Date: April 9th 2009

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) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 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 3499)
---------------------------------------

Vector Time (GMT): 2009/098/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4157292
47                 A    =         6737485
44  meter
 Y    =        5232170
79  meter          E    =           
0015536
 Z    =        -773338
58                 I    =           51
37961
 XDOT =      -3362
729842                 Wp   =          174
80642
 YDOT =      -3548
212933  meter/sec      RA   =          303
16496  deg
 ZDOT =      -5953
383761                 TA   =           13
65442
                                          MA   =           13
61244
                                          Ha   =            193
764  n
mi
                                          Hp   =            187
855

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13639410
98                 X    =        -4211733
73
 Y    =       17165914
66  feet           Y    =         5185377
06  meter
 Z    =       -2537200
05                 Z    =         -793667
52
 XDOT =     -11032
578222                 XDOT =       -3293
882533
 YDOT =     -11641
118548  feet/sec       YDOT =       -3585
432498  meter/sec
 ZDOT =     -19532
098954                 ZDOT =       -5969
552486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         549013
84                 X    =          167339
42
 Y    =       21908755
24  feet           Y    =         6677788
60  meter
 Z    =       -2616212
87                 Z    =         -797421
68
 XDOT =     -14245
837101                 XDOT =       -4342
131148
 YDOT =      -1973
663072  feet/sec       YDOT =        -601
572504  meter/sec
 ZDOT =     -19595
472069                 ZDOT =       -5972
699887


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   09098
59607907  
00010596  00000-0  82463-4 0  9009
2 25544  51
6376 303
6172 0009096 215
2519 144
8042 15
72041062 35000


Satellite: ISS
Catalog Number: 25544
Epoch time:      09098
59607907   =   yrday
fracday
Element set:     900
Inclination:       51
6376  deg
RA of node:       303
6172  deg
Eccentricity:     
0009096     
Arg of perigee:   215
2519  deg
Mean anomaly:     144
8042  deg
Mean motion:   15
72041062  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3500
Checksum:              299


Coasting Arc #2 (Orbit 3515)
---------------------------------------

Vector Time (GMT): 2009/099/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3630285
94                 A    =         6725860
50  meter
 Y    =        2124955
63  meter          E    =           
0007614
 Z    =        5250697
08                 I    =           51
32395
 XDOT =      -3724
286679                 Wp   =          204
59881
 YDOT =       6733
021991  meter/sec      RA   =          298
01385  deg
 ZDOT =       -156
818586                 TA   =          246
85670
                                          MA   =          246
93694
                                          Ha   =            193
741  n
mi
                                          Hp   =            188
059

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11910386
96                 X    =         3580747
28
 Y    =        6971639
22  feet           Y    =         2165274
99  meter
 Z    =       17226696
45                 Z    =         5268212
73
 XDOT =     -12218
788318                 XDOT =       -3798
537855
 YDOT =      22089
967162  feet/sec       YDOT =        6690
959673  meter/sec
 ZDOT =       -514
496674                 ZDOT =        -175
092211

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13493488
45                 X    =         4112815
28
 Y    =       -2453762
89  feet           Y    =         -747906
93  meter
 Z    =       17295229
36                 Z    =         5271585
91
 XDOT =       5033
818522                 XDOT =        1534
307885
 YDOT =      23714
515257  feet/sec       YDOT =        7228
184250  meter/sec
 ZDOT =       -585
379249                 ZDOT =        -178
423595


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   09099
61319201  
00010596  00000-0  82463-4 0  9011
2 25544  51
6367 298
4078 0009171 217
7582 142
2937 15
71983744 35160


Satellite: ISS
Catalog Number: 25544
Epoch time:      09099
61319201   =   yrday
fracday
Element set:     901
Inclination:       51
6367  deg
RA of node:       298
4078  deg
Eccentricity:     
0009171     
Arg of perigee:   217
7582  deg
Mean anomaly:     142
2937  deg
Mean motion:   15
71983744  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3516
Checksum:              331


Coasting Arc #3 (Orbit 3530)
---------------------------------------

Vector Time (GMT): 2009/100/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2250219
46                 A    =         6737598
91  meter
 Y    =       -6331314
27  meter          E    =           
0001947
 Z    =        -483917
76                 I    =           51
35188
 XDOT =       4682
546077                 Wp   =           41
80917
 YDOT =       1208
137473  meter/sec      RA   =          292
86734  deg
 ZDOT =       5982
515329                 TA   =          312
91352
                                          MA   =          312
92986
                                          Ha   =            193
574  n
mi
                                          Hp   =            188
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7382609
77                 X    =         2323200
85
 Y    =      -20772028
45  feet           Y    =        -6305742
97  meter
 Z    =       -1587656
69                 Z    =         -472808
45
 XDOT =      15362
683981                 XDOT =        4639
626058
 YDOT =       3963
705621  feet/sec       YDOT =        1260
260753  meter/sec
 ZDOT =      19627
674965                 ZDOT =        6005
159154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8351178
01                 X    =        -2545439
06
 Y    =      -20405205
70  feet           Y    =        -6219506
70  meter
 Z    =       -1544717
76                 Z    =         -470829
97
 XDOT =      12516
044466                 XDOT =        3814
890353
 YDOT =      -6611
063593  feet/sec       YDOT =       -2015
052183  meter/sec
 ZDOT =      19716
165967                 ZDOT =        6009
487387


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   09100
56671842  
00010596  00000-0  82463-4 0  9021
2 25544  51
6372 293
5239 0009272 221
3463 138
6998 15
72060148 35310


Satellite: ISS
Catalog Number: 25544
Epoch time:      09100
56671842   =   yrday
fracday
Element set:     902
Inclination:       51
6372  deg
RA of node:       293
5239  deg
Eccentricity:     
0009272     
Arg of perigee:   221
3463  deg
Mean anomaly:     138
6998  deg
Mean motion:   15
72060148  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3531
Checksum:              311


Coasting Arc #4 (Orbit 3546)
---------------------------------------

Vector Time (GMT): 2009/101/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4344430
11                 A    =         6726039
98  meter
 Y    =          66715
77  meter          E    =           
0008679
 Z    =       -5140143
76                 I    =           51
30343
 XDOT =       1346
708556                 Wp   =          118
28548
 YDOT =      -7471
977450  meter/sec      RA   =          287
73975  deg
 ZDOT =      -1240
858982                 TA   =          139
81966
                                          MA   =          139
75546
                                          Ha   =            193
236  n
mi
                                          Hp   =            188
229

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14253379
63                 X    =        -4319882
97
 Y    =         218883
76  feet           Y    =           18270
94  meter
 Z    =      -16863988
70                 Z    =        -5161189
70
 XDOT =       4418
335157                 XDOT =        1436
189330
 YDOT =     -24514
361713  feet/sec       YDOT =       -7456
417488  meter/sec
 ZDOT =      -4071
059653                 ZDOT =       -1234
099027

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10232453
08                 X    =        -3118851
70
 Y    =        9783946
09  feet           Y    =         2982146
77  meter
 Z    =      -16946154
69                 Z    =        -5165187
95
 XDOT =     -12695
000243                 XDOT =       -3869
436074
 YDOT =     -20251
431818  feet/sec       YDOT =       -6172
636418  meter/sec
 ZDOT =      -4045
178621                 ZDOT =       -1232
970444


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   09101
58380068  
00010596  00000-0  82463-4 0  9032
2 25544  51
6376 288
3158 0009113 224
8829 135
1597 15
72092718 35476


Satellite: ISS
Catalog Number: 25544
Epoch time:      09101
58380068   =   yrday
fracday
Element set:     903
Inclination:       51
6376  deg
RA of node:       288
3158  deg
Eccentricity:     
0009113     
Arg of perigee:   224
8829  deg
Mean anomaly:     135
1597  deg
Mean motion:   15
72092718  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3547
Checksum:              328


Coasting Arc #5 (Orbit 3562)
---------------------------------------

Vector Time (GMT): 2009/102/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -79663
79                 A    =         6736357
80  meter
 Y    =        6515237
67  meter          E    =           
0013343
 Z    =        1674388
21                 I    =           51
32993
 XDOT =      -4986
719838                 Wp   =          155
05058
 YDOT =       1405
013318  meter/sec      RA   =          282
56848  deg
 ZDOT =      -5699
757999                 TA   =            6
36024
                                          MA   =            6
34332
                                          Ha   =            193
055  n
mi
                                          Hp   =            188
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -261364
14                 X    =         -160646
34
 Y    =       21375451
67  feet           Y    =         6513894
03  meter
 Z    =        5493399
63                 Z    =         1673804
47
 XDOT =     -16360
629389                 XDOT =       -4974
371513
 YDOT =       4609
623747  feet/sec       YDOT =        1349
317936  meter/sec
 ZDOT =     -18699
993435                 ZDOT =       -5723
953840

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14587933
05                 X    =         4446401
99
 Y    =       15626598
84  feet           Y    =         4762987
33  meter
 Z    =        5491566
50                 Z    =         1673829
47
 XDOT =      -7396
006078                 XDOT =       -2254
302653
 YDOT =      13514
476578  feet/sec       YDOT =        4119
212461  meter/sec
 ZDOT =     -18794
369144                 ZDOT =       -5728
523715


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   09102
60086699  
00010596  00000-0  82463-4 0  9040
2 25544  51
6371 283
1060 0009226 230
0632 129
9720 15
72106303 35635


Satellite: ISS
Catalog Number: 25544
Epoch time:      09102
60086699   =   yrday
fracday
Element set:     904
Inclination:       51
6371  deg
RA of node:       283
1060  deg
Eccentricity:     
0009226     
Arg of perigee:   230
0632  deg
Mean anomaly:     129
9720  deg
Mean motion:   15
72106303  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3563
Checksum:              285


Coasting Arc #6 (Orbit 3578)
---------------------------------------

Vector Time (GMT): 2009/103/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4147790
56                 A    =         6727572
73  meter
 Y    =       -2348473
56  meter          E    =           
0009177
 Z    =        4752300
51                 I    =           51
29636
 XDOT =       1124
501329                 Wp   =          186
49921
 YDOT =       7169
949419  meter/sec      RA   =          277
45930  deg
 ZDOT =       2553
246225                 TA   =          238
28919
                                          MA   =          238
37869
                                          Ha   =            192
833  n
mi
                                          Hp   =            188
695

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13608236
73                 X    =         4150657
22
 Y    =       -7704965
74  feet           Y    =        -2302074
59  meter
 Z    =       15591537
09                 Z    =         4772457
64
 XDOT =       3689
308821                 XDOT =        1031
838821
 YDOT =      23523
456098  feet/sec       YDOT =        7182
006106  meter/sec
 ZDOT =       8376
792077                 ZDOT =        2558
484146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4162141
78                 X    =         1268620
81
 Y    =      -14992388
45  feet           Y    =        -4569680
00  meter
 Z    =       15670082
87                 Z    =         4776241
26
 XDOT =      18066
236165                 XDOT =        5506
588783
 YDOT =      13821
869000  feet/sec       YDOT =        4212
905671  meter/sec
 ZDOT =       8397
736179                 ZDOT =        2559
629987


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   09103
61791899  
00010596  00000-0  82463-4 0  9058
2 25544  51
6379 277
8970 0009253 233
7843 126
2464 15
72144489 35796


Satellite: ISS
Catalog Number: 25544
Epoch time:      09103
61791899   =   yrday
fracday
Element set:     905
Inclination:       51
6379  deg
RA of node:       277
8970  deg
Eccentricity:     
0009253     
Arg of perigee:   233
7843  deg
Mean anomaly:     126
2464  deg
Mean motion:   15
72144489  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3579
Checksum:              354


Coasting Arc #7 (Orbit 3593)
---------------------------------------

Vector Time (GMT): 2009/104/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1974349
87                 A    =         6734138
97  meter
 Y    =       -5820581
64  meter          E    =           
0004372
 Z    =       -2752071
58                 I    =           51
31713
 XDOT =       4252
273842                 Wp   =          234
79471
 YDOT =      -3864
947992  meter/sec      RA   =          272
27129  deg
 ZDOT =       5115
478088                 TA   =           93
63709
                                          MA   =           93
58709
                                          Ha   =            192
671  n
mi
                                          Hp   =            188
915

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6477525
83                 X    =        -1895747
23
 Y    =      -19096396
47  feet           Y    =        -5842220
42  meter
 Z    =       -9029106
22                 Z    =        -2761472
27
 XDOT =      13951
029665                 XDOT =        4270
326015
 YDOT =     -12680
275563  feet/sec       YDOT =       -3817
295779  meter/sec
 ZDOT =      16783
064594                 ZDOT =        5136
179566

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18168079
99                 X    =        -5537630
78
 Y    =       -8710915
21  feet           Y    =        -2655086
96  meter
 Z    =       -9066216
63                 Z    =        -2763382
83
 XDOT =        -63
471753                 XDOT =         -19
346190
 YDOT =     -17447
024551  feet/sec       YDOT =       -5317
853083  meter/sec
 ZDOT =      16863
635191                 ZDOT =        5140
036006


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   09104
57139231  
00010596  00000-0  82463-4 0  9061
2 25544  51
6391 273
0142 0009123 236
9965 123
0320 15
72147917 35947


Satellite: ISS
Catalog Number: 25544
Epoch time:      09104
57139231   =   yrday
fracday
Element set:     906
Inclination:       51
6391  deg
RA of node:       273
0142  deg
Eccentricity:     
0009123     
Arg of perigee:   236
9965  deg
Mean anomaly:     123
0320  deg
Mean motion:   15
72147917  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3594
Checksum:              298


Coasting Arc #8 (Orbit 3609)
---------------------------------------

Vector Time (GMT): 2009/105/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3109804
87                 A    =         6729879
00  meter
 Y    =        4295785
85  meter          E    =           
0001723
 Z    =       -4141679
90                 I    =           51
30310
 XDOT =      -3254
739841                 Wp   =          199
11550
 YDOT =      -5916
596120  meter/sec      RA   =          267
17503  deg
 ZDOT =      -3694
074929                 TA   =           32
94315
                                          MA   =           32
93241
                                          Ha   =            192
311  n
mi
                                          Hp   =            189
188

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10202771
87                 X    =        -3137490
29
 Y    =       14093785
60  feet           Y    =         4260855
51  meter
 Z    =      -13588188
65                 Z    =        -4156854
55
 XDOT =     -10678
280318                 XDOT =       -3170
392325
 YDOT =     -19411
404593  feet/sec       YDOT =       -5952
520811  meter/sec
 ZDOT =     -12119
668402                 ZDOT =       -3709
681814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3335648
21                 X    =         1016705
58
 Y    =       17029356
89  feet           Y    =         5190547
98  meter
 Z    =      -13647148
87                 Z    =        -4159650
98
 XDOT =     -20167
713072                 XDOT =       -6147
118944
 YDOT =      -5808
304252  feet/sec       YDOT =       -1770
371136  meter/sec
 ZDOT =     -12181
028274                 ZDOT =       -3712
777418


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   09105
58841471  
00010596  00000-0  82463-4 0  9070
2 25544  51
6391 267
8059 0009125 241
7309 118
2932 15
72169280 36104


Satellite: ISS
Catalog Number: 25544
Epoch time:      09105
58841471   =   yrday
fracday
Element set:     907
Inclination:       51
6391  deg
RA of node:       267
8059  deg
Eccentricity:     
0009125     
Arg of perigee:   241
7309  deg
Mean anomaly:     118
2932  deg
Mean motion:   15
72169280  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3610
Checksum:              314


Coasting Arc #9 (Orbit 3625)
---------------------------------------

Vector Time (GMT): 2009/106/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3579934
25                 A    =         6731479
04  meter
 Y    =        4360303
36  meter          E    =           
0004412
 Z    =        3666752
62                 I    =           51
31127
 XDOT =      -2661
238301                 Wp   =          127
45461
 YDOT =       5803
290435  meter/sec      RA   =          261
97837  deg
 ZDOT =      -4301
834973                 TA   =            8
26541
                                          MA   =            8
25814
                                          Ha   =            192
127  n
mi
                                          Hp   =            189
411

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11745191
11                 X    =         3513098
07
 Y    =       14305457
23  feet           Y    =         4399962
50  meter
 Z    =       12030028
27                 Z    =         3683981
73
 XDOT =      -8731
096789                 XDOT =       -2705
036283
 YDOT =      19039
666780  feet/sec       YDOT =        5773
286113  meter/sec
 ZDOT =     -14113
631801                 ZDOT =       -4314
869576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18439561
41                 X    =         5620378
32
 Y    =         973281
73  feet           Y    =          296656
27  meter
 Z    =       12097623
68                 Z    =         3687355
70
 XDOT =       8351
980056                 XDOT =        2545
683521
 YDOT =      17857
917217  feet/sec       YDOT =        5443
093168  meter/sec
 ZDOT =     -14164
127537                 ZDOT =       -4317
226073


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   09106
60542258  
00010596  00000-0  82463-4 0  9086
2 25544  51
6391 262
5969 0009100 245
2471 114
7745 15
72172411 36268


Satellite: ISS
Catalog Number: 25544
Epoch time:      09106
60542258   =   yrday
fracday
Element set:     908
Inclination:       51
6391  deg
RA of node:       262
5969  deg
Eccentricity:     
0009100     
Arg of perigee:   245
2471  deg
Mean anomaly:     114
7745  deg
Mean motion:   15
72172411  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3626
Checksum:              304


Coasting Arc #10 (Orbit 3641)
---------------------------------------

Vector Time (GMT): 2009/107/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1427164
52                 A    =         6732289
55  meter
 Y    =       -5666842
78  meter          E    =           
0005071
 Z    =        3342461
93                 I    =           51
32101
 XDOT =       4723
844688                 Wp   =          127
32177
 YDOT =       3927
363357  meter/sec      RA   =          256
88474  deg
 ZDOT =       4633
649469                 TA   =          272
17169
                                          MA   =          272
22976
                                          Ha   =            191
876  n
mi
                                          Hp   =            189
490

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4682298
29                 X    =         1474188
94
 Y    =      -18592003
86  feet           Y    =        -5650620
49  meter
 Z    =       10966082
45                 Z    =         3349509
28
 XDOT =      15498
178110                 XDOT =        4657
067709
 YDOT =      12885
050384  feet/sec       YDOT =        3979
814736  meter/sec
 ZDOT =      15202
262037                 ZDOT =        4656
435761

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10931351
87                 X    =        -3331876
05
 Y    =      -15732024
21  feet           Y    =        -4795120
98  meter
 Z    =       10993200
16                 Z    =         3350727
41
 XDOT =      18701
188486                 XDOT =        5700
122251
 YDOT =      -2291
107024  feet/sec       YDOT =        -698
329421  meter/sec
 ZDOT =      15291
540540                 ZDOT =        4660
861557


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   09107
62241216  
00010596  00000-0  82463-4 0  9090
2 25544  51
6401 257
3878 0009160 249
7393 110
2785 15
72251350 36422


Satellite: ISS
Catalog Number: 25544
Epoch time:      09107
62241216   =   yrday
fracday
Element set:     909
Inclination:       51
6401  deg
RA of node:       257
3878  deg
Eccentricity:     
0009160     
Arg of perigee:   249
7393  deg
Mean anomaly:     110
2785  deg
Mean motion:   15
72251350  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3642
Checksum:              302


Coasting Arc #11 (Orbit 3656)
---------------------------------------

Vector Time (GMT): 2009/108/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4497923
93                 A    =         6728748
85  meter
 Y    =       -2418942
04  meter          E    =           
0005754
 Z    =       -4384268
64                 I    =           51
31685
 XDOT =        496
787445                 Wp   =          180
45422
 YDOT =      -6929
195450  meter/sec      RA   =          251
69120  deg
 ZDOT =       3307
691740                 TA   =          122
98914
                                          MA   =          122
93383
                                          Ha   =            191
588  n
mi
                                          Hp   =            189
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14756968
27                 X    =        -4449242
62
 Y    =       -7936161
55  feet           Y    =        -2468968
29  meter
 Z    =      -14384083
46                 Z    =        -4406001
30
 XDOT =       1629
880069                 XDOT =         558
165770
 YDOT =     -22733
580874  feet/sec       YDOT =       -6923
296880  meter/sec
 ZDOT =      10852
007022                 ZDOT =        3310
254264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15540214
43                 X    =        -4736657
36
 Y    =        6066148
73  feet           Y    =         1848962
13  meter
 Z    =      -14469146
65                 Z    =        -4410195
90
 XDOT =     -15890
648287                 XDOT =       -4843
469598
 YDOT =     -14757
007711  feet/sec       YDOT =       -4497
935950  meter/sec
 ZDOT =      10861
509305                 ZDOT =        3310
588036


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   09108
57582886  
00010596  00000-0  82463-4 0  9108
2 25544  51
6399 252
5052 0009105 254
3727 105
6431 15
72241550 36574


Satellite: ISS
Catalog Number: 25544
Epoch time:      09108
57582886   =   yrday
fracday
Element set:     910
Inclination:       51
6399  deg
RA of node:       252
5052  deg
Eccentricity:     
0009105     
Arg of perigee:   254
3727  deg
Mean anomaly:     105
6431  deg
Mean motion:   15
72241550  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3657
Checksum:              312


Coasting Arc #12 (Orbit 3672)
---------------------------------------

Vector Time (GMT): 2009/109/13:34:46
084
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         600833
83                 A    =         6734584
71  meter
 Y    =        6252221
25  meter          E    =           
0007382
 Z    =       -2416251
61                 I    =           51
34743
 XDOT =      -5325
178469                 Wp   =          220
88574
 YDOT =      -1552
938833  meter/sec      RA   =          246
59173  deg
 ZDOT =      -5338
820098                 TA   =          346
48520
                                          MA   =          346
50496
                                          Ha   =            191
319  n
mi
                                          Hp   =            190
016

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1971239
62                 X    =          542613
53
 Y    =       20512536
90  feet           Y    =         6258614
55  meter
 Z    =       -7927334
69                 Z    =        -2413474
31
 XDOT =     -17471
057969                 XDOT =       -5281
482400
 YDOT =      -5094
943679  feet/sec       YDOT =       -1612
243880  meter/sec
 ZDOT =     -17515
813969                 ZDOT =       -5364
583685

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17154155
20                 X    =         5228586
50
 Y    =       11426467
64  feet           Y    =         3482787
34  meter
 Z    =       -7916020
96                 Z    =        -2412803
19
 XDOT =     -14108
165182                 XDOT =       -4300
168747
 YDOT =       8967
286788  feet/sec       YDOT =        2733
229013  meter/sec
 ZDOT =     -17616
565355                 ZDOT =       -5369
529120


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   09109
59279034  
00010596  00000-0  82463-4 0  9110
2 25544  51
6402 247
2958 0009044 258
4338 101
5809 15
72267270 36739


Satellite: ISS
Catalog Number: 25544
Epoch time:      09109
59279034   =   yrday
fracday
Element set:     911
Inclination:       51
6402  deg
RA of node:       247
2958  deg
Eccentricity:     
0009044     
Arg of perigee:   258
4338  deg
Mean anomaly:     101
5809  deg
Mean motion:   15
72267270  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3673
Checksum:              319

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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