Date: June 5th 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


156/03:22:07 072 -1 3 14 0 14 0
N/A -12 0 0 0 190 9
000/00:04:10 144 -7 1 0 1 187 6

158/23:59:56 243 -0 7 2 6 2 6
N/A -2 2 0 0 191 2
000/00:09:52 486 -1 2 0 2 188 8

159/01:30:56 154 -0 8 2 7 2 7
N/A -2 2 0 0 191 0
000/00:09:52 307 -1 3 0 2 190 2

Coasting Arc #1 (Orbit 2147)
---------------------------------------

Vector Time (GMT): 2010/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 816195
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3759909
11                 A    =         6727767
21  meter
 Y    =        5398886
29  meter          E    =           
0008720
 Z    =       -1419713
34                 I    =           51
35730
 XDOT =      -3323
196815                 Wp   =           77
16511
 YDOT =      -3828
875202  meter/sec      RA   =          294
91948  deg
 ZDOT =      -5787
395930                 TA   =          118
50300
                                          MA   =          118
41516
                                          Ha   =            190
819  n
mi
                                          Hp   =            179
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12335659
81                 X    =        -3813104
26
 Y    =       17712881
54  feet           Y    =         5356543
46  meter
 Z    =       -4657852
16                 Z    =        -1438107
67
 XDOT =     -10902
876689                 XDOT =       -3252
020474
 YDOT =     -12561
926516  feet/sec       YDOT =       -3865
638607  meter/sec
 ZDOT =     -18987
519455                 ZDOT =       -5803
367559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13056200
81                 X    =         3979530
01
 Y    =       17168644
54  feet           Y    =         5233002
86  meter
 Z    =       -4731123
27                 Z    =        -1442046
37
 XDOT =     -14025
079983                 XDOT =       -4274
844379
 YDOT =       5440
631745  feet/sec       YDOT =        1658
304556  meter/sec
 ZDOT =     -19051
143468                 ZDOT =       -5806
788529


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
52897141  
00016717  00000-0  10270-3 0  9006
2 25544  51
6461 295
4165 0009326  21
1728 338
9820 15
75229238 21480


Satellite: ISS
Catalog Number: 25544
Epoch time:      10155
52897141   =   yrday
fracday
Element set:     900
Inclination:       51
6461  deg
RA of node:       295
4165  deg
Eccentricity:     
0009326     
Arg of perigee:    21
1728  deg
Mean anomaly:     338
9820  deg
Mean motion:   15
75229238  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2148
Checksum:              310


Coasting Arc #2 (Orbit 2157)
---------------------------------------

Vector Time (GMT): 2010/156/03:24:12
144
Vector Time (MET): N/A
Weight (LBS)     : 814961
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4630883
20                 A    =         6727535
07  meter
 Y    =        2046383
32  meter          E    =           
0006720
 Z    =       -4436715
90                 I    =           51
32620
 XDOT =         -1
756190                 Wp   =           38
45762
 YDOT =      -6986
913755  meter/sec      RA   =          291
61926  deg
 ZDOT =      -3218
227638                 TA   =          199
12693
                                          MA   =          199
15217
                                          Ha   =            190
867  n
mi
                                          Hp   =            187
613

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15193186
36                 X    =        -4631869
20
 Y    =        6713856
03  feet           Y    =         1994592
95  meter
 Z    =      -14556154
52                 Z    =        -4459215
02
 XDOT =         -5
761778                 XDOT =          92
006505
 YDOT =     -22922
945392  feet/sec       YDOT =       -6986
408819  meter/sec
 ZDOT =     -10558
489627                 ZDOT =       -3218
009114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13971768
73                 X    =        -4258595
11
 Y    =       -8836362
61  feet           Y    =        -2693323
32  meter
 Z    =      -14645776
98                 Z    =        -4464032
82
 XDOT =      18451
700747                 XDOT =        5624
078388
 YDOT =     -11662
654319  feet/sec       YDOT =       -3554
777036  meter/sec
 ZDOT =     -10557
626552                 ZDOT =       -3217
964573


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
16339712  
00016717  00000-0  10270-3 0  9013
2 25544  51
6489 292
1590 0005184 291
0460  69
0148 15
72595514 21581


Satellite: ISS
Catalog Number: 25544
Epoch time:      10156
16339712   =   yrday
fracday
Element set:     901
Inclination:       51
6489  deg
RA of node:       292
1590  deg
Eccentricity:     
0005184     
Arg of perigee:   291
0460  deg
Mean anomaly:      69
0148  deg
Mean motion:   15
72595514  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2158
Checksum:              308


Coasting Arc #3 (Orbit 2173)
---------------------------------------

Vector Time (GMT): 2010/157/03:24:12
144
Vector Time (MET): N/A
Weight (LBS)     : 814961
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         921047
87                 A    =         6731806
92  meter
 Y    =        5861309
35  meter          E    =           
0008348
 Z    =        3174701
77                 I    =           51
32979
 XDOT =      -4990
510639                 Wp   =           80
52712
 YDOT =       3383
087933  meter/sec      RA   =          286
42396  deg
 ZDOT =      -4786
136046                 TA   =           62
29714
                                          MA   =           62
21247
                                          Ha   =            191
013  n
mi
                                          Hp   =            187
684

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3021810
60                 X    =          840014
95
 Y    =       19230017
57  feet           Y    =         5871155
66  meter
 Z    =       10415688
21                 Z    =         3178980
01
 XDOT =     -16373
066401                 XDOT =       -5004
719668
 YDOT =      11099
369860  feet/sec       YDOT =        3327
202101  meter/sec
 ZDOT =     -15702
546083                 ZDOT =       -4810
414315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14121452
89                 X    =        -4304218
84
 Y    =       13384840
12  feet           Y    =         4079699
27  meter
 Z    =       10432741
69                 Z    =         3179899
67
 XDOT =     -17418
578620                 XDOT =       -5309
182763
 YDOT =      -6031
762642  feet/sec       YDOT =       -1838
481253  meter/sec
 ZDOT =     -15799
251618                 ZDOT =       -4815
611893


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
18014300  
00016717  00000-0  10270-3 0  9020
2 25544  51
6482 286
9492 0005161 294
9023  65
1603 15
72589072 21741


Satellite: ISS
Catalog Number: 25544
Epoch time:      10157
18014300   =   yrday
fracday
Element set:     902
Inclination:       51
6482  deg
RA of node:       286
9492  deg
Eccentricity:     
0005161     
Arg of perigee:   294
9023  deg
Mean anomaly:      65
1603  deg
Mean motion:   15
72589072  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2174
Checksum:              295


Coasting Arc #4 (Orbit 2189)
---------------------------------------

Vector Time (GMT): 2010/158/03:24:12
144
Vector Time (MET): N/A
Weight (LBS)     : 814961
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3947381
67                 A    =         6729419
17  meter
 Y    =       -3798808
00  meter          E    =           
0006392
 Z    =        3902013
79                 I    =           51
31524
 XDOT =       2031
731734                 Wp   =           84
38562
 YDOT =       6245
477311  meter/sec      RA   =          281
32674  deg
 ZDOT =       4019
904815                 TA   =          323
61946
                                          MA   =          323
66289
                                          Ha   =            191
033  n
mi
                                          Hp   =            187
586

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12950727
26                 X    =         3970611
76
 Y    =      -12463280
86  feet           Y    =        -3754536
56  meter
 Z    =       12801882
52                 Z    =         3921246
41
 XDOT =       6665
786529                 XDOT =        1942
214483
 YDOT =      20490
411125  feet/sec       YDOT =        6267
696396  meter/sec
 ZDOT =      13188
664092                 ZDOT =        4029
558312

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17633973
96                 X    =         5374835
26
 Y    =        3182836
81  feet           Y    =          970128
66  meter
 Z    =       12878486
50                 Z    =         3925362
68
 XDOT =     -12563
807015                 XDOT =       -3829
448378
 YDOT =      16021
284955  feet/sec       YDOT =        4883
287654  meter/sec
 ZDOT =      13227
134514                 ZDOT =        4031
630600


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
19687126  
00016717  00000-0  10270-3 0  9035
2 25544  51
6488 281
7387 0005271 299
8955  60
1684 15
72617941 21902


Satellite: ISS
Catalog Number: 25544
Epoch time:      10158
19687126   =   yrday
fracday
Element set:     903
Inclination:       51
6488  deg
RA of node:       281
7387  deg
Eccentricity:     
0005271     
Arg of perigee:   299
8955  deg
Mean anomaly:      60
1684  deg
Mean motion:   15
72617941  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2190
Checksum:              341


Coasting Arc #5 (Orbit 2202)
---------------------------------------

Vector Time (GMT): 2010/159/00:04:52
486
Vector Time (MET): N/A
Weight (LBS)     : 814706
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4192431
14                 A    =         6726894
57  meter
 Y    =        1908205
78  meter          E    =           
0007881
 Z    =       -4909252
80                 I    =           51
29622
 XDOT =       -837
601852                 Wp   =           49
94566
 YDOT =      -7341
913965  meter/sec      RA   =          276
88174  deg
 ZDOT =      -2135
735384                 TA   =          199
19741
                                          MA   =          199
22712
                                          Ha   =            191
194  n
mi
                                          Hp   =            188
835

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13754695
34                 X    =        -4189608
86
 Y    =        6260517
64  feet           Y    =         1861339
88  meter
 Z    =      -16106472
44                 Z    =        -4929612
83
 XDOT =      -2748
037573                 XDOT =        -745
065832
 YDOT =     -24087
644243  feet/sec       YDOT =       -7350
762875  meter/sec
 ZDOT =      -7007
005854                 ZDOT =       -2139
580619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2954284
79                 X    =         -900466
00
 Y    =      -14732238
83  feet           Y    =        -4490386
40  meter
 Z    =      -16187573
00                 Z    =        -4933972
25
 XDOT =      22991
060413                 XDOT =        7007
675214
 YDOT =       3115
421031  feet/sec       YDOT =         949
580330  meter/sec
 ZDOT =      -7022
344323                 ZDOT =       -2140
410550


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
02295497  
00016717  00000-0  10270-3 0  9045
2 25544  51
6470 277
5048 0006344 284
9612  75
0848 15
72150099 22035


Satellite: ISS
Catalog Number: 25544
Epoch time:      10159
02295497   =   yrday
fracday
Element set:     904
Inclination:       51
6470  deg
RA of node:       277
5048  deg
Eccentricity:     
0006344     
Arg of perigee:   284
9612  deg
Mean anomaly:      75
0848  deg
Mean motion:   15
72150099  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2203
Checksum:              314


Coasting Arc #6 (Orbit 2203)
---------------------------------------

Vector Time (GMT): 2010/159/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4150450
80                 A    =         6728655
66  meter
 Y    =        2166261
72  meter          E    =           
0005468
 Z    =       -4837557
98                 I    =           51
29824
 XDOT =      -1054
089997                 Wp   =           45
60229
 YDOT =      -7251
783263  meter/sec      RA   =          276
55861  deg
 ZDOT =      -2340
841727                 TA   =          201
43734
                                          MA   =          201
46025
                                          Ha   =            191
034  n
mi
                                          Hp   =            190
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13616964
56                 X    =        -4150865
55
 Y    =        7107157
88  feet           Y    =         2119847
18  meter
 Z    =      -15871253
22                 Z    =        -4857721
90
 XDOT =      -3458
300516                 XDOT =        -961
549360
 YDOT =     -23791
939840  feet/sec       YDOT =       -7263
053020  meter/sec
 ZDOT =      -7679
926925                 ZDOT =       -2345
738662

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9247316
66                 X    =        -2818582
12
 Y    =      -12159958
19  feet           Y    =        -3706355
26  meter
 Z    =      -15951571
94                 Z    =        -4862039
13
 XDOT =      22012
168626                 XDOT =        6709
308997
 YDOT =      -6630
255840  feet/sec       YDOT =       -2020
901980  meter/sec
 ZDOT =      -7699
454834                 ZDOT =       -2346
793833


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
08652384  
00016717  00000-0  10270-3 0  9054
2 25544  51
6482 277
1799 0007721 272
0285  87
9992 15
71640092 22040


Satellite: ISS
Catalog Number: 25544
Epoch time:      10159
08652384   =   yrday
fracday
Element set:     905
Inclination:       51
6482  deg
RA of node:       277
1799  deg
Eccentricity:     
0007721     
Arg of perigee:   272
0285  deg
Mean anomaly:      87
9992  deg
Mean motion:   15
71640092  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2204
Checksum:              328


Coasting Arc #7 (Orbit 2219)
---------------------------------------

Vector Time (GMT): 2010/160/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2041004
15                 A    =         6735685
99  meter
 Y    =        5809399
36  meter          E    =           
0005918
 Z    =        2722895
48                 I    =           51
31930
 XDOT =      -4207
766651                 Wp   =          107
72061
 YDOT =       3889
777708  meter/sec      RA   =          271
37626  deg
 ZDOT =      -5137
568653                 TA   =           41
07625
                                          MA   =           41
03170
                                          Ha   =            191
492  n
mi
                                          Hp   =            190
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6696207
85                 X    =         1962663
17
 Y    =       19059709
19  feet           Y    =         5831784
67  meter
 Z    =        8933384
14                 Z    =         2732621
37
 XDOT =     -13805
008699                 XDOT =       -4225
992356
 YDOT =      12761
737886  feet/sec       YDOT =        3842
622780  meter/sec
 ZDOT =     -16855
540200                 ZDOT =       -5158
054018

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17527606
07                 X    =        -5342414
33
 Y    =       10010028
38  feet           Y    =         3051056
65  meter
 Z    =        8972147
09                 Z    =         2734710
43
 XDOT =     -14318
021113                 XDOT =       -4364
132835
 YDOT =      -9868
239815  feet/sec       YDOT =       -3007
839495  meter/sec
 ZDOT =     -16937
136857                 ZDOT =       -5162
439314


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
10388864  
00016717  00000-0  10270-3 0  9069
2 25544  51
6480 271
9745 0007753 275
7419  84
2859 15
71630606 22205


Satellite: ISS
Catalog Number: 25544
Epoch time:      10160
10388864   =   yrday
fracday
Element set:     906
Inclination:       51
6480  deg
RA of node:       271
9745  deg
Eccentricity:     
0007753     
Arg of perigee:   275
7419  deg
Mean anomaly:      84
2859  deg
Mean motion:   15
71630606  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2220
Checksum:              318


Coasting Arc #8 (Orbit 2235)
---------------------------------------

Vector Time (GMT): 2010/161/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2966335
10                 A    =         6731639
33  meter
 Y    =       -4476157
21  meter          E    =           
0002879
 Z    =        4057979
40                 I    =           51
30698
 XDOT =       3433
504755                 Wp   =          111
60155
 YDOT =       5735
599635  meter/sec      RA   =          266
28346  deg
 ZDOT =       3813
591365                 TA   =          298
97328
                                          MA   =          299
00214
                                          Ha   =            191
774  n
mi
                                          Hp   =            190
599

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9732070
54                 X    =         2996454
61
 Y    =      -14685555
16  feet           Y    =        -4442818
16  meter
 Z    =       13313580
72                 Z    =         4072462
49
 XDOT =      11264
779379                 XDOT =        3350
587043
 YDOT =      18817
584104  feet/sec       YDOT =        5773
530876  meter/sec
 ZDOT =      12511
782695                 ZDOT =        3830
071131

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16314916
42                 X    =         4972786
53
 Y    =        6531682
48  feet           Y    =         1990856
82  meter
 Z    =       13371267
14                 Z    =         4075562
22
 XDOT =     -15732
756406                 XDOT =       -4795
344152
 YDOT =      13528
164326  feet/sec       YDOT =        4123
384487  meter/sec
 ZDOT =      12577
455627                 ZDOT =        3833
608475


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
12123751  
00016717  00000-0  10270-3 0  9075
2 25544  51
6486 266
7684 0007785 280
5736  79
4549 15
71660772 22362


Satellite: ISS
Catalog Number: 25544
Epoch time:      10161
12123751   =   yrday
fracday
Element set:     907
Inclination:       51
6486  deg
RA of node:       266
7684  deg
Eccentricity:     
0007785     
Arg of perigee:   280
5736  deg
Mean anomaly:      79
4549  deg
Mean motion:   15
71660772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2236
Checksum:              331


Coasting Arc #9 (Orbit 2250)
---------------------------------------

Vector Time (GMT): 2010/162/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3770450
55                 A    =         6732153
13  meter
 Y    =       -4008748
56  meter          E    =           
0001283
 Z    =       -3876378
12                 I    =           51
31270
 XDOT =       2328
569812                 Wp   =          274
87513
 YDOT =      -6112
045158  meter/sec      RA   =          261
09111  deg
 ZDOT =       4054
775100                 TA   =           37
58538
                                          MA   =           37
57642
                                          Ha   =            192
019  n
mi
                                          Hp   =            190
415

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12370244
58                 X    =        -3706512
79
 Y    =      -13152062
22  feet           Y    =        -4050553
76  meter
 Z    =      -12717775
98                 Z    =        -3894540
65
 XDOT =       7639
664739                 XDOT =        2377
045139
 YDOT =     -20052
641596  feet/sec       YDOT =       -6085
735435  meter/sec
 ZDOT =      13303
067914                 ZDOT =        4066
204020

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10183238
62                 X    =         3103851
13
 Y    =      -14847731
05  feet           Y    =        -4525588
43  meter
 Z    =      -12790154
46                 Z    =        -3898439
08
 XDOT =      20129
931532                 XDOT =        6135
603131
 YDOT =       2304
312489  feet/sec       YDOT =         702
354447  meter/sec
 ZDOT =      13348
584145                 ZDOT =        4068
648447


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
07498806  
00016717  00000-0  10270-3 0  9087
2 25544  51
6490 261
8881 0007907 284
6790  75
3496 15
71694308 22518


Satellite: ISS
Catalog Number: 25544
Epoch time:      10162
07498806   =   yrday
fracday
Element set:     908
Inclination:       51
6490  deg
RA of node:       261
8881  deg
Eccentricity:     
0007907     
Arg of perigee:   284
6790  deg
Mean anomaly:      75
3496  deg
Mean motion:   15
71694308  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2251
Checksum:              339


Coasting Arc #10 (Orbit 2266)
---------------------------------------

Vector Time (GMT): 2010/163/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -964820
34                 A    =         6734896
70  meter
 Y    =        5964959
76  meter          E    =           
0003511
 Z    =       -2972594
18                 I    =           51
32781
 XDOT =      -4899
715830                 Wp   =          284
44845
 YDOT =      -3263
963799  meter/sec      RA   =          256
00089  deg
 ZDOT =      -4953
576055                 TA   =          289
98145
                                          MA   =          290
01926
                                          Ha   =            192
384  n
mi
                                          Hp   =            190
370

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3165421
06                 X    =        -1017009
46
 Y    =       19570077
94  feet           Y    =         5953879
37  meter
 Z    =       -9752605
58                 Z    =        -2977406
85
 XDOT =     -16075
183168                 XDOT =       -4838
789681
 YDOT =     -10708
542648  feet/sec       YDOT =       -3318
413663  meter/sec
 ZDOT =     -16251
889944                 ZDOT =       -4977
231742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19755310
01                 X    =        -6021418
49
 Y    =        1536742
16  feet           Y    =          468399
01  meter
 Z    =       -9771760
66                 Z    =        -2978432
65
 XDOT =       6803
984717                 XDOT =        2073
854542
 YDOT =     -16593
538214  feet/sec       YDOT =       -5057
710448  meter/sec
 ZDOT =     -16346
163625                 ZDOT =       -4982
310673


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
09230815  
00016717  00000-0  10270-3 0  9095
2 25544  51
6491 256
6827 0008032 288
0693  71
9594 15
71695575 22676


Satellite: ISS
Catalog Number: 25544
Epoch time:      10163
09230815   =   yrday
fracday
Element set:     909
Inclination:       51
6491  deg
RA of node:       256
6827  deg
Eccentricity:     
0008032     
Arg of perigee:   288
0693  deg
Mean anomaly:      71
9594  deg
Mean motion:   15
71695575  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2267
Checksum:              335


Coasting Arc #11 (Orbit 2282)
---------------------------------------

Vector Time (GMT): 2010/164/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4543210
04                 A    =         6728821
95  meter
 Y    =        1604734
23  meter          E    =           
0006851
 Z    =        4700456
63                 I    =           51
31638
 XDOT =        234
754975                 Wp   =          354
19305
 YDOT =       7207
662046  meter/sec      RA   =          250
81549  deg
 ZDOT =      -2681
216040                 TA   =          122
35528
                                          MA   =          122
28894
                                          Ha   =            192
510  n
mi
                                          Hp   =            190
001

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14905544
74                 X    =         4502093
94
 Y    =        5264876
09  feet           Y    =         1655308
23  meter
 Z    =       15421445
63                 Z    =         4722428
05
 XDOT =        770
193487                 XDOT =         167
165029
 YDOT =      23647
185189  feet/sec       YDOT =        7209
909865  meter/sec
 ZDOT =      -8796
640551                 ZDOT =       -2680
238255

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1400187
90                 X    =         -426777
27
 Y    =       15659666
03  feet           Y    =         4773066
21  meter
 Z    =       15509013
62                 Z    =         4727147
35
 XDOT =     -21550
940660                 XDOT =       -6568
726713
 YDOT =       6801
783262  feet/sec       YDOT =        2073
183538  meter/sec
 ZDOT =      -8792
711423                 ZDOT =       -2680
018442


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
10961219  
00016717  00000-0  10270-3 0  9109
2 25544  51
6488 251
4769 0008099 293
2884  66
7425 15
71777997 22835


Satellite: ISS
Catalog Number: 25544
Epoch time:      10164
10961219   =   yrday
fracday
Element set:     910
Inclination:       51
6488  deg
RA of node:       251
4769  deg
Eccentricity:     
0008099     
Arg of perigee:   293
2884  deg
Mean anomaly:      66
7425  deg
Mean motion:   15
71777997  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2283
Checksum:              348


Coasting Arc #12 (Orbit 2298)
---------------------------------------

Vector Time (GMT): 2010/165/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1399801
59                 A    =         6737359
69  meter
 Y    =       -6365042
97  meter          E    =           
0011292
 Z    =        1678700
91                 I    =           51
35530
 XDOT =       5165
447313                 Wp   =           29
06141
 YDOT =        368
669508  meter/sec      RA   =          245
71157  deg
 ZDOT =       5698
817761                 TA   =          349
56352
                                          MA   =          349
58694
                                          Ha   =            192
749  n
mi
                                          Hp   =            189
867

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4592524
90                 X    =        -1336677
28
 Y    =      -20882686
92  feet           Y    =        -6380343
78  meter
 Z    =        5507548
91                 Z    =         1672052
73
 XDOT =      16947
005619                 XDOT =        5133
257164
 YDOT =       1209
545629  feet/sec       YDOT =         426
251475  meter/sec
 ZDOT =      18696
908665                 ZDOT =        5723
833295

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18897067
19                 X    =         5759826
08
 Y    =      -10018498
82  feet           Y    =        -3053638
44  meter
 Z    =        5481015
07                 Z    =         1670613
39
 XDOT =       2586
072956                 XDOT =         788
235037
 YDOT =      15172
701756  feet/sec       YDOT =        4624
639495  meter/sec
 ZDOT =      18796
615216                 ZDOT =        5729
208318


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
12690369  
00016717  00000-0  10270-3 0  9118
2 25544  51
6483 246
2704 0008108 297
4801  62
5537 15
71757470 22996


Satellite: ISS
Catalog Number: 25544
Epoch time:      10165
12690369   =   yrday
fracday
Element set:     911
Inclination:       51
6483  deg
RA of node:       246
2704  deg
Eccentricity:     
0008108     
Arg of perigee:   297
4801  deg
Mean anomaly:      62
5537  deg
Mean motion:   15
71757470  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2299
Checksum:              318


Coasting Arc #13 (Orbit 2313)
---------------------------------------

Vector Time (GMT): 2010/166/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4217593
14                 A    =         6726782
20  meter
 Y    =         932760
62  meter          E    =           
0007526
 Z    =       -5162599
06                 I    =           51
33293
 XDOT =      -2929
482753                 Wp   =           74
29932
 YDOT =      -7022
989074  meter/sec      RA   =          240
54685  deg
 ZDOT =       1127
726892                 TA   =          206
50336
                                          MA   =          206
54187
                                          Ha   =            192
807  n
mi
                                          Hp   =            189
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13837247
84                 X    =        -4202631
21
 Y    =        3060238
24  feet           Y    =          885681
59  meter
 Z    =      -16937660
97                 Z    =        -5183051
46
 XDOT =      -9611
163888                 XDOT =       -2856
210940
 YDOT =     -23041
302735  feet/sec       YDOT =       -7055
338818  meter/sec
 ZDOT =       3699
891378                 ZDOT =        1113
672259

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6819819
04                 X    =        -2078680
84
 Y    =      -12310824
13  feet           Y    =        -3752339
19  meter
 Z    =      -17019181
02                 Z    =        -5187446
38
 XDOT =      18478
454071                 XDOT =        5632
232801
 YDOT =     -15258
699268  feet/sec       YDOT =       -4650
851537  meter/sec
 ZDOT =       3643
816646                 ZDOT =        1110
635314


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
08059966  
00016717  00000-0  10270-3 0  9127
2 25544  51
6475 241
3894 0008165 300
9784  59
0576 15
71799161 23141


Satellite: ISS
Catalog Number: 25544
Epoch time:      10166
08059966   =   yrday
fracday
Element set:     912
Inclination:       51
6475  deg
RA of node:       241
3894  deg
Eccentricity:     
0008165     
Arg of perigee:   300
9784  deg
Mean anomaly:      59
0576  deg
Mean motion:   15
71799161  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2314
Checksum:              332


Coasting Arc #14 (Orbit 2329)
---------------------------------------

Vector Time (GMT): 2010/167/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3626364
31                 A    =         6738508
27  meter
 Y    =        5668944
79  meter          E    =           
0004218
 Z    =        -289982
14                 I    =           51
38761
 XDOT =      -4187
281325                 Wp   =          162
98418
 YDOT =       2372
819579  meter/sec      RA   =          235
42121  deg
 ZDOT =      -6002
992300                 TA   =           20
17414
                                          MA   =           20
15748
                                          Ha   =            193
078  n
mi
                                          Hp   =            189
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11897520
69                 X    =         3564112
29
 Y    =       18598900
22  feet           Y    =         5709148
93  meter
 Z    =        -951384
98                 Z    =         -272515
74
 XDOT =     -13737
799624                 XDOT =       -4184
342251
 YDOT =       7784
841138  feet/sec       YDOT =        2326
012293  meter/sec
 ZDOT =     -19694
856626                 ZDOT =       -6023
326402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14184195
68                 X    =        -4323342
84
 Y    =       16923546
11  feet           Y    =         5158296
86  meter
 Z    =        -881703
63                 Z    =         -268743
27
 XDOT =     -10269
829897                 XDOT =       -3130
244153
 YDOT =      -9633
007094  feet/sec       YDOT =       -2936
140562  meter/sec
 ZDOT =     -19775
899129                 ZDOT =       -6027
694054


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
09786297  
00016717  00000-0  10270-3 0  9134
2 25544  51
6472 236
1836 0008093 303
9957  56
0436 15
71765589 23308


Satellite: ISS
Catalog Number: 25544
Epoch time:      10167
09786297   =   yrday
fracday
Element set:     913
Inclination:       51
6472  deg
RA of node:       236
1836  deg
Eccentricity:     
0008093     
Arg of perigee:   303
9957  deg
Mean anomaly:      56
0436  deg
Mean motion:   15
71765589  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2330
Checksum:              336


Coasting Arc #15 (Orbit 2345)
---------------------------------------

Vector Time (GMT): 2010/168/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2889382
92                 A    =         6726413
82  meter
 Y    =       -3076746
10  meter          E    =           
0005640
 Z    =        5240343
66                 I    =           51
36497
 XDOT =       5189
747245                 Wp   =          317
49321
 YDOT =       5662
658602  meter/sec      RA   =          230
28420  deg
 ZDOT =        467
601994                 TA   =          128
07071
                                          MA   =          128
01981
                                          Ha   =            193
174  n
mi
                                          Hp   =            189
138

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9479602
74                 X    =         2898116
48
 Y    =      -10094311
36  feet           Y    =        -3044387
17  meter
 Z    =       17192728
55                 Z    =         5254400
97
 XDOT =      17026
729805                 XDOT =        5123
769150
 YDOT =      18578
276252  feet/sec       YDOT =        5720
324482  meter/sec
 ZDOT =       1534
127276                 ZDOT =         492
654075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12537808
11                 X    =         3821523
91
 Y    =        5712457
61  feet           Y    =         1741157
08  meter
 Z    =       17248742
01                 Z    =         5257416
56
 XDOT =     -11840
602411                 XDOT =       -3609
015615
 YDOT =      21097
253829  feet/sec       YDOT =        6430
442967  meter/sec
 ZDOT =       1634
066768                 ZDOT =         498
063551


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
11511022  
00016717  00000-0  10270-3 0  9141
2 25544  51
6467 230
9761 0008184 309
1030  50
9404 15
71814235 23460


Satellite: ISS
Catalog Number: 25544
Epoch time:      10168
11511022   =   yrday
fracday
Element set:     914
Inclination:       51
6467  deg
RA of node:       230
9761  deg
Eccentricity:     
0008184     
Arg of perigee:   309
1030  deg
Mean anomaly:      50
9404  deg
Mean motion:   15
71814235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2346
Checksum:              275


Coasting Arc #16 (Orbit 2360)
---------------------------------------

Vector Time (GMT): 2010/169/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5264596
06                 A    =         6737793
37  meter
 Y    =       -4043752
56  meter          E    =           
0013143
 Z    =       -1101277
70                 I    =           51
42275
 XDOT =       2192
260969                 Wp   =          358
74048
 YDOT =      -4454
403606  meter/sec      RA   =          225
13195  deg
 ZDOT =       5887
627169                 TA   =          349
17556
                                          MA   =          349
20382
                                          Ha   =            193
363  n
mi
                                          Hp   =            188
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17272296
80                 X    =        -5213637
03
 Y    =      -13266904
72  feet           Y    =        -4102339
36  meter
 Z    =       -3613115
83                 Z    =        -1126729
67
 XDOT =       7192
457248                 XDOT =        2213
307110
 YDOT =     -14614
185060  feet/sec       YDOT =       -4429
771450  meter/sec
 ZDOT =      19316
362102                 ZDOT =        5898
327717

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6789091
70                 X    =         2069315
15
 Y    =      -20676248
44  feet           Y    =        -6302120
52  meter
 Z    =       -3714645
09                 Z    =        -1132223
82
 XDOT =      14626
755116                 XDOT =        4458
234959
 YDOT =       1331
390807  feet/sec       YDOT =         405
807918  meter/sec
 ZDOT =      19358
975680                 ZDOT =        5900
615787


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
06876654  
00016717  00000-0  10270-3 0  9152
2 25544  51
6457 226
0939 0008366 312
6986  47
3470 15
71833604 23614


Satellite: ISS
Catalog Number: 25544
Epoch time:      10169
06876654   =   yrday
fracday
Element set:     915
Inclination:       51
6457  deg
RA of node:       226
0939  deg
Eccentricity:     
0008366     
Arg of perigee:   312
6986  deg
Mean anomaly:      47
3470  deg
Mean motion:   15
71833604  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2361
Checksum:              330


Coasting Arc #17 (Orbit 2376)
---------------------------------------

Vector Time (GMT): 2010/170/01:35:52
307
Vector Time (MET): N/A
Weight (LBS)     : 814451
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -816129
31                 A    =         6727583
33  meter
 Y    =        4482176
58  meter          E    =           
0011496
 Z    =       -4958816
38                 I    =           51
40963
 XDOT =      -6581
630749                 Wp   =           35
61887
 YDOT =      -3431
255632  meter/sec      RA   =          220
02379  deg
 ZDOT =      -2011
373352                 TA   =          214
79349
                                          MA   =          214
86871
                                          Ha   =            193
526  n
mi
                                          Hp   =            188
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2677589
59                 X    =         -842100
15
 Y    =       14705303
74  feet           Y    =         4472905
48  meter
 Z    =      -16269082
60                 Z    =        -4962843
71
 XDOT =     -21593
276737                 XDOT =       -6533
001785
 YDOT =     -11257
400369  feet/sec       YDOT =       -3504
583228  meter/sec
 ZDOT =      -6598
993936                 ZDOT =       -2043
229153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14683722
55                 X    =        -4475598
63
 Y    =        2698658
22  feet           Y    =          822551
03  meter
 Z    =      -16285086
08                 Z    =        -4963694
24
 XDOT =       3247
533813                 XDOT =         989
848306
 YDOT =     -23053
890126  feet/sec       YDOT =       -7026
825711  meter/sec
 ZDOT =      -6726
060500                 ZDOT =       -2050
103241


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
08598699  
00016717  00000-0  10270-3 0  9167
2 25544  51
6447 220
8866 0008317 316
4229  43
6275 15
71867423 23777


Satellite: ISS
Catalog Number: 25544
Epoch time:      10170
08598699   =   yrday
fracday
Element set:     916
Inclination:       51
6447  deg
RA of node:       220
8866  deg
Eccentricity:     
0008317     
Arg of perigee:   316
4229  deg
Mean anomaly:      43
6275  deg
Mean motion:   15
71867423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2377
Checksum:              338

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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