Date: May 12th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9256 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 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 2242)
---------------------------------------

Vector Time (GMT): 2008/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         213473
80                 A    =         6715477
05  meter
 Y    =       -4599788
86  meter          E    =           
0010581
 Z    =        4887941
70                 I    =           51
43921
 XDOT =       6887
627628                 Wp   =          157
41052
 YDOT =       2664
431997  meter/sec      RA   =          214
85672  deg
 ZDOT =       2195
354167                 TA   =          271
15777
                                          MA   =          271
27900
                                          Ha   =            187
506  n
mi
                                          Hp   =            180
502

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         700373
36                 X    =          241148
65
 Y    =      -15091170
79  feet           Y    =        -4597247
58  meter
 Z    =       16036554
15                 Z    =         4889045
38
 XDOT =      22597
203505                 XDOT =        6846
656947
 YDOT =       8741
574793  feet/sec       YDOT =        2741
224018  meter/sec
 ZDOT =       7202
605534                 ZDOT =        2228
715248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10607075
96                 X    =        -3233036
75
 Y    =      -10751900
35  feet           Y    =        -3277179
23  meter
 Z    =       16040311
91                 Z    =         4889087
07
 XDOT =      21006
359462                 XDOT =        6402
738364
 YDOT =      -9731
818552  feet/sec       YDOT =       -2966
258295  meter/sec
 ZDOT =       7330
989741                 ZDOT =        2234
485673


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   08130
55138401  
00020000  00000-0  20000-3 0  9008
2 25544  51
6409 215
5337 0006386 192
6751 167
4254 15
76207648 22433


Satellite: ISS
Catalog Number: 25544
Epoch time:      08130
55138401   =   yrday
fracday
Element set:     900
Inclination:       51
6409  deg
RA of node:       215
5337  deg
Eccentricity:     
0006386     
Arg of perigee:   192
6751  deg
Mean anomaly:     167
4254  deg
Mean motion:   15
76207648  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2243
Checksum:              283


Coasting Arc #2 (Orbit 2257)
---------------------------------------

Vector Time (GMT): 2008/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6162633
98                 A    =         6725319
13  meter
 Y    =       -2408145
20  meter          E    =           
0004049
 Z    =       -1203364
35                 I    =           51
49652
 XDOT =        782
369713                 Wp   =           69
57242
 YDOT =      -4924
759337  meter/sec      RA   =          209
66306  deg
 ZDOT =       5865
947790                 TA   =          277
20961
                                          MA   =          277
25564
                                          Ha   =            187
335  n
mi
                                          Hp   =            180
733

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20218615
42                 X    =        -6129401
97
 Y    =       -7900738
86  feet           Y    =        -2476873
36  meter
 Z    =       -3948045
78                 Z    =        -1233222
01
 XDOT =       2566
829767                 XDOT =         808
885264
 YDOT =     -16157
346907  feet/sec       YDOT =       -4915
862835  meter/sec
 ZDOT =      19245
235531                 ZDOT =        5869
812398

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19400529
75                 X    =        -5913281
47
 Y    =        9690866
66  feet           Y    =         2953776
16  meter
 Z    =       -4062966
71                 Z    =        -1238392
25
 XDOT =      -9636
110057                 XDOT =       -2937
086346
 YDOT =     -11239
297033  feet/sec       YDOT =       -3425
737736  meter/sec
 ZDOT =      19259
559056                 ZDOT =        5870
313600


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   08131
50239849  
00020000  00000-0  20000-3 0  9013
2 25544  51
6403 210
6345 0006099 196
9589 163
1372 15
76174627 22589


Satellite: ISS
Catalog Number: 25544
Epoch time:      08131
50239849   =   yrday
fracday
Element set:     901
Inclination:       51
6403  deg
RA of node:       210
6345  deg
Eccentricity:     
0006099     
Arg of perigee:   196
9589  deg
Mean anomaly:     163
1372  deg
Mean motion:   15
76174627  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2258
Checksum:              304


Coasting Arc #3 (Orbit 2273)
---------------------------------------

Vector Time (GMT): 2008/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1216464
82                 A    =         6713884
76  meter
 Y    =        4029818
22  meter          E    =           
0013511
 Z    =       -5240915
63                 I    =           51
48350
 XDOT =      -7145
192114                 Wp   =          110
46711
 YDOT =      -2812
644158  meter/sec      RA   =          204
51633  deg
 ZDOT =       -509
923934                 TA   =          154
70807
                                          MA   =          154
64186
                                          Ha   =            187
136  n
mi
                                          Hp   =            180
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3991026
32                 X    =        -1235977
07
 Y    =       13221188
39  feet           Y    =         4016106
39  meter
 Z    =      -17194605
10                 Z    =        -5246872
25
 XDOT =     -23442
231344                 XDOT =       -7110
732522
 YDOT =      -9227
835164  feet/sec       YDOT =       -2892
353064  meter/sec
 ZDOT =      -1672
978787                 ZDOT =        -544
551813

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7402543
75                 X    =         2256295
34
 Y    =       11625742
48  feet           Y    =         3543526
31  meter
 Z    =      -17217055
96                 Z    =        -5247758
66
 XDOT =     -21511
003366                 XDOT =       -6556
553826
 YDOT =      11049
544541  feet/sec       YDOT =        3367
901176  meter/sec
 ZDOT =      -1806
279139                 ZDOT =        -550
553882


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   08132
51679482  
00020000  00000-0  20000-3 0  9027
2 25544  51
6395 205
4079 0006152 200
8933 159
1980 15
76218254 22746


Satellite: ISS
Catalog Number: 25544
Epoch time:      08132
51679482   =   yrday
fracday
Element set:     902
Inclination:       51
6395  deg
RA of node:       205
4079  deg
Eccentricity:     
0006152     
Arg of perigee:   200
8933  deg
Mean anomaly:     159
1980  deg
Mean motion:   15
76218254  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2274
Checksum:              295


Coasting Arc #4 (Orbit 2289)
---------------------------------------

Vector Time (GMT): 2008/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6239207
20                 A    =         6725696
31  meter
 Y    =        2465221
07  meter          E    =           
0015115
 Z    =        -325264
52                 I    =           51
55110
 XDOT =      -2030
777869                 Wp   =          158
83513
 YDOT =       4357
843401  meter/sec      RA   =          199
35365  deg
 ZDOT =      -6026
068256                 TA   =           24
71009
                                          MA   =           24
63776
                                          Ha   =            186
970  n
mi
                                          Hp   =            180
860

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20469839
89                 X    =         6212757
07
 Y    =        8087995
64  feet           Y    =         2534843
59  meter
 Z    =       -1067140
82                 Z    =         -295018
51
 XDOT =      -6662
657049                 XDOT =       -2050
083458
 YDOT =      14297
386487  feet/sec       YDOT =        4335
026551  meter/sec
 ZDOT =     -19770
565144                 ZDOT =       -6035
980376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19379159
86                 X    =         5906767
92
 Y    =      -10445723
99  feet           Y    =        -3183856
67  meter
 Z    =        -950695
36                 Z    =         -289771
95
 XDOT =       5950
567328                 XDOT =        1813
732922
 YDOT =      12808
770434  feet/sec       YDOT =        3904
113228  meter/sec
 ZDOT =     -19808
173628                 ZDOT =       -6037
531322


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   08133
53117264  
00020000  00000-0  20000-3 0  9036
2 25544  51
6396 200
1812 0005982 203
4523 156
6370 15
76269579 22907


Satellite: ISS
Catalog Number: 25544
Epoch time:      08133
53117264   =   yrday
fracday
Element set:     903
Inclination:       51
6396  deg
RA of node:       200
1812  deg
Eccentricity:     
0005982     
Arg of perigee:   203
4523  deg
Mean anomaly:     156
6370  deg
Mean motion:   15
76269579  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2290
Checksum:              285


Coasting Arc #5 (Orbit 2305)
---------------------------------------

Vector Time (GMT): 2008/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2342842
94                 A    =         6713950
27  meter
 Y    =       -3622114
48  meter          E    =           
0002976
 Z    =        5143893
03                 I    =           51
54057
 XDOT =       7067
728678                 Wp   =          172
61509
 YDOT =       2806
434975  meter/sec      RA   =          194
18073  deg
 ZDOT =      -1245
725566                 TA   =          289
28310
                                          MA   =          289
31529
                                          Ha   =            186
653  n
mi
                                          Hp   =            181
012

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7686492
59                 X    =         2358183
68
 Y    =      -11883577
69  feet           Y    =        -3595829
97  meter
 Z    =       16876289
46                 Z    =         5155311
67
 XDOT =      23188
086215                 XDOT =        7041
872923
 YDOT =       9207
463829  feet/sec       YDOT =        2885
325861  meter/sec
 ZDOT =      -4087
026136                 ZDOT =       -1211
453067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4427053
80                 X    =        -1349366
00
 Y    =      -13387810
97  feet           Y    =        -4080604
78  meter
 Z    =       16919764
92                 Z    =         5157144
35
 XDOT =      20815
105478                 XDOT =        6344
444150
 YDOT =     -11869
901092  feet/sec       YDOT =       -3617
945853  meter/sec
 ZDOT =      -3955
066487                 ZDOT =       -1205
504265


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   08134
54552997  
00020000  00000-0  20000-3 0  9045
2 25544  51
6400 194
9542 0005994 209
1928 150
8902 15
76327109 23067


Satellite: ISS
Catalog Number: 25544
Epoch time:      08134
54552997   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:       194
9542  deg
Eccentricity:     
0005994     
Arg of perigee:   209
1928  deg
Mean anomaly:     150
8902  deg
Mean motion:   15
76327109  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2306
Checksum:              304


Coasting Arc #6 (Orbit 2321)
---------------------------------------

Vector Time (GMT): 2008/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5991732
27                 A    =         6724224
00  meter
 Y    =       -2428862
29  meter          E    =           
0009999
 Z    =        1837399
76                 I    =           51
60299
 XDOT =       3364
710745                 Wp   =           84
96355
 YDOT =      -4002
707185  meter/sec      RA   =          189
05000  deg
 ZDOT =       5655
654648                 TA   =          295
45077
                                          MA   =          295
55420
                                          Ha   =            186
605  n
mi
                                          Hp   =            181
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19657914
28                 X    =        -5973052
86
 Y    =       -7968708
30  feet           Y    =        -2495760
91  meter
 Z    =        6028214
43                 Z    =         1808336
95
 XDOT =      11039
077246                 XDOT =        3381
745207
 YDOT =     -13132
241419  feet/sec       YDOT =       -3964
986089  meter/sec
 ZDOT =      18555
297402                 ZDOT =        5672
041728

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18430477
45                 X    =        -5617609
53
 Y    =       10563529
63  feet           Y    =         3219763
83  meter
 Z    =        5916301
03                 Z    =         1803288
55
 XDOT =      -2803
355763                 XDOT =        -854
462837
 YDOT =     -15365
957174  feet/sec       YDOT =       -4683
543747  meter/sec
 ZDOT =      18617
821637                 ZDOT =        5674
712035


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   08135
55987296  
00020000  00000-0  20000-3 0  9052
2 25544  51
6395 189
7270 0005679 211
4440 148
6385 15
76302181 23226


Satellite: ISS
Catalog Number: 25544
Epoch time:      08135
55987296   =   yrday
fracday
Element set:     905
Inclination:       51
6395  deg
RA of node:       189
7270  deg
Eccentricity:     
0005679     
Arg of perigee:   211
4440  deg
Mean anomaly:     148
6385  deg
Mean motion:   15
76302181  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2322
Checksum:              310


Coasting Arc #7 (Orbit 2336)
---------------------------------------

Vector Time (GMT): 2008/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3516258
05                 A    =         6716202
96  meter
 Y    =        3416476
50  meter          E    =           
0010622
 Z    =       -4600007
59                 I    =           51
60589
 XDOT =      -6548
635874                 Wp   =          140
87911
 YDOT =      -2775
983071  meter/sec      RA   =          183
85502  deg
 ZDOT =       2939
621288                 TA   =          158
30924
                                          MA   =          158
26422
                                          Ha   =            186
351  n
mi
                                          Hp   =            181
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11536279
68                 X    =        -3531854
00
 Y    =       11208912
39  feet           Y    =         3377068
72  meter
 Z    =      -15091888
42                 Z    =        -4617127
49
 XDOT =     -21485
025834                 XDOT =       -6531
388010
 YDOT =      -9107
556007  feet/sec       YDOT =       -2849
117380  meter/sec
 ZDOT =       9644
426798                 ZDOT =        2907
849369

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2015584
40                 X    =          614350
13
 Y    =       15896048
47  feet           Y    =         4845115
57  meter
 Z    =      -15157296
08                 Z    =        -4619943
85
 XDOT =     -19110
594464                 XDOT =       -5824
909192
 YDOT =      11516
483492  feet/sec       YDOT =        3510
224168  meter/sec
 ZDOT =       9522
061610                 ZDOT =        2902
324379


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   08136
51080025  
00020000  00000-0  20000-3 0  9064
2 25544  51
6396 184
8264 0005636 215
5282 144
5508 15
76350772 23375


Satellite: ISS
Catalog Number: 25544
Epoch time:      08136
51080025   =   yrday
fracday
Element set:     906
Inclination:       51
6396  deg
RA of node:       184
8264  deg
Eccentricity:     
0005636     
Arg of perigee:   215
5282  deg
Mean anomaly:     144
5508  deg
Mean motion:   15
76350772  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2337
Checksum:              291


Coasting Arc #8 (Orbit 2352)
---------------------------------------

Vector Time (GMT): 2008/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5350320
38                 A    =         6720882
57  meter
 Y    =        2449195
66  meter          E    =           
0005111
 Z    =       -3242828
78                 I    =           51
65154
 XDOT =      -4655
343320                 Wp   =          168
22624
 YDOT =       3871
050036  meter/sec      RA   =          178
74828  deg
 ZDOT =      -4763
373448                 TA   =           49
75764
                                          MA   =           49
71295
                                          Ha   =            186
251  n
mi
                                          Hp   =            181
303

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17553544
56                 X    =         5338288
78
 Y    =        8035418
82  feet           Y    =         2508958
94  meter
 Z    =      -10639202
03                 Z    =        -3216865
56
 XDOT =     -15273
436088                 XDOT =       -4675
144025
 YDOT =      12700
295394  feet/sec       YDOT =        3818
880923  meter/sec
 ZDOT =     -15627
865644                 ZDOT =       -4786
037322

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16883363
15                 X    =         5146049
09
 Y    =       -9474447
30  feet           Y    =        -2887811
54  meter
 Z    =      -10539183
99                 Z    =        -3212343
28
 XDOT =        597
482437                 XDOT =         182
112647
 YDOT =      18522
303816  feet/sec       YDOT =        5645
598203  meter/sec
 ZDOT =     -15714
532555                 ZDOT =       -4789
789523


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   08137
52510631  
00020000  00000-0  20000-3 0  9078
2 25544  51
6400 179
5991 0005562 218
8350 141
2415 15
76389579 23535


Satellite: ISS
Catalog Number: 25544
Epoch time:      08137
52510631   =   yrday
fracday
Element set:     907
Inclination:       51
6400  deg
RA of node:       179
5991  deg
Eccentricity:     
0005562     
Arg of perigee:   218
8350  deg
Mean anomaly:     141
2415  deg
Mean motion:   15
76389579  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2353
Checksum:              295


Coasting Arc #9 (Orbit 2368)
---------------------------------------

Vector Time (GMT): 2008/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4542347
80                 A    =         6719506
80  meter
 Y    =       -3382714
65  meter          E    =           
0008665
 Z    =        3606366
16                 I    =           51
67565
 XDOT =       5637
445300                 Wp   =          110
62773
 YDOT =       2867
011623  meter/sec      RA   =          173
54523  deg
 ZDOT =      -4405
874775                 TA   =           26
16397
                                          MA   =           26
12022
                                          Ha   =            185
856  n
mi
                                          Hp   =            181
330

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14902715
88                 X    =         4562316
84
 Y    =      -11098145
17  feet           Y    =        -3331808
17  meter
 Z    =       11831909
99                 Z    =         3628481
53
 XDOT =      18495
555446                 XDOT =        5626
370288
 YDOT =       9406
206111  feet/sec       YDOT =        2929
991212  meter/sec
 ZDOT =     -14454
969733                 ZDOT =       -4378
514196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -519858
34                 X    =         -158452
82
 Y    =      -18519716
32  feet           Y    =        -5644809
53  meter
 Z    =       11916531
18                 Z    =         3632158
70
 XDOT =      17043
046804                 XDOT =        5194
720666
 YDOT =      -9723
112974  feet/sec       YDOT =       -2963
604834  meter/sec
 ZDOT =     -14349
533032                 ZDOT =       -4373
737668


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   08138
53939355  
00020000  00000-0  20000-3 0  9089
2 25544  51
6389 174
3719 0005492 223
8315 136
2414 15
76432258 23694


Satellite: ISS
Catalog Number: 25544
Epoch time:      08138
53939355   =   yrday
fracday
Element set:     908
Inclination:       51
6389  deg
RA of node:       174
3719  deg
Eccentricity:     
0005492     
Arg of perigee:   223
8315  deg
Mean anomaly:     136
2414  deg
Mean motion:   15
76432258  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2369
Checksum:              315


Coasting Arc #10 (Orbit 2384)
---------------------------------------

Vector Time (GMT): 2008/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4402505
92                 A    =         6717109
57  meter
 Y    =       -2607875
93  meter          E    =           
0008636
 Z    =        4351189
41                 I    =           51
69559
 XDOT =       5695
060121                 Wp   =          143
01536
 YDOT =      -3911
627592  meter/sec      RA   =          168
44463  deg
 ZDOT =       3407
541362                 TA   =          272
62511
                                          MA   =          272
72396
                                          Ha   =            185
882  n
mi
                                          Hp   =            181
409

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14443917
07                 X    =        -4394154
76
 Y    =       -8556023
41  feet           Y    =        -2657061
04  meter
 Z    =       14275555
80                 Z    =         4329821
60
 XDOT =      18684
580450                 XDOT =        5721
823725
 YDOT =     -12833
423858  feet/sec       YDOT =       -3847
792892  meter/sec
 ZDOT =      11179
597645                 ZDOT =        3435
273126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15241510
44                 X    =        -4645612
38
 Y    =        7202365
00  feet           Y    =         2195280
85  meter
 Z    =       14193169
78                 Z    =         4326078
15
 XDOT =        379
883597                 XDOT =         115
788520
 YDOT =     -21502
820751  feet/sec       YDOT =       -6554
059765  meter/sec
 ZDOT =      11285
757883                 ZDOT =        3439
899003


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   08139
55366473  
00020000  00000-0  20000-3 0  9098
2 25544  51
6383 169
1438 0005356 226
3990 133
6731 15
76431267 23854


Satellite: ISS
Catalog Number: 25544
Epoch time:      08139
55366473   =   yrday
fracday
Element set:     909
Inclination:       51
6383  deg
RA of node:       169
1438  deg
Eccentricity:     
0005356     
Arg of perigee:   226
3990  deg
Mean anomaly:     133
6731  deg
Mean motion:   15
76431267  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2385
Checksum:              314


Coasting Arc #11 (Orbit 2399)
---------------------------------------

Vector Time (GMT): 2008/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5309715
75                 A    =         6722797
10  meter
 Y    =        3452787
75  meter          E    =           
0000755
 Z    =       -2252759
75                 I    =           51
74503
 XDOT =      -4389
238832                 Wp   =          358
37021
 YDOT =      -3182
164942  meter/sec      RA   =          163
25188  deg
 ZDOT =       5468
775077                 TA   =          336
36793
                                          MA   =          336
37139
                                          Ha   =            185
588  n
mi
                                          Hp   =            181
371

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17420327
26                 X    =        -5336987
01
 Y    =       11328043
81  feet           Y    =         3393259
28  meter
 Z    =       -7390944
08                 Z    =        -2278620
68
 XDOT =     -14400
389869                 XDOT =       -4379
895995
 YDOT =     -10440
173694  feet/sec       YDOT =       -3231
196379  meter/sec
 ZDOT =      17942
175449                 ZDOT =        5447
474013

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -44221
90                 X    =          -13478
84
 Y    =       20744076
68  feet           Y    =         6322794
57  meter
 Z    =       -7489977
29                 Z    =        -2282945
08
 XDOT =     -15166
469553                 XDOT =       -4622
739920
 YDOT =       6415
484854  feet/sec       YDOT =        1955
439783  meter/sec
 ZDOT =      17859
981515                 ZDOT =        5443
722366


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   08140
50452668  
00020000  00000-0  20000-3 0  9109
2 25544  51
6391 164
2431 0005395 229
8014 130
2679 15
76499141 24007


Satellite: ISS
Catalog Number: 25544
Epoch time:      08140
50452668   =   yrday
fracday
Element set:     910
Inclination:       51
6391  deg
RA of node:       164
2431  deg
Eccentricity:     
0005395     
Arg of perigee:   229
8014  deg
Mean anomaly:     130
2679  deg
Mean motion:   15
76499141  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2400
Checksum:              278


Coasting Arc #12 (Orbit 2415)
---------------------------------------

Vector Time (GMT): 2008/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3214303
74                 A    =         6714002
10  meter
 Y    =        3018585
74  meter          E    =           
0008760
 Z    =       -5070482
78                 I    =           51
74207
 XDOT =      -6374
060232                 Wp   =           90
85950
 YDOT =       3979
701126  meter/sec      RA   =          158
13899  deg
 ZDOT =      -1674
060955                 TA   =          163
07846
                                          MA   =          163
04923
                                          Ha   =            185
445  n
mi
                                          Hp   =            181
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10545615
95                 X    =         3204942
48
 Y    =        9903496
54  feet           Y    =         3054478
32  meter
 Z    =      -16635442
21                 Z    =        -5054889
71
 XDOT =     -20912
271101                 XDOT =       -6409
955705
 YDOT =      13056
762223  feet/sec       YDOT =        3908
222280  meter/sec
 ZDOT =      -5492
325967                 ZDOT =       -1705
113320

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14052373
83                 X    =         4283163
54
 Y    =       -3717627
58  feet           Y    =        -1133132
89  meter
 Z    =      -16575199
30                 Z    =        -5052120
75
 XDOT =       -364
540034                 XDOT =        -111
111802
 YDOT =      23601
949669  feet/sec       YDOT =        7193
874259  meter/sec
 ZDOT =      -5611
275091                 ZDOT =       -1710
316648


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   08141
51876241  
00020000  00000-0  20000-3 0  9119
2 25544  51
6386 159
0150 0005417 235
2106 124
8549 15
76481403 24163


Satellite: ISS
Catalog Number: 25544
Epoch time:      08141
51876241   =   yrday
fracday
Element set:     911
Inclination:       51
6386  deg
RA of node:       159
0150  deg
Eccentricity:     
0005417     
Arg of perigee:   235
2106  deg
Mean anomaly:     124
8549  deg
Mean motion:   15
76481403  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2416
Checksum:              274

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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