Date: March 19th 2009

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) : 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 3160)
---------------------------------------

Vector Time (GMT): 2009/077/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5090588
96                 A    =         6731840
65  meter
 Y    =        1278392
49  meter          E    =           
0017775
 Z    =       -4234416
91                 I    =           51
90061
 XDOT =       1367
258186                 Wp   =          123
84208
 YDOT =       6622
086070  meter/sec      RA   =           53
33696  deg
 ZDOT =       3644
177932                 TA   =          183
22810
                                          MA   =          183
23959
                                          Ha   =            197
372  n
mi
                                          Hp   =            184
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16701407
34                 X    =         5096485
32
 Y    =        4194201
07  feet           Y    =         1335351
30  meter
 Z    =      -13892443
92                 Z    =        -4209672
68
 XDOT =       4485
755205                 XDOT =        1275
404647
 YDOT =      21726
004166  feet/sec       YDOT =        6636
862045  meter/sec
 ZDOT =      11955
964345                 ZDOT =        3650
596780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17154320
50                 X    =        -5228636
89
 Y    =       -2221619
82  feet           Y    =         -677149
72  meter
 Z    =      -13795724
76                 Z    =        -4204936
91
 XDOT =      -7065
921893                 XDOT =       -2153
692993
 YDOT =     -19817
218761  feet/sec       YDOT =       -6040
288278  meter/sec
 ZDOT =      11981
488954                 ZDOT =        3651
957833


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   09077
04181804  
00010596  00000-0  82463-4 0  9009
2 25544  51
6403  53
9169 0010078 135
3244 224
8732 15
71437771 31614


Satellite: ISS
Catalog Number: 25544
Epoch time:      09077
04181804   =   yrday
fracday
Element set:     900
Inclination:       51
6403  deg
RA of node:        53
9169  deg
Eccentricity:     
0010078     
Arg of perigee:   135
3244  deg
Mean anomaly:     224
8732  deg
Mean motion:   15
71437771  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3161
Checksum:              293


Coasting Arc #2 (Orbit 3176)
---------------------------------------

Vector Time (GMT): 2009/078/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2473655
45                 A    =         6736614
28  meter
 Y    =       -5736366
22  meter          E    =           
0015246
 Z    =       -2513128
28                 I    =           51
89844
 XDOT =       5545
304286                 Wp   =          135
59402
 YDOT =        -66
873119  meter/sec      RA   =           48
28477  deg
 ZDOT =      -5335
567639                 TA   =           72
71890
                                          MA   =           72
55214
                                          Ha   =            197
242  n
mi
                                          Hp   =            184
827

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8115667
48                 X    =        -2397118
38
 Y    =      -18820099
15  feet           Y    =        -5763600
19  meter
 Z    =       -8245171
54                 Z    =        -2524959
16
 XDOT =      18193
255530                 XDOT =        5571
558923
 YDOT =       -219
399997  feet/sec       YDOT =          -4
715617  meter/sec
 ZDOT =     -17505
143174                 ZDOT =       -5308
565023

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10497925
06                 X    =         3199767
56
 Y    =       17580762
88  feet           Y    =         5358616
53  meter
 Z    =       -8291766
42                 Z    =        -2527330
41
 XDOT =     -16820
598307                 XDOT =       -5126
918364
 YDOT =       1883
809324  feet/sec       YDOT =         574
185082  meter/sec
 ZDOT =     -17399
694314                 ZDOT =       -5303
426827


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   09078
05929528  
00010596  00000-0  82463-4 0  9015
2 25544  51
6402  48
7107 0010055 139
1814 221
0103 15
71468682 31770


Satellite: ISS
Catalog Number: 25544
Epoch time:      09078
05929528   =   yrday
fracday
Element set:     901
Inclination:       51
6402  deg
RA of node:        48
7107  deg
Eccentricity:     
0010055     
Arg of perigee:   139
1814  deg
Mean anomaly:     221
0103  deg
Mean motion:   15
71468682  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3177
Checksum:              295


Coasting Arc #3 (Orbit 3192)
---------------------------------------

Vector Time (GMT): 2009/079/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4293845
22                 A    =         6728695
93  meter
 Y    =        1348485
17  meter          E    =           
0012065
 Z    =        4991075
86                 I    =           51
85148
 XDOT =      -4238
282617                 Wp   =          112
61622
 YDOT =      -6119
144552  meter/sec      RA   =           43
14787  deg
 ZDOT =      -1993
692230                 TA   =          356
58709
                                          MA   =          356
59531
                                          Ha   =            197
377  n
mi
                                          Hp   =            184
951

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14087418
71                 X    =        -4332850
54
 Y    =        4424163
94  feet           Y    =         1300250
95  meter
 Z    =       16374920
80                 Z    =         4970121
82
 XDOT =     -13905
126697                 XDOT =       -4159
857440
 YDOT =     -20075
933570  feet/sec       YDOT =       -6166
101059  meter/sec
 ZDOT =      -6540
985005                 ZDOT =       -2014
090891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13358046
25                 X    =         4071532
50
 Y    =       -6500889
31  feet           Y    =        -1981471
06  meter
 Z    =       16293178
40                 Z    =         4966160
78
 XDOT =      16246
684885                 XDOT =        4951
989553
 YDOT =      16795
513328  feet/sec       YDOT =        5119
272463  meter/sec
 ZDOT =      -6621
064537                 ZDOT =       -2018
100471


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   09079
07676044  
00010596  00000-0  82463-4 0  9021
2 25544  51
6408  43
5055 0010131 142
5838 217
6031 15
71454565 31934


Satellite: ISS
Catalog Number: 25544
Epoch time:      09079
07676044   =   yrday
fracday
Element set:     902
Inclination:       51
6408  deg
RA of node:        43
5055  deg
Eccentricity:     
0010131     
Arg of perigee:   142
5838  deg
Mean anomaly:     217
6031  deg
Mean motion:   15
71454565  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3193
Checksum:              295


Coasting Arc #4 (Orbit 3208)
---------------------------------------

Vector Time (GMT): 2009/080/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4764241
00                 A    =         6738843
74  meter
 Y    =        4669799
26  meter          E    =           
0016826
 Z    =         940470
27                 I    =           51
86487
 XDOT =      -3966
709280                 Wp   =           91
84538
 YDOT =       2829
569076  meter/sec      RA   =           38
07206  deg
 ZDOT =       5952
965566                 TA   =          278
37735
                                          MA   =          278
56807
                                          Ha   =            197
058  n
mi
                                          Hp   =            185
007

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15630711
94                 X    =         4707099
86
 Y    =       15320863
72  feet           Y    =         4722756
33  meter
 Z    =        3085532
39                 Z    =          963475
65
 XDOT =     -13014
138059                 XDOT =       -4026
973223
 YDOT =       9283
363109  feet/sec       YDOT =        2784
874321  meter/sec
 ZDOT =      19530
726922                 ZDOT =        5933
549053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17951156
09                 X    =        -5471512
38
 Y    =      -12499579
71  feet           Y    =        -3809871
89  meter
 Z    =        3175694
13                 Z    =          967951
57
 XDOT =      10481
366075                 XDOT =        3194
720380
 YDOT =     -10035
602912  feet/sec       YDOT =       -3058
851768  meter/sec
 ZDOT =      19455
087803                 ZDOT =        5929
910762


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   09080
09420859  
00010596  00000-0  82463-4 0  9037
2 25544  51
6417  38
2998 0010076 146
7810 213
3986 15
71517803 32090


Satellite: ISS
Catalog Number: 25544
Epoch time:      09080
09420859   =   yrday
fracday
Element set:     903
Inclination:       51
6417  deg
RA of node:        38
2998  deg
Eccentricity:     
0010076     
Arg of perigee:   146
7810  deg
Mean anomaly:     213
3986  deg
Mean motion:   15
71517803  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3209
Checksum:              317


Coasting Arc #5 (Orbit 3223)
---------------------------------------

Vector Time (GMT): 2009/081/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2439961
00                 A    =         6727128
38  meter
 Y    =       -3383540
73  meter          E    =           
0021931
 Z    =       -5294916
79                 I    =           51
80175
 XDOT =       6365
791368                 Wp   =          114
15343
 YDOT =       4296
199664  meter/sec      RA   =           32
95881  deg
 ZDOT =        179
900016                 TA   =          157
60217
                                          MA   =          157
50626
                                          Ha   =            196
915  n
mi
                                          Hp   =            185
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8005121
40                 X    =         2503336
36
 Y    =      -11100855
43  feet           Y    =        -3355901
63  meter
 Z    =      -17371774
24                 Z    =        -5282909
49
 XDOT =      20885
142284                 XDOT =        6316
403518
 YDOT =      14095
143255  feet/sec       YDOT =        4367
109522  meter/sec
 ZDOT =        590
223150                 ZDOT =         210
704376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5926044
89                 X    =        -1806258
48
 Y    =       12402100
36  feet           Y    =         3780160
19  meter
 Z    =      -17325108
91                 Z    =        -5280693
20
 XDOT =     -22212
688720                 XDOT =       -6770
427522
 YDOT =      -9583
188108  feet/sec       YDOT =       -2920
955735  meter/sec
 ZDOT =        710
818115                 ZDOT =         216
657361


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   09081
04805529  
00010596  00000-0  82463-4 0  9045
2 25544  51
6419  33
4201 0009969 150
2534 209
9197 15
71545927 32248


Satellite: ISS
Catalog Number: 25544
Epoch time:      09081
04805529   =   yrday
fracday
Element set:     904
Inclination:       51
6419  deg
RA of node:        33
4201  deg
Eccentricity:     
0009969     
Arg of perigee:   150
2534  deg
Mean anomaly:     209
9197  deg
Mean motion:   15
71545927  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3224
Checksum:              313


Coasting Arc #6 (Orbit 3239)
---------------------------------------

Vector Time (GMT): 2009/082/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6136762
74                 A    =         6739033
94  meter
 Y    =       -2680303
49  meter          E    =           
0022706
 Z    =         631829
90                 I    =           51
81660
 XDOT =       1386
194353                 Wp   =          139
39859
 YDOT =      -4615
432624  meter/sec      RA   =           27
84930  deg
 ZDOT =      -6012
342593                 TA   =           33
73794
                                          MA   =           33
59364
                                          Ha   =            196
848  n
mi
                                          Hp   =            185
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20133736
02                 X    =        -6109404
31
 Y    =       -8793646
61  feet           Y    =        -2748775
33  meter
 Z    =        2072932
74                 Z    =          602084
57
 XDOT =       4547
881735                 XDOT =        1466
908355
 YDOT =     -15142
495484  feet/sec       YDOT =       -4599
480560  meter/sec
 ZDOT =     -19725
533442                 ZDOT =       -6005
412142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21500609
16                 X    =         6553385
67
 Y    =        4570358
82  feet           Y    =         1393045
37  meter
 Z    =        1956584
49                 Z    =          596366
95
 XDOT =      -1193
716758                 XDOT =        -363
844868
 YDOT =      14202
421764  feet/sec       YDOT =        4328
898154  meter/sec
 ZDOT =     -19698
779542                 ZDOT =       -6004
188004


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   09082
06547834  
00010596  00000-0  82463-4 0  9051
2 25544  51
6422  28
2138 0010034 154
5401 205
6257 15
71542559 32404


Satellite: ISS
Catalog Number: 25544
Epoch time:      09082
06547834   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:        28
2138  deg
Eccentricity:     
0010034     
Arg of perigee:   154
5401  deg
Mean anomaly:     205
6257  deg
Mean motion:   15
71542559  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3240
Checksum:              285


Coasting Arc #7 (Orbit 3255)
---------------------------------------

Vector Time (GMT): 2009/083/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         131034
83                 A    =         6727763
63  meter
 Y    =        4400487
70  meter          E    =           
0014325
 Z    =        5083614
34                 I    =           51
75362
 XDOT =      -7335
030509                 Wp   =          147
20759
 YDOT =      -1682
789519  meter/sec      RA   =           22
76205  deg
 ZDOT =       1631
781989                 TA   =          287
06026
                                          MA   =          287
21714
                                          Ha   =            196
610  n
mi
                                          Hp   =            185
399

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         429904
28                 X    =           57123
08
 Y    =       14437295
61  feet           Y    =         4401540
23  meter
 Z    =       16678524
75                 Z    =         5084070
96
 XDOT =     -24065
060726                 XDOT =       -7323
594939
 YDOT =      -5520
962989  feet/sec       YDOT =       -1764
750013  meter/sec
 ZDOT =       5353
615449                 ZDOT =        1596
176731

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3466709
50                 X    =        -1056653
05
 Y    =      -14019016
21  feet           Y    =        -4272996
14  meter
 Z    =       16680606
09                 Z    =         5084248
74
 XDOT =      23697
294764                 XDOT =        7222
935444
 YDOT =        398
861953  feet/sec       YDOT =         121
573123  meter/sec
 ZDOT =       5214
453772                 ZDOT =        1589
365510


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   09083
08288547  
00010596  00000-0  82463-4 0  9068
2 25544  51
6431  23
0080 0009932 158
5355 201
6225 15
71608087 32567


Satellite: ISS
Catalog Number: 25544
Epoch time:      09083
08288547   =   yrday
fracday
Element set:     906
Inclination:       51
6431  deg
RA of node:        23
0080  deg
Eccentricity:     
0009932     
Arg of perigee:   158
5355  deg
Mean anomaly:     201
6225  deg
Mean motion:   15
71608087  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3256
Checksum:              305


Coasting Arc #8 (Orbit 3270)
---------------------------------------

Vector Time (GMT): 2009/084/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6379705
03                 A    =         6737134
91  meter
 Y    =         234105
18  meter          E    =           
0008536
 Z    =       -2167358
66                 I    =           51
75718
 XDOT =       1680
934170                 Wp   =          121
38669
 YDOT =       5089
659972  meter/sec      RA   =           17
62127  deg
 ZDOT =       5509
204024                 TA   =          214
45123
                                          MA   =          214
50660
                                          Ha   =            196
541  n
mi
                                          Hp   =            185
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20930790
78                 X    =         6387141
64
 Y    =         768061
60  feet           Y    =          305488
11  meter
 Z    =       -7110756
75                 Z    =        -2136348
22
 XDOT =       5514
875887                 XDOT =        1597
133262
 YDOT =      16698
359489  feet/sec       YDOT =        5107
989191  meter/sec
 ZDOT =      18074
816351                 ZDOT =        5517
165854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20567598
92                 X    =        -6269004
15
 Y    =        4167679
31  feet           Y    =         1270308
65  meter
 Z    =       -6989642
82                 Z    =        -2130443
13
 XDOT =      -8868
730504                 XDOT =       -2703
189058
 YDOT =     -13465
958028  feet/sec       YDOT =       -4104
424007  meter/sec
 ZDOT =      18106
252496                 ZDOT =        5518
785761


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   09084
03669432  
00010596  00000-0  82463-4 0  9071
2 25544  51
6434  18
1281 0009750 161
7822 198
3691 15
71567098 32713


Satellite: ISS
Catalog Number: 25544
Epoch time:      09084
03669432   =   yrday
fracday
Element set:     907
Inclination:       51
6434  deg
RA of node:        18
1281  deg
Eccentricity:     
0009750     
Arg of perigee:   161
7822  deg
Mean anomaly:     198
3691  deg
Mean motion:   15
71567098  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3271
Checksum:              324


Coasting Arc #9 (Orbit 3286)
---------------------------------------

Vector Time (GMT): 2009/085/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2752626
12                 A    =         6730315
80  meter
 Y    =       -4224432
42  meter          E    =           
0013065
 Z    =       -4464642
91                 I    =           51
70628
 XDOT =       6891
779255                 Wp   =          117
86953
 YDOT =      -1083
703540  meter/sec      RA   =           12
55329  deg
 ZDOT =      -3236
818318                 TA   =          119
76699
                                          MA   =          119
63697
                                          Ha   =            196
403  n
mi
                                          Hp   =            185
697

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9030925
61                 X    =        -2683494
82
 Y    =      -13859686
42  feet           Y    =        -4254827
85  meter
 Z    =      -14647778
58                 Z    =        -4477846
77
 XDOT =      22610
824329                 XDOT =        6919
109060
 YDOT =      -3555
457808  feet/sec       YDOT =       -1006
483194  meter/sec
 ZDOT =     -10619
482672                 ZDOT =       -3203
271591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12138741
02                 X    =         3699888
26
 Y    =       11170407
41  feet           Y    =         3404740
18  meter
 Z    =      -14699622
69                 Z    =        -4480444
99
 XDOT =     -20238
862501                 XDOT =       -6168
805290
 YDOT =       8247
605871  feet/sec       YDOT =        2513
870270  meter/sec
 ZDOT =     -10488
560470                 ZDOT =       -3196
913231


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   09085
05407562  
00010596  00000-0  82463-4 0  9089
2 25544  51
6435  12
9224 0009902 166
1138 194
0298 15
71600117 32874


Satellite: ISS
Catalog Number: 25544
Epoch time:      09085
05407562   =   yrday
fracday
Element set:     908
Inclination:       51
6435  deg
RA of node:        12
9224  deg
Eccentricity:     
0009902     
Arg of perigee:   166
1138  deg
Mean anomaly:     194
0298  deg
Mean motion:   15
71600117  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3287
Checksum:              303


Coasting Arc #10 (Orbit 3302)
---------------------------------------

Vector Time (GMT): 2009/086/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5395412
21                 A    =         6733846
43  meter
 Y    =        2047405
64  meter          E    =           
0017234
 Z    =        3448524
86                 I    =           51
68902
 XDOT =      -4534
056657                 Wp   =          123
02119
 YDOT =      -4232
202796  meter/sec      RA   =            7
39206  deg
 ZDOT =      -4573
917476                 TA   =           16
15411
                                          MA   =           16
09923
                                          Ha   =            196
375  n
mi
                                          Hp   =            185
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17701483
63                 X    =        -5434658
03
 Y    =        6717210
09  feet           Y    =         1986851
91  meter
 Z    =       11314057
92                 Z    =         3422218
29
 XDOT =     -14875
513968                 XDOT =       -4464
175109
 YDOT =     -13885
179776  feet/sec       YDOT =       -4282
515007  meter/sec
 ZDOT =     -15006
290933                 ZDOT =       -4595
773838

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15320715
23                 X    =         4669754
00
 Y    =      -11227190
51  feet           Y    =        -3422047
67  meter
 Z    =       11211477
11                 Z    =         3417258
22
 XDOT =      17146
507878                 XDOT =        5226
255601
 YDOT =       8303
693718  feet/sec       YDOT =        2530
965845  meter/sec
 ZDOT =     -15091
915101                 ZDOT =       -4600
015723


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   09086
07144310  
00010596  00000-0  82463-4 0  9092
2 25544  51
6434   7
7170 0009826 168
8665 191
2716 15
71632803 33034


Satellite: ISS
Catalog Number: 25544
Epoch time:      09086
07144310   =   yrday
fracday
Element set:     909
Inclination:       51
6434  deg
RA of node:         7
7170  deg
Eccentricity:     
0009826     
Arg of perigee:   168
8665  deg
Mean anomaly:     191
2716  deg
Mean motion:   15
71632803  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3303
Checksum:              306


Coasting Arc #11 (Orbit 3318)
---------------------------------------

Vector Time (GMT): 2009/087/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4988443
40                 A    =         6733572
78  meter
 Y    =        2929254
98  meter          E    =           
0016839
 Z    =        3444422
39                 I    =           51
65940
 XDOT =      -5171
517403                 Wp   =          126
35601
 YDOT =       3405
711517  meter/sec      RA   =            2
32801  deg
 ZDOT =       4568
153515                 TA   =          274
35667
                                          MA   =          274
54905
                                          Ha   =            196
049  n
mi
                                          Hp   =            185
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16366284
11                 X    =         4938584
69
 Y    =        9610416
61  feet           Y    =         2984760
19  meter
 Z    =       11300598
40                 Z    =         3468535
11
 XDOT =     -16966
920612                 XDOT =       -5231
407744
 YDOT =      11173
594217  feet/sec       YDOT =        3347
546124  meter/sec
 ZDOT =      14987
380300                 ZDOT =        4542
884292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18359674
27                 X    =        -5596028
72
 Y    =       -4582206
74  feet           Y    =        -1396656
61  meter
 Z    =       11394938
76                 Z    =         3473177
33
 XDOT =      12840
910775                 XDOT =        3913
909604
 YDOT =     -14220
259728  feet/sec       YDOT =       -4334
335165  meter/sec
 ZDOT =      14888
942431                 ZDOT =        4538
149653


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   09087
08879455  
00010596  00000-0  82463-4 0  9101
2 25544  51
6435   2
5108 0009811 173
5483 186
5807 15
71676824 33190


Satellite: ISS
Catalog Number: 25544
Epoch time:      09087
08879455   =   yrday
fracday
Element set:     910
Inclination:       51
6435  deg
RA of node:         2
5108  deg
Eccentricity:     
0009811     
Arg of perigee:   173
5483  deg
Mean anomaly:     186
5807  deg
Mean motion:   15
71676824  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3319
Checksum:              331


Coasting Arc #12 (Orbit 3333)
---------------------------------------

Vector Time (GMT): 2009/088/00:46:46
579
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3467337
68                 A    =         6730251
73  meter
 Y    =       -3696127
82  meter          E    =           
0016036
 Z    =       -4443886
27                 I    =           51
61793
 XDOT =       6585
113361                 Wp   =          143
82585
 YDOT =       2255
316519  meter/sec      RA   =          357
16196  deg
 ZDOT =       3255
474141                 TA   =          158
92162
                                          MA   =          158
85545
                                          Ha   =            195
925  n
mi
                                          Hp   =            186
207

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11375779
80                 X    =         3529998
55
 Y    =      -12126403
60  feet           Y    =        -3657003
94  meter
 Z    =      -14579679
35                 Z    =        -4426889
32
 XDOT =      21604
702628                 XDOT =        6543
589923
 YDOT =       7399
332413  feet/sec       YDOT =        2328
723127  meter/sec
 ZDOT =      10680
689440                 ZDOT =        3287
363987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7284354
58                 X    =        -2220271
28
 Y    =       15010659
63  feet           Y    =         4575249
06  meter
 Z    =      -14513557
66                 Z    =        -4423732
38
 XDOT =     -21675
940719                 XDOT =       -6606
826731
 YDOT =        -49
912869  feet/sec       YDOT =         -15
213442  meter/sec
 ZDOT =      10805
344590                 ZDOT =        3293
469031


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   09088
04255061  
00010596  00000-0  82463-4 0  9110
2 25544  51
6428 357
6307 0009725 176
5009 183
6223 15
71706859 33347


Satellite: ISS
Catalog Number: 25544
Epoch time:      09088
04255061   =   yrday
fracday
Element set:     911
Inclination:       51
6428  deg
RA of node:       357
6307  deg
Eccentricity:     
0009725     
Arg of perigee:   176
5009  deg
Mean anomaly:     183
6223  deg
Mean motion:   15
71706859  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3334
Checksum:              317

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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