Date: March 23rd 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


080/15:37:31 822 1 4 -1 4 6 4
N/A -4 0 -0 2 197 0
000/02:29:03 644 -4 8 -6 3 185 5

Coasting Arc #1 (Orbit 3203)
---------------------------------------

Vector Time (GMT): 2009/079/18:27:19
449
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5655208
13                 A    =         6734128
05  meter
 Y    =        1075888
98  meter          E    =           
0012913
 Z    =       -3510474
49                 I    =           51
85413
 XDOT =       1672
322178                 Wp   =          124
89010
 YDOT =       5976
822289  meter/sec      RA   =           39
38806  deg
 ZDOT =       4530
310956                 TA   =          193
65547
                                          MA   =          193
69043
                                          Ha   =            196
807  n
mi
                                          Hp   =            185
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18553832
45                 X    =         5659810
08
 Y    =        3529819
49  feet           Y    =         1139154
41  meter
 Z    =      -11517304
74                 Z    =        -3482990
71
 XDOT =       5486
621320                 XDOT =        1583
356918
 YDOT =      19608
997010  feet/sec       YDOT =        5995
025914  meter/sec
 ZDOT =      14863
224920                 ZDOT =        4538
218665

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2062185
97                 X    =          628554
28
 Y    =      -18839169
29  feet           Y    =        -5742178
80  meter
 Z    =      -11409895
81                 Z    =        -3477736
24
 XDOT =      17752
751611                 XDOT =        5411
038691
 YDOT =      -7068
524795  feet/sec       YDOT =       -2154
486358  meter/sec
 ZDOT =      14894
511883                 ZDOT =        4539
847222


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
77626166  
00010596  00000-0  82463-4 0  9006
2 25544  51
6413  39
9332 0008975 142
4108 217
7683 15
71478567 32044


Satellite: ISS
Catalog Number: 25544
Epoch time:      09079
77626166   =   yrday
fracday
Element set:     900
Inclination:       51
6413  deg
RA of node:        39
9332  deg
Eccentricity:     
0008975     
Arg of perigee:   142
4108  deg
Mean anomaly:     217
7683  deg
Mean motion:   15
71478567  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3204
Checksum:              330


Coasting Arc #2 (Orbit 3218)
---------------------------------------

Vector Time (GMT): 2009/080/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3991038
67                 A    =         6737498
20  meter
 Y    =       -4926131
04  meter          E    =           
0015021
 Z    =       -2267119
99                 I    =           51
84335
 XDOT =       5148
756306                 Wp   =          140
86937
 YDOT =      -1667
024753  meter/sec      RA   =           34
66894  deg
 ZDOT =      -5472
630677                 TA   =           64
48459
                                          MA   =           64
32932
                                          Ha   =            197
034  n
mi
                                          Hp   =            185
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13093958
88                 X    =        -3924644
12
 Y    =      -16161847
24  feet           Y    =        -4970390
05  meter
 Z    =       -7438057
70                 Z    =        -2286346
65
 XDOT =      16892
245097                 XDOT =        5193
599267
 YDOT =      -5469
241317  feet/sec       YDOT =       -1609
197922  meter/sec
 ZDOT =     -17954
825056                 ZDOT =       -5447
509362

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19456178
66                 X    =        -5930243
25
 Y    =        7279183
36  feet           Y    =         2218695
09  meter
 Z    =       -7513479
18                 Z    =        -2290108
45
 XDOT =        708
340087                 XDOT =         215
902059
 YDOT =     -16434
481615  feet/sec       YDOT =       -5009
229996  meter/sec
 ZDOT =     -17856
827412                 ZDOT =       -5442
760995


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
73014015  
00010596  00000-0  82463-4 0  9019
2 25544  51
6424  35
0527 0009194 144
8075 215
3696 15
71332956 32197


Satellite: ISS
Catalog Number: 25544
Epoch time:      09080
73014015   =   yrday
fracday
Element set:     901
Inclination:       51
6424  deg
RA of node:        35
0527  deg
Eccentricity:     
0009194     
Arg of perigee:   144
8075  deg
Mean anomaly:     215
3696  deg
Mean motion:   15
71332956  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3219
Checksum:              296


Coasting Arc #3 (Orbit 3234)
---------------------------------------

Vector Time (GMT): 2009/081/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3571819
17                 A    =         6728383
46  meter
 Y    =        2572722
29  meter          E    =           
0010136
 Z    =        5079800
64                 I    =           51
78852
 XDOT =      -5803
876000                 Wp   =          117
11877
 YDOT =      -4788
079669  meter/sec      RA   =           29
53191  deg
 ZDOT =      -1657
981109                 TA   =          348
76517
                                          MA   =          348
78778
                                          Ha   =            196
912  n
mi
                                          Hp   =            185
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11718566
82                 X    =        -3624998
73
 Y    =        8440689
92  feet           Y    =         2532483
14  meter
 Z    =       16666012
61                 Z    =         5062319
63
 XDOT =     -19041
587926                 XDOT =       -5741
849475
 YDOT =     -15708
922800  feet/sec       YDOT =       -4852
635304  meter/sec
 ZDOT =      -5439
570568                 ZDOT =       -1686
024946

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4516011
20                 X    =         1376480
21
 Y    =       13800031
09  feet           Y    =         4206249
48  meter
 Z    =       16597916
01                 Z    =         5059044
80
 XDOT =     -19673
883964                 XDOT =       -5996
599832
 YDOT =      13104
771932  feet/sec       YDOT =        3994
334485  meter/sec
 ZDOT =      -5549
416998                 ZDOT =       -1691
462301


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
74766860  
00010596  00000-0  82463-4 0  9024
2 25544  51
6425  29
8474 0009040 148
1291 212
0420 15
71423723 32357


Satellite: ISS
Catalog Number: 25544
Epoch time:      09081
74766860   =   yrday
fracday
Element set:     902
Inclination:       51
6425  deg
RA of node:        29
8474  deg
Eccentricity:     
0009040     
Arg of perigee:   148
1291  deg
Mean anomaly:     212
0420  deg
Mean motion:   15
71423723  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3235
Checksum:              291


Coasting Arc #4 (Orbit 3250)
---------------------------------------

Vector Time (GMT): 2009/082/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5896093
67                 A    =         6739316
20  meter
 Y    =        3204445
21  meter          E    =           
0014707
 Z    =         606306
57                 I    =           51
79882
 XDOT =      -2767
331451                 Wp   =           88
74751
 YDOT =       3932
236188  meter/sec      RA   =           24
44620  deg
 ZDOT =       6004
074134                 TA   =          277
82761
                                          MA   =          277
99455
                                          Ha   =            196
736  n
mi
                                          Hp   =            185
632

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19344139
33                 X    =         5856877
52
 Y    =       10513271
69  feet           Y    =         3270159
55  meter
 Z    =        1989194
78                 Z    =          634853
91
 XDOT =      -9079
171427                 XDOT =       -2840
263067
 YDOT =      12901
037362  feet/sec       YDOT =        3900
883028  meter/sec
 ZDOT =      19698
405952                 ZDOT =        5990
453098

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15553971
19                 X    =         4740850
42
 Y    =      -15567328
36  feet           Y    =        -4744921
68  meter
 Z    =        2100897
89                 Z    =          640353
68
 XDOT =       8637
493661                 XDOT =        2632
708068
 YDOT =      11333
553612  feet/sec       YDOT =        3454
467141  meter/sec
 ZDOT =      19645
477905                 ZDOT =        5987
941666


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
76518462  
00010596  00000-0  82463-4 0  9031
2 25544  51
6422  24
6415 0009073 152
2349 207
9299 15
71431663 32515


Satellite: ISS
Catalog Number: 25544
Epoch time:      09082
76518462   =   yrday
fracday
Element set:     903
Inclination:       51
6422  deg
RA of node:        24
6415  deg
Eccentricity:     
0009073     
Arg of perigee:   152
2349  deg
Mean anomaly:     207
9299  deg
Mean motion:   15
71431663  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3251
Checksum:              306


Coasting Arc #5 (Orbit 3265)
---------------------------------------

Vector Time (GMT): 2009/083/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1129249
73                 A    =         6727412
18  meter
 Y    =       -4024159
62  meter          E    =           
0020259
 Z    =       -5287343
84                 I    =           51
73079
 XDOT =       7307
690312                 Wp   =          112
19871
 YDOT =       2360
174123  meter/sec      RA   =           19
33407  deg
 ZDOT =       -243
797073                 TA   =          155
53315
                                          MA   =          155
43687
                                          Ha   =            196
612  n
mi
                                          Hp   =            185
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3704887
56                 X    =         1199849
38
 Y    =      -13202623
42  feet           Y    =        -4011137
49  meter
 Z    =      -17346928
62                 Z    =        -5281686
09
 XDOT =      23975
361915                 XDOT =        7281
939640
 YDOT =       7743
353421  feet/sec       YDOT =        2441
748972  meter/sec
 ZDOT =       -799
859162                 ZDOT =        -208
359393

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11711797
87                 X    =        -3569755
99
 Y    =       -7185112
99  feet           Y    =        -2190022
44  meter
 Z    =      -17325106
96                 Z    =        -5280692
60
 XDOT =      13328
263437                 XDOT =        4062
454696
 YDOT =     -20195
813013  feet/sec       YDOT =       -6155
683806  meter/sec
 ZDOT =       -661
310168                 ZDOT =        -201
567339


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
71909371  
00010596  00000-0  82463-4 0  9041
2 25544  51
6416  19
7606 0008985 155
7688 204
3898 15
71444797 32664


Satellite: ISS
Catalog Number: 25544
Epoch time:      09083
71909371   =   yrday
fracday
Element set:     904
Inclination:       51
6416  deg
RA of node:        19
7606  deg
Eccentricity:     
0008985     
Arg of perigee:   155
7688  deg
Mean anomaly:     204
3898  deg
Mean motion:   15
71444797  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3266
Checksum:              355


Coasting Arc #6 (Orbit 3281)
---------------------------------------

Vector Time (GMT): 2009/084/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6594678
20                 A    =         6739060
29  meter
 Y    =        -830623
66  meter          E    =           
0021751
 Z    =        1032395
17                 I    =           51
74210
 XDOT =       -319
466645                 Wp   =          137
77355
 YDOT =      -4906
624241  meter/sec      RA   =           14
21413  deg
 ZDOT =      -5932
284645                 TA   =           30
95479
                                          MA   =           30
82677
                                          Ha   =            196
574  n
mi
                                          Hp   =            185
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21636083
33                 X    =        -6589915
07
 Y    =       -2725143
24  feet           Y    =         -904342
45  meter
 Z    =        3387123
27                 Z    =         1000369
98
 XDOT =      -1048
118915                 XDOT =        -235
758322
 YDOT =     -16097
848561  feet/sec       YDOT =       -4909
729321  meter/sec
 ZDOT =     -19462
876133                 ZDOT =       -5933
632741

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8048322
51                 X    =        -2453128
70
 Y    =       20287998
94  feet           Y    =         6183782
08  meter
 Z    =        3262010
95                 Z    =          994260
94
 XDOT =     -14341
936573                 XDOT =       -4371
422267
 YDOT =      -2528
548629  feet/sec       YDOT =        -770
701622  meter/sec
 ZDOT =     -19468
471811                 ZDOT =       -5933
990208


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
73658349  
00010596  00000-0  82463-4 0  9051
2 25544  51
6421  14
5560 0009066 159
5734 200
5792 15
71436994 32826


Satellite: ISS
Catalog Number: 25544
Epoch time:      09084
73658349   =   yrday
fracday
Element set:     905
Inclination:       51
6421  deg
RA of node:        14
5560  deg
Eccentricity:     
0009066     
Arg of perigee:   159
5734  deg
Mean anomaly:     200
5792  deg
Mean motion:   15
71436994  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3282
Checksum:              327


Coasting Arc #7 (Orbit 3297)
---------------------------------------

Vector Time (GMT): 2009/085/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1703619
43                 A    =         6728826
39  meter
 Y    =        4231387
78  meter          E    =           
0014200
 Z    =        4943882
48                 I    =           51
67814
 XDOT =      -7388
786225                 Wp   =          146
94477
 YDOT =        498
040721  meter/sec      RA   =            9
12881  deg
 ZDOT =       2105
333899                 TA   =          282
57688
                                          MA   =          282
73566
                                          Ha   =            196
394  n
mi
                                          Hp   =            186
115

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5589302
59                 X    =         1632160
17
 Y    =       13882505
83  feet           Y    =         4250039
62  meter
 Z    =       16220086
87                 Z    =         4951984
66
 XDOT =     -24241
424624                 XDOT =       -7404
033608
 YDOT =       1633
991866  feet/sec       YDOT =         415
329977  meter/sec
 ZDOT =       6907
263448                 ZDOT =        2069
401994

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14781231
67                 X    =         4505319
41
 Y    =       -2107827
06  feet           Y    =         -642465
69  meter
 Z    =       16252007
41                 Z    =         4953611
86
 XDOT =      -4224
856413                 XDOT =       -1287
736235
 YDOT =      22915
059888  feet/sec       YDOT =        6984
510254  meter/sec
 ZDOT =       6766
993106                 ZDOT =        2062
579499


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
75405885  
00010596  00000-0  82463-4 0  9060
2 25544  51
6414   9
3498 0008967 163
4159 196
7298 15
71438101 32980


Satellite: ISS
Catalog Number: 25544
Epoch time:      09085
75405885   =   yrday
fracday
Element set:     906
Inclination:       51
6414  deg
RA of node:         9
3498  deg
Eccentricity:     
0008967     
Arg of perigee:   163
4159  deg
Mean anomaly:     196
7298  deg
Mean motion:   15
71438101  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3298
Checksum:              350


Coasting Arc #8 (Orbit 3312)
---------------------------------------

Vector Time (GMT): 2009/086/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6009813
53                 A    =         6736501
29  meter
 Y    =       -1629756
06  meter          E    =           
0008073
 Z    =       -2583845
09                 I    =           51
67399
 XDOT =       3456
061991                 Wp   =          132
91811
 YDOT =       4409
792502  meter/sec      RA   =            3
97559  deg
 ZDOT =       5262
012561                 TA   =          197
83661
                                          MA   =          197
86497
                                          Ha   =            196
242  n
mi
                                          Hp   =            186
311

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19717235
98                 X    =         6040143
02
 Y    =       -5346968
70  feet           Y    =        -1562381
48  meter
 Z    =       -8477182
04                 Z    =        -2554575
37
 XDOT =      11338
786060                 XDOT =        3380
931985
 YDOT =      14467
823169  feet/sec       YDOT =        4448
020618  meter/sec
 ZDOT =      17263
820738                 ZDOT =        5278
619335

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -944043
52                 X    =         -287744
47
 Y    =      -20454608
14  feet           Y    =        -6234564
56  meter
 Z    =       -8363006
15                 Z    =        -2549044
27
 XDOT =      15065
256053                 XDOT =        4591
890045
 YDOT =      -7773
621497  feet/sec       YDOT =       -2369
399832  meter/sec
 ZDOT =      17328
954430                 ZDOT =        5281
865310


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
70792737  
00010596  00000-0  82463-4 0  9072
2 25544  51
6404   4
4687 0009008 168
1877 191
9498 15
71493026 33135


Satellite: ISS
Catalog Number: 25544
Epoch time:      09086
70792737   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:         4
4687  deg
Eccentricity:     
0009008     
Arg of perigee:   168
1877  deg
Mean anomaly:     191
9498  deg
Mean motion:   15
71493026  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3313
Checksum:              337


Coasting Arc #9 (Orbit 3328)
---------------------------------------

Vector Time (GMT): 2009/087/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4193417
18                 A    =         6731635
80  meter
 Y    =       -3221699
46  meter          E    =           
0010816
 Z    =       -4169088
44                 I    =           51
62759
 XDOT =       6012
786275                 Wp   =          123
98949
 YDOT =      -3048
696634  meter/sec      RA   =          358
90691  deg
 ZDOT =      -3704
739417                 TA   =          108
16808
                                          MA   =          108
05029
                                          Ha   =            196
060  n
mi
                                          Hp   =            186
289

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13757930
38                 X    =        -4136827
03
 Y    =      -10569880
12  feet           Y    =        -3268276
58  meter
 Z    =      -13678111
67                 Z    =        -4189322
59
 XDOT =      19726
989090                 XDOT =        6064
427577
 YDOT =     -10002
285544  feet/sec       YDOT =       -2981
169670  meter/sec
 ZDOT =     -12154
656881                 ZDOT =       -3675
403332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13086690
70                 X    =        -3988823
33
 Y    =       11294614
85  feet           Y    =         3442598
61  meter
 Z    =      -13757323
67                 Z    =        -4193232
26
 XDOT =      -5027
692970                 XDOT =       -1532
440817
 YDOT =     -20440
292530  feet/sec       YDOT =       -6230
201163  meter/sec
 ZDOT =     -12040
317107                 ZDOT =       -3669
888654


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
72537512  
00010596  00000-0  82463-4 0  9084
2 25544  51
6395 359
2629 0008999 171
6810 188
4503 15
71514467 33293


Satellite: ISS
Catalog Number: 25544
Epoch time:      09087
72537512   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:       359
2629  deg
Eccentricity:     
0008999     
Arg of perigee:   171
6810  deg
Mean anomaly:     188
4503  deg
Mean motion:   15
71514467  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3329
Checksum:              347


Coasting Arc #10 (Orbit 3344)
---------------------------------------

Vector Time (GMT): 2009/088/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4254577
28                 A    =         6732855
19  meter
 Y    =        3523057
94  meter          E    =           
0013986
 Z    =        3833275
10                 I    =           51
60263
 XDOT =      -5931
045924                 Wp   =          121
37801
 YDOT =      -2651
502463  meter/sec      RA   =          353
73751  deg
 ZDOT =      -4142
075822                 TA   =           11
94891
                                          MA   =           11
91576
                                          Ha   =            195
987  n
mi
                                          Hp   =            186
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13958586
87                 X    =        -4312278
07
 Y    =       11558589
05  feet           Y    =         3475158
32  meter
 Z    =       12576361
88                 Z    =         3812465
82
 XDOT =     -19458
812085                 XDOT =       -5880
833876
 YDOT =      -8699
155063  feet/sec       YDOT =       -2717
546302  meter/sec
 ZDOT =     -13589
487606                 ZDOT =       -4170
767099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8801666
65                 X    =         2682747
99
 Y    =       15906133
55  feet           Y    =         4848189
51  meter
 Z    =       12495342
57                 Z    =         3808580
42
 XDOT =     -10932
603118                 XDOT =       -3332
257430
 YDOT =      16823
291876  feet/sec       YDOT =        5127
739364  meter/sec
 ZDOT =     -13701
677382                 ZDOT =       -4176
271266


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
74280770  
00010596  00000-0  82463-4 0  9099
2 25544  51
6399 354
0566 0008981 176
7325 183
3897 15
71549202 33451


Satellite: ISS
Catalog Number: 25544
Epoch time:      09088
74280770   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:       354
0566  deg
Eccentricity:     
0008981     
Arg of perigee:   176
7325  deg
Mean anomaly:     183
3897  deg
Mean motion:   15
71549202  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3345
Checksum:              350


Coasting Arc #11 (Orbit 3360)
---------------------------------------

Vector Time (GMT): 2009/089/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5905464
71                 A    =         6735121
66  meter
 Y    =        1236167
50  meter          E    =           
0015232
 Z    =        2991365
87                 I    =           51
58033
 XDOT =      -3513
313386                 Wp   =          120
07161
 YDOT =       4716
751366  meter/sec      RA   =          348
66651  deg
 ZDOT =       4960
402955                 TA   =          274
46655
                                          MA   =          274
64055
                                          Ha   =            195
800  n
mi
                                          Hp   =            186
587

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19374884
22                 X    =         5876671
11
 Y    =        4055667
64  feet           Y    =         1302044
90  meter
 Z    =        9814192
49                 Z    =         3019984
94
 XDOT =     -11526
618719                 XDOT =       -3589
892745
 YDOT =      15474
906056  feet/sec       YDOT =        4677
035349  meter/sec
 ZDOT =      16274
287909                 ZDOT =        4943
149025

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7200664
77                 X    =         2194762
62
 Y    =      -18378730
28  feet           Y    =        -5601836
99  meter
 Z    =        9926008
93                 Z    =         3025447
52
 XDOT =      11995
418081                 XDOT =        3656
203431
 YDOT =      13499
019958  feet/sec       YDOT =        4114
501283  meter/sec
 ZDOT =      16207
221892                 ZDOT =        4939
961233


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   09089
76022726  
00010596  00000-0  82463-4 0  9109
2 25544  51
6387 348
8497 0009153 180
2538 179
8621 15
71576155 33610


Satellite: ISS
Catalog Number: 25544
Epoch time:      09089
76022726   =   yrday
fracday
Element set:     910
Inclination:       51
6387  deg
RA of node:       348
8497  deg
Eccentricity:     
0009153     
Arg of perigee:   180
2538  deg
Mean anomaly:     179
8621  deg
Mean motion:   15
71576155  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3361
Checksum:              339


Coasting Arc #12 (Orbit 3375)
---------------------------------------

Vector Time (GMT): 2009/090/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1785246
47                 A    =         6729434
32  meter
 Y    =       -4451946
81  meter          E    =           
0016356
 Z    =       -4734224
08                 I    =           51
53198
 XDOT =       7211
927717                 Wp   =          141
01454
 YDOT =         62
266142  meter/sec      RA   =          343
49773  deg
 ZDOT =       2653
501069                 TA   =          155
19309
                                          MA   =          155
11436
                                          Ha   =            195
758  n
mi
                                          Hp   =            186
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5857107
86                 X    =         1857894
33
 Y    =      -14606124
69  feet           Y    =        -4431576
93  meter
 Z    =      -15532231
23                 Z    =        -4725374
86
 XDOT =      23661
180174                 XDOT =        7197
805139
 YDOT =        204
285244  feet/sec       YDOT =         142
835148  meter/sec
 ZDOT =       8705
712170                 ZDOT =        2688
502501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13559500
11                 X    =        -4132935
63
 Y    =       -8052824
94  feet           Y    =        -2454501
04  meter
 Z    =      -15497960
03                 Z    =        -4723778
22
 XDOT =       3126
040168                 XDOT =         952
817043
 YDOT =     -22328
744305  feet/sec       YDOT =       -6805
801264  meter/sec
 ZDOT =       8842
376198                 ZDOT =        2695
156265


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   09090
71404655  
00010596  00000-0  82463-4 0  9112
2 25544  51
6385 343
9678 0009166 182
6380 177
4735 15
71577685 33765


Satellite: ISS
Catalog Number: 25544
Epoch time:      09090
71404655   =   yrday
fracday
Element set:     911
Inclination:       51
6385  deg
RA of node:       343
9678  deg
Eccentricity:     
0009166     
Arg of perigee:   182
6380  deg
Mean anomaly:     177
4735  deg
Mean motion:   15
71577685  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3376
Checksum:              347


Coasting Arc #13 (Orbit 3391)
---------------------------------------

Vector Time (GMT): 2009/091/16:52:03
644
Vector Time (MET): N/A
Weight (LBS)     : 638776
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6428132
56                 A    =         6737769
38  meter
 Y    =        1168349
13  meter          E    =           
0015603
 Z    =       -1609872
07                 I    =           51
53301
 XDOT =        503
515248                 Wp   =          165
63719
 YDOT =      -5106
581875  meter/sec      RA   =          338
40906  deg
 ZDOT =      -5743
258326                 TA   =           32
15509
                                          MA   =           32
06003
                                          Ha   =            195
408  n
mi
                                          Hp   =            186
923

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21089673
76                 X    =        -6432899
02
 Y    =        3833166
43  feet           Y    =         1096439
37  meter
 Z    =       -5281732
52                 Z    =        -1641111
51
 XDOT =       1651
952913                 XDOT =         588
480189
 YDOT =     -16753
877543  feet/sec       YDOT =       -5100
476154  meter/sec
 ZDOT =     -18842
711044                 ZDOT =       -5740
605920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1026712
16                 X    =          312941
87
 Y    =       21380149
52  feet           Y    =         6516669
57  meter
 Z    =       -5403635
02                 Z    =        -1647027
95
 XDOT =     -14817
237948                 XDOT =       -4516
294126
 YDOT =      -4026
597418  feet/sec       YDOT =       -1227
306893  meter/sec
 ZDOT =     -18832
675360                 ZDOT =       -5740
199450


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   09091
73143833  
00010596  00000-0  82463-4 0  9124
2 25544  51
6387 338
7617 0008961 186
7122 173
3921 15
71624246 33929


Satellite: ISS
Catalog Number: 25544
Epoch time:      09091
73143833   =   yrday
fracday
Element set:     912
Inclination:       51
6387  deg
RA of node:       338
7617  deg
Eccentricity:     
0008961     
Arg of perigee:   186
7122  deg
Mean anomaly:     173
3921  deg
Mean motion:   15
71624246  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3392
Checksum:              323

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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