Date: May 14th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13831 62 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 1791)
---------------------------------------

Vector Time (GMT): 2010/132/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5307490
26                 A    =         6727247
12  meter
 Y    =       -2216603
08  meter          E    =           
0007366
 Z    =        3491151
51                 I    =           51
91058
 XDOT =       -414
983443                 Wp   =           35
65484
 YDOT =      -6192
064441  meter/sec      RA   =           51
07506  deg
 ZDOT =      -4551
711427                 TA   =          103
10164
                                          MA   =          103
01942
                                          Ha   =            190
244  n
mi
                                          Hp   =            186
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17413025
78                 X    =        -5299269
10
 Y    =       -7272319
82  feet           Y    =        -2275908
88  meter
 Z    =       11453909
15                 Z    =         3465386
94
 XDOT =      -1361
494234                 XDOT =        -323
599925
 YDOT =     -20315
172051  feet/sec       YDOT =       -6196
193760  meter/sec
 ZDOT =     -14933
436439                 ZDOT =       -4553
505923

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18597323
63                 X    =         5668464
24
 Y    =        3546816
93  feet           Y    =         1081069
80  meter
 Z    =       11351289
82                 Z    =         3459873
14
 XDOT =       5656
329289                 XDOT =        1724
049167
 YDOT =      18270
637957  feet/sec       YDOT =        5568
890449  meter/sec
 ZDOT =     -14940
615447                 ZDOT =       -4553
899588


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   10132
93350123  
00016717  00000-0  10270-3 0  9000
2 25544  51
6441  51
5074 0009858 305
2561  54
7679 15
73905187 17920


Satellite: ISS
Catalog Number: 25544
Epoch time:      10132
93350123   =   yrday
fracday
Element set:     900
Inclination:       51
6441  deg
RA of node:        51
5074  deg
Eccentricity:     
0009858     
Arg of perigee:   305
2561  deg
Mean anomaly:      54
7679  deg
Mean motion:   15
73905187  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1792
Checksum:              304


Coasting Arc #2 (Orbit 1807)
---------------------------------------

Vector Time (GMT): 2010/133/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         839186
72                 A    =         6725351
22  meter
 Y    =        5356916
89  meter          E    =           
0005012
 Z    =        3973077
11                 I    =           51
88658
 XDOT =      -6276
184183                 Wp   =           35
98526
 YDOT =      -1982
825599  meter/sec      RA   =           46
00999  deg
 ZDOT =       4000
533676                 TA   =           12
71063
                                          MA   =           12
69800
                                          Ha   =            190
333  n
mi
                                          Hp   =            185
745

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2753237
26                 X    =          759921
42
 Y    =       17575186
64  feet           Y    =         5365857
59  meter
 Z    =       13035029
90                 Z    =         3976961
95
 XDOT =     -20591
155455                 XDOT =       -6272
979705
 YDOT =      -6505
333329  feet/sec       YDOT =       -2052
992094  meter/sec
 ZDOT =      13125
110485                 ZDOT =        3970
050884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6496741
73                 X    =        -1980206
88
 Y    =      -16548589
56  feet           Y    =        -5044010
10  meter
 Z    =       13050518
60                 Z    =         3977798
07
 XDOT =      20388
220279                 XDOT =        6214
329541
 YDOT =       2247
119576  feet/sec       YDOT =         684
922047  meter/sec
 ZDOT =      13003
704286                 ZDOT =        3963
529066


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   10133
94937388  
00016717  00000-0  10270-3 0  9017
2 25544  51
6455  46
2916 0009948 308
8807  51
1468 15
73978309 18084


Satellite: ISS
Catalog Number: 25544
Epoch time:      10133
94937388   =   yrday
fracday
Element set:     901
Inclination:       51
6455  deg
RA of node:        46
2916  deg
Eccentricity:     
0009948     
Arg of perigee:   308
8807  deg
Mean anomaly:      51
1468  deg
Mean motion:   15
73978309  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1808
Checksum:              345


Coasting Arc #3 (Orbit 1822)
---------------------------------------

Vector Time (GMT): 2010/134/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5611884
37                 A    =         6727084
86  meter
 Y    =        1227997
19  meter          E    =           
0006952
 Z    =       -3492000
42                 I    =           51
87043
 XDOT =       1510
547538                 Wp   =          340
53703
 YDOT =       6027
848267  meter/sec      RA   =           40
84149  deg
 ZDOT =       4551
143514                 TA   =          338
13750
                                          MA   =          338
16715
                                          Ha   =            190
705  n
mi
                                          Hp   =            185
531

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18411694
14                 X    =         5614699
43
 Y    =        4028862
18  feet           Y    =         1290768
78  meter
 Z    =      -11456694
30                 Z    =        -3464730
37
 XDOT =       4955
864627                 XDOT =        1420
921722
 YDOT =      19776
405076  feet/sec       YDOT =        6044
238440  meter/sec
 ZDOT =      14931
573209                 ZDOT =        4558
264914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18906766
72                 X    =        -5762782
50
 Y    =         482909
78  feet           Y    =          147190
90  meter
 Z    =      -11348084
70                 Z    =        -3458896
22
 XDOT =      -9397
366274                 XDOT =       -2864
317240
 YDOT =     -16672
479277  feet/sec       YDOT =       -5081
771684  meter/sec
 ZDOT =      14959
943337                 ZDOT =        4559
790729


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   10134
90174065  
00016717  00000-0  10270-3 0  9020
2 25544  51
6458  41
4026 0010051 313
1520  46
8803 15
73958136 18231


Satellite: ISS
Catalog Number: 25544
Epoch time:      10134
90174065   =   yrday
fracday
Element set:     902
Inclination:       51
6458  deg
RA of node:        41
4026  deg
Eccentricity:     
0010051     
Arg of perigee:   313
1520  deg
Mean anomaly:      46
8803  deg
Mean motion:   15
73958136  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1823
Checksum:              275


Coasting Arc #4 (Orbit 1838)
---------------------------------------

Vector Time (GMT): 2010/135/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1764392
94                 A    =         6725270
43  meter
 Y    =       -5128854
00  meter          E    =           
0009458
 Z    =       -3983215
79                 I    =           51
84148
 XDOT =       6529
879922                 Wp   =          358
83773
 YDOT =        851
232843  meter/sec      RA   =           35
77307  deg
 ZDOT =      -3979
093896                 TA   =          229
99427
                                          MA   =          230
07732
                                          Ha   =            190
674  n
mi
                                          Hp   =            185
249

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5788690
75                 X    =        -1687560
00
 Y    =      -16826948
83  feet           Y    =        -5148154
36  meter
 Z    =      -13068293
27                 Z    =        -3991601
40
 XDOT =      21423
490559                 XDOT =        6539
205973
 YDOT =       2792
758672  feet/sec       YDOT =         924
306529  meter/sec
 ZDOT =     -13054
770000                 ZDOT =       -3947
348486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9806872
96                 X    =         2989134
88
 Y    =       14819122
04  feet           Y    =         4516868
40  meter
 Z    =      -13101690
78                 Z    =        -3993395
35
 XDOT =     -20422
015927                 XDOT =       -6224
630455
 YDOT =       2057
415171  feet/sec       YDOT =         627
100144  meter/sec
 ZDOT =     -12928
333162                 ZDOT =       -3940
555948


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   10135
91758036  
00016717  00000-0  10270-3 0  9039
2 25544  51
6461  36
1866 0009991 316
5726  43
4649 15
73993609 18396


Satellite: ISS
Catalog Number: 25544
Epoch time:      10135
91758036   =   yrday
fracday
Element set:     903
Inclination:       51
6461  deg
RA of node:        36
1866  deg
Eccentricity:     
0009991     
Arg of perigee:   316
5726  deg
Mean anomaly:      43
4649  deg
Mean motion:   15
73993609  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1839
Checksum:              339


Coasting Arc #5 (Orbit 1854)
---------------------------------------

Vector Time (GMT): 2010/136/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5769248
14                 A    =         6727066
59  meter
 Y    =        -258068
48  meter          E    =           
0009990
 Z    =        3452527
86                 I    =           51
82228
 XDOT =      -2496
084937                 Wp   =           38
13359
 YDOT =      -5659
484050  meter/sec      RA   =           30
60048  deg
 ZDOT =      -4579
340038                 TA   =          101
11658
                                          MA   =          101
00423
                                          Ha   =            190
856  n
mi
                                          Hp   =            185
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18927979
45                 X    =        -5782705
50
 Y    =        -846681
38  feet           Y    =         -322659
38  meter
 Z    =       11327191
14                 Z    =         3424467
85
 XDOT =      -8189
255044                 XDOT =       -2410
368229
 YDOT =     -18567
861058  feet/sec       YDOT =       -5686
916844  meter/sec
 ZDOT =     -15024
081488                 ZDOT =       -4591
258729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18512326
31                 X    =         5642557
06
 Y    =       -4335722
04  feet           Y    =        -1321528
08  meter
 Z    =       11215427
93                 Z    =         3418462
43
 XDOT =      12515
717687                 XDOT =        3814
790751
 YDOT =      14326
272242  feet/sec       YDOT =        4366
647779  meter/sec
 ZDOT =     -15071
546605                 ZDOT =       -4593
807405


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   10136
93340273  
00016717  00000-0  10270-3 0  9043
2 25544  51
6461  30
9707 0009913 320
9595  39
0852 15
74012319 18555


Satellite: ISS
Catalog Number: 25544
Epoch time:      10136
93340273   =   yrday
fracday
Element set:     904
Inclination:       51
6461  deg
RA of node:        30
9707  deg
Eccentricity:     
0009913     
Arg of perigee:   320
9595  deg
Mean anomaly:      39
0852  deg
Mean motion:   15
74012319  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1855
Checksum:              302


Coasting Arc #6 (Orbit 1870)
---------------------------------------

Vector Time (GMT): 2010/137/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2569272
45                 A    =         6724837
89  meter
 Y    =        4733162
35  meter          E    =           
0007448
 Z    =        4019124
34                 I    =           51
78965
 XDOT =      -6623
510024                 Wp   =           38
55064
 YDOT =        262
538856  meter/sec      RA   =           25
52719  deg
 ZDOT =       3926
807184                 TA   =           11
01740
                                          MA   =           11
00110
                                          Ha   =            190
885  n
mi
                                          Hp   =            184
621

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8429371
55                 X    =         2496630
15
 Y    =       15528747
86  feet           Y    =         4761486
78  meter
 Z    =       13186103
47                 Z    =         4031430
11
 XDOT =     -21730
675933                 XDOT =       -6645
029314
 YDOT =        861
347954  feet/sec       YDOT =         188
349976  meter/sec
 ZDOT =      12883
225670                 ZDOT =        3894
577777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12465699
91                 X    =        -3799545
33
 Y    =      -12470276
93  feet           Y    =        -3800940
41  meter
 Z    =       13235110
82                 Z    =         4034061
78
 XDOT =      19727
274231                 XDOT =        6012
873185
 YDOT =      -6189
252335  feet/sec       YDOT =       -1886
484112  meter/sec
 ZDOT =      12754
849788                 ZDOT =        3887
678215


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   10137
94920493  
00016717  00000-0  10270-3 0  9054
2 25544  51
6467  25
7537 0010012 324
7058  35
3442 15
74087879 18717


Satellite: ISS
Catalog Number: 25544
Epoch time:      10137
94920493   =   yrday
fracday
Element set:     905
Inclination:       51
6467  deg
RA of node:        25
7537  deg
Eccentricity:     
0010012     
Arg of perigee:   324
7058  deg
Mean anomaly:      35
3442  deg
Mean motion:   15
74087879  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1871
Checksum:              315


Coasting Arc #7 (Orbit 1885)
---------------------------------------

Vector Time (GMT): 2010/138/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5753718
00                 A    =         6727041
60  meter
 Y    =        -722854
02  meter          E    =           
0008751
 Z    =       -3400213
93                 I    =           51
76881
 XDOT =       3378
755273                 Wp   =          356
20319
 YDOT =       5144
913228  meter/sec      RA   =           20
35097  deg
 ZDOT =       4631
527733                 TA   =          323
71212
                                          MA   =          323
77144
                                          Ha   =            191
255  n
mi
                                          Hp   =            184
437

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18877027
55                 X    =         5777891
09
 Y    =       -2371568
30  feet           Y    =         -658376
96  meter
 Z    =      -11155557
52                 Z    =        -3372203
70
 XDOT =      11085
155095                 XDOT =        3298
473656
 YDOT =      16879
636575  feet/sec       YDOT =        5182
247057  meter/sec
 ZDOT =      15195
300960                 ZDOT =        4647
747350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17324074
25                 X    =        -5280377
83
 Y    =        8019965
45  feet           Y    =         2444485
47  meter
 Z    =      -11043983
62                 Z    =        -3366206
21
 XDOT =     -15023
029041                 XDOT =       -4579
019252
 YDOT =     -11473
677289  feet/sec       YDOT =       -3497
176838  meter/sec
 ZDOT =      15259
897832                 ZDOT =        4651
216859


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   10138
90150622  
00016717  00000-0  10270-3 0  9061
2 25544  51
6467  20
8641 0010206 328
2833  31
7714 15
74069427 18861


Satellite: ISS
Catalog Number: 25544
Epoch time:      10138
90150622   =   yrday
fracday
Element set:     906
Inclination:       51
6467  deg
RA of node:        20
8641  deg
Eccentricity:     
0010206     
Arg of perigee:   328
2833  deg
Mean anomaly:      31
7714  deg
Mean motion:   15
74069427  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1886
Checksum:              296


Coasting Arc #8 (Orbit 1901)
---------------------------------------

Vector Time (GMT): 2010/139/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3282407
44                 A    =         6724600
33  meter
 Y    =       -4230862
12  meter          E    =           
0011716
 Z    =       -4077784
83                 I    =           51
73224
 XDOT =       6526
904398                 Wp   =           11
62066
 YDOT =      -1355
838832  meter/sec      RA   =           15
27397  deg
 ZDOT =      -3837
740958                 TA   =          218
88210
                                          MA   =          218
96644
                                          Ha   =            191
226  n
mi
                                          Hp   =            184
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10769053
29                 X    =        -3215044
08
 Y    =      -13880781
23  feet           Y    =        -4267190
92  meter
 Z    =      -13378559
16                 Z    =        -4093567
54
 XDOT =      21413
728340                 XDOT =        6560
223590
 YDOT =      -4448
290130  feet/sec       YDOT =       -1282
664442  meter/sec
 ZDOT =     -12591
013643                 ZDOT =       -3805
952443

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14574377
86                 X    =         4442270
37
 Y    =        9723694
00  feet           Y    =         2963781
93  meter
 Z    =      -13441418
32                 Z    =        -4096944
30
 XDOT =     -18219
930183                 XDOT =       -5553
434720
 YDOT =      10036
810662  feet/sec       YDOT =        3059
219890  meter/sec
 ZDOT =     -12464
387969                 ZDOT =       -3799
145453


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   10139
91727641  
00016717  00000-0  10270-3 0  9075
2 25544  51
6465  15
6477 0010109 332
1463  27
9158 15
74102516 19028


Satellite: ISS
Catalog Number: 25544
Epoch time:      10139
91727641   =   yrday
fracday
Element set:     907
Inclination:       51
6465  deg
RA of node:        15
6477  deg
Eccentricity:     
0010109     
Arg of perigee:   332
1463  deg
Mean anomaly:      27
9158  deg
Mean motion:   15
74102516  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1902
Checksum:              297


Coasting Arc #9 (Orbit 1917)
---------------------------------------

Vector Time (GMT): 2010/140/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5629639
40                 A    =         6727151
55  meter
 Y    =        1642500
27  meter          E    =           
0012492
 Z    =        3298143
86                 I    =           51
71138
 XDOT =      -4087
577885                 Wp   =           44
25455
 YDOT =      -4506
839680  meter/sec      RA   =           10
09297  deg
 ZDOT =      -4713
227225                 TA   =           97
09725
                                          MA   =           96
95518
                                          Ha   =            191
419  n
mi
                                          Hp   =            183
868

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18469945
54                 X    =        -5663609
54
 Y    =        5388780
42  feet           Y    =         1579356
12  meter
 Z    =       10820681
95                 Z    =         3270712
62
 XDOT =     -13410
688600                 XDOT =       -4013
981747
 YDOT =     -14786
219422  feet/sec       YDOT =       -4552
137574  meter/sec
 ZDOT =     -15463
343913                 ZDOT =       -4732
906272

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15636937
86                 X    =         4766138
66
 Y    =      -11314450
17  feet           Y    =        -3448644
41  meter
 Z    =       10711414
10                 Z    =         3264839
02
 XDOT =      16695
073792                 XDOT =        5088
658492
 YDOT =       8298
674455  feet/sec       YDOT =        2529
435974  meter/sec
 ZDOT =     -15541
722060                 ZDOT =       -4737
116884


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   10140
93302931  
00016717  00000-0  10270-3 0  9081
2 25544  51
6465  10
4309 0010175 336
9350  23
1355 15
74139233 19185


Satellite: ISS
Catalog Number: 25544
Epoch time:      10140
93302931   =   yrday
fracday
Element set:     908
Inclination:       51
6465  deg
RA of node:        10
4309  deg
Eccentricity:     
0010175     
Arg of perigee:   336
9350  deg
Mean anomaly:      23
1355  deg
Mean motion:   15
74139233  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1918
Checksum:              280


Coasting Arc #10 (Orbit 1933)
---------------------------------------

Vector Time (GMT): 2010/141/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3829666
87                 A    =         6724044
45  meter
 Y    =        3633084
00  meter          E    =           
0009307
 Z    =        4155019
10                 I    =           51
67191
 XDOT =      -6308
819740                 Wp   =           42
44619
 YDOT =       2398
601521  meter/sec      RA   =            5
01020  deg
 ZDOT =       3719
448347                 TA   =            9
59291
                                          MA   =            9
57515
                                          Ha   =            191
396  n
mi
                                          Hp   =            183
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12564523
86                 X    =         3768572
00
 Y    =       11919566
94  feet           Y    =         3675567
78  meter
 Z    =       13631952
44                 Z    =         4173475
54
 XDOT =     -20698
227492                 XDOT =       -6353
240953
 YDOT =       7869
427563  feet/sec       YDOT =        2327
803953  meter/sec
 ZDOT =      12202
914523                 ZDOT =        3688
692169

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15886803
87                 X    =        -4842297
82
 Y    =       -6748577
64  feet           Y    =        -2056966
47  meter
 Z    =       13705459
71                 Z    =         4177424
12
 XDOT =      16165
175844                 XDOT =        4927
145597
 YDOT =     -13533
491182  feet/sec       YDOT =       -4125
008112  meter/sec
 ZDOT =      12080
405289                 ZDOT =        3682
107532


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   10141
94876340  
00016717  00000-0  10270-3 0  9094
2 25544  51
6467   5
2136 0010223 340
0943  19
9820 15
74184575 19342


Satellite: ISS
Catalog Number: 25544
Epoch time:      10141
94876340   =   yrday
fracday
Element set:     909
Inclination:       51
6467  deg
RA of node:         5
2136  deg
Eccentricity:     
0010223     
Arg of perigee:   340
0943  deg
Mean anomaly:      19
9820  deg
Mean motion:   15
74184575  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1934
Checksum:              300


Coasting Arc #11 (Orbit 1948)
---------------------------------------

Vector Time (GMT): 2010/142/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5343330
89                 A    =         6727277
51  meter
 Y    =       -2540530
66  meter          E    =           
0010911
 Z    =       -3190805
80                 I    =           51
65184
 XDOT =       4669
300502                 Wp   =            8
01282
 YDOT =       3792
718927  meter/sec      RA   =          359
82613  deg
 ZDOT =       4812
013107                 TA   =          314
74007
                                          MA   =          314
82883
                                          Ha   =            191
702  n
mi
                                          Hp   =            183
306

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17530613
14                 X    =         5386842
95
 Y    =       -8335074
36  feet           Y    =        -2480534
88  meter
 Z    =      -10468522
97                 Z    =        -3164742
08
 XDOT =      15319
227368                 XDOT =        4603
166466
 YDOT =      12443
303565  feet/sec       YDOT =        3844
563772  meter/sec
 ZDOT =      15787
444578                 ZDOT =        4834
536386

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13276673
77                 X    =        -4046730
17
 Y    =       14236874
77  feet           Y    =         4339399
43  meter
 Z    =      -10364707
68                 Z    =        -3159162
90
 XDOT =     -17704
161807                 XDOT =       -5396
228519
 YDOT =      -4981
574393  feet/sec       YDOT =       -1518
383875  meter/sec
 ZDOT =      15877
145125                 ZDOT =        4839
353834


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   10142
90100036  
00016717  00000-0  10270-3 0  9105
2 25544  51
6462    
3238 0010326 343
8467  16
2366 15
74192755 19492


Satellite: ISS
Catalog Number: 25544
Epoch time:      10142
90100036   =   yrday
fracday
Element set:     910
Inclination:       51
6462  deg
RA of node:          
3238  deg
Eccentricity:     
0010326     
Arg of perigee:   343
8467  deg
Mean anomaly:      16
2366  deg
Mean motion:   15
74192755  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1949
Checksum:              281


Coasting Arc #12 (Orbit 1964)
---------------------------------------

Vector Time (GMT): 2010/143/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4271853
43                 A    =         6723650
96  meter
 Y    =       -2993011
18  meter          E    =           
0014389
 Z    =       -4255962
90                 I    =           51
60907
 XDOT =       5921
174867                 Wp   =           23
66969
 YDOT =      -3377
394866  meter/sec      RA   =          354
73846  deg
 ZDOT =      -3559
338382                 TA   =          210
09423
                                          MA   =          210
17698
                                          Ha   =            191
755  n
mi
                                          Hp   =            182
927

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14015267
16                 X    =        -4217392
53
 Y    =       -9819590
48  feet           Y    =        -3040476
78  meter
 Z    =      -13963132
88                 Z    =        -4276583
81
 XDOT =      19426
426729                 XDOT =        5975
792310
 YDOT =     -11080
691818  feet/sec       YDOT =       -3310
875125  meter/sec
 ZDOT =     -11677
619363                 ZDOT =       -3530
440451

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16638646
13                 X    =         5071459
34
 Y    =        3702360
92  feet           Y    =         1128479
61  meter
 Z    =      -14045252
91                 Z    =        -4280993
09
 XDOT =     -13459
653903                 XDOT =       -4102
502510
 YDOT =      16516
325147  feet/sec       YDOT =        5034
175905  meter/sec
 ZDOT =     -11562
516449                 ZDOT =       -3524
255014


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   10143
91670274  
00016717  00000-0  10270-3 0  9114
2 25544  51
6456 355
1067 0010344 347
9624  12
1290 15
74202508 19653


Satellite: ISS
Catalog Number: 25544
Epoch time:      10143
91670274   =   yrday
fracday
Element set:     911
Inclination:       51
6456  deg
RA of node:       355
1067  deg
Eccentricity:     
0010344     
Arg of perigee:   347
9624  deg
Mean anomaly:      12
1290  deg
Mean motion:   15
74202508  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1965
Checksum:              291


Coasting Arc #13 (Orbit 1980)
---------------------------------------

Vector Time (GMT): 2010/144/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4987656
89                 A    =         6727499
27  meter
 Y    =        3355662
56  meter          E    =           
0014679
 Z    =        3021366
80                 I    =           51
59298
 XDOT =      -5056
829046                 Wp   =           52
10237
 YDOT =      -3047
815803  meter/sec      RA   =          349
54951  deg
 ZDOT =      -4937
621540                 TA   =           92
93245
                                          MA   =           92
76445
                                          Ha   =            191
889  n
mi
                                          Hp   =            182
694

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16363703
71                 X    =        -5039487
34
 Y    =       11009391
61  feet           Y    =         3299597
53  meter
 Z    =        9912620
74                 Z    =         2997010
74
 XDOT =     -16590
646475                 XDOT =       -4998
385471
 YDOT =      -9999
395678  feet/sec       YDOT =       -3104
037035  meter/sec
 ZDOT =     -16199
545734                 ZDOT =       -4962
046392

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10635540
88                 X    =         3241712
86
 Y    =      -16666633
67  feet           Y    =        -5079989
94  meter
 Z    =        9815607
21                 Z    =         2991797
08
 XDOT =      17904
119242                 XDOT =        5457
175545
 YDOT =       1778
385349  feet/sec       YDOT =         542
051854  meter/sec
 ZDOT =     -16296
810176                 ZDOT =       -4967
267742


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   10144
93238617  
00016717  00000-0  10270-3 0  9129
2 25544  51
6461 349
8892 0010593 351
8144   8
2844 15
74277796 19812


Satellite: ISS
Catalog Number: 25544
Epoch time:      10144
93238617   =   yrday
fracday
Element set:     912
Inclination:       51
6461  deg
RA of node:       349
8892  deg
Eccentricity:     
0010593     
Arg of perigee:   351
8144  deg
Mean anomaly:       8
2844  deg
Mean motion:   15
74277796  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1981
Checksum:              335


Coasting Arc #14 (Orbit 1996)
---------------------------------------

Vector Time (GMT): 2010/145/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4538577
84                 A    =         6722958
34  meter
 Y    =        2335072
75  meter          E    =           
0010723
 Z    =        4364757
75                 I    =           51
54791
 XDOT =      -5445
535838                 Wp   =           47
52847
 YDOT =       4291
168716  meter/sec      RA   =          344
45567  deg
 ZDOT =       3368
583540                 TA   =            8
56033
                                          MA   =            8
54206
                                          Ha   =            191
868  n
mi
                                          Hp   =            182
420

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14890347
24                 X    =         4490925
70
 Y    =        7660999
83  feet           Y    =         2385558
86  meter
 Z    =       14320071
36                 Z    =         4386691
12
 XDOT =     -17865
931228                 XDOT =       -5509
480015
 YDOT =      14078
637520  feet/sec       YDOT =        4229
915556  meter/sec
 ZDOT =      11051
783268                 ZDOT =        3341
973808

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16651167
62                 X    =        -5075275
89
 Y    =        -801802
54  feet           Y    =         -244389
41  meter
 Z    =       14407412
41                 Z    =         4391379
30
 XDOT =      10382
897688                 XDOT =        3164
707215
 YDOT =     -19051
735393  feet/sec       YDOT =       -5806
968948  meter/sec
 ZDOT =      10945
788211                 ZDOT =        3336
276247


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   10145
94805370  
00016717  00000-0  10270-3 0  9138
2 25544  51
6455 344
6717 0010499 355
9402   4
1674 15
74283211 19973


Satellite: ISS
Catalog Number: 25544
Epoch time:      10145
94805370   =   yrday
fracday
Element set:     913
Inclination:       51
6455  deg
RA of node:       344
6717  deg
Eccentricity:     
0010499     
Arg of perigee:   355
9402  deg
Mean anomaly:       4
1674  deg
Mean motion:   15
74283211  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1997
Checksum:              315


Coasting Arc #15 (Orbit 2011)
---------------------------------------

Vector Time (GMT): 2010/146/21:28:05
923
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4479797
27                 A    =         6727801
24  meter
 Y    =       -4120015
09  meter          E    =           
0013409
 Z    =       -2853540
60                 I    =           51
53507
 XDOT =       5326
521741                 Wp   =           17
52576
 YDOT =       2291
810826  meter/sec      RA   =          339
26358  deg
 ZDOT =       5071
897493                 TA   =          309
64344
                                          MA   =          309
76168
                                          Ha   =            192
123  n
mi
                                          Hp   =            182
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14697497
61                 X    =         4539397
30
 Y    =      -13517109
89  feet           Y    =        -4069585
68  meter
 Z    =       -9362009
85                 Z    =        -2831633
18
 XDOT =      17475
465029                 XDOT =        5275
859620
 YDOT =       7519
064391  feet/sec       YDOT =        2351
091168  meter/sec
 ZDOT =      16640
083637                 ZDOT =        5097
651467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7467172
69                 X    =        -2275994
24
 Y    =       18563309
81  feet           Y    =         5658096
83  meter
 Z    =       -9274739
08                 Z    =        -2826940
47
 XDOT =     -17566
740125                 XDOT =       -5354
342390
 YDOT =       1267
806753  feet/sec       YDOT =         386
427498  meter/sec
 ZDOT =      16742
639490                 ZDOT =        5103
156517


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   10146
90022678  
00016717  00000-0  10270-3 0  9148
2 25544  51
6452 339
7803 0010568    
0563    
0600 15
74312747 20124


Satellite: ISS
Catalog Number: 25544
Epoch time:      10146
90022678   =   yrday
fracday
Element set:     914
Inclination:       51
6452  deg
RA of node:       339
7803  deg
Eccentricity:     
0010568     
Arg of perigee:      
0563  deg
Mean anomaly:        
0600  deg
Mean motion:   15
74312747  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2012
Checksum:              266

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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