Date: February 11th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12852 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 806)
---------------------------------------

Vector Time (GMT): 2008/039/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -885763
36                 A    =         6709267
84  meter
 Y    =       -4330490
13  meter          E    =           
0015329
 Z    =       -5059789
46                 I    =           51
43344
 XDOT =       6775
380586                 Wp   =           80
39121
 YDOT =      -3272
709208  meter/sec      RA   =          324
32364  deg
 ZDOT =       1621
579994                 TA   =          205
20245
                                          MA   =          205
27732
                                          Ha   =            185
109  n
mi
                                          Hp   =            176
493

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2906047
75                 X    =         -812694
48
 Y    =      -14207644
77  feet           Y    =        -4339986
79  meter
 Z    =      -16600359
13                 Z    =        -5063914
81
 XDOT =      22228
938932                 XDOT =        6803
595852
 YDOT =     -10737
234933  feet/sec       YDOT =       -3196
785250  meter/sec
 ZDOT =       5320
144337                 ZDOT =        1654
562443

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5200643
22                 X    =         1585156
05
 Y    =      -13517276
46  feet           Y    =        -4120065
87  meter
 Z    =      -16616580
70                 Z    =        -5064733
80
 XDOT =      23518
224403                 XDOT =        7168
354798
 YDOT =       2380
667415  feet/sec       YDOT =         725
627428  meter/sec
 ZDOT =       5445
982011                 ZDOT =        1659
935317


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   08039
54220430  
00020000  00000-0  20000-3 0  9009
2 25544  51
6407 324
8051 0005721  18
4029 341
7342 15
78127916  8073


Satellite: ISS
Catalog Number: 25544
Epoch time:      08039
54220430   =   yrday
fracday
Element set:     900
Inclination:       51
6407  deg
RA of node:       324
8051  deg
Eccentricity:     
0005721     
Arg of perigee:    18
4029  deg
Mean anomaly:     341
7342  deg
Mean motion:   15
78127916  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             807
Checksum:              264


Coasting Arc #2 (Orbit 822)
---------------------------------------

Vector Time (GMT): 2008/040/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5770132
27                 A    =         6717033
84  meter
 Y    =        2135086
03  meter          E    =           
0006715
 Z    =       -2704656
72                 I    =           51
43760
 XDOT =        306
166255                 Wp   =           65
96830
 YDOT =      -5703
334923  meter/sec      RA   =          319
17892  deg
 ZDOT =      -5162
824682                 TA   =          145
00704
                                          MA   =          144
96290
                                          Ha   =            185
081  n
mi
                                          Hp   =            176
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18930880
14                 X    =        -5780439
86
 Y    =        7004875
42  feet           Y    =         2070503
39  meter
 Z    =       -8873545
66                 Z    =        -2732712
46
 XDOT =       1004
482465                 XDOT =         394
998535
 YDOT =     -18711
728749  feet/sec       YDOT =       -5699
414705  meter/sec
 ZDOT =     -16938
401188                 ZDOT =       -5161
121379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19774721
52                 X    =        -6027335
12
 Y    =       -3807186
94  feet           Y    =        -1160430
58  meter
 Z    =       -8980647
60                 Z    =        -2737301
39
 XDOT =      10371
181008                 XDOT =        3161
135971
 YDOT =     -13983
357961  feet/sec       YDOT =       -4262
127506  meter/sec
 ZDOT =     -16932
472547                 ZDOT =       -5161
017632


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   08040
55535989  
00020000  00000-0  20000-3 0  9011
2 25544  51
6409 319
5700 0005643  21
7976 338
3429 15
78180126  8236


Satellite: ISS
Catalog Number: 25544
Epoch time:      08040
55535989   =   yrday
fracday
Element set:     901
Inclination:       51
6409  deg
RA of node:       319
5700  deg
Eccentricity:     
0005643     
Arg of perigee:    21
7976  deg
Mean anomaly:     338
3429  deg
Mean motion:   15
78180126  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             823
Checksum:              299


Coasting Arc #3 (Orbit 838)
---------------------------------------

Vector Time (GMT): 2008/041/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1301811
61                 A    =         6714489
12  meter
 Y    =        5504070
66  meter          E    =           
0015677
 Z    =        3611693
02                 I    =           51
40716
 XDOT =      -6196
835067                 Wp   =           67
34863
 YDOT =       1411
240670  meter/sec      RA   =          313
94622  deg
 ZDOT =      -4363
310721                 TA   =           69
13315
                                          MA   =           68
96536
                                          Ha   =            185
109  n
mi
                                          Hp   =            176
172

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4271035
45                 X    =        -1380806
85
 Y    =       18057974
61  feet           Y    =         5489071
53  meter
 Z    =       11849386
55                 Z    =         3605176
82
 XDOT =     -20330
823709                 XDOT =       -6190
959434
 YDOT =       4630
054691  feet/sec       YDOT =        1341
976793  meter/sec
 ZDOT =     -14315
323888                 ZDOT =       -4393
400174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12848686
30                 X    =        -3916279
58
 Y    =       13409699
18  feet           Y    =         4087276
31  meter
 Z    =       11825031
96                 Z    =         3604269
74
 XDOT =     -18844
884917                 XDOT =       -5743
920923
 YDOT =      -5270
682796  feet/sec       YDOT =       -1606
504116  meter/sec
 ZDOT =     -14430
275688                 ZDOT =       -4398
348030


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   08041
56848114  
00020000  00000-0  20000-3 0  9021
2 25544  51
6401 314
3346 0005658  26
2005 333
9446 15
78230766  8399


Satellite: ISS
Catalog Number: 25544
Epoch time:      08041
56848114   =   yrday
fracday
Element set:     902
Inclination:       51
6401  deg
RA of node:       314
3346  deg
Eccentricity:     
0005658     
Arg of perigee:    26
2005  deg
Mean anomaly:     333
9446  deg
Mean motion:   15
78230766  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             839
Checksum:              282


Coasting Arc #4 (Orbit 854)
---------------------------------------

Vector Time (GMT): 2008/042/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4854276
05                 A    =         6710526
47  meter
 Y    =        -143281
56  meter          E    =           
0009966
 Z    =        4621969
26                 I    =           51
37554
 XDOT =      -2502
986460                 Wp   =           82
44310
 YDOT =       6724
398664  meter/sec      RA   =          308
80798  deg
 ZDOT =       2833
344544                 TA   =          339
49467
                                          MA   =          339
53465
                                          Ha   =            184
919  n
mi
                                          Hp   =            175
999

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15926102
53                 X    =         4833065
08
 Y    =        -470083
84  feet           Y    =          -89116
71  meter
 Z    =       15163941
14                 Z    =         4645499
50
 XDOT =      -8211
897835                 XDOT =       -2591
757387
 YDOT =      22061
675407  feet/sec       YDOT =        6695
912600  meter/sec
 ZDOT =       9295
749817                 ZDOT =        2820
969342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14045870
08                 X    =         4281181
20
 Y    =        7337432
12  feet           Y    =         2236449
31  meter
 Z    =       15253932
44                 Z    =         4649398
61
 XDOT =     -17463
953249                 XDOT =       -5323
012950
 YDOT =      14176
199218  feet/sec       YDOT =        4320
905522  meter/sec
 ZDOT =       9249
113858                 ZDOT =        2819
129904


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   08042
58156662  
00020000  00000-0  20000-3 0  9035
2 25544  51
6404 309
0985 0005620  29
4150 330
7331 15
78289290  8559


Satellite: ISS
Catalog Number: 25544
Epoch time:      08042
58156662   =   yrday
fracday
Element set:     903
Inclination:       51
6404  deg
RA of node:       309
0985  deg
Eccentricity:     
0005620     
Arg of perigee:    29
4150  deg
Mean anomaly:     330
7331  deg
Mean motion:   15
78289290  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             855
Checksum:              286


Coasting Arc #5 (Orbit 869)
---------------------------------------

Vector Time (GMT): 2008/043/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2880316
87                 A    =         6719273
39  meter
 Y    =       -5958169
73  meter          E    =           
0015088
 Z    =       -1122857
87                 I    =           51
38848
 XDOT =       4824
463067                 Wp   =           35
30668
 YDOT =       1232
630468  meter/sec      RA   =          303
58787  deg
 ZDOT =       5886
253831                 TA   =          312
33183
                                          MA   =          312
45954
                                          Ha   =            184
961  n
mi
                                          Hp   =            175
842

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9449858
50                 X    =         2952182
56
 Y    =      -19547800
95  feet           Y    =        -5925558
58  meter
 Z    =       -3683916
90                 Z    =        -1108690
78
 XDOT =      15828
290901                 XDOT =        4781
726968
 YDOT =       4044
063216  feet/sec       YDOT =        1286
341503  meter/sec
 ZDOT =      19311
856400                 ZDOT =        5909
587012

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17605236
44                 X    =         5366076
07
 Y    =      -12722571
12  feet           Y    =        -3877839
68  meter
 Z    =       -3630347
84                 Z    =        -1106530
02
 XDOT =      10995
582783                 XDOT =        3351
453632
 YDOT =       9728
167489  feet/sec       YDOT =        2965
145451  meter/sec
 ZDOT =      19401
237205                 ZDOT =        5913
497100


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   08043
53130272  
00020000  00000-0  20000-3 0  9041
2 25544  51
6406 304
1895 0005552  31
6956 328
4543 15
78355025  8706


Satellite: ISS
Catalog Number: 25544
Epoch time:      08043
53130272   =   yrday
fracday
Element set:     904
Inclination:       51
6406  deg
RA of node:       304
1895  deg
Eccentricity:     
0005552     
Arg of perigee:    31
6956  deg
Mean anomaly:     328
4543  deg
Mean motion:   15
78355025  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             870
Checksum:              279


Coasting Arc #6 (Orbit 885)
---------------------------------------

Vector Time (GMT): 2008/044/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3477250
45                 A    =         6707609
99  meter
 Y    =       -2376946
52  meter          E    =           
0018487
 Z    =       -5235577
05                 I    =           51
33435
 XDOT =       3929
647622                 Wp   =           78
17409
 YDOT =      -6604
318051  meter/sec      RA   =          298
40589  deg
 ZDOT =        393
350130                 TA   =          195
55115
                                          MA   =          195
60802
                                          Ha   =            184
895  n
mi
                                          Hp   =            175
569

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11408302
01                 X    =        -3424979
39
 Y    =       -7798380
97  feet           Y    =        -2415538
79  meter
 Z    =      -17177090
04                 Z    =        -5252342
43
 XDOT =      12892
544691                 XDOT =        4001
295258
 YDOT =     -21667
710140  feet/sec       YDOT =       -6559
973895  meter/sec
 ZDOT =       1290
518799                 ZDOT =         412
614135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6471943
43                 X    =        -1972648
36
 Y    =      -12118672
18  feet           Y    =        -3693771
28  meter
 Z    =      -17241469
08                 Z    =        -5255199
77
 XDOT =      20506
573409                 XDOT =        6250
403575
 YDOT =     -12868
579758  feet/sec       YDOT =       -3922
343110  meter/sec
 ZDOT =       1363
518332                 ZDOT =         415
600388


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   08044
54432111  
00020000  00000-0  20000-3 0  9051
2 25544  51
6404 298
9528 0005533  34
4665 325
6858 15
78413368  8864


Satellite: ISS
Catalog Number: 25544
Epoch time:      08044
54432111   =   yrday
fracday
Element set:     905
Inclination:       51
6404  deg
RA of node:       298
9528  deg
Eccentricity:     
0005533     
Arg of perigee:    34
4665  deg
Mean anomaly:     325
6858  deg
Mean motion:   15
78413368  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             886
Checksum:              307


Coasting Arc #7 (Orbit 901)
---------------------------------------

Vector Time (GMT): 2008/045/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3813850
75                 A    =         6718172
44  meter
 Y    =        5229702
95  meter          E    =           
0007952
 Z    =       -1802712
22                 I    =           51
35737
 XDOT =      -3110
100975                 Wp   =          101
08493
 YDOT =      -4208
283746  meter/sec      RA   =          293
23598  deg
 ZDOT =      -5651
073493                 TA   =           99
00594
                                          MA   =           98
91593
                                          Ha   =            184
874  n
mi
                                          Hp   =            175
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12512633
70                 X    =        -3863289
49
 Y    =       17157818
07  feet           Y    =         5186777
94  meter
 Z    =       -5914410
18                 Z    =        -1821359
59
 XDOT =     -10203
743357                 XDOT =       -3035
360574
 YDOT =     -13806
705205  feet/sec       YDOT =       -4242
644564  meter/sec
 ZDOT =     -18540
267364                 ZDOT =       -5666
000801

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18793666
02                 X    =        -5728309
40
 Y    =        9844414
74  feet           Y    =         3000577
61  meter
 Z    =       -5985197
30                 Z    =        -1824288
14
 XDOT =      -2210
537173                 XDOT =        -673
771730
 YDOT =     -15482
702356  feet/sec       YDOT =       -4719
127678  meter/sec
 ZDOT =     -18597
809464                 ZDOT =       -5668
612325


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   08045
55730602  
00020000  00000-0  20000-3 0  9060
2 25544  51
6403 293
7163 0005323  38
0166 322
1374 15
78419045  9026


Satellite: ISS
Catalog Number: 25544
Epoch time:      08045
55730602   =   yrday
fracday
Element set:     906
Inclination:       51
6403  deg
RA of node:       293
7163  deg
Eccentricity:     
0005323     
Arg of perigee:    38
0166  deg
Mean anomaly:     322
1374  deg
Mean motion:   15
78419045  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             902
Checksum:              268


Coasting Arc #8 (Orbit 917)
---------------------------------------

Vector Time (GMT): 2008/046/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1970418
08                 A    =         6711469
81  meter
 Y    =        4836531
42  meter          E    =           
0014942
 Z    =        4208654
64                 I    =           51
32554
 XDOT =      -4639
188412                 Wp   =           61
24581
 YDOT =       5015
877502  meter/sec      RA   =          288
00201  deg
 ZDOT =      -3575
526602                 TA   =           65
26664
                                          MA   =           65
11120
                                          Ha   =            184
727  n
mi
                                          Hp   =            175
373

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6464626
23                 X    =         1895744
24
 Y    =       15867885
23  feet           Y    =         4858148
01  meter
 Z    =       13807922
06                 Z    =         4218045
66
 XDOT =     -15220
434421                 XDOT =       -4677
562954
 YDOT =      16456
291018  feet/sec       YDOT =        4963
785083  meter/sec
 ZDOT =     -11730
730320                 ZDOT =       -3598
156357

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1019366
47                 X    =         -310702
90
 Y    =       17074384
08  feet           Y    =         5204272
27  meter
 Z    =       13844355
75                 Z    =         4219759
63
 XDOT =     -19493
666354                 XDOT =       -5941
669505
 YDOT =       8461
774926  feet/sec       YDOT =        2579
148997  meter/sec
 ZDOT =     -11816
777917                 ZDOT =       -3601
753909


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   08046
57025435  
00020000  00000-0  20000-3 0  9075
2 25544  51
6403 288
4792 0005495  39
5556 320
6010 15
78549462  9188


Satellite: ISS
Catalog Number: 25544
Epoch time:      08046
57025435   =   yrday
fracday
Element set:     907
Inclination:       51
6403  deg
RA of node:       288
4792  deg
Eccentricity:     
0005495     
Arg of perigee:    39
5556  deg
Mean anomaly:     320
6010  deg
Mean motion:   15
78549462  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             918
Checksum:              305


Coasting Arc #9 (Orbit 933)
---------------------------------------

Vector Time (GMT): 2008/047/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4158060
69                 A    =         6711596
11  meter
 Y    =       -3198458
88  meter          E    =           
0013601
 Z    =        4174003
67                 I    =           51
31724
 XDOT =       1462
648517                 Wp   =           85
15792
 YDOT =       6649
467889  meter/sec      RA   =          282
85912  deg
 ZDOT =       3629
313434                 TA   =          327
74413
                                          MA   =          327
82724
                                          Ha   =            184
754  n
mi
                                          Hp   =            175
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13641931
39                 X    =         4173241
21
 Y    =      -10493631
51  feet           Y    =        -3151876
43  meter
 Z    =       13694237
77                 Z    =         4194239
78
 XDOT =       4798
715608                 XDOT =        1370
554278
 YDOT =      21815
839532  feet/sec       YDOT =        6665
308932  meter/sec
 ZDOT =      11907
196306                 ZDOT =        3636
195499

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16684400
89                 X    =         5085405
39
 Y    =       -3966382
36  feet           Y    =        -1208953
34  meter
 Z    =       13771322
40                 Z    =         4197499
07
 XDOT =      -4975
367325                 XDOT =       -1516
491961
 YDOT =      20608
893579  feet/sec       YDOT =        6281
590763  meter/sec
 ZDOT =      11934
229370                 ZDOT =        3637
553112


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   08047
58317213  
00020000  00000-0  20000-3 0  9086
2 25544  51
6395 283
2418 0005529  43
9926 316
1679 15
78530773  9348


Satellite: ISS
Catalog Number: 25544
Epoch time:      08047
58317213   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:       283
2418  deg
Eccentricity:     
0005529     
Arg of perigee:    43
9926  deg
Mean anomaly:     316
1679  deg
Mean motion:   15
78530773  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             934
Checksum:              316


Coasting Arc #10 (Orbit 948)
---------------------------------------

Vector Time (GMT): 2008/048/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -614730
57                 A    =         6717659
40  meter
 Y    =       -6430818
05  meter          E    =           
0012632
 Z    =       -1827445
78                 I    =           51
33224
 XDOT =       4830
962358                 Wp   =           41
33785
 YDOT =      -2056
350793  meter/sec      RA   =          277
62299  deg
 ZDOT =       5642
750092                 TA   =          298
25898
                                          MA   =          298
38643
                                          Ha   =            184
702  n
mi
                                          Hp   =            175
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2016832
57                 X    =         -533897
32
 Y    =      -21098484
43  feet           Y    =        -6437240
28  meter
 Z    =       -5995557
03                 Z    =        -1830236
00
 XDOT =      15849
614034                 XDOT =        4826
187045
 YDOT =      -6746
557720  feet/sec       YDOT =       -2002
355163  meter/sec
 ZDOT =      18512
959621                 ZDOT =        5666
206570

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6548380
52                 X    =         1995946
38
 Y    =      -20154304
11  feet           Y    =        -6143031
89  meter
 Z    =       -6006921
12                 Z    =        -1830909
56
 XDOT =      15659
266537                 XDOT =        4772
944440
 YDOT =       -425
788906  feet/sec       YDOT =        -129
780459  meter/sec
 ZDOT =      18602
490803                 ZDOT =        5670
039197


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   08048
53274804  
00020000  00000-0  20000-3 0  9091
2 25544  51
6386 278
3317 0005356  45
6379 314
5224 15
78595110  9490


Satellite: ISS
Catalog Number: 25544
Epoch time:      08048
53274804   =   yrday
fracday
Element set:     909
Inclination:       51
6386  deg
RA of node:       278
3317  deg
Eccentricity:     
0005356     
Arg of perigee:    45
6379  deg
Mean anomaly:     314
5224  deg
Mean motion:   15
78595110  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             949
Checksum:              313


Coasting Arc #11 (Orbit 964)
---------------------------------------

Vector Time (GMT): 2008/049/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4207935
56                 A    =         6706864
16  meter
 Y    =         210365
38  meter          E    =           
0019518
 Z    =       -5234945
99                 I    =           51
29248
 XDOT =         50
623778                 Wp   =           77
70854
 YDOT =      -7686
375290  meter/sec      RA   =          272
44794  deg
 ZDOT =       -346
557931                 TA   =          188
96513
                                          MA   =          189
00004
                                          Ha   =            184
637  n
mi
                                          Hp   =            174
882

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13805562
85                 X    =        -4184545
54
 Y    =         690175
13  feet           Y    =          163440
73  meter
 Z    =      -17175019
64                 Z    =        -5255330
67
 XDOT =        166
088510                 XDOT =         138
253712
 YDOT =     -25217
766701  feet/sec       YDOT =       -7685
319216  meter/sec
 ZDOT =      -1137
001085                 ZDOT =        -346
099315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12938049
93                 X    =        -3943517
62
 Y    =       -4581707
77  feet           Y    =        -1396504
53  meter
 Z    =      -17253000
45                 Z    =        -5258714
54
 XDOT =       9428
189558                 XDOT =        2873
712177
 YDOT =     -22308
705178  feet/sec       YDOT =       -6799
693338  meter/sec
 ZDOT =      -1136
081501                 ZDOT =        -346
277641


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   08049
54559684  
00020000  00000-0  20000-3 0  9107
2 25544  51
6372 273
0934 0005320  49
8089 310
3542 15
78671552  9657


Satellite: ISS
Catalog Number: 25544
Epoch time:      08049
54559684   =   yrday
fracday
Element set:     910
Inclination:       51
6372  deg
RA of node:       273
0934  deg
Eccentricity:     
0005320     
Arg of perigee:    49
8089  deg
Mean anomaly:     310
3542  deg
Mean motion:   15
78671552  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             965
Checksum:              306


Coasting Arc #12 (Orbit 980)
---------------------------------------

Vector Time (GMT): 2008/050/12:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -702453
56                 A    =         6718132
65  meter
 Y    =        6558715
59  meter          E    =           
0010500
 Z    =       -1268134
75                 I    =           51
33050
 XDOT =      -4755
287569                 Wp   =          113
00960
 YDOT =      -1629
907078  meter/sec      RA   =          267
26283  deg
 ZDOT =      -5838
009836                 TA   =           80
98363
                                          MA   =           80
86482
                                          Ha   =            184
597  n
mi
                                          Hp   =            174
964

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2304637
66                 X    =         -769581
76
 Y    =       21518095
78  feet           Y    =         6550485
02  meter
 Z    =       -4160547
07                 Z    =        -1271710
26
 XDOT =     -15601
337169                 XDOT =       -4708
349217
 YDOT =      -5347
464167  feet/sec       YDOT =       -1682
821015  meter/sec
 ZDOT =     -19153
575576                 ZDOT =       -5860
996235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9974279
88                 X    =        -3040160
51
 Y    =       19202748
61  feet           Y    =         5852997
78  meter
 Z    =       -4173504
47                 Z    =        -1272084
16
 XDOT =     -11073
463592                 XDOT =       -3375
191703
 YDOT =      -9903
670550  feet/sec       YDOT =       -3018
638784  meter/sec
 ZDOT =     -19241
720551                 ZDOT =       -5864
876424


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   08050
55841160  
00020000  00000-0  20000-3 0  9114
2 25544  51
6367 267
8561 0005207  53
4678 306
6967 15
78697029  9811


Satellite: ISS
Catalog Number: 25544
Epoch time:      08050
55841160   =   yrday
fracday
Element set:     911
Inclination:       51
6367  deg
RA of node:       267
8561  deg
Eccentricity:     
0005207     
Arg of perigee:    53
4678  deg
Mean anomaly:     306
6967  deg
Mean motion:   15
78697029  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             981
Checksum:              317

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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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