Date: March 8th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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


077/02:55:34 912 -0 4 0 8 0 8
N/A -0 3 -0 0 186 1
000/00:05:09 824 0 7 -0 1 180 9

Coasting Arc #1 (Orbit 1248)
---------------------------------------

Vector Time (GMT): 2008/067/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6066602
22                 A    =         6724182
55  meter
 Y    =        1760281
32  meter          E    =           
0006873
 Z    =       -2296107
68                 I    =           51
65393
 XDOT =      -3311
606568                 Wp   =          156
18595
 YDOT =       4333
567668  meter/sec      RA   =          179
46968  deg
 ZDOT =      -5439
205602                 TA   =           49
63679
                                          MA   =           49
57680
                                          Ha   =            186
734  n
mi
                                          Hp   =            181
144

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19903550
59                 X    =         6057621
48
 Y    =        5775201
19  feet           Y    =         1828071
09  meter
 Z    =       -7533161
67                 Z    =        -2266658
65
 XDOT =     -10864
850946                 XDOT =       -3333
396858
 YDOT =      14217
741692  feet/sec       YDOT =        4296
413005  meter/sec
 ZDOT =     -17845
162736                 ZDOT =       -5455
346465

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18999626
76                 X    =         5791086
24
 Y    =        8379067
44  feet           Y    =         2553939
76  meter
 Z    =       -7420122
08                 Z    =        -2261653
21
 XDOT =     -11949
342546                 XDOT =       -3642
159608
 YDOT =      11272
928192  feet/sec       YDOT =        3435
988513  meter/sec
 ZDOT =     -17906
461063                 ZDOT =       -5457
889332


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08067
54809357  
00020000  00000-0  20000-3 0  9001
2 25544  51
6386 180
3116 0002341 213
2993 146
8024 15
76027442 12499


Satellite: ISS
Catalog Number: 25544
Epoch time:      08067
54809357   =   yrday
fracday
Element set:     900
Inclination:       51
6386  deg
RA of node:       180
3116  deg
Eccentricity:     
0002341     
Arg of perigee:   213
2993  deg
Mean anomaly:     146
8024  deg
Mean motion:   15
76027442  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1249
Checksum:              282


Coasting Arc #2 (Orbit 1264)
---------------------------------------

Vector Time (GMT): 2008/068/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3329763
01                 A    =         6717786
81  meter
 Y    =       -3828604
98  meter          E    =           
0007503
 Z    =        4397255
01                 I    =           51
66243
 XDOT =       6667
308207                 Wp   =           77
64230
 YDOT =       1973
593449  meter/sec      RA   =          174
27616  deg
 ZDOT =      -3324
040161                 TA   =           45
74674
                                          MA   =           45
68518
                                          Ha   =            186
513  n
mi
                                          Hp   =            181
043

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10924419
33                 X    =         3350966
77
 Y    =      -12561039
94  feet           Y    =        -3791250
63  meter
 Z    =       14426689
65                 Z    =         4413482
72
 XDOT =      21874
370758                 XDOT =        6660
891052
 YDOT =       6475
044123  feet/sec       YDOT =        2048
114854  meter/sec
 ZDOT =     -10905
643573                 ZDOT =       -3291
666563

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12226910
65                 X    =         3726762
36
 Y    =      -11217904
48  feet           Y    =        -3419217
29  meter
 Z    =       14488385
41                 Z    =         4416059
87
 XDOT =      20218
175990                 XDOT =        6162
500042
 YDOT =       8085
471477  feet/sec       YDOT =        2464
451706  meter/sec
 ZDOT =     -10781
367597                 ZDOT =       -3286
160843


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08068
56260503  
00020000  00000-0  20000-3 0  9019
2 25544  51
6389 175
0860 0002112 217
6492 142
4525 15
76068214 12655


Satellite: ISS
Catalog Number: 25544
Epoch time:      08068
56260503   =   yrday
fracday
Element set:     901
Inclination:       51
6389  deg
RA of node:       175
0860  deg
Eccentricity:     
0002112     
Arg of perigee:   217
6492  deg
Mean anomaly:     142
4525  deg
Mean motion:   15
76068214  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1265
Checksum:              276


Coasting Arc #3 (Orbit 1280)
---------------------------------------

Vector Time (GMT): 2008/069/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5490745
42                 A    =         6720991
57  meter
 Y    =       -1732031
41  meter          E    =           
0011132
 Z    =        3459883
52                 I    =           51
70240
 XDOT =       4296
880279                 Wp   =           99
45125
 YDOT =      -4486
654074  meter/sec      RA   =          169
17738  deg
 ZDOT =       4558
820833                 TA   =          301
56923
                                          MA   =          301
67786
                                          Ha   =            186
470  n
mi
                                          Hp   =            181
046

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18014256
64                 X    =        -5487776
89
 Y    =       -5682517
75  feet           Y    =        -1793415
11  meter
 Z    =       11351323
90                 Z    =         3433217
02
 XDOT =      14097
376245                 XDOT =        4324
585578
 YDOT =     -14719
993680  feet/sec       YDOT =       -4438
448530  meter/sec
 ZDOT =      14956
761263                 ZDOT =        4579
762714

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17427333
54                 X    =        -5311851
26
 Y    =       -7443548
30  feet           Y    =        -2268793
52  meter
 Z    =       11248939
45                 Z    =         3428676
74
 XDOT =      14857
320596                 XDOT =        4528
511318
 YDOT =     -11990
434478  feet/sec       YDOT =       -3654
684429  meter/sec
 ZDOT =      15036
441203                 ZDOT =        4583
107279


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08069
57708638  
00020000  00000-0  20000-3 0  9028
2 25544  51
6388 169
8596 0002136 223
6238 136
4757 15
76133834 12811


Satellite: ISS
Catalog Number: 25544
Epoch time:      08069
57708638   =   yrday
fracday
Element set:     902
Inclination:       51
6388  deg
RA of node:       169
8596  deg
Eccentricity:     
0002136     
Arg of perigee:   223
6238  deg
Mean anomaly:     136
4757  deg
Mean motion:   15
76133834  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1281
Checksum:              321


Coasting Arc #4 (Orbit 1295)
---------------------------------------

Vector Time (GMT): 2008/070/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4120977
01                 A    =         6720735
81  meter
 Y    =        4026825
44  meter          E    =           
0003919
 Z    =       -3464561
98                 I    =           51
73002
 XDOT =      -5848
834698                 Wp   =          116
31776
 YDOT =      -2063
829125  meter/sec      RA   =          163
98037  deg
 ZDOT =       4560
475717                 TA   =          202
65860
                                          MA   =          202
67590
                                          Ha   =            186
270  n
mi
                                          Hp   =            180
973

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13520265
78                 X    =        -4148869
11
 Y    =       13211369
56  feet           Y    =         3980586
08  meter
 Z    =      -11366673
15                 Z    =        -3484649
74
 XDOT =     -19189
090216                 XDOT =       -5847
475891
 YDOT =      -6771
092930  feet/sec       YDOT =       -2129
226160  meter/sec
 ZDOT =      14962
190673                 ZDOT =        4532
065579

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14491415
09                 X    =        -4416983
32
 Y    =       12066169
36  feet           Y    =         3677768
42  meter
 Z    =      -11443145
40                 Z    =        -3487870
72
 XDOT =     -17775
137390                 XDOT =       -5417
861876
 YDOT =      -7268
676103  feet/sec       YDOT =       -2215
492476  meter/sec
 ZDOT =      14853
080468                 ZDOT =        4527
218927


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08070
52813879  
00020000  00000-0  20000-3 0  9030
2 25544  51
6383 164
9609 0002060 230
9243 129
1738 15
76159338 12961


Satellite: ISS
Catalog Number: 25544
Epoch time:      08070
52813879   =   yrday
fracday
Element set:     903
Inclination:       51
6383  deg
RA of node:       164
9609  deg
Eccentricity:     
0002060     
Arg of perigee:   230
9243  deg
Mean anomaly:     129
1738  deg
Mean motion:   15
76159338  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1296
Checksum:              303


Coasting Arc #5 (Orbit 1311)
---------------------------------------

Vector Time (GMT): 2008/071/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4663301
61                 A    =         6717511
00  meter
 Y    =        1946299
50  meter          E    =           
0007432
 Z    =       -4433389
35                 I    =           51
74578
 XDOT =      -5097
629314                 Wp   =           73
26867
 YDOT =       4742
743119  meter/sec      RA   =          158
88507  deg
 ZDOT =      -3282
293839                 TA   =          163
85482
                                          MA   =          163
83112
                                          Ha   =            186
228  n
mi
                                          Hp   =            181
112

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15299545
97                 X    =         4662727
83
 Y    =        6385497
03  feet           Y    =         1998443
75  meter
 Z    =      -14545240
65                 Z    =        -4410736
51
 XDOT =     -16724
505622                 XDOT =       -5134
339728
 YDOT =      15560
180835  feet/sec       YDOT =        4685
533080  meter/sec
 ZDOT =     -10768
680574                 ZDOT =       -3307
147572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14936700
09                 X    =         4552706
19
 Y    =        7366826
38  feet           Y    =         2245408
68  meter
 Z    =      -14458200
59                 Z    =        -4406859
54
 XDOT =     -17097
268820                 XDOT =       -5211
247536
 YDOT =      13360
929137  feet/sec       YDOT =        4072
411201  meter/sec
 ZDOT =     -10863
338553                 ZDOT =       -3311
145591


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08071
54256685  
00020000  00000-0  20000-3 0  9040
2 25544  51
6373 159
7343 0002001 235
8108 124
2867 15
76183993 13128


Satellite: ISS
Catalog Number: 25544
Epoch time:      08071
54256685   =   yrday
fracday
Element set:     904
Inclination:       51
6373  deg
RA of node:       159
7343  deg
Eccentricity:     
0002001     
Arg of perigee:   235
8108  deg
Mean anomaly:     124
2867  deg
Mean motion:   15
76183993  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1312
Checksum:              290


Coasting Arc #6 (Orbit 1327)
---------------------------------------

Vector Time (GMT): 2008/072/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4706839
59                 A    =         6723615
95  meter
 Y    =       -4257595
27  meter          E    =           
0012849
 Z    =        2199513
09                 I    =           51
79387
 XDOT =       4803
716203                 Wp   =          114
37420
 YDOT =       2457
377399  meter/sec      RA   =          153
69827  deg
 ZDOT =      -5503
130998                 TA   =           40
99848
                                          MA   =           40
90196
                                          Ha   =            186
067  n
mi
                                          Hp   =            180
863

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15442387
11                 X    =         4743414
02
 Y    =      -13968488
41  feet           Y    =        -4204756
14  meter
 Z    =        7216250
30                 Z    =         2222467
86
 XDOT =      15760
223763                 XDOT =        4802
613615
 YDOT =       8062
261808  feet/sec       YDOT =        2511
088987  meter/sec
 ZDOT =     -18054
891726                 ZDOT =       -5479
797295

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16047182
01                 X    =         4891181
08
 Y    =      -13221350
27  feet           Y    =        -4029867
56  meter
 Z    =        7303704
74                 Z    =         2226169
20
 XDOT =      14497
506782                 XDOT =        4418
840067
 YDOT =       7636
326609  feet/sec       YDOT =        2327
552351  meter/sec
 ZDOT =     -17965
174956                 ZDOT =       -5475
785327


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   08072
55696646  
00020000  00000-0  20000-3 0  9058
2 25544  51
6372 154
5075 0001774 243
5440 116
5542 15
76253457 13287


Satellite: ISS
Catalog Number: 25544
Epoch time:      08072
55696646   =   yrday
fracday
Element set:     905
Inclination:       51
6372  deg
RA of node:       154
5075  deg
Eccentricity:     
0001774     
Arg of perigee:   243
5440  deg
Mean anomaly:     116
5542  deg
Mean motion:   15
76253457  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1328
Checksum:              297


Coasting Arc #7 (Orbit 1343)
---------------------------------------

Vector Time (GMT): 2008/073/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3691746
34                 A    =         6714544
73  meter
 Y    =       -2414099
66  meter          E    =           
0004528
 Z    =        5061191
81                 I    =           51
78913
 XDOT =       5611
435680                 Wp   =          145
70410
 YDOT =      -4998
712167  meter/sec      RA   =          148
59005  deg
 ZDOT =       1704
405132                 TA   =          287
92168
                                          MA   =          287
97104
                                          Ha   =            186
068  n
mi
                                          Hp   =            180
865

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12112028
66                 X    =        -3689063
38
 Y    =       -7920274
48  feet           Y    =        -2455367
85  meter
 Z    =       16604960
01                 Z    =         5043263
91
 XDOT =      18410
222046                 XDOT =        5658
635341
 YDOT =     -16399
974300  feet/sec       YDOT =       -4935
697977  meter/sec
 ZDOT =       5591
880354                 ZDOT =        1731
780045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11960444
93                 X    =        -3645543
61
 Y    =       -8286523
75  feet           Y    =        -2525732
44  meter
 Z    =       16535959
74                 Z    =         5040160
53
 XDOT =      18262
428306                 XDOT =        5566
388148
 YDOT =     -14963
417316  feet/sec       YDOT =       -4560
849598  meter/sec
 ZDOT =       5696
201913                 ZDOT =        1736
202343


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   08073
57133728  
00020000  00000-0  20000-3 0  9069
2 25544  51
6372 149
2800 0001853 248
9898 111
1068 15
76302321 13445


Satellite: ISS
Catalog Number: 25544
Epoch time:      08073
57133728   =   yrday
fracday
Element set:     906
Inclination:       51
6372  deg
RA of node:       149
2800  deg
Eccentricity:     
0001853     
Arg of perigee:   248
9898  deg
Mean anomaly:     111
1068  deg
Mean motion:   15
76302321  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1344
Checksum:              286


Coasting Arc #8 (Orbit 1358)
---------------------------------------

Vector Time (GMT): 2008/074/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5006417
49                 A    =         6725440
88  meter
 Y    =        4424472
42  meter          E    =           
0009369
 Z    =        -726117
04                 I    =           51
84948
 XDOT =      -3655
194963                 Wp   =           32
93888
 YDOT =      -3158
206909  meter/sec      RA   =          143
42832  deg
 ZDOT =       6001
415900                 TA   =          319
16426
                                          MA   =          319
23443
                                          Ha   =            185
986  n
mi
                                          Hp   =            180
868

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16425254
25                 X    =        -5051993
23
 Y    =       14515985
65  feet           Y    =         4368232
98  meter
 Z    =       -2382273
76                 Z    =         -750548
67
 XDOT =     -11992
109459                 XDOT =       -3648
761264
 YDOT =     -10361
571225  feet/sec       YDOT =       -3199
045435  meter/sec
 ZDOT =      19689
684711                 ZDOT =        5983
674744

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16600262
33                 X    =        -5059759
96
 Y    =       14299711
12  feet           Y    =         4358551
95  meter
 Z    =       -2475398
35                 Z    =         -754501
42
 XDOT =     -10924
076664                 XDOT =       -3329
658567
 YDOT =      -9308
802247  feet/sec       YDOT =       -2837
322925  meter/sec
 ZDOT =      19621
305317                 ZDOT =        5980
573861


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   08074
52228630  
00020000  00000-0  20000-3 0  9073
2 25544  51
6366 144
3796 0001663 261
9607  98
1368 15
76281109 13593


Satellite: ISS
Catalog Number: 25544
Epoch time:      08074
52228630   =   yrday
fracday
Element set:     907
Inclination:       51
6366  deg
RA of node:       144
3796  deg
Eccentricity:     
0001663     
Arg of perigee:   261
9607  deg
Mean anomaly:      98
1368  deg
Mean motion:   15
76281109  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1359
Checksum:              308


Coasting Arc #9 (Orbit 1374)
---------------------------------------

Vector Time (GMT): 2008/075/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2689183
32                 A    =         6713425
76  meter
 Y    =        3167364
90  meter          E    =           
0013444
 Z    =       -5284640
93                 I    =           51
83221
 XDOT =      -5791
179947                 Wp   =           91
67075
 YDOT =       5066
407314  meter/sec      RA   =          138
29554  deg
 ZDOT =         89
432070                 TA   =          179
17736
                                          MA   =          179
17514
                                          Ha   =            185
906  n
mi
                                          Hp   =            180
833

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8822779
92                 X    =         2679236
94
 Y    =       10391617
14  feet           Y    =         3197381
26  meter
 Z    =      -17338060
80                 Z    =        -5271601
24
 XDOT =     -18999
934208                 XDOT =       -5847
837326
 YDOT =      16622
071241  feet/sec       YDOT =        5001
330248  meter/sec
 ZDOT =        293
412303                 ZDOT =          61
161300

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8963540
22                 X    =         2732087
06
 Y    =       10354998
03  feet           Y    =         3156203
40  meter
 Z    =      -17287696
99                 Z    =        -5269290
04
 XDOT =     -18177
898794                 XDOT =       -5540
623552
 YDOT =      16046
188729  feet/sec       YDOT =        4890
878325  meter/sec
 ZDOT =        185
632814                 ZDOT =          56
580882


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   08075
53660476  
00020000  00000-0  20000-3 0  9084
2 25544  51
6367 139
1518 0001644 262
8649  97
2328 15
76345916 13754


Satellite: ISS
Catalog Number: 25544
Epoch time:      08075
53660476   =   yrday
fracday
Element set:     908
Inclination:       51
6367  deg
RA of node:       139
1518  deg
Eccentricity:     
0001644     
Arg of perigee:   262
8649  deg
Mean anomaly:      97
2328  deg
Mean motion:   15
76345916  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1375
Checksum:              320


Coasting Arc #10 (Orbit 1390)
---------------------------------------

Vector Time (GMT): 2008/076/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5043020
72                 A    =         6724961
53  meter
 Y    =       -4350749
37  meter          E    =           
0009363
 Z    =        -894764
03                 I    =           51
89356
 XDOT =       2529
479034                 Wp   =          148
22628
 YDOT =       4153
464965  meter/sec      RA   =          133
16682  deg
 ZDOT =      -5975
406986                 TA   =           41
51554
                                          MA   =           41
44446
                                          Ha   =            185
881  n
mi
                                          Hp   =            180
583

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16545343
58                 X    =         5095643
19
 Y    =      -14274112
11  feet           Y    =        -4294061
23  meter
 Z    =       -2935577
54                 Z    =         -870137
59
 XDOT =       8298
815729                 XDOT =        2511
873252
 YDOT =      13626
853559  feet/sec       YDOT =        4181
652477  meter/sec
 ZDOT =     -19604
353627                 ZDOT =       -5963
161860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16253943
61                 X    =         4954202
01
 Y    =      -14623627
92  feet           Y    =        -4457281
79  meter
 Z    =       -2841673
73                 Z    =         -866142
15
 XDOT =       7631
899342                 XDOT =        2326
202920
 YDOT =      12259
420840  feet/sec       YDOT =        3736
671472  meter/sec
 ZDOT =     -19556
914326                 ZDOT =       -5960
947486


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   08076
55089515  
00020000  00000-0  20000-3 0  9097
2 25544  51
6374 133
9241 0001442 271
2134  88
8865 15
76423956 13917


Satellite: ISS
Catalog Number: 25544
Epoch time:      08076
55089515   =   yrday
fracday
Element set:     909
Inclination:       51
6374  deg
RA of node:       133
9241  deg
Eccentricity:     
0001442     
Arg of perigee:   271
2134  deg
Mean anomaly:      88
8865  deg
Mean motion:   15
76423956  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1391
Checksum:              306


Coasting Arc #11 (Orbit 1400)
---------------------------------------

Vector Time (GMT): 2008/077/02:58:09
824
Vector Time (MET): N/A
Weight (LBS)     : 567143
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4940918
54                 A    =         6725078
28  meter
 Y    =        4384838
30  meter          E    =           
0013046
 Z    =        1222361
18                 I    =           51
90139
 XDOT =      -2388
725400                 Wp   =           51
34677
 YDOT =      -4345
682364  meter/sec      RA   =          130
07047  deg
 ZDOT =       5899
315269                 TA   =          322
02141
                                          MA   =          322
11333
                                          Ha   =            186
054  n
mi
                                          Hp   =            180
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16210362
67                 X    =        -4995521
16
 Y    =       14385952
42  feet           Y    =         4329280
87  meter
 Z    =        4010371
34                 Z    =         1198225
90
 XDOT =      -7837
025591                 XDOT =       -2368
611002
 YDOT =     -14257
488070  feet/sec       YDOT =       -4372
281776  meter/sec
 ZDOT =      19354
708887                 ZDOT =        5887
760090

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3615834
95                 X    =         1102106
49
 Y    =      -21386604
12  feet           Y    =        -6518636
94  meter
 Z    =        3918349
78                 Z    =         1194313
01
 XDOT =      13573
427462                 XDOT =        4137
180691
 YDOT =       5853
623219  feet/sec       YDOT =        1784
184357  meter/sec
 ZDOT =      19309
889397                 ZDOT =        5885
654288


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   08077
18481792  
00020000  00000-0  20000-3 0  9102
2 25544  51
6346 130
6544 0001850 296
9494  63
1481 15
76282470 14018


Satellite: ISS
Catalog Number: 25544
Epoch time:      08077
18481792   =   yrday
fracday
Element set:     910
Inclination:       51
6346  deg
RA of node:       130
6544  deg
Eccentricity:     
0001850     
Arg of perigee:   296
9494  deg
Mean anomaly:      63
1481  deg
Mean motion:   15
76282470  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1401
Checksum:              292


Coasting Arc #12 (Orbit 1415)
---------------------------------------

Vector Time (GMT): 2008/078/02:58:09
824
Vector Time (MET): N/A
Weight (LBS)     : 567143
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1720527
15                 A    =         6715118
48  meter
 Y    =        4260919
49  meter          E    =           
0010844
 Z    =       -4906541
89                 I    =           51
88584
 XDOT =      -5540
233426                 Wp   =          104
30177
 YDOT =       4839
646138  meter/sec      RA   =          124
90498  deg
 ZDOT =       2261
606999                 TA   =          187
62143
                                          MA   =          187
63792
                                          Ha   =            186
039  n
mi
                                          Hp   =            180
760

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5644774
12                 X    =         1696587
63
 Y    =       13979394
67  feet           Y    =         4280025
25  meter
 Z    =      -16097578
37                 Z    =        -4898242
15
 XDOT =     -18176
618853                 XDOT =       -5604
925596
 YDOT =      15878
104126  feet/sec       YDOT =        4777
330512  meter/sec
 ZDOT =       7419
970468                 ZDOT =        2234
535660

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13360361
00                 X    =        -4072238
03
 Y    =       -7058862
18  feet           Y    =        -2151541
19  meter
 Z    =      -16065248
15                 Z    =        -4896687
63
 XDOT =       3301
291679                 XDOT =        1006
233704
 YDOT =     -22889
168198  feet/sec       YDOT =       -6976
618467  meter/sec
 ZDOT =       7316
738202                 ZDOT =        2230
141804


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   08078
13576680  
00020000  00000-0  20000-3 0  9110
2 25544  51
6343 125
7529 0001684 301
0141  59
0858 15
76328554 14167


Satellite: ISS
Catalog Number: 25544
Epoch time:      08078
13576680   =   yrday
fracday
Element set:     911
Inclination:       51
6343  deg
RA of node:       125
7529  deg
Eccentricity:     
0001684     
Arg of perigee:   301
0141  deg
Mean anomaly:      59
0858  deg
Mean motion:   15
76328554  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1416
Checksum:              289


Coasting Arc #13 (Orbit 1431)
---------------------------------------

Vector Time (GMT): 2008/079/02:58:09
824
Vector Time (MET): N/A
Weight (LBS)     : 567143
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4709144
27                 A    =         6722278
59  meter
 Y    =       -3965731
16  meter          E    =           
0003195
 Z    =       -2699145
07                 I    =           51
92618
 XDOT =       1593
098810                 Wp   =          121
80409
 YDOT =       5437
034697  meter/sec      RA   =          119
81148  deg
 ZDOT =      -5215
066565                 TA   =           88
86349
                                          MA   =           88
82689
                                          Ha   =            186
028  n
mi
                                          Hp   =            180
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15449948
38                 X    =         4766251
42
 Y    =      -13010929
01  feet           Y    =        -3912751
75  meter
 Z    =       -8855462
84                 Z    =        -2676129
42
 XDOT =       5226
702131                 XDOT =        1557
516038
 YDOT =      17838
040344  feet/sec       YDOT =        5454
650239  meter/sec
 ZDOT =     -17109
798443                 ZDOT =       -5207
414325

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3222434
57                 X    =         -982198
06
 Y    =       19978693
69  feet           Y    =         6089505
84  meter
 Z    =       -8767674
41                 Z    =        -2672387
16
 XDOT =     -14233
631497                 XDOT =       -4338
410880
 YDOT =      -9782
379990  feet/sec       YDOT =       -2981
669421  meter/sec
 ZDOT =     -17079
810021                 ZDOT =       -5205
926094


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   08079
15008518  
00020000  00000-0  20000-3 0  9124
2 25544  51
6344 120
5256 0001727 310
4570  49
6443 15
76386766 14328


Satellite: ISS
Catalog Number: 25544
Epoch time:      08079
15008518   =   yrday
fracday
Element set:     912
Inclination:       51
6344  deg
RA of node:       120
5256  deg
Eccentricity:     
0001727     
Arg of perigee:   310
4570  deg
Mean anomaly:      49
6443  deg
Mean motion:   15
76386766  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1432
Checksum:              284

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data may contain past, current and future orbital data These sources include:

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

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

   David Cottle
   Director Of Engineering
   IDB Communications

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