Date: June 27th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 2983)
---------------------------------------

Vector Time (GMT): 2008/177/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6274479
02                 A    =         6728320
47  meter
 Y    =        1447428
58  meter          E    =           
0004162
 Z    =       -1943578
61                 I    =           51
50416
 XDOT =        523
728044                 Wp   =          242
15532
 YDOT =      -5258
347926  meter/sec      RA   =          333
12032  deg
 ZDOT =      -5599
574251                 TA   =          319
51106
                                          MA   =          319
54202
                                          Ha   =            188
055  n
mi
                                          Hp   =            185
508

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20585561
09                 X    =        -6280756
53
 Y    =        4748781
42  feet           Y    =         1377228
90  meter
 Z    =       -6376570
24                 Z    =        -1974075
02
 XDOT =       1718
267861                 XDOT =         609
690441
 YDOT =     -17251
797657  feet/sec       YDOT =       -5252
009962  meter/sec
 ZDOT =     -18371
306599                 ZDOT =       -5596
821839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5904963
04                 X    =         1799832
74
 Y    =       20246917
73  feet           Y    =         6171260
52  meter
 Z    =       -6493891
92                 Z    =        -1979338
26
 XDOT =     -15851
016448                 XDOT =       -4831
389813
 YDOT =      -1273
581028  feet/sec       YDOT =        -388
187497  meter/sec
 ZDOT =     -18361
124696                 ZDOT =       -5596
470807


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   08177
52784643  
00020000  00000-0  20000-3 0  9001
2 25544  51
6376 333
4771 0008696 292
6787  67
3457 15
74756549 29846


Satellite: ISS
Catalog Number: 25544
Epoch time:      08177
52784643   =   yrday
fracday
Element set:     900
Inclination:       51
6376  deg
RA of node:       333
4771  deg
Eccentricity:     
0008696     
Arg of perigee:   292
6787  deg
Mean anomaly:      67
3457  deg
Mean motion:   15
74756549  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2984
Checksum:              349


Coasting Arc #2 (Orbit 2999)
---------------------------------------

Vector Time (GMT): 2008/178/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -353861
26                 A    =         6720218
90  meter
 Y    =        4715615
26  meter          E    =           
0007443
 Z    =        4778947
23                 I    =           51
45044
 XDOT =      -6991
611574                 Wp   =          348
90778
 YDOT =       2023
021662  meter/sec      RA   =          327
92942  deg
 ZDOT =      -2507
366665                 TA   =          125
73878
                                          MA   =          125
66953
                                          Ha   =            188
249  n
mi
                                          Hp   =            185
456

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1160962
15                 X    =         -429781
03
 Y    =       15471178
66  feet           Y    =         4711233
09  meter
 Z    =       15678960
73                 Z    =         4777044
35
 XDOT =     -22938
358181                 XDOT =       -7001
533332
 YDOT =       6637
210178  feet/sec       YDOT =        1944
782292  meter/sec
 ZDOT =      -8226
268585                 ZDOT =       -2541
355833

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15521343
15                 X    =         4730905
39
 Y    =         105132
84  feet           Y    =           32044
49  meter
 Z    =       15672008
99                 Z    =         4776828
34
 XDOT =       8316
160808                 XDOT =        2534
765814
 YDOT =      21206
964850  feet/sec       YDOT =        6463
882886  meter/sec
 ZDOT =      -8356
991501                 ZDOT =       -2547
211010


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   08178
54320270  
00020000  00000-0  20000-3 0  9017
2 25544  51
6374 328
2564 0008576 295
6132  64
4144 15
74715556 30004


Satellite: ISS
Catalog Number: 25544
Epoch time:      08178
54320270   =   yrday
fracday
Element set:     901
Inclination:       51
6374  deg
RA of node:       328
2564  deg
Eccentricity:     
0008576     
Arg of perigee:   295
6132  deg
Mean anomaly:      64
4144  deg
Mean motion:   15
74715556  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3000
Checksum:              283


Coasting Arc #3 (Orbit 3015)
---------------------------------------

Vector Time (GMT): 2008/179/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5917929
23                 A    =         6727264
33  meter
 Y    =       -2055002
14  meter          E    =           
0009693
 Z    =        2434037
27                 I    =           51
45209
 XDOT =       -271
583697                 Wp   =           36
54447
 YDOT =       5547
163074  meter/sec      RA   =          322
81595  deg
 ZDOT =       5340
442402                 TA   =          351
04112
                                          MA   =          351
05841
                                          Ha   =            188
208  n
mi
                                          Hp   =            185
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19415778
32                 X    =         5928644
57
 Y    =       -6742133
01  feet           Y    =        -1988764
89  meter
 Z    =        7985686
57                 Z    =         2462812
49
 XDOT =       -891
022629                 XDOT =        -359
535829
 YDOT =      18199
353918  feet/sec       YDOT =        5543
633570  meter/sec
 ZDOT =      17521
136491                 ZDOT =        5338
910166

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8475774
53                 X    =        -2583416
08
 Y    =      -18676474
85  feet           Y    =        -5692589
53  meter
 Z    =        8096328
08                 Z    =         2467760
80
 XDOT =      16852
231818                 XDOT =        5136
560258
 YDOT =        -50
276114  feet/sec       YDOT =         -15
324159  meter/sec
 ZDOT =      17515
678313                 ZDOT =        5338
778750


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   08179
55854189  
00020000  00000-0  20000-3 0  9021
2 25544  51
6384 323
0359 0008676 299
1302  60
8992 15
74797206 30169


Satellite: ISS
Catalog Number: 25544
Epoch time:      08179
55854189   =   yrday
fracday
Element set:     902
Inclination:       51
6384  deg
RA of node:       323
0359  deg
Eccentricity:     
0008676     
Arg of perigee:   299
1302  deg
Mean anomaly:      60
8992  deg
Mean motion:   15
74797206  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3016
Checksum:              322


Coasting Arc #4 (Orbit 3030)
---------------------------------------

Vector Time (GMT): 2008/180/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          95265
99                 A    =         6721040
66  meter
 Y    =       -4972526
82  meter          E    =           
0002529
 Z    =       -4521920
18                 I    =           51
40860
 XDOT =       6543
718682                 Wp   =           57
90149
 YDOT =      -2659
957900  meter/sec      RA   =          317
61572  deg
 ZDOT =       3065
454183                 TA   =          242
70506
                                          MA   =          242
73082
                                          Ha   =            188
528  n
mi
                                          Hp   =            184
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         312552
46                 X    =          172829
35
 Y    =      -16314064
36  feet           Y    =        -4971027
09  meter
 Z    =      -14835696
13                 Z    =        -4521269
77
 XDOT =      21468
893315                 XDOT =        6558
084857
 YDOT =      -8726
895998  feet/sec       YDOT =       -2586
702455  meter/sec
 ZDOT =      10057
264379                 ZDOT =        3097
278319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16261526
45                 X    =        -4956513
26
 Y    =        1368113
16  feet           Y    =          417000
89  meter
 Z    =      -14833586
50                 Z    =        -4521277
16
 XDOT =     -10889
728858                 XDOT =       -3319
189356
 YDOT =     -19156
940095  feet/sec       YDOT =       -5839
035341  meter/sec
 ZDOT =      10179
599633                 ZDOT =        3102
741968


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   08180
51041297  
00020000  00000-0  20000-3 0  9038
2 25544  51
6387 318
1425 0008727 303
6148  56
4182 15
74785196 30311


Satellite: ISS
Catalog Number: 25544
Epoch time:      08180
51041297   =   yrday
fracday
Element set:     903
Inclination:       51
6387  deg
RA of node:       318
1425  deg
Eccentricity:     
0008727     
Arg of perigee:   303
6148  deg
Mean anomaly:      56
4182  deg
Mean motion:   15
74785196  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3031
Checksum:              291


Coasting Arc #5 (Orbit 3046)
---------------------------------------

Vector Time (GMT): 2008/181/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5497901
78                 A    =         6726070
83  meter
 Y    =        2546770
62  meter          E    =           
0004560
 Z    =       -2922456
24                 I    =           51
40527
 XDOT =        -49
294084                 Wp   =          323
16622
 YDOT =      -5852
105830  meter/sec      RA   =          312
50388  deg
 ZDOT =      -4999
453719                 TA   =          250
60227
                                          MA   =          250
65156
                                          Ha   =            188
714  n
mi
                                          Hp   =            184
512

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18037735
49                 X    =        -5511774
67
 Y    =        8355546
65  feet           Y    =         2485212
92  meter
 Z    =       -9588111
04                 Z    =        -2949198
50
 XDOT =       -161
725998                 XDOT =          40
435402
 YDOT =     -19199
822278  feet/sec       YDOT =       -5852
154410  meter/sec
 ZDOT =     -16402
407213                 ZDOT =       -4999
476351

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10540300
20                 X    =         3212683
50
 Y    =       16795703
23  feet           Y    =         5119330
34  meter
 Z    =       -9690890
56                 Z    =        -2953783
44
 XDOT =     -17815
673582                 XDOT =       -5430
217308
 YDOT =       1701
837056  feet/sec       YDOT =         518
719935  meter/sec
 ZDOT =     -16402
956824                 ZDOT =       -4999
621240


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   08181
52572800  
00020000  00000-0  20000-3 0  9040
2 25544  51
6388 312
9213 0008759 307
8321  52
2049 15
74812817 30477


Satellite: ISS
Catalog Number: 25544
Epoch time:      08181
52572800   =   yrday
fracday
Element set:     904
Inclination:       51
6388  deg
RA of node:       312
9213  deg
Eccentricity:     
0008759     
Arg of perigee:   307
8321  deg
Mean anomaly:      52
2049  deg
Mean motion:   15
74812817  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3047
Checksum:              289


Coasting Arc #6 (Orbit 3062)
---------------------------------------

Vector Time (GMT): 2008/182/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         205863
44                 A    =         6722249
89  meter
 Y    =        5254957
74  meter          E    =           
0009221
 Z    =        4189849
78                 I    =           51
37386
 XDOT =      -6026
251688                 Wp   =           20
91475
 YDOT =       3133
788280  meter/sec      RA   =          307
29494  deg
 ZDOT =      -3623
396799                 TA   =          106
18280
                                          MA   =          106
08130
                                          Ha   =            188
906  n
mi
                                          Hp   =            184
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         675404
99                 X    =          126732
73
 Y    =       17240675
01  feet           Y    =         5256816
47  meter
 Z    =       13746226
32                 Z    =         4190658
81
 XDOT =     -19771
166956                 XDOT =       -6043
244420
 YDOT =      10281
457612  feet/sec       YDOT =        3066
305064  meter/sec
 ZDOT =     -11887
784774                 ZDOT =       -3652
713087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16980677
90                 X    =         5175710
62
 Y    =       -3042461
91  feet           Y    =         -927342
39  meter
 Z    =       13749755
95                 Z    =         4190925
61
 XDOT =      12756
730145                 XDOT =        3888
251348
 YDOT =      16802
606873  feet/sec       YDOT =        5121
434575  meter/sec
 ZDOT =     -12000
437692                 ZDOT =       -3657
733409


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   08182
54103071  
00020000  00000-0  20000-3 0  9054
2 25544  51
6394 307
7007 0008690 311
9980  48
0443 15
74805481 30636


Satellite: ISS
Catalog Number: 25544
Epoch time:      08182
54103071   =   yrday
fracday
Element set:     905
Inclination:       51
6394  deg
RA of node:       307
7007  deg
Eccentricity:     
0008690     
Arg of perigee:   311
9980  deg
Mean anomaly:      48
0443  deg
Mean motion:   15
74805481  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3063
Checksum:              282


Coasting Arc #7 (Orbit 3078)
---------------------------------------

Vector Time (GMT): 2008/183/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5025712
09                 A    =         6724543
76  meter
 Y    =       -2889020
21  meter          E    =           
0008764
 Z    =        3396522
65                 I    =           51
36686
 XDOT =        447
387356                 Wp   =           45
53355
 YDOT =       6174
404314  meter/sec      RA   =          302
18441  deg
 ZDOT =       4588
641684                 TA   =          354
79422
                                          MA   =          354
80333
                                          Ha   =            188
860  n
mi
                                          Hp   =            184
044

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16488556
74                 X    =         5041144
37
 Y    =       -9478412
78  feet           Y    =        -2832734
34  meter
 Z    =       11143447
00                 Z    =         3420974
35
 XDOT =       1467
806285                 XDOT =         356
020166
 YDOT =      20257
232000  feet/sec       YDOT =        6178
895308  meter/sec
 ZDOT =      15054
598701                 ZDOT =        4590
594623

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11972285
88                 X    =        -3649152
74
 Y    =      -14706277
44  feet           Y    =        -4482473
36  meter
 Z    =       11237392
83                 Z    =         3425157
33
 XDOT =      18706
567939                 XDOT =        5701
761908
 YDOT =      -3716
213416  feet/sec       YDOT =       -1132
701849  meter/sec
 ZDOT =      15062
607458                 ZDOT =        4591
082753


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   08183
55631690  
00020000  00000-0  20000-3 0  9060
2 25544  51
6404 302
4798 0008823 315
7404  44
3053 15
74887866 30798


Satellite: ISS
Catalog Number: 25544
Epoch time:      08183
55631690   =   yrday
fracday
Element set:     906
Inclination:       51
6404  deg
RA of node:       302
4798  deg
Eccentricity:     
0008823     
Arg of perigee:   315
7404  deg
Mean anomaly:      44
3053  deg
Mean motion:   15
74887866  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3079
Checksum:              310


Coasting Arc #8 (Orbit 3093)
---------------------------------------

Vector Time (GMT): 2008/184/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -605799
92                 A    =         6723430
59  meter
 Y    =       -5510501
46  meter          E    =           
0005323
 Z    =       -3800035
26                 I    =           51
34825
 XDOT =       5487
048384                 Wp   =            2
53684
 YDOT =      -3462
137344  meter/sec      RA   =          296
97114  deg
 ZDOT =       4151
230743                 TA   =          311
07976
                                          MA   =          311
12573
                                          Ha   =            189
216  n
mi
                                          Hp   =            183
806

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1987532
55                 X    =         -525675
87
 Y    =      -18079073
02  feet           Y    =        -5516826
96  meter
 Z    =      -12467307
29                 Z    =        -3802784
91
 XDOT =      18002
127245                 XDOT =        5505
188985
 YDOT =     -11358
718321  feet/sec       YDOT =       -3400
677588  meter/sec
 ZDOT =      13619
523436                 ZDOT =        4177
929850

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17458836
15                 X    =        -5321453
26
 Y    =        5071199
43  feet           Y    =         1545701
59  meter
 Z    =      -12478337
03                 Z    =        -3803397
13
 XDOT =     -13968
704944                 XDOT =       -4257
661267
 YDOT =     -14369
775993  feet/sec       YDOT =       -4379
907723  meter/sec
 ZDOT =      13722
087365                 ZDOT =        4182
492229


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   08184
50813916  
00020000  00000-0  20000-3 0  9070
2 25544  51
6404 297
5865 0009019 319
9854  40
0644 15
74858109 30944


Satellite: ISS
Catalog Number: 25544
Epoch time:      08184
50813916   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:       297
5865  deg
Eccentricity:     
0009019     
Arg of perigee:   319
9854  deg
Mean anomaly:      40
0644  deg
Mean motion:   15
74858109  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3094
Checksum:              316


Coasting Arc #9 (Orbit 3109)
---------------------------------------

Vector Time (GMT): 2008/185/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4562623
58                 A    =         6723140
04  meter
 Y    =        3105566
64  meter          E    =           
0009097
 Z    =       -3847172
32                 I    =           51
33573
 XDOT =       -936
709577                 Wp   =            6
23750
 YDOT =      -6450
863809  meter/sec      RA   =          291
85999  deg
 ZDOT =      -4088
434542                 TA   =          220
84644
                                          MA   =          220
91465
                                          Ha   =            189
357  n
mi
                                          Hp   =            183
436

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14969237
46                 X    =        -4578322
83
 Y    =       10188866
94  feet           Y    =         3054457
85  meter
 Z    =      -12621956
42                 Z    =        -3869374
66
 XDOT =      -3073
194149                 XDOT =        -844
644804
 YDOT =     -21164
251343  feet/sec       YDOT =       -6460
822960  meter/sec
 ZDOT =     -13413
499153                 ZDOT =       -4092
762827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12873186
74                 X    =         3923747
32
 Y    =       12649591
70  feet           Y    =         3855595
55  meter
 Z    =      -12707232
45                 Z    =        -3873164
45
 XDOT =     -19265
180224                 XDOT =       -5872
026932
 YDOT =       6087
591353  feet/sec       YDOT =        1855
497844  meter/sec
 ZDOT =     -13430
694068                 ZDOT =       -4093
675552


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   08185
52340238  
00020000  00000-0  20000-3 0  9086
2 25544  51
6407 292
3660 0008940 323
9638  36
0922 15
74885384 31108


Satellite: ISS
Catalog Number: 25544
Epoch time:      08185
52340238   =   yrday
fracday
Element set:     908
Inclination:       51
6407  deg
RA of node:       292
3660  deg
Eccentricity:     
0008940     
Arg of perigee:   323
9638  deg
Mean anomaly:      36
0922  deg
Mean motion:   15
74885384  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3110
Checksum:              296


Coasting Arc #10 (Orbit 3125)
---------------------------------------

Vector Time (GMT): 2008/186/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1055396
59                 A    =         6724809
81  meter
 Y    =        5751381
72  meter          E    =           
0010949
 Z    =        3322165
60                 I    =           51
33132
 XDOT =      -4962
699719                 Wp   =           47
23233
 YDOT =       3606
815255  meter/sec      RA   =          286
64469  deg
 ZDOT =      -4650
571680                 TA   =           93
51909
                                          MA   =           93
39385
                                          Ha   =            189
546  n
mi
                                          Hp   =            183
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3462587
22                 X    =          974867
12
 Y    =       18869362
60  feet           Y    =         5762732
86  meter
 Z    =       10899493
43                 Z    =         3327098
14
 XDOT =     -16281
823224                 XDOT =       -4980
071663
 YDOT =      11833
383383  feet/sec       YDOT =        3551
223284  meter/sec
 ZDOT =     -15257
781103                 ZDOT =       -4674
721506

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17735231
17                 X    =         5405698
46
 Y    =       -7285531
10  feet           Y    =        -2220629
88  meter
 Z    =       10918970
83                 Z    =         3328102
31
 XDOT =      14437
834137                 XDOT =        4400
651845
 YDOT =      12056
411412  feet/sec       YDOT =        3674
794198  meter/sec
 ZDOT =     -15350
520157                 ZDOT =       -4678
838544


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   08186
53865302  
00020000  00000-0  20000-3 0  9093
2 25544  51
6403 287
1459 0008922 328
9594  31
1041 15
74897927 31269


Satellite: ISS
Catalog Number: 25544
Epoch time:      08186
53865302   =   yrday
fracday
Element set:     909
Inclination:       51
6403  deg
RA of node:       287
1459  deg
Eccentricity:     
0008922     
Arg of perigee:   328
9594  deg
Mean anomaly:      31
1041  deg
Mean motion:   15
74897927  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3126
Checksum:              314


Coasting Arc #11 (Orbit 3141)
---------------------------------------

Vector Time (GMT): 2008/187/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4123367
11                 A    =         6721460
17  meter
 Y    =       -3161664
45  meter          E    =           
0007157
 Z    =        4256265
17                 I    =           51
31362
 XDOT =       1506
004436                 Wp   =           45
90359
 YDOT =       6691
607488  meter/sec      RA   =          281
52929  deg
 ZDOT =       3512
985232                 TA   =            8
36982
                                          MA   =            8
35789
                                          Ha   =            189
513  n
mi
                                          Hp   =            182
944

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13528107
32                 X    =         4137739
14
 Y    =      -10372914
86  feet           Y    =        -3115474
94  meter
 Z    =       13964124
59                 Z    =         4276330
48
 XDOT =       4940
959436                 XDOT =        1414
000789
 YDOT =      21954
092807  feet/sec       YDOT =        6707
933492  meter/sec
 ZDOT =      11525
542100                 ZDOT =        3520
078892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13151498
89                 X    =        -4008576
86
 Y    =      -10746516
80  feet           Y    =        -3275538
32  meter
 Z    =       14041163
75                 Z    =         4279746
71
 XDOT =      19493
722955                 XDOT =        5941
686757
 YDOT =      -8766
186998  feet/sec       YDOT =       -2671
933797  meter/sec
 ZDOT =      11553
436931                 ZDOT =        3521
487577


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   08187
55388835  
00020000  00000-0  20000-3 0  9109
2 25544  51
6404 281
9245 0009048 332
5811  27
4874 15
74960532 31421


Satellite: ISS
Catalog Number: 25544
Epoch time:      08187
55388835   =   yrday
fracday
Element set:     910
Inclination:       51
6404  deg
RA of node:       281
9245  deg
Eccentricity:     
0009048     
Arg of perigee:   332
5811  deg
Mean anomaly:      27
4874  deg
Mean motion:   15
74960532  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3142
Checksum:              302


Coasting Arc #12 (Orbit 3156)
---------------------------------------

Vector Time (GMT): 2008/188/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1597786
75                 A    =         6726101
88  meter
 Y    =       -5898854
27  meter          E    =           
0010776
 Z    =       -2794690
23                 I    =           51
32392
 XDOT =       4502
898603                 Wp   =            1
89838
 YDOT =      -3627
131697  meter/sec      RA   =          276
31621  deg
 ZDOT =       5092
690595                 TA   =          325
91388
                                          MA   =          325
98304
                                          Ha   =            189
828  n
mi
                                          Hp   =            182
724

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5242082
52                 X    =        -1518130
23
 Y    =      -19353196
43  feet           Y    =        -5916275
87  meter
 Z    =       -9168931
19                 Z    =        -2802259
47
 XDOT =      14773
289380                 XDOT =        4518
384182
 YDOT =     -11900
038376  feet/sec       YDOT =       -3576
691826  meter/sec
 ZDOT =      16708
302478                 ZDOT =        5114
602393

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17507835
21                 X    =        -5336388
17
 Y    =        9744554
72  feet           Y    =         2970140
28  meter
 Z    =       -9198603
16                 Z    =        -2803734
24
 XDOT =     -14404
286796                 XDOT =       -4390
426615
 YDOT =     -10062
792296  feet/sec       YDOT =       -3067
139092  meter/sec
 ZDOT =      16792
413394                 ZDOT =        5118
327602


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   08188
50566242  
00020000  00000-0  20000-3 0  9116
2 25544  51
6400 277
0309 0009277 336
2518  23
8217 15
74930063 31576


Satellite: ISS
Catalog Number: 25544
Epoch time:      08188
50566242   =   yrday
fracday
Element set:     911
Inclination:       51
6400  deg
RA of node:       277
0309  deg
Eccentricity:     
0009277     
Arg of perigee:   336
2518  deg
Mean anomaly:      23
8217  deg
Mean motion:   15
74930063  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3157
Checksum:              284

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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