Date: May 24th 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 2463)
---------------------------------------

Vector Time (GMT): 2008/144/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1488663
28                 A    =         6713593
70  meter
 Y    =       -3996881
51  meter          E    =           
0002249
 Z    =        5186653
94                 I    =           51
81192
 XDOT =       6550
993734                 Wp   =          276
26149
 YDOT =      -3895
144356  meter/sec      RA   =          142
61786  deg
 ZDOT =      -1121
551983                 TA   =          184
41205
                                          MA   =          184
41403
                                          Ha   =            184
928  n
mi
                                          Hp   =            182
088

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4884065
87                 X    =        -1469054
89
 Y    =      -13113128
32  feet           Y    =        -4013419
82  meter
 Z    =       17016581
16                 Z    =         5179468
92
 XDOT =      21492
761595                 XDOT =        6599
511300
 YDOT =     -12779
345001  feet/sec       YDOT =       -3821
615936  meter/sec
 ZDOT =      -3679
632490                 ZDOT =       -1089
609816

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14012843
15                 X    =        -4271114
59
 Y    =        -633600
39  feet           Y    =         -193121
40  meter
 Z    =       16988556
32                 Z    =         5178111
97
 XDOT =      -3235
916246                 XDOT =        -986
307272
 YDOT =     -23796
753658  feet/sec       YDOT =       -7253
250515  meter/sec
 ZDOT =      -3557
197883                 ZDOT =       -1084
233915


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   08144
56204941  
00020000  00000-0  20000-3 0  9007
2 25544  51
6336 143
3443 0005688 251
0919 108
9629 15
76422474 24645


Satellite: ISS
Catalog Number: 25544
Epoch time:      08144
56204941   =   yrday
fracday
Element set:     900
Inclination:       51
6336  deg
RA of node:       143
3443  deg
Eccentricity:     
0005688     
Arg of perigee:   251
0919  deg
Mean anomaly:     108
9629  deg
Mean motion:   15
76422474  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2464
Checksum:              294


Coasting Arc #2 (Orbit 2479)
---------------------------------------

Vector Time (GMT): 2008/145/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5607788
31                 A    =         6723775
86  meter
 Y    =        3248769
30  meter          E    =           
0008466
 Z    =        1774419
69                 I    =           51
86956
 XDOT =      -1116
548397                 Wp   =           59
43263
 YDOT =      -5053
325188  meter/sec      RA   =          137
50432  deg
 ZDOT =       5707
597682                 TA   =          320
18326
                                          MA   =          320
24535
                                          Ha   =            184
637  n
mi
                                          Hp   =            182
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18398255
62                 X    =        -5652319
62
 Y    =       10658691
94  feet           Y    =         3185810
54  meter
 Z    =        5821586
92                 Z    =         1747069
29
 XDOT =      -3663
216527                 XDOT =       -1087
684920
 YDOT =     -16579
150879  feet/sec       YDOT =       -5065
650589  meter/sec
 ZDOT =      18725
714179                 ZDOT =        5702
242778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2830204
17                 X    =          862646
23
 Y    =       21102211
73  feet           Y    =         6431954
14  meter
 Z    =        5716730
06                 Z    =         1742459
32
 XDOT =     -15225
767602                 XDOT =       -4640
813965
 YDOT =      -3039
450732  feet/sec       YDOT =        -926
424583  meter/sec
 ZDOT =      18704
620957                 ZDOT =        5701
168468


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   08145
57630880  
00020000  00000-0  20000-3 0  9015
2 25544  51
6338 138
1167 0005781 253
7300 106
3228 15
76493036 24806


Satellite: ISS
Catalog Number: 25544
Epoch time:      08145
57630880   =   yrday
fracday
Element set:     901
Inclination:       51
6338  deg
RA of node:       138
1167  deg
Eccentricity:     
0005781     
Arg of perigee:   253
7300  deg
Mean anomaly:     106
3228  deg
Mean motion:   15
76493036  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2480
Checksum:              283


Coasting Arc #3 (Orbit 2494)
---------------------------------------

Vector Time (GMT): 2008/146/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         515738
74                 A    =         6715885
91  meter
 Y    =        4838250
31  meter          E    =           
0006483
 Z    =       -4635134
23                 I    =           51
86334
 XDOT =      -6235
661952                 Wp   =          135
53747
 YDOT =       3453
989344  meter/sec      RA   =          132
32734  deg
 ZDOT =       2909
426872                 TA   =          163
18740
                                          MA   =          163
16590
                                          Ha   =            184
476  n
mi
                                          Hp   =            182
100

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1692056
24                 X    =          484115
02
 Y    =       15873524
65  feet           Y    =         4843841
45  meter
 Z    =      -15207133
29                 Z    =        -4632704
88
 XDOT =     -20458
208505                 XDOT =       -6287
955049
 YDOT =      11331
986036  feet/sec       YDOT =        3383
965801  meter/sec
 ZDOT =       9545
363754                 ZDOT =        2879
007443

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15426873
30                 X    =         4702110
98
 Y    =        4140292
53  feet           Y    =         1261961
16  meter
 Z    =      -15197312
26                 Z    =        -4632140
78
 XDOT =       3361
597774                 XDOT =        1024
615002
 YDOT =      22108
735199  feet/sec       YDOT =        6738
742489  meter/sec
 ZDOT =       9428
711477                 ZDOT =        2873
871258


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   08146
52716762  
00020000  00000-0  20000-3 0  9026
2 25544  51
6338 133
2149 0005649 259
9177 100
1350 15
76441525 24955


Satellite: ISS
Catalog Number: 25544
Epoch time:      08146
52716762   =   yrday
fracday
Element set:     902
Inclination:       51
6338  deg
RA of node:       133
2149  deg
Eccentricity:     
0005649     
Arg of perigee:   259
9177  deg
Mean anomaly:     100
1350  deg
Mean motion:   15
76441525  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2495
Checksum:              293


Coasting Arc #4 (Orbit 2510)
---------------------------------------

Vector Time (GMT): 2008/147/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5236204
65                 A    =         6720582
02  meter
 Y    =       -2682096
81  meter          E    =           
0001578
 Z    =       -3246614
36                 I    =           51
89870
 XDOT =        124
951986                 Wp   =          220
43188
 YDOT =       6035
280314  meter/sec      RA   =          127
23685  deg
 ZDOT =      -4784
235665                 TA   =          357
44667
                                          MA   =          357
44748
                                          Ha   =            184
359  n
mi
                                          Hp   =            182
075

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17179149
11                 X    =         5281578
59
 Y    =       -8799530
22  feet           Y    =        -2623288
47  meter
 Z    =      -10651621
92                 Z    =        -3221066
97
 XDOT =        409
947460                 XDOT =          80
696226
 YDOT =      19800
788432  feet/sec       YDOT =        6036
430756  meter/sec
 ZDOT =     -15696
311236                 ZDOT =       -4783
735382

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2228150
82                 X    =         -679140
37
 Y    =      -19226761
44  feet           Y    =        -5860316
89  meter
 Z    =      -10553621
85                 Z    =        -3216743
94
 XDOT =      17327
419755                 XDOT =        5281
397541
 YDOT =       6606
529115  feet/sec       YDOT =        2013
670074  meter/sec
 ZDOT =     -15693
792275                 ZDOT =       -4783
467885


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   08147
54140095  
00020000  00000-0  20000-3 0  9030
2 25544  51
6342 127
9863 0005610 264
3341  95
7184 15
76491877 25112


Satellite: ISS
Catalog Number: 25544
Epoch time:      08147
54140095   =   yrday
fracday
Element set:     903
Inclination:       51
6342  deg
RA of node:       127
9863  deg
Eccentricity:     
0005610     
Arg of perigee:   264
3341  deg
Mean anomaly:      95
7184  deg
Mean motion:   15
76491877  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2511
Checksum:              294


Coasting Arc #5 (Orbit 2526)
---------------------------------------

Vector Time (GMT): 2008/148/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         221183
75                 A    =         6719368
94  meter
 Y    =       -5667550
05  meter          E    =           
0006317
 Z    =        3598065
80                 I    =           51
91153
 XDOT =       5734
434117                 Wp   =           83
42185
 YDOT =      -2600
139829  meter/sec      RA   =          122
05011  deg
 ZDOT =      -4440
845459                 TA   =           53
68713
                                          MA   =           53
62882
                                          Ha   =            184
162  n
mi
                                          Hp   =            181
993

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         725668
46                 X    =          267063
94
 Y    =      -18594324
32  feet           Y    =        -5664820
52  meter
 Z    =       11804677
81                 Z    =         3599251
13
 XDOT =      18813
760225                 XDOT =        5784
655976
 YDOT =      -8530
642482  feet/sec       YDOT =       -2535
732811  meter/sec
 ZDOT =     -14569
702948                 ZDOT =       -4412
865793

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17314479
18                 X    =        -5277453
26
 Y    =       -6811004
56  feet           Y    =        -2075994
19  meter
 Z    =       11808680
59                 Z    =         3599285
84
 XDOT =      -2250
087916                 XDOT =        -685
826797
 YDOT =     -19395
873289  feet/sec       YDOT =       -5911
862178  meter/sec
 ZDOT =     -14462
330844                 ZDOT =       -4408
118441


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   08148
55561910  
00020000  00000-0  20000-3 0  9046
2 25544  51
6340 122
7582 0005752 269
1343  90
9162 15
76518967 25273


Satellite: ISS
Catalog Number: 25544
Epoch time:      08148
55561910   =   yrday
fracday
Element set:     904
Inclination:       51
6340  deg
RA of node:       122
7582  deg
Eccentricity:     
0005752     
Arg of perigee:   269
1343  deg
Mean anomaly:      90
9162  deg
Mean motion:   15
76518967  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2527
Checksum:              301


Coasting Arc #6 (Orbit 2542)
---------------------------------------

Vector Time (GMT): 2008/149/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4760963
59                 A    =         6716528
37  meter
 Y    =        1753983
29  meter          E    =           
0004294
 Z    =        4400185
70                 I    =           51
91744
 XDOT =        562
872855                 Wp   =          136
12645
 YDOT =      -6910
661533  meter/sec      RA   =          116
96513  deg
 ZDOT =       3358
753263                 TA   =          280
21659
                                          MA   =          280
26501
                                          Ha   =            184
153  n
mi
                                          Hp   =            181
970

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15619959
30                 X    =        -4801598
50
 Y    =        5754538
34  feet           Y    =         1700515
83  meter
 Z    =       14436304
79                 Z    =         4376958
26
 XDOT =       1846
695718                 XDOT =         623
790812
 YDOT =     -22672
774057  feet/sec       YDOT =       -6904
026886  meter/sec
 ZDOT =      11019
531702                 ZDOT =        3361
635009

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         486737
67                 X    =          148357
64
 Y    =       16716095
76  feet           Y    =         5095065
99  meter
 Z    =       14347123
92                 Z    =         4373003
37
 XDOT =     -19722
361116                 XDOT =       -6011
375668
 YDOT =      -8906
605385  feet/sec       YDOT =       -2714
733321  meter/sec
 ZDOT =      11029
941907                 ZDOT =        3361
926293


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   08149
56982136  
00020000  00000-0  20000-3 0  9056
2 25544  51
6347 117
5301 0005870 271
8574  88
1919 15
76571789 25436


Satellite: ISS
Catalog Number: 25544
Epoch time:      08149
56982136   =   yrday
fracday
Element set:     905
Inclination:       51
6347  deg
RA of node:       117
5301  deg
Eccentricity:     
0005870     
Arg of perigee:   271
8574  deg
Mean anomaly:      88
1919  deg
Mean motion:   15
76571789  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2543
Checksum:              324


Coasting Arc #7 (Orbit 2557)
---------------------------------------

Vector Time (GMT): 2008/150/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -692435
48                 A    =         6722856
74  meter
 Y    =        6319513
87  meter          E    =           
0005513
 Z    =       -2175264
25                 I    =           51
95050
 XDOT =      -5194
907112                 Wp   =          343
95884
 YDOT =       1333
890249  meter/sec      RA   =          111
78675  deg
 ZDOT =       5530
712165                 TA   =          351
76667
                                          MA   =          351
77571
                                          Ha   =            184
212  n
mi
                                          Hp   =            181
956

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2271769
95                 X    =         -752482
66
 Y    =       20733313
21  feet           Y    =         6311435
12  meter
 Z    =       -7136693
73                 Z    =        -2178773
40
 XDOT =     -17043
658503                 XDOT =       -5236
304263
 YDOT =       4376
280345  feet/sec       YDOT =        1275
565844  meter/sec
 ZDOT =      18145
381118                 ZDOT =        5505
374609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19106591
64                 X    =         5823689
13
 Y    =        8353757
01  feet           Y    =         2546225
14  meter
 Z    =       -7149581
29                 Z    =        -2179192
38
 XDOT =       -365
104867                 XDOT =        -111
283963
 YDOT =      16276
251408  feet/sec       YDOT =        4961
001429  meter/sec
 ZDOT =      18048
036632                 ZDOT =        5501
041566


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   08150
52062455  
00020000  00000-0  20000-3 0  9068
2 25544  51
6344 112
6278 0005738 276
9872  83
0639 15
76549255 25584


Satellite: ISS
Catalog Number: 25544
Epoch time:      08150
52062455   =   yrday
fracday
Element set:     906
Inclination:       51
6344  deg
RA of node:       112
6278  deg
Eccentricity:     
0005738     
Arg of perigee:   276
9872  deg
Mean anomaly:      83
0639  deg
Mean motion:   15
76549255  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2558
Checksum:              314


Coasting Arc #8 (Orbit 2573)
---------------------------------------

Vector Time (GMT): 2008/151/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4329902
07                 A    =         6713555
22  meter
 Y    =        -493430
00  meter          E    =           
0008730
 Z    =       -5114428
02                 I    =           51
92974
 XDOT =       -976
777725                 Wp   =           63
44660
 YDOT =       7478
297627  meter/sec      RA   =          106
68486  deg
 ZDOT =      -1546
635683                 TA   =          191
75879
                                          MA   =          191
77920
                                          Ha   =            184
264  n
mi
                                          Hp   =            182
070

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14205715
44                 X    =         4359943
21
 Y    =       -1618864
82  feet           Y    =         -444842
08  meter
 Z    =      -16779619
49                 Z    =        -5093320
11
 XDOT =      -3204
651328                 XDOT =       -1052
815238
 YDOT =      24535
097200  feet/sec       YDOT =        7466
949745  meter/sec
 ZDOT =      -5074
264053                 ZDOT =       -1551
564898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2506557
11                 X    =          763998
61
 Y    =      -14172411
88  feet           Y    =        -4319751
14  meter
 Z    =      -16698461
54                 Z    =        -5089691
08
 XDOT =      21591
345997                 XDOT =        6581
042260
 YDOT =       9825
866143  feet/sec       YDOT =        2994
924000  meter/sec
 ZDOT =      -5092
512832                 ZDOT =       -1552
197911


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   08151
53479850  
00020000  00000-0  20000-3 0  9072
2 25544  51
6351 107
3988 0005822 280
9258  79
1251 15
76580185 25749


Satellite: ISS
Catalog Number: 25544
Epoch time:      08151
53479850   =   yrday
fracday
Element set:     907
Inclination:       51
6351  deg
RA of node:       107
3988  deg
Eccentricity:     
0005822     
Arg of perigee:   280
9258  deg
Mean anomaly:      79
1251  deg
Mean motion:   15
76580185  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2574
Checksum:              313


Coasting Arc #9 (Orbit 2589)
---------------------------------------

Vector Time (GMT): 2008/152/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         970547
26                 A    =         6724690
41  meter
 Y    =       -6631981
83  meter          E    =           
0008233
 Z    =         479696
87                 I    =           51
97536
 XDOT =       4771
093281                 Wp   =          147
59121
 YDOT =        258
107098  meter/sec      RA   =          101
53400  deg
 ZDOT =      -6044
098409                 TA   =           27
20948
                                          MA   =           27
16637
                                          Ha   =            184
384  n
mi
                                          Hp   =            181
907

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3184210
16                 X    =         1042304
66
 Y    =      -21758470
57  feet           Y    =        -6620727
45  meter
 Z    =        1573808
64                 Z    =          484585
40
 XDOT =      15653
193178                 XDOT =        4797
214196
 YDOT =        846
808065  feet/sec       YDOT =         311
606959  meter/sec
 ZDOT =     -19829
719191                 ZDOT =       -6020
856501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20118169
89                 X    =        -6132018
18
 Y    =       -8875353
74  feet           Y    =        -2705207
82  meter
 Z    =        1591994
32                 Z    =          485239
87
 XDOT =       4382
675576                 XDOT =        1335
839516
 YDOT =     -13498
892347  feet/sec       YDOT =       -4114
462387  meter/sec
 ZDOT =     -19740
276362                 ZDOT =       -6016
836235


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   08152
54895733  
00020000  00000-0  20000-3 0  9087
2 25544  51
6358 102
1701 0005825 284
8879  75
1640 15
76599186 25904


Satellite: ISS
Catalog Number: 25544
Epoch time:      08152
54895733   =   yrday
fracday
Element set:     908
Inclination:       51
6358  deg
RA of node:       102
1701  deg
Eccentricity:     
0005825     
Arg of perigee:   284
8879  deg
Mean anomaly:      75
1640  deg
Mean motion:   15
76599186  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2590
Checksum:              323


Coasting Arc #10 (Orbit 2605)
---------------------------------------

Vector Time (GMT): 2008/153/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4043834
88                 A    =         6712638
98  meter
 Y    =        -974549
55  meter          E    =           
0004212
 Z    =        5271339
21                 I    =           51
94023
 XDOT =       1218
958320                 Wp   =          312
58524
 YDOT =      -7591
993469  meter/sec      RA   =           96
40215  deg
 ZDOT =       -465
923444                 TA   =          141
83532
                                          MA   =          141
80548
                                          Ha   =            184
587  n
mi
                                          Hp   =            181
834

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13267174
81                 X    =        -4058244
53
 Y    =       -3197341
03  feet           Y    =        -1019851
38  meter
 Z    =       17294419
96                 Z    =         5251658
68
 XDOT =       3999
207086                 XDOT =        1306
026010
 YDOT =     -24908
115056  feet/sec       YDOT =       -7577
875490  meter/sec
 ZDOT =      -1528
620224                 ZDOT =        -459
791255

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6445482
67                 X    =        -1964583
12
 Y    =       12137261
62  feet           Y    =         3699437
34  meter
 Z    =       17218609
49                 Z    =         5248232
17
 XDOT =     -22223
177114                 XDOT =       -6773
624384
 YDOT =      -9653
552929  feet/sec       YDOT =       -2942
402933  meter/sec
 ZDOT =      -1505
722451                 ZDOT =        -458
944203


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   08153
56309975  
00020000  00000-0  20000-3 0  9099
2 25544  51
6363  96
9418 0005932 289
0490  71
0032 15
76646215 26064


Satellite: ISS
Catalog Number: 25544
Epoch time:      08153
56309975   =   yrday
fracday
Element set:     909
Inclination:       51
6363  deg
RA of node:        96
9418  deg
Eccentricity:     
0005932     
Arg of perigee:   289
0490  deg
Mean anomaly:      71
0032  deg
Mean motion:   15
76646215  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2606
Checksum:              305


Coasting Arc #11 (Orbit 2621)
---------------------------------------

Vector Time (GMT): 2008/154/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1152041
71                 A    =         6723935
34  meter
 Y    =        6490781
16  meter          E    =           
0011513
 Z    =        1287002
14                 I    =           51
98062
 XDOT =      -4561
110324                 Wp   =           34
55103
 YDOT =      -1980
478110  meter/sec      RA   =           91
28478  deg
 ZDOT =       5889
216635                 TA   =          339
52589
                                          MA   =          339
57200
                                          Ha   =            184
719  n
mi
                                          Hp   =            181
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3779664
41                 X    =        -1230789
18
 Y    =       21295213
78  feet           Y    =         6477457
83  meter
 Z    =        4222447
95                 Z    =         1281215
32
 XDOT =     -14964
272716                 XDOT =       -4567
234638
 YDOT =      -6497
631596  feet/sec       YDOT =       -2031
518384  meter/sec
 ZDOT =      19321
576885                 ZDOT =        5867
043064

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19814137
43                 X    =         6039349
09
 Y    =        8680703
69  feet           Y    =         2645878
49  meter
 Z    =        4200761
96                 Z    =         1280392
25
 XDOT =      -9211
191775                 XDOT =       -2807
571253
 YDOT =      11690
464176  feet/sec       YDOT =        3563
253481  meter/sec
 ZDOT =      19236
079731                 ZDOT =        5863
157102


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   08154
57722804  
00020000  00000-0  20000-3 0  9103
2 25544  51
6365  91
7123 0005925 293
1210  66
9329 15
76652170 26227


Satellite: ISS
Catalog Number: 25544
Epoch time:      08154
57722804   =   yrday
fracday
Element set:     910
Inclination:       51
6365  deg
RA of node:        91
7123  deg
Eccentricity:     
0005925     
Arg of perigee:   293
1210  deg
Mean anomaly:      66
9329  deg
Mean motion:   15
76652170  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2622
Checksum:              282


Coasting Arc #12 (Orbit 2636)
---------------------------------------

Vector Time (GMT): 2008/155/12:23:29
943
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3961842
99                 A    =         6714453
09  meter
 Y    =        2457309
68  meter          E    =           
0006161
 Z    =       -4837655
60                 I    =           51
94923
 XDOT =      -1441
239429                 Wp   =           98
61448
 YDOT =       7154
508125  meter/sec      RA   =           86
12033  deg
 ZDOT =       2455
584889                 TA   =          195
26519
                                          MA   =          195
28379
                                          Ha   =            184
893  n
mi
                                          Hp   =            181
773

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12998172
53                 X    =         3957571
32
 Y    =        8062039
65  feet           Y    =         2501590
43  meter
 Z    =      -15871573
48                 Z    =        -4818418
51
 XDOT =      -4728
475817                 XDOT =       -1533
064115
 YDOT =      23472
795686  feet/sec       YDOT =        7137
877418  meter/sec
 ZDOT =       8056
380869                 ZDOT =        2448
361724

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10712524
94                 X    =         3265177
60
 Y    =      -11024608
09  feet           Y    =        -3360300
54  meter
 Z    =      -15797330
25                 Z    =        -4815026
26
 XDOT =      21071
362764                 XDOT =        6422
551370
 YDOT =       8977
896288  feet/sec       YDOT =        2736
462789  meter/sec
 ZDOT =       8029
210309                 ZDOT =        2447
303302


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   08155
52795862  
00020000  00000-0  20000-3 0  9114
2 25544  51
6375  86
8104 0005935 296
9059  63
1498 15
76678865 26376


Satellite: ISS
Catalog Number: 25544
Epoch time:      08155
52795862   =   yrday
fracday
Element set:     911
Inclination:       51
6375  deg
RA of node:        86
8104  deg
Eccentricity:     
0005935     
Arg of perigee:   296
9059  deg
Mean anomaly:      63
1498  deg
Mean motion:   15
76678865  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2637
Checksum:              342

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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