Date: June 2nd 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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 303)
---------------------------------------

Vector Time (GMT): 2009/149/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2882645
29                 A    =         6731175
29  meter
 Y    =       -5429083
90  meter          E    =           
0012091
 Z    =       -2757261
52                 I    =           51
86773
 XDOT =       5679
293072                 Wp   =           75
66601
 YDOT =       -399
250867  meter/sec      RA   =           41
41604  deg
 ZDOT =      -5167
304279                 TA   =          135
68725
                                          MA   =          135
59040
                                          Ha   =            194
553  n
mi
                                          Hp   =            182
044

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9457497
66                 X    =        -2808327
87
 Y    =      -17811955
05  feet           Y    =        -5460903
44  meter
 Z    =       -9046133
59                 Z    =        -2771085
56
 XDOT =      18632
851286                 XDOT =        5708
437225
 YDOT =      -1309
878173  feet/sec       YDOT =        -335
578074  meter/sec
 ZDOT =     -16953
098028                 ZDOT =       -5139
643603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9251795
97                 X    =        -2819947
41
 Y    =       17892093
09  feet           Y    =         5453509
97  meter
 Z    =       -9100539
23                 Z    =        -2773844
36
 XDOT =     -10466
866215                 XDOT =       -3190
300822
 YDOT =     -13953
776076  feet/sec       YDOT =       -4253
110948  meter/sec
 ZDOT =     -16844
747238                 ZDOT =       -5134
278958


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   09149
68811709  
00010596  00000-0  82463-4 0  9003
2 25544  51
6385  41
8232 0009332  55
1592 305
0448 15
73177262  3046


Satellite: ISS
Catalog Number: 25544
Epoch time:      09149
68811709   =   yrday
fracday
Element set:     900
Inclination:       51
6385  deg
RA of node:        41
8232  deg
Eccentricity:     
0009332     
Arg of perigee:    55
1592  deg
Mean anomaly:     305
0448  deg
Mean motion:   15
73177262  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             304
Checksum:              299


Coasting Arc #2 (Orbit 319)
---------------------------------------

Vector Time (GMT): 2009/150/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4753727
74                 A    =         6725215
36  meter
 Y    =        1032459
36  meter          E    =           
0017432
 Z    =        4634605
35                 I    =           51
82461
 XDOT =      -4109
441793                 Wp   =           61
23877
 YDOT =      -5839
182540  meter/sec      RA   =           36
25545  deg
 ZDOT =      -2897
865708                 TA   =           57
42430
                                          MA   =           57
25608
                                          Ha   =            194
627  n
mi
                                          Hp   =            182
011

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15596219
62                 X    =        -4787433
63
 Y    =        3387333
87  feet           Y    =          979111
44  meter
 Z    =       15205398
13                 Z    =         4611429
99
 XDOT =     -13482
420581                 XDOT =       -4029
764343
 YDOT =     -19157
423032  feet/sec       YDOT =       -5884
690905  meter/sec
 ZDOT =      -9507
433425                 ZDOT =       -2917
636465

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11923656
10                 X    =         3634330
38
 Y    =       10737507
01  feet           Y    =         3272792
14  meter
 Z    =       15114648
45                 Z    =         4606944
85
 XDOT =      -6897
539520                 XDOT =       -2102
370046
 YDOT =      21228
207094  feet/sec       YDOT =        6470
357522  meter/sec
 ZDOT =      -9585
154407                 ZDOT =       -2921
555063


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   09150
70447378  
00010596  00000-0  82463-4 0  9016
2 25544  51
6386  36
6088 0009167  59
2125 300
9939 15
73198879  3205


Satellite: ISS
Catalog Number: 25544
Epoch time:      09150
70447378   =   yrday
fracday
Element set:     901
Inclination:       51
6386  deg
RA of node:        36
6088  deg
Eccentricity:     
0009167     
Arg of perigee:    59
2125  deg
Mean anomaly:     300
9939  deg
Mean motion:   15
73198879  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             320
Checksum:              331


Coasting Arc #3 (Orbit 335)
---------------------------------------

Vector Time (GMT): 2009/151/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4244982
44                 A    =         6732003
06  meter
 Y    =        4677782
05  meter          E    =           
0023069
 Z    =        2294696
13                 I    =           51
82281
 XDOT =      -5093
611128                 Wp   =           68
86725
 YDOT =       1929
642974  meter/sec      RA   =           31
18034  deg
 ZDOT =       5453
571394                 TA   =          316
87635
                                          MA   =          317
05683
                                          Ha   =            194
462  n
mi
                                          Hp   =            181
821

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13927107
74                 X    =         4181211
94
 Y    =       15347053
96  feet           Y    =         4724895
14  meter
 Z    =        7528530
62                 Z    =         2315163
88
 XDOT =     -16711
322600                 XDOT =       -5141
302705
 YDOT =       6330
849652  feet/sec       YDOT =        1872
416055  meter/sec
 ZDOT =      17892
294600                 ZDOT =        5428
710887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3974728
86                 X    =         1211497
36
 Y    =      -20309626
72  feet           Y    =        -6190374
23  meter
 Z    =        7608926
43                 Z    =         2319200
78
 XDOT =      13659
976271                 XDOT =        4163
560768
 YDOT =       9383
394461  feet/sec       YDOT =        2860
058632  meter/sec
 ZDOT =      17794
984201                 ZDOT =        5423
911185


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   09151
72080978  
00010596  00000-0  82463-4 0  9029
2 25544  51
6381  31
3944 0009171  63
7781 296
4323 15
73242137  3366


Satellite: ISS
Catalog Number: 25544
Epoch time:      09151
72080978   =   yrday
fracday
Element set:     902
Inclination:       51
6381  deg
RA of node:        31
3944  deg
Eccentricity:     
0009171     
Arg of perigee:    63
7781  deg
Mean anomaly:     296
4323  deg
Mean motion:   15
73242137  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             336
Checksum:              305


Coasting Arc #4 (Orbit 350)
---------------------------------------

Vector Time (GMT): 2009/152/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4074792
57                 A    =         6724137
69  meter
 Y    =       -2270966
05  meter          E    =           
0019986
 Z    =       -4859917
15                 I    =           51
77061
 XDOT =       5513
315257                 Wp   =           89
93127
 YDOT =       4789
428195  meter/sec      RA   =           26
02179  deg
 ZDOT =       2393
068767                 TA   =          203
37648
                                          MA   =          203
46747
                                          Ha   =            194
522  n
mi
                                          Hp   =            181
798

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13368742
01                 X    =         4123492
83
 Y    =       -7450676
02  feet           Y    =        -2225126
57  meter
 Z    =      -15944610
06                 Z    =        -4840003
57
 XDOT =      18088
304650                 XDOT =        5447
724110
 YDOT =      15713
347098  feet/sec       YDOT =        4850
714337  meter/sec
 ZDOT =       7851
275481                 ZDOT =        2419
693809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14135554
66                 X    =        -4308517
06
 Y    =       -6074576
19  feet           Y    =        -1851530
82  meter
 Z    =      -15866696
09                 Z    =        -4836168
97
 XDOT =        923
271559                 XDOT =         281
413171
 YDOT =     -22855
979699  feet/sec       YDOT =       -6966
502612  meter/sec
 ZDOT =       7955
792433                 ZDOT =        2424
925533


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   09152
67360641  
00010596  00000-0  82463-4 0  9033
2 25544  51
6384  26
5061 0009246  67
8998 292
3146 15
73266570  3515


Satellite: ISS
Catalog Number: 25544
Epoch time:      09152
67360641   =   yrday
fracday
Element set:     903
Inclination:       51
6384  deg
RA of node:        26
5061  deg
Eccentricity:     
0009246     
Arg of perigee:    67
8998  deg
Mean anomaly:     292
3146  deg
Mean motion:   15
73266570  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             351
Checksum:              318


Coasting Arc #5 (Orbit 366)
---------------------------------------

Vector Time (GMT): 2009/153/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5324902
53                 A    =         6732437
44  meter
 Y    =       -3651466
02  meter          E    =           
0013346
 Z    =       -1913795
50                 I    =           51
77252
 XDOT =       4176
925663                 Wp   =           99
35978
 YDOT =      -3155
554385  meter/sec      RA   =           20
93765  deg
 ZDOT =      -5636
445924                 TA   =          101
84880
                                          MA   =          101
69909
                                          Ha   =            194
432  n
mi
                                          Hp   =            181
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17470152
67                 X    =        -5274378
48
 Y    =      -11979875
38  feet           Y    =        -3710729
49  meter
 Z    =       -6278856
64                 Z    =        -1939541
86
 XDOT =      13703
824354                 XDOT =        4239
282330
 YDOT =     -10352
868718  feet/sec       YDOT =       -3108
496304  meter/sec
 ZDOT =     -18492
276653                 ZDOT =       -5616
003043

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1574596
93                 X    =          479937
14
 Y    =       21094206
07  feet           Y    =         6429514
01  meter
 Z    =       -6379874
93                 Z    =        -1944585
88
 XDOT =     -15181
721680                 XDOT =       -4627
388768
 YDOT =      -4400
958338  feet/sec       YDOT =       -1341
412101  meter/sec
 ZDOT =     -18412
326752                 ZDOT =       -5612
077194


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   09153
68990138  
00010596  00000-0  82463-4 0  9046
2 25544  51
6387  21
2923 0009300  70
5837 289
6330 15
73328635  3673


Satellite: ISS
Catalog Number: 25544
Epoch time:      09153
68990138   =   yrday
fracday
Element set:     904
Inclination:       51
6387  deg
RA of node:        21
2923  deg
Eccentricity:     
0009300     
Arg of perigee:    70
5837  deg
Mean anomaly:     289
6330  deg
Mean motion:   15
73328635  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             367
Checksum:              319


Coasting Arc #6 (Orbit 382)
---------------------------------------

Vector Time (GMT): 2009/154/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3162565
22                 A    =         6723409
60  meter
 Y    =        3197611
64  meter          E    =           
0014911
 Z    =        4987633
43                 I    =           51
71288
 XDOT =      -6601
644897                 Wp   =           67
52458
 YDOT =      -3467
512404  meter/sec      RA   =           15
78081  deg
 ZDOT =      -1952
714678                 TA   =           41
36063
                                          MA   =           41
24782
                                          Ha   =            194
597  n
mi
                                          Hp   =            181
576

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10375870
14                 X    =        -3222315
78
 Y    =       10490851
84  feet           Y    =         3161911
28  meter
 Z    =       16363626
74                 Z    =         4972124
72
 XDOT =     -21658
939950                 XDOT =       -6552
893860
 YDOT =     -11376
353032  feet/sec       YDOT =       -3541
063026  meter/sec
 ZDOT =      -6406
544220                 ZDOT =       -1984
667967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14761336
52                 X    =         4499255
37
 Y    =        1341597
25  feet           Y    =          408918
84  meter
 Z    =       16303005
69                 Z    =         4969156
13
 XDOT =       5177
047596                 XDOT =        1577
964107
 YDOT =      22821
519485  feet/sec       YDOT =        6955
999139  meter/sec
 ZDOT =      -6531
863855                 ZDOT =       -1990
912103


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   09154
70617785  
00010596  00000-0  82463-4 0  9055
2 25544  51
6382  16
0780 0009225  75
7852 284
4335 15
73297317  3839


Satellite: ISS
Catalog Number: 25544
Epoch time:      09154
70617785   =   yrday
fracday
Element set:     905
Inclination:       51
6382  deg
RA of node:        16
0780  deg
Eccentricity:     
0009225     
Arg of perigee:    75
7852  deg
Mean anomaly:     284
4335  deg
Mean motion:   15
73297317  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             383
Checksum:              324


Coasting Arc #7 (Orbit 398)
---------------------------------------

Vector Time (GMT): 2009/155/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6117746
82                 A    =         6732948
81  meter
 Y    =        2354716
52  meter          E    =           
0022968
 Z    =        1494428
29                 I    =           51
71782
 XDOT =      -3005
570764                 Wp   =           68
67344
 YDOT =       4089
357455  meter/sec      RA   =           10
68613  deg
 ZDOT =       5797
620702                 TA   =          307
77539
                                          MA   =          307
98320
                                          Ha   =            194
354  n
mi
                                          Hp   =            181
415

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20071347
84                 X    =         6083701
52
 Y    =        7725447
90  feet           Y    =         2422938
16  meter
 Z    =        4902979
94                 Z    =         1524066
42
 XDOT =      -9860
796470                 XDOT =       -3079
239499
 YDOT =      13416
527082  feet/sec       YDOT =        4055
334646  meter/sec
 ZDOT =      19021
065296                 ZDOT =        5782
841069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7225597
95                 X    =        -2202362
25
 Y    =      -20228181
49  feet           Y    =        -6165549
72  meter
 Z    =        5019180
13                 Z    =         1529846
10
 XDOT =      15197
985904                 XDOT =        4632
346104
 YDOT =       -673
479208  feet/sec       YDOT =        -205
276463  meter/sec
 ZDOT =      18963
332707                 ZDOT =        5780
023809


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   09155
72243098  
00010596  00000-0  82463-4 0  9061
2 25544  51
6391  10
8641 0009155  79
9303 280
2893 15
73374451  3991


Satellite: ISS
Catalog Number: 25544
Epoch time:      09155
72243098   =   yrday
fracday
Element set:     906
Inclination:       51
6391  deg
RA of node:        10
8641  deg
Eccentricity:     
0009155     
Arg of perigee:    79
9303  deg
Mean anomaly:     280
2893  deg
Mean motion:   15
73374451  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             399
Checksum:              322


Coasting Arc #8 (Orbit 413)
---------------------------------------

Vector Time (GMT): 2009/156/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2076002
61                 A    =         6722641
46  meter
 Y    =       -3863670
41  meter          E    =           
0022681
 Z    =       -5114480
28                 I    =           51
65420
 XDOT =       7285
091192                 Wp   =           93
98625
 YDOT =       1911
487199  meter/sec      RA   =            5
53233  deg
 ZDOT =       1517
281323                 TA   =          190
57418
                                          MA   =          190
62195
                                          Ha   =            194
368  n
mi
                                          Hp   =            181
417

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6811032
18                 X    =         2143898
11
 Y    =      -12676084
02  feet           Y    =        -3840074
85  meter
 Z    =      -16779790
94                 Z    =        -5104230
64
 XDOT =      23901
217820                 XDOT =        7255
804385
 YDOT =       6271
283460  feet/sec       YDOT =        1992
789334  meter/sec
 ZDOT =       4977
957097                 ZDOT =        1552
602007

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14058971
59                 X    =        -4285174
54
 Y    =        3280150
01  feet           Y    =          999789
72  meter
 Z    =      -16739790
42                 Z    =        -5102288
12
 XDOT =     -10967
160129                 XDOT =       -3342
790407
 YDOT =     -20966
106206  feet/sec       YDOT =       -6390
469172  meter/sec
 ZDOT =       5116
399232                 ZDOT =        1559
478486


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   09156
67515114  
00010596  00000-0  82463-4 0  9078
2 25544  51
6396   5
9765 0009196  83
3013 276
9196 15
73393443  4148


Satellite: ISS
Catalog Number: 25544
Epoch time:      09156
67515114   =   yrday
fracday
Element set:     907
Inclination:       51
6396  deg
RA of node:         5
9765  deg
Eccentricity:     
0009196     
Arg of perigee:    83
3013  deg
Mean anomaly:     276
9196  deg
Mean motion:   15
73393443  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             414
Checksum:              326


Coasting Arc #9 (Orbit 429)
---------------------------------------

Vector Time (GMT): 2009/157/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6553873
07                 A    =         6733103
34  meter
 Y    =        -981275
59  meter          E    =           
0016158
 Z    =       -1179136
05                 I    =           51
65992
 XDOT =       1741
628741                 Wp   =          113
90010
 YDOT =      -4642
657822  meter/sec      RA   =             
42560  deg
 ZDOT =      -5886
373309                 TA   =           79
00552
                                          MA   =           78
82380
                                          Ha   =            194
240  n
mi
                                          Hp   =            181
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21502208
22                 X    =        -6536685
08
 Y    =       -3219408
11  feet           Y    =        -1054468
50  meter
 Z    =       -3868556
58                 Z    =        -1210933
59
 XDOT =       5714
005057                 XDOT =        1822
009564
 YDOT =     -15231
817002  feet/sec       YDOT =       -4622
731386  meter/sec
 ZDOT =     -19312
248390                 ZDOT =       -5877
717988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12202823
03                 X    =         3719420
46
 Y    =       17967221
34  feet           Y    =         5476409
06  meter
 Z    =       -3993162
22                 Z    =        -1217115
85
 XDOT =     -13834
240911                 XDOT =       -4216
676630
 YDOT =       5160
440327  feet/sec       YDOT =        1572
902212  meter/sec
 ZDOT =     -19278
519127                 ZDOT =       -5876
092630


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   09157
69136452  
00010596  00000-0  82463-4 0  9086
2 25544  51
6391    
7609 0009136  86
0575 274
1632 15
73446100  4302


Satellite: ISS
Catalog Number: 25544
Epoch time:      09157
69136452   =   yrday
fracday
Element set:     908
Inclination:       51
6391  deg
RA of node:          
7609  deg
Eccentricity:     
0009136     
Arg of perigee:    86
0575  deg
Mean anomaly:     274
1632  deg
Mean motion:   15
73446100  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             430
Checksum:              298


Coasting Arc #10 (Orbit 445)
---------------------------------------

Vector Time (GMT): 2009/158/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -935456
41                 A    =         6722195
31  meter
 Y    =        4186298
72  meter          E    =           
0012688
 Z    =        5165385
50                 I    =           51
59371
 XDOT =      -7618
545346                 Wp   =           79
30085
 YDOT =       -281
970617  meter/sec      RA   =          355
27241  deg
 ZDOT =      -1146
513530                 TA   =           21
66576
                                          MA   =           21
61213
                                          Ha   =            194
358  n
mi
                                          Hp   =            181
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3069082
72                 X    =        -1007291
51
 Y    =       13734575
85  feet           Y    =         4175435
24  meter
 Z    =       16946802
82                 Z    =         5160667
34
 XDOT =     -24995
227512                 XDOT =       -7609
256470
 YDOT =       -925
100449  feet/sec       YDOT =        -367
113477  meter/sec
 ZDOT =      -3761
527328                 ZDOT =       -1183
502242

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12118965
67                 X    =         3693860
74
 Y    =       -7197867
95  feet           Y    =        -2193910
15  meter
 Z    =       16928477
09                 Z    =         5159799
82
 XDOT =      16057
452338                 XDOT =        4894
311473
 YDOT =      17812
054775  feet/sec       YDOT =        5429
114295  meter/sec
 ZDOT =      -3906
447030                 ZDOT =       -1190
685055


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   09158
70755965  
00010596  00000-0  82463-4 0  9096
2 25544  51
6397 355
5467 0009190  90
2057 270
0159 15
73424908  4461


Satellite: ISS
Catalog Number: 25544
Epoch time:      09158
70755965   =   yrday
fracday
Element set:     909
Inclination:       51
6397  deg
RA of node:       355
5467  deg
Eccentricity:     
0009190     
Arg of perigee:    90
2057  deg
Mean anomaly:     270
0159  deg
Mean motion:   15
73424908  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             446
Checksum:              337


Coasting Arc #11 (Orbit 461)
---------------------------------------

Vector Time (GMT): 2009/159/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6657026
26                 A    =         6733281
28  meter
 Y    =        -488525
77  meter          E    =           
0021384
 Z    =         828707
42                 I    =           51
60342
 XDOT =       -399
502002                 Wp   =           69
57174
 YDOT =       4862
835670  meter/sec      RA   =          350
15642  deg
 ZDOT =       5959
606658                 TA   =          299
47296
                                          MA   =          299
68613
                                          Ha   =            194
165  n
mi
                                          Hp   =            181
217

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21840637
33                 X    =         6657968
54
 Y    =       -1602774
84  feet           Y    =         -414077
91  meter
 Z    =        2718856
37                 Z    =          861049
60
 XDOT =      -1310
702107                 XDOT =        -482
800180
 YDOT =      15954
185268  feet/sec       YDOT =        4857
901270  meter/sec
 ZDOT =      19552
515281                 ZDOT =        5957
464507

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16485143
71                 X    =        -5024671
80
 Y    =      -14391573
89  feet           Y    =        -4386551
72  meter
 Z    =        2845548
10                 Z    =          867323
06
 XDOT =      11296
497599                 XDOT =        3443
172468
 YDOT =      -9003
398105  feet/sec       YDOT =       -2744
235742  meter/sec
 ZDOT =      19544
305682                 ZDOT =        5957
104372


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   09159
72373036  
00010596  00000-0  82463-4 0  9106
2 25544  51
6408 350
3324 0009082  94
1853 266
0348 15
73499149  4628


Satellite: ISS
Catalog Number: 25544
Epoch time:      09159
72373036   =   yrday
fracday
Element set:     910
Inclination:       51
6408  deg
RA of node:       350
3324  deg
Eccentricity:     
0009082     
Arg of perigee:    94
1853  deg
Mean anomaly:     266
0348  deg
Mean motion:   15
73499149  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             462
Checksum:              314


Coasting Arc #12 (Orbit 476)
---------------------------------------

Vector Time (GMT): 2009/160/15:53:07
067
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -204607
21                 A    =         6721661
62  meter
 Y    =       -4244964
60  meter          E    =           
0023699
 Z    =       -5228143
53                 I    =           51
53555
 XDOT =       7519
581494                 Wp   =           96
29377
 YDOT =      -1352
523206  meter/sec      RA   =          345
00521  deg
 ZDOT =        804
459902                 TA   =          181
38840
                                          MA   =          181
39499
                                          Ha   =            194
081  n
mi
                                          Hp   =            181
180

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -671283
50                 X    =         -131726
70
 Y    =      -13927049
20  feet           Y    =        -4246844
11  meter
 Z    =      -17152701
89                 Z    =        -5228961
33
 XDOT =      24670
542959                 XDOT =        7530
238841
 YDOT =      -4437
412092  feet/sec       YDOT =       -1268
375425  meter/sec
 ZDOT =       2639
304139                 ZDOT =         841
015682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9324299
25                 X    =        -2842046
41
 Y    =       10361241
72  feet           Y    =         3158106
48  meter
 Z    =      -17156066
46                 Z    =        -5229169
06
 XDOT =     -19980
129554                 XDOT =       -6089
943488
 YDOT =     -13376
430346  feet/sec       YDOT =       -4077
135970  meter/sec
 ZDOT =       2782
476275                 ZDOT =         848
098769


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   09160
67637324  
00010596  00000-0  82463-4 0  9116
2 25544  51
6409 345
4445 0009028  96
9973 263
2217 15
73539207  4771


Satellite: ISS
Catalog Number: 25544
Epoch time:      09160
67637324   =   yrday
fracday
Element set:     911
Inclination:       51
6409  deg
RA of node:       345
4445  deg
Eccentricity:     
0009028     
Arg of perigee:    96
9973  deg
Mean anomaly:     263
2217  deg
Mean motion:   15
73539207  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             477
Checksum:              327

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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