Date: June 17th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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


171/06:52:31 233 9 6 11 3 11 4
N/A -3 1 0 1 186 8
000/00:19:02 466 -5 1 0 2 186 2

Coasting Arc #1 (Orbit 2841)
---------------------------------------

Vector Time (GMT): 2008/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1494715
34                 A    =         6713854
08  meter
 Y    =       -4507150
27  meter          E    =           
0012509
 Z    =       -4757185
98                 I    =           51
73507
 XDOT =       7229
688977                 Wp   =           40
97885
 YDOT =        366
682718  meter/sec      RA   =           19
44898  deg
 ZDOT =      -2613
588693                 TA   =          203
36568
                                          MA   =          203
42257
                                          Ha   =            185
900  n
mi
                                          Hp   =            179
870

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4903921
70                 X    =        -1421094
83
 Y    =      -14787238
42  feet           Y    =        -4523452
45  meter
 Z    =      -15607565
57                 Z    =        -4764269
45
 XDOT =      23719
452025                 XDOT =        7237
747793
 YDOT =       1203
027290  feet/sec       YDOT =         447
574819  meter/sec
 ZDOT =      -8574
766052                 ZDOT =       -2578
446905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15187984
57                 X    =        -4629297
70
 Y    =        3342626
26  feet           Y    =         1018832
48  meter
 Z    =      -15635182
94                 Z    =        -4765603
76
 XDOT =       3770
079512                 XDOT =        1149
120235
 YDOT =     -22428
130892  feet/sec       YDOT =       -6836
094296  meter/sec
 ZDOT =      -8439
441069                 ZDOT =       -2572
341638


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   08168
52029744  
00020000  00000-0  20000-3 0  9005
2 25544  51
6396  19
8295 0006367 334
5059  25
5791 15
76967779 28426


Satellite: ISS
Catalog Number: 25544
Epoch time:      08168
52029744   =   yrday
fracday
Element set:     900
Inclination:       51
6396  deg
RA of node:        19
8295  deg
Eccentricity:     
0006367     
Arg of perigee:   334
5059  deg
Mean anomaly:      25
5791  deg
Mean motion:   15
76967779  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2842
Checksum:              333


Coasting Arc #2 (Orbit 2857)
---------------------------------------

Vector Time (GMT): 2008/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6561945
65                 A    =         6722878
22  meter
 Y    =        -588783
33  meter          E    =           
0009724
 Z    =        1326628
59                 I    =           51
73821
 XDOT =       -746
011833                 Wp   =           96
28651
 YDOT =      -4952
152092  meter/sec      RA   =           14
26493  deg
 ZDOT =      -5852
433847                 TA   =           69
15294
                                          MA   =           69
04883
                                          Ha   =            186
004  n
mi
                                          Hp   =            179
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21528693
08                 X    =        -6561318
64
 Y    =       -1931703
84  feet           Y    =         -662159
54  meter
 Z    =        4352456
00                 Z    =         1294751
87
 XDOT =      -2447
545385                 XDOT =        -662
150425
 YDOT =     -16247
218149  feet/sec       YDOT =       -4960
024292  meter/sec
 ZDOT =     -19200
898447                 ZDOT =       -5855
855340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3668185
23                 X    =        -1118062
86
 Y    =       21326373
33  feet           Y    =         6500278
59  meter
 Z    =        4229680
39                 Z    =         1289206
58
 XDOT =     -14828
036145                 XDOT =       -4519
585417
 YDOT =       1284
099747  feet/sec       YDOT =         391
393603  meter/sec
 ZDOT =     -19214
447598                 ZDOT =       -5856
563628


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   08169
53420817  
00020000  00000-0  20000-3 0  9014
2 25544  51
6401  14
5995 0006469 338
8758  21
2139 15
77018311 28584


Satellite: ISS
Catalog Number: 25544
Epoch time:      08169
53420817   =   yrday
fracday
Element set:     901
Inclination:       51
6401  deg
RA of node:        14
5995  deg
Eccentricity:     
0006469     
Arg of perigee:   338
8758  deg
Mean anomaly:      21
2139  deg
Mean motion:   15
77018311  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2858
Checksum:              300


Coasting Arc #3 (Orbit 2873)
---------------------------------------

Vector Time (GMT): 2008/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -250131
36                 A    =         6711624
82  meter
 Y    =        4167277
15  meter          E    =           
0005401
 Z    =        5254511
16                 I    =           51
67020
 XDOT =      -7641
958196                 Wp   =            5
00921
 YDOT =       -926
357275  meter/sec      RA   =            9
12569  deg
 ZDOT =        376
155996                 TA   =           81
45430
                                          MA   =           81
39311
                                          Ha   =            186
159  n
mi
                                          Hp   =            179
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -820640
96                 X    =         -322237
42
 Y    =       13672169
13  feet           Y    =         4164075
73  meter
 Z    =       17239209
85                 Z    =         5253121
78
 XDOT =     -25072
041326                 XDOT =       -7632
858855
 YDOT =      -3039
229904  feet/sec       YDOT =       -1011
763231  meter/sec
 ZDOT =       1234
107597                 ZDOT =         339
053198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13585956
19                 X    =         4140999
45
 Y    =        1788026
74  feet           Y    =          544990
55  meter
 Z    =       17234174
52                 Z    =         5252976
39
 XDOT =      -4500
302297                 XDOT =       -1371
692140
 YDOT =      23843
411269  feet/sec       YDOT =        7267
471755  meter/sec
 ZDOT =       1091
179133                 ZDOT =         332
591400


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   08170
54810481  
00020000  00000-0  20000-3 0  9028
2 25544  51
6391   9
3682 0006351 342
5070  17
5875 15
76989413 28748


Satellite: ISS
Catalog Number: 25544
Epoch time:      08170
54810481   =   yrday
fracday
Element set:     902
Inclination:       51
6391  deg
RA of node:         9
3682  deg
Eccentricity:     
0006351     
Arg of perigee:   342
5070  deg
Mean anomaly:      17
5875  deg
Mean motion:   15
76989413  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2874
Checksum:              298


Coasting Arc #4 (Orbit 2885)
---------------------------------------

Vector Time (GMT): 2008/171/07:02:02
466
Vector Time (MET): N/A
Weight (LBS)     : 661038
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         592665
98                 A    =         6718465
15  meter
 Y    =       -4132509
24  meter          E    =           
0005618
 Z    =       -5268729
42                 I    =           51
64927
 XDOT =       7649
903609                 Wp   =           88
16827
 YDOT =        836
463568  meter/sec      RA   =            5
03357  deg
 ZDOT =        204
804353                 TA   =          183
77368
                                          MA   =          183
77792
                                          Ha   =            186
838  n
mi
                                          Hp   =            186
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1944442
19                 X    =          664426
78
 Y    =      -13558101
20  feet           Y    =        -4125479
33  meter
 Z    =      -17285857
68                 Z    =        -5265676
85
 XDOT =      25098
108954                 XDOT =        7638
986683
 YDOT =       2744
303045  feet/sec       YDOT =         921
948085  meter/sec
 ZDOT =        671
930291                 ZDOT =         241
941191

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -973289
49                 X    =         -296658
64
 Y    =      -13676663
91  feet           Y    =        -4168647
16  meter
 Z    =      -17274414
93                 Z    =        -5265241
67
 XDOT =      24088
932026                 XDOT =        7342
306482
 YDOT =      -2742
140976  feet/sec       YDOT =        -835
804569  meter/sec
 ZDOT =        814
988173                 ZDOT =         248
408395


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   08171
30853553  
00020000  00000-0  20000-3 0  9031
2 25544  51
6413   5
4475 0009429 273
9651  86
0434 15
74579497 28861


Satellite: ISS
Catalog Number: 25544
Epoch time:      08171
30853553   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:         5
4475  deg
Eccentricity:     
0009429     
Arg of perigee:   273
9651  deg
Mean anomaly:      86
0434  deg
Mean motion:   15
74579497  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2886
Checksum:              314


Coasting Arc #5 (Orbit 2901)
---------------------------------------

Vector Time (GMT): 2008/172/07:02:02
466
Vector Time (MET): N/A
Weight (LBS)     : 661038
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6707618
13                 A    =         6730495
12  meter
 Y    =        -297047
57  meter          E    =           
0007493
 Z    =        -390297
42                 I    =           51
66064
 XDOT =        562
533306                 Wp   =          194
14006
 YDOT =      -4765
120317  meter/sec      RA   =          359
90069  deg
 ZDOT =      -6023
932497                 TA   =          350
10300
                                          MA   =          350
11775
                                          Ha   =            187
370  n
mi
                                          Hp   =            186
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22006621
17                 X    =        -6701901
99
 Y    =        -974565
51  feet           Y    =         -372023
95  meter
 Z    =       -1280503
35                 Z    =         -422869
03
 XDOT =       1845
581713                 XDOT =         645
038827
 YDOT =     -15633
596841  feet/sec       YDOT =       -4758
367157  meter/sec
 ZDOT =     -19763
558062                 ZDOT =       -6021
000332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21609446
83                 X    =        -6586559
39
 Y    =        4235086
86  feet           Y    =         1290854
48  meter
 Z    =       -1405947
77                 Z    =         -428532
88
 XDOT =      -1470
835989                 XDOT =        -448
310810
 YDOT =     -14079
254291  feet/sec       YDOT =       -4291
356708  meter/sec
 ZDOT =     -19752
626888                 ZDOT =       -6020
600675


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   08172
32399557  
00020000  00000-0  20000-3 0  9044
2 25544  51
6415    
2281 0009499 277
4183  82
5901 15
74563747 29027


Satellite: ISS
Catalog Number: 25544
Epoch time:      08172
32399557   =   yrday
fracday
Element set:     904
Inclination:       51
6415  deg
RA of node:          
2281  deg
Eccentricity:     
0009499     
Arg of perigee:   277
4183  deg
Mean anomaly:      82
5901  deg
Mean motion:   15
74563747  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2902
Checksum:              303


Coasting Arc #6 (Orbit 2917)
---------------------------------------

Vector Time (GMT): 2008/173/07:02:02
466
Vector Time (MET): N/A
Weight (LBS)     : 661038
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -396874
83                 A    =         6718445
40  meter
 Y    =        4202648
97  meter          E    =           
0007565
 Z    =        5232757
14                 I    =           51
59152
 XDOT =      -7663
940183                 Wp   =          297
10671
 YDOT =        148
594809  meter/sec      RA   =          354
74925  deg
 ZDOT =       -697
993730                 TA   =          159
55392
                                          MA   =          159
52363
                                          Ha   =            187
700  n
mi
                                          Hp   =            186
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1302082
78                 X    =         -469259
58
 Y    =       13788218
42  feet           Y    =         4197805
13  meter
 Z    =       17167838
38                 Z    =         5230654
15
 XDOT =     -25144
160704                 XDOT =       -7661
641496
 YDOT =        487
515777  feet/sec       YDOT =          62
905232  meter/sec
 ZDOT =      -2290
005677                 ZDOT =        -735
219223

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2123415
58                 X    =          647217
07
 Y    =       13695565
77  feet           Y    =         4174408
45  meter
 Z    =       17160059
61                 Z    =         5230386
17
 XDOT =     -23196
354482                 XDOT =       -7070
248846
 YDOT =       6656
103215  feet/sec       YDOT =        2028
780260  meter/sec
 ZDOT =      -2433
341986                 ZDOT =        -741
682637


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   08173
33944023  
00020000  00000-0  20000-3 0  9051
2 25544  51
6416 355
0084 0009658 282
2435  77
7647 15
74645836 29181


Satellite: ISS
Catalog Number: 25544
Epoch time:      08173
33944023   =   yrday
fracday
Element set:     905
Inclination:       51
6416  deg
RA of node:       355
0084  deg
Eccentricity:     
0009658     
Arg of perigee:   282
2435  deg
Mean anomaly:      77
7647  deg
Mean motion:   15
74645836  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2918
Checksum:              314


Coasting Arc #7 (Orbit 2933)
---------------------------------------

Vector Time (GMT): 2008/174/07:02:02
466
Vector Time (MET): N/A
Weight (LBS)     : 661038
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6648500
55                 A    =         6730077
33  meter
 Y    =        -546290
62  meter          E    =           
0010855
 Z    =         833468
68                 I    =           51
60198
 XDOT =       -347
463230                 Wp   =            9
09428
 YDOT =       4867
276632  meter/sec      RA   =          349
61997  deg
 ZDOT =       5961
909157                 TA   =             
00765
                                          MA   =             
00763
                                          Ha   =            188
006  n
mi
                                          Hp   =            186
008

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21812665
85                 X    =         6650066
33
 Y    =       -1792292
06  feet           Y    =         -471934
67  meter
 Z    =        2734477
29                 Z    =          865770
48
 XDOT =      -1139
971226                 XDOT =        -430
825639
 YDOT =      15968
755353  feet/sec       YDOT =        4862
923934  meter/sec
 ZDOT =      19560
069414                 ZDOT =        5960
019579

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20512296
42                 X    =         6252147
95
 Y    =       -7586493
18  feet           Y    =        -2312363
12  meter
 Z    =        2858825
78                 Z    =          871370
10
 XDOT =       2534
717984                 XDOT =         772
582042
 YDOT =      14221
577724  feet/sec       YDOT =        4334
736890  meter/sec
 ZDOT =      19553
166490                 ZDOT =        5959
805146


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   08174
35487483  
00020000  00000-0  20000-3 0  9067
2 25544  51
6420 349
7883 0009652 286
8640  73
1464 15
74625273 29343


Satellite: ISS
Catalog Number: 25544
Epoch time:      08174
35487483   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:       349
7883  deg
Eccentricity:     
0009652     
Arg of perigee:   286
8640  deg
Mean anomaly:      73
1464  deg
Mean motion:   15
74625273  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2934
Checksum:              322


Coasting Arc #8 (Orbit 2948)
---------------------------------------

Vector Time (GMT): 2008/175/07:02:02
466
Vector Time (MET): N/A
Weight (LBS)     : 661038
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         204237
66                 A    =         6718717
01  meter
 Y    =       -4308096
34  meter          E    =           
0005029
 Z    =       -5155706
28                 I    =           51
53569
 XDOT =       7523
779836                 Wp   =           77
83232
 YDOT =      -1092
547718  meter/sec      RA   =          344
45586  deg
 ZDOT =       1213
011626                 TA   =          203
76460
                                          MA   =          203
78783
                                          Ha   =            188
204  n
mi
                                          Hp   =            185
749

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         670071
05                 X    =          277441
53
 Y    =      -14134174
33  feet           Y    =        -4305402
32  meter
 Z    =      -16915046
85                 Z    =        -5154536
97
 XDOT =      24684
317048                 XDOT =        7529
545162
 YDOT =      -3584
474140  feet/sec       YDOT =       -1008
380455  meter/sec
 ZDOT =       3979
696936                 ZDOT =        1249
575629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3299070
03                 X    =        -1005556
55
 Y    =      -13765210
26  feet           Y    =        -4195636
09  meter
 Z    =      -16910878
53                 Z    =        -5154435
78
 XDOT =      21608
903470                 XDOT =        6586
393778
 YDOT =     -10232
769743  feet/sec       YDOT =       -3118
948218  meter/sec
 ZDOT =       4120
417081                 ZDOT =        1255
903126


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   08175
30683099  
00020000  00000-0  20000-3 0  9075
2 25544  51
6422 344
8951 0009732 290
4976  69
5143 15
74666326 29492


Satellite: ISS
Catalog Number: 25544
Epoch time:      08175
30683099   =   yrday
fracday
Element set:     907
Inclination:       51
6422  deg
RA of node:       344
8951  deg
Eccentricity:     
0009732     
Arg of perigee:   290
4976  deg
Mean anomaly:      69
5143  deg
Mean motion:   15
74666326  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2949
Checksum:              329


Coasting Arc #9 (Orbit 2964)
---------------------------------------

Vector Time (GMT): 2008/176/07:02:02
466
Vector Time (MET): N/A
Weight (LBS)     : 661038
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6463848
66                 A    =         6729596
01  meter
 Y    =        1340070
81  meter          E    =           
0004800
 Z    =       -1293982
26                 I    =           51
54444
 XDOT =        133
261911                 Wp   =          228
44953
 YDOT =      -5010
709555  meter/sec      RA   =          339
33167  deg
 ZDOT =      -5844
061902                 TA   =          325
77015
                                          MA   =          325
80108
                                          Ha   =            188
456  n
mi
                                          Hp   =            185
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21206852
56                 X    =        -6472067
25
 Y    =        4396557
78  feet           Y    =         1267742
58  meter
 Z    =       -4245348
63                 Z    =        -1325403
19
 XDOT =        437
210993                 XDOT =         217
671733
 YDOT =     -16439
335811  feet/sec       YDOT =       -5008
746583  meter/sec
 ZDOT =     -19173
431436                 ZDOT =       -5843
210178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18867393
10                 X    =        -5750781
42
 Y    =       10584928
28  feet           Y    =         3226286
14  meter
 Z    =       -4366242
30                 Z    =        -1330830
65
 XDOT =      -3668
978166                 XDOT =       -1118
304545
 YDOT =     -14461
860462  feet/sec       YDOT =       -4407
975069  meter/sec
 ZDOT =     -19170
544997                 ZDOT =       -5843
182115


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   08176
32223943  
00020000  00000-0  20000-3 0  9087
2 25544  51
6423 339
6758 0009786 293
5684  66
4451 15
74636414 29650


Satellite: ISS
Catalog Number: 25544
Epoch time:      08176
32223943   =   yrday
fracday
Element set:     908
Inclination:       51
6423  deg
RA of node:       339
6758  deg
Eccentricity:     
0009786     
Arg of perigee:   293
5684  deg
Mean anomaly:      66
4451  deg
Mean motion:   15
74636414  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2965
Checksum:              329


Coasting Arc #10 (Orbit 2980)
---------------------------------------

Vector Time (GMT): 2008/177/07:02:02
466
Vector Time (MET): N/A
Weight (LBS)     : 661038
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -21974
36                 A    =         6719106
65  meter
 Y    =        4460083
20  meter          E    =           
0008959
 Z    =        5031088
31                 I    =           51
48284
 XDOT =      -7235
563166                 Wp   =          330
87544
 YDOT =       1952
128944  meter/sec      RA   =          334
15435  deg
 ZDOT =      -1755
781395                 TA   =          136
11029
                                          MA   =          136
03908
                                          Ha   =            188
632  n
mi
                                          Hp   =            185
163

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -72094
35                 X    =          -96286
11
 Y    =       14632818
90  feet           Y    =         4459421
34  meter
 Z    =       16506195
23                 Z    =         5030801
61
 XDOT =     -23738
724299                 XDOT =       -7248
325181
 YDOT =       6404
622520  feet/sec       YDOT =        1871
145594  meter/sec
 ZDOT =      -5760
437649                 ZDOT =       -1790
962392

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4498359
84                 X    =         1371100
08
 Y    =       13925305
19  feet           Y    =         4244433
02  meter
 Z    =       16505444
61                 Z    =         5030859
52
 XDOT =     -19420
202678                 XDOT =       -5919
277776
 YDOT =      13286
415685  feet/sec       YDOT =        4049
699501  meter/sec
 ZDOT =      -5895
759549                 ZDOT =       -1797
027510


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   08177
33763212  
00020000  00000-0  20000-3 0  9098
2 25544  51
6423 334
4557 0009948 298
5896  61
4266 15
74726511 29815


Satellite: ISS
Catalog Number: 25544
Epoch time:      08177
33763212   =   yrday
fracday
Element set:     909
Inclination:       51
6423  deg
RA of node:       334
4557  deg
Eccentricity:     
0009948     
Arg of perigee:   298
5896  deg
Mean anomaly:      61
4266  deg
Mean motion:   15
74726511  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2981
Checksum:              325


Coasting Arc #11 (Orbit 2996)
---------------------------------------

Vector Time (GMT): 2008/178/07:02:02
466
Vector Time (MET): N/A
Weight (LBS)     : 661038
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6151265
80                 A    =         6728705
49  meter
 Y    =       -2045846
38  meter          E    =           
0012006
 Z    =        1772939
73                 I    =           51
48874
 XDOT =         96
443338                 Wp   =           21
32386
 YDOT =       5210
283034  meter/sec      RA   =          329
03328  deg
 ZDOT =       5676
692142                 TA   =          358
37873
                                          MA   =          358
38261
                                          Ha   =            188
783  n
mi
                                          Hp   =            184
958

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20181318
25                 X    =         6165072
98
 Y    =       -6712094
42  feet           Y    =        -1976982
42  meter
 Z    =        5816731
41                 Z    =         1802855
90
 XDOT =        316
415152                 XDOT =          10
597591
 YDOT =      17094
104441  feet/sec       YDOT =        5210
880827  meter/sec
 ZDOT =      18624
318051                 ZDOT =        5676
952790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16742805
91                 X    =         5103207
24
 Y    =      -13063871
96  feet           Y    =        -3981868
17  meter
 Z    =        5931768
88                 Z    =         1808003
15
 XDOT =       4962
505601                 XDOT =        1512
571707
 YDOT =      14818
634642  feet/sec       YDOT =        4516
719839  meter/sec
 ZDOT =      18625
736669                 ZDOT =        5677
124537


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   08178
35301375  
00020000  00000-0  20000-3 0  9101
2 25544  51
6416 329
2351 0010014 302
6593  57
3604 15
74723159 29970


Satellite: ISS
Catalog Number: 25544
Epoch time:      08178
35301375   =   yrday
fracday
Element set:     910
Inclination:       51
6416  deg
RA of node:       329
2351  deg
Eccentricity:     
0010014     
Arg of perigee:   302
6593  deg
Mean anomaly:      57
3604  deg
Mean motion:   15
74723159  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2997
Checksum:              283


Coasting Arc #12 (Orbit 3011)
---------------------------------------

Vector Time (GMT): 2008/179/07:02:02
466
Vector Time (MET): N/A
Weight (LBS)     : 661038
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -209667
96                 A    =         6719784
85  meter
 Y    =       -4642304
19  meter          E    =           
0004295
 Z    =       -4856118
05                 I    =           51
43347
 XDOT =       6827
593769                 Wp   =           55
84339
 YDOT =      -2714
137221  meter/sec      RA   =          323
84367  deg
 ZDOT =       2303
669385                 TA   =          236
63326
                                          MA   =          236
67437
                                          Ha   =            189
005  n
mi
                                          Hp   =            184
693

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -687886
99                 X    =         -134151
12
 Y    =      -15230656
79  feet           Y    =        -4644225
93  meter
 Z    =      -15932145
83                 Z    =        -4856953
81
 XDOT =      22400
242023                 XDOT =        6846
245369
 YDOT =      -8904
649674  feet/sec       YDOT =       -2637
683176  meter/sec
 ZDOT =       7557
970423                 ZDOT =        2336
882961

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5899089
12                 X    =        -1798042
36
 Y    =      -14054625
14  feet           Y    =        -4283849
74  meter
 Z    =      -15935734
21                 Z    =        -4857211
79
 XDOT =      16790
753399                 XDOT =        5117
821636
 YDOT =     -15747
611178  feet/sec       YDOT =       -4799
871887  meter/sec
 ZDOT =       7685
650297                 ZDOT =        2342
586211


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   08179
30492159  
00020000  00000-0  20000-3 0  9119
2 25544  51
6407 324
3408 0010051 306
3481  53
6755 15
74744542 30121


Satellite: ISS
Catalog Number: 25544
Epoch time:      08179
30492159   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:       324
3408  deg
Eccentricity:     
0010051     
Arg of perigee:   306
3481  deg
Mean anomaly:      53
6755  deg
Mean motion:   15
74744542  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3012
Checksum:              272


Coasting Arc #13 (Orbit 3027)
---------------------------------------

Vector Time (GMT): 2008/180/07:02:02
466
Vector Time (MET): N/A
Weight (LBS)     : 661038
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5754708
58                 A    =         6727803
26  meter
 Y    =        2655427
88  meter          E    =           
0004324
 Z    =       -2258176
07                 I    =           51
43711
 XDOT =       -372
671879                 Wp   =          301
29582
 YDOT =      -5437
616601  meter/sec      RA   =          318
72739  deg
 ZDOT =      -5434
610601                 TA   =          264
12354
                                          MA   =          264
17283
                                          Ha   =            189
244  n
mi
                                          Hp   =            184
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18880277
50                 X    =        -5773004
39
 Y    =        8712033
73  feet           Y    =         2590973
49  meter
 Z    =       -7408714
15                 Z    =        -2286176
71
 XDOT =      -1222
676768                 XDOT =        -285
439318
 YDOT =     -17839
949478  feet/sec       YDOT =       -5441
295446  meter/sec
 ZDOT =     -17830
087274                 ZDOT =       -5436
210011

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14331374
01                 X    =        -4368202
80
 Y    =       15012328
88  feet           Y    =         4575757
84  meter
 Z    =       -7516325
97                 Z    =        -2290976
16
 XDOT =      -6489
454798                 XDOT =       -1977
985822
 YDOT =     -15141
477363  feet/sec       YDOT =       -4615
122300  meter/sec
 ZDOT =     -17836
678372                 ZDOT =       -5436
619568


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   08180
32027722  
00020000  00000-0  20000-3 0  9124
2 25544  51
6401 319
1212 0010110 309
9147  50
1127 15
74735011 30287


Satellite: ISS
Catalog Number: 25544
Epoch time:      08180
32027722   =   yrday
fracday
Element set:     912
Inclination:       51
6401  deg
RA of node:       319
1212  deg
Eccentricity:     
0010110     
Arg of perigee:   309
9147  deg
Mean anomaly:      50
1127  deg
Mean motion:   15
74735011  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3028
Checksum:              233

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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