Date: February 17th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3171)
---------------------------------------

Vector Time (GMT): 2007/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5585221
11                 A    =         6716824
59  meter
 Y    =        2741938
20  meter          E    =           
0014461
 Z    =        2551245
53                 I    =           51
68316
 XDOT =      -4222
643134                 Wp   =          173
27438
 YDOT =       3670
911635  meter/sec      RA   =            7
24121  deg
 ZDOT =       5281
862221                 TA   =          215
64256
                                          MA   =          215
73921
                                          Ha   =            187
713  n
mi
                                          Hp   =            174
769

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18324216
25                 X    =         5541752
19
 Y    =        8995860
24  feet           Y    =         2804152
20  meter
 Z    =        8370228
13                 Z    =         2578272
06
 XDOT =     -13853
816056                 XDOT =       -4289
035432
 YDOT =      12043
673344  feet/sec       YDOT =        3623
320449  meter/sec
 ZDOT =      17328
944294                 ZDOT =        5261
188057

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9926865
87                 X    =         3025708
72
 Y    =       17788884
87  feet           Y    =         5422052
11  meter
 Z    =        8472073
57                 Z    =         2582288
02
 XDOT =     -17025
462057                 XDOT =       -5189
360835
 YDOT =       1258
175678  feet/sec       YDOT =         383
491947  meter/sec
 ZDOT =      17251
742750                 ZDOT =        5258
331190


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   07047
55813942  
00020000  00000-0  20000-3 0  9004
2 25544  51
6336   7
4001 0021150 214
3143 145
6658 15
78384820 31729


Satellite: ISS
Catalog Number: 25544
Epoch time:      07047
55813942   =   yrday
fracday
Element set:     900
Inclination:       51
6336  deg
RA of node:         7
4001  deg
Eccentricity:     
0021150     
Arg of perigee:   214
3143  deg
Mean anomaly:     145
6658  deg
Mean motion:   15
78384820  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3172
Checksum:              265


Coasting Arc #2 (Orbit 3186)
---------------------------------------

Vector Time (GMT): 2007/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4864038
25                 A    =         6713837
88  meter
 Y    =       -2770450
44  meter          E    =           
0019083
 Z    =       -3715992
82                 I    =           51
64422
 XDOT =       5317
064345                 Wp   =          202
04535
 YDOT =       3571
278291  meter/sec      RA   =            2
02498  deg
 ZDOT =       4272
743489                 TA   =          113
10156
                                          MA   =          112
90031
                                          Ha   =            187
438  n
mi
                                          Hp   =            175
168

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15958130
75                 X    =         4912707
35
 Y    =       -9089404
33  feet           Y    =        -2715786
03  meter
 Z    =      -12191577
50                 Z    =        -3692245
81
 XDOT =      17444
436829                 XDOT =        5255
979097
 YDOT =      11716
792293  feet/sec       YDOT =        3630
395254  meter/sec
 ZDOT =      14018
187299                 ZDOT =        4298
424460

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18377029
32                 X    =         5601318
54
 Y    =        1312463
23  feet           Y    =          400038
79  meter
 Z    =      -12102727
12                 Z    =        -3688911
23
 XDOT =       8061
042373                 XDOT =        2457
005715
 YDOT =      18035
657176  feet/sec       YDOT =        5497
268307  meter/sec
 ZDOT =      14115
085222                 ZDOT =        4302
277976


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   07048
50784269  
00020000  00000-0  20000-3 0  9010
2 25544  51
6338   2
4903 0020954 218
2779 141
6900 15
78368391 31873


Satellite: ISS
Catalog Number: 25544
Epoch time:      07048
50784269   =   yrday
fracday
Element set:     901
Inclination:       51
6338  deg
RA of node:         2
4903  deg
Eccentricity:     
0020954     
Arg of perigee:   218
2779  deg
Mean anomaly:     141
6900  deg
Mean motion:   15
78368391  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3187
Checksum:              305


Coasting Arc #3 (Orbit 3202)
---------------------------------------

Vector Time (GMT): 2007/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3423273
07                 A    =         6710223
56  meter
 Y    =       -3468491
80  meter          E    =           
0012514
 Z    =       -4603930
19                 I    =           51
60508
 XDOT =       6621
327530                 Wp   =          197
63016
 YDOT =      -2674
214691  meter/sec      RA   =          356
90315  deg
 ZDOT =      -2918
305871                 TA   =           43
55861
                                          MA   =           43
45986
                                          Ha   =            187
000  n
mi
                                          Hp   =            175
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11231210
86                 X    =        -3361869
06
 Y    =      -11379566
27  feet           Y    =        -3506429
69  meter
 Z    =      -15104757
84                 Z    =        -4620410
62
 XDOT =      21723
515517                 XDOT =        6664
915065
 YDOT =      -8773
670247  feet/sec       YDOT =       -2599
927766  meter/sec
 ZDOT =      -9574
494326                 ZDOT =       -2886
034376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3243596
15                 X    =         -988648
11
 Y    =      -15595731
31  feet           Y    =        -4753578
90  meter
 Z    =      -15167088
85                 Z    =        -4622928
68
 XDOT =      21930
728427                 XDOT =        6684
486025
 YDOT =       4601
891419  feet/sec       YDOT =        1402
656504  meter/sec
 ZDOT =      -9453
619395                 ZDOT =       -2881
463191


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   07049
52083616  
00020000  00000-0  20000-3 0  9022
2 25544  51
6347 357
2534 0020921 222
1704 137
7853 15
78430306 32038


Satellite: ISS
Catalog Number: 25544
Epoch time:      07049
52083616   =   yrday
fracday
Element set:     902
Inclination:       51
6347  deg
RA of node:       357
2534  deg
Eccentricity:     
0020921     
Arg of perigee:   222
1704  deg
Mean anomaly:     137
7853  deg
Mean motion:   15
78430306  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3203
Checksum:              272


Coasting Arc #4 (Orbit 3218)
---------------------------------------

Vector Time (GMT): 2007/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6336781
64                 A    =         6719016
87  meter
 Y    =        1856679
06  meter          E    =           
0022363
 Z    =        1163964
13                 I    =           51
60666
 XDOT =      -2360
672294                 Wp   =          188
24592
 YDOT =      -4380
369445  meter/sec      RA   =          351
69867  deg
 ZDOT =      -5900
176237                 TA   =          338
95748
                                          MA   =          339
04935
                                          Ha   =            186
824  n
mi
                                          Hp   =            175
275

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20789966
01                 X    =        -6362726
53
 Y    =        6091466
72  feet           Y    =         1785672
64  meter
 Z    =        3818779
94                 Z    =         1133117
60
 XDOT =      -7744
987842                 XDOT =       -2282
853599
 YDOT =     -14371
290829  feet/sec       YDOT =       -4406
333120  meter/sec
 ZDOT =     -19357
533587                 ZDOT =       -5911
454784

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20909566
24                 X    =        -6373235
79
 Y    =       -5743550
87  feet           Y    =        -1750634
30  meter
 Z    =        3703160
38                 Z    =         1128723
28
 XDOT =        627
715721                 XDOT =         191
327752
 YDOT =     -14715
956598  feet/sec       YDOT =       -4485
423571  meter/sec
 ZDOT =     -19400
442101                 ZDOT =       -5913
254752


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   07050
53380745  
00020000  00000-0  20000-3 0  9039
2 25544  51
6353 352
0171 0020950 225
9584 133
9856 15
78442711 32195


Satellite: ISS
Catalog Number: 25544
Epoch time:      07050
53380745   =   yrday
fracday
Element set:     903
Inclination:       51
6353  deg
RA of node:       352
0171  deg
Eccentricity:     
0020950     
Arg of perigee:   225
9584  deg
Mean anomaly:     133
9856  deg
Mean motion:   15
78442711  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3219
Checksum:              286


Coasting Arc #5 (Orbit 3234)
---------------------------------------

Vector Time (GMT): 2007/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         570884
64                 A    =         6707338
73  meter
 Y    =        4150393
94  meter          E    =           
0018562
 Z    =        5248901
62                 I    =           51
53974
 XDOT =      -7542
580046                 Wp   =          226
71905
 YDOT =       1497
968705  meter/sec      RA   =          346
53266  deg
 ZDOT =       -377
462598                 TA   =          226
79300
                                          MA   =          226
94819
                                          Ha   =            186
397  n
mi
                                          Hp   =            175
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1872981
10                 X    =          498934
12
 Y    =       13616778
01  feet           Y    =         4156375
96  meter
 Z    =       17220805
84                 Z    =         5251499
87
 XDOT =     -24745
997525                 XDOT =       -7556
936354
 YDOT =       4914
595489  feet/sec       YDOT =        1413
543065  meter/sec
 ZDOT =      -1238
394350                 ZDOT =        -414
138805

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5421296
44                 X    =        -1652411
16
 Y    =       12616660
02  feet           Y    =         3845557
97  meter
 Z    =       17231085
01                 Z    =         5252034
71
 XDOT =     -22862
383795                 XDOT =       -6968
454581
 YDOT =      -8004
389088  feet/sec       YDOT =       -2439
737794  meter/sec
 ZDOT =      -1375
948334                 ZDOT =        -419
389052


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   07051
54675409  
00020000  00000-0  20000-3 0  9046
2 25544  51
6354 346
7807 0020978 230
2317 129
7001 15
78510099 32353


Satellite: ISS
Catalog Number: 25544
Epoch time:      07051
54675409   =   yrday
fracday
Element set:     904
Inclination:       51
6354  deg
RA of node:       346
7807  deg
Eccentricity:     
0020978     
Arg of perigee:   230
2317  deg
Mean anomaly:     129
7001  deg
Mean motion:   15
78510099  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3235
Checksum:              291


Coasting Arc #6 (Orbit 3250)
---------------------------------------

Vector Time (GMT): 2007/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6440093
17                 A    =         6717821
01  meter
 Y    =        -647099
29  meter          E    =           
0007762
 Z    =        1817860
19                 I    =           51
54757
 XDOT =      -1082
821273                 Wp   =          210
11875
 YDOT =       5105
542341  meter/sec      RA   =          341
37547  deg
 ZDOT =       5657
303766                 TA   =          170
08003
                                          MA   =          170
06470
                                          Ha   =            186
120  n
mi
                                          Hp   =            175
336

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21128914
60                 X    =         6438019
76
 Y    =       -2123029
17  feet           Y    =         -575094
07  meter
 Z    =        5964108
24                 Z    =         1849140
78
 XDOT =      -3552
563232                 XDOT =       -1167
313526
 YDOT =      16750
466997  feet/sec       YDOT =        5092
961512  meter/sec
 ZDOT =      18560
707894                 ZDOT =        5651
837982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19375561
17                 X    =         5905671
05
 Y    =        8608823
01  feet           Y    =         2623969
25  meter
 Z    =        6081502
10                 Z    =         1853641
84
 XDOT =     -10847
515636                 XDOT =       -3306
322766
 YDOT =      11325
032116  feet/sec       YDOT =        3451
869789  meter/sec
 ZDOT =      18540
820927                 ZDOT =        5651
242219


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   07052
55967923  
00020000  00000-0  20000-3 0  9054
2 25544  51
6351 341
5425 0020944 234
0934 125
8288 15
78528643 32515


Satellite: ISS
Catalog Number: 25544
Epoch time:      07052
55967923   =   yrday
fracday
Element set:     905
Inclination:       51
6351  deg
RA of node:       341
5425  deg
Eccentricity:     
0020944     
Arg of perigee:   234
0934  deg
Mean anomaly:     125
8288  deg
Mean motion:   15
78528643  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3251
Checksum:              301


Coasting Arc #7 (Orbit 3265)
---------------------------------------

Vector Time (GMT): 2007/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2342693
71                 A    =         6711547
68  meter
 Y    =       -4685105
30  meter          E    =           
0017216
 Z    =       -4196525
66                 I    =           51
50008
 XDOT =       6802
058897                 Wp   =          215
25616
 YDOT =        140
695402  meter/sec      RA   =          336
15397  deg
 ZDOT =       3618
935706                 TA   =           91
71711
                                          MA   =           91
51991
                                          Ha   =            185
805  n
mi
                                          Hp   =            175
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7686002
97                 X    =         2415294
87
 Y    =      -15371080
39  feet           Y    =        -4658502
18  meter
 Z    =      -13768128
80                 Z    =        -4184968
49
 XDOT =      22316
466196                 XDOT =        6782
400119
 YDOT =        461
599089  feet/sec       YDOT =         216
650009  meter/sec
 ZDOT =      11873
148643                 ZDOT =        3651
932020

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14193302
12                 X    =         4326118
49
 Y    =       -9750494
16  feet           Y    =        -2971950
62  meter
 Z    =      -13725311
04                 Z    =        -4183474
80
 XDOT =      18580
532056                 XDOT =        5663
346171
 YDOT =      10060
750581  feet/sec       YDOT =        3066
516777  meter/sec
 ZDOT =      11997
083765                 ZDOT =        3656
711132


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   07053
50927507  
00020000  00000-0  20000-3 0  9065
2 25544  51
6354 336
6321 0020915 237
7039 122
2101 15
78571580 32661


Satellite: ISS
Catalog Number: 25544
Epoch time:      07053
50927507   =   yrday
fracday
Element set:     906
Inclination:       51
6354  deg
RA of node:       336
6321  deg
Eccentricity:     
0020915     
Arg of perigee:   237
7039  deg
Mean anomaly:     122
2101  deg
Mean motion:   15
78571580  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3266
Checksum:              278


Coasting Arc #8 (Orbit 3281)
---------------------------------------

Vector Time (GMT): 2007/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5109218
33                 A    =         6711153
58  meter
 Y    =       -1010568
25  meter          E    =           
0012456
 Z    =       -4219264
59                 I    =           51
47425
 XDOT =       4049
211781                 Wp   =          235
99723
 YDOT =      -5504
420263  meter/sec      RA   =          331
02318  deg
 ZDOT =      -3584
272475                 TA   =          357
57643
                                          MA   =          357
58246
                                          Ha   =            185
303  n
mi
                                          Hp   =            175
407

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16762527
33                 X    =        -5077042
08
 Y    =       -3315512
62  feet           Y    =        -1067522
48  meter
 Z    =      -13842731
60                 Z    =        -4244006
75
 XDOT =      13284
815555                 XDOT =        4127
873612
 YDOT =     -18059
121598  feet/sec       YDOT =       -5458
699907  meter/sec
 ZDOT =     -11759
424129                 ZDOT =       -3564
410528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13225930
86                 X    =        -4031263
73
 Y    =      -10698832
04  feet           Y    =        -3261004
01  meter
 Z    =      -13935778
07                 Z    =        -4247625
16
 XDOT =      19439
899636                 XDOT =        5925
281409
 YDOT =      -8807
944478  feet/sec       YDOT =       -2684
661477  meter/sec
 ZDOT =     -11685
516440                 ZDOT =       -3561
745411


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   07054
52215497  
00020000  00000-0  20000-3 0  9077
2 25544  51
6359 331
3948 0020856 241
7542 118
1518 15
78617174 32825


Satellite: ISS
Catalog Number: 25544
Epoch time:      07054
52215497   =   yrday
fracday
Element set:     907
Inclination:       51
6359  deg
RA of node:       331
3948  deg
Eccentricity:     
0020856     
Arg of perigee:   241
7542  deg
Mean anomaly:     118
1518  deg
Mean motion:   15
78617174  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3282
Checksum:              304


Coasting Arc #9 (Orbit 3297)
---------------------------------------

Vector Time (GMT): 2007/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4433616
80                 A    =         6717734
88  meter
 Y    =        4715638
09  meter          E    =           
0015970
 Z    =        1768295
52                 I    =           51
47158
 XDOT =      -4685
738966                 Wp   =          202
46865
 YDOT =      -2286
328845  meter/sec      RA   =          325
79862  deg
 ZDOT =      -5682
685790                 TA   =          317
84450
                                          MA   =          317
96721
                                          Ha   =            185
215  n
mi
                                          Hp   =            175
425

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14545986
88                 X    =        -4494608
17
 Y    =       15471253
58  feet           Y    =         4665717
87  meter
 Z    =        5801494
50                 Z    =         1746609
23
 XDOT =     -15373
159336                 XDOT =       -4632
219572
 YDOT =      -7501
078888  feet/sec       YDOT =       -2338
428064  meter/sec
 ZDOT =     -18643
982250                 ZDOT =       -5705
318839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19980983
31                 X    =        -6090203
71
 Y    =        7255165
16  feet           Y    =         2211374
34  meter
 Z    =        5720633
24                 Z    =         1743649
01
 XDOT =      -9730
739704                 XDOT =       -2965
929462
 YDOT =     -12113
128418  feet/sec       YDOT =       -3692
081542  meter/sec
 ZDOT =     -18729
269300                 ZDOT =       -5708
681283


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   07055
53501268  
00020000  00000-0  20000-3 0  9084
2 25544  51
6357 326
1570 0020917 245
4622 114
4363 15
78619728 32985


Satellite: ISS
Catalog Number: 25544
Epoch time:      07055
53501268   =   yrday
fracday
Element set:     908
Inclination:       51
6357  deg
RA of node:       326
1570  deg
Eccentricity:     
0020917     
Arg of perigee:   245
4622  deg
Mean anomaly:     114
4363  deg
Mean motion:   15
78619728  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3298
Checksum:              301


Coasting Arc #10 (Orbit 3313)
---------------------------------------

Vector Time (GMT): 2007/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2891527
61                 A    =         6706768
57  meter
 Y    =        3042328
26  meter          E    =           
0018978
 Z    =        5246165
59                 I    =           51
41253
 XDOT =      -5807
156018                 Wp   =          245
22175
 YDOT =       5042
668549  meter/sec      RA   =          320
63171  deg
 ZDOT =        269
340307                 TA   =          202
17087
                                          MA   =          202
25304
                                          Ha   =            184
832  n
mi
                                          Hp   =            175
183

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9486639
13                 X    =         2831808
49
 Y    =        9981391
91  feet           Y    =         3074328
90  meter
 Z    =       17211829
35                 Z    =         5260067
39
 XDOT =     -19052
349139                 XDOT =       -5864
420643
 YDOT =      16544
188154  feet/sec       YDOT =        4977
409500  meter/sec
 ZDOT =        883
662426                 ZDOT =         240
990680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4119467
35                 X    =         1255613
65
 Y    =       13070627
66  feet           Y    =         3983927
31  meter
 Z    =       17264421
73                 Z    =         5262195
74
 XDOT =     -23400
241425                 XDOT =       -7132
393586
 YDOT =       6317
123666  feet/sec       YDOT =        1925
459293  meter/sec
 ZDOT =        777
811810                 ZDOT =         237
077040


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   07056
54784526  
00020000  00000-0  20000-3 0  9097
2 25544  51
6358 320
9187 0021017 249
6696 110
2211 15
78699902 33148


Satellite: ISS
Catalog Number: 25544
Epoch time:      07056
54784526   =   yrday
fracday
Element set:     909
Inclination:       51
6358  deg
RA of node:       320
9187  deg
Eccentricity:     
0021017     
Arg of perigee:   249
6696  deg
Mean anomaly:     110
2211  deg
Mean motion:   15
78699902  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3314
Checksum:              307


Coasting Arc #11 (Orbit 3329)
---------------------------------------

Vector Time (GMT): 2007/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5378113
07                 A    =         6718024
33  meter
 Y    =       -3799093
77  meter          E    =           
0007983
 Z    =        1335523
24                 I    =           51
42956
 XDOT =       1867
107101                 Wp   =          277
52027
 YDOT =       4680
088509  meter/sec      RA   =          315
45466  deg
 ZDOT =       5825
108350                 TA   =           97
20841
                                          MA   =           97
11765
                                          Ha   =            184
591  n
mi
                                          Hp   =            175
306

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17644727
92                 X    =         5413707
79
 Y    =      -12464218
41  feet           Y    =        -3738753
72  meter
 Z    =        4381637
93                 Z    =         1361735
89
 XDOT =       6125
679466                 XDOT =        1786
338243
 YDOT =      15354
621094  feet/sec       YDOT =        4700
515822  meter/sec
 ZDOT =      19111
247869                 ZDOT =        5833
982462

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21221567
87                 X    =         6468333
89
 Y    =       -3933189
00  feet           Y    =        -1198836
01  meter
 Z    =        4479620
12                 Z    =         1365388
21
 XDOT =      -1255
981895                 XDOT =        -382
823282
 YDOT =      14916
140106  feet/sec       YDOT =        4546
439504  meter/sec
 ZDOT =      19145
165449                 ZDOT =        5835
446429


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   07057
56065778  
00020000  00000-0  20000-3 0  9103
2 25544  51
6361 315
6799 0020925 253
8307 106
0555 15
78699282 33308


Satellite: ISS
Catalog Number: 25544
Epoch time:      07057
56065778   =   yrday
fracday
Element set:     910
Inclination:       51
6361  deg
RA of node:       315
6799  deg
Eccentricity:     
0020925     
Arg of perigee:   253
8307  deg
Mean anomaly:     106
0555  deg
Mean motion:   15
78699282  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3330
Checksum:              313


Coasting Arc #12 (Orbit 3344)
---------------------------------------

Vector Time (GMT): 2007/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -411172
96                 A    =         6710047
41  meter
 Y    =       -5007539
59  meter          E    =           
0013961
 Z    =       -4441951
78                 I    =           51
38370
 XDOT =       6170
566147                 Wp   =          235
05004
 YDOT =      -3349
388001  meter/sec      RA   =          310
22940  deg
 ZDOT =       3189
724314                 TA   =           66
98711
                                          MA   =           66
83992
                                          Ha   =            184
363  n
mi
                                          Hp   =            175
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1348992
64                 X    =         -333569
76
 Y    =      -16428935
67  feet           Y    =        -5011703
63  meter
 Z    =      -14573332
61                 Z    =        -4443760
75
 XDOT =      20244
639590                 XDOT =        6192
066192
 YDOT =     -10988
805778  feet/sec       YDOT =       -3280
265094  meter/sec
 ZDOT =      10464
974783                 ZDOT =        3219
752311

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5466865
00                 X    =         1666300
45
 Y    =      -15544342
10  feet           Y    =        -4737915
47  meter
 Z    =      -14580759
50                 Z    =        -4444215
50
 XDOT =      21770
130687                 XDOT =        6635
535833
 YDOT =      -2311
216053  feet/sec       YDOT =        -704
458653  meter/sec
 ZDOT =      10577
346350                 ZDOT =        3223
975167


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   07058
51014692  
00020000  00000-0  20000-3 0  9119
2 25544  51
6364 310
7692 0021021 257
5490 102
3324 15
78747508 33455


Satellite: ISS
Catalog Number: 25544
Epoch time:      07058
51014692   =   yrday
fracday
Element set:     911
Inclination:       51
6364  deg
RA of node:       310
7692  deg
Eccentricity:     
0021021     
Arg of perigee:   257
5490  deg
Mean anomaly:     102
3324  deg
Mean motion:   15
78747508  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3345
Checksum:              276

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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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