Date: September 1st 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 1776)
---------------------------------------

Vector Time (GMT): 2009/243/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4251951
70                 A    =         6720731
65  meter
 Y    =         -29406
97  meter          E    =           
0009917
 Z    =        5196962
76                 I    =           51
29087
 XDOT =       -882
775797                 Wp   =           55
74679
 YDOT =       7618
541549  meter/sec      RA   =          281
22348  deg
 ZDOT =        769
830353                 TA   =           26
92554
                                          MA   =           26
87411
                                          Ha   =            193
022  n
mi
                                          Hp   =            181
643

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13949972
77                 X    =         4226718
95
 Y    =         -96479
55  feet           Y    =           17999
69  meter
 Z    =       17050402
76                 Z    =         5217557
18
 XDOT =      -2896
246053                 XDOT =        -971
641677
 YDOT =      24995
215057  feet/sec       YDOT =        7608
172945  meter/sec
 ZDOT =       2525
690136                 ZDOT =         765
326147

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10591018
73                 X    =         3228142
51
 Y    =       -8925935
33  feet           Y    =        -2720625
09  meter
 Z    =       17131412
19                 Z    =         5221654
44
 XDOT =      13085
068382                 XDOT =        3988
328843
 YDOT =      20312
275210  feet/sec       YDOT =        6191
181484  meter/sec
 ZDOT =       2508
363210                 ZDOT =         764
549107


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   09243
21844157  
00020000  00000-0  20000-3 0  9009
2 25544  51
6380 281
6777 0008941  37
7731 322
4058 15
73842617 17773


Satellite: ISS
Catalog Number: 25544
Epoch time:      09243
21844157   =   yrday
fracday
Element set:     900
Inclination:       51
6380  deg
RA of node:       281
6777  deg
Eccentricity:     
0008941     
Arg of perigee:    37
7731  deg
Mean anomaly:     322
4058  deg
Mean motion:   15
73842617  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1777
Checksum:              304


Coasting Arc #2 (Orbit 1791)
---------------------------------------

Vector Time (GMT): 2009/244/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         139613
81                 A    =         6732293
97  meter
 Y    =       -6684836
29  meter          E    =           
0019499
 Z    =        -707111
84                 I    =           51
32663
 XDOT =       4853
159365                 Wp   =           40
75356
 YDOT =       -517
936561  meter/sec      RA   =          276
05209  deg
 ZDOT =       5961
484655                 TA   =          311
50473
                                          MA   =          311
67190
                                          Ha   =            193
103  n
mi
                                          Hp   =            181
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         458050
54                 X    =          217789
39
 Y    =      -21931877
58  feet           Y    =        -6682837
94  meter
 Z    =       -2319920
75                 Z    =         -706243
71
 XDOT =      15922
438863                 XDOT =        4829
630924
 YDOT =      -1699
266933  feet/sec       YDOT =        -463
797224  meter/sec
 ZDOT =      19558
676690                 ZDOT =        5985
003815

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13947594
66                 X    =        -4251226
85
 Y    =      -16932095
51  feet           Y    =        -5160902
71  meter
 Z    =       -2316860
26                 Z    =         -706179
01
 XDOT =       9639
846449                 XDOT =        2938
225198
 YDOT =     -10581
590397  feet/sec       YDOT =       -3225
268753  meter/sec
 ZDOT =      19651
168867                 ZDOT =        5989
676271


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   09244
17085959  
00020000  00000-0  20000-3 0  9013
2 25544  51
6390 276
7878 0008858  41
9620 318
2221 15
73882500 17929


Satellite: ISS
Catalog Number: 25544
Epoch time:      09244
17085959   =   yrday
fracday
Element set:     901
Inclination:       51
6390  deg
RA of node:       276
7878  deg
Eccentricity:     
0008858     
Arg of perigee:    41
9620  deg
Mean anomaly:     318
2221  deg
Mean motion:   15
73882500  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1792
Checksum:              314


Coasting Arc #3 (Orbit 1807)
---------------------------------------

Vector Time (GMT): 2009/245/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4187924
37                 A    =         6720574
98  meter
 Y    =         841896
21  meter          E    =           
0022450
 Z    =       -5207365
52                 I    =           51
28549
 XDOT =       -524
906377                 Wp   =           69
54458
 YDOT =      -7624
097432  meter/sec      RA   =          270
90835  deg
 ZDOT =       -805
554541                 TA   =          192
70609
                                          MA   =          192
76277
                                          Ha   =            193
165  n
mi
                                          Hp   =            181
120

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13739909
34                 X    =        -4171731
26
 Y    =        2762126
67  feet           Y    =          795154
80  meter
 Z    =      -17084532
54                 Z    =        -5227670
85
 XDOT =      -1722
133782                 XDOT =        -435
700212
 YDOT =     -25013
443017  feet/sec       YDOT =       -7629
468483  meter/sec
 ZDOT =      -2642
895477                 ZDOT =        -807
887656

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8347553
42                 X    =        -2544334
28
 Y    =       11135465
25  feet           Y    =         3394089
81  meter
 Z    =      -17164366
29                 Z    =        -5231698
85
 XDOT =     -17101
058059                 XDOT =       -5212
402496
 YDOT =     -16932
929166  feet/sec       YDOT =       -5161
156810  meter/sec
 ZDOT =      -2652
492113                 ZDOT =        -808
479596


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   09245
18676352  
00020000  00000-0  20000-3 0  9029
2 25544  51
6390 271
5723 0008949  45
9080 314
2818 15
73913829 18081


Satellite: ISS
Catalog Number: 25544
Epoch time:      09245
18676352   =   yrday
fracday
Element set:     902
Inclination:       51
6390  deg
RA of node:       271
5723  deg
Eccentricity:     
0008949     
Arg of perigee:    45
9080  deg
Mean anomaly:     314
2818  deg
Mean motion:   15
73913829  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1808
Checksum:              312


Coasting Arc #4 (Orbit 1823)
---------------------------------------

Vector Time (GMT): 2009/246/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1049692
61                 A    =         6732181
88  meter
 Y    =        6610408
50  meter          E    =           
0017461
 Z    =         693457
86                 I    =           51
32467
 XDOT =      -4677
769448                 Wp   =           97
72346
 YDOT =       1380
810003  meter/sec      RA   =          265
73416  deg
 ZDOT =      -5956
091612                 TA   =           74
69122
                                          MA   =           74
49830
                                          Ha   =            193
174  n
mi
                                          Hp   =            181
190

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3443873
40                 X    =          972327
22
 Y    =       21687691
94  feet           Y    =         6621714
24  meter
 Z    =        2275124
22                 Z    =          698369
01
 XDOT =     -15347
012625                 XDOT =       -4663
928984
 YDOT =       4530
216544  feet/sec       YDOT =        1328
577568  meter/sec
 ZDOT =     -19540
982979                 ZDOT =       -5978
782371

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17224751
74                 X    =         5250104
33
 Y    =       13617421
44  feet           Y    =         4150590
05  meter
 Z    =        2294819
55                 Z    =          699461
00
 XDOT =      -7134
017812                 XDOT =       -2174
448629
 YDOT =      12400
878933  feet/sec       YDOT =        3779
787899  meter/sec
 ZDOT =     -19630
171018                 ZDOT =       -5983
276126


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   09246
20265693  
00020000  00000-0  20000-3 0  9036
2 25544  51
6381 266
3541 0008887  49
0099 311
1832 15
73924204 18246


Satellite: ISS
Catalog Number: 25544
Epoch time:      09246
20265693   =   yrday
fracday
Element set:     903
Inclination:       51
6381  deg
RA of node:       266
3541  deg
Eccentricity:     
0008887     
Arg of perigee:    49
0099  deg
Mean anomaly:     311
1832  deg
Mean motion:   15
73924204  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1824
Checksum:              294


Coasting Arc #5 (Orbit 1839)
---------------------------------------

Vector Time (GMT): 2009/247/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3955865
58                 A    =         6720456
91  meter
 Y    =       -1574546
75  meter          E    =           
0010541
 Z    =        5190743
72                 I    =           51
28985
 XDOT =       1892
349739                 Wp   =           69
03191
 YDOT =       7429
013586  meter/sec      RA   =          260
58931  deg
 ZDOT =        813
736955                 TA   =           13
20773
                                          MA   =           13
18016
                                          Ha   =            193
048  n
mi
                                          Hp   =            181
085

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12978561
60                 X    =         3947962
95
 Y    =       -5165835
80  feet           Y    =        -1530353
80  meter
 Z    =       17029999
08                 Z    =         5209942
04
 XDOT =       6208
496519                 XDOT =        1805
183635
 YDOT =      24373
404153  feet/sec       YDOT =        7449
687632  meter/sec
 ZDOT =       2669
740665                 ZDOT =         822
717724

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5749376
50                 X    =         1752409
96
 Y    =      -12629272
93  feet           Y    =        -3849402
39  meter
 Z    =       17105435
52                 Z    =         5213736
75
 XDOT =      20388
030997                 XDOT =        6214
271848
 YDOT =      12935
288191  feet/sec       YDOT =        3942
675841  meter/sec
 ZDOT =       2705
505542                 ZDOT =         824
638089


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   09247
21854050  
00020000  00000-0  20000-3 0  9040
2 25544  51
6391 261
1375 0008868  52
5730 307
6238 15
73949812 18405


Satellite: ISS
Catalog Number: 25544
Epoch time:      09247
21854050   =   yrday
fracday
Element set:     904
Inclination:       51
6391  deg
RA of node:       261
1375  deg
Eccentricity:     
0008868     
Arg of perigee:    52
5730  deg
Mean anomaly:     307
6238  deg
Mean motion:   15
73949812  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1840
Checksum:              297


Coasting Arc #6 (Orbit 1854)
---------------------------------------

Vector Time (GMT): 2009/248/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2238887
53                 A    =         6732113
93  meter
 Y    =       -6299416
20  meter          E    =           
0019310
 Z    =        -725724
88                 I    =           51
33592
 XDOT =       4348
843831                 Wp   =           47
51277
 YDOT =      -2219
003667  meter/sec      RA   =          255
41692  deg
 ZDOT =       5958
398737                 TA   =          304
54285
                                          MA   =          304
72496
                                          Ha   =            193
239  n
mi
                                          Hp   =            180
963

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7345431
54                 X    =        -2164754
55
 Y    =      -20667376
00  feet           Y    =        -6324038
32  meter
 Z    =       -2380987
13                 Z    =         -736420
80
 XDOT =      14267
860338                 XDOT =        4344
389208
 YDOT =      -7280
195759  feet/sec       YDOT =       -2170
396798  meter/sec
 ZDOT =      19548
552286                 ZDOT =        5979
514663

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19740820
88                 X    =        -6017002
21
 Y    =       -9549440
22  feet           Y    =        -2910669
38  meter
 Z    =       -2423443
23                 Z    =         -738665
50
 XDOT =       4255
645890                 XDOT =        1297
120867
 YDOT =     -13686
650677  feet/sec       YDOT =       -4171
691126  meter/sec
 ZDOT =      19631
493042                 ZDOT =        5983
679079


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   09248
17092259  
00020000  00000-0  20000-3 0  9052
2 25544  51
6398 256
2473 0008961  56
5720 303
6299 15
73937999 18555


Satellite: ISS
Catalog Number: 25544
Epoch time:      09248
17092259   =   yrday
fracday
Element set:     905
Inclination:       51
6398  deg
RA of node:       256
2473  deg
Eccentricity:     
0008961     
Arg of perigee:    56
5720  deg
Mean anomaly:     303
6299  deg
Mean motion:   15
73937999  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1855
Checksum:              339


Coasting Arc #7 (Orbit 1870)
---------------------------------------

Vector Time (GMT): 2009/249/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3623951
74                 A    =         6720428
28  meter
 Y    =        2257181
54  meter          E    =           
0023171
 Z    =       -5209993
18                 I    =           51
30565
 XDOT =      -3174
108524                 Wp   =           74
86585
 YDOT =      -6951
514011  meter/sec      RA   =          250
27342  deg
 ZDOT =       -800
853764                 TA   =          187
44270
                                          MA   =          187
47716
                                          Ha   =            193
255  n
mi
                                          Hp   =            180
719

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11889605
46                 X    =        -3623613
38
 Y    =        7405451
25  feet           Y    =         2216657
85  meter
 Z    =      -17093153
48                 Z    =        -5227597
70
 XDOT =     -10413
741878                 XDOT =       -3092
249186
 YDOT =     -22806
804498  feet/sec       YDOT =       -6986
551125  meter/sec
 ZDOT =      -2627
472979                 ZDOT =        -816
074188

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2948723
89                 X    =         -898771
04
 Y    =       13606639
22  feet           Y    =         4147303
63  meter
 Z    =      -17162276
03                 Z    =        -5231061
73
 XDOT =     -22583
782408                 XDOT =       -6883
536878
 YDOT =      -8296
633543  feet/sec       YDOT =       -2528
813904  meter/sec
 ZDOT =      -2687
776545                 ZDOT =        -819
234291


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   09249
18678591  
00020000  00000-0  20000-3 0  9064
2 25544  51
6400 251
0310 0008947  60
0380 300
1670 15
73967232 18714


Satellite: ISS
Catalog Number: 25544
Epoch time:      09249
18678591   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:       251
0310  deg
Eccentricity:     
0008947     
Arg of perigee:    60
0380  deg
Mean anomaly:     300
1670  deg
Mean motion:   15
73967232  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1871
Checksum:              280


Coasting Arc #8 (Orbit 1886)
---------------------------------------

Vector Time (GMT): 2009/250/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3294408
90                 A    =         6732042
81  meter
 Y    =        5827421
42  meter          E    =           
0019112
 Z    =         668889
57                 I    =           51
35648
 XDOT =      -3906
590037                 Wp   =          103
21426
 YDOT =       2908
941243  meter/sec      RA   =          245
10154  deg
 ZDOT =      -5963
713182                 TA   =           69
47223
                                          MA   =           69
26723
                                          Ha   =            193
272  n
mi
                                          Hp   =            180
760

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10808428
16                 X    =         3225751
46
 Y    =       19118836
67  feet           Y    =         5863877
60  meter
 Z    =        2194519
59                 Z    =          684726
67
 XDOT =     -12816
896447                 XDOT =       -3909
857185
 YDOT =       9543
770481  feet/sec       YDOT =        2865
236732  meter/sec
 ZDOT =     -19565
988129                 ZDOT =       -5982
699645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21311012
93                 X    =         6495596
74
 Y    =        5283350
17  feet           Y    =         1610365
13  meter
 Z    =        2257186
31                 Z    =          687990
39
 XDOT =      -1401
634179                 XDOT =        -427
218098
 YDOT =      14233
368200  feet/sec       YDOT =        4338
330627  meter/sec
 ZDOT =     -19640
507167                 ZDOT =       -5986
426585


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   09250
20263881  
00020000  00000-0  20000-3 0  9072
2 25544  51
6403 245
8134 0008929  64
3374 295
8711 15
73976075 18870


Satellite: ISS
Catalog Number: 25544
Epoch time:      09250
20263881   =   yrday
fracday
Element set:     907
Inclination:       51
6403  deg
RA of node:       245
8134  deg
Eccentricity:     
0008929     
Arg of perigee:    64
3374  deg
Mean anomaly:     295
8711  deg
Mean motion:   15
73976075  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1887
Checksum:              314


Coasting Arc #9 (Orbit 1902)
---------------------------------------

Vector Time (GMT): 2009/251/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3174736
73                 A    =         6720193
71  meter
 Y    =       -2820419
00  meter          E    =           
0011143
 Z    =        5198727
32                 I    =           51
33178
 XDOT =       4358
243342                 Wp   =           80
54401
 YDOT =       6314
065583  meter/sec      RA   =          239
95830  deg
 ZDOT =        764
458136                 TA   =            2
16278
                                          MA   =            2
15797
                                          Ha   =            193
094  n
mi
                                          Hp   =            180
654

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10415802
92                 X    =         3180784
49
 Y    =       -9253343
17  feet           Y    =        -2784883
08  meter
 Z    =       17056192
01                 Z    =         5214165
20
 XDOT =      14298
698630                 XDOT =        4283
600824
 YDOT =      20715
438264  feet/sec       YDOT =        6362
384723  meter/sec
 ZDOT =       2508
064750                 ZDOT =         785
448961

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         120703
64                 X    =           36790
47
 Y    =      -13857455
77  feet           Y    =        -4223752
52  meter
 Z    =       17116756
31                 Z    =         5217187
32
 XDOT =      23919
210454                 XDOT =        7290
575346
 YDOT =       3407
117683  feet/sec       YDOT =        1038
489470  meter/sec
 ZDOT =       2591
042819                 ZDOT =         789
749851


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   09251
21847913  
00020000  00000-0  20000-3 0  9089
2 25544  51
6412 240
5966 0008900  67
4662 292
7442 15
74035415 19039


Satellite: ISS
Catalog Number: 25544
Epoch time:      09251
21847913   =   yrday
fracday
Element set:     908
Inclination:       51
6412  deg
RA of node:       240
5966  deg
Eccentricity:     
0008900     
Arg of perigee:    67
4662  deg
Mean anomaly:     292
7442  deg
Mean motion:   15
74035415  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1903
Checksum:              290


Coasting Arc #10 (Orbit 1917)
---------------------------------------

Vector Time (GMT): 2009/252/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4278805
46                 A    =         6731987
06  meter
 Y    =       -5146928
00  meter          E    =           
0019055
 Z    =        -661608
45                 I    =           51
38756
 XDOT =       3344
893405                 Wp   =           54
17213
 YDOT =      -3531
494011  meter/sec      RA   =          234
79005  deg
 ZDOT =       5971
484129                 TA   =          298
59573
                                          MA   =          298
78732
                                          Ha   =            193
303  n
mi
                                          Hp   =            180
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14038075
66                 X    =        -4217719
60
 Y    =      -16886246
73  feet           Y    =        -5194434
60  meter
 Z    =       -2170631
41                 Z    =         -682246
52
 XDOT =      10974
059727                 XDOT =        3355
125871
 YDOT =     -11586
266439  feet/sec       YDOT =       -3494
031980  meter/sec
 ZDOT =      19591
483362                 ZDOT =        5987
758800

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21941565
35                 X    =        -6687789
12
 Y    =        -648112
22  feet           Y    =         -197544
61  meter
 Z    =       -2252154
15                 Z    =         -686456
59
 XDOT =      -1555
329928                 XDOT =        -474
064562
 YDOT =     -14207
991832  feet/sec       YDOT =       -4330
595910  meter/sec
 ZDOT =      19655
298693                 ZDOT =        5990
935042


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   09252
17082188  
00020000  00000-0  20000-3 0  9091
2 25544  51
6415 235
7066 0009050  70
4985 289
7155 15
73993486 19181


Satellite: ISS
Catalog Number: 25544
Epoch time:      09252
17082188   =   yrday
fracday
Element set:     909
Inclination:       51
6415  deg
RA of node:       235
7066  deg
Eccentricity:     
0009050     
Arg of perigee:    70
4985  deg
Mean anomaly:     289
7155  deg
Mean motion:   15
73993486  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1918
Checksum:              324


Coasting Arc #11 (Orbit 1933)
---------------------------------------

Vector Time (GMT): 2009/253/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2673381
31                 A    =         6720236
16  meter
 Y    =        3304287
14  meter          E    =           
0023615
 Z    =       -5225864
12                 I    =           51
36631
 XDOT =      -5367
604525                 Wp   =           80
87311
 YDOT =      -5452
697273  meter/sec      RA   =          229
64887  deg
 ZDOT =       -700
833454                 TA   =          182
41552
                                          MA   =          182
42695
                                          Ha   =            193
276  n
mi
                                          Hp   =            180
463

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8770936
04                 X    =        -2684745
14
 Y    =       10840837
06  feet           Y    =         3274328
17  meter
 Z    =      -17145223
49                 Z    =        -5238879
21
 XDOT =     -17610
251066                 XDOT =       -5302
828030
 YDOT =     -17889
426750  feet/sec       YDOT =       -5512
358813  meter/sec
 ZDOT =      -2299
322355                 ZDOT =        -726
752104

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2631426
08                 X    =          802058
67
 Y    =       13630002
75  feet           Y    =         4154424
84  meter
 Z    =      -17196231
49                 Z    =        -5241411
36
 XDOT =     -24034
843453                 XDOT =       -7325
820284
 YDOT =       1606
090862  feet/sec       YDOT =         489
536495  meter/sec
 ZDOT =      -2401
648985                 ZDOT =        -732
022611


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   09253
18664150  
00020000  00000-0  20000-3 0  9100
2 25544  51
6415 230
4902 0008928  74
5093 285
7055 15
74018564 19349


Satellite: ISS
Catalog Number: 25544
Epoch time:      09253
18664150   =   yrday
fracday
Element set:     910
Inclination:       51
6415  deg
RA of node:       230
4902  deg
Eccentricity:     
0008928     
Arg of perigee:    74
5093  deg
Mean anomaly:     285
7055  deg
Mean motion:   15
74018564  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1934
Checksum:              291


Coasting Arc #12 (Orbit 1949)
---------------------------------------

Vector Time (GMT): 2009/254/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5084199
01                 A    =         6731926
72  meter
 Y    =        4367802
76  meter          E    =           
0020297
 Z    =         559680
00                 I    =           51
42554
 XDOT =      -2750
310352                 Wp   =          109
16404
 YDOT =       3990
146544  meter/sec      RA   =          224
48418  deg
 ZDOT =      -5985
659241                 TA   =           64
72613
                                          MA   =           64
51594
                                          Ha   =            193
310  n
mi
                                          Hp   =            180
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16680442
96                 X    =         5032260
77
 Y    =       14330061
55  feet           Y    =         4424366
86  meter
 Z    =        1836220
47                 Z    =          584253
08
 XDOT =      -9023
327926                 XDOT =       -2765
646957
 YDOT =      13091
031968  feet/sec       YDOT =        3959
305208  meter/sec
 ZDOT =     -19637
989635                 ZDOT =       -5999
057609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21656105
26                 X    =         6600780
88
 Y    =       -3772984
17  feet           Y    =        -1150005
58  meter
 Z    =        1933194
81                 Z    =          589237
78
 XDOT =       4177
240080                 XDOT =        1273
222776
 YDOT =      13616
471703  feet/sec       YDOT =        4150
300575  meter/sec
 ZDOT =     -19690
467782                 ZDOT =       -6001
654580


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   09254
20245002  
00020000  00000-0  20000-3 0  9116
2 25544  51
6407 225
2735 0009053  78
9933 281
2248 15
74036566 19502


Satellite: ISS
Catalog Number: 25544
Epoch time:      09254
20245002   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:       225
2735  deg
Eccentricity:     
0009053     
Arg of perigee:    78
9933  deg
Mean anomaly:     281
2248  deg
Mean motion:   15
74036566  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1950
Checksum:              280


Coasting Arc #13 (Orbit 1965)
---------------------------------------

Vector Time (GMT): 2009/255/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2109604
53                 A    =         6719938
61  meter
 Y    =       -3656134
40  meter          E    =           
0011497
 Z    =        5218881
06                 I    =           51
40837
 XDOT =       6243
215939                 Wp   =           90
66180
 YDOT =       4482
768658  meter/sec      RA   =          219
34331  deg
 ZDOT =        615
482100                 TA   =          353
46903
                                          MA   =          353
48401
                                          Ha   =            193
115  n
mi
                                          Hp   =            180
392

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6921274
71                 X    =         2124978
78
 Y    =      -11995191
61  feet           Y    =        -3632457
67  meter
 Z    =       17122313
19                 Z    =         5229166
86
 XDOT =      20482
991927                 XDOT =        6189
634923
 YDOT =      14707
246252  feet/sec       YDOT =        4552
284374  meter/sec
 ZDOT =       2019
298227                 ZDOT =         645
681668

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5152782
83                 X    =        -1570568
21
 Y    =      -12800679
92  feet           Y    =        -3901647
24  meter
 Z    =       17162566
74                 Z    =         5231150
34
 XDOT =      23313
651263                 XDOT =        7106
000905
 YDOT =      -6511
869129  feet/sec       YDOT =       -1984
817711  meter/sec
 ZDOT =       2138
436752                 ZDOT =         651
795522


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   09255
21824409  
00020000  00000-0  20000-3 0  9123
2 25544  51
6411 220
0563 0008936  82
2136 278
0042 15
74101959 19663


Satellite: ISS
Catalog Number: 25544
Epoch time:      09255
21824409   =   yrday
fracday
Element set:     912
Inclination:       51
6411  deg
RA of node:       220
0563  deg
Eccentricity:     
0008936     
Arg of perigee:    82
2136  deg
Mean anomaly:     278
0042  deg
Mean motion:   15
74101959  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1966
Checksum:              278


Coasting Arc #14 (Orbit 1980)
---------------------------------------

Vector Time (GMT): 2009/256/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5766015
93                 A    =         6731907
08  meter
 Y    =       -3427116
55  meter          E    =           
0018690
 Z    =        -508031
20                 I    =           51
47165
 XDOT =       2078
715040                 Wp   =           60
73100
 YDOT =      -4360
528001  meter/sec      RA   =          214
18320  deg
 ZDOT =       5997
072430                 TA   =          293
72904
                                          MA   =          293
92500
                                          Ha   =            193
275  n
mi
                                          Hp   =            180
419

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18917375
08                 X    =        -5724796
85
 Y    =      -11243820
69  feet           Y    =        -3491365
05  meter
 Z    =       -1666769
04                 Z    =         -535942
39
 XDOT =       6819
931234                 XDOT =        2098
188059
 YDOT =     -14306
194230  feet/sec       YDOT =       -4337
173771  meter/sec
 ZDOT =      19675
434482                 ZDOT =        6007
218071

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20424898
28                 X    =        -6225509
00
 Y    =        8169151
33  feet           Y    =         2489957
32  meter
 Z    =       -1776850
99                 Z    =         -541584
18
 XDOT =      -6681
559327                 XDOT =       -2036
539283
 YDOT =     -12534
068726  feet/sec       YDOT =       -3820
384148  meter/sec
 ZDOT =      19715
094288                 ZDOT =        6009
160739


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   09256
17054268  
00020000  00000-0  20000-3 0  9138
2 25544  51
6406 215
1661 0009042  84
4196 275
7998 15
74048457 19814


Satellite: ISS
Catalog Number: 25544
Epoch time:      09256
17054268   =   yrday
fracday
Element set:     913
Inclination:       51
6406  deg
RA of node:       215
1661  deg
Eccentricity:     
0009042     
Arg of perigee:    84
4196  deg
Mean anomaly:     275
7998  deg
Mean motion:   15
74048457  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1981
Checksum:              314


Coasting Arc #15 (Orbit 1996)
---------------------------------------

Vector Time (GMT): 2009/257/04:04:04
831
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1544020
02                 A    =         6719983
13  meter
 Y    =        3927187
58  meter          E    =           
0023837
 Z    =       -5250407
51                 I    =           51
45617
 XDOT =      -6886
412392                 Wp   =           87
33105
 YDOT =      -3371
041669  meter/sec      RA   =          209
04400  deg
 ZDOT =       -497
185270                 TA   =          177
92812
                                          MA   =          177
91822
                                          Ha   =            193
228  n
mi
                                          Hp   =            180
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5065682
47                 X    =        -1562314
36
 Y    =       12884473
67  feet           Y    =         3909819
12  meter
 Z    =      -17225746
43                 Z    =        -5257952
78
 XDOT =     -22593
216508                 XDOT =       -6845
789785
 YDOT =     -11059
847995  feet/sec       YDOT =       -3447
822452  meter/sec
 ZDOT =      -1631
185270                 ZDOT =        -530
540581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7408591
38                 X    =         2258138
65
 Y    =       11651955
51  feet           Y    =         3551516
04  meter
 Z    =      -17255197
70                 Z    =        -5259384
26
 XDOT =     -21469
056911                 XDOT =       -6543
768546
 YDOT =      11044
295350  feet/sec       YDOT =        3366
301223  meter/sec
 ZDOT =      -1762
712710                 ZDOT =        -537
274834


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   09257
18631463  
00020000  00000-0  20000-3 0  9149
2 25544  51
6397 209
9488 0008945  88
9224 271
2964 15
74078605 19972


Satellite: ISS
Catalog Number: 25544
Epoch time:      09257
18631463   =   yrday
fracday
Element set:     914
Inclination:       51
6397  deg
RA of node:       209
9488  deg
Eccentricity:     
0008945     
Arg of perigee:    88
9224  deg
Mean anomaly:     271
2964  deg
Mean motion:   15
74078605  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1997
Checksum:              343

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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