Date: March 21st 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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 1449)
---------------------------------------

Vector Time (GMT): 2008/080/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2935987
41                 A    =         6714561
53  meter
 Y    =       -3230019
53  meter          E    =           
0004199
 Z    =        5100244
26                 I    =           51
91754
 XDOT =       4161
914504                 Wp   =           46
66406
 YDOT =      -6289
649110  meter/sec      RA   =          114
02141  deg
 ZDOT =      -1583
815295                 TA   =           58
49175
                                          MA   =           58
45074
                                          Ha   =            186
452  n
mi
                                          Hp   =            180
676

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9632504
62                 X    =        -2924426
36
 Y    =      -10597176
93  feet           Y    =        -3262786
25  meter
 Z    =       16733084
83                 Z    =         5086009
83
 XDOT =      13654
575145                 XDOT =        4239
630803
 YDOT =     -20635
331726  feet/sec       YDOT =       -6242
673833  meter/sec
 ZDOT =      -5196
244405                 ZDOT =       -1563
407569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11261191
39                 X    =         3432411
13
 Y    =       -8950275
67  feet           Y    =        -2728044
02  meter
 Z    =       16678116
38                 Z    =         5083489
87
 XDOT =      18958
904325                 XDOT =        5778
674038
 YDOT =      14293
393135  feet/sec       YDOT =        4356
626228  meter/sec
 ZDOT =      -5118
727722                 ZDOT =       -1560
188210


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   08080
29086815  
00020000  00000-0  20000-3 0  9004
2 25544  51
6382 114
6530 0000895 274
1102  85
9960 15
76227791 14500


Satellite: ISS
Catalog Number: 25544
Epoch time:      08080
29086815   =   yrday
fracday
Element set:     900
Inclination:       51
6382  deg
RA of node:       114
6530  deg
Eccentricity:     
0000895     
Arg of perigee:   274
1102  deg
Mean anomaly:      85
9960  deg
Mean motion:   15
76227791  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1450
Checksum:              286


Coasting Arc #2 (Orbit 1465)
---------------------------------------

Vector Time (GMT): 2008/081/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3552943
30                 A    =         6723784
94  meter
 Y    =        5300484
27  meter          E    =           
0013277
 Z    =        2098857
74                 I    =           51
96029
 XDOT =      -3128
477450                 Wp   =           67
95545
 YDOT =      -4311
474450  meter/sec      RA   =          108
92153  deg
 ZDOT =       5569
409823                 TA   =          315
41781
                                          MA   =          315
52453
                                          Ha   =            186
284  n
mi
                                          Hp   =            180
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11656638
13                 X    =        -3622145
87
 Y    =       17390040
25  feet           Y    =         5260366
52  meter
 Z    =        6886016
22                 Z    =         2081429
02
 XDOT =     -10264
033628                 XDOT =       -3107
088329
 YDOT =     -14145
257381  feet/sec       YDOT =       -4346
338675  meter/sec
 ZDOT =      18272
341939                 ZDOT =        5554
264227

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16735117
60                 X    =        -5100863
85
 Y    =      -12614835
21  feet           Y    =        -3845001
77  meter
 Z    =        6819802
29                 Z    =         2078675
74
 XDOT =      13763
090890                 XDOT =        4194
990103
 YDOT =      -8370
614428  feet/sec       YDOT =       -2551
363278  meter/sec
 ZDOT =      18213
753321                 ZDOT =        5551
552012


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   08081
30524119  
00020000  00000-0  20000-3 0  9012
2 25544  51
6387 109
4258 0000923 275
0739  85
0320 15
76293109 14666


Satellite: ISS
Catalog Number: 25544
Epoch time:      08081
30524119   =   yrday
fracday
Element set:     901
Inclination:       51
6387  deg
RA of node:       109
4258  deg
Eccentricity:     
0000923     
Arg of perigee:   275
0739  deg
Mean anomaly:      85
0320  deg
Mean motion:   15
76293109  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1466
Checksum:              280


Coasting Arc #3 (Orbit 1480)
---------------------------------------

Vector Time (GMT): 2008/082/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2575730
76                 A    =         6716870
90  meter
 Y    =        4282916
73  meter          E    =           
0008829
 Z    =       -4496329
62                 I    =           51
94523
 XDOT =      -3986
435648                 Wp   =          111
45897
 YDOT =       5754
332844  meter/sec      RA   =          103
74902  deg
 ZDOT =       3199
408258                 TA   =          190
39574
                                          MA   =          190
41401
                                          Ha   =            186
217  n
mi
                                          Hp   =            180
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8450560
23                 X    =         2549489
38
 Y    =       14051564
09  feet           Y    =         4311572
83  meter
 Z    =      -14751737
61                 Z    =        -4483880
95
 XDOT =     -13078
857112                 XDOT =       -4066
027315
 YDOT =      18879
044763  feet/sec       YDOT =        5709
309559  meter/sec
 ZDOT =      10496
746252                 ZDOT =        3179
848280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14354983
67                 X    =        -4375399
02
 Y    =        8013348
29  feet           Y    =         2442468
56  meter
 Z    =      -14703498
79                 Z    =        -4481626
43
 XDOT =     -17800
402819                 XDOT =       -5425
562779
 YDOT =     -12774
618321  feet/sec       YDOT =       -3893
703664  meter/sec
 ZDOT =      10422
406042                 ZDOT =        3176
749362


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   08082
25620233  
00020000  00000-0  20000-3 0  9022
2 25544  51
6385 104
5261 0000989 283
2577  76
8477 15
76307353 14812


Satellite: ISS
Catalog Number: 25544
Epoch time:      08082
25620233   =   yrday
fracday
Element set:     902
Inclination:       51
6385  deg
RA of node:       104
5261  deg
Eccentricity:     
0000989     
Arg of perigee:   283
2577  deg
Mean anomaly:      76
8477  deg
Mean motion:   15
76307353  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1481
Checksum:              296


Coasting Arc #4 (Orbit 1496)
---------------------------------------

Vector Time (GMT): 2008/083/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3428621
06                 A    =         6720490
71  meter
 Y    =       -4650079
65  meter          E    =           
0004055
 Z    =       -3436970
68                 I    =           51
96348
 XDOT =       2815
416092                 Wp   =           84
22854
 YDOT =       5482
931504  meter/sec      RA   =           98
66652  deg
 ZDOT =      -4613
827983                 TA   =          136
24753
                                          MA   =          136
21539
                                          Ha   =            186
221  n
mi
                                          Hp   =            180
604

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11248756
75                 X    =         3497060
36
 Y    =      -15256166
85  feet           Y    =        -4611356
51  meter
 Z    =      -11276150
52                 Z    =        -3420147
74
 XDOT =       9236
929435                 XDOT =        2776
309031
 YDOT =      17988
620419  feet/sec       YDOT =        5514
196005  meter/sec
 ZDOT =     -15137
230916                 ZDOT =       -4600
246177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15033105
91                 X    =         4582090
68
 Y    =       11607311
18  feet           Y    =         3537908
45  meter
 Z    =      -11212171
05                 Z    =        -3417469
73
 XDOT =     -17320
255777                 XDOT =       -5279
213961
 YDOT =       7874
637175  feet/sec       YDOT =        2400
189411  meter/sec
 ZDOT =     -15084
513672                 ZDOT =       -4597
759767


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   08083
27054311  
00020000  00000-0  20000-3 0  9034
2 25544  51
6388  99
2983 0000959 286
2659  73
8400 15
76320625 14974


Satellite: ISS
Catalog Number: 25544
Epoch time:      08083
27054311   =   yrday
fracday
Element set:     903
Inclination:       51
6388  deg
RA of node:        99
2983  deg
Eccentricity:     
0000959     
Arg of perigee:   286
2659  deg
Mean anomaly:      73
8400  deg
Mean motion:   15
76320625  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1497
Checksum:              310


Coasting Arc #5 (Orbit 1512)
---------------------------------------

Vector Time (GMT): 2008/084/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2393685
55                 A    =         6720350
73  meter
 Y    =       -5233502
50  meter          E    =           
0011693
 Z    =        3461094
10                 I    =           51
96624
 XDOT =       3888
175993                 Wp   =           86
84440
 YDOT =      -4820
897396  meter/sec      RA   =           93
48500  deg
 ZDOT =      -4586
777066                 TA   =           52
28631
                                          MA   =           52
18037
                                          Ha   =            186
297  n
mi
                                          Hp   =            180
463

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7853299
06                 X    =        -2351799
26
 Y    =      -17170283
81  feet           Y    =        -5260035
60  meter
 Z    =       11355295
59                 Z    =         3449567
66
 XDOT =      12756
482916                 XDOT =        3964
076877
 YDOT =     -15816
592506  feet/sec       YDOT =       -4776
993555  meter/sec
 ZDOT =     -15048
481189                 ZDOT =       -4567
703493

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17188154
27                 X    =         5238949
42
 Y    =       -7878813
34  feet           Y    =        -2401462
31  meter
 Z    =       11310497
04                 Z    =         3447439
50
 XDOT =      15212
973422                 XDOT =        4636
914299
 YDOT =      11623
998790  feet/sec       YDOT =        3542
994831  meter/sec
 ZDOT =     -14975
881428                 ZDOT =       -4564
648659


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   08084
28486659  
00020000  00000-0  20000-3 0  9041
2 25544  51
6387  94
0713 0000829 297
0618  63
0462 15
76337649 15130


Satellite: ISS
Catalog Number: 25544
Epoch time:      08084
28486659   =   yrday
fracday
Element set:     904
Inclination:       51
6387  deg
RA of node:        94
0713  deg
Eccentricity:     
0000829     
Arg of perigee:   297
0618  deg
Mean anomaly:      63
0462  deg
Mean motion:   15
76337649  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1513
Checksum:              313


Coasting Arc #6 (Orbit 1528)
---------------------------------------

Vector Time (GMT): 2008/085/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3396562
37                 A    =         6716680
99  meter
 Y    =        3681464
22  meter          E    =           
0008130
 Z    =        4469922
10                 I    =           51
95562
 XDOT =      -2714
772899                 Wp   =          111
09945
 YDOT =      -6445
637460  meter/sec      RA   =           88
40265  deg
 ZDOT =       3238
253674                 TA   =          306
62053
                                          MA   =          306
69528
                                          Ha   =            186
208  n
mi
                                          Hp   =            180
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11143577
34                 X    =        -3459190
84
 Y    =       12078294
70  feet           Y    =         3643132
00  meter
 Z    =       14665098
74                 Z    =         4453269
17
 XDOT =      -8906
735232                 XDOT =       -2658
225958
 YDOT =     -21147
104529  feet/sec       YDOT =       -6475
679253  meter/sec
 ZDOT =      10624
191843                 ZDOT =        3225
202937

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12244668
41                 X    =        -3732174
93
 Y    =      -11044894
84  feet           Y    =        -3366483
95  meter
 Z    =       14601644
88                 Z    =         4450581
36
 XDOT =      20205
371986                 XDOT =        6158
597381
 YDOT =      -8388
990344  feet/sec       YDOT =       -2556
964257  meter/sec
 ZDOT =      10573
419637                 ZDOT =        3222
778305


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   08085
29916947  
00020000  00000-0  20000-3 0  9052
2 25544  51
6393  88
8433 0000949 300
0067  60
1003 15
76410379 15291


Satellite: ISS
Catalog Number: 25544
Epoch time:      08085
29916947   =   yrday
fracday
Element set:     905
Inclination:       51
6393  deg
RA of node:        88
8433  deg
Eccentricity:     
0000949     
Arg of perigee:   300
0067  deg
Mean anomaly:      60
1003  deg
Mean motion:   15
76410379  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1529
Checksum:              295


Coasting Arc #7 (Orbit 1543)
---------------------------------------

Vector Time (GMT): 2008/086/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2364539
32                 A    =         6723499
09  meter
 Y    =        5927119
82  meter          E    =           
0006573
 Z    =       -2109278
71                 I    =           51
97634
 XDOT =      -3961
271838                 Wp   =           30
95376
 YDOT =       3556
655594  meter/sec      RA   =           83
23012  deg
 ZDOT =       5566
741836                 TA   =          305
56842
                                          MA   =          305
62967
                                          Ha   =            186
189  n
mi
                                          Hp   =            180
446

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7757674
94                 X    =         2308332
16
 Y    =       19445931
16  feet           Y    =         5953247
10  meter
 Z    =       -6920205
75                 Z    =        -2097928
45
 XDOT =     -12996
298680                 XDOT =       -4027
790892
 YDOT =      11668
817566  feet/sec       YDOT =        3511
986659  meter/sec
 ZDOT =      18263
588701                 ZDOT =        5547
336162

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19185309
92                 X    =        -5847682
46
 Y    =        8417791
66  feet           Y    =         2565742
90  meter
 Z    =       -6876021
63                 Z    =        -2095811
39
 XDOT =     -11469
940696                 XDOT =       -3496
037924
 YDOT =     -11318
933258  feet/sec       YDOT =       -3450
010857  meter/sec
 ZDOT =      18189
555063                 ZDOT =        5544
176383


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   08086
25006451  
00020000  00000-0  20000-3 0  9060
2 25544  51
6395  83
9433 0001131 311
8168  48
2900 15
76377305 15446


Satellite: ISS
Catalog Number: 25544
Epoch time:      08086
25006451   =   yrday
fracday
Element set:     906
Inclination:       51
6395  deg
RA of node:        83
9433  deg
Eccentricity:     
0001131     
Arg of perigee:   311
8168  deg
Mean anomaly:      48
2900  deg
Mean motion:   15
76377305  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1544
Checksum:              278


Coasting Arc #8 (Orbit 1559)
---------------------------------------

Vector Time (GMT): 2008/087/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3582149
69                 A    =         6713960
70  meter
 Y    =       -2468507
50  meter          E    =           
0013281
 Z    =       -5125597
14                 I    =           51
93941
 XDOT =       2691
892493                 Wp   =           74
95371
 YDOT =       7048
126128  meter/sec      RA   =           78
13041  deg
 ZDOT =      -1512
972708                 TA   =          180
58450
                                          MA   =          180
58605
                                          Ha   =            186
115  n
mi
                                          Hp   =            180
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11752459
60                 X    =         3634386
03
 Y    =       -8098777
90  feet           Y    =        -2428157
89  meter
 Z    =      -16816263
59                 Z    =        -5108068
05
 XDOT =       8831
668285                 XDOT =        2620
228965
 YDOT =      23123
773385  feet/sec       YDOT =        7077
827687  meter/sec
 ZDOT =      -4963
821222                 ZDOT =       -1500
069642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8673306
60                 X    =         2643623
85
 Y    =       11433805
95  feet           Y    =         3485024
05  meter
 Z    =      -16749300
44                 Z    =        -5105186
77
 XDOT =     -21824
838657                 XDOT =       -6652
210823
 YDOT =       9357
090149  feet/sec       YDOT =        2852
041077  meter/sec
 ZDOT =      -4913
567022                 ZDOT =       -1497
655228


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   08087
26433380  
00020000  00000-0  20000-3 0  9078
2 25544  51
6391  78
7160 0001045 310
6852  49
4221 15
76418664 15603


Satellite: ISS
Catalog Number: 25544
Epoch time:      08087
26433380   =   yrday
fracday
Element set:     907
Inclination:       51
6391  deg
RA of node:        78
7160  deg
Eccentricity:     
0001045     
Arg of perigee:   310
6852  deg
Mean anomaly:      49
4221  deg
Mean motion:   15
76418664  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1560
Checksum:              283


Coasting Arc #9 (Orbit 1575)
---------------------------------------

Vector Time (GMT): 2008/088/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2326690
05                 A    =         6725075
92  meter
 Y    =       -6284379
38  meter          E    =           
0012191
 Z    =         492859
22                 I    =           51
96983
 XDOT =       4307
117022                 Wp   =          128
79438
 YDOT =      -2075
731128  meter/sec      RA   =           72
98143  deg
 ZDOT =      -6042
490767                 TA   =           45
86252
                                          MA   =           45
76233
                                          Ha   =            186
141  n
mi
                                          Hp   =            180
203

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7633497
54                 X    =        -2258638
44
 Y    =      -20618042
59  feet           Y    =        -6310017
26  meter
 Z    =        1616992
18                 Z    =          481721
49
 XDOT =      14130
961357                 XDOT =        4359
361447
 YDOT =      -6810
141497  feet/sec       YDOT =       -2027
274427  meter/sec
 ZDOT =     -19824
444774                 ZDOT =       -6021
439828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20064169
34                 X    =         6115558
81
 Y    =       -8996750
92  feet           Y    =        -2742209
68  meter
 Z    =        1573597
98                 Z    =          479632
67
 XDOT =       7086
165182                 XDOT =        2159
863147
 YDOT =      12295
756894  feet/sec       YDOT =        3747
746701  meter/sec
 ZDOT =     -19743
924391                 ZDOT =       -6017
948155


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   08088
27858460  
00020000  00000-0  20000-3 0  9081
2 25544  51
6389  73
4885 0000954 324
1006  36
0095 15
76464624 15760


Satellite: ISS
Catalog Number: 25544
Epoch time:      08088
27858460   =   yrday
fracday
Element set:     908
Inclination:       51
6389  deg
RA of node:        73
4885  deg
Eccentricity:     
0000954     
Arg of perigee:   324
1006  deg
Mean anomaly:      36
0095  deg
Mean motion:   15
76464624  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1576
Checksum:              313


Coasting Arc #10 (Orbit 1591)
---------------------------------------

Vector Time (GMT): 2008/089/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3990163
04                 A    =         6712953
16  meter
 Y    =        1154150
16  meter          E    =           
0002447
 Z    =        5272115
93                 I    =           51
92039
 XDOT =      -2614
884044                 Wp   =           46
81474
 YDOT =      -7239
199061  meter/sec      RA   =           67
84966  deg
 ZDOT =       -392
527181                 TA   =           46
90530
                                          MA   =           46
88483
                                          Ha   =            186
127  n
mi
                                          Hp   =            180
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13091086
10                 X    =        -4028383
34
 Y    =        3786581
89  feet           Y    =         1109316
21  meter
 Z    =       17296968
26                 Z    =         5252638
89
 XDOT =      -8579
015893                 XDOT =       -2531
833026
 YDOT =     -23750
653087  feet/sec       YDOT =       -7267
975828  meter/sec
 ZDOT =      -1287
818835                 ZDOT =        -405
028501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4876599
69                 X    =        -1486387
59
 Y    =      -12826075
76  feet           Y    =        -3909387
89  meter
 Z    =       17222380
92                 Z    =         5249381
71
 XDOT =      22015
061666                 XDOT =        6710
190796
 YDOT =     -10172
755808  feet/sec       YDOT =       -3100
655970  meter/sec
 ZDOT =      -1336
540664                 ZDOT =        -407
377594


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   08089
29281412  
00020000  00000-0  20000-3 0  9092
2 25544  51
6396  68
2604 0001089 320
9980  39
1106 15
76528592 15924


Satellite: ISS
Catalog Number: 25544
Epoch time:      08089
29281412   =   yrday
fracday
Element set:     909
Inclination:       51
6396  deg
RA of node:        68
2604  deg
Eccentricity:     
0001089     
Arg of perigee:   320
9980  deg
Mean anomaly:      39
1106  deg
Mean motion:   15
76528592  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1592
Checksum:              308


Coasting Arc #11 (Orbit 1607)
---------------------------------------

Vector Time (GMT): 2008/090/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2181595
50                 A    =         6724459
60  meter
 Y    =        6243107
10  meter          E    =           
0014178
 Z    =        1176908
94                 I    =           51
94618
 XDOT =      -4905
046037                 Wp   =           53
37339
 YDOT =        591
208271  meter/sec      RA   =           62
73072  deg
 ZDOT =       5915
677896                 TA   =          319
48285
                                          MA   =          319
58832
                                          Ha   =            186
170  n
mi
                                          Hp   =            180
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7157465
55                 X    =         2105904
78
 Y    =       20482634
83  feet           Y    =         6267079
75  meter
 Z    =        3861249
81                 Z    =         1187323
18
 XDOT =     -16092
670724                 XDOT =       -4940
029645
 YDOT =       1939
659682  feet/sec       YDOT =         536
161702  meter/sec
 ZDOT =      19408
392047                 ZDOT =        5891
764298

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19659210
93                 X    =        -5992127
49
 Y    =        9163395
96  feet           Y    =         2793003
09  meter
 Z    =        3901857
62                 Z    =         1189286
20
 XDOT =      -2894
487841                 XDOT =        -882
239894
 YDOT =     -14491
045999  feet/sec       YDOT =       -4416
870820  meter/sec
 ZDOT =      19316
722332                 ZDOT =        5887
736967


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   08090
30702820  
00020000  00000-0  20000-3 0  9109
2 25544  51
6390  63
0325 0001115 339
8240  20
2880 15
76502401 16088


Satellite: ISS
Catalog Number: 25544
Epoch time:      08090
30702820   =   yrday
fracday
Element set:     910
Inclination:       51
6390  deg
RA of node:        63
0325  deg
Eccentricity:     
0001115     
Arg of perigee:   339
8240  deg
Mean anomaly:      20
2880  deg
Mean motion:   15
76502401  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1608
Checksum:              239


Coasting Arc #12 (Orbit 1622)
---------------------------------------

Vector Time (GMT): 2008/091/05:54:08
675
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4606164
49                 A    =         6714601
99  meter
 Y    =          91307
78  meter          E    =           
0011683
 Z    =       -4895354
74                 I    =           51
89836
 XDOT =       2299
686237                 Wp   =          101
97511
 YDOT =       6976
104618  meter/sec      RA   =           57
56596  deg
 ZDOT =       2296
160239                 TA   =          190
29409
                                          MA   =          190
31803
                                          Ha   =            186
115  n
mi
                                          Hp   =            180
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15112088
21                 X    =         4628581
72
 Y    =         299566
21  feet           Y    =          142941
78  meter
 Z    =      -16060875
13                 Z    =        -4872923
69
 XDOT =       7544
902351                 XDOT =        2210
353174
 YDOT =      22887
482344  feet/sec       YDOT =        7001
321585  meter/sec
 ZDOT =       7533
334117                 ZDOT =        2307
114904

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1494651
41                 X    =          455569
75
 Y    =       15132345
85  feet           Y    =         4612339
01  meter
 Z    =      -15974817
25                 Z    =        -4869124
30
 XDOT =     -20740
071333                 XDOT =       -6321
573742
 YDOT =      10038
724840  feet/sec       YDOT =        3059
803331  meter/sec
 ZDOT =       7576
091156                 ZDOT =        2309
192584


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   08091
25783298  
00020000  00000-0  20000-3 0  9113
2 25544  51
6386  58
1310 0001133 342
5905  17
5220 15
76551440 16232


Satellite: ISS
Catalog Number: 25544
Epoch time:      08091
25783298   =   yrday
fracday
Element set:     911
Inclination:       51
6386  deg
RA of node:        58
1310  deg
Eccentricity:     
0001133     
Arg of perigee:   342
5905  deg
Mean anomaly:      17
5220  deg
Mean motion:   15
76551440  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1623
Checksum:              267

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 may contain past, current and future orbital data 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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