Date: July 18th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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 2806)
---------------------------------------

Vector Time (GMT): 2010/197/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2790626
11                 A    =         6731867
13  meter
 Y    =       -4248105
09  meter          E    =           
0016093
 Z    =       -4427904
91                 I    =           51
97133
 XDOT =       3652
461781                 Wp   =           89
53365
 YDOT =       5875
425885  meter/sec      RA   =           80
35335  deg
 ZDOT =      -3345
210658                 TA   =          146
96808
                                          MA   =          146
86745
                                          Ha   =            197
342  n
mi
                                          Hp   =            185
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9155597
47                 X    =         2859431
48
 Y    =      -13937352
67  feet           Y    =        -4216513
57  meter
 Z    =      -14527247
08                 Z    =        -4414181
44
 XDOT =      11983
142325                 XDOT =        3602
740468
 YDOT =      19276
331643  feet/sec       YDOT =        5915
992162  meter/sec
 ZDOT =     -10975
100583                 ZDOT =       -3327
587503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11310611
90                 X    =        -3447474
51
 Y    =      -12318119
00  feet           Y    =        -3754562
67  meter
 Z    =      -14472376
27                 Z    =        -4411180
29
 XDOT =      20706
931695                 XDOT =        6311
472781
 YDOT =      -6241
355603  feet/sec       YDOT =       -1902
365188  meter/sec
 ZDOT =     -10904
643248                 ZDOT =       -3323
735262


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   10197
41843322  
00016717  00000-0  10270-3 0  9002
2 25544  51
6447  80
9500 0008050 113
3232 246
8777 15
71157114 28070


Satellite: ISS
Catalog Number: 25544
Epoch time:      10197
41843322   =   yrday
fracday
Element set:     900
Inclination:       51
6447  deg
RA of node:        80
9500  deg
Eccentricity:     
0008050     
Arg of perigee:   113
3232  deg
Mean anomaly:     246
8777  deg
Mean motion:   15
71157114  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2807
Checksum:              286


Coasting Arc #2 (Orbit 2822)
---------------------------------------

Vector Time (GMT): 2010/198/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4004318
98                 A    =         6734572
40  meter
 Y    =       -3980930
65  meter          E    =           
0019242
 Z    =        3651739
89                 I    =           51
97383
 XDOT =       1963
275785                 Wp   =           98
05386
 YDOT =      -6018
777423  meter/sec      RA   =           75
21389  deg
 ZDOT =      -4391
597074                 TA   =           38
36379
                                          MA   =           38
22709
                                          Ha   =            197
379  n
mi
                                          Hp   =            185
480

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13137529
46                 X    =        -3977245
23
 Y    =      -13060796
09  feet           Y    =        -4025558
28  meter
 Z    =       11980773
93                 Z    =         3632352
48
 XDOT =       6441
193521                 XDOT =        2051
766350
 YDOT =     -19746
645087  feet/sec       YDOT =       -5996
327738  meter/sec
 ZDOT =     -14408
126884                 ZDOT =       -4381
845140

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15681218
47                 X    =        -4779635
39
 Y    =        9956387
14  feet           Y    =         3034706
80  meter
 Z    =       11903266
82                 Z    =         3628115
73
 XDOT =     -17063
834852                 XDOT =       -5201
056863
 YDOT =      -9629
714218  feet/sec       YDOT =       -2935
136894  meter/sec
 ZDOT =     -14369
125535                 ZDOT =       -4379
709463


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   10198
43610761  
00016717  00000-0  10270-3 0  9015
2 25544  51
6445  75
7463 0008016 117
4063 242
7915 15
71154390 28237


Satellite: ISS
Catalog Number: 25544
Epoch time:      10198
43610761   =   yrday
fracday
Element set:     901
Inclination:       51
6445  deg
RA of node:        75
7463  deg
Eccentricity:     
0008016     
Arg of perigee:   117
4063  deg
Mean anomaly:     242
7915  deg
Mean motion:   15
71154390  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2823
Checksum:              296


Coasting Arc #3 (Orbit 2838)
---------------------------------------

Vector Time (GMT): 2010/199/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -455131
49                 A    =         6736005
20  meter
 Y    =        5942907
73  meter          E    =           
0020059
 Z    =        3124704
69                 I    =           51
97068
 XDOT =      -5143
138365                 Wp   =           98
47962
 YDOT =      -2982
012103  meter/sec      RA   =           70
17313  deg
 ZDOT =       4892
950951                 TA   =          297
63903
                                          MA   =          297
84251
                                          Ha   =            197
208  n
mi
                                          Hp   =            185
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1493213
54                 X    =         -536731
51
 Y    =       19497728
76  feet           Y    =         5937361
61  meter
 Z    =       10251655
80                 Z    =         3122296
07
 XDOT =     -16873
813535                 XDOT =       -5133
179666
 YDOT =      -9783
504274  feet/sec       YDOT =       -3039
470565  meter/sec
 ZDOT =      16052
988686                 ZDOT =        4867
989589

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18756276
93                 X    =         5716913
21
 Y    =        5548961
76  feet           Y    =         1691323
54  meter
 Z    =       10242004
66                 Z    =         3121763
02
 XDOT =     -12673
242567                 XDOT =       -3862
804334
 YDOT =      13213
269939  feet/sec       YDOT =        4027
404677  meter/sec
 ZDOT =      15953
197802                 ZDOT =        4862
534690


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   10199
45376820  
00016717  00000-0  10270-3 0  9024
2 25544  51
6450  70
5422 0007936 120
8506 239
3438 15
71176308 28393


Satellite: ISS
Catalog Number: 25544
Epoch time:      10199
45376820   =   yrday
fracday
Element set:     902
Inclination:       51
6450  deg
RA of node:        70
5422  deg
Eccentricity:     
0007936     
Arg of perigee:   120
8506  deg
Mean anomaly:     239
3438  deg
Mean motion:   15
71176308  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2839
Checksum:              311


Coasting Arc #4 (Orbit 2853)
---------------------------------------

Vector Time (GMT): 2010/200/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4640154
89                 A    =         6730484
76  meter
 Y    =        1141019
71  meter          E    =           
0018887
 Z    =       -4757908
86                 I    =           51
94175
 XDOT =        999
580732                 Wp   =          115
06656
 YDOT =       7127
018108  meter/sec      RA   =           65
03615  deg
 ZDOT =       2684
471232                 TA   =          181
28145
                                          MA   =          181
28630
                                          Ha   =            197
066  n
mi
                                          Hp   =            185
711

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15223605
29                 X    =         4650163
91
 Y    =        3743502
97  feet           Y    =         1192965
23  meter
 Z    =      -15609937
19                 Z    =        -4735342
62
 XDOT =       3279
464345                 XDOT =         906
770202
 YDOT =      23382
605341  feet/sec       YDOT =        7137
676760  meter/sec
 ZDOT =       8807
320316                 ZDOT =        2689
102605

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6581251
83                 X    =         2005965
56
 Y    =      -14327164
51  feet           Y    =        -4366919
74  meter
 Z    =      -15519716
27                 Z    =        -4730409
52
 XDOT =      22525
702437                 XDOT =        6865
834103
 YDOT =        788
502076  feet/sec       YDOT =         240
335433  meter/sec
 ZDOT =       8825
800213                 ZDOT =        2690
103905


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   10200
40781242  
00016717  00000-0  10270-3 0  9031
2 25544  51
6459  65
6634 0007816 124
5077 235
6823 15
71204376 28544


Satellite: ISS
Catalog Number: 25544
Epoch time:      10200
40781242   =   yrday
fracday
Element set:     903
Inclination:       51
6459  deg
RA of node:        65
6634  deg
Eccentricity:     
0007816     
Arg of perigee:   124
5077  deg
Mean anomaly:     235
6823  deg
Mean motion:   15
71204376  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2854
Checksum:              299


Coasting Arc #5 (Orbit 2869)
---------------------------------------

Vector Time (GMT): 2010/201/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2195638
24                 A    =         6739146
04  meter
 Y    =       -6181068
61  meter          E    =           
0015919
 Z    =       -1522733
68                 I    =           51
95757
 XDOT =       5036
007648                 Wp   =          135
99690
 YDOT =       -369
507836  meter/sec      RA   =           59
97823  deg
 ZDOT =      -5808
755066                 TA   =           60
68929
                                          MA   =           60
53031
                                          Ha   =            197
014  n
mi
                                          Hp   =            185
715

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7203537
52                 X    =        -2118960
09
 Y    =      -20279096
50  feet           Y    =        -6205192
61  meter
 Z    =       -4995845
40                 Z    =        -1533214
65
 XDOT =      16522
334804                 XDOT =        5067
983002
 YDOT =      -1212
296051  feet/sec       YDOT =        -313
012599  meter/sec
 ZDOT =     -19057
595362                 ZDOT =       -5784
212643

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21213988
66                 X    =        -6466023
74
 Y    =        3560806
74  feet           Y    =         1085333
90  meter
 Z    =       -5037709
73                 Z    =        -1535493
93
 XDOT =       1940
157524                 XDOT =         591
360013
 YDOT =     -15047
144034  feet/sec       YDOT =       -4586
369502  meter/sec
 ZDOT =     -18959
461107                 ZDOT =       -5778
843745


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   10201
42544775  
00016717  00000-0  10270-3 0  9043
2 25544  51
6463  60
4593 0007802 129
5317 230
6536 15
71194939 28700


Satellite: ISS
Catalog Number: 25544
Epoch time:      10201
42544775   =   yrday
fracday
Element set:     904
Inclination:       51
6463  deg
RA of node:        60
4593  deg
Eccentricity:     
0007802     
Arg of perigee:   129
5317  deg
Mean anomaly:     230
6536  deg
Mean motion:   15
71194939  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2870
Checksum:              307


Coasting Arc #6 (Orbit 2885)
---------------------------------------

Vector Time (GMT): 2010/202/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3819626
09                 A    =         6728015
55  meter
 Y    =        1729623
06  meter          E    =           
0009110
 Z    =        5254162
28                 I    =           51
90478
 XDOT =      -3949
021481                 Wp   =          113
72839
 YDOT =      -6576
585148  meter/sec      RA   =           54
86435  deg
 ZDOT =       -708
501086                 TA   =          342
96731
                                          MA   =          342
99786
                                          Ha   =            196
902  n
mi
                                          Hp   =            185
715

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12531581
67                 X    =        -3864206
73
 Y    =        5674616
32  feet           Y    =         1686659
65  meter
 Z    =       17238065
21                 Z    =         5235498
66
 XDOT =     -12956
107222                 XDOT =       -3871
745665
 YDOT =     -21576
722928  feet/sec       YDOT =       -6620
313284  meter/sec
 ZDOT =      -2324
478627                 ZDOT =        -727
498581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3636626
07                 X    =         1108443
63
 Y    =       13363554
89  feet           Y    =         4073211
53  meter
 Z    =       17163421
96                 Z    =         5231411
01
 XDOT =     -22355
908482                 XDOT =       -6814
080905
 YDOT =       9155
520768  feet/sec       YDOT =        2790
602730  meter/sec
 ZDOT =      -2400
386556                 ZDOT =        -731
637822


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   10202
44306766  
00016717  00000-0  10270-3 0  9053
2 25544  51
6463  55
2555 0007612 132
7732 227
4071 15
71283659 28869


Satellite: ISS
Catalog Number: 25544
Epoch time:      10202
44306766   =   yrday
fracday
Element set:     905
Inclination:       51
6463  deg
RA of node:        55
2555  deg
Eccentricity:     
0007612     
Arg of perigee:   132
7732  deg
Mean anomaly:     227
4071  deg
Mean motion:   15
71283659  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2886
Checksum:              306


Coasting Arc #7 (Orbit 2900)
---------------------------------------

Vector Time (GMT): 2010/203/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4518523
88                 A    =         6739891
12  meter
 Y    =        4990307
52  meter          E    =           
0013609
 Z    =        -289729
86                 I    =           51
92658
 XDOT =      -3351
769660                 Wp   =           76
71316
 YDOT =       3372
052407  meter/sec      RA   =           49
77243  deg
 ZDOT =       6046
819108                 TA   =          280
15581
                                          MA   =          280
30928
                                          Ha   =            196
737  n
mi
                                          Hp   =            185
820

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14824553
42                 X    =         4463792
96
 Y    =       16372400
00  feet           Y    =         5040530
38  meter
 Z    =        -950557
30                 Z    =         -267911
29
 XDOT =     -10996
619620                 XDOT =       -3418
601446
 YDOT =      11063
164066  feet/sec       YDOT =        3334
196291  meter/sec
 ZDOT =      19838
645369                 ZDOT =        6030
374605

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18273017
34                 X    =         5569615
68
 Y    =      -12412810
99  feet           Y    =        -3783424
79  meter
 Z    =        -863357
18                 Z    =         -263151
27
 XDOT =       8508
234728                 XDOT =        2593
309945
 YDOT =      11209
973426  feet/sec       YDOT =        3416
799900  meter/sec
 ZDOT =      19772
854702                 ZDOT =        6026
766113


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   10203
39707692  
00016717  00000-0  10270-3 0  9062
2 25544  51
6466  50
3765 0007598 136
1055 224
0711 15
71279956 29017


Satellite: ISS
Catalog Number: 25544
Epoch time:      10203
39707692   =   yrday
fracday
Element set:     906
Inclination:       51
6466  deg
RA of node:        50
3765  deg
Eccentricity:     
0007598     
Arg of perigee:   136
1055  deg
Mean anomaly:     224
0711  deg
Mean motion:   15
71279956  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2901
Checksum:              313


Coasting Arc #8 (Orbit 2916)
---------------------------------------

Vector Time (GMT): 2010/204/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1819008
73                 A    =         6728332
88  meter
 Y    =       -3915779
23  meter          E    =           
0019080
 Z    =       -5175761
20                 I    =           51
86722
 XDOT =       6057
042808                 Wp   =           99
57933
 YDOT =       4540
821090  meter/sec      RA   =           44
68885  deg
 ZDOT =      -1313
868747                 TA   =          157
90547
                                          MA   =          157
82312
                                          Ha   =            196
594  n
mi
                                          Hp   =            185
955

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5967876
41                 X    =         1887802
99
 Y    =      -12847044
72  feet           Y    =        -3895052
55  meter
 Z    =      -16980843
84                 Z    =        -5166758
10
 XDOT =      19872
187691                 XDOT =        6012
198778
 YDOT =      14897
706989  feet/sec       YDOT =        4608
304024  meter/sec
 ZDOT =      -4310
593002                 ZDOT =       -1284
552341

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12012814
58                 X    =        -3661505
88
 Y    =       -7587963
82  feet           Y    =        -2312811
37  meter
 Z    =      -16944800
25                 Z    =        -5164775
12
 XDOT =      16656
879866                 XDOT =        5077
016983
 YDOT =     -17058
643125  feet/sec       YDOT =       -5199
474424  meter/sec
 ZDOT =      -4193
404482                 ZDOT =       -1278
149686


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   10204
41467213  
00016717  00000-0  10270-3 0  9079
2 25544  51
6463  45
1718 0007451 139
7774 220
3940 15
71305474 29174


Satellite: ISS
Catalog Number: 25544
Epoch time:      10204
41467213   =   yrday
fracday
Element set:     907
Inclination:       51
6463  deg
RA of node:        45
1718  deg
Eccentricity:     
0007451     
Arg of perigee:   139
7774  deg
Mean anomaly:     220
3940  deg
Mean motion:   15
71305474  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2917
Checksum:              297


Coasting Arc #9 (Orbit 2932)
---------------------------------------

Vector Time (GMT): 2010/205/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5799442
06                 A    =         6738257
29  meter
 Y    =       -2769694
34  meter          E    =           
0020926
 Z    =        1986051
67                 I    =           51
87796
 XDOT =        570
722944                 Wp   =          122
59953
 YDOT =      -5244
129601  meter/sec      RA   =           39
56214  deg
 ZDOT =      -5615
217197                 TA   =           35
35767
                                          MA   =           35
21908
                                          Ha   =            196
641  n
mi
                                          Hp   =            186
033

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19027040
87                 X    =        -5777687
49
 Y    =       -9086923
70  feet           Y    =        -2834425
81  meter
 Z    =        6515917
56                 Z    =         1957930
99
 XDOT =       1872
450605                 XDOT =         656
598500
 YDOT =     -17205
149610  feet/sec       YDOT =       -5237
266486  meter/sec
 ZDOT =     -18422
628598                 ZDOT =       -5612
236834

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11033117
27                 X    =        -3362894
14
 Y    =       18008978
15  feet           Y    =         5489136
54  meter
 Z    =        6403489
45                 Z    =         1951783
58
 XDOT =     -15590
455451                 XDOT =       -4751
970821
 YDOT =      -2967
660805  feet/sec       YDOT =        -904
543013  meter/sec
 ZDOT =     -18410
653635                 ZDOT =       -5611
567228


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   10205
43225570  
00016717  00000-0  10270-3 0  9081
2 25544  51
6462  39
9677 0007546 143
3385 216
8295 15
71289029 29330


Satellite: ISS
Catalog Number: 25544
Epoch time:      10205
43225570   =   yrday
fracday
Element set:     908
Inclination:       51
6462  deg
RA of node:        39
9677  deg
Eccentricity:     
0007546     
Arg of perigee:   143
3385  deg
Mean anomaly:     216
8295  deg
Mean motion:   15
71289029  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2933
Checksum:              325


Coasting Arc #10 (Orbit 2948)
---------------------------------------

Vector Time (GMT): 2010/206/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         919042
32                 A    =         6731072
11  meter
 Y    =        4919788
15  meter          E    =           
0015502
 Z    =        4495481
29                 I    =           51
82962
 XDOT =      -6814
705254                 Wp   =          127
85968
 YDOT =      -1649
336019  meter/sec      RA   =           34
50228  deg
 ZDOT =       3181
448514                 TA   =          290
34946
                                          MA   =          290
51594
                                          Ha   =            196
419  n
mi
                                          Hp   =            186
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3015230
71                 X    =          842122
30
 Y    =       16141037
22  feet           Y    =         4929634
78  meter
 Z    =       14748954
35                 Z    =         4499759
67
 XDOT =     -22357
956870                 XDOT =       -6811
210148
 YDOT =      -5411
207412  feet/sec       YDOT =       -1725
522977  meter/sec
 ZDOT =      10437
823210                 ZDOT =        3148
351701

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16335937
58                 X    =         4979193
77
 Y    =       -1502796
36  feet           Y    =         -458052
33  meter
 Z    =       14766011
64                 Z    =         4500680
35
 XDOT =      -7463
357763                 XDOT =       -2274
831446
 YDOT =      20668
011420  feet/sec       YDOT =        6299
609881  meter/sec
 ZDOT =      10305
480066                 ZDOT =        3141
110324


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   10206
44982437  
00016717  00000-0  10270-3 0  9096
2 25544  51
6458  34
7625 0007342 146
9501 213
2121 15
71303992 29496


Satellite: ISS
Catalog Number: 25544
Epoch time:      10206
44982437   =   yrday
fracday
Element set:     909
Inclination:       51
6458  deg
RA of node:        34
7625  deg
Eccentricity:     
0007342     
Arg of perigee:   146
9501  deg
Mean anomaly:     213
2121  deg
Mean motion:   15
71303992  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2949
Checksum:              306


Coasting Arc #11 (Orbit 2963)
---------------------------------------

Vector Time (GMT): 2010/207/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5771260
39                 A    =         6734581
44  meter
 Y    =         102598
02  meter          E    =           
0010669
 Z    =       -3483051
43                 I    =           51
81537
 XDOT =       2646
696258                 Wp   =          127
87693
 YDOT =       5596
894418  meter/sec      RA   =           29
35071  deg
 ZDOT =       4553
360677                 TA   =          191
02925
                                          MA   =          191
05265
                                          Ha   =            196
221  n
mi
                                          Hp   =            186
390

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18934581
32                 X    =         5786603
82
 Y    =         336607
67  feet           Y    =          167221
85  meter
 Z    =      -11427334
08                 Z    =        -3454978
02
 XDOT =       8683
386673                 XDOT =        2561
795174
 YDOT =      18362
514495  feet/sec       YDOT =        5626
016173  meter/sec
 ZDOT =      14938
847366                 ZDOT =        4566
012393

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1673921
05                 X    =          510211
14
 Y    =      -18931005
55  feet           Y    =        -5770170
49  meter
 Z    =      -11315063
23                 Z    =        -3448831
27
 XDOT =      17542
348879                 XDOT =        5346
907938
 YDOT =      -7402
004572  feet/sec       YDOT =       -2256
130993  meter/sec
 ZDOT =      14989
385262                 ZDOT =        4568
764628


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   10207
40378154  
00016717  00000-0  10270-3 0  9100
2 25544  51
6451  29
8823 0007215 152
1589 207
9960 15
71349785 29646


Satellite: ISS
Catalog Number: 25544
Epoch time:      10207
40378154   =   yrday
fracday
Element set:     910
Inclination:       51
6451  deg
RA of node:        29
8823  deg
Eccentricity:     
0007215     
Arg of perigee:   152
1589  deg
Mean anomaly:     207
9960  deg
Mean motion:   15
71349785  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2964
Checksum:              320


Coasting Arc #12 (Orbit 2979)
---------------------------------------

Vector Time (GMT): 2010/208/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3621902
22                 A    =         6734680
34  meter
 Y    =       -4558733
51  meter          E    =           
0010159
 Z    =       -3384695
32                 I    =           51
78844
 XDOT =       5985
876814                 Wp   =          129
41341
 YDOT =      -1314
487863  meter/sec      RA   =           24
29758  deg
 ZDOT =      -4650
490469                 TA   =           90
35050
                                          MA   =           90
23410
                                          Ha   =            196
083  n
mi
                                          Hp   =            186
382

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11882881
31                 X    =        -3554214
58
 Y    =      -14956474
78  feet           Y    =        -4598857
04  meter
 Z    =      -11104643
44                 Z    =        -3402126
10
 XDOT =      19638
703457                 XDOT =        6022
721497
 YDOT =      -4312
624222  feet/sec       YDOT =       -1247
343808  meter/sec
 ZDOT =     -15257
514663                 ZDOT =       -4621
322361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15565115
31                 X    =        -4744247
15
 Y    =       11003371
89  feet           Y    =         3353827
75  meter
 Z    =      -11174305
53                 Z    =        -3405928
33
 XDOT =      -2453
620722                 XDOT =        -747
863596
 YDOT =     -18795
408222  feet/sec       YDOT =       -5728
840426  meter/sec
 ZDOT =     -15140
852356                 ZDOT =       -4614
931798


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   10208
42132415  
00016717  00000-0  10270-3 0  9112
2 25544  51
6444  24
6775 0007184 156
4200 203
7292 15
71355825 29801


Satellite: ISS
Catalog Number: 25544
Epoch time:      10208
42132415   =   yrday
fracday
Element set:     911
Inclination:       51
6444  deg
RA of node:        24
6775  deg
Eccentricity:     
0007184     
Arg of perigee:   156
4200  deg
Mean anomaly:     203
7292  deg
Mean motion:   15
71355825  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2980
Checksum:              287


Coasting Arc #13 (Orbit 2995)
---------------------------------------

Vector Time (GMT): 2010/209/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4390383
84                 A    =         6730635
42  meter
 Y    =        2277162
03  meter          E    =           
0010817
 Z    =        4554706
33                 I    =           51
74756
 XDOT =      -5488
205856                 Wp   =          106
66782
 YDOT =      -4457
657482  meter/sec      RA   =           19
14280  deg
 ZDOT =      -3058
649339                 TA   =           13
71765
                                          MA   =           13
68828
                                          Ha   =            196
021  n
mi
                                          Hp   =            186
509

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14404146
45                 X    =        -4437646
65
 Y    =        7471004
04  feet           Y    =         2227801
57  meter
 Z    =       14943262
22                 Z    =         4533263
64
 XDOT =     -18005
924726                 XDOT =       -5423
093568
 YDOT =     -14624
860504  feet/sec       YDOT =       -4518
665615  meter/sec
 ZDOT =     -10034
938777                 ZDOT =       -3085
152629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6943623
92                 X    =         2116416
57
 Y    =       14752543
83  feet           Y    =         4496575
36  meter
 Z    =       14857488
33                 Z    =         4528562
44
 XDOT =     -14187
523535                 XDOT =       -4324
357174
 YDOT =      16900
390055  feet/sec       YDOT =        5151
238889  meter/sec
 ZDOT =     -10140
883214                 ZDOT =       -3090
941204


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   10209
43885212  
00016717  00000-0  10270-3 0  9125
2 25544  51
6449  19
4721 0007079 160
5899 199
5533 15
71412492 29963


Satellite: ISS
Catalog Number: 25544
Epoch time:      10209
43885212   =   yrday
fracday
Element set:     912
Inclination:       51
6449  deg
RA of node:        19
4721  deg
Eccentricity:     
0007079     
Arg of perigee:   160
5899  deg
Mean anomaly:     199
5533  deg
Mean motion:   15
71412492  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2996
Checksum:              332


Coasting Arc #14 (Orbit 3011)
---------------------------------------

Vector Time (GMT): 2010/210/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5732545
43                 A    =         6737875
65  meter
 Y    =        2981663
23  meter          E    =           
0015018
 Z    =        1899889
69                 I    =           51
74231
 XDOT =      -3771
927981                 Wp   =           95
39138
 YDOT =       3635
853735  meter/sec      RA   =           14
07386  deg
 ZDOT =       5635
562952                 TA   =          285
66208
                                          MA   =          285
82774
                                          Ha   =            195
809  n
mi
                                          Hp   =            186
564

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18807563
75                 X    =         5689548
72
 Y    =        9782359
69  feet           Y    =         3045527
48  meter
 Z    =        6233233
90                 Z    =         1927633
62
 XDOT =     -12375
091801                 XDOT =       -3839
680482
 YDOT =      11928
653985  feet/sec       YDOT =        3593
294666  meter/sec
 ZDOT =      18489
379765                 ZDOT =        5617
074870

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10135428
24                 X    =         3089278
53
 Y    =      -18582170
54  feet           Y    =        -5663845
58  meter
 Z    =        6344151
07                 Z    =         1933697
25
 XDOT =      10336
228967                 XDOT =        3150
482589
 YDOT =      11968
385216  feet/sec       YDOT =        3647
963814  meter/sec
 ZDOT =      18415
411527                 ZDOT =        5613
017434


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   10210
45636725  
00016717  00000-0  10270-3 0  9133
2 25544  51
6439  14
2663 0007177 164
7454 195
3926 15
71433031 30124


Satellite: ISS
Catalog Number: 25544
Epoch time:      10210
45636725   =   yrday
fracday
Element set:     913
Inclination:       51
6439  deg
RA of node:        14
2663  deg
Eccentricity:     
0007177     
Arg of perigee:   164
7454  deg
Mean anomaly:     195
3926  deg
Mean motion:   15
71433031  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3012
Checksum:              291


Coasting Arc #15 (Orbit 3026)
---------------------------------------

Vector Time (GMT): 2010/211/09:31:03
569
Vector Time (MET): N/A
Weight (LBS)     : 828730
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2037668
50                 A    =         6727999
17  meter
 Y    =       -3814986
77  meter          E    =           
0018139
 Z    =       -5168692
67                 I    =           51
67848
 XDOT =       7265
536102                 Wp   =          120
89460
 YDOT =       2155
959606  meter/sec      RA   =            8
93378  deg
 ZDOT =       1267
164843                 TA   =          161
27299
                                          MA   =          161
20616
                                          Ha   =            195
753  n
mi
                                          Hp   =            186
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6685264
11                 X    =         2105285
16
 Y    =      -12516360
80  feet           Y    =        -3791822
06  meter
 Z    =      -16957653
10                 Z    =        -5158629
74
 XDOT =      23837
060701                 XDOT =        7234
732205
 YDOT =       7073
358289  feet/sec       YDOT =        2237
034888  meter/sec
 ZDOT =       4157
364970                 ZDOT =        1302
385595

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12505411
03                 X    =        -3811649
28
 Y    =       -6806694
78  feet           Y    =        -2074680
57  meter
 Z    =      -16917376
98                 Z    =        -5156416
50
 XDOT =       6617
400471                 XDOT =        2016
983664
 YDOT =     -22888
126501  feet/sec       YDOT =       -6976
300958  meter/sec
 ZDOT =       4298
183432                 ZDOT =        1310
086310


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   10211
41027645  
00016717  00000-0  10270-3 0  9146
2 25544  51
6431   9
3854 0007145 167
2492 192
8851 15
71434949 30272


Satellite: ISS
Catalog Number: 25544
Epoch time:      10211
41027645   =   yrday
fracday
Element set:     914
Inclination:       51
6431  deg
RA of node:         9
3854  deg
Eccentricity:     
0007145     
Arg of perigee:   167
2492  deg
Mean anomaly:     192
8851  deg
Mean motion:   15
71434949  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3027
Checksum:              302

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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