Date: April 5th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16145 87 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 1688)
---------------------------------------

Vector Time (GMT): 2008/095/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1839877
42                 A    =         6717045
02  meter
 Y    =       -5150377
66  meter          E    =           
0006822
 Z    =       -3907252
28                 I    =           51
82805
 XDOT =       6485
219398                 Wp   =           62
71809
 YDOT =        773
126576  meter/sec      RA   =           36
17341  deg
 ZDOT =      -4075
259062                 TA   =          164
96472
                                          MA   =          164
94443
                                          Ha   =            185
438  n
mi
                                          Hp   =            179
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6036343
24                 X    =        -1763167
60
 Y    =      -16897564
51  feet           Y    =        -5170523
68  meter
 Z    =      -12819069
15                 Z    =        -3916003
61
 XDOT =      21276
966530                 XDOT =        6495
889079
 YDOT =       2536
504514  feet/sec       YDOT =         845
707292  meter/sec
 ZDOT =     -13370
272512                 ZDOT =       -4043
727986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -557640
17                 X    =         -169968
72
 Y    =      -17910291
05  feet           Y    =        -5459056
71  meter
 Z    =      -12853177
50                 Z    =        -3917648
50
 XDOT =      18271
417946                 XDOT =        5569
128190
 YDOT =       8933
819371  feet/sec       YDOT =        2723
028144  meter/sec
 ZDOT =     -13249
238015                 ZDOT =       -4038
367747


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   08095
43992638  
00020000  00000-0  20000-3 0  9005
2 25544  51
6387  36
5664 0001170 340
7826  19
3295 15
76971058 16893


Satellite: ISS
Catalog Number: 25544
Epoch time:      08095
43992638   =   yrday
fracday
Element set:     900
Inclination:       51
6387  deg
RA of node:        36
5664  deg
Eccentricity:     
0001170     
Arg of perigee:   340
7826  deg
Mean anomaly:      19
3295  deg
Mean motion:   15
76971058  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1689
Checksum:              320


Coasting Arc #2 (Orbit 1704)
---------------------------------------

Vector Time (GMT): 2008/096/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6030828
06                 A    =         6720354
85  meter
 Y    =       -1110653
01  meter          E    =           
0013033
 Z    =        2736239
49                 I    =           51
81548
 XDOT =      -1335
574451                 Wp   =           96
26922
 YDOT =      -5551
312577  meter/sec      RA   =           30
97925  deg
 ZDOT =      -5177
443183                 TA   =           52
50530
                                          MA   =           52
38687
                                          Ha   =            185
373  n
mi
                                          Hp   =            179
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19786181
30                 X    =        -6031252
60
 Y    =       -3643874
72  feet           Y    =        -1178095
31  meter
 Z    =        8977163
69                 Z    =         2706940
58
 XDOT =      -4381
805941                 XDOT =       -1248
248266
 YDOT =     -18212
967773  feet/sec       YDOT =       -5565
759932  meter/sec
 ZDOT =     -16986
362149                 ZDOT =       -5183
718840

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17957874
46                 X    =        -5473560
13
 Y    =       -9181109
32  feet           Y    =        -2798402
12  meter
 Z    =        8864662
32                 Z    =         2701949
07
 XDOT =        449
840807                 XDOT =         137
111478
 YDOT =     -17367
255588  feet/sec       YDOT =       -5293
539503  meter/sec
 ZDOT =     -17011
010231                 ZDOT =       -5184
955918


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   08096
45382081  
00020000  00000-0  20000-3 0  9014
2 25544  51
6389  31
3365 0001255 338
7871  21
3241 15
77041112 17050


Satellite: ISS
Catalog Number: 25544
Epoch time:      08096
45382081   =   yrday
fracday
Element set:     901
Inclination:       51
6389  deg
RA of node:        31
3365  deg
Eccentricity:     
0001255     
Arg of perigee:   338
7871  deg
Mean anomaly:      21
3241  deg
Mean motion:   15
77041112  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1705
Checksum:              266


Coasting Arc #3 (Orbit 1720)
---------------------------------------

Vector Time (GMT): 2008/097/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         370392
60                 A    =         6712554
38  meter
 Y    =        4514677
79  meter          E    =           
0004969
 Z    =        4950581
56                 I    =           51
76544
 XDOT =      -7229
253101                 Wp   =          116
79303
 YDOT =      -1687
805911  meter/sec      RA   =           25
87176  deg
 ZDOT =       2076
283337                 TA   =          313
13209
                                          MA   =          313
17364
                                          Ha   =            185
139  n
mi
                                          Hp   =            179
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1215198
81                 X    =          295831
88
 Y    =       14811935
02  feet           Y    =         4518403
20  meter
 Z    =       16242065
49                 Z    =         4952199
52
 XDOT =     -23718
021986                 XDOT =       -7219
928842
 YDOT =      -5537
420967  feet/sec       YDOT =       -1768
595268  meter/sec
 ZDOT =       6811
953204                 ZDOT =        2041
185925

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2923066
31                 X    =         -890950
61
 Y    =       14563967
14  feet           Y    =         4439097
18  meter
 Z    =       16248734
20                 Z    =         4952614
18
 XDOT =     -20312
773413                 XDOT =       -6191
333336
 YDOT =     -11540
315509  feet/sec       YDOT =       -3517
488167  meter/sec
 ZDOT =       6677
157089                 ZDOT =        2035
197481


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   08097
46767141  
00020000  00000-0  20000-3 0  9021
2 25544  51
6399  26
1068 0001231 332
9376  27
1725 15
77132940 17212


Satellite: ISS
Catalog Number: 25544
Epoch time:      08097
46767141   =   yrday
fracday
Element set:     902
Inclination:       51
6399  deg
RA of node:        26
1068  deg
Eccentricity:     
0001231     
Arg of perigee:   332
9376  deg
Mean anomaly:      27
1725  deg
Mean motion:   15
77132940  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1721
Checksum:              285


Coasting Arc #4 (Orbit 1735)
---------------------------------------

Vector Time (GMT): 2008/098/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6433045
74                 A    =         6722918
02  meter
 Y    =        1764473
11  meter          E    =           
0011183
 Z    =        -790989
57                 I    =           51
77360
 XDOT =       -591
264829                 Wp   =           33
90810
 YDOT =       4817
037323  meter/sec      RA   =           20
69727  deg
 ZDOT =       5986
172254                 TA   =          317
47110
                                          MA   =          317
55767
                                          Ha   =            185
168  n
mi
                                          Hp   =            179
040

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21105793
10                 X    =         6416679
55
 Y    =        5788953
78  feet           Y    =         1836319
57  meter
 Z    =       -2595110
14                 Z    =         -759777
14
 XDOT =      -1939
845238                 XDOT =        -674
165981
 YDOT =      15803
928225  feet/sec       YDOT =        4809
962192  meter/sec
 ZDOT =      19639
672750                 ZDOT =        5983
098267

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18960128
03                 X    =         5779047
02
 Y    =       10958464
76  feet           Y    =         3340140
06  meter
 Z    =       -2475213
16                 Z    =         -754444
97
 XDOT =      -5195
119377                 XDOT =       -1583
472386
 YDOT =      13383
594469  feet/sec       YDOT =        4079
319594  meter/sec
 ZDOT =      19628
368437                 ZDOT =        5982
726700


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   08098
41811899  
00020000  00000-0  20000-3 0  9038
2 25544  51
6397  21
2030 0001177 340
3492  19
7627 15
77170309 17361


Satellite: ISS
Catalog Number: 25544
Epoch time:      08098
41811899   =   yrday
fracday
Element set:     903
Inclination:       51
6397  deg
RA of node:        21
2030  deg
Eccentricity:     
0001177     
Arg of perigee:   340
3492  deg
Mean anomaly:      19
7627  deg
Mean motion:   15
77170309  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1736
Checksum:              291


Coasting Arc #5 (Orbit 1751)
---------------------------------------

Vector Time (GMT): 2008/099/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1477677
01                 A    =         6710965
62  meter
 Y    =       -3904974
46  meter          E    =           
0014536
 Z    =       -5266421
77                 I    =           51
70671
 XDOT =       7330
480174                 Wp   =           88
03702
 YDOT =       2317
873969  meter/sec      RA   =           15
54906  deg
 ZDOT =        339
440590                 TA   =          185
17713
                                          MA   =          185
19218
                                          Ha   =            185
028  n
mi
                                          Hp   =            179
005

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4848021
69                 X    =         1546816
97
 Y    =      -12811596
00  feet           Y    =        -3888063
70  meter
 Z    =      -17278286
66                 Z    =        -5259075
12
 XDOT =      24050
131803                 XDOT =        7302
367556
 YDOT =       7604
573389  feet/sec       YDOT =        2399
690404  meter/sec
 ZDOT =       1113
650229                 ZDOT =         374
984351

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7842188
19                 X    =         2390298
96
 Y    =      -11273862
48  feet           Y    =        -3436273
28  meter
 Z    =      -17250495
80                 Z    =        -5257951
12
 XDOT =      20733
214297                 XDOT =        6319
483718
 YDOT =      12515
684422  feet/sec       YDOT =        3814
780612  meter/sec
 ZDOT =       1250
212913                 ZDOT =         381
064896


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   08099
43188691  
00020000  00000-0  20000-3 0  9049
2 25544  51
6405  15
9721 0001254 338
6824  21
4288 15
77227664 17521


Satellite: ISS
Catalog Number: 25544
Epoch time:      08099
43188691   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:        15
9721  deg
Eccentricity:     
0001254     
Arg of perigee:   338
6824  deg
Mean anomaly:      21
4288  deg
Mean motion:   15
77227664  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1752
Checksum:              302


Coasting Arc #6 (Orbit 1767)
---------------------------------------

Vector Time (GMT): 2008/100/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6175080
66                 A    =         6721901
47  meter
 Y    =       -2252536
94  meter          E    =           
0007386
 Z    =       -1393150
61                 I    =           51
71645
 XDOT =       2828
936403                 Wp   =          139
52078
 YDOT =      -4161
459124  meter/sec      RA   =           10
41075  deg
 ZDOT =      -5833
307462                 TA   =           55
79537
                                          MA   =           55
72539
                                          Ha   =            184
906  n
mi
                                          Hp   =            178
834

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20259451
00                 X    =        -6142665
73
 Y    =       -7390213
06  feet           Y    =        -2321408
95  meter
 Z    =       -4570704
09                 Z    =        -1423070
86
 XDOT =       9281
287413                 XDOT =        2903
597766
 YDOT =     -13653
081114  feet/sec       YDOT =       -4129
406767  meter/sec
 ZDOT =     -19138
147840                 ZDOT =       -5819
383036

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18107848
11                 X    =        -5519272
10
 Y    =      -11666279
67  feet           Y    =        -3555882
04  meter
 Z    =       -4685690
45                 Z    =        -1428198
45
 XDOT =      11316
350820                 XDOT =        3449
223730
 YDOT =      -9928
433234  feet/sec       YDOT =       -3026
186450  meter/sec
 ZDOT =     -19085
145563                 ZDOT =       -5817
152368


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   08100
44561166  
00020000  00000-0  20000-3 0  9056
2 25544  51
6410  10
7411 0001255 340
5042  19
6075 15
77303232 17687


Satellite: ISS
Catalog Number: 25544
Epoch time:      08100
44561166   =   yrday
fracday
Element set:     905
Inclination:       51
6410  deg
RA of node:        10
7411  deg
Eccentricity:     
0001255     
Arg of perigee:   340
5042  deg
Mean anomaly:      19
6075  deg
Mean motion:   15
77303232  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1768
Checksum:              245


Coasting Arc #7 (Orbit 1783)
---------------------------------------

Vector Time (GMT): 2008/101/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3426149
58                 A    =         6713178
39  meter
 Y    =        3393511
68  meter          E    =           
0008323
 Z    =        4666738
99                 I    =           51
65831
 XDOT =      -6608
162877                 Wp   =           54
36373
 YDOT =      -2820
986011  meter/sec      RA   =            5
21882  deg
 ZDOT =      -2791
906257                 TA   =           63
18093
                                          MA   =           63
09584
                                          Ha   =            184
928  n
mi
                                          Hp   =            178
746

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11240648
22                 X    =        -3486512
07
 Y    =       11133568
49  feet           Y    =         3354860
84  meter
 Z    =       15310823
44                 Z    =         4649948
12
 XDOT =     -21680
324399                 XDOT =       -6562
564351
 YDOT =      -9255
203449  feet/sec       YDOT =       -2894
627204  meter/sec
 ZDOT =      -9159
797430                 ZDOT =       -2823
898318

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13356102
00                 X    =        -4070939
89
 Y    =        8595413
26  feet           Y    =         2619881
96  meter
 Z    =       15246745
38                 Z    =         4647207
99
 XDOT =     -18665
124503                 XDOT =       -5689
129948
 YDOT =     -12488
936683  feet/sec       YDOT =       -3806
627901  meter/sec
 ZDOT =      -9282
788821                 ZDOT =       -2829
394033


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   08101
45929349  
00020000  00000-0  20000-3 0  9060
2 25544  51
6409   5
5102 0001234 342
0372  18
0749 15
77365014 17849


Satellite: ISS
Catalog Number: 25544
Epoch time:      08101
45929349   =   yrday
fracday
Element set:     906
Inclination:       51
6409  deg
RA of node:         5
5102  deg
Eccentricity:     
0001234     
Arg of perigee:   342
0372  deg
Mean anomaly:      18
0749  deg
Mean motion:   15
77365014  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1784
Checksum:              271


Coasting Arc #8 (Orbit 1799)
---------------------------------------

Vector Time (GMT): 2008/102/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5144797
13                 A    =         6717369
76  meter
 Y    =        2680338
56  meter          E    =           
0012198
 Z    =        3375138
21                 I    =           51
64407
 XDOT =      -4956
106322                 Wp   =           84
53609
 YDOT =       3659
238160  meter/sec      RA   =             
10532  deg
 ZDOT =       4635
617139                 TA   =          315
35248
                                          MA   =          315
45064
                                          Ha   =            184
680  n
mi
                                          Hp   =            178
608

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16879255
67                 X    =         5098046
94
 Y    =        8793761
69  feet           Y    =         2737609
10  meter
 Z    =       11073288
10                 Z    =         3400018
25
 XDOT =     -16260
191345                 XDOT =       -5019
175187
 YDOT =      12005
374540  feet/sec       YDOT =        3603
463330  meter/sec
 ZDOT =      15208
717648                 ZDOT =        4611
387265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14879437
05                 X    =         4535252
41
 Y    =       11777660
07  feet           Y    =         3589830
79  meter
 Z    =       11168988
41                 Z    =         3404307
67
 XDOT =     -17440
847313                 XDOT =       -5315
970261
 YDOT =       7658
665218  feet/sec       YDOT =        2334
361159  meter/sec
 ZDOT =      15116
124737                 ZDOT =        4607
394820


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   08102
47293199  
00020000  00000-0  20000-3 0  9071
2 25544  51
6409    
2780 0001243 342
9791  17
1332 15
77432123 18000


Satellite: ISS
Catalog Number: 25544
Epoch time:      08102
47293199   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:          
2780  deg
Eccentricity:     
0001243     
Arg of perigee:   342
9791  deg
Mean anomaly:      17
1332  deg
Mean motion:   15
77432123  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1800
Checksum:              263


Coasting Arc #9 (Orbit 1814)
---------------------------------------

Vector Time (GMT): 2008/103/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5091614
46                 A    =         6717843
69  meter
 Y    =       -2998038
45  meter          E    =           
0004581
 Z    =       -3197511
26                 I    =           51
61706
 XDOT =       4993
603788                 Wp   =           62
98899
 YDOT =       3370
119543  meter/sec      RA   =          354
89155  deg
 ZDOT =       4799
068960                 TA   =          259
62712
                                          MA   =          259
67876
                                          Ha   =            184
670  n
mi
                                          Hp   =            178
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16704771
86                 X    =         5140293
47
 Y    =       -9836084
16  feet           Y    =        -2940828
84  meter
 Z    =      -10490522
50                 Z    =        -3172658
09
 XDOT =      16383
214528                 XDOT =        4932
234496
 YDOT =      11056
822649  feet/sec       YDOT =        3425
617610  meter/sec
 ZDOT =      15744
976903                 ZDOT =        4823
178856

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18190157
90                 X    =         5544360
13
 Y    =       -6848455
52  feet           Y    =        -2087409
24  meter
 Z    =      -10395471
57                 Z    =        -3168539
74
 XDOT =      13681
382868                 XDOT =        4170
085498
 YDOT =      12335
071978  feet/sec       YDOT =        3759
729939  meter/sec
 ZDOT =      15837
793724                 ZDOT =        4827
359527


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   08103
42317911  
00020000  00000-0  20000-3 0  9087
2 25544  51
6412 355
3728 0001280 341
9561  18
1558 15
77501226 18153


Satellite: ISS
Catalog Number: 25544
Epoch time:      08103
42317911   =   yrday
fracday
Element set:     908
Inclination:       51
6412  deg
RA of node:       355
3728  deg
Eccentricity:     
0001280     
Arg of perigee:   341
9561  deg
Mean anomaly:      18
1558  deg
Mean motion:   15
77501226  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1815
Checksum:              272


Coasting Arc #10 (Orbit 1830)
---------------------------------------

Vector Time (GMT): 2008/104/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3400335
72                 A    =         6711892
11  meter
 Y    =       -3253852
78  meter          E    =           
0012112
 Z    =       -4796753
74                 I    =           51
56965
 XDOT =       6551
972308                 Wp   =           65
75159
 YDOT =      -3185
123853  meter/sec      RA   =          349
77055  deg
 ZDOT =      -2483
985976                 TA   =          179
91991
                                          MA   =          179
91971
                                          Ha   =            184
546  n
mi
                                          Hp   =            178
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11155957
08                 X    =        -3340396
27
 Y    =      -10675370
03  feet           Y    =        -3291542
11  meter
 Z    =      -15737381
03                 Z    =        -4813126
91
 XDOT =      21495
972140                 XDOT =        6599
168595
 YDOT =     -10449
881407  feet/sec       YDOT =       -3111
592049  meter/sec
 ZDOT =      -8149
560290                 ZDOT =       -2452
042044

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9306124
51                 X    =        -2836506
75
 Y    =      -12240260
88  feet           Y    =        -3730831
52  meter
 Z    =      -15800510
29                 Z    =        -4815995
54
 XDOT =      21992
610557                 XDOT =        6703
347698
 YDOT =      -6358
613311  feet/sec       YDOT =       -1938
105337  meter/sec
 ZDOT =      -8027
324932                 ZDOT =       -2446
728639


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   08104
43673480  
00020000  00000-0  20000-3 0  9096
2 25544  51
6419 350
1403 0001315 346
5500  13
5629 15
77582580 18314


Satellite: ISS
Catalog Number: 25544
Epoch time:      08104
43673480   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:       350
1403  deg
Eccentricity:     
0001315     
Arg of perigee:   346
5500  deg
Mean anomaly:      13
5629  deg
Mean motion:   15
77582580  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1831
Checksum:              272


Coasting Arc #11 (Orbit 1846)
---------------------------------------

Vector Time (GMT): 2008/105/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6141404
62                 A    =         6721500
86  meter
 Y    =        2523856
27  meter          E    =           
0012788
 Z    =        1007522
97                 I    =           51
57365
 XDOT =      -2680
131101                 Wp   =          120
56394
 YDOT =      -4136
766053  meter/sec      RA   =          344
57355  deg
 ZDOT =      -5925
140443                 TA   =           48
39569
                                          MA   =           48
28619
                                          Ha   =            184
485  n
mi
                                          Hp   =            178
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20148965
28                 X    =        -6174064
67
 Y    =        8280368
35  feet           Y    =         2454996
98  meter
 Z    =        3305521
55                 Z    =          977608
82
 XDOT =      -8793
081040                 XDOT =       -2604
890844
 YDOT =     -13572
067103  feet/sec       YDOT =       -4166
316220  meter/sec
 ZDOT =     -19439
437149                 ZDOT =       -5937
977620

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21104547
20                 X    =        -6432665
99
 Y    =        5466929
35  feet           Y    =         1666320
07  meter
 Z    =        3191010
13                 Z    =          972619
89
 XDOT =      -6361
723018                 XDOT =       -1939
053176
 YDOT =     -13085
793190  feet/sec       YDOT =       -3988
549764  meter/sec
 ZDOT =     -19489
090585                 ZDOT =       -5940
274810


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   08105
45024857  
00020000  00000-0  20000-3 0  9109
2 25544  51
6419 344
9076 0001263 344
5398  15
5728 15
77615028 18479


Satellite: ISS
Catalog Number: 25544
Epoch time:      08105
45024857   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:       344
9076  deg
Eccentricity:     
0001263     
Arg of perigee:   344
5398  deg
Mean anomaly:      15
5728  deg
Mean motion:   15
77615028  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1847
Checksum:              300


Coasting Arc #12 (Orbit 1862)
---------------------------------------

Vector Time (GMT): 2008/106/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1212886
09                 A    =         6709496
14  meter
 Y    =        4001010
54  meter          E    =           
0002715
 Z    =        5246104
93                 I    =           51
50644
 XDOT =      -7278
808738                 Wp   =           44
90277
 YDOT =       2527
867788  meter/sec      RA   =          339
41062  deg
 ZDOT =       -243
098998                 TA   =           47
41775
                                          MA   =           47
39485
                                          Ha   =            184
225  n
mi
                                          Hp   =            178
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3979285
08                 X    =         1142571
48
 Y    =       13126675
01  feet           Y    =         4014180
77  meter
 Z    =       17211630
34                 Z    =         5251826
16
 XDOT =     -23880
606097                 XDOT =       -7305
353847
 YDOT =       8293
529489  feet/sec       YDOT =        2446
323557  meter/sec
 ZDOT =       -797
568891                 ZDOT =        -278
523894

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2296631
03                 X    =          700013
14
 Y    =       13494448
45  feet           Y    =         4113107
89  meter
 Z    =       17233974
36                 Z    =         5252915
39
 XDOT =     -23706
996430                 XDOT =       -7225
892512
 YDOT =       5234
783955  feet/sec       YDOT =        1595
562149  meter/sec
 ZDOT =       -933
216703                 ZDOT =        -284
444451


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   08106
46371760  
00020000  00000-0  20000-3 0  9110
2 25544  51
6419 339
6749 0001418 340
0453  20
0656 15
77735104 18639


Satellite: ISS
Catalog Number: 25544
Epoch time:      08106
46371760   =   yrday
fracday
Element set:     911
Inclination:       51
6419  deg
RA of node:       339
6749  deg
Eccentricity:     
0001418     
Arg of perigee:   340
0453  deg
Mean anomaly:      20
0656  deg
Mean motion:   15
77735104  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1863
Checksum:              281

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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