21
 XDOT =     -12949
220860                 XDOT =       -3874
570379
 YDOT =     -13936
669748  feet/sec       YDOT =       -4291
628515  meter/sec
 ZDOT =     -16585
584634                 ZDOT =       -5074
285503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19805282
82                 X    =        -6036650
20
 Y    =       -2931314
80  feet           Y    =         -893464
75  meter
 Z    =       -9351938
43                 Z    =        -2850470
83
 XDOT =      10027
517818                 XDOT =        3056
387431
 YDOT =     -14509
226763  feet/sec       YDOT =       -4422
412317  meter/sec
 ZDOT =     -16661
285790                 ZDOT =       -5078
359909


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   10160
10398191  
00016717  00000-0  10270-3 0  9030
2 25544  51
6493 271
9776 0009124 301
9248  58
1027 15
71733156 22200


Satellite: ISS
Catalog Number: 25544
Epoch time:      10160
10398191   =   yrday
fracday
Element set:     903
Inclination:       51
6493  deg
RA of node:       271
9776  deg
Eccentricity:     
0009124     
Arg of perigee:   301
9248  deg
Mean anomaly:      58
1027  deg
Mean motion:   15
71733156  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2220
Checksum:              294


Coasting Arc #5 (Orbit 2235)
---------------------------------------

Vector Time (GMT): 2010/161/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3998303
21                 A    =         6728532
44  meter
 Y    =        2573011
09  meter          E    =           
0009148
 Z    =        4765510
51                 I    =           51
29818
 XDOT =      -1552
064739                 Wp   =          352
96695
 YDOT =       7099
977123  meter/sec      RA   =          266
18288  deg
 ZDOT =      -2522
807823                 TA   =          121
92513
                                          MA   =          121
83613
                                          Ha   =            193
366  n
mi
                                          Hp   =            189
251

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13117792
69                 X    =         3946083
84
 Y    =        8441637
43  feet           Y    =         2617429
73  meter
 Z    =       15634877
00                 Z    =         4784808
15
 XDOT =      -5092
075915                 XDOT =       -1619
087088
 YDOT =      23293
888198  feet/sec       YDOT =        7082
246690  meter/sec
 ZDOT =      -8276
928552                 ZDOT =       -2530
509479

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4626069
70                 X    =        -1410026
04
 Y    =       14816442
81  feet           Y    =         4516051
77  meter
 Z    =       15711766
55                 Z    =         4788946
44
 XDOT =     -22711
088218                 XDOT =       -6922
339689
 YDOT =       1747
844283  feet/sec       YDOT =         532
742938  meter/sec
 ZDOT =      -8307
589668                 ZDOT =       -2532
153331


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   10161
12127037  
00016717  00000-0  10270-3 0  9043
2 25544  51
6490 266
7716 0009227 306
4384  53
5927 15
71791059 22369


Satellite: ISS
Catalog Number: 25544
Epoch time:      10161
12127037   =   yrday
fracday
Element set:     904
Inclination:       51
6490  deg
RA of node:       266
7716  deg
Eccentricity:     
0009227     
Arg of perigee:   306
4384  deg
Mean anomaly:      53
5927  deg
Mean motion:   15
71791059  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2236
Checksum:              306


Coasting Arc #6 (Orbit 2251)
---------------------------------------

Vector Time (GMT): 2010/162/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         219508
15                 A    =         6737498
08  meter
 Y    =       -6546054
52  meter          E    =           
0013665
 Z    =        1540019
55                 I    =           51
33174
 XDOT =       4895
468466                 Wp   =           23
46197
 YDOT =       1517
907670  meter/sec      RA   =          261
07524  deg
 ZDOT =       5749
153718                 TA   =          353
58471
                                          MA   =          353
60219
                                          Ha   =            193
598  n
mi
                                          Hp   =            189
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         720171
11                 X    =          285209
78
 Y    =      -21476556
83  feet           Y    =        -6543232
79  meter
 Z    =        5052557
58                 Z    =         1541244
28
 XDOT =      16061
248249                 XDOT =        4850
202418
 YDOT =       4980
012040  feet/sec       YDOT =        1572
397524  meter/sec
 ZDOT =      18862
052881                 ZDOT =        5772
826535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20779045
51                 X    =         6333453
07
 Y    =       -5472046
41  feet           Y    =        -1667879
75  meter
 Z    =        5057415
71                 Z    =         1541500
31
 XDOT =       -617
019868                 XDOT =        -188
067656
 YDOT =      15192
534856  feet/sec       YDOT =        4630
684624  meter/sec
 ZDOT =      18956
377893                 ZDOT =        5777
903982


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   10162
13854544  
00016717  00000-0  10270-3 0  9056
2 25544  51
6495 261
5651 0009249 310
8317  49
2043 15
71772436 22521


Satellite: ISS
Catalog Number: 25544
Epoch time:      10162
13854544   =   yrday
fracday
Element set:     905
Inclination:       51
6495  deg
RA of node:       261
5651  deg
Eccentricity:     
0009249     
Arg of perigee:   310
8317  deg
Mean anomaly:      49
2043  deg
Mean motion:   15
71772436  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2252
Checksum:              301


Coasting Arc #7 (Orbit 2266)
---------------------------------------

Vector Time (GMT): 2010/163/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4292946
51                 A    =         6726605
71  meter
 Y    =         -43212
85  meter          E    =           
0009008
 Z    =       -5184450
38                 I    =           51
30157
 XDOT =      -1091
895072                 Wp   =           59
42265
 YDOT =      -7552
270791  meter/sec      RA   =          255
91122  deg
 ZDOT =        972
856227                 TA   =          219
86982
                                          MA   =          219
93602
                                          Ha   =            193
648  n
mi
                                          Hp   =            188
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14084470
17                 X    =        -4266958
92
 Y    =        -141774
44  feet           Y    =          -91072
76  meter
 Z    =      -17009351
63                 Z    =        -5205242
56
 XDOT =      -3582
332914                 XDOT =       -1012
089056
 YDOT =     -24777
791309  feet/sec       YDOT =       -7564
034993  meter/sec
 ZDOT =       3191
785523                 ZDOT =         967
744054

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4088000
56                 X    =        -1246022
57
 Y    =      -13373678
76  feet           Y    =        -4076297
28  meter
 Z    =      -17092203
22                 Z    =        -5209703
54
 XDOT =      21557
535082                 XDOT =        6570
736693
 YDOT =     -10618
702674  feet/sec       YDOT =       -3236
580575  meter/sec
 ZDOT =       3171
386743                 ZDOT =         966
638679


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   10163
09222496  
00016717  00000-0  10270-3 0  9068
2 25544  51
6495 256
6846 0009313 314
1297  45
9099 15
71825724 22677


Satellite: ISS
Catalog Number: 25544
Epoch time:      10163
09222496   =   yrday
fracday
Element set:     906
Inclination:       51
6495  deg
RA of node:       256
6846  deg
Eccentricity:     
0009313     
Arg of perigee:   314
1297  deg
Mean anomaly:      45
9099  deg
Mean motion:   15
71825724  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2267
Checksum:              329


Coasting Arc #8 (Orbit 2282)
---------------------------------------

Vector Time (GMT): 2010/164/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2092958
96                 A    =         6738445
85  meter
 Y    =        6401826
39  meter          E    =           
0002715
 Z    =        -163940
42                 I    =           51
34937
 XDOT =      -4612
898698                 Wp   =          131
99211
 YDOT =       1356
009762  meter/sec      RA   =          250
78040  deg
 ZDOT =      -6004
693662                 TA   =           49
79340
                                          MA   =           49
76964
                                          Ha   =            193
911  n
mi
                                          Hp   =            188
648

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6866663
24                 X    =         2022013
41
 Y    =       21003367
42  feet           Y    =         6424834
46  meter
 Z    =        -537862
27                 Z    =         -153943
78
 XDOT =     -15134
182081                 XDOT =       -4598
549244
 YDOT =       4448
850926  feet/sec       YDOT =        1304
507080  meter/sec
 ZDOT =     -19700
438524                 ZDOT =       -6027
068025

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17723022
15                 X    =        -5401977
15
 Y    =       13199556
44  feet           Y    =         4023224
80  meter
 Z    =        -497994
65                 Z    =         -151788
77
 XDOT =      -8035
704979                 XDOT =       -2449
282878
 YDOT =     -11527
391176  feet/sec       YDOT =       -3513
548830  meter/sec
 ZDOT =     -19789
599014                 ZDOT =       -6031
869779


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   10164
10947050  
00016717  00000-0  10270-3 0  9072
2 25544  51
6493 251
4788 0009228 317
3243  42
7201 15
71794325 22834


Satellite: ISS
Catalog Number: 25544
Epoch time:      10164
10947050   =   yrday
fracday
Element set:     907
Inclination:       51
6493  deg
RA of node:       251
4788  deg
Eccentricity:     
0009228     
Arg of perigee:   317
3243  deg
Mean anomaly:      42
7201  deg
Mean motion:   15
71794325  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2283
Checksum:              300


Coasting Arc #9 (Orbit 2298)
---------------------------------------

Vector Time (GMT): 2010/165/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3537016
87                 A    =         6726333
45  meter
 Y    =       -2332498
52  meter          E    =           
0006923
 Z    =        5226406
92                 I    =           51
31986
 XDOT =       3594
873443                 Wp   =          332
93540
 YDOT =       6778
516358  meter/sec      RA   =          245
64313  deg
 ZDOT =        598
717316                 TA   =          111
38228
                                          MA   =          111
30839
                                          Ha   =            193
969  n
mi
                                          Hp   =            188
264

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11604386
05                 X    =         3537447
58
 Y    =       -7652554
20  feet           Y    =        -2292944
14  meter
 Z    =       17147004
34                 Z    =         5243590
26
 XDOT =      11794
204210                 XDOT =        3515
899219
 YDOT =      22239
226896  feet/sec       YDOT =        6818
274684  meter/sec
 ZDOT =       1964
295657                 ZDOT =         615
990691

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11060283
62                 X    =         3371174
45
 Y    =        8278921
04  feet           Y    =         2523415
13  meter
 Z    =       17215478
84                 Z    =         5247277
95
 XDOT =     -16410
275656                 XDOT =       -5001
852020
 YDOT =      17738
967956  feet/sec       YDOT =        5406
837433  meter/sec
 ZDOT =       2033
180963                 ZDOT =         619
713557


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   10165
12669891  
00016717  00000-0  10270-3 0  9080
2 25544  51
6489 246
2721 0009392 322
1075  37
9425 15
71857273 22990


Satellite: ISS
Catalog Number: 25544
Epoch time:      10165
12669891   =   yrday
fracday
Element set:     908
Inclination:       51
6489  deg
RA of node:       246
2721  deg
Eccentricity:     
0009392     
Arg of perigee:   322
1075  deg
Mean anomaly:      37
9425  deg
Mean motion:   15
71857273  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2299
Checksum:              334


Coasting Arc #10 (Orbit 2313)
---------------------------------------

Vector Time (GMT): 2010/166/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4064012
11                 A    =         6737574
59  meter
 Y    =       -5224295
42  meter          E    =           
0015169
 Z    =       -1204987
06                 I    =           51
37053
 XDOT =       3204
977501                 Wp   =             
88180
 YDOT =      -3840
594175  meter/sec      RA   =          240
48577  deg
 ZDOT =       5857
740366                 TA   =          345
86382
                                          MA   =          345
90623
                                          Ha   =            194
170  n
mi
                                          Hp   =            188
011

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13333373
08                 X    =        -3999437
49
 Y    =      -17140076
85  feet           Y    =        -5269380
35  meter
 Z    =       -3953369
60                 Z    =        -1224573
98
 XDOT =      10515
018048                 XDOT =        3219
229911
 YDOT =     -12600
374590  feet/sec       YDOT =       -3804
675596  meter/sec
 ZDOT =      19218
308286                 ZDOT =        5873
343935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11381614
18                 X    =         3469116
00
 Y    =      -18476909
82  feet           Y    =        -5631762
11  meter
 Z    =       -4031484
24                 Z    =        -1228796
40
 XDOT =      14100
548306                 XDOT =        4297
847124
 YDOT =       4490
166336  feet/sec       YDOT =        1368
602699  meter/sec
 ZDOT =      19280
479095                 ZDOT =        5876
690028


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   10166
08033764  
00016717  00000-0  10270-3 0  9091
2 25544  51
6480 241
3905 0009572 325
6369  34
4173 15
71875847 23142


Satellite: ISS
Catalog Number: 25544
Epoch time:      10166
08033764   =   yrday
fracday
Element set:     909
Inclination:       51
6480  deg
RA of node:       241
3905  deg
Eccentricity:     
0009572     
Arg of perigee:   325
6369  deg
Mean anomaly:      34
4173  deg
Mean motion:   15
71875847  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2314
Checksum:              317


Coasting Arc #11 (Orbit 2329)
---------------------------------------

Vector Time (GMT): 2010/167/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1889819
27                 A    =         6727608
86  meter
 Y    =        4190454
49  meter          E    =           
0013745
 Z    =       -4922204
94                 I    =           51
35178
 XDOT =      -5479
669778                 Wp   =           31
85917
 YDOT =      -4962
895548  meter/sec      RA   =          235
37516  deg
 ZDOT =      -2112
432892                 TA   =          217
49671
                                          MA   =          217
59266
                                          Ha   =            194
348  n
mi
                                          Hp   =            187
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6200194
45                 X    =        -1912626
29
 Y    =       13748210
27  feet           Y    =         4169194
67  meter
 Z    =      -16148966
34                 Z    =        -4931440
33
 XDOT =     -17977
919218                 XDOT =       -5413
504803
 YDOT =     -16282
465708  feet/sec       YDOT =       -5023
802196  meter/sec
 ZDOT =      -6930
554108                 ZDOT =       -2138
892950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15028726
81                 X    =        -4580755
93
 Y    =        -635435
87  feet           Y    =         -193680
85  meter
 Z    =      -16185746
88                 Z    =        -4933415
65
 XDOT =       8520
581954                 XDOT =        2597
073380
 YDOT =     -21563
705872  feet/sec       YDOT =       -6572
617550  meter/sec
 ZDOT =      -7036
083334                 ZDOT =       -2144
598200


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   10167
09753789  
00016717  00000-0  10270-3 0  9101
2 25544  51
6467 236
1834 0009628 329
2172  30
8424 15
71905470 23307


Satellite: ISS
Catalog Number: 25544
Epoch time:      10167
09753789   =   yrday
fracday
Element set:     910
Inclination:       51
6467  deg
RA of node:       236
1834  deg
Eccentricity:     
0009628     
Arg of perigee:   329
2172  deg
Mean anomaly:      30
8424  deg
Mean motion:   15
71905470  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2330
Checksum:              312


Coasting Arc #12 (Orbit 2345)
---------------------------------------

Vector Time (GMT): 2010/168/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5318985
51                 A    =         6735336
27  meter
 Y    =        3327217
63  meter          E    =           
0010416
 Z    =        2450620
33                 I    =           51
39694
 XDOT =       -964
440365                 Wp   =           60
51420
 YDOT =       5474
550229  meter/sec      RA   =          230
19821  deg
 ZDOT =      -5317
523169                 TA   =           91
73891
                                          MA   =           91
61960
                                          Ha   =            194
477  n
mi
                                          Hp   =            187
344

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17450739
87                 X    =         5269480
08
 Y    =       10916068
35  feet           Y    =         3386420
57  meter
 Z    =        8040092
93                 Z    =         2476339
94
 XDOT =      -3164
174425                 XDOT =        -999
754756
 YDOT =      17961
122798  feet/sec       YDOT =        5463
568543  meter/sec
 ZDOT =     -17445
942154                 ZDOT =       -5322
293423

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3422619
60                 X    =        -1043214
45
 Y    =       20256222
97  feet           Y    =         6174096
76  meter
 Z    =        8142669
74                 Z    =         2481885
74
 XDOT =     -16287
125967                 XDOT =       -4964
315995
 YDOT =       4297
295225  feet/sec       YDOT =        1309
815584  meter/sec
 ZDOT =     -17464
903821                 ZDOT =       -5323
302685


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   10168
11472342  
00016717  00000-0  10270-3 0  9119
2 25544  51
6471 230
9764 0009718 333
5322  26
5343 15
71954239 23467


Satellite: ISS
Catalog Number: 25544
Epoch time:      10168
11472342   =   yrday
fracday
Element set:     911
Inclination:       51
6471  deg
RA of node:       230
9764  deg
Eccentricity:     
0009718     
Arg of perigee:   333
5322  deg
Mean anomaly:      26
5343  deg
Mean motion:   15
71954239  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2346
Checksum:              300


Coasting Arc #13 (Orbit 2361)
---------------------------------------

Vector Time (GMT): 2010/169/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -288842
85                 A    =         6730074
30  meter
 Y    =       -5158684
45  meter          E    =           
0008037
 Z    =        4304319
35                 I    =           51
39775
 XDOT =       6405
351538                 Wp   =           43
34374
 YDOT =       2521
877843  meter/sec      RA   =          225
10594  deg
 ZDOT =       3454
229485                 TA   =           11
64409
                                          MA   =           11
62551
                                          Ha   =            194
669  n
mi
                                          Hp   =            187
261

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -947647
16                 X    =         -252045
54
 Y    =      -16924817
76  feet           Y    =        -5161709
23  meter
 Z    =       14121782
65                 Z    =         4303004
94
 XDOT =      21014
932868                 XDOT =        6359
895450
 YDOT =       8273
877437  feet/sec       YDOT =        2593
251740  meter/sec
 ZDOT =      11332
773900                 ZDOT =        3485
236405

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15110350
61                 X    =         4605634
87
 Y    =       -7692495
03  feet           Y    =        -2344672
49  meter
 Z    =       14116481
90                 Z    =         4302703
68
 XDOT =        201
530980                 XDOT =          61
426643
 YDOT =      21407
799477  feet/sec       YDOT =        6525
097281  meter/sec
 ZDOT =      11456
434338                 ZDOT =        3491
921186


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   10169
13189638  
00016717  00000-0  10270-3 0  9126
2 25544  51
6459 225
7680 0009708 337
4558  22
6176 15
71913765 23623


Satellite: ISS
Catalog Number: 25544
Epoch time:      10169
13189638   =   yrday
fracday
Element set:     912
Inclination:       51
6459  deg
RA of node:       225
7680  deg
Eccentricity:     
0009708     
Arg of perigee:   337
4558  deg
Mean anomaly:      22
6176  deg
Mean motion:   15
71913765  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2362
Checksum:              333


Coasting Arc #14 (Orbit 2376)
---------------------------------------

Vector Time (GMT): 2010/170/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5629673
41                 A    =         6732415
39  meter
 Y    =       -1029642
36  meter          E    =           
0008578
 Z    =       -3539695
39                 I    =           51
42775
 XDOT =      -1689
040024                 Wp   =           14
54026
 YDOT =      -6046
227581  meter/sec      RA   =          219
91899  deg
 ZDOT =       4455
573039                 TA   =          303
17561
                                          MA   =          303
25785
                                          Ha   =            194
586  n
mi
                                          Hp   =            186
948

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18470057
12                 X    =        -5600546
17
 Y    =       -3378091
72  feet           Y    =        -1092433
47  meter
 Z    =      -11613173
84                 Z    =        -3566973
69
 XDOT =      -5541
469896                 XDOT =       -1642
948827
 YDOT =     -19836
704663  feet/sec       YDOT =       -6064
858221  meter/sec
 ZDOT =      14618
021783                 ZDOT =        4447
478970

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4550068
90                 X    =        -1386861
00
 Y    =      -18146980
19  feet           Y    =        -5531199
56  meter
 Z    =      -11721958
16                 Z    =        -3572852
85
 XDOT =      14397
901363                 XDOT =        4388
480335
 YDOT =     -13009
543339  feet/sec       YDOT =       -3965
308810  meter/sec
 ZDOT =      14585
672004                 ZDOT =        4445
712827


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   10170
08548002  
00016717  00000-0  10270-3 0  9137
2 25544  51
6451 220
8854 0009601 340
3750  19
7042 15
71969419 23775


Satellite: ISS
Catalog Number: 25544
Epoch time:      10170
08548002   =   yrday
fracday
Element set:     913
Inclination:       51
6451  deg
RA of node:       220
8854  deg
Eccentricity:     
0009601     
Arg of perigee:   340
3750  deg
Mean anomaly:      19
7042  deg
Mean motion:   15
71969419  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2377
Checksum:              296


Coasting Arc #15 (Orbit 2392)
---------------------------------------

Vector Time (GMT): 2010/171/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2625036
19                 A    =         6732818
77  meter
 Y    =        5166059
15  meter          E    =           
0009741
 Z    =       -3439641
01                 I    =           51
45235
 XDOT =      -6192
831431                 Wp   =           14
55267
 YDOT =        110
556499  meter/sec      RA   =          214
83675  deg
 ZDOT =      -4553
665707                 TA   =          206
18899
                                          MA   =          206
23829
                                          Ha   =            194
838  n
mi
                                          Hp   =            186
753

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8612323
46                 X    =         2583782
49
 Y    =       16949012
94  feet           Y    =         5195183
62  meter
 Z    =      -11284911
44                 Z    =        -3426988
12
 XDOT =     -20317
688422                 XDOT =       -6171
486464
 YDOT =        362
718173  feet/sec       YDOT =          41
424457  meter/sec
 ZDOT =     -14939
848119                 ZDOT =       -4583
698733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11570474
36                 X    =        -3526680
58
 Y    =       15122929
52  feet           Y    =         4609468
92  meter
 Z    =      -11234389
50                 Z    =        -3424241
92
 XDOT =      -7921
994918                 XDOT =       -2414
624051
 YDOT =     -17264
294006  feet/sec       YDOT =       -5262
156813  meter/sec
 ZDOT =     -15059
611008                 ZDOT =       -4590
169435


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   10171
10262333  
00016717  00000-0  10270-3 0  9142
2 25544  51
6444 215
6785 0009651 344
7016  15
3853 15
71992634 23935


Satellite: ISS
Catalog Number: 25544
Epoch time:      10171
10262333   =   yrday
fracday
Element set:     914
Inclination:       51
6444  deg
RA of node:       215
6785  deg
Eccentricity:     
0009651     
Arg of perigee:   344
7016  deg
Mean anomaly:      15
3853  deg
Mean motion:   15
71992634  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2393
Checksum:              301


Coasting Arc #16 (Orbit 2408)
---------------------------------------

Vector Time (GMT): 2010/172/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4986505
79                 A    =         6729460
66  meter
 Y    =       -1163795
78  meter          E    =           
0014313
 Z    =        4367907
07                 I    =           51
46716
 XDOT =       4231
990318                 Wp   =           28
26559
 YDOT =       5482
603709  meter/sec      RA   =          209
65367  deg
 ZDOT =      -3353
651419                 TA   =           95
67329
                                          MA   =           95
51006
                                          Ha   =            194
838  n
mi
                                          Hp   =            186
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16359927
14                 X    =         4977930
32
 Y    =       -3818227
63  feet           Y    =        -1108082
25  meter
 Z    =       14330403
78                 Z    =         4392110
69
 XDOT =      13884
482671                 XDOT =        4186
659856
 YDOT =      17987
544977  feet/sec       YDOT =        5529
675356  meter/sec
 ZDOT =     -11002
793370                 ZDOT =       -3333
201619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10667450
90                 X    =         3251439
03
 Y    =       12870748
18  feet           Y    =         3923004
04  meter
 Z    =       14426915
24                 Z    =         4397323
77
 XDOT =      -8952
314078                 XDOT =       -2728
665331
 YDOT =      19723
116462  feet/sec       YDOT =        6011
605898  meter/sec
 ZDOT =     -10921
169196                 ZDOT =       -3328
772371


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   10172
11975152  
00016717  00000-0  10270-3 0  9155
2 25544  51
6447 210
4702 0009605 347
7656  12
3272 15
72011022 24096


Satellite: ISS
Catalog Number: 25544
Epoch time:      10172
11975152   =   yrday
fracday
Element set:     915
Inclination:       51
6447  deg
RA of node:       210
4702  deg
Eccentricity:     
0009605     
Arg of perigee:   347
7656  deg
Mean anomaly:      12
3272  deg
Mean motion:   15
72011022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2409
Checksum:              275


Coasting Arc #17 (Orbit 2424)
---------------------------------------

Vector Time (GMT): 2010/173/01:52:15
699
Vector Time (MET): N/A
Weight (LBS)     : 798910
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4669250
89                 A    =         6735366
62  meter
 Y    =       -4213263
61  meter          E    =           
0017997
 Z    =        2377903
66                 I    =           51
51279
 XDOT =       4947
996372                 Wp   =           42
34665
 YDOT =      -2441
256457  meter/sec      RA   =          204
56684  deg
 ZDOT =       5379
916987                 TA   =          344
51386
                                          MA   =          344
56886
                                          Ha   =            194
998  n
mi
                                          Hp   =            186
285

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15319064
59                 X    =        -4633341
89
 Y    =      -13823043
33  feet           Y    =        -4265277
56  meter
 Z    =        7801521
21                 Z    =         2355306
81
 XDOT =      16233
583896                 XDOT =        4948
792337
 YDOT =      -8009
371578  feet/sec       YDOT =       -2385
921433  meter/sec
 ZDOT =      17650
646282                 ZDOT =        5403
956077

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5188475
98                 X    =         1581447
48
 Y    =      -20005721
85  feet           Y    =        -6097744
02  meter
 Z    =        7711342
95                 Z    =         2350417
33
 XDOT =      13080
811708                 XDOT =        3987
031409
 YDOT =      10246
385248  feet/sec       YDOT =        3123
098224  meter/sec
 ZDOT =      17746
496052                 ZDOT =        5409
131997


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   10173
13686574  
00016717  00000-0  10270-3 0  9166
2 25544  51
6436 205
2619 0009493 352
1876   7
9136 15
72039952 24251


Satellite: ISS
Catalog Number: 25544
Epoch time:      10173
13686574   =   yrday
fracday
Element set:     916
Inclination:       51
6436  deg
RA of node:       205
2619  deg
Eccentricity:     
0009493     
Arg of perigee:   352
1876  deg
Mean anomaly:       7
9136  deg
Mean motion:   15
72039952  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2425
Checksum:              321

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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