Date: April 27th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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


There are no maneuvers



Coasting Arc #1 (Orbit 2021)
---------------------------------------

Vector Time (GMT): 2008/116/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4172485
01                 A    =         6715360
79  meter
 Y    =        -692346
68  meter          E    =           
0020440
 Z    =       -5232827
73                 I    =           51
30555
 XDOT =       1865
276442                 Wp   =          103
24436
 YDOT =      -7442
319548  meter/sec      RA   =          287
11578  deg
 ZDOT =       -508
910734                 TA   =          161
92766
                                          MA   =          161
85490
                                          Ha   =            189
866  n
mi
                                          Hp   =            178
947

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13689255
29                 X    =        -4139012
57
 Y    =       -2271478
60  feet           Y    =         -738818
28  meter
 Z    =      -17168069
97                 Z    =        -5253016
62
 XDOT =       6119
673365                 XDOT =        1950
831213
 YDOT =     -24417
058886  feet/sec       YDOT =       -7420
982565  meter/sec
 ZDOT =      -1669
654640                 ZDOT =        -499
641816

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11792245
11                 X    =        -3594276
31
 Y    =        7129556
56  feet           Y    =         2173088
84  meter
 Z    =      -17245588
72                 Z    =        -5256455
44
 XDOT =     -10734
153113                 XDOT =       -3271
769869
 YDOT =     -21659
079505  feet/sec       YDOT =       -6601
687433  meter/sec
 ZDOT =      -1634
833793                 ZDOT =        -498
297340


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   08116
53756166  
00020000  00000-0  20000-3 0  9004
2 25544  51
6370 287
6963 0007595 139
0624 221
1111 15
75695371 20220


Satellite: ISS
Catalog Number: 25544
Epoch time:      08116
53756166   =   yrday
fracday
Element set:     900
Inclination:       51
6370  deg
RA of node:       287
6963  deg
Eccentricity:     
0007595     
Arg of perigee:   139
0624  deg
Mean anomaly:     221
1111  deg
Mean motion:   15
75695371  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2022
Checksum:              286


Coasting Arc #2 (Orbit 2037)
---------------------------------------

Vector Time (GMT): 2008/117/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1507221
44                 A    =         6727196
57  meter
 Y    =        6544755
84  meter          E    =           
0019218
 Z    =        -150621
19                 I    =           51
33822
 XDOT =      -4665
906749                 Wp   =          138
48285
 YDOT =      -1202
616349  meter/sec      RA   =          281
94069  deg
 ZDOT =      -6016
784763                 TA   =           43
16258
                                          MA   =           43
01209
                                          Ha   =            189
607  n
mi
                                          Hp   =            179
201

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4944952
24                 X    =        -1579562
21
 Y    =       21472296
08  feet           Y    =         6527496
77  meter
 Z    =        -494164
00                 Z    =         -158118
61
 XDOT =     -15308
093009                 XDOT =       -4622
883454
 YDOT =      -3945
591697  feet/sec       YDOT =       -1254
552235  meter/sec
 ZDOT =     -19740
107491                 ZDOT =       -6039
347483

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10570674
08                 X    =         3221941
46
 Y    =       19332468
24  feet           Y    =         5892536
32  meter
 Z    =        -522274
90                 Z    =         -159189
39
 XDOT =     -12569
312801                 XDOT =       -3831
126542
 YDOT =       6374
912865  feet/sec       YDOT =        1943
073441  meter/sec
 ZDOT =     -19826
789668                 ZDOT =       -6043
205491


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   08117
55229402  
00020000  00000-0  20000-3 0  9016
2 25544  51
6366 282
4706 0007295 142
7063 217
4609 15
75750334 20386


Satellite: ISS
Catalog Number: 25544
Epoch time:      08117
55229402   =   yrday
fracday
Element set:     901
Inclination:       51
6366  deg
RA of node:       282
4706  deg
Eccentricity:     
0007295     
Arg of perigee:   142
7063  deg
Mean anomaly:     217
4609  deg
Mean motion:   15
75750334  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2038
Checksum:              284


Coasting Arc #3 (Orbit 2053)
---------------------------------------

Vector Time (GMT): 2008/118/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4017844
70                 A    =         6715475
89  meter
 Y    =        1410255
40  meter          E    =           
0008385
 Z    =        5186248
45                 I    =           51
29362
 XDOT =      -1562
269618                 Wp   =          122
91341
 YDOT =       7504
003577  meter/sec      RA   =          276
76011  deg
 ZDOT =       -833
724777                 TA   =          335
03138
                                          MA   =          335
07192
                                          Ha   =            189
606  n
mi
                                          Hp   =            179
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13181905
20                 X    =         3976582
42
 Y    =        4626822
17  feet           Y    =         1454954
23  meter
 Z    =       17015250
83                 Z    =         5205667
09
 XDOT =      -5125
556488                 XDOT =       -1642
014344
 YDOT =      24619
434309  feet/sec       YDOT =        7486
087557  meter/sec
 ZDOT =      -2735
317509                 ZDOT =        -841
507596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12762066
27                 X    =         3889877
80
 Y    =       -5454717
08  feet           Y    =        -1662597
77  meter
 Z    =       17089897
45                 Z    =         5209000
74
 XDOT =      12511
234865                 XDOT =        3813
424387
 YDOT =      20646
806935  feet/sec       YDOT =        6293
146754  meter/sec
 ZDOT =      -2764
421905                 ZDOT =        -842
595797


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   08118
56701152  
00020000  00000-0  20000-3 0  9026
2 25544  51
6367 277
2460 0007508 146
1217 214
0428 15
75702844 20545


Satellite: ISS
Catalog Number: 25544
Epoch time:      08118
56701152   =   yrday
fracday
Element set:     902
Inclination:       51
6367  deg
RA of node:       277
2460  deg
Eccentricity:     
0007508     
Arg of perigee:   146
1217  deg
Mean anomaly:     214
0428  deg
Mean motion:   15
75702844  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2054
Checksum:              273


Coasting Arc #4 (Orbit 2069)
---------------------------------------

Vector Time (GMT): 2008/119/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1229435
03                 A    =         6726314
79  meter
 Y    =       -6479146
23  meter          E    =           
0015707
 Z    =        1308488
79                 I    =           51
33002
 XDOT =       4602
420446                 Wp   =           88
03595
 YDOT =       2060
915168  meter/sec      RA   =          271
60770  deg
 ZDOT =       5820
918137                 TA   =          286
39837
                                          MA   =          286
57098
                                          Ha   =            189
493  n
mi
                                          Hp   =            179
313

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4033579
49                 X    =         1295438
06
 Y    =      -21257041
44  feet           Y    =        -6465029
00  meter
 Z    =        4292942
22                 Z    =         1314621
45
 XDOT =      15099
804612                 XDOT =        4550
755845
 YDOT =       6761
532705  feet/sec       YDOT =        2112
092944  meter/sec
 ZDOT =      19097
500450                 ZDOT =        5843
151366

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11756555
43                 X    =        -3583398
09
 Y    =      -18158141
35  feet           Y    =        -5534601
48  meter
 Z    =        4315812
15                 Z    =         1315459
54
 XDOT =      14194
673343                 XDOT =        4326
536435
 YDOT =      -4584
759239  feet/sec       YDOT =       -1397
434616  meter/sec
 ZDOT =      19183
018666                 ZDOT =        5846
984090


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   08119
58170492  
00020000  00000-0  20000-3 0  9037
2 25544  51
6377 272
0214 0007504 151
1996 208
9583 15
75799755 20701


Satellite: ISS
Catalog Number: 25544
Epoch time:      08119
58170492   =   yrday
fracday
Element set:     903
Inclination:       51
6377  deg
RA of node:       272
0214  deg
Eccentricity:     
0007504     
Arg of perigee:   151
1996  deg
Mean anomaly:     208
9583  deg
Mean motion:   15
75799755  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2070
Checksum:              310


Coasting Arc #5 (Orbit 2084)
---------------------------------------

Vector Time (GMT): 2008/120/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4064659
34                 A    =         6716561
24  meter
 Y    =       -2197402
39  meter          E    =           
0018300
 Z    =       -4891182
24                 I    =           51
29776
 XDOT =       1294
956899                 Wp   =          123
54567
 YDOT =      -7259
461459  meter/sec      RA   =          266
40533  deg
 ZDOT =       2181
136438                 TA   =          167
78871
                                          MA   =          167
74429
                                          Ha   =            189
368  n
mi
                                          Hp   =            179
328

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13335496
52                 X    =        -4016024
98
 Y    =       -7209325
42  feet           Y    =        -2242583
67  meter
 Z    =      -16047185
84                 Z    =        -4910810
36
 XDOT =       4248
546255                 XDOT =        1365
441483
 YDOT =     -23817
130770  feet/sec       YDOT =       -7244
586469  meter/sec
 ZDOT =       7155
959443                 ZDOT =        2187
598374

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14493086
03                 X    =        -4417492
62
 Y    =        4162943
09  feet           Y    =         1268865
05  meter
 Z    =      -16122728
56                 Z    =        -4914207
66
 XDOT =     -13419
265957                 XDOT =       -4090
192264
 YDOT =     -18859
096234  feet/sec       YDOT =       -5748
252532  meter/sec
 ZDOT =       7180
004919                 ZDOT =        2188
465499


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   08120
53296601  
00020000  00000-0  20000-3 0  9046
2 25544  51
6378 267
1237 0007362 154
2789 205
8743 15
75803812 20858


Satellite: ISS
Catalog Number: 25544
Epoch time:      08120
53296601   =   yrday
fracday
Element set:     904
Inclination:       51
6378  deg
RA of node:       267
1237  deg
Eccentricity:     
0007362     
Arg of perigee:   154
2789  deg
Mean anomaly:     205
8743  deg
Mean motion:   15
75803812  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2085
Checksum:              296


Coasting Arc #6 (Orbit 2100)
---------------------------------------

Vector Time (GMT): 2008/121/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1067013
80                 A    =         6724259
77  meter
 Y    =        6152464
76  meter          E    =           
0012239
 Z    =       -2484292
12                 I    =           51
32705
 XDOT =      -4745
803307                 Wp   =          146
59679
 YDOT =      -2954
319299  meter/sec      RA   =          261
27091  deg
 ZDOT =      -5300
602852                 TA   =           61
66443
                                          MA   =           61
54104
                                          Ha   =            189
183  n
mi
                                          Hp   =            179
564

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3500701
44                 X    =        -1123664
01
 Y    =       20185251
85  feet           Y    =         6140216
09  meter
 Z    =       -8150564
70                 Z    =        -2489613
24
 XDOT =     -15570
220823                 XDOT =       -4686
665405
 YDOT =      -9692
648620  feet/sec       YDOT =       -3007
058869  meter/sec
 ZDOT =     -17390
429304                 ZDOT =       -5323
514486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11997142
67                 X    =         3656729
09
 Y    =       16596539
26  feet           Y    =         5058625
17  meter
 Z    =       -8170340
26                 Z    =        -2490319
71
 XDOT =     -16541
476329                 XDOT =       -5041
841985
 YDOT =       3388
889918  feet/sec       YDOT =        1032
933647  meter/sec
 ZDOT =     -17478
656053                 ZDOT =       -5327
494365


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   08121
54762496  
00020000  00000-0  20000-3 0  9059
2 25544  51
6377 261
8976 0007262 158
0740 202
0736 15
75832867 21018


Satellite: ISS
Catalog Number: 25544
Epoch time:      08121
54762496   =   yrday
fracday
Element set:     905
Inclination:       51
6377  deg
RA of node:       261
8976  deg
Eccentricity:     
0007262     
Arg of perigee:   158
0740  deg
Mean anomaly:     202
0736  deg
Mean motion:   15
75832867  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2101
Checksum:              299


Coasting Arc #7 (Orbit 2116)
---------------------------------------

Vector Time (GMT): 2008/122/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4261607
07                 A    =         6718846
70  meter
 Y    =        2913305
49  meter          E    =           
0012099
 Z    =        4288328
10                 I    =           51
31510
 XDOT =      -1163
480678                 Wp   =          108
20650
 YDOT =       6794
740086  meter/sec      RA   =          256
05225  deg
 ZDOT =      -3455
595807                 TA   =           16
84881
                                          MA   =           16
80866
                                          Ha   =            189
039  n
mi
                                          Hp   =            179
695

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13981650
50                 X    =         4207881
17
 Y    =        9558088
86  feet           Y    =         2960660
82  meter
 Z    =       14069317
93                 Z    =         4308900
70
 XDOT =      -3817
193824                 XDOT =       -1222
587225
 YDOT =      22292
454350  feet/sec       YDOT =        6781
398899  meter/sec
 ZDOT =     -11337
256586                 ZDOT =       -3461
391621

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16498723
26                 X    =         5028810
85
 Y    =       -3521282
12  feet           Y    =        -1073286
79  meter
 Z    =       14148569
67                 Z    =         4312484
03
 XDOT =      13348
904820                 XDOT =        4068
746189
 YDOT =      16850
188351  feet/sec       YDOT =        5135
937410  meter/sec
 ZDOT =     -11358
780487                 ZDOT =       -3462
156293


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   08122
56226621  
00020000  00000-0  20000-3 0  9068
2 25544  51
6383 256
6727 0007274 161
3439 198
7993 15
75830691 21172


Satellite: ISS
Catalog Number: 25544
Epoch time:      08122
56226621   =   yrday
fracday
Element set:     906
Inclination:       51
6383  deg
RA of node:       256
6727  deg
Eccentricity:     
0007274     
Arg of perigee:   161
3439  deg
Mean anomaly:     198
7993  deg
Mean motion:   15
75830691  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2117
Checksum:              312


Coasting Arc #8 (Orbit 2132)
---------------------------------------

Vector Time (GMT): 2008/123/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1015912
30                 A    =         6721343
51  meter
 Y    =       -5642204
01  meter          E    =           
0015860
 Z    =        3503658
93                 I    =           51
33366
 XDOT =       5064
999678                 Wp   =          118
14428
 YDOT =       3702
313206  meter/sec      RA   =          250
93018  deg
 ZDOT =       4470
727813                 TA   =          283
75862
                                          MA   =          283
93510
                                          Ha   =            188
861  n
mi
                                          Hp   =            179
741

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3333045
62                 X    =         1061908
40
 Y    =      -18511168
00  feet           Y    =        -5630586
31  meter
 Z    =       11494944
00                 Z    =         3508706
04
 XDOT =      16617
453012                 XDOT =        5001
505065
 YDOT =      12146
696871  feet/sec       YDOT =        3758
597919  meter/sec
 ZDOT =      14667
742170                 ZDOT =        4495
179725

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11451788
98                 X    =        -3490505
28
 Y    =      -14906280
41  feet           Y    =        -4543434
27  meter
 Z    =       11513713
77                 Z    =         3509379
96
 XDOT =      19035
496695                 XDOT =        5802
019393
 YDOT =      -3164
269021  feet/sec       YDOT =        -964
469198  meter/sec
 ZDOT =      14761
967409                 ZDOT =        4499
447666


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   08123
57688507  
00020000  00000-0  20000-3 0  9076
2 25544  51
6393 251
4471 0007154 166
1961 193
9400 15
75925728 21336


Satellite: ISS
Catalog Number: 25544
Epoch time:      08123
57688507   =   yrday
fracday
Element set:     907
Inclination:       51
6393  deg
RA of node:       251
4471  deg
Eccentricity:     
0007154     
Arg of perigee:   166
1961  deg
Mean anomaly:     193
9400  deg
Mean motion:   15
75925728  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2133
Checksum:              304


Coasting Arc #9 (Orbit 2147)
---------------------------------------

Vector Time (GMT): 2008/124/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4598937
86                 A    =         6721565
17  meter
 Y    =       -3508226
88  meter          E    =           
0009467
 Z    =       -3436150
40                 I    =           51
34535
 XDOT =       1243
471454                 Wp   =          138
61535
 YDOT =      -6081
605018  meter/sec      RA   =          245
70689  deg
 ZDOT =       4545
046931                 TA   =          180
54035
                                          MA   =          180
54138
                                          Ha   =            188
735  n
mi
                                          Hp   =            179
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15088378
80                 X    =        -4542673
96
 Y    =      -11509930
71  feet           Y    =        -3559340
21  meter
 Z    =      -11273459
31                 Z    =        -3458355
88
 XDOT =       4079
630753                 XDOT =        1289
305012
 YDOT =     -19952
772369  feet/sec       YDOT =       -6067
443593  meter/sec
 ZDOT =      14911
571296                 ZDOT =        4551
199105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18573775
70                 X    =        -5661286
83
 Y    =        3635312
33  feet           Y    =         1108043
20  meter
 Z    =      -11359045
95                 Z    =        -3462237
20
 XDOT =     -12040
064023                 XDOT =       -3669
811514
 YDOT =     -14852
191051  feet/sec       YDOT =       -4526
947832  meter/sec
 ZDOT =      14934
535443                 ZDOT =        4552
046403


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   08124
52807691  
00020000  00000-0  20000-3 0  9080
2 25544  51
6395 246
5488 0006888 169
7813 190
3493 15
75897335 21480


Satellite: ISS
Catalog Number: 25544
Epoch time:      08124
52807691   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:       246
5488  deg
Eccentricity:     
0006888     
Arg of perigee:   169
7813  deg
Mean anomaly:     190
3493  deg
Mean motion:   15
75897335  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2148
Checksum:              342


Coasting Arc #10 (Orbit 2163)
---------------------------------------

Vector Time (GMT): 2008/125/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1229002
85                 A    =         6718306
54  meter
 Y    =        4950364
35  meter          E    =           
0010081
 Z    =       -4378534
33                 I    =           51
34832
 XDOT =      -5465
152587                 Wp   =          111
26859
 YDOT =      -4285
484003  meter/sec      RA   =          240
58560  deg
 ZDOT =      -3320
894234                 TA   =          125
24790
                                          MA   =          125
15351
                                          Ha   =            188
567  n
mi
                                          Hp   =            180
051

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4032161
58                 X    =        -1262996
59
 Y    =       16241352
86  feet           Y    =         4936431
04  meter
 Z    =      -14365270
11                 Z    =        -4384587
36
 XDOT =     -17930
290639                 XDOT =       -5400
692737
 YDOT =     -14059
986887  feet/sec       YDOT =       -4346
237923  meter/sec
 ZDOT =     -10895
322289                 ZDOT =       -3347
288206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9788073
55                 X    =         2983404
82
 Y    =       13549191
47  feet           Y    =         4129793
56  meter
 Z    =      -14387976
99                 Z    =        -4385455
39
 XDOT =     -21306
455593                 XDOT =       -6494
207665
 YDOT =       3748
007169  feet/sec       YDOT =        1142
392585  meter/sec
 ZDOT =     -10997
067646                 ZDOT =       -3351
906218


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   08125
54266243  
00020000  00000-0  20000-3 0  9096
2 25544  51
6401 241
3232 0006940 173
7247 186
4006 15
75931933 21640


Satellite: ISS
Catalog Number: 25544
Epoch time:      08125
54266243   =   yrday
fracday
Element set:     909
Inclination:       51
6401  deg
RA of node:       241
3232  deg
Eccentricity:     
0006940     
Arg of perigee:   173
7247  deg
Mean anomaly:     186
4006  deg
Mean motion:   15
75931933  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2164
Checksum:              278


Coasting Arc #11 (Orbit 2179)
---------------------------------------

Vector Time (GMT): 2008/126/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4945410
70                 A    =         6724224
60  meter
 Y    =        3904779
80  meter          E    =           
0017619
 Z    =        2316662
24                 I    =           51
38397
 XDOT =      -1613
431651                 Wp   =          128
40367
 YDOT =       5259
483199  meter/sec      RA   =          235
37132  deg
 ZDOT =      -5403
893265                 TA   =           25
38771
                                          MA   =           25
30125
                                          Ha   =            188
406  n
mi
                                          Hp   =            180
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16225100
71                 X    =         4890125
06
 Y    =       12810957
36  feet           Y    =         3959772
92  meter
 Z    =        7600597
91                 Z    =         2340553
68
 XDOT =      -5293
410929                 XDOT =       -1645
872281
 YDOT =      17255
522305  feet/sec       YDOT =        5241
259906  meter/sec
 ZDOT =     -17729
308612                 ZDOT =       -5411
809925

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20177955
23                 X    =         6150240
75
 Y    =       -4337747
33  feet           Y    =        -1322145
39  meter
 Z    =        7692703
10                 Z    =         2344735
90
 XDOT =       9695
884422                 XDOT =        2955
305572
 YDOT =      13510
937968  feet/sec       YDOT =        4118
133893  meter/sec
 ZDOT =     -17759
140814                 ZDOT =       -5412
986120


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   08126
55723018  
00020000  00000-0  20000-3 0  9108
2 25544  51
6399 236
0985 0006897 176
2509 183
8708 15
75955991 21800


Satellite: ISS
Catalog Number: 25544
Epoch time:      08126
55723018   =   yrday
fracday
Element set:     910
Inclination:       51
6399  deg
RA of node:       236
0985  deg
Eccentricity:     
0006897     
Arg of perigee:   176
2509  deg
Mean anomaly:     183
8708  deg
Mean motion:   15
75955991  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2180
Checksum:              330


Coasting Arc #12 (Orbit 2195)
---------------------------------------

Vector Time (GMT): 2008/127/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1651164
67                 A    =         6715620
45  meter
 Y    =       -4213221
16  meter          E    =           
0011136
 Z    =        4960952
00                 I    =           51
37369
 XDOT =       5860
240960                 Wp   =          154
84321
 YDOT =       4606
756434  meter/sec      RA   =          230
23887  deg
 ZDOT =       1950
389685                 TA   =          276
18761
                                          MA   =          276
31446
                                          Ha   =            188
175  n
mi
                                          Hp   =            180
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5417206
91                 X    =         1674054
88
 Y    =      -13822904
06  feet           Y    =        -4194629
45  meter
 Z    =       16276089
25                 Z    =         4969028
68
 XDOT =      19226
512336                 XDOT =        5798
817081
 YDOT =      15114
030295  feet/sec       YDOT =        4671
945344  meter/sec
 ZDOT =       6398
916289                 ZDOT =        1978
710701

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7500303
80                 X    =        -2286092
60
 Y    =      -12773740
44  feet           Y    =        -3893436
09  meter
 Z    =       16306651
61                 Z    =         4970267
41
 XDOT =      22844
140590                 XDOT =        6962
894052
 YDOT =      -5056
948311  feet/sec       YDOT =       -1541
357845  meter/sec
 ZDOT =       6508
104133                 ZDOT =        1983
670140


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   08127
57177735  
00020000  00000-0  20000-3 0  9111
2 25544  51
6404 230
8727 0006741 180
9817 179
1336 15
76033524 21967


Satellite: ISS
Catalog Number: 25544
Epoch time:      08127
57177735   =   yrday
fracday
Element set:     911
Inclination:       51
6404  deg
RA of node:       230
8727  deg
Eccentricity:     
0006741     
Arg of perigee:   180
9817  deg
Mean anomaly:     179
1336  deg
Mean motion:   15
76033524  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2196
Checksum:              300

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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