Date: April 27th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5812 51 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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


118/10:40:40 784 7 5 7 6 7 6
N/A 0 8 -0 0 188 9
000/00:01:17 567 1 0 -0 0 175 1

Coasting Arc #1 (Orbit 260)
---------------------------------------

Vector Time (GMT): 2007/116/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5644452
77                 A    =         6714446
54  meter
 Y    =        1556989
05  meter          E    =           
0029860
 Z    =        3255650
58                 I    =           51
69811
 XDOT =      -4019
569544                 Wp   =           99
81826
 YDOT =      -4571
970549  meter/sec      RA   =           10
62840  deg
 ZDOT =      -4750
750598                 TA   =           41
92091
                                          MA   =           41
69268
                                          Ha   =            189
238  n
mi
                                          Hp   =            170
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18518545
83                 X    =        -5677259
09
 Y    =        5108231
79  feet           Y    =         1493686
18  meter
 Z    =       10681268
32                 Z    =         3228150
17
 XDOT =     -13187
564121                 XDOT =       -3945
068094
 YDOT =     -14999
903376  feet/sec       YDOT =       -4616
503060  meter/sec
 ZDOT =     -15586
452092                 ZDOT =       -4770
096697

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16027832
95                 X    =        -4885283
48
 Y    =       10692864
17  feet           Y    =         3259185
00  meter
 Z    =       10577867
99                 Z    =         3224134
16
 XDOT =     -16374
133389                 XDOT =       -4990
835857
 YDOT =      -8948
526368  feet/sec       YDOT =       -2727
510837  meter/sec
 ZDOT =     -15659
870932                 ZDOT =       -4773
128660


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   07116
49673213  
00020000  00000-0  20000-3 0  9009
2 25544  51
6352  10
9408 0017178 106
0785 254
2273 15
78642941  2618


Satellite: ISS
Catalog Number: 25544
Epoch time:      07116
49673213   =   yrday
fracday
Element set:     900
Inclination:       51
6352  deg
RA of node:        10
9408  deg
Eccentricity:     
0017178     
Arg of perigee:   106
0785  deg
Mean anomaly:     254
2273  deg
Mean motion:   15
78642941  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             261
Checksum:              279


Coasting Arc #2 (Orbit 276)
---------------------------------------

Vector Time (GMT): 2007/117/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2079658
68                 A    =         6708283
58  meter
 Y    =        4082696
94  meter          E    =           
0023292
 Z    =        4884494
97                 I    =           51
65015
 XDOT =      -7320
389444                 Wp   =          113
03457
 YDOT =       1056
451684  meter/sec      RA   =            5
50299  deg
 ZDOT =       2216
464462                 TA   =          315
40026
                                          MA   =          315
58744
                                          Ha   =            188
946  n
mi
                                          Hp   =            170
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6823027
16                 X    =         2010122
74
 Y    =       13394675
01  feet           Y    =         4105564
10  meter
 Z    =       16025245
96                 Z    =         4894429
04
 XDOT =     -24017
025734                 XDOT =       -7342
425987
 YDOT =       3466
048833  feet/sec       YDOT =         974
467793  meter/sec
 ZDOT =       7271
865034                 ZDOT =        2180
848375

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10785947
29                 X    =         3287556
73
 Y    =       10412395
38  feet           Y    =         3173698
11  meter
 Z    =       16063153
18                 Z    =         4896049
09
 XDOT =     -20796
354430                 XDOT =       -6338
728830
 YDOT =      10443
648166  feet/sec       YDOT =        3183
223961  meter/sec
 ZDOT =       7137
838506                 ZDOT =        2175
613177


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   07117
50955147  
00020000  00000-0  20000-3 0  9012
2 25544  51
6357   5
7029 0017039 110
0659 250
2342 15
78707598  2775


Satellite: ISS
Catalog Number: 25544
Epoch time:      07117
50955147   =   yrday
fracday
Element set:     901
Inclination:       51
6357  deg
RA of node:         5
7029  deg
Eccentricity:     
0017039     
Arg of perigee:   110
0659  deg
Mean anomaly:     250
2342  deg
Mean motion:   15
78707598  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             277
Checksum:              289


Coasting Arc #3 (Orbit 291)
---------------------------------------

Vector Time (GMT): 2007/118/10:41:19
567
Vector Time (MET): N/A
Weight (LBS)     : 464165
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1435756
38                 A    =         6711367
79  meter
 Y    =       -4075403
41  meter          E    =           
0024761
 Z    =       -5156933
39                 I    =           51
61867
 XDOT =       7510
961208                 Wp   =          108
77083
 YDOT =       1047
141444  meter/sec      RA   =             
37038  deg
 ZDOT =       1260
721193                 TA   =          173
32129
                                          MA   =          173
28823
                                          Ha   =            188
905  n
mi
                                          Hp   =            175
123

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4710486
82                 X    =         1506273
06
 Y    =      -13370746
09  feet           Y    =        -4058953
75  meter
 Z    =      -16919072
79                 Z    =        -5149787
10
 XDOT =      24642
261181                 XDOT =        7492
569288
 YDOT =       3435
503426  feet/sec       YDOT =        1131
030400  meter/sec
 ZDOT =       4136
224386                 ZDOT =        1297
165023

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1026005
05                 X    =          312726
34
 Y    =      -14170619
44  feet           Y    =        -4319204
81  meter
 Z    =      -16892643
94                 Z    =        -5148877
87
 XDOT =      23601
005744                 XDOT =        7193
586551
 YDOT =      -3397
074298  feet/sec       YDOT =       -1035
428246  meter/sec
 ZDOT =       4273
616209                 ZDOT =        1302
598221


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   07118
45904855  
00020000  00000-0  20000-3 0  9028
2 25544  51
6362    
7919 0010998 121
1269 239
0976 15
77271257  2923


Satellite: ISS
Catalog Number: 25544
Epoch time:      07118
45904855   =   yrday
fracday
Element set:     902
Inclination:       51
6362  deg
RA of node:          
7919  deg
Eccentricity:     
0010998     
Arg of perigee:   121
1269  deg
Mean anomaly:     239
0976  deg
Mean motion:   15
77271257  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             292
Checksum:              303


Coasting Arc #4 (Orbit 307)
---------------------------------------

Vector Time (GMT): 2007/119/10:41:19
567
Vector Time (MET): N/A
Weight (LBS)     : 464165
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6242209
60                 A    =         6720742
83  meter
 Y    =       -1204972
49  meter          E    =           
0016949
 Z    =       -2170462
64                 I    =           51
62202
 XDOT =       2791
036756                 Wp   =          129
52379
 YDOT =      -4609
044016  meter/sec      RA   =          355
23886  deg
 ZDOT =      -5507
162846                 TA   =           74
81590
                                          MA   =           74
62851
                                          Ha   =            188
758  n
mi
                                          Hp   =            175
212

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20479690
30                 X    =        -6217727
65
 Y    =       -3953321
83  feet           Y    =        -1274639
50  meter
 Z    =       -7120940
43                 Z    =        -2200728
19
 XDOT =       9156
944737                 XDOT =        2869
121441
 YDOT =     -15121
535485  feet/sec       YDOT =       -4577
396502  meter/sec
 ZDOT =     -18068
119574                 ZDOT =       -5493
414143

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20716812
81                 X    =        -6314484
54
 Y    =        2054653
33  feet           Y    =          626258
34  meter
 Z    =       -7235076
19                 Z    =        -2205251
22
 XDOT =       4698
427157                 XDOT =        1432
080598
 YDOT =     -15626
092891  feet/sec       YDOT =       -4762
833113  meter/sec
 ZDOT =     -18016
886538                 ZDOT =       -5491
547017


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   07119
47276343  
00020000  00000-0  20000-3 0  9036
2 25544  51
6364 355
5599 0010912 125
8421 234
3759 15
77275932  3086


Satellite: ISS
Catalog Number: 25544
Epoch time:      07119
47276343   =   yrday
fracday
Element set:     903
Inclination:       51
6364  deg
RA of node:       355
5599  deg
Eccentricity:     
0010912     
Arg of perigee:   125
8421  deg
Mean anomaly:     234
3759  deg
Mean motion:   15
77275932  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             308
Checksum:              304


Coasting Arc #5 (Orbit 323)
---------------------------------------

Vector Time (GMT): 2007/120/10:41:19
567
Vector Time (MET): N/A
Weight (LBS)     : 464165
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3336710
63                 A    =         6714865
77  meter
 Y    =        3991694
88  meter          E    =           
0018498
 Z    =        4227400
65                 I    =           51
57382
 XDOT =      -6614
224675                 Wp   =          101
50086
 YDOT =      -1723
798315  meter/sec      RA   =          350
03030  deg
 ZDOT =      -3583
446428                 TA   =           24
89230
                                          MA   =           24
80320
                                          Ha   =            188
664  n
mi
                                          Hp   =            175
239

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10947213
35                 X    =        -3401634
63
 Y    =       13096111
80  feet           Y    =         3954018
86  meter
 Z    =       13869424
70                 Z    =         4211032
98
 XDOT =     -21700
212188                 XDOT =       -6577
049308
 YDOT =      -5655
506283  feet/sec       YDOT =       -1797
554387  meter/sec
 ZDOT =     -11756
714004                 ZDOT =       -3615
488572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6549593
65                 X    =        -1996316
14
 Y    =       15815989
47  feet           Y    =         4820713
59  meter
 Z    =       13808253
55                 Z    =         4208755
68
 XDOT =     -21178
404974                 XDOT =       -6455
177836
 YDOT =       1626
948125  feet/sec       YDOT =         495
893788  meter/sec
 ZDOT =     -11877
598441                 ZDOT =       -3620
292005


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   07120
48645512  
00020000  00000-0  20000-3 0  9048
2 25544  51
6360 350
3281 0010775 128
6166 231
5965 15
77362091  3246


Satellite: ISS
Catalog Number: 25544
Epoch time:      07120
48645512   =   yrday
fracday
Element set:     904
Inclination:       51
6360  deg
RA of node:       350
3281  deg
Eccentricity:     
0010775     
Arg of perigee:   128
6166  deg
Mean anomaly:     231
5965  deg
Mean motion:   15
77362091  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             324
Checksum:              276


Coasting Arc #6 (Orbit 339)
---------------------------------------

Vector Time (GMT): 2007/121/10:41:19
567
Vector Time (MET): N/A
Weight (LBS)     : 464165
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5110522
51                 A    =         6715784
93  meter
 Y    =        1856557
16  meter          E    =           
0020965
 Z    =        3932638
91                 I    =           51
54914
 XDOT =      -4754
596820                 Wp   =          116
21069
 YDOT =       4568
269215  meter/sec      RA   =          344
91430  deg
 ZDOT =       3996
526317                 TA   =          292
23524
                                          MA   =          292
45748
                                          Ha   =            188
477  n
mi
                                          Hp   =            175
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16766806
14                 X    =         5070277
97
 Y    =        6091066
80  feet           Y    =         1913480
76  meter
 Z    =       12902358
61                 Z    =         3957368
60
 XDOT =     -15599
070931                 XDOT =       -4824
741275
 YDOT =      14987
759893  feet/sec       YDOT =        4514
708340  meter/sec
 ZDOT =      13111
962983                 ZDOT =        3973
257779

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17765229
20                 X    =         5414841
86
 Y    =         453614
26  feet           Y    =          138261
63  meter
 Z    =       12995714
93                 Z    =         3961093
91
 XDOT =     -10045
988008                 XDOT =       -3062
017145
 YDOT =      17904
871694  feet/sec       YDOT =        5457
404892  meter/sec
 ZDOT =      13024
867997                 ZDOT =        3969
979766


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   07121
50012602  
00020000  00000-0  20000-3 0  9051
2 25544  51
6361 345
0956 0010757 132
5267 227
6808 15
77359071  3407


Satellite: ISS
Catalog Number: 25544
Epoch time:      07121
50012602   =   yrday
fracday
Element set:     905
Inclination:       51
6361  deg
RA of node:       345
0956  deg
Eccentricity:     
0010757     
Arg of perigee:   132
5267  deg
Mean anomaly:     227
6808  deg
Mean motion:   15
77359071  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             340
Checksum:              270


Coasting Arc #7 (Orbit 354)
---------------------------------------

Vector Time (GMT): 2007/122/10:41:19
567
Vector Time (MET): N/A
Weight (LBS)     : 464165
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4811965
84                 A    =         6719710
74  meter
 Y    =       -3944176
41  meter          E    =           
0012058
 Z    =       -2554590
89                 I    =           51
53501
 XDOT =       4948
715782                 Wp   =          110
62654
 YDOT =       2633
905621  meter/sec      RA   =          339
69717  deg
 ZDOT =       5270
867037                 TA   =          220
35549
                                          MA   =          220
44503
                                          Ha   =            188
340  n
mi
                                          Hp   =            175
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15787289
50                 X    =         4868122
56
 Y    =      -12940211
33  feet           Y    =        -3890052
20  meter
 Z    =       -8381203
72                 Z    =        -2531077
65
 XDOT =      16235
944167                 XDOT =        4893
289805
 YDOT =       8641
422641  feet/sec       YDOT =        2688
934773  meter/sec
 ZDOT =      17292
870857                 ZDOT =        5294
773905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10585530
38                 X    =         3226469
66
 Y    =      -17495799
95  feet           Y    =        -5332719
82  meter
 Z    =       -8293110
75                 Z    =        -2527740
16
 XDOT =      16825
458092                 XDOT =        5128
399626
 YDOT =       1965
089300  feet/sec       YDOT =         598
959219  meter/sec
 ZDOT =      17383
217302                 ZDOT =        5298
404634


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   07122
45042068  
00020000  00000-0  20000-3 0  9066
2 25544  51
6359 340
1899 0010546 136
7134 223
4861 15
77404576  3551


Satellite: ISS
Catalog Number: 25544
Epoch time:      07122
45042068   =   yrday
fracday
Element set:     906
Inclination:       51
6359  deg
RA of node:       340
1899  deg
Eccentricity:     
0010546     
Arg of perigee:   136
7134  deg
Mean anomaly:     223
4861  deg
Mean motion:   15
77404576  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             355
Checksum:              289


Coasting Arc #8 (Orbit 370)
---------------------------------------

Vector Time (GMT): 2007/123/10:41:19
567
Vector Time (MET): N/A
Weight (LBS)     : 464165
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3421800
08                 A    =         6711180
12  meter
 Y    =       -2824709
89  meter          E    =           
0020578
 Z    =       -5050979
49                 I    =           51
47964
 XDOT =       6092
458784                 Wp   =          104
05214
 YDOT =      -4384
265827  meter/sec      RA   =          334
56119  deg
 ZDOT =      -1686
134149                 TA   =          149
73893
                                          MA   =          149
61993
                                          Ha   =            188
128  n
mi
                                          Hp   =            175
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11226378
23                 X    =        -3365422
19
 Y    =       -9267420
89  feet           Y    =        -2862658
79  meter
 Z    =      -16571455
03                 Z    =        -5067466
21
 XDOT =      19988
381836                 XDOT =        6149
222579
 YDOT =     -14384
074234  feet/sec       YDOT =       -4315
819037  meter/sec
 ZDOT =      -5531
936184                 ZDOT =       -1656
398789

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13678585
53                 X    =        -4169232
87
 Y    =       -4768671
05  feet           Y    =        -1453490
94  meter
 Z    =      -16633876
70                 Z    =        -5070005
62
 XDOT =      13347
114227                 XDOT =        4068
200416
 YDOT =     -19499
102998  feet/sec       YDOT =       -5943
326594  meter/sec
 ZDOT =      -5420
456348                 ZDOT =       -1652
155095


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   07123
46404740  
00020000  00000-0  20000-3 0  9078
2 25544  51
6352 334
9565 0010429 140
8391 219
3530 15
77452513  3715


Satellite: ISS
Catalog Number: 25544
Epoch time:      07123
46404740   =   yrday
fracday
Element set:     907
Inclination:       51
6352  deg
RA of node:       334
9565  deg
Eccentricity:     
0010429     
Arg of perigee:   140
8391  deg
Mean anomaly:     219
3530  deg
Mean motion:   15
77452513  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             371
Checksum:              275


Coasting Arc #9 (Orbit 386)
---------------------------------------

Vector Time (GMT): 2007/124/10:41:19
567
Vector Time (MET): N/A
Weight (LBS)     : 464165
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5634113
33                 A    =         6722402
90  meter
 Y    =        3630746
25  meter          E    =           
0023243
 Z    =         318968
11                 I    =           51
49191
 XDOT =      -2855
183567                 Wp   =          137
56204
 YDOT =      -3880
519733  meter/sec      RA   =          329
37137  deg
 ZDOT =      -6024
852968                 TA   =           38
95536
                                          MA   =           38
78813
                                          Ha   =            188
128  n
mi
                                          Hp   =            175
736

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18484623
77                 X    =        -5675843
63
 Y    =       11911897
15  feet           Y    =         3567509
09  meter
 Z    =        1046483
31                 Z    =          291496
03
 XDOT =      -9367
400154                 XDOT =       -2782
310619
 YDOT =     -12731
363953  feet/sec       YDOT =       -3912
039984  meter/sec
 ZDOT =     -19766
577979                 ZDOT =       -6038
547066

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12825846
78                 X    =        -3909318
10
 Y    =       17868332
96  feet           Y    =         5446267
89  meter
 Z    =         943434
51                 Z    =          287558
84
 XDOT =     -11981
586446                 XDOT =       -3651
987549
 YDOT =      -7508
459904  feet/sec       YDOT =       -2288
578579  meter/sec
 ZDOT =     -19818
603907                 ZDOT =       -6040
710471


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   07124
47765390  
00020000  00000-0  20000-3 0  9082
2 25544  51
6353 329
7240 0010576 145
2300 214
9558 15
77432237  3879


Satellite: ISS
Catalog Number: 25544
Epoch time:      07124
47765390   =   yrday
fracday
Element set:     908
Inclination:       51
6353  deg
RA of node:       329
7240  deg
Eccentricity:     
0010576     
Arg of perigee:   145
2300  deg
Mean anomaly:     214
9558  deg
Mean motion:   15
77432237  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             387
Checksum:              293


Coasting Arc #10 (Orbit 402)
---------------------------------------

Vector Time (GMT): 2007/125/10:41:19
567
Vector Time (MET): N/A
Weight (LBS)     : 464165
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1554777
22                 A    =         6710409
13  meter
 Y    =        3967740
56  meter          E    =           
0010813
 Z    =        5175440
81                 I    =           51
42781
 XDOT =      -6623
492018                 Wp   =          129
35866
 YDOT =       3837
203583  meter/sec      RA   =          324
19022  deg
 ZDOT =       -957
430639                 TA   =          329
74418
                                          MA   =          329
80657
                                          Ha   =            187
803  n
mi
                                          Hp   =            175
828

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5100975
13                 X    =         1485152
06
 Y    =       13017521
52  feet           Y    =         3984737
09  meter
 Z    =       16979792
69                 Z    =         5182825
35
 XDOT =     -21730
616856                 XDOT =       -6661
256811
 YDOT =      12589
250602  feet/sec       YDOT =        3762
924937  meter/sec
 ZDOT =      -3141
176636                 ZDOT =        -989
699397

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9610910
71                 X    =         2929405
58
 Y    =       10106696
21  feet           Y    =         3080521
00  meter
 Z    =       17008064
58                 Z    =         5184058
08
 XDOT =     -14496
870288                 XDOT =       -4418
646064
 YDOT =      19245
663266  feet/sec       YDOT =        5866
078163  meter/sec
 ZDOT =      -3262
274162                 ZDOT =        -994
341165


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   07125
49123531  
00020000  00000-0  20000-3 0  9091
2 25544  51
6349 324
4905 0010312 149
1572 211
0200 15
77516865  4037


Satellite: ISS
Catalog Number: 25544
Epoch time:      07125
49123531   =   yrday
fracday
Element set:     909
Inclination:       51
6349  deg
RA of node:       324
4905  deg
Eccentricity:     
0010312     
Arg of perigee:   149
1572  deg
Mean anomaly:     211
0200  deg
Mean motion:   15
77516865  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             403
Checksum:              260


Coasting Arc #11 (Orbit 418)
---------------------------------------

Vector Time (GMT): 2007/126/10:41:19
567
Vector Time (MET): N/A
Weight (LBS)     : 464165
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5731473
23                 A    =         6720320
16  meter
 Y    =       -2904661
94  meter          E    =           
0018138
 Z    =        1961651
97                 I    =           51
43832
 XDOT =        736
272667                 Wp   =          102
26551
 YDOT =       5255
895095  meter/sec      RA   =          319
03852  deg
 ZDOT =       5584
148393                 TA   =          279
66097
                                          MA   =          279
86582
                                          Ha   =            187
653  n
mi
                                          Hp   =            175
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18804046
03                 X    =         5753998
14
 Y    =       -9529730
78  feet           Y    =        -2840443
69  meter
 Z    =        6435866
03                 Z    =         1989550
17
 XDOT =       2415
592738                 XDOT =         650
318662
 YDOT =      17243
750313  feet/sec       YDOT =        5263
647263  meter/sec
 ZDOT =      18320
696829                 ZDOT =        5587
517079

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13408495
19                 X    =         4086909
33
 Y    =      -16225316
55  feet           Y    =        -4945476
48  meter
 Z    =        6540615
21                 Z    =         1993579
52
 XDOT =       7816
727551                 XDOT =        2382
538558
 YDOT =      13911
714594  feet/sec       YDOT =        4240
290608  meter/sec
 ZDOT =      18333
992239                 ZDOT =        5588
200834


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   07126
50479536  
00020000  00000-0  20000-3 0  9105
2 25544  51
6339 319
2564 0010237 153
7835 206
3850 15
77567262  4190


Satellite: ISS
Catalog Number: 25544
Epoch time:      07126
50479536   =   yrday
fracday
Element set:     910
Inclination:       51
6339  deg
RA of node:       319
2564  deg
Eccentricity:     
0010237     
Arg of perigee:   153
7835  deg
Mean anomaly:     206
3850  deg
Mean motion:   15
77567262  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             419
Checksum:              297


Coasting Arc #12 (Orbit 433)
---------------------------------------

Vector Time (GMT): 2007/127/10:41:19
567
Vector Time (MET): N/A
Weight (LBS)     : 464165
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         209642
53                 A    =         6713987
72  meter
 Y    =       -5171361
75  meter          E    =           
0017366
 Z    =       -4294749
23                 I    =           51
39521
 XDOT =       6347
952783                 Wp   =          135
47965
 YDOT =      -2622
018282  meter/sec      RA   =          313
81523  deg
 ZDOT =       3463
332649                 TA   =          169
71934
                                          MA   =          169
68377
                                          Ha   =            187
549  n
mi
                                          Hp   =            176
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         687803
57                 X    =          288317
13
 Y    =      -16966409
93  feet           Y    =        -5168577
02  meter
 Z    =      -14090384
61                 Z    =        -4293540
27
 XDOT =      20826
616741                 XDOT =        6359
976409
 YDOT =      -8602
422184  feet/sec       YDOT =       -2550
965090  meter/sec
 ZDOT =      11362
639923                 ZDOT =        3494
200141

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6337143
64                 X    =        -1931561
38
 Y    =      -15757036
38  feet           Y    =        -4802744
69  meter
 Z    =      -14086429
39                 Z    =        -4293543
68
 XDOT =      14178
344283                 XDOT =        4321
559337
 YDOT =     -15974
814697  feet/sec       YDOT =       -4869
123520  meter/sec
 ZDOT =      11478
611916                 ZDOT =        3498
680912


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   07127
45498954  
00020000  00000-0  20000-3 0  9116
2 25544  51
6331 314
3490 0010183 157
0716 203
0906 15
77578769  4348


Satellite: ISS
Catalog Number: 25544
Epoch time:      07127
45498954   =   yrday
fracday
Element set:     911
Inclination:       51
6331  deg
RA of node:       314
3490  deg
Eccentricity:     
0010183     
Arg of perigee:   157
0716  deg
Mean anomaly:     203
0906  deg
Mean motion:   15
77578769  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             434
Checksum:              296


Coasting Arc #13 (Orbit 448)
---------------------------------------

Vector Time (GMT): 2007/128/10:41:19
567
Vector Time (MET): N/A
Weight (LBS)     : 464165
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5232179
45                 A    =         6715072
95  meter
 Y    =        1507779
40  meter          E    =           
0012419
 Z    =       -3932762
48                 I    =           51
37958
 XDOT =       1115
884104                 Wp   =          126
35060
 YDOT =      -6493
285610  meter/sec      RA   =          308
68513  deg
 ZDOT =      -3990
011638                 TA   =          102
18832
                                          MA   =          102
04919
                                          Ha   =            187
310  n
mi
                                          Hp   =            176
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17165943
06                 X    =        -5229546
06
 Y    =        4946782
79  feet           Y    =         1449285
37  meter
 Z    =      -12902764
05                 Z    =        -3958173
96
 XDOT =       3661
037086                 XDOT =        1207
792859
 YDOT =     -21303
430479  feet/sec       YDOT =       -6480
292863  meter/sec
 ZDOT =     -13090
589364                 ZDOT =       -3984
368085

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13302750
30                 X    =        -4054678
29
 Y    =       11819567
44  feet           Y    =         3602604
16  meter
 Z    =      -12998316
86                 Z    =        -3961886
98
 XDOT =      -4932
240314                 XDOT =       -1503
346848
 YDOT =     -19867
503181  feet/sec       YDOT =       -6055
614970  meter/sec
 ZDOT =     -13070
086117                 ZDOT =       -3983
762248


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   07128
46850758  
00020000  00000-0  20000-3 0  9123
2 25544  51
6323 309
1157 0010108 160
9405 199
2140 15
77607401  4494


Satellite: ISS
Catalog Number: 25544
Epoch time:      07128
46850758   =   yrday
fracday
Element set:     912
Inclination:       51
6323  deg
RA of node:       309
1157  deg
Eccentricity:     
0010108     
Arg of perigee:   160
9405  deg
Mean anomaly:     199
2140  deg
Mean motion:   15
77607401  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             449
Checksum:              279

INTERNATIONAL SPACE STATION ORBITAL DATA:

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

DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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