Date: March 1st 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


There are no maneuvers



Coasting Arc #1 (Orbit 1139)
---------------------------------------

Vector Time (GMT): 2008/060/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5965025
78                 A    =         6724293
52  meter
 Y    =        1661343
66  meter          E    =           
0014472
 Z    =        2601611
68                 I    =           51
45976
 XDOT =        728
125979                 Wp   =          114
50933
 YDOT =       5610
489770  meter/sec      RA   =          215
11676  deg
 ZDOT =      -5235
392495                 TA   =           35
80593
                                          MA   =           35
70899
                                          Ha   =            187
624  n
mi
                                          Hp   =            181
130

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19570294
57                 X    =         5933367
05
 Y    =        5450602
56  feet           Y    =         1727870
97  meter
 Z    =        8535471
39                 Z    =         2630512
52
 XDOT =       2388
864762                 XDOT =         690
766779
 YDOT =      18407
118668  feet/sec       YDOT =        5618
423205  meter/sec
 ZDOT =     -17176
484565                 ZDOT =       -5231
946046

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20256648
77                 X    =         6174226
54
 Y    =         684924
90  feet           Y    =          208765
11  meter
 Z    =        8646318
77                 Z    =         2635397
96
 XDOT =       6813
964357                 XDOT =        2076
896336
 YDOT =      15821
782138  feet/sec       YDOT =        4822
479196  meter/sec
 ZDOT =     -17162
625684                 ZDOT =       -5231
168308


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   08060
63602189  
00020000  00000-0  20000-3 0  9008
2 25544  51
6369 215
9045 0003004 184
1180 175
9960 15
75709479 11405


Satellite: ISS
Catalog Number: 25544
Epoch time:      08060
63602189   =   yrday
fracday
Element set:     900
Inclination:       51
6369  deg
RA of node:       215
9045  deg
Eccentricity:     
0003004     
Arg of perigee:   184
1180  deg
Mean anomaly:     175
9960  deg
Mean motion:   15
75709479  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1140
Checksum:              285


Coasting Arc #2 (Orbit 1155)
---------------------------------------

Vector Time (GMT): 2008/061/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -379947
01                 A    =         6716928
50  meter
 Y    =       -4656163
58  meter          E    =           
0008457
 Z    =        4823955
56                 I    =           51
46086
 XDOT =       7078
676420                 Wp   =          139
69655
 YDOT =       1897
241747  meter/sec      RA   =          209
99680  deg
 ZDOT =       2380
111980                 TA   =          286
99678
                                          MA   =          287
08944
                                          Ha   =            187
462  n
mi
                                          Hp   =            181
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1246545
32                 X    =         -351286
38
 Y    =      -15276127
23  feet           Y    =        -4660252
13  meter
 Z    =       15826625
84                 Z    =         4822179
40
 XDOT =      23224
004004                 XDOT =        7045
373094
 YDOT =       6224
546414  feet/sec       YDOT =        1976
213327  meter/sec
 ZDOT =       7808
766337                 ZDOT =        2414
418771

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5156185
26                 X    =        -1571605
27
 Y    =      -14441620
79  feet           Y    =        -4401806
02  meter
 Z    =       15819271
99                 Z    =         4821714
10
 XDOT =      22946
927701                 XDOT =        6994
223563
 YDOT =        536
111839  feet/sec       YDOT =         163
406889  meter/sec
 ZDOT =       7940
354089                 ZDOT =        2420
219926


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   08061
65072648  
00020000  00000-0  20000-3 0  9013
2 25544  51
6376 210
6797 0002858 190
0418 170
0689 15
75796962 11569


Satellite: ISS
Catalog Number: 25544
Epoch time:      08061
65072648   =   yrday
fracday
Element set:     901
Inclination:       51
6376  deg
RA of node:       210
6797  deg
Eccentricity:     
0002858     
Arg of perigee:   190
0418  deg
Mean anomaly:     170
0689  deg
Mean motion:   15
75796962  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1156
Checksum:              314


Coasting Arc #3 (Orbit 1170)
---------------------------------------

Vector Time (GMT): 2008/062/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6351073
47                 A    =         6726072
70  meter
 Y    =       -1615378
38  meter          E    =           
0005920
 Z    =       -1507028
20                 I    =           51
51774
 XDOT =        -71
325485                 Wp   =           47
55973
 YDOT =      -5091
353842  meter/sec      RA   =          204
80370  deg
 ZDOT =       5776
299032                 TA   =          295
80373
                                          MA   =          295
86479
                                          Ha   =            187
357  n
mi
                                          Hp   =            181
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20836855
21                 X    =        -6325217
30
 Y    =       -5299797
83  feet           Y    =        -1686255
14  meter
 Z    =       -4944318
23                 Z    =        -1537818
32
 XDOT =       -234
007497                 XDOT =         -42
447563
 YDOT =     -16703
916806  feet/sec       YDOT =       -5091
989969  meter/sec
 ZDOT =      18951
112309                 ZDOT =        5776
022692

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21466863
80                 X    =        -6543100
09
 Y    =         504304
58  feet           Y    =          153712
04  meter
 Z    =       -5062421
36                 Z    =        -1543026
03
 XDOT =      -4793
874765                 XDOT =       -1461
173028
 YDOT =     -14428
472323  feet/sec       YDOT =       -4397
798364  meter/sec
 ZDOT =      18949
445907                 ZDOT =        5775
791113


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   08062
60199182  
00020000  00000-0  20000-3 0  9023
2 25544  51
6376 205
7817 0002593 194
0443 166
0649 15
75779854 11714


Satellite: ISS
Catalog Number: 25544
Epoch time:      08062
60199182   =   yrday
fracday
Element set:     902
Inclination:       51
6376  deg
RA of node:       205
7817  deg
Eccentricity:     
0002593     
Arg of perigee:   194
0443  deg
Mean anomaly:     166
0649  deg
Mean motion:   15
75779854  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1171
Checksum:              309


Coasting Arc #4 (Orbit 1186)
---------------------------------------

Vector Time (GMT): 2008/063/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -319516
30                 A    =         6715260
32  meter
 Y    =        4266376
95  meter          E    =           
0013465
 Z    =       -5187444
44                 I    =           51
50872
 XDOT =      -7413
516874                 Wp   =           92
13344
 YDOT =      -1789
987262  meter/sec      RA   =          199
66898  deg
 ZDOT =      -1018
294838                 TA   =          168
14766
                                          MA   =          168
11594
                                          Ha   =            187
197  n
mi
                                          Hp   =            181
212

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1048281
84                 X    =         -342000
74
 Y    =       13997299
70  feet           Y    =         4262678
14  meter
 Z    =      -17019174
68                 Z    =        -5189051
29
 XDOT =     -24322
561923                 XDOT =       -7388
003392
 YDOT =      -5872
661622  feet/sec       YDOT =       -1872
746798  meter/sec
 ZDOT =      -3340
862328                 ZDOT =       -1054
246903

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3091686
38                 X    =          942346
01
 Y    =       13684763
12  feet           Y    =         4171115
80  meter
 Z    =      -17024815
24                 Z    =        -5189163
69
 XDOT =     -23969
696210                 XDOT =       -7305
963405
 YDOT =       1098
708922  feet/sec       YDOT =         334
886479  meter/sec
 ZDOT =      -3478
770598                 ZDOT =       -1060
329278


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   08063
61664902  
00020000  00000-0  20000-3 0  9033
2 25544  51
6377 200
5569 0002617 199
6326 160
4738 15
75830951 11870


Satellite: ISS
Catalog Number: 25544
Epoch time:      08063
61664902   =   yrday
fracday
Element set:     903
Inclination:       51
6377  deg
RA of node:       200
5569  deg
Eccentricity:     
0002617     
Arg of perigee:   199
6326  deg
Mean anomaly:     160
4738  deg
Mean motion:   15
75830951  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1187
Checksum:              305


Coasting Arc #5 (Orbit 1202)
---------------------------------------

Vector Time (GMT): 2008/064/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6547496
57                 A    =         6726836
65  meter
 Y    =        1488116
61  meter          E    =           
0013937
 Z    =         250577
85                 I    =           51
57578
 XDOT =       -836
759806                 Wp   =          142
28822
 YDOT =       4724
840245  meter/sec      RA   =          194
50113  deg
 ZDOT =      -6030
469360                 TA   =           34
98334
                                          MA   =           34
89186
                                          Ha   =            187
126  n
mi
                                          Hp   =            181
180

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21481287
96                 X    =         6529152
37
 Y    =        4882272
36  feet           Y    =         1561231
90  meter
 Z    =         822105
82                 Z    =          282340
21
 XDOT =      -2745
274954                 XDOT =        -860
237292
 YDOT =      15501
444374  feet/sec       YDOT =        4715
351637  meter/sec
 ZDOT =     -19785
004462                 ZDOT =       -6034
591433

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21947046
15                 X    =         6689459
67
 Y    =       -1842364
28  feet           Y    =         -561552
63  meter
 Z    =         943945
42                 Z    =          287714
56
 XDOT =       2044
720553                 XDOT =         623
230824
 YDOT =      13971
387751  feet/sec       YDOT =        4258
478987  meter/sec
 ZDOT =     -19800
219254                 ZDOT =       -6035
106829


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   08064
63128135  
00020000  00000-0  20000-3 0  9040
2 25544  51
6374 195
3319 0002572 201
0157 159
0902 15
75867794 12032


Satellite: ISS
Catalog Number: 25544
Epoch time:      08064
63128135   =   yrday
fracday
Element set:     904
Inclination:       51
6374  deg
RA of node:       195
3319  deg
Eccentricity:     
0002572     
Arg of perigee:   201
0157  deg
Mean anomaly:     159
0902  deg
Mean motion:   15
75867794  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1203
Checksum:              284


Coasting Arc #6 (Orbit 1218)
---------------------------------------

Vector Time (GMT): 2008/065/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1166315
79                 A    =         6714578
65  meter
 Y    =       -4025989
76  meter          E    =           
0001847
 Z    =        5244442
48                 I    =           51
56480
 XDOT =       7524
944210                 Wp   =          135
61084
 YDOT =       1598
351271  meter/sec      RA   =          189
34479  deg
 ZDOT =       -447
679770                 TA   =          318
63555
                                          MA   =          318
64954
                                          Ha   =            186
834  n
mi
                                          Hp   =            181
169

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3826495
38                 X    =         1185772
42
 Y    =      -13208627
83  feet           Y    =        -4012838
25  meter
 Z    =       17206176
11                 Z    =         5250155
80
 XDOT =      24688
137171                 XDOT =        7508
686626
 YDOT =       5243
934616  feet/sec       YDOT =        1682
408563  meter/sec
 ZDOT =      -1468
765648                 ZDOT =        -411
164074

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -676961
22                 X    =         -206337
78
 Y    =      -13708210
41  feet           Y    =        -4178262
53  meter
 Z    =       17227568
12                 Z    =         5250962
76
 XDOT =      24079
563142                 XDOT =        7339
450846
 YDOT =      -2853
989408  feet/sec       YDOT =        -869
895972  meter/sec
 ZDOT =      -1328
692194                 ZDOT =        -404
985381


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   08065
64588585  
00020000  00000-0  20000-3 0  9052
2 25544  51
6383 190
1059 0002431 209
0787 151
0243 15
75956803 12194


Satellite: ISS
Catalog Number: 25544
Epoch time:      08065
64588585   =   yrday
fracday
Element set:     905
Inclination:       51
6383  deg
RA of node:       190
1059  deg
Eccentricity:     
0002431     
Arg of perigee:   209
0787  deg
Mean anomaly:     151
0243  deg
Mean motion:   15
75956803  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1219
Checksum:              298


Coasting Arc #7 (Orbit 1234)
---------------------------------------

Vector Time (GMT): 2008/066/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6510533
25                 A    =         6726201
71  meter
 Y    =       -1304770
77  meter          E    =           
0011748
 Z    =        1040585
94                 I    =           51
63294
 XDOT =       1867
626512                 Wp   =           60
59081
 YDOT =      -4562
184127  meter/sec      RA   =          184
20576  deg
 ZDOT =       5920
343727                 TA   =          310
79816
                                          MA   =          310
90001
                                          Ha   =            186
834  n
mi
                                          Hp   =            181
218

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21360017
22                 X    =        -6500514
09
 Y    =       -4280743
98  feet           Y    =        -1377519
16  meter
 Z    =        3413995
87                 Z    =         1008982
92
 XDOT =       6127
383570                 XDOT =        1889
743429
 YDOT =     -14967
795691  feet/sec       YDOT =       -4541
175098  meter/sec
 ZDOT =      19423
699893                 ZDOT =        5929
470562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21577511
63                 X    =        -6576825
55
 Y    =        3130358
89  feet           Y    =          954133
39  meter
 Z    =        3292767
43                 Z    =         1003635
51
 XDOT =        882
133275                 XDOT =         268
874222
 YDOT =     -14545
310609  feet/sec       YDOT =       -4433
410674  meter/sec
 ZDOT =      19458
099798                 ZDOT =        5930
828818


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   08066
66046794  
00020000  00000-0  20000-3 0  9067
2 25544  51
6384 184
8809 0002226 212
2108 147
8920 15
75950649 12358


Satellite: ISS
Catalog Number: 25544
Epoch time:      08066
66046794   =   yrday
fracday
Element set:     906
Inclination:       51
6384  deg
RA of node:       184
8809  deg
Eccentricity:     
0002226     
Arg of perigee:   212
2108  deg
Mean anomaly:     147
8920  deg
Mean motion:   15
75950649  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1235
Checksum:              307


Coasting Arc #8 (Orbit 1249)
---------------------------------------

Vector Time (GMT): 2008/067/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2103829
46                 A    =         6715596
32  meter
 Y    =        3986765
67  meter          E    =           
0012475
 Z    =       -4989092
28                 I    =           51
62649
 XDOT =      -7307
806027                 Wp   =          113
59414
 YDOT =      -1418
261901  meter/sec      RA   =          179
02928  deg
 ZDOT =       1947
196065                 TA   =          175
24342
                                          MA   =          175
23155
                                          Ha   =            186
668  n
mi
                                          Hp   =            181
081

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6902327
63                 X    =        -2124018
04
 Y    =       13079939
85  feet           Y    =         3963126
05  meter
 Z    =      -16368412
99                 Z    =        -4999361
95
 XDOT =     -23975
741557                 XDOT =       -7300
862636
 YDOT =      -4653
090226  feet/sec       YDOT =       -1499
942938  meter/sec
 ZDOT =       6388
438533                 ZDOT =        1911
712376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1781370
71                 X    =         -542961
79
 Y    =       14638319
01  feet           Y    =         4461759
63  meter
 Z    =      -16407261
57                 Z    =        -5000933
33
 XDOT =     -23048
641581                 XDOT =       -7025
225954
 YDOT =       4206
971158  feet/sec       YDOT =        1282
284809  meter/sec
 ZDOT =       6252
321732                 ZDOT =        1905
707664


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   08067
61161342  
00020000  00000-0  20000-3 0  9071
2 25544  51
6379 179
9823 0002114 217
7212 142
3804 15
76005261 12505


Satellite: ISS
Catalog Number: 25544
Epoch time:      08067
61161342   =   yrday
fracday
Element set:     907
Inclination:       51
6379  deg
RA of node:       179
9823  deg
Eccentricity:     
0002114     
Arg of perigee:   217
7212  deg
Mean anomaly:     142
3804  deg
Mean motion:   15
76005261  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1250
Checksum:              268


Coasting Arc #9 (Orbit 1265)
---------------------------------------

Vector Time (GMT): 2008/068/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6182651
45                 A    =         6724077
09  meter
 Y    =        1204874
66  meter          E    =           
0006305
 Z    =       -2345399
44                 I    =           51
68390
 XDOT =      -2949
418108                 Wp   =          154
78602
 YDOT =       4616
825310  meter/sec      RA   =          173
91609  deg
 ZDOT =      -5414
048354                 TA   =           51
62060
                                          MA   =           51
56398
                                          Ha   =            186
645  n
mi
                                          Hp   =            181
177

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20284289
54                 X    =         6180112
25
 Y    =        3953000
85  feet           Y    =         1273998
15  meter
 Z    =       -7694880
04                 Z    =        -2315370
75
 XDOT =      -9676
568595                 XDOT =       -2974
524779
 YDOT =      15147
064664  feet/sec       YDOT =        4583
702265  meter/sec
 ZDOT =     -17762
625832                 ZDOT =       -5428
437950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20358754
97                 X    =         6205348
51
 Y    =       -3789365
99  feet           Y    =        -1154998
76  meter
 Z    =       -7579683
26                 Z    =        -2310287
46
 XDOT =      -3619
343411                 XDOT =       -1103
175872
 YDOT =      16120
889635  feet/sec       YDOT =        4913
647161  meter/sec
 ZDOT =     -17817
181450                 ZDOT =       -5430
676906


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   08068
62614483  
00020000  00000-0  20000-3 0  9083
2 25544  51
6375 174
7564 0002054 221
1809 138
9201 15
76030445 12661


Satellite: ISS
Catalog Number: 25544
Epoch time:      08068
62614483   =   yrday
fracday
Element set:     908
Inclination:       51
6375  deg
RA of node:       174
7564  deg
Eccentricity:     
0002054     
Arg of perigee:   221
1809  deg
Mean anomaly:     138
9201  deg
Mean motion:   15
76030445  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1266
Checksum:              286


Coasting Arc #10 (Orbit 1281)
---------------------------------------

Vector Time (GMT): 2008/069/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3008790
18                 A    =         6717784
38  meter
 Y    =       -4117908
30  meter          E    =           
0007477
 Z    =        4367468
89                 I    =           51
69311
 XDOT =       6789
350746                 Wp   =           74
52412
 YDOT =       1368
795977  meter/sec      RA   =          168
72365  deg
 ZDOT =      -3379
933685                 TA   =           49
48840
                                          MA   =           49
42328
                                          Ha   =            186
294  n
mi
                                          Hp   =            181
093

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9871358
85                 X    =         3033397
38
 Y    =      -13510197
82  feet           Y    =        -4084124
26  meter
 Z    =       14328966
18                 Z    =         4382145
71
 XDOT =      22274
772789                 XDOT =        6789
959084
 YDOT =       4490
800448  feet/sec       YDOT =        1444
721433  meter/sec
 ZDOT =     -11089
021276                 ZDOT =       -3346
949852

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3864898
20                 X    =         1178020
97
 Y    =      -16230580
49  feet           Y    =        -4947080
93  meter
 Z    =       14384688
44                 Z    =         4384453
04
 XDOT =      21169
381070                 XDOT =        6452
427350
 YDOT =      -4694
273284  feet/sec       YDOT =       -1430
814497  meter/sec
 ZDOT =     -10962
477323                 ZDOT =       -3341
363088


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   08069
64064822  
00020000  00000-0  20000-3 0  9093
2 25544  51
6380 169
5302 0002008 232
4685 127
6297 15
76112107 12829


Satellite: ISS
Catalog Number: 25544
Epoch time:      08069
64064822   =   yrday
fracday
Element set:     909
Inclination:       51
6380  deg
RA of node:       169
5302  deg
Eccentricity:     
0002008     
Arg of perigee:   232
4685  deg
Mean anomaly:     127
6297  deg
Mean motion:   15
76112107  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1282
Checksum:              284


Coasting Arc #11 (Orbit 1297)
---------------------------------------

Vector Time (GMT): 2008/070/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5594134
54                 A    =         6720884
23  meter
 Y    =       -1238575
85  meter          E    =           
0010993
 Z    =        3505283
57                 I    =           51
73088
 XDOT =       3915
187710                 Wp   =           98
16831
 YDOT =      -4863
611693  meter/sec      RA   =          163
62740  deg
 ZDOT =       4516
242989                 TA   =          303
49151
                                          MA   =          303
59651
                                          Ha   =            186
443  n
mi
                                          Hp   =            181
064

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18353459
77                 X    =        -5596896
85
 Y    =       -4063569
06  feet           Y    =        -1301147
82  meter
 Z    =       11500274
17                 Z    =         3478100
67
 XDOT =      12845
104036                 XDOT =        3947
343304
 YDOT =     -15956
731275  feet/sec       YDOT =       -4819
649673  meter/sec
 ZDOT =      14817
070173                 ZDOT =        4535
341454

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18509889
90                 X    =        -5641814
44
 Y    =        3624125
43  feet           Y    =         1104633
43  meter
 Z    =       11395967
52                 Z    =         3473490
90
 XDOT =       5597
200303                 XDOT =        1706
026652
 YDOT =     -18373
771390  feet/sec       YDOT =       -5600
325520  meter/sec
 ZDOT =      14889
649514                 ZDOT =        4538
365172


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   08070
65512836  
00020000  00000-0  20000-3 0  9101
2 25544  51
6371 164
3039 0001838 232
9216 127
1780 15
76123918 12985


Satellite: ISS
Catalog Number: 25544
Epoch time:      08070
65512836   =   yrday
fracday
Element set:     910
Inclination:       51
6371  deg
RA of node:       164
3039  deg
Eccentricity:     
0001838     
Arg of perigee:   232
9216  deg
Mean anomaly:     127
1780  deg
Mean motion:   15
76123918  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1298
Checksum:              288


Coasting Arc #12 (Orbit 1312)
---------------------------------------

Vector Time (GMT): 2008/071/14:22:32
614
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3770524
98                 A    =         6720809
49  meter
 Y    =        4390156
74  meter          E    =           
0003806
 Z    =       -3421732
80                 I    =           51
75858
 XDOT =      -5972
922520                 Wp   =          108
08923
 YDOT =      -1542
247031  meter/sec      RA   =          158
43138  deg
 ZDOT =       4606
042971                 TA   =          211
51839
                                          MA   =          211
54120
                                          Ha   =            186
271  n
mi
                                          Hp   =            180
875

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12370488
78                 X    =        -3802713
98
 Y    =       14403401
37  feet           Y    =         4347812
42  meter
 Z    =      -11226157
47                 Z    =        -3440128
44
 XDOT =     -19596
202492                 XDOT =       -5977
608300
 YDOT =      -5059
865588  feet/sec       YDOT =       -1609
065618  meter/sec
 ZDOT =      15111
689539                 ZDOT =        4577
015188

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5223833
95                 X    =        -1592224
59
 Y    =       18210518
09  feet           Y    =         5550565
91  meter
 Z    =      -11296112
82                 Z    =        -3443055
19
 XDOT =     -18679
548644                 XDOT =       -5693
526427
 YDOT =       3940
305536  feet/sec       YDOT =        1201
005127  meter/sec
 ZDOT =      15000
270146                 ZDOT =        4572
082340


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   08071
60617994  
00020000  00000-0  20000-3 0  9119
2 25544  51
6366 159
4040 0001666 236
6302 123
4703 15
76180814 13132


Satellite: ISS
Catalog Number: 25544
Epoch time:      08071
60617994   =   yrday
fracday
Element set:     911
Inclination:       51
6366  deg
RA of node:       159
4040  deg
Eccentricity:     
0001666     
Arg of perigee:   236
6302  deg
Mean anomaly:     123
4703  deg
Mean motion:   15
76180814  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1313
Checksum:              273

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 may contain past, current and future orbital data 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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