Date: July 28th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 2690 98 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 1715)
---------------------------------------

Vector Time (GMT): 2007/208/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4095696
27                 A    =         6714568
69  meter
 Y    =        -928572
89  meter          E    =           
0009435
 Z    =        5235593
51                 I    =           51
30243
 XDOT =       1933
134913                 Wp   =          156
08589
 YDOT =       7458
968440  meter/sec      RA   =          254
29243  deg
 ZDOT =       -197
739693                 TA   =          295
74912
                                          MA   =          295
84648
                                          Ha   =            189
247  n
mi
                                          Hp   =            179
490

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13437323
73                 X    =         4080342
12
 Y    =       -3046498
97  feet           Y    =         -882859
25  meter
 Z    =       17177144
08                 Z    =         5255452
66
 XDOT =       6342
306146                 XDOT =        1850
544523
 YDOT =      24471
681232  feet/sec       YDOT =        7480
124089  meter/sec
 ZDOT =       -648
752275                 ZDOT =        -188
547998

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13322385
28                 X    =        -4060663
03
 Y    =       -3126067
76  feet           Y    =         -952825
45  meter
 Z    =       17252213
03                 Z    =         5258474
53
 XDOT =       4826
017195                 XDOT =        1470
970041
 YDOT =     -23799
272928  feet/sec       YDOT =       -7254
018389  meter/sec
 ZDOT =       -613
087811                 ZDOT =        -186
869165


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   07208
63003017  
00020000  00000-0  20000-3 0  9006
2 25544  51
6322 254
8574 0009105 171
0255 189
1073 15
75945050 17167


Satellite: ISS
Catalog Number: 25544
Epoch time:      07208
63003017   =   yrday
fracday
Element set:     900
Inclination:       51
6322  deg
RA of node:       254
8574  deg
Eccentricity:     
0009105     
Arg of perigee:   171
0255  deg
Mean anomaly:     189
1073  deg
Mean motion:   15
75945050  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1716
Checksum:              265


Coasting Arc #2 (Orbit 1731)
---------------------------------------

Vector Time (GMT): 2007/209/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1747163
54                 A    =         6726280
77  meter
 Y    =       -6441798
95  meter          E    =           
0011724
 Z    =         828299
49                 I    =           51
35125
 XDOT =       4871
328463                 Wp   =           95
12961
 YDOT =       -548
518726  meter/sec      RA   =          249
12975  deg
 ZDOT =       5936
260556                 TA   =          273
94320
                                          MA   =          274
07722
                                          Ha   =            189
187  n
mi
                                          Hp   =            179
667

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5732163
84                 X    =        -1679024
19
 Y    =      -21134510
98  feet           Y    =        -6460955
86  meter
 Z    =        2717518
02                 Z    =          819976
42
 XDOT =      15982
048763                 XDOT =        4848
263320
 YDOT =      -1799
602119  feet/sec       YDOT =        -494
174698  meter/sec
 ZDOT =      19475
920458                 ZDOT =        5959
868901

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3754465
44                 X    =        -1144361
07
 Y    =       21577849
54  feet           Y    =         6576928
54  meter
 Z    =        2685248
46                 Z    =          818463
73
 XDOT =     -13565
115147                 XDOT =       -4134
647097
 YDOT =      -4825
277872  feet/sec       YDOT =       -1470
744695  meter/sec
 ZDOT =      19565
235113                 ZDOT =        5963
483662


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   07209
64460674  
00020000  00000-0  20000-3 0  9015
2 25544  51
6321 249
6317 0009082 175
4582 184
6666 15
75972941 17323


Satellite: ISS
Catalog Number: 25544
Epoch time:      07209
64460674   =   yrday
fracday
Element set:     901
Inclination:       51
6321  deg
RA of node:       249
6317  deg
Eccentricity:     
0009082     
Arg of perigee:   175
4582  deg
Mean anomaly:     184
6666  deg
Mean motion:   15
75972941  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1732
Checksum:              310


Coasting Arc #3 (Orbit 1746)
---------------------------------------

Vector Time (GMT): 2007/210/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4462244
79                 A    =         6715554
49  meter
 Y    =          45670
24  meter          E    =           
0017885
 Z    =       -5032952
82                 I    =           51
32557
 XDOT =      -2010
879524                 Wp   =          132
09413
 YDOT =      -7224
820512  meter/sec      RA   =          243
93456  deg
 ZDOT =       1709
365972                 TA   =          154
48829
                                          MA   =          154
39991
                                          Ha   =            189
047  n
mi
                                          Hp   =            179
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14639910
74                 X    =        -4437975
24
 Y    =         149836
75  feet           Y    =           -4092
70  meter
 Z    =      -16512312
40                 Z    =        -5054570
95
 XDOT =      -6597
373768                 XDOT =       -1938
244661
 YDOT =     -23703
479370  feet/sec       YDOT =       -7246
901411  meter/sec
 ZDOT =       5608
156075                 ZDOT =        1699
772777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13340484
22                 X    =         4066179
59
 Y    =        5802692
44  feet           Y    =         1768660
66  meter
 Z    =      -16594159
80                 Z    =        -5057899
91
 XDOT =      -3203
917675                 XDOT =        -976
554107
 YDOT =      23371
404045  feet/sec       YDOT =        7123
603953  meter/sec
 ZDOT =       5570
970262                 ZDOT =        1698
031736


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   07210
59576731  
00020000  00000-0  20000-3 0  9024
2 25544  51
6314 244
7316 0008941 179
3776 180
7400 15
75936680 17470


Satellite: ISS
Catalog Number: 25544
Epoch time:      07210
59576731   =   yrday
fracday
Element set:     902
Inclination:       51
6314  deg
RA of node:       244
7316  deg
Eccentricity:     
0008941     
Arg of perigee:   179
3776  deg
Mean anomaly:     180
7400  deg
Mean motion:   15
75936680  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1747
Checksum:              306


Coasting Arc #4 (Orbit 1762)
---------------------------------------

Vector Time (GMT): 2007/211/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1723008
20                 A    =         6724653
09  meter
 Y    =        6132612
20  meter          E    =           
0014227
 Z    =       -2131570
04                 I    =           51
36896
 XDOT =      -5381
110196                 Wp   =          164
73190
 YDOT =       -393
624597  meter/sec      RA   =          238
79587  deg
 ZDOT =      -5504
008887                 TA   =           39
23541
                                          MA   =           39
13238
                                          Ha   =            188
927  n
mi
                                          Hp   =            180
088

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5652914
04                 X    =         1664658
89
 Y    =       20120118
76  feet           Y    =         6151553
83  meter
 Z    =       -6993340
02                 Z    =        -2123340
93
 XDOT =     -17654
561012                 XDOT =       -5349
571878
 YDOT =      -1291
419283  feet/sec       YDOT =        -453
622258  meter/sec
 ZDOT =     -18057
771940                 ZDOT =       -5530
073116

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2662669
85                 X    =          811581
77
 Y    =      -20739576
25  feet           Y    =        -6321422
84  meter
 Z    =       -6961435
72                 Z    =        -2121845
61
 XDOT =      14124
896108                 XDOT =        4305
268334
 YDOT =       7883
692249  feet/sec       YDOT =        2402
949397  meter/sec
 ZDOT =     -18156
515489                 ZDOT =       -5534
105921


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   07211
61033132  
00020000  00000-0  20000-3 0  9032
2 25544  51
6301 239
5045 0008932 182
6970 177
4147 15
75955881 17633


Satellite: ISS
Catalog Number: 25544
Epoch time:      07211
61033132   =   yrday
fracday
Element set:     903
Inclination:       51
6301  deg
RA of node:       239
5045  deg
Eccentricity:     
0008932     
Arg of perigee:   182
6970  deg
Mean anomaly:     177
4147  deg
Mean motion:   15
75955881  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1763
Checksum:              287


Coasting Arc #5 (Orbit 1778)
---------------------------------------

Vector Time (GMT): 2007/212/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4948748
46                 A    =         6717629
78  meter
 Y    =         669504
78  meter          E    =           
0008670
 Z    =        4484465
34                 I    =           51
36130
 XDOT =       1907
923011                 Wp   =          127
32726
 YDOT =       6787
160369  meter/sec      RA   =          233
58258  deg
 ZDOT =      -3119
804267                 TA   =          353
87012
                                          MA   =          353
88072
                                          Ha   =            188
576  n
mi
                                          Hp   =            180
301

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16236051
38                 X    =         4919109
95
 Y    =        2196537
99  feet           Y    =          724678
40  meter
 Z    =       14712812
80                 Z    =         4508433
86
 XDOT =       6259
589932                 XDOT =        1847
041268
 YDOT =      22267
586512  feet/sec       YDOT =        6808
155680  meter/sec
 ZDOT =     -10235
578303                 ZDOT =       -3110
683131

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14136319
64                 X    =        -4308750
23
 Y    =       -8118932
69  feet           Y    =        -2474650
69  meter
 Z    =       14803661
81                 Z    =         4512156
12
 XDOT =       1943
513034                 XDOT =         592
382773
 YDOT =     -21976
157304  feet/sec       YDOT =       -6698
332746  meter/sec
 ZDOT =     -10200
202256                 ZDOT =       -3109
021648


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   07212
62488722  
00020000  00000-0  20000-3 0  9044
2 25544  51
6296 234
2777 0008790 187
4425 172
6610 15
75988159 17793


Satellite: ISS
Catalog Number: 25544
Epoch time:      07212
62488722   =   yrday
fracday
Element set:     904
Inclination:       51
6296  deg
RA of node:       234
2777  deg
Eccentricity:     
0008790     
Arg of perigee:   187
4425  deg
Mean anomaly:     172
6610  deg
Mean motion:   15
75988159  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1779
Checksum:              329


Coasting Arc #6 (Orbit 1794)
---------------------------------------

Vector Time (GMT): 2007/213/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1533293
03                 A    =         6721801
28  meter
 Y    =       -5668601
19  meter          E    =           
0013740
 Z    =        3270339
97                 I    =           51
39361
 XDOT =       5996
399857                 Wp   =          126
98853
 YDOT =       1104
425527  meter/sec      RA   =          228
46172  deg
 ZDOT =       4704
003947                 TA   =          271
51908
                                          MA   =          271
67647
                                          Ha   =            188
540  n
mi
                                          Hp   =            180
468

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5030488
96                 X    =        -1485678
34
 Y    =      -18597772
94  feet           Y    =        -5685481
29  meter
 Z    =       10729461
86                 Z    =         3263006
73
 XDOT =      19673
227877                 XDOT =        5960
753601
 YDOT =       3623
443331  feet/sec       YDOT =        1171
281081  meter/sec
 ZDOT =      15433
083815                 ZDOT =        4733
047355

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1959627
24                 X    =         -597294
38
 Y    =       19182104
59  feet           Y    =         5846705
48  meter
 Z    =       10700983
78                 Z    =         3261659
86
 XDOT =     -15562
486618                 XDOT =       -4743
445921
 YDOT =     -10300
724863  feet/sec       YDOT =       -3139
660938  meter/sec
 ZDOT =      15543
212152                 ZDOT =        4737
571064


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   07213
63943584  
00020000  00000-0  20000-3 0  9059
2 25544  51
6296 229
0512 0008866 191
8908 168
2048 15
76022843 17955


Satellite: ISS
Catalog Number: 25544
Epoch time:      07213
63943584   =   yrday
fracday
Element set:     905
Inclination:       51
6296  deg
RA of node:       229
0512  deg
Eccentricity:     
0008866     
Arg of perigee:   191
8908  deg
Mean anomaly:     168
2048  deg
Mean motion:   15
76022843  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1795
Checksum:              316


Coasting Arc #7 (Orbit 1809)
---------------------------------------

Vector Time (GMT): 2007/214/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5524618
11                 A    =         6720671
06  meter
 Y    =       -1203281
70  meter          E    =           
0010061
 Z    =       -3644313
04                 I    =           51
40978
 XDOT =      -1517
606455                 Wp   =          160
37017
 YDOT =      -6174
143179  meter/sec      RA   =          223
24125  deg
 ZDOT =       4333
333750                 TA   =          155
75263
                                          MA   =          155
70525
                                          Ha   =            188
410  n
mi
                                          Hp   =            180
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18125387
50                 X    =        -5493049
08
 Y    =       -3947774
59  feet           Y    =        -1264884
43  meter
 Z    =      -11956407
62                 Z    =        -3671074
61
 XDOT =      -4979
023803                 XDOT =       -1469
503726
 YDOT =     -20256
375259  feet/sec       YDOT =       -6190
845127  meter/sec
 ZDOT =      14216
974244                 ZDOT =        4326
077917

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15591919
57                 X    =         4752417
09
 Y    =        9928195
62  feet           Y    =         3026114
02  meter
 Z    =      -12057912
56                 Z    =        -3675251
75
 XDOT =      -1506
860138                 XDOT =        -459
290970
 YDOT =      19622
051540  feet/sec       YDOT =        5980
801309  meter/sec
 ZDOT =      14188
718234                 ZDOT =        4324
721318


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   07214
59057094  
00020000  00000-0  20000-3 0  9068
2 25544  51
6296 224
1505 0008630 194
7852 165
3061 15
75979715 18101


Satellite: ISS
Catalog Number: 25544
Epoch time:      07214
59057094   =   yrday
fracday
Element set:     906
Inclination:       51
6296  deg
RA of node:       224
1505  deg
Eccentricity:     
0008630     
Arg of perigee:   194
7852  deg
Mean anomaly:     165
3061  deg
Mean motion:   15
75979715  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1810
Checksum:              301


Coasting Arc #8 (Orbit 1825)
---------------------------------------

Vector Time (GMT): 2007/215/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1045631
07                 A    =         6718682
06  meter
 Y    =        5112366
32  meter          E    =           
0007284
 Z    =       -4233131
56                 I    =           51
42545
 XDOT =      -6636
999130                 Wp   =          136
35618
 YDOT =      -1590
358609  meter/sec      RA   =          218
12479  deg
 ZDOT =      -3568
926861                 TA   =           97
33427
                                          MA   =           97
25149
                                          Ha   =            188
220  n
mi
                                          Hp   =            180
913

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3430548
14                 X    =         1008949
73
 Y    =       16772855
37  feet           Y    =         5123854
22  meter
 Z    =      -13888226
91                 Z    =        -4228140
83
 XDOT =     -21774
931528                 XDOT =       -6601
385183
 YDOT =      -5217
711973  feet/sec       YDOT =       -1664
378003  meter/sec
 ZDOT =     -11709
077628                 ZDOT =       -3601
082674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2193867
84                 X    =          668690
92
 Y    =      -16994907
09  feet           Y    =        -5180047
68  meter
 Z    =      -13868679
15                 Z    =        -4227173
41
 XDOT =      17552
522094                 XDOT =        5350
008734
 YDOT =      11896
901649  feet/sec       YDOT =        3626
175623  meter/sec
 ZDOT =     -11831
067002                 ZDOT =       -3606
109222


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   07215
60510708  
00020000  00000-0  20000-3 0  9078
2 25544  51
6300 218
9231 0008612 198
8340 161
2506 15
76005789 18269


Satellite: ISS
Catalog Number: 25544
Epoch time:      07215
60510708   =   yrday
fracday
Element set:     907
Inclination:       51
6300  deg
RA of node:       218
9231  deg
Eccentricity:     
0008612     
Arg of perigee:   198
8340  deg
Mean anomaly:     161
2506  deg
Mean motion:   15
76005789  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1826
Checksum:              279


Coasting Arc #9 (Orbit 1841)
---------------------------------------

Vector Time (GMT): 2007/216/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6033057
31                 A    =         6723537
39  meter
 Y    =        1499515
82  meter          E    =           
0014867
 Z    =        2535509
09                 I    =           51
46584
 XDOT =        841
730946                 Wp   =          138
00703
 YDOT =       5554
915166  meter/sec      RA   =          212
91291  deg
 ZDOT =      -5281
165177                 TA   =           13
12519
                                          MA   =           13
08654
                                          Ha   =            187
897  n
mi
                                          Hp   =            181
132

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19793495
13                 X    =         6003524
13
 Y    =        4919671
34  feet           Y    =         1566815
60  meter
 Z    =        8318599
37                 Z    =         2564745
90
 XDOT =       2761
584470                 XDOT =         805
207338
 YDOT =      18224
787291  feet/sec       YDOT =        5564
123948  meter/sec
 ZDOT =     -17326
657406                 ZDOT =       -5277
164481

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17225047
80                 X    =        -5250194
57
 Y    =      -10836304
61  feet           Y    =        -3302905
65  meter
 Z    =        8429527
95                 Z    =         2569320
12
 XDOT =       2181
344544                 XDOT =         664
873817
 YDOT =     -16950
751364  feet/sec       YDOT =       -5166
589016  meter/sec
 ZDOT =     -17310
802106                 ZDOT =       -5276
332482


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   07216
61963555  
00020000  00000-0  20000-3 0  9083
2 25544  51
6301 213
6967 0008522 203
7153 156
3619 15
76027463 18427


Satellite: ISS
Catalog Number: 25544
Epoch time:      07216
61963555   =   yrday
fracday
Element set:     908
Inclination:       51
6301  deg
RA of node:       213
6967  deg
Eccentricity:     
0008522     
Arg of perigee:   203
7153  deg
Mean anomaly:     156
3619  deg
Mean motion:   15
76027463  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1842
Checksum:              292


Coasting Arc #10 (Orbit 1857)
---------------------------------------

Vector Time (GMT): 2007/217/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -355235
86                 A    =         6715899
05  meter
 Y    =       -4590776
94  meter          E    =           
0011195
 Z    =        4891503
38                 I    =           51
46570
 XDOT =       7160
265942                 Wp   =          172
92032
 YDOT =       1797
278883  meter/sec      RA   =          207
79010  deg
 ZDOT =       2195
308394                 TA   =          255
64774
                                          MA   =          255
77205
                                          Ha   =            187
810  n
mi
                                          Hp   =            181
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1165471
97                 X    =         -327636
70
 Y    =      -15061604
12  feet           Y    =        -4594595
45  meter
 Z    =       16048239
42                 Z    =         4889844
32
 XDOT =      23491
686162                 XDOT =        7128
971950
 YDOT =       5896
584261  feet/sec       YDOT =        1877
173862  meter/sec
 ZDOT =       7202
455360                 ZDOT =        2230
017023

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3254175
54                 X    =         -991872
70
 Y    =       14759431
81  feet           Y    =         4498674
82  meter
 Z    =       16041376
07                 Z    =         4889411
43
 XDOT =     -19582
514308                 XDOT =       -5968
750361
 YDOT =     -12329
681263  feet/sec       YDOT =       -3758
086849  meter/sec
 ZDOT =       7334
156293                 ZDOT =        2235
450838


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   07217
63415604  
00020000  00000-0  20000-3 0  9094
2 25544  51
6306 208
4706 0008611 208
3445 151
7252 15
76062043 18581


Satellite: ISS
Catalog Number: 25544
Epoch time:      07217
63415604   =   yrday
fracday
Element set:     909
Inclination:       51
6306  deg
RA of node:       208
4706  deg
Eccentricity:     
0008611     
Arg of perigee:   208
3445  deg
Mean anomaly:     151
7252  deg
Mean motion:   15
76062043  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1858
Checksum:              277


Coasting Arc #11 (Orbit 1872)
---------------------------------------

Vector Time (GMT): 2007/218/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6413721
49                 A    =         6725625
04  meter
 Y    =       -1592895
29  meter          E    =           
0001062
 Z    =       -1250656
02                 I    =           51
52431
 XDOT =        100
469884                 Wp   =           96
01845
 YDOT =      -4997
814156  meter/sec      RA   =          202
59793  deg
 ZDOT =       5854
354589                 TA   =          250
24138
                                          MA   =          250
25283
                                          Ha   =            187
663  n
mi
                                          Hp   =            181
494

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21042393
34                 X    =        -6389357
38
 Y    =       -5226034
41  feet           Y    =        -1664480
77  meter
 Z    =       -4103202
18                 Z    =        -1281754
79
 XDOT =        329
625603                 XDOT =         127
909402
 YDOT =     -16397
028070  feet/sec       YDOT =       -4996
537845  meter/sec
 ZDOT =      19207
200096                 ZDOT =        5854
908790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18723966
47                 X    =         5707064
98
 Y    =       10886893
49  feet           Y    =         3318325
14  meter
 Z    =       -4221214
41                 Z    =        -1286626
15
 XDOT =      -3997
386095                 XDOT =       -1218
403282
 YDOT =      14317
687498  feet/sec       YDOT =        4364
031149  meter/sec
 ZDOT =      19208
671181                 ZDOT =        5854
802976


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   07218
58526386  
00020000  00000-0  20000-3 0  9101
2 25544  51
6302 203
5701 0008499 211
2076 148
8585 15
76048301 18739


Satellite: ISS
Catalog Number: 25544
Epoch time:      07218
58526386   =   yrday
fracday
Element set:     910
Inclination:       51
6302  deg
RA of node:       203
5701  deg
Eccentricity:     
0008499     
Arg of perigee:   211
2076  deg
Mean anomaly:     148
8585  deg
Mean motion:   15
76048301  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1873
Checksum:              292


Coasting Arc #12 (Orbit 1888)
---------------------------------------

Vector Time (GMT): 2007/219/13:59:11
277
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -578084
35                 A    =         6714407
73  meter
 Y    =        4178470
31  meter          E    =           
0011241
 Z    =       -5231796
64                 I    =           51
51410
 XDOT =      -7453
719774                 Wp   =          119
79188
 YDOT =      -1816
000013  meter/sec      RA   =          197
45556  deg
 ZDOT =       -633
293402                 TA   =          144
21284
                                          MA   =          144
13746
                                          Ha   =            187
431  n
mi
                                          Hp   =            181
771

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1896602
21                 X    =         -599350
70
 Y    =       13708892
08  feet           Y    =         4171887
60  meter
 Z    =      -17164687
15                 Z    =        -5234656
08
 XDOT =     -24454
461200                 XDOT =       -7429
782612
 YDOT =      -5958
005293  feet/sec       YDOT =       -1899
217783  meter/sec
 ZDOT =      -2077
734259                 ZDOT =        -669
445435

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5337735
01                 X    =         1626941
63
 Y    =      -12754817
84  feet           Y    =        -3887668
48  meter
 Z    =      -17174996
76                 Z    =        -5234939
01
 XDOT =      21089
298791                 XDOT =        6428
018271
 YDOT =      11779
406223  feet/sec       YDOT =        3590
363017  meter/sec
 ZDOT =      -2214
933991                 ZDOT =        -675
111881


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   07219
59977057  
00020000  00000-0  20000-3 0  9119
2 25544  51
6308 198
3430 0008482 216
0003 144
0591 15
76052097 18899


Satellite: ISS
Catalog Number: 25544
Epoch time:      07219
59977057   =   yrday
fracday
Element set:     911
Inclination:       51
6308  deg
RA of node:       198
3430  deg
Eccentricity:     
0008482     
Arg of perigee:   216
0003  deg
Mean anomaly:     144
0591  deg
Mean motion:   15
76052097  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1889
Checksum:              300

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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