Date: June 28th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 3015)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5917694
75                 A    =         6727204
12  meter
 Y    =       -2050028
82  meter          E    =           
0009675
 Z    =        2438648
70                 I    =           51
45201
 XDOT =       -278
421843                 Wp   =           36
27577
 YDOT =       5549
508643  meter/sec      RA   =          322
81730  deg
 ZDOT =       5337
691650                 TA   =          351
36682
                                          MA   =          351
38345
                                          Ha   =            188
193  n
mi
                                          Hp   =            185
123

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19415009
01                 X    =         5928332
09
 Y    =       -6725816
34  feet           Y    =        -1983794
63  meter
 Z    =        8000815
96                 Z    =         2467422
60
 XDOT =       -913
457489                 XDOT =        -366
386332
 YDOT =      18207
049355  feet/sec       YDOT =        5545
902602  meter/sec
 ZDOT =      17512
111712                 ZDOT =        5336
126164

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8459447
59                 X    =        -2578439
63
 Y    =      -18677106
76  feet           Y    =        -5692782
14  meter
 Z    =        8111452
76                 Z    =         2472370
80
 XDOT =      16861
884892                 XDOT =        5139
502515
 YDOT =        -29
876298  feet/sec       YDOT =          -9
106296  meter/sec
 ZDOT =      17506
525686                 ZDOT =        5335
989029


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
55853120  
00020000  00000-0  20000-3 0  9003
2 25544  51
6384 323
0373 0008732 299
1474  60
8815 15
74814860 30168


Satellite: ISS
Catalog Number: 25544
Epoch time:      08179
55853120   =   yrday
fracday
Element set:     900
Inclination:       51
6384  deg
RA of node:       323
0373  deg
Eccentricity:     
0008732     
Arg of perigee:   299
1474  deg
Mean anomaly:      60
8815  deg
Mean motion:   15
74814860  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3016
Checksum:              293


Coasting Arc #2 (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    =         107798
35                 A    =         6721006
41  meter
 Y    =       -4977494
33  meter          E    =           
0002483
 Z    =       -4516020
65                 I    =           51
40863
 XDOT =       6543
593896                 Wp   =           56
03973
 YDOT =      -2647
457526  meter/sec      RA   =          317
61684  deg
 ZDOT =       3076
760299                 TA   =          244
69155
                                          MA   =          244
71728
                                          Ha   =            188
511  n
mi
                                          Hp   =            184
864

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         353669
13                 X    =          185387
67
 Y    =      -16330361
98  feet           Y    =        -4975854
32  meter
 Z    =      -14816340
70                 Z    =        -4515309
29
 XDOT =      21468
483911                 XDOT =        6557
765375
 YDOT =      -8685
884271  feet/sec       YDOT =       -2574
204567  meter/sec
 ZDOT =      10094
357935                 ZDOT =        3108
583358

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16282159
72                 X    =        -4962802
28
 Y    =        1329108
85  feet           Y    =          405112
38  meter
 Z    =      -14813996
78                 Z    =        -4515306
22
 XDOT =     -10851
734236                 XDOT =       -3307
608595
 YDOT =     -19159
250028  feet/sec       YDOT =       -5839
739409  meter/sec
 ZDOT =      10216
690036                 ZDOT =        3114
047123


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
51039074  
00020000  00000-0  20000-3 0  9016
2 25544  51
6387 318
1438 0008786 303
6382  56
3943 15
74805365 30315


Satellite: ISS
Catalog Number: 25544
Epoch time:      08180
51039074   =   yrday
fracday
Element set:     901
Inclination:       51
6387  deg
RA of node:       318
1438  deg
Eccentricity:     
0008786     
Arg of perigee:   303
6382  deg
Mean anomaly:      56
3943  deg
Mean motion:   15
74805365  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3031
Checksum:              293


Coasting Arc #3 (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    =       -5498025
11                 A    =         6725966
72  meter
 Y    =        2528636
44  meter          E    =           
0004660
 Z    =       -2937770
49                 I    =           51
40509
 XDOT =        -27
018058                 Wp   =          323
60283
 YDOT =      -5862
360262  meter/sec      RA   =          312
50496  deg
 ZDOT =      -4987
626913                 TA   =          250
36715
                                          MA   =          250
41745
                                          Ha   =            188
694  n
mi
                                          Hp   =            184
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18038140
12                 X    =        -5511620
82
 Y    =        8296051
31  feet           Y    =         2467078
92  meter
 Z    =       -9638354
61                 Z    =        -2964512
67
 XDOT =        -88
641923                 XDOT =          62
766986
 YDOT =     -19233
465427  feet/sec       YDOT =       -5862
159430  meter/sec
 ZDOT =     -16363
605359                 ZDOT =       -4987
541195

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10481287
10                 X    =         3194696
31
 Y    =       16803266
05  feet           Y    =         5121635
49  meter
 Z    =       -9741135
29                 Z    =        -2969098
04
 XDOT =     -17857
618972                 XDOT =       -5443
002263
 YDOT =       1638
061960  feet/sec       YDOT =         499
281285  meter/sec
 ZDOT =     -16363
738536                 ZDOT =       -4987
667506


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
52569184  
00020000  00000-0  20000-3 0  9029
2 25544  51
6388 312
9225 0008821 307
8582  52
1783 15
74835534 30474


Satellite: ISS
Catalog Number: 25544
Epoch time:      08181
52569184   =   yrday
fracday
Element set:     902
Inclination:       51
6388  deg
RA of node:       312
9225  deg
Eccentricity:     
0008821     
Arg of perigee:   307
8582  deg
Mean anomaly:      52
1783  deg
Mean motion:   15
74835534  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3047
Checksum:              305


Coasting Arc #4 (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    =         179194
45                 A    =         6722235
87  meter
 Y    =        5268690
13  meter          E    =           
0009235
 Z    =        4173798
67                 I    =           51
37400
 XDOT =      -6027
419106                 Wp   =           21
09403
 YDOT =       3103
298369  meter/sec      RA   =          307
29568  deg
 ZDOT =      -3647
598872                 TA   =          106
29296
                                          MA   =          106
19136
                                          Ha   =            188
883  n
mi
                                          Hp   =            184
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         587908
29                 X    =           99990
14
 Y    =       17285728
76  feet           Y    =         5270250
21  meter
 Z    =       13693565
18                 Z    =         4174477
96
 XDOT =     -19774
997068                 XDOT =       -6043
953238
 YDOT =      10181
425094  feet/sec       YDOT =        3035
804667  meter/sec
 ZDOT =     -11967
187901                 ZDOT =       -3676
919724

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17037672
21                 X    =         5193082
49
 Y    =       -2962559
45  feet           Y    =         -902988
12  meter
 Z    =       13696596
26                 Z    =         4174722
54
 XDOT =      12664
020423                 XDOT =        3859
993425
 YDOT =      16816
017751  feet/sec       YDOT =        5125
522211  meter/sec
 ZDOT =     -12079
860799                 ZDOT =       -3681
941571


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
54097893  
00020000  00000-0  20000-3 0  9036
2 25544  51
6393 307
7018 0008754 312
0258  48
0160 15
74831116 30638


Satellite: ISS
Catalog Number: 25544
Epoch time:      08182
54097893   =   yrday
fracday
Element set:     903
Inclination:       51
6393  deg
RA of node:       307
7018  deg
Eccentricity:     
0008754     
Arg of perigee:   312
0258  deg
Mean anomaly:      48
0160  deg
Mean motion:   15
74831116  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3063
Checksum:              286


Coasting Arc #5 (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    =        5028214
67                 A    =         6724383
34  meter
 Y    =       -2852506
80  meter          E    =           
0008653
 Z    =        3423393
29                 I    =           51
36653
 XDOT =        408
476666                 Wp   =           45
30007
 YDOT =       6196
623807  meter/sec      RA   =          302
18507  deg
 ZDOT =       4562
264197                 TA   =          355
41449
                                          MA   =          355
42241
                                          Ha   =            188
835  n
mi
                                          Hp   =            183
995

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16496767
29                 X    =         5043107
93
 Y    =       -9358618
10  feet           Y    =        -2796195
96  meter
 Z    =       11231605
29                 Z    =         3447855
85
 XDOT =       1340
146542                 XDOT =         316
992044
 YDOT =      20330
130601  feet/sec       YDOT =        6200
679029  meter/sec
 ZDOT =      14968
058388                 ZDOT =        4564
027828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11855245
55                 X    =        -3613478
84
 Y    =      -14732958
07  feet           Y    =        -4490605
62  meter
 Z    =       11325595
82                 Z    =         3452041
61
 XDOT =      18796
835292                 XDOT =        5729
275397
 YDOT =      -3610
811435  feet/sec       YDOT =       -1100
575325  meter/sec
 ZDOT =      14975
339793                 ZDOT =        4564
483569


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
55624785  
00020000  00000-0  20000-3 0  9045
2 25544  51
6404 302
4808 0008890 315
7837  44
2615 15
74915840 30791


Satellite: ISS
Catalog Number: 25544
Epoch time:      08183
55624785   =   yrday
fracday
Element set:     904
Inclination:       51
6404  deg
RA of node:       302
4808  deg
Eccentricity:     
0008890     
Arg of perigee:   315
7837  deg
Mean anomaly:      44
2615  deg
Mean motion:   15
74915840  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3079
Checksum:              308


Coasting Arc #6 (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    =        -564682
52                 A    =         6723449
54  meter
 Y    =       -5536076
33  meter          E    =           
0005489
 Z    =       -3768793
44                 I    =           51
34854
 XDOT =       5492
913049                 Wp   =             
93730
 YDOT =      -3407
942396  meter/sec      RA   =          296
97148  deg
 ZDOT =       4188
500891                 TA   =          313
17034
                                          MA   =          313
21621
                                          Ha   =            189
192  n
mi
                                          Hp   =            183
753

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1852632
94                 X    =         -484427
31
 Y    =      -18162980
07  feet           Y    =        -5541941
30  meter
 Z    =      -12364807
87                 Z    =        -3771343
03
 XDOT =      18021
368270                 XDOT =        5510
266147
 YDOT =     -11180
913372  feet/sec       YDOT =       -3346
421469  meter/sec
 ZDOT =      13741
800825                 ZDOT =        4215
226588

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17565090
80                 X    =        -5353839
67
 Y    =        4953768
15  feet           Y    =         1509908
53  meter
 Z    =      -12375069
05                 Z    =        -3771921
05
 XDOT =     -13805
509582                 XDOT =       -4207
919321
 YDOT =     -14411
602885  feet/sec       YDOT =       -4392
656559  meter/sec
 ZDOT =      13844
471489                 ZDOT =        4219
794910


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
50805239  
00020000  00000-0  20000-3 0  9057
2 25544  51
6404 297
5874 0009090 320
0420  40
0074 15
74887832 30947


Satellite: ISS
Catalog Number: 25544
Epoch time:      08184
50805239   =   yrday
fracday
Element set:     905
Inclination:       51
6404  deg
RA of node:       297
5874  deg
Eccentricity:     
0009090     
Arg of perigee:   320
0420  deg
Mean anomaly:      40
0074  deg
Mean motion:   15
74887832  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3094
Checksum:              286


Coasting Arc #7 (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    =       -4570978
58                 A    =         6722920
37  meter
 Y    =        3045905
37  meter          E    =           
0009296
 Z    =       -3884550
84                 I    =           51
33524
 XDOT =       -881
616533                 Wp   =            6
73982
 YDOT =      -6487
970448  meter/sec      RA   =          291
86007  deg
 ZDOT =      -4041
736801                 TA   =          220
94785
                                          MA   =          221
01770
                                          Ha   =            189
327  n
mi
                                          Hp   =            183
376

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14996648
87                 X    =        -4585828
49
 Y    =        9993127
87  feet           Y    =         2994707
91  meter
 Z    =      -12744589
38                 Z    =        -3906791
72
 XDOT =      -2892
442694                 XDOT =        -789
367769
 YDOT =     -21285
992282  feet/sec       YDOT =       -6497
312497  meter/sec
 ZDOT =     -13260
291341                 ZDOT =       -4045
797010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12686286
62                 X    =         3866780
16
 Y    =       12713590
87  feet           Y    =         3875102
50  meter
 Z    =      -12830018
69                 Z    =        -3910589
70
 XDOT =     -19414
690408                 XDOT =       -5917
597636
 YDOT =       5948
234036  feet/sec       YDOT =        1813
021734  meter/sec
 ZDOT =     -13276
456581                 ZDOT =       -4046
663966


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
52329511  
00020000  00000-0  20000-3 0  9065
2 25544  51
6407 292
3668 0009011 324
0077  36
0479 15
74918072 31103


Satellite: ISS
Catalog Number: 25544
Epoch time:      08185
52329511   =   yrday
fracday
Element set:     906
Inclination:       51
6407  deg
RA of node:       292
3668  deg
Eccentricity:     
0009011     
Arg of perigee:   324
0077  deg
Mean anomaly:      36
0479  deg
Mean motion:   15
74918072  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3110
Checksum:              280


Coasting Arc #8 (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    =        1000152
45                 A    =         6724858
62  meter
 Y    =        5790928
36  meter          E    =           
0010903
 Z    =        3270230
49                 I    =           51
33175
 XDOT =      -4977
689579                 Wp   =           48
02271
 YDOT =       3522
832705  meter/sec      RA   =          286
64469  deg
 ZDOT =      -4698
650784                 TA   =           93
45726
                                          MA   =           93
33254
                                          Ha   =            189
512  n
mi
                                          Hp   =            183
161

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3281340
06                 X    =          919437
16
 Y    =       18999108
79  feet           Y    =         5801660
69  meter
 Z    =       10729102
65                 Z    =         3274894
22
 XDOT =     -16331
002557                 XDOT =       -4993
887748
 YDOT =      11557
850083  feet/sec       YDOT =        3467
079681  meter/sec
 ZDOT =     -15415
520944                 ZDOT =       -4722
870594

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17899927
29                 X    =         5455897
84
 Y    =       -7136511
21  feet           Y    =        -2175208
62  meter
 Z    =       10747547
72                 Z    =         3275852
54
 XDOT =      14189
439929                 XDOT =        4324
941290
 YDOT =      12149
442834  feet/sec       YDOT =        3703
150176  meter/sec
 ZDOT =     -15508
536546                 ZDOT =       -4727
001939


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
53852360  
00020000  00000-0  20000-3 0  9071
2 25544  51
6403 287
1465 0008993 328
9915  31
0716 15
74933487 31261


Satellite: ISS
Catalog Number: 25544
Epoch time:      08186
53852360   =   yrday
fracday
Element set:     907
Inclination:       51
6403  deg
RA of node:       287
1465  deg
Eccentricity:     
0008993     
Arg of perigee:   328
9915  deg
Mean anomaly:      31
0716  deg
Mean motion:   15
74933487  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3126
Checksum:              314


Coasting Arc #9 (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    =        4142623
83                 A    =         6721179
82  meter
 Y    =       -3073362
68  meter          E    =           
0006943
 Z    =        4301827
10                 I    =           51
31298
 XDOT =       1434
734340                 Wp   =           44
59866
 YDOT =       6745
424164  meter/sec      RA   =          281
52859  deg
 ZDOT =       3439
036054                 TA   =           10
53857
                                          MA   =           10
52402
                                          Ha   =            189
477  n
mi
                                          Hp   =            182
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13591285
54                 X    =         4155785
70
 Y    =      -10083210
89  feet           Y    =        -3026964
61  meter
 Z    =       14113605
96                 Z    =         4321983
02
 XDOT =       4707
133663                 XDOT =        1342
493429
 YDOT =      22130
656707  feet/sec       YDOT =        6760
951871  meter/sec
 ZDOT =      11282
926686                 ZDOT =        3445
782923

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12883465
74                 X    =        -3926880
36
 Y    =      -10872894
68  feet           Y    =        -3314058
30  meter
 Z    =       14191001
72                 Z    =         4325417
32
 XDOT =      19709
166856                 XDOT =        6007
354058
 YDOT =      -8599
373695  feet/sec       YDOT =       -2621
089102  meter/sec
 ZDOT =      11309
489973                 ZDOT =        3447
132544


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
55373516  
00020000  00000-0  20000-3 0  9086
2 25544  51
6404 281
9249 0009122 332
6327  27
4355 15
74998683 31423


Satellite: ISS
Catalog Number: 25544
Epoch time:      08187
55373516   =   yrday
fracday
Element set:     908
Inclination:       51
6404  deg
RA of node:       281
9249  deg
Eccentricity:     
0009122     
Arg of perigee:   332
6327  deg
Mean anomaly:      27
4355  deg
Mean motion:   15
74998683  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3142
Checksum:              311


Coasting Arc #10 (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    =       -1528743
48                 A    =         6726181
85  meter
 Y    =       -5953187
28  meter          E    =           
0011161
 Z    =       -2716440
72                 I    =           51
32450
 XDOT =       4534
350838                 Wp   =            1
51244
 YDOT =      -3508
286978  meter/sec      RA   =          276
31587  deg
 ZDOT =       5148
214018                 TA   =          327
30317
                                          MA   =          327
37221
                                          Ha   =            189
796  n
mi
                                          Hp   =            182
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5015562
61                 X    =        -1448864
64
 Y    =      -19531454
32  feet           Y    =        -5969835
56  meter
 Z    =       -8912207
07                 Z    =        -2723674
02
 XDOT =      14876
479127                 XDOT =        4548
235421
 YDOT =     -11510
127879  feet/sec       YDOT =       -3457
504349  meter/sec
 ZDOT =      16890
465939                 ZDOT =        5170
274736

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17735512
13                 X    =        -5405784
10
 Y    =        9569664
67  feet           Y    =         2916833
79  meter
 Z    =       -8940589
39                 Z    =        -2725091
65
 XDOT =     -14063
721923                 XDOT =       -4286
622442
 YDOT =     -10240
178379  feet/sec       YDOT =       -3121
206370  meter/sec
 ZDOT =      16975
160870                 ZDOT =        5174
029033


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
50548548  
00020000  00000-0  20000-3 0  9092
2 25544  51
6400 277
0311 0009360 336
3284  23
7448 15
74968562 31573


Satellite: ISS
Catalog Number: 25544
Epoch time:      08188
50548548   =   yrday
fracday
Element set:     909
Inclination:       51
6400  deg
RA of node:       277
0311  deg
Eccentricity:     
0009360     
Arg of perigee:   336
3284  deg
Mean anomaly:      23
7448  deg
Mean motion:   15
74968562  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3157
Checksum:              307


Coasting Arc #11 (Orbit 3172)
---------------------------------------

Vector Time (GMT): 2008/189/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3802067
45                 A    =         6719789
64  meter
 Y    =        3005398
65  meter          E    =           
0014368
 Z    =       -4666619
90                 I    =           51
30034
 XDOT =      -2058
368767                 Wp   =           30
59003
 YDOT =      -6883
762873  meter/sec      RA   =          271
19390  deg
 ZDOT =      -2747
770433                 TA   =          212
12733
                                          MA   =          212
21497
                                          Ha   =            189
918  n
mi
                                          Hp   =            182
278

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12473974
58                 X    =        -3812722
46
 Y    =        9860231
80  feet           Y    =         2962822
74  meter
 Z    =      -15310432
73                 Z    =        -4685115
59
 XDOT =      -6753
178370                 XDOT =       -1967
892481
 YDOT =     -22584
523862  feet/sec       YDOT =       -6906
274523  meter/sec
 ZDOT =      -9014
994859                 ZDOT =       -2757
550912

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12742184
30                 X    =         3883817
77
 Y    =        9395840
72  feet           Y    =         2863852
25  meter
 Z    =      -15381432
96                 Z    =        -4688260
77
 XDOT =     -19379
393929                 XDOT =       -5906
839270
 YDOT =      11415
386596  feet/sec       YDOT =        3479
409835  meter/sec
 ZDOT =      -9053
282767                 ZDOT =       -2759
440587


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   08189
52067132  
00020000  00000-0  20000-3 0  9102
2 25544  51
6390 271
8100 0009275 340
3408  19
7397 15
74999291 31736


Satellite: ISS
Catalog Number: 25544
Epoch time:      08189
52067132   =   yrday
fracday
Element set:     910
Inclination:       51
6390  deg
RA of node:       271
8100  deg
Eccentricity:     
0009275     
Arg of perigee:   340
3408  deg
Mean anomaly:      19
7397  deg
Mean motion:   15
74999291  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3173
Checksum:              300


Coasting Arc #12 (Orbit 3188)
---------------------------------------

Vector Time (GMT): 2008/190/12:00:00
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2080644
69                 A    =         6727334
78  meter
 Y    =        6055157
77  meter          E    =           
0011568
 Z    =        2063707
34                 I    =           51
32664
 XDOT =      -4197
993080                 Wp   =           69
05522
 YDOT =       3334
955610  meter/sec      RA   =          265
98681  deg
 ZDOT =      -5523
697051                 TA   =           87
80706
                                          MA   =           87
67461
                                          Ha   =            190
082  n
mi
                                          Hp   =            182
006

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6826262
10                 X    =         2002755
30
 Y    =       19866003
17  feet           Y    =         6077988
99  meter
 Z    =        6770693
37                 Z    =         2073626
50
 XDOT =     -13772
943176                 XDOT =       -4208
140239
 YDOT =      10941
455412  feet/sec       YDOT =        3287
955129  meter/sec
 ZDOT =     -18122
365653                 ZDOT =       -5544
114964

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17213039
19                 X    =         5246534
34
 Y    =      -12018356
23  feet           Y    =        -3663194
98  meter
 Z    =        6809450
81                 Z    =         2075520
61
 XDOT =      13419
442809                 XDOT =        4090
246168
 YDOT =       8853
794455  feet/sec       YDOT =        2698
636550  meter/sec
 ZDOT =     -18200
741277                 ZDOT =       -5547
585941


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   08190
53584295  
00020000  00000-0  20000-3 0  9110
2 25544  51
6388 266
5884 0009399 345
3707  14
7183 15
75044616 31895


Satellite: ISS
Catalog Number: 25544
Epoch time:      08190
53584295   =   yrday
fracday
Element set:     911
Inclination:       51
6388  deg
RA of node:       266
5884  deg
Eccentricity:     
0009399     
Arg of perigee:   345
3707  deg
Mean anomaly:      14
7183  deg
Mean motion:   15
75044616  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3189
Checksum:              327

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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