Date: June 26th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11302 11 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 710)
---------------------------------------

Vector Time (GMT): 2009/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1498042
88                 A    =         6731140
10  meter
 Y    =        6331888
25  meter          E    =           
0021821
 Z    =        1675120
37                 I    =           51
32539
 XDOT =      -4500
873492                 Wp   =          128
09474
 YDOT =       2582
919116  meter/sec      RA   =          268
58121  deg
 ZDOT =      -5701
287484                 TA   =           33
28183
                                          MA   =           33
14480
                                          Ha   =            192
726  n
mi
                                          Hp   =            181
808

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4914838
85                 X    =         1418989
97
 Y    =       20773911
59  feet           Y    =         6348197
89  meter
 Z    =        5495801
75                 Z    =         1682207
06
 XDOT =     -14766
645314                 XDOT =       -4501
726156
 YDOT =       8474
144082  feet/sec       YDOT =        2532
584127  meter/sec
 ZDOT =     -18705
011431                 ZDOT =       -5723
153989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20590002
34                 X    =         6275832
71
 Y    =       -5608336
88  feet           Y    =        -1709421
08  meter
 Z    =        5523879
19                 Z    =         1683678
38
 XDOT =       8573
645567                 XDOT =        2613
247169
 YDOT =      12850
143599  feet/sec       YDOT =        3916
723769  meter/sec
 ZDOT =     -18790
607319                 ZDOT =       -5727
377111


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   09175
53508363  
00010596  00000-0  82463-4 0  9005
2 25544  51
6420 269
1845 0008574 148
7064 211
4611 15
73933443  7116


Satellite: ISS
Catalog Number: 25544
Epoch time:      09175
53508363   =   yrday
fracday
Element set:     900
Inclination:       51
6420  deg
RA of node:       269
1845  deg
Eccentricity:     
0008574     
Arg of perigee:   148
7064  deg
Mean anomaly:     211
4611  deg
Mean motion:   15
73933443  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             711
Checksum:              301


Coasting Arc #2 (Orbit 726)
---------------------------------------

Vector Time (GMT): 2009/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3705769
15                 A    =         6721339
84  meter
 Y    =       -2599191
78  meter          E    =           
0013766
 Z    =        4964395
55                 I    =           51
29513
 XDOT =       2364
930073                 Wp   =          141
25590
 YDOT =       7075
252956  meter/sec      RA   =          263
45390  deg
 ZDOT =       1925
537047                 TA   =          289
99144
                                          MA   =          290
13962
                                          Ha   =            192
441  n
mi
                                          Hp   =            181
888

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12158035
27                 X    =         3710442
56
 Y    =       -8527532
09  feet           Y    =        -2557726
45  meter
 Z    =       16287386
99                 Z    =         4982408
81
 XDOT =       7758
956933                 XDOT =        2276
283858
 YDOT =      23212
772166  feet/sec       YDOT =        7101
203001  meter/sec
 ZDOT =       6317
378764                 ZDOT =        1936
811635

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9145938
37                 X    =        -2787682
01
 Y    =      -11601173
40  feet           Y    =        -3536037
65  meter
 Z    =       16357878
45                 Z    =         4985881
35
 XDOT =      21931
693403                 XDOT =        6684
780149
 YDOT =      -8257
606797  feet/sec       YDOT =       -2516
918552  meter/sec
 ZDOT =       6361
924829                 ZDOT =        1939
114688


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   09176
55093721  
00010596  00000-0  82463-4 0  9016
2 25544  51
6421 263
9678 0008399 152
8650 207
2953 15
74002171  7270


Satellite: ISS
Catalog Number: 25544
Epoch time:      09176
55093721   =   yrday
fracday
Element set:     901
Inclination:       51
6421  deg
RA of node:       263
9678  deg
Eccentricity:     
0008399     
Arg of perigee:   152
8650  deg
Mean anomaly:     207
2953  deg
Mean motion:   15
74002171  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             727
Checksum:              316


Coasting Arc #3 (Orbit 741)
---------------------------------------

Vector Time (GMT): 2009/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2605930
85                 A    =         6731033
63  meter
 Y    =       -5980567
17  meter          E    =           
0008184
 Z    =       -1668230
21                 I    =           51
33148
 XDOT =       3968
355254                 Wp   =           99
02992
 YDOT =      -3312
001704  meter/sec      RA   =          258
26408  deg
 ZDOT =       5697
053322                 TA   =          242
46970
                                          MA   =          242
55289
                                          Ha   =            192
428  n
mi
                                          Hp   =            182
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8549641
90                 X    =        -2530757
61
 Y    =      -19621283
38  feet           Y    =        -6009287
65  meter
 Z    =       -5473196
23                 Z    =        -1680707
94
 XDOT =      13019
538236                 XDOT =        3977
420812
 YDOT =     -10866
147322  feet/sec       YDOT =       -3267
575392  meter/sec
 ZDOT =      18691
119824                 ZDOT =        5716
352859

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18982709
24                 X    =        -5785929
78
 Y    =        9859343
06  feet           Y    =         3005127
76  meter
 Z    =       -5522419
72                 Z    =        -1683233
53
 XDOT =     -11016
958328                 XDOT =       -3357
968898
 YDOT =     -10741
017510  feet/sec       YDOT =       -3273
862137  meter/sec
 ZDOT =      18766
617864                 ZDOT =        5720
065125


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   09177
50328800  
00010596  00000-0  82463-4 0  9022
2 25544  51
6414 259
0779 0008142 155
7789 204
3759 15
73965589  7420


Satellite: ISS
Catalog Number: 25544
Epoch time:      09177
50328800   =   yrday
fracday
Element set:     902
Inclination:       51
6414  deg
RA of node:       259
0779  deg
Eccentricity:     
0008142     
Arg of perigee:   155
7789  deg
Mean anomaly:     204
3759  deg
Mean motion:   15
73965589  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             742
Checksum:              342


Coasting Arc #4 (Orbit 757)
---------------------------------------

Vector Time (GMT): 2009/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3226999
52                 A    =         6721261
19  meter
 Y    =        3149856
50  meter          E    =           
0016288
 Z    =       -4996200
63                 I    =           51
30505
 XDOT =      -3546
150818                 Wp   =          106
16551
 YDOT =      -6566
191120  meter/sec      RA   =          253
13639  deg
 ZDOT =      -1858
717443                 TA   =          145
84800
                                          MA   =          145
74311
                                          Ha   =            192
271  n
mi
                                          Hp   =            182
122

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10587268
76                 X    =        -3237711
53
 Y    =       10334174
87  feet           Y    =         3113711
06  meter
 Z    =      -16391734
34                 Z    =        -5011902
84
 XDOT =     -11634
353077                 XDOT =       -3463
433777
 YDOT =     -21542
621784  feet/sec       YDOT =       -6605
383517  meter/sec
 ZDOT =      -6098
154340                 ZDOT =       -1875
744398

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11203405
07                 X    =         3414797
86
 Y    =        9557847
34  feet           Y    =         2913231
87  meter
 Z    =      -16453135
08                 Z    =        -5014915
57
 XDOT =     -19760
738378                 XDOT =       -6023
073058
 YDOT =      12603
244233  feet/sec       YDOT =        3841
468842  meter/sec
 ZDOT =      -6165
256632                 ZDOT =       -1879
170222


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   09178
51911306  
00010596  00000-0  82463-4 0  9034
2 25544  51
6404 253
8609 0008213 159
8925 200
2564 15
74000737  7581


Satellite: ISS
Catalog Number: 25544
Epoch time:      09178
51911306   =   yrday
fracday
Element set:     903
Inclination:       51
6404  deg
RA of node:       253
8609  deg
Eccentricity:     
0008213     
Arg of perigee:   159
8925  deg
Mean anomaly:     200
2564  deg
Mean motion:   15
74000737  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             758
Checksum:              305


Coasting Arc #5 (Orbit 773)
---------------------------------------

Vector Time (GMT): 2009/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3581637
74                 A    =         6730900
14  meter
 Y    =        5458123
11  meter          E    =           
0020594
 Z    =        1588382
50                 I    =           51
34805
 XDOT =      -3373
128374                 Wp   =          133
16923
 YDOT =       3892
306728  meter/sec      RA   =          247
94775  deg
 ZDOT =      -5736
276790                 TA   =           29
20985
                                          MA   =           29
09484
                                          Ha   =            192
075  n
mi
                                          Hp   =            182
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11750780
00                 X    =         3512621
86
 Y    =       17907228
05  feet           Y    =         5497789
00  meter
 Z    =        5211228
66                 Z    =         1605615
01
 XDOT =     -11066
694142                 XDOT =       -3388
536488
 YDOT =      12770
035197  feet/sec       YDOT =        3854
500979  meter/sec
 ZDOT =     -18819
805743                 ZDOT =       -5752
700304

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16595417
70                 X    =         5058283
31
 Y    =      -13514062
75  feet           Y    =        -4119086
33  meter
 Z    =        5279088
07                 Z    =         1609066
04
 XDOT =      12851
632630                 XDOT =        3917
177626
 YDOT =       8363
777280  feet/sec       YDOT =        2549
279315  meter/sec
 ZDOT =     -18883
993985                 ZDOT =       -5755
841367


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   09179
53492256  
00010596  00000-0  82463-4 0  9046
2 25544  51
6405 248
6439 0008085 162
3108 197
8339 15
74055148  7749


Satellite: ISS
Catalog Number: 25544
Epoch time:      09179
53492256   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:       248
6439  deg
Eccentricity:     
0008085     
Arg of perigee:   162
3108  deg
Mean anomaly:     197
8339  deg
Mean motion:   15
74055148  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             774
Checksum:              335


Coasting Arc #6 (Orbit 789)
---------------------------------------

Vector Time (GMT): 2009/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2647289
08                 A    =         6720956
94  meter
 Y    =       -3616190
25  meter          E    =           
0012680
 Z    =        5006149
43                 I    =           51
32712
 XDOT =       4633
661344                 Wp   =          150
20217
 YDOT =       5887
714377  meter/sec      RA   =          242
82007  deg
 ZDOT =       1789
873745                 TA   =          282
41263
                                          MA   =          282
55451
                                          Ha   =            191
919  n
mi
                                          Hp   =            182
400

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8685331
61                 X    =         2663210
26
 Y    =      -11864141
24  feet           Y    =        -3586498
32  meter
 Z    =       16424374
77                 Z    =         5019048
16
 XDOT =      15202
300999                 XDOT =        4558
784672
 YDOT =      19316
648217  feet/sec       YDOT =        5939
111808  meter/sec
 ZDOT =       5872
289189                 ZDOT =        1812
202887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12814549
81                 X    =        -3905874
78
 Y    =       -7093843
37  feet           Y    =        -2162203
46  meter
 Z    =       16474757
01                 Z    =         5021505
94
 XDOT =      16825
884356                 XDOT =        5128
529552
 YDOT =     -16455
699183  feet/sec       YDOT =       -5015
697111  meter/sec
 ZDOT =       5960
163281                 ZDOT =        1816
657768


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   09180
55071603  
00010596  00000-0  82463-4 0  9050
2 25544  51
6405 243
4267 0008055 166
9225 193
2149 15
74083439  7909


Satellite: ISS
Catalog Number: 25544
Epoch time:      09180
55071603   =   yrday
fracday
Element set:     905
Inclination:       51
6405  deg
RA of node:       243
4267  deg
Eccentricity:     
0008055     
Arg of perigee:   166
9225  deg
Mean anomaly:     193
2149  deg
Mean motion:   15
74083439  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             790
Checksum:              309


Coasting Arc #7 (Orbit 804)
---------------------------------------

Vector Time (GMT): 2009/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4476171
68                 A    =         6730944
90  meter
 Y    =       -4794562
20  meter          E    =           
0006485
 Z    =       -1519507
26                 I    =           51
37489
 XDOT =       2696
475967                 Wp   =          100
83700
 YDOT =      -4335
084178  meter/sec      RA   =          237
63374  deg
 ZDOT =       5754
964526                 TA   =          242
37246
                                          MA   =          242
43832
                                          Ha   =            191
857  n
mi
                                          Hp   =            182
581

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14685602
62                 X    =        -4414843
89
 Y    =      -15730190
95  feet           Y    =        -4844274
26  meter
 Z    =       -4985260
03                 Z    =        -1541104
22
 XDOT =       8846
705927                 XDOT =        2716
794594
 YDOT =     -14222
717118  feet/sec       YDOT =       -4304
817778  meter/sec
 ZDOT =      18881
117212                 ZDOT =        5768
112793

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13559756
83                 X    =        -4133013
88
 Y    =       16684861
68  feet           Y    =         5085545
84  meter
 Z    =       -5070210
49                 Z    =        -1545400
16
 XDOT =     -14074
289336                 XDOT =       -4289
843389
 YDOT =      -5704
147617  feet/sec       YDOT =       -1738
624194  meter/sec
 ZDOT =      18932
440343                 ZDOT =        5770
607817


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   09181
50301045  
00010596  00000-0  82463-4 0  9063
2 25544  51
6399 238
5356 0007848 169
7043 190
4282 15
74064770  8054


Satellite: ISS
Catalog Number: 25544
Epoch time:      09181
50301045   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       238
5356  deg
Eccentricity:     
0007848     
Arg of perigee:   169
7043  deg
Mean anomaly:     190
4282  deg
Mean motion:   15
74064770  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             805
Checksum:              317


Coasting Arc #8 (Orbit 820)
---------------------------------------

Vector Time (GMT): 2009/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2077699
58                 A    =         6720770
60  meter
 Y    =        3928413
01  meter          E    =           
0015001
 Z    =       -5052750
80                 I    =           51
35800
 XDOT =      -5552
006757                 Wp   =          109
17498
 YDOT =      -5058
414500  meter/sec      RA   =          232
50591  deg
 ZDOT =      -1658
679763                 TA   =          144
84763
                                          MA   =          144
74857
                                          Ha   =            191
710  n
mi
                                          Hp   =            182
627

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6816599
69                 X    =        -2096927
93
 Y    =       12888494
14  feet           Y    =         3905072
22  meter
 Z    =      -16577266
42                 Z    =        -5062890
41
 XDOT =     -18215
245265                 XDOT =       -5486
972478
 YDOT =     -16595
848097  feet/sec       YDOT =       -5120
136408  meter/sec
 ZDOT =      -5441
862740                 ZDOT =       -1685
494298

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13773429
85                 X    =         4198141
42
 Y    =        4643180
72  feet           Y    =         1415241
48  meter
 Z    =      -16616816
10                 Z    =        -5064805
55
 XDOT =     -13241
189249                 XDOT =       -4035
914483
 YDOT =      19529
705001  feet/sec       YDOT =        5952
654084  meter/sec
 ZDOT =      -5547
295801                 ZDOT =       -1690
815760


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   09182
51877647  
00010596  00000-0  82463-4 0  9072
2 25544  51
6402 233
3178 0007914 173
1298 186
9975 15
74094733  8218


Satellite: ISS
Catalog Number: 25544
Epoch time:      09182
51877647   =   yrday
fracday
Element set:     907
Inclination:       51
6402  deg
RA of node:       233
3178  deg
Eccentricity:     
0007914     
Arg of perigee:   173
1298  deg
Mean anomaly:     186
9975  deg
Mean motion:   15
74094733  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             821
Checksum:              340


Coasting Arc #9 (Orbit 836)
---------------------------------------

Vector Time (GMT): 2009/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5206130
86                 A    =         6730862
00  meter
 Y    =        4015232
68  meter          E    =           
0019356
 Z    =        1385846
88                 I    =           51
41195
 XDOT =      -2025
842272                 Wp   =          139
06339
 YDOT =       4643
051998  meter/sec      RA   =          227
32423  deg
 ZDOT =      -5810
766333                 TA   =           25
63676
                                          MA   =           25
54092
                                          Ha   =            191
448  n
mi
                                          Hp   =            182
756

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17080481
84                 X    =         5154112
71
 Y    =       13173335
55  feet           Y    =         4073159
59  meter
 Z    =        4546741
75                 Z    =         1411012
68
 XDOT =      -6646
464148                 XDOT =       -2049
383378
 YDOT =      15233
110231  feet/sec       YDOT =        4620
267213  meter/sec
 ZDOT =     -19064
194007                 ZDOT =       -5820
664292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10047028
94                 X    =         3062334
42
 Y    =      -19063775
36  feet           Y    =        -5810638
73  meter
 Z    =        4645661
23                 Z    =         1415997
54
 XDOT =      14739
083935                 XDOT =        4492
472783
 YDOT =       3088
210641  feet/sec       YDOT =         941
286603  meter/sec
 ZDOT =     -19102
760353                 ZDOT =       -5822
521355


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   09183
53452656  
00010596  00000-0  82463-4 0  9085
2 25544  51
6403 228
1007 0007725 176
3034 183
8187 15
74157788  8373


Satellite: ISS
Catalog Number: 25544
Epoch time:      09183
53452656   =   yrday
fracday
Element set:     908
Inclination:       51
6403  deg
RA of node:       228
1007  deg
Eccentricity:     
0007725     
Arg of perigee:   176
3034  deg
Mean anomaly:     183
8187  deg
Mean motion:   15
74157788  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             837
Checksum:              328


Coasting Arc #10 (Orbit 852)
---------------------------------------

Vector Time (GMT): 2009/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1458806
86                 A    =         6720432
02  meter
 Y    =       -4150824
01  meter          E    =           
0011329
 Z    =        5078994
97                 I    =           51
39707
 XDOT =       6337
128490                 Wp   =          159
42259
 YDOT =       4104
566725  meter/sec      RA   =          222
19751  deg
 ZDOT =       1522
813932                 TA   =          275
85834
                                          MA   =          275
98747
                                          Ha   =            191
395  n
mi
                                          Hp   =            182
883

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4786111
73                 X    =         1480440
80
 Y    =      -13618189
00  feet           Y    =        -4134390
77  meter
 Z    =       16663369
31                 Z    =         5086133
63
 XDOT =      20791
103969                 XDOT =        6283
361977
 YDOT =      13466
426263  feet/sec       YDOT =        4175
131291  meter/sec
 ZDOT =       4996
108701                 ZDOT =        1553
469901

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14258207
37                 X    =        -4345901
61
 Y    =       -2034470
45  feet           Y    =         -620106
59  meter
 Z    =       16691143
36                 Z    =         5087460
50
 XDOT =       9157
200114                 XDOT =        2791
114595
 YDOT =     -21890
669569  feet/sec       YDOT =       -6672
276085  meter/sec
 ZDOT =       5116
578837                 ZDOT =        1559
533229


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   09184
55026291  
00010596  00000-0  82463-4 0  9091
2 25544  51
6394 222
8835 0007756 179
5330 180
5842 15
74166515  8538


Satellite: ISS
Catalog Number: 25544
Epoch time:      09184
55026291   =   yrday
fracday
Element set:     909
Inclination:       51
6394  deg
RA of node:       222
8835  deg
Eccentricity:     
0007756     
Arg of perigee:   179
5330  deg
Mean anomaly:     180
5842  deg
Mean motion:   15
74166515  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             853
Checksum:              329


Coasting Arc #11 (Orbit 867)
---------------------------------------

Vector Time (GMT): 2009/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5822500
53                 A    =         6730894
78  meter
 Y    =       -3136896
47  meter          E    =           
0005064
 Z    =       -1256645
85                 I    =           51
45603
 XDOT =       1340
251991                 Wp   =           96
41974
 YDOT =      -4821
177890  meter/sec      RA   =          217
02038  deg
 ZDOT =       5844
554962                 TA   =          249
77262
                                          MA   =          249
82708
                                          Ha   =            191
247  n
mi
                                          Hp   =            183
009

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19102692
02                 X    =        -5780885
93
 Y    =      -10291655
08  feet           Y    =        -3201774
14  meter
 Z    =       -4122853
82                 Z    =        -1284831
03
 XDOT =       4397
152202                 XDOT =        1365
671897
 YDOT =     -15817
512764  feet/sec       YDOT =       -4806
049436  meter/sec
 ZDOT =      19175
049088                 ZDOT =        5851
126682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6148920
29                 X    =        -1874190
90
 Y    =       20786928
42  feet           Y    =         6335855
78  meter
 Z    =       -4233593
79                 Z    =        -1290399
39
 XDOT =     -14844
589329                 XDOT =       -4524
630827
 YDOT =       -493
376789  feet/sec       YDOT =        -150
381245  meter/sec
 ZDOT =      19200
564762                 ZDOT =        5852
332139


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   09185
50250261  
00010596  00000-0  82463-4 0  9105
2 25544  51
6398 217
9921 0007695 183
1365 176
9751 15
74192870  8681


Satellite: ISS
Catalog Number: 25544
Epoch time:      09185
50250261   =   yrday
fracday
Element set:     910
Inclination:       51
6398  deg
RA of node:       217
9921  deg
Eccentricity:     
0007695     
Arg of perigee:   183
1365  deg
Mean anomaly:     176
9751  deg
Mean motion:   15
74192870  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             868
Checksum:              336


Coasting Arc #12 (Orbit 883)
---------------------------------------

Vector Time (GMT): 2009/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -905082
97                 A    =         6720171
07  meter
 Y    =        4254778
70  meter          E    =           
0013853
 Z    =       -5132395
56                 I    =           51
44432
 XDOT =      -6929
438234                 Wp   =          111
80954
 YDOT =      -3065
845548  meter/sec      RA   =          211
89324  deg
 ZDOT =      -1327
537421                 TA   =          145
48674
                                          MA   =          145
39672
                                          Ha   =            191
096  n
mi
                                          Hp   =            183
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2969432
33                 X    =         -927661
28
 Y    =       13959247
71  feet           Y    =         4244532
33  meter
 Z    =      -16838568
12                 Z    =        -5136846
42
 XDOT =     -22734
377407                 XDOT =       -6888
191522
 YDOT =     -10058
548385  feet/sec       YDOT =       -3143
103688  meter/sec
 ZDOT =      -4355
437732                 ZDOT =       -1361
100852

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14247965
43                 X    =         4342779
86
 Y    =        -305189
17  feet           Y    =          -93021
66  meter
 Z    =      -16855795
50                 Z    =        -5137646
47
 XDOT =      -4777
983841                 XDOT =       -1456
329475
 YDOT =      23338
130320  feet/sec       YDOT =        7113
462122  meter/sec
 ZDOT =      -4487
290723                 ZDOT =       -1367
726212


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   09186
51821026  
00010596  00000-0  82463-4 0  9111
2 25544  51
6399 212
7741 0007675 187
2493 172
8560 15
74190610  8841


Satellite: ISS
Catalog Number: 25544
Epoch time:      09186
51821026   =   yrday
fracday
Element set:     911
Inclination:       51
6399  deg
RA of node:       212
7741  deg
Eccentricity:     
0007675     
Arg of perigee:   187
2493  deg
Mean anomaly:     172
8560  deg
Mean motion:   15
74190610  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             884
Checksum:              322


Coasting Arc #13 (Orbit 899)
---------------------------------------

Vector Time (GMT): 2009/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6258877
95                 A    =         6731012
89  meter
 Y    =        2199969
80  meter          E    =           
0018178
 Z    =        1068090
41                 I    =           51
50582
 XDOT =       -709
319278                 Wp   =          145
96505
 YDOT =       4901
850022  meter/sec      RA   =          206
72245  deg
 ZDOT =      -5906
506633                 TA   =           22
31749
                                          MA   =           22
23849
                                          Ha   =            190
907  n
mi
                                          Hp   =            183
306

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20534376
47                 X    =         6228623
80
 Y    =        7217748
69  feet           Y    =         2269790
86  meter
 Z    =        3504233
63                 Z    =         1098422
68
 XDOT =      -2327
162987                 XDOT =        -735
387442
 YDOT =      16082
185110  feet/sec       YDOT =        4893
773410  meter/sec
 ZDOT =     -19378
302603                 ZDOT =       -5910
014823

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2102293
65                 X    =          640779
10
 Y    =      -21644575
59  feet           Y    =        -6597266
64  meter
 Z    =        3623378
99                 Z    =         1104405
92
 XDOT =      14566
410630                 XDOT =        4439
841960
 YDOT =      -1849
201337  feet/sec       YDOT =        -563
636568  meter/sec
 ZDOT =     -19391
794412                 ZDOT =       -5910
618937


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   09187
53390333  
00010596  00000-0  82463-4 0  9127
2 25544  51
6384 207
5561 0007577 190
1254 169
9757 15
74224828  9009


Satellite: ISS
Catalog Number: 25544
Epoch time:      09187
53390333   =   yrday
fracday
Element set:     912
Inclination:       51
6384  deg
RA of node:       207
5561  deg
Eccentricity:     
0007577     
Arg of perigee:   190
1254  deg
Mean anomaly:     169
9757  deg
Mean motion:   15
74224828  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             900
Checksum:              326


Coasting Arc #14 (Orbit 915)
---------------------------------------

Vector Time (GMT): 2009/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         342418
00                 A    =         6719846
89  meter
 Y    =       -4284546
28  meter          E    =           
0009626
 Z    =        5165802
62                 I    =           51
49481
 XDOT =       7364
256839                 Wp   =          171
74075
 YDOT =       1954
126283  meter/sec      RA   =          201
59519  deg
 ZDOT =       1122
984392                 TA   =          267
46529
                                          MA   =          267
57550
                                          Ha   =            190
780  n
mi
                                          Hp   =            183
483

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1123418
63                 X    =          365208
89
 Y    =      -14056910
37  feet           Y    =        -4280590
70  meter
 Z    =       16948171
33                 Z    =         5167520
62
 XDOT =      24160
947636                 XDOT =        7336
402961
 YDOT =       6411
175470  feet/sec       YDOT =        2036
321760  meter/sec
 ZDOT =       3684
331996                 ZDOT =        1158
692177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13851029
28                 X    =        -4221793
72
 Y    =        2605273
08  feet           Y    =          794087
24  meter
 Z    =       16954670
46                 Z    =         5167783
56
 XDOT =        212
425012                 XDOT =          64
747144
 YDOT =     -23965
974889  feet/sec       YDOT =       -7304
829146  meter/sec
 ZDOT =       3824
577069                 ZDOT =        1165
731091


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   09188
54958145  
00010596  00000-0  82463-4 0  9131
2 25544  51
6378 202
3377 0007505 194
2224 165
8729 15
74246668  9160


Satellite: ISS
Catalog Number: 25544
Epoch time:      09188
54958145   =   yrday
fracday
Element set:     913
Inclination:       51
6378  deg
RA of node:       202
3377  deg
Eccentricity:     
0007505     
Arg of perigee:   194
2224  deg
Mean anomaly:     165
8729  deg
Mean motion:   15
74246668  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             916
Checksum:              341


Coasting Arc #15 (Orbit 930)
---------------------------------------

Vector Time (GMT): 2009/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6562982
18                 A    =         6730898
66  meter
 Y    =       -1209985
33  meter          E    =           
0004028
 Z    =        -876865
31                 I    =           51
56167
 XDOT =        109
846977                 Wp   =           81
54130
 YDOT =      -4886
176536  meter/sec      RA   =          196
43198  deg
 ZDOT =       5944
058460                 TA   =          268
88486
                                          MA   =          268
93101
                                          Ha   =            190
570  n
mi
                                          Hp   =            183
537

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21532093
78                 X    =        -6544704
56
 Y    =       -3969768
14  feet           Y    =        -1283274
09  meter
 Z    =       -2876854
69                 Z    =         -908703
58
 XDOT =        360
390346                 XDOT =         135
602180
 YDOT =     -16030
762914  feet/sec       YDOT =       -4884
805188  meter/sec
 ZDOT =      19501
504134                 ZDOT =        5944
653800

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2041405
83                 X    =          622220
50
 Y    =       21782739
53  feet           Y    =         6639379
01  meter
 Z    =       -3001888
60                 Z    =         -914975
65
 XDOT =     -13902
996586                 XDOT =       -4237
633360
 YDOT =       3980
428106  feet/sec       YDOT =        1213
234487  meter/sec
 ZDOT =      19503
558818                 ZDOT =        5944
684728


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   09189
50176615  
00010596  00000-0  82463-4 0  9143
2 25544  51
6384 197
4464 0007614 197
7258 162
3641 15
74318175  9319


Satellite: ISS
Catalog Number: 25544
Epoch time:      09189
50176615   =   yrday
fracday
Element set:     914
Inclination:       51
6384  deg
RA of node:       197
4464  deg
Eccentricity:     
0007614     
Arg of perigee:   197
7258  deg
Mean anomaly:     162
3641  deg
Mean motion:   15
74318175  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             931
Checksum:              332

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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