Date: November 19th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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 2994)
---------------------------------------

Vector Time (GMT): 2009/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4552721
49                 A    =         6721857
67  meter
 Y    =       -4050930
82  meter          E    =           
0008173
 Z    =       -2827348
23                 I    =           51
35309
 XDOT =       1772
145974                 Wp   =           12
47929
 YDOT =      -5523
664973  meter/sec      RA   =          243
43888  deg
 ZDOT =       5071
125726                 TA   =          314
91391
                                          MA   =          314
98021
                                          Ha   =            186
837  n
mi
                                          Hp   =            180
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14936750
30                 X    =        -4493349
72
 Y    =      -13290455
46  feet           Y    =        -4101509
88  meter
 Z    =       -9276076
86                 Z    =        -2849322
11
 XDOT =       5814
127211                 XDOT =        1809
145458
 YDOT =     -18122
260411  feet/sec       YDOT =       -5503
641271  meter/sec
 ZDOT =      16637
551593                 ZDOT =        5079
824572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19429282
15                 X    =         5922045
20
 Y    =       -4541681
65  feet           Y    =        -1384304
57  meter
 Z    =       -9362929
08                 Z    =        -2853820
78
 XDOT =      11214
232539                 XDOT =        3418
098078
 YDOT =      13675
845118  feet/sec       YDOT =        4168
397592  meter/sec
 ZDOT =      16671
645269                 ZDOT =        5081
517478


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   09320
50577560  
00016717  00000-0  10270-3 0  9006
2 25544  51
6451 244
3179 0006373 337
9041  22
1847 15
76378503 29954


Satellite: ISS
Catalog Number: 25544
Epoch time:      09320
50577560   =   yrday
fracday
Element set:     900
Inclination:       51
6451  deg
RA of node:       244
3179  deg
Eccentricity:     
0006373     
Arg of perigee:   337
9041  deg
Mean anomaly:      22
1847  deg
Mean motion:   15
76378503  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2995
Checksum:              314


Coasting Arc #2 (Orbit 3010)
---------------------------------------

Vector Time (GMT): 2009/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1858400
15                 A    =         6715111
04  meter
 Y    =        4314015
79  meter          E    =           
0013543
 Z    =       -4810604
04                 I    =           51
34603
 XDOT =      -5341
498109                 Wp   =           44
73587
 YDOT =      -4989
221705  meter/sec      RA   =          238
30769  deg
 ZDOT =      -2405
325687                 TA   =          201
63975
                                          MA   =          201
69703
                                          Ha   =            186
962  n
mi
                                          Hp   =            180
262

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6097113
36                 X    =        -1883132
39
 Y    =       14153595
10  feet           Y    =         4293096
20  meter
 Z    =      -15782821
66                 Z    =        -4819692
11
 XDOT =     -17524
600094                 XDOT =       -5273
625789
 YDOT =     -16368
837616  feet/sec       YDOT =       -5048
573779  meter/sec
 ZDOT =      -7891
488474                 ZDOT =       -2431
111013

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8355278
47                 X    =        -2546688
88
 Y    =      -12905842
19  feet           Y    =        -3933700
70  meter
 Z    =      -15818503
86                 Z    =        -4821479
98
 XDOT =      22411
532004                 XDOT =        6831
034955
 YDOT =      -4690
287215  feet/sec       YDOT =       -1429
599543  meter/sec
 ZDOT =      -7993
424290                 ZDOT =       -2436
395724


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   09321
52005649  
00016717  00000-0  10270-3 0  9014
2 25544  51
6458 239
0911 0006342 342
5699  17
5247 15
76445153 30111


Satellite: ISS
Catalog Number: 25544
Epoch time:      09321
52005649   =   yrday
fracday
Element set:     901
Inclination:       51
6458  deg
RA of node:       239
0911  deg
Eccentricity:     
0006342     
Arg of perigee:   342
5699  deg
Mean anomaly:      17
5247  deg
Mean motion:   15
76445153  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3011
Checksum:              299


Coasting Arc #3 (Orbit 3026)
---------------------------------------

Vector Time (GMT): 2009/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4742711
47                 A    =         6724402
76  meter
 Y    =        4581222
38  meter          E    =           
0010574
 Z    =        1305401
37                 I    =           51
39432
 XDOT =      -2568
047951                 Wp   =           95
49585
 YDOT =       4330
593521  meter/sec      RA   =          233
10251  deg
 ZDOT =      -5828
429946                 TA   =           70
11489
                                          MA   =           70
00097
                                          Ha   =            187
020  n
mi
                                          Hp   =            180
150

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15560077
00                 X    =         4684789
39
 Y    =       15030257
15  feet           Y    =         4633934
18  meter
 Z    =        4282812
90                 Z    =         1328301
81
 XDOT =      -8425
354171                 XDOT =       -2587
968370
 YDOT =      14207
983994  feet/sec       YDOT =        4301
765306  meter/sec
 ZDOT =     -19122
145492                 ZDOT =       -5840
953786

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21075228
75                 X    =        -6423729
72
 Y    =        4803702
93  feet           Y    =         1464168
65  meter
 Z    =        4373360
66                 Z    =         1333000
33
 XDOT =      -7010
290910                 XDOT =       -2136
736669
 YDOT =     -13186
945742  feet/sec       YDOT =       -4019
381062  meter/sec
 ZDOT =     -19171
387680                 ZDOT =       -5843
438965


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   09322
53430932  
00016717  00000-0  10270-3 0  9024
2 25544  51
6455 233
8642 0006290 345
7512  14
3474 15
76462580 30279


Satellite: ISS
Catalog Number: 25544
Epoch time:      09322
53430932   =   yrday
fracday
Element set:     902
Inclination:       51
6455  deg
RA of node:       233
8642  deg
Eccentricity:     
0006290     
Arg of perigee:   345
7512  deg
Mean anomaly:      14
3474  deg
Mean motion:   15
76462580  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3027
Checksum:              297


Coasting Arc #4 (Orbit 3042)
---------------------------------------

Vector Time (GMT): 2009/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2691824
15                 A    =         6712945
70  meter
 Y    =       -3245228
86  meter          E    =           
0005187
 Z    =        5222103
99                 I    =           51
37520
 XDOT =       5465
533026                 Wp   =           14
59658
 YDOT =       5406
230050  meter/sec      RA   =          227
94766  deg
 ZDOT =        547
182309                 TA   =           70
21733
                                          MA   =           70
16140
                                          Ha   =            186
878  n
mi
                                          Hp   =            179
958

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8831444
06                 X    =         2702544
24
 Y    =      -10647076
32  feet           Y    =        -3215067
92  meter
 Z    =       17132887
12                 Z    =         5235206
84
 XDOT =      17931
538800                 XDOT =        5402
015236
 YDOT =      17736
975231  feet/sec       YDOT =        5466
993657  meter/sec
 ZDOT =       1795
217550                 ZDOT =         573
580717

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4374837
49                 X    =         1333450
47
 Y    =       13055477
21  feet           Y    =         3979309
45  meter
 Z    =       17184463
08                 Z    =         5237824
35
 XDOT =     -23598
430787                 XDOT =       -7192
801704
 YDOT =       5428
153789  feet/sec       YDOT =        1654
501275  meter/sec
 ZDOT =       1899
615602                 ZDOT =         579
002836


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   09323
54853202  
00016717  00000-0  10270-3 0  9036
2 25544  51
6452 228
6371 0006325 348
3018  11
7998 15
76548165 30430


Satellite: ISS
Catalog Number: 25544
Epoch time:      09323
54853202   =   yrday
fracday
Element set:     903
Inclination:       51
6452  deg
RA of node:       228
6371  deg
Eccentricity:     
0006325     
Arg of perigee:   348
3018  deg
Mean anomaly:      11
7998  deg
Mean motion:   15
76548165  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3043
Checksum:              310


Coasting Arc #5 (Orbit 3058)
---------------------------------------

Vector Time (GMT): 2009/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4714767
10                 A    =         6724894
51  meter
 Y    =       -4766232
79  meter          E    =           
0017342
 Z    =         372095
94                 I    =           51
43663
 XDOT =       3661
529323                 Wp   =           31
03242
 YDOT =      -3143
977646  meter/sec      RA   =          222
77492  deg
 ZDOT =       6013
700262                 TA   =          333
03170
                                          MA   =          333
12172
                                          Ha   =            187
103  n
mi
                                          Hp   =            179
771

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15468395
99                 X    =        -4662927
44
 Y    =      -15637246
67  feet           Y    =        -4818666
28  meter
 Z    =        1220787
20                 Z    =          349316
63
 XDOT =      12012
891481                 XDOT =        3667
199733
 YDOT =     -10314
887290  feet/sec       YDOT =       -3103
001192  meter/sec
 ZDOT =      19729
987737                 ZDOT =        6031
501719

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21386206
50                 X    =         6518515
74
 Y    =       -5161085
66  feet           Y    =        -1573098
91  meter
 Z    =        1130683
76                 Z    =          344632
41
 XDOT =       2300
955386                 XDOT =         701
331202
 YDOT =      13957
138325  feet/sec       YDOT =        4254
135762  meter/sec
 ZDOT =      19800
116795                 ZDOT =        6035
075599


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   09324
56272992  
00016717  00000-0  10270-3 0  9041
2 25544  51
6453 223
4095 0006428 352
8632   7
2440 15
76547500 30594


Satellite: ISS
Catalog Number: 25544
Epoch time:      09324
56272992   =   yrday
fracday
Element set:     904
Inclination:       51
6453  deg
RA of node:       223
4095  deg
Eccentricity:     
0006428     
Arg of perigee:   352
8632  deg
Mean anomaly:       7
2440  deg
Mean motion:   15
76547500  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3059
Checksum:              309


Coasting Arc #6 (Orbit 3073)
---------------------------------------

Vector Time (GMT): 2009/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3738501
20                 A    =         6713301
95  meter
 Y    =        2262978
02  meter          E    =           
0013902
 Z    =       -5106903
51                 I    =           51
42135
 XDOT =      -5235
192217                 Wp   =           74
50059
 YDOT =      -5459
585443  meter/sec      RA   =          217
58949  deg
 ZDOT =       1420
015175                 TA   =          209
11240
                                          MA   =          209
18997
                                          Ha   =            187
079  n
mi
                                          Hp   =            179
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12265423
89                 X    =        -3738719
60
 Y    =        7424468
58  feet           Y    =         2221171
17  meter
 Z    =      -16754932
78                 Z    =        -5125065
72
 XDOT =     -17175
827484                 XDOT =       -5180
651359
 YDOT =     -17912
025732  feet/sec       YDOT =       -5517
823631  meter/sec
 ZDOT =       4658
842438                 ZDOT =        1394
714210

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -308892
11                 X    =          -94150
31
 Y    =      -14250039
97  feet           Y    =        -4343412
18  meter
 Z    =      -16826528
94                 Z    =        -5128726
02
 XDOT =      23089
757470                 XDOT =        7037
758077
 YDOT =      -5857
035108  feet/sec       YDOT =       -1785
224301  meter/sec
 ZDOT =       4558
741741                 ZDOT =        1389
504483


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   09325
51351288  
00016717  00000-0  10270-3 0  9054
2 25544  51
6455 218
5087 0006395 355
8954   4
2157 15
76610381 30742


Satellite: ISS
Catalog Number: 25544
Epoch time:      09325
51351288   =   yrday
fracday
Element set:     905
Inclination:       51
6455  deg
RA of node:       218
5087  deg
Eccentricity:     
0006395     
Arg of perigee:   355
8954  deg
Mean anomaly:       4
2157  deg
Mean motion:   15
76610381  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3074
Checksum:              320


Coasting Arc #7 (Orbit 3089)
---------------------------------------

Vector Time (GMT): 2009/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4311558
05                 A    =         6722873
16  meter
 Y    =        4716858
81  meter          E    =           
0004279
 Z    =       -2093811
87                 I    =           51
47815
 XDOT =      -4943
593974                 Wp   =           72
56020
 YDOT =       2069
424074  meter/sec      RA   =          212
45136  deg
 ZDOT =      -5525
883666                 TA   =          130
89104
                                          MA   =          130
85396
                                          Ha   =            187
150  n
mi
                                          Hp   =            179
472

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14145531
66                 X    =         4268664
35
 Y    =       15475258
57  feet           Y    =         4764833
54  meter
 Z    =       -6869461
51                 Z    =        -2072969
86
 XDOT =     -16219
140335                 XDOT =       -4939
523137
 YDOT =       6789
449062  feet/sec       YDOT =        2014
165107  meter/sec
 ZDOT =     -18129
539586                 ZDOT =       -5549
889888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20425939
00                 X    =        -6225826
21
 Y    =        4846350
79  feet           Y    =         1477167
72  meter
 Z    =       -6786979
83                 Z    =        -2068671
45
 XDOT =       2276
655419                 XDOT =         693
924572
 YDOT =     -15889
130796  feet/sec       YDOT =       -4843
007067  meter/sec
 ZDOT =     -18224
220545                 ZDOT =       -5554
742422


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   09326
52765597  
00016717  00000-0  10270-3 0  9069
2 25544  51
6455 213
2806 0006283 358
4850   1
6294 15
76615465 30902


Satellite: ISS
Catalog Number: 25544
Epoch time:      09326
52765597   =   yrday
fracday
Element set:     906
Inclination:       51
6455  deg
RA of node:       213
2806  deg
Eccentricity:     
0006283     
Arg of perigee:   358
4850  deg
Mean anomaly:       1
6294  deg
Mean motion:   15
76615465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3090
Checksum:              325


Coasting Arc #8 (Orbit 3105)
---------------------------------------

Vector Time (GMT): 2009/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4882196
07                 A    =         6715925
31  meter
 Y    =       -1414240
87  meter          E    =           
0013246
 Z    =        4387376
16                 I    =           51
48190
 XDOT =       4520
531077                 Wp   =           42
28485
 YDOT =       5290
286729  meter/sec      RA   =          207
24109  deg
 ZDOT =      -3309
652022                 TA   =           81
08585
                                          MA   =           80
93592
                                          Ha   =            187
070  n
mi
                                          Hp   =            179
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16017703
65                 X    =         4876334
16
 Y    =       -4639897
87  feet           Y    =        -1359678
34  meter
 Z    =       14394278
74                 Z    =         4411079
83
 XDOT =      14831
138703                 XDOT =        4477
116077
 YDOT =      17356
583755  feet/sec       YDOT =        5340
595451  meter/sec
 ZDOT =     -10858
438391                 ZDOT =       -3287
796108

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3433962
92                 X    =        -1046671
90
 Y    =       16235831
99  feet           Y    =         4948681
59  meter
 Z    =       14487801
80                 Z    =         4415881
99
 XDOT =     -21148
664425                 XDOT =       -6446
112917
 YDOT =       5183
983043  feet/sec       YDOT =        1580
078031  meter/sec
 ZDOT =     -10771
916237                 ZDOT =       -3283
280069


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   09327
54177034  
00016717  00000-0  10270-3 0  9076
2 25544  51
6453 208
0523 0006525   2
2263 357
8929 15
76723749 31063


Satellite: ISS
Catalog Number: 25544
Epoch time:      09327
54177034   =   yrday
fracday
Element set:     907
Inclination:       51
6453  deg
RA of node:       208
0523  deg
Eccentricity:     
0006525     
Arg of perigee:     2
2263  deg
Mean anomaly:     357
8929  deg
Mean motion:   15
76723749  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3106
Checksum:              313


Coasting Arc #9 (Orbit 3121)
---------------------------------------

Vector Time (GMT): 2009/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3455630
67                 A    =         6718901
43  meter
 Y    =       -4489973
96  meter          E    =           
0014035
 Z    =        3595261
08                 I    =           51
51874
 XDOT =       6209
811877                 Wp   =           66
32335
 YDOT =      -1250
288050  meter/sec      RA   =          202
12480  deg
 ZDOT =       4399
279559                 TA   =          336
86830
                                          MA   =          336
93142
                                          Ha   =            187
335  n
mi
                                          Hp   =            178
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11337370
97                 X    =        -3422631
53
 Y    =      -14730885
70  feet           Y    =        -4528432
55  meter
 Z    =       11795475
98                 Z    =         3578553
31
 XDOT =      20373
398545                 XDOT =        6201
960090
 YDOT =      -4101
994914  feet/sec       YDOT =       -1180
890406  meter/sec
 ZDOT =      14433
331887                 ZDOT =        4429
428099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18314890
42                 X    =         5582378
60
 Y    =       -3414148
79  feet           Y    =        -1040632
55  meter
 Z    =       11729305
38                 Z    =         3575092
28
 XDOT =      -5871
872044                 XDOT =       -1789
746599
 YDOT =      18585
194201  feet/sec       YDOT =        5664
767193  meter/sec
 ZDOT =      14552
317157                 ZDOT =        4435
546269


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   09328
55586080  
00016717  00000-0  10270-3 0  9084
2 25544  51
6452 202
8235 0006540   6
6127 353
5123 15
76705939 31226


Satellite: ISS
Catalog Number: 25544
Epoch time:      09328
55586080   =   yrday
fracday
Element set:     908
Inclination:       51
6452  deg
RA of node:       202
8235  deg
Eccentricity:     
0006540     
Arg of perigee:     6
6127  deg
Mean anomaly:     353
5123  deg
Mean motion:   15
76705939  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3122
Checksum:              304


Coasting Arc #10 (Orbit 3136)
---------------------------------------

Vector Time (GMT): 2009/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5876987
88                 A    =         6719904
32  meter
 Y    =         826172
10  meter          E    =           
0009036
 Z    =       -3148505
54                 I    =           51
55110
 XDOT =      -3288
442381                 Wp   =           37
30169
 YDOT =      -5013
647187  meter/sec      RA   =          196
90965  deg
 ZDOT =       4836
883755                 TA   =          285
94235
                                          MA   =          286
04189
                                          Ha   =            187
156  n
mi
                                          Hp   =            178
753

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19281456
29                 X    =        -5870494
37
 Y    =        2710538
40  feet           Y    =          760488
60  meter
 Z    =      -10329742
60                 Z    =        -3177040
61
 XDOT =     -10788
852955                 XDOT =       -3255
631581
 YDOT =     -16448
973711  feet/sec       YDOT =       -5050
237241  meter/sec
 ZDOT =      15869
041190                 ZDOT =        4820
987729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6056163
78                 X    =         1845918
72
 Y    =      -18441926
02  feet           Y    =        -5621099
05  meter
 Z    =      -10442384
89                 Z    =        -3182838
91
 XDOT =      18218
352357                 XDOT =        5552
953798
 YDOT =      -2940
885306  feet/sec       YDOT =        -896
381841  meter/sec
 ZDOT =      15806
044854                 ZDOT =        4817
682471


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   09329
50654378  
00016717  00000-0  10270-3 0  9097
2 25544  51
6450 197
9217 0006515   8
0220 352
1048 15
76760685 31376


Satellite: ISS
Catalog Number: 25544
Epoch time:      09329
50654378   =   yrday
fracday
Element set:     909
Inclination:       51
6450  deg
RA of node:       197
9217  deg
Eccentricity:     
0006515     
Arg of perigee:     8
0220  deg
Mean anomaly:     352
1048  deg
Mean motion:   15
76760685  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3137
Checksum:              317


Coasting Arc #11 (Orbit 3152)
---------------------------------------

Vector Time (GMT): 2009/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2159677
07                 A    =         6714565
29  meter
 Y    =        4276811
02  meter          E    =           
0015526
 Z    =       -4718722
89                 I    =           51
56170
 XDOT =      -7181
663664                 Wp   =           50
20600
 YDOT =        670
023949  meter/sec      RA   =          191
79297  deg
 ZDOT =      -2675
692010                 TA   =          193
41180
                                          MA   =          193
45312
                                          Ha   =            187
241  n
mi
                                          Hp   =            178
669

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7085554
69                 X    =         2134615
66
 Y    =       14031532
22  feet           Y    =         4300821
85  meter
 Z    =      -15481374
31                 Z    =        -4708291
69
 XDOT =     -23561
888660                 XDOT =       -7175
623944
 YDOT =       2198
241302  feet/sec       YDOT =         589
748216  meter/sec
 ZDOT =      -8778
517092                 ZDOT =       -2710
566521

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15751360
29                 X    =        -4801014
62
 Y    =         513205
70  feet           Y    =          156425
10  meter
 Z    =      -15439987
08                 Z    =        -4706108
06
 XDOT =       8066
632179                 XDOT =        2458
709488
 YDOT =     -21057
027791  feet/sec       YDOT =       -6418
182071  meter/sec
 ZDOT =      -8916
210075                 ZDOT =       -2717
660831


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   09330
52058117  
00016717  00000-0  10270-3 0  9102
2 25544  51
6443 192
6927 0006499  11
3014 348
8296 15
76806756 31532


Satellite: ISS
Catalog Number: 25544
Epoch time:      09330
52058117   =   yrday
fracday
Element set:     910
Inclination:       51
6443  deg
RA of node:       192
6927  deg
Eccentricity:     
0006499     
Arg of perigee:    11
3014  deg
Mean anomaly:     348
8296  deg
Mean motion:   15
76806756  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3153
Checksum:              318


Coasting Arc #12 (Orbit 3168)
---------------------------------------

Vector Time (GMT): 2009/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6553901
79                 A    =         6723144
98  meter
 Y    =        -385745
61  meter          E    =           
0014165
 Z    =        1434699
82                 I    =           51
62122
 XDOT =       1565
323490                 Wp   =           92
27204
 YDOT =       4811
827203  meter/sec      RA   =          186
59812  deg
 ZDOT =      -5808
292165                 TA   =           71
92459
                                          MA   =           71
77033
                                          Ha   =            187
281  n
mi
                                          Hp   =            178
362

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21502302
47                 X    =         6550758
49
 Y    =       -1265569
60  feet           Y    =         -312473
65  meter
 Z    =        4707020
42                 Z    =         1466531
78
 XDOT =       5135
575753                 XDOT =        1539
616752
 YDOT =      15786
834656  feet/sec       YDOT =        4829
188070  meter/sec
 ZDOT =     -19056
076657                 ZDOT =       -5800
749898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7660821
70                 X    =        -2335018
45
 Y    =       20101326
89  feet           Y    =         6126884
44  meter
 Z    =        4832720
48                 Z    =         1473013
20
 XDOT =     -15083
097098                 XDOT =       -4597
327995
 YDOT =      -1136
800684  feet/sec       YDOT =        -346
496849  meter/sec
 ZDOT =     -19026
072897                 ZDOT =       -5799
147019


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   09331
53459335  
00016717  00000-0  10270-3 0  9112
2 25544  51
6446 187
4640 0006516  16
0878 344
0493 15
76845831 31690


Satellite: ISS
Catalog Number: 25544
Epoch time:      09331
53459335   =   yrday
fracday
Element set:     911
Inclination:       51
6446  deg
RA of node:       187
4640  deg
Eccentricity:     
0006516     
Arg of perigee:    16
0878  deg
Mean anomaly:     344
0493  deg
Mean motion:   15
76845831  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3169
Checksum:              326


Coasting Arc #13 (Orbit 3184)
---------------------------------------

Vector Time (GMT): 2009/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -517752
47                 A    =         6712043
77  meter
 Y    =       -4162293
42  meter          E    =           
0006824
 Z    =        5235635
05                 I    =           51
61302
 XDOT =       7685
439414                 Wp   =           44
37729
 YDOT =       -251
641247  meter/sec      RA   =          181
45766  deg
 ZDOT =        564
317839                 TA   =           40
29017
                                          MA   =           40
23962
                                          Ha   =            187
314  n
mi
                                          Hp   =            178
268

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1698662
94                 X    =         -496604
95
 Y    =      -13655818
32  feet           Y    =        -4167965
27  meter
 Z    =       17177280
34                 Z    =         5233170
89
 XDOT =      25214
696240                 XDOT =        7684
940677
 YDOT =       -825
594643  feet/sec       YDOT =        -165
700946  meter/sec
 ZDOT =       1851
436480                 ZDOT =         601
653489

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13256718
97                 X    =         4040647
94
 Y    =        3737221
63  feet           Y    =         1139105
15  meter
 Z    =       17167363
41                 Z    =         5232612
37
 XDOT =      -8917
550067                 XDOT =       -2718
069260
 YDOT =      22516
007590  feet/sec       YDOT =        6862
879113  meter/sec
 ZDOT =       1998
891015                 ZDOT =         609
261981


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   09332
54857896  
00016717  00000-0  10270-3 0  9129
2 25544  51
6436 182
2343 0006494  19
3226 340
8184 15
76868871 31858


Satellite: ISS
Catalog Number: 25544
Epoch time:      09332
54857896   =   yrday
fracday
Element set:     912
Inclination:       51
6436  deg
RA of node:       182
2343  deg
Eccentricity:     
0006494     
Arg of perigee:    19
3226  deg
Mean anomaly:     340
8184  deg
Mean motion:   15
76868871  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3185
Checksum:              341


Coasting Arc #14 (Orbit 3200)
---------------------------------------

Vector Time (GMT): 2009/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6696258
12                 A    =         6723786
12  meter
 Y    =          56180
65  meter          E    =           
0019036
 Z    =         475934
13                 I    =           51
68196
 XDOT =        396
547609                 Wp   =           40
89575
 YDOT =      -4796
829266  meter/sec      RA   =          176
29955  deg
 ZDOT =       6024
868269                 TA   =          324
28846
                                          MA   =          324
41564
                                          Ha   =            187
269  n
mi
                                          Hp   =            178
105

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21969350
79                 X    =        -6698700
73
 Y    =         184319
72  feet           Y    =          -18714
55  meter
 Z    =        1561463
69                 Z    =          443396
82
 XDOT =       1301
009217                 XDOT =         420
888541
 YDOT =     -15737
628824  feet/sec       YDOT =       -4792
259194  meter/sec
 ZDOT =      19766
628179                 ZDOT =        6026
853517

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8156199
41                 X    =         2486009
58
 Y    =      -20409498
01  feet           Y    =        -6220814
99  meter
 Z    =        1432940
62                 Z    =          436760
30
 XDOT =      12626
588893                 XDOT =        3848
584294
 YDOT =       6464
565280  feet/sec       YDOT =        1970
399497  meter/sec
 ZDOT =      19774
262828                 ZDOT =        6027
195310


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   09333
56253782  
00016717  00000-0  10270-3 0  9137
2 25544  51
6423 177
0042 0006478  22
1497 337
9947 15
76927148 32012


Satellite: ISS
Catalog Number: 25544
Epoch time:      09333
56253782   =   yrday
fracday
Element set:     913
Inclination:       51
6423  deg
RA of node:       177
0042  deg
Eccentricity:     
0006478     
Arg of perigee:    22
1497  deg
Mean anomaly:     337
9947  deg
Mean motion:   15
76927148  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3201
Checksum:              323


Coasting Arc #15 (Orbit 3215)
---------------------------------------

Vector Time (GMT): 2009/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1218166
47                 A    =         6712519
90  meter
 Y    =        4245200
72  meter          E    =           
0016472
 Z    =       -5068141
64                 I    =           51
67310
 XDOT =      -7508
621595                 Wp   =           80
33427
 YDOT =       -166
079836  meter/sec      RA   =          171
12520  deg
 ZDOT =       1672
947346                 TA   =          205
71493
                                          MA   =          205
79692
                                          Ha   =            187
278  n
mi
                                          Hp   =            177
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3996609
14                 X    =        -1240925
66
 Y    =       13927823
89  feet           Y    =         4231451
74  meter
 Z    =      -16627761
28                 Z    =        -5074114
50
 XDOT =     -24634
585287                 XDOT =       -7514
333513
 YDOT =       -544
881352  feet/sec       YDOT =        -250
077785  meter/sec
 ZDOT =       5488
672396                 ZDOT =        1636
455485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11562986
09                 X    =        -3524398
16
 Y    =       -8687645
35  feet           Y    =        -2647994
30  meter
 Z    =      -16651179
51                 Z    =        -5075279
52
 XDOT =       8825
330228                 XDOT =        2689
960654
 YDOT =     -21943
910592  feet/sec       YDOT =       -6688
503948  meter/sec
 ZDOT =       5344
503020                 ZDOT =        1629
004521


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   09334
51310148  
00016717  00000-0  10270-3 0  9144
2 25544  51
6409 172
1004 0006461  26
0847 334
0642 15
76970754 32161


Satellite: ISS
Catalog Number: 25544
Epoch time:      09334
51310148   =   yrday
fracday
Element set:     914
Inclination:       51
6409  deg
RA of node:       172
1004  deg
Eccentricity:     
0006461     
Arg of perigee:    26
0847  deg
Mean anomaly:     334
0642  deg
Mean motion:   15
76970754  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3216
Checksum:              289

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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