Date: October 28th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4574 66 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 3148)
---------------------------------------

Vector Time (GMT): 2007/299/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         106959
75                 A    =         6716244
31  meter
 Y    =       -4656370
87  meter          E    =           
0007679
 Z    =        4833322
93                 I    =           51
80305
 XDOT =       6925
436434                 Wp   =           74
41987
 YDOT =      -2362
526715  meter/sec      RA   =          146
05405  deg
 ZDOT =      -2424
097904                 TA   =           39
19555
                                          MA   =           39
13996
                                          Ha   =            187
625  n
mi
                                          Hp   =            180
120

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         350917
80                 X    =          135539
78
 Y    =      -15276807
33  feet           Y    =        -4655014
95  meter
 Z    =       15857358
70                 Z    =         4833912
02
 XDOT =      22721
248142                 XDOT =        6963
116097
 YDOT =      -7751
071900  feet/sec       YDOT =       -2284
871905  meter/sec
 ZDOT =      -7953
077114                 ZDOT =       -2390
361379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3508911
70                 X    =         1069516
29
 Y    =       14870745
74  feet           Y    =         4532603
30  meter
 Z    =       15859012
27                 Z    =         4833826
94
 XDOT =     -19071
030791                 XDOT =       -5812
850185
 YDOT =      12863
296841  feet/sec       YDOT =        3920
732877  meter/sec
 ZDOT =      -7825
085551                 ZDOT =       -2385
086076


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   07299
48950989  
00020000  00000-0  20000-3 0  9008
2 25544  51
6372 146
8010 0002098 134
7911 225
3424 15
76014798 31498


Satellite: ISS
Catalog Number: 25544
Epoch time:      07299
48950989   =   yrday
fracday
Element set:     900
Inclination:       51
6372  deg
RA of node:       146
8010  deg
Eccentricity:     
0002098     
Arg of perigee:   134
7911  deg
Mean anomaly:     225
3424  deg
Mean motion:   15
76014798  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3149
Checksum:              308


Coasting Arc #2 (Orbit 3164)
---------------------------------------

Vector Time (GMT): 2007/300/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5819828
91                 A    =         6723383
15  meter
 Y    =        1982663
62  meter          E    =           
0014836
 Z    =        2706419
61                 I    =           51
84898
 XDOT =        499
330335                 Wp   =           85
41112
 YDOT =      -5664
953636  meter/sec      RA   =          140
95749  deg
 ZDOT =       5200
661060                 TA   =          305
40773
                                          MA   =          305
54621
                                          Ha   =            187
648  n
mi
                                          Hp   =            180
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19093926
87                 X    =        -5854714
57
 Y    =        6504801
90  feet           Y    =         1917387
86  meter
 Z    =        8879329
41                 Z    =         2678061
20
 XDOT =       1638
222885                 XDOT =         537
374825
 YDOT =     -18585
805893  feet/sec       YDOT =       -5659
157279  meter/sec
 ZDOT =      17062
536285                 ZDOT =        5203
179137

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16759833
14                 X    =         5108397
14
 Y    =      -11309189
55  feet           Y    =        -3447040
98  meter
 Z    =        8771727
69                 Z    =         2673622
60
 XDOT =       2574
075513                 XDOT =         784
578216
 YDOT =      17115
288978  feet/sec       YDOT =        5216
740080  meter/sec
 ZDOT =      17071
409801                 ZDOT =        5203
365707


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   07300
50406180  
00020000  00000-0  20000-3 0  9014
2 25544  51
6361 141
5741 0002041 138
0283 222
1038 15
76000474 31656


Satellite: ISS
Catalog Number: 25544
Epoch time:      07300
50406180   =   yrday
fracday
Element set:     901
Inclination:       51
6361  deg
RA of node:       141
5741  deg
Eccentricity:     
0002041     
Arg of perigee:   138
0283  deg
Mean anomaly:     222
1038  deg
Mean motion:   15
76000474  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3165
Checksum:              232


Coasting Arc #3 (Orbit 3179)
---------------------------------------

Vector Time (GMT): 2007/301/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -717999
92                 A    =         6718888
11  meter
 Y    =        5244894
55  meter          E    =           
0009678
 Z    =       -4147852
23                 I    =           51
85538
 XDOT =      -6381
051828                 Wp   =          116
85588
 YDOT =       2094
856422  meter/sec      RA   =          135
77246  deg
 ZDOT =       3755
892267                 TA   =          191
49505
                                          MA   =          191
51717
                                          Ha   =            187
486  n
mi
                                          Hp   =            180
182

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2355642
79                 X    =         -756445
62
 Y    =       17207659
28  feet           Y    =         5236650
75  meter
 Z    =      -13608439
08                 Z    =        -4151433
46
 XDOT =     -20935
209409                 XDOT =       -6422
248581
 YDOT =       6872
888523  feet/sec       YDOT =        2023
269324  meter/sec
 ZDOT =      12322
481190                 ZDOT =        3724
792206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2621025
72                 X    =         -798888
64
 Y    =      -17158944
46  feet           Y    =        -5230046
27  meter
 Z    =      -13621418
96                 Z    =        -4151808
50
 XDOT =      16995
198757                 XDOT =        5180
136581
 YDOT =     -12278
100055  feet/sec       YDOT =       -3742
364897  meter/sec
 ZDOT =      12204
449472                 ZDOT =        3719
916199


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   07301
45518671  
00020000  00000-0  20000-3 0  9029
2 25544  51
6354 136
6737 0002030 143
5037 216
6266 15
76035209 31806


Satellite: ISS
Catalog Number: 25544
Epoch time:      07301
45518671   =   yrday
fracday
Element set:     902
Inclination:       51
6354  deg
RA of node:       136
6737  deg
Eccentricity:     
0002030     
Arg of perigee:   143
5037  deg
Mean anomaly:     216
6266  deg
Mean motion:   15
76035209  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3180
Checksum:              267


Coasting Arc #4 (Orbit 3195)
---------------------------------------

Vector Time (GMT): 2007/302/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5308374
56                 A    =         6720144
11  meter
 Y    =       -1592300
40  meter          E    =           
0007003
 Z    =       -3806601
55                 I    =           51
87869
 XDOT =      -1106
844056                 Wp   =           91
75773
 YDOT =       6350
850685  meter/sec      RA   =          130
68872  deg
 ZDOT =      -4206
894371                 TA   =          134
26966
                                          MA   =          134
21218
                                          Ha   =            187
455  n
mi
                                          Hp   =            180
321

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17415927
03                 X    =         5344277
61
 Y    =       -5224082
67  feet           Y    =        -1532738
13  meter
 Z    =      -12488850
22                 Z    =        -3780725
73
 XDOT =      -3631
378135                 XDOT =       -1157
341120
 YDOT =      20836
124294  feet/sec       YDOT =        6338
191292  meter/sec
 ZDOT =     -13802
146888                 ZDOT =       -4212
393751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15156559
76                 X    =        -4619719
42
 Y    =       10165055
63  feet           Y    =         3098308
96  meter
 Z    =      -12390612
34                 Z    =        -3776658
64
 XDOT =      -2030
887870                 XDOT =        -619
014623
 YDOT =     -19849
230136  feet/sec       YDOT =       -6050
045345  meter/sec
 ZDOT =     -13822
298948                 ZDOT =       -4213
036719


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   07302
46970316  
00020000  00000-0  20000-3 0  9030
2 25544  51
6347 131
4474 0001974 148
1611 211
9673 15
76047159 31968


Satellite: ISS
Catalog Number: 25544
Epoch time:      07302
46970316   =   yrday
fracday
Element set:     903
Inclination:       51
6347  deg
RA of node:       131
4474  deg
Eccentricity:     
0001974     
Arg of perigee:   148
1611  deg
Mean anomaly:     211
9673  deg
Mean motion:   15
76047159  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3196
Checksum:              290


Coasting Arc #5 (Orbit 3211)
---------------------------------------

Vector Time (GMT): 2007/303/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1144851
78                 A    =         6721846
50  meter
 Y    =       -5829658
92  meter          E    =           
0014056
 Z    =        3129675
43                 I    =           51
90412
 XDOT =       5772
276185                 Wp   =          100
55968
 YDOT =      -1497
300076  meter/sec      RA   =          125
50378  deg
 ZDOT =      -4884
680462                 TA   =           43
12461
                                          MA   =           43
01458
                                          Ha   =            187
213  n
mi
                                          Hp   =            180
187

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3756075
38                 X    =         1194751
13
 Y    =      -19126177
56  feet           Y    =        -5816577
76  meter
 Z    =       10267964
01                 Z    =         3135358
02
 XDOT =      18937
913992                 XDOT =        5812
319550
 YDOT =      -4912
401824  feet/sec       YDOT =       -1432
526979  meter/sec
 ZDOT =     -16025
854535                 ZDOT =       -4856
541052

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2460724
21                 X    =          750028
74
 Y    =       19324428
77  feet           Y    =         5890085
89  meter
 Z    =       10288884
50                 Z    =         3136051
99
 XDOT =     -15132
404992                 XDOT =       -4612
357041
 YDOT =      10430
322235  feet/sec       YDOT =        3179
162217  meter/sec
 ZDOT =     -15918
979315                 ZDOT =       -4852
104895


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   07303
48420029  
00020000  00000-0  20000-3 0  9045
2 25544  51
6356 126
2204 0001765 152
2346 207
8913 15
76126158 32127


Satellite: ISS
Catalog Number: 25544
Epoch time:      07303
48420029   =   yrday
fracday
Element set:     904
Inclination:       51
6356  deg
RA of node:       126
2204  deg
Eccentricity:     
0001765     
Arg of perigee:   152
2346  deg
Mean anomaly:     207
8913  deg
Mean motion:   15
76126158  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3212
Checksum:              264


Coasting Arc #6 (Orbit 3227)
---------------------------------------

Vector Time (GMT): 2007/304/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4766646
13                 A    =         6717013
31  meter
 Y    =         944760
54  meter          E    =           
0009822
 Z    =        4632717
77                 I    =           51
90190
 XDOT =       1454
393882                 Wp   =          122
49855
 YDOT =      -6986
123936  meter/sec      RA   =          120
41686  deg
 ZDOT =       2911
522931                 TA   =          298
76368
                                          MA   =          298
86231
                                          Ha   =            187
415  n
mi
                                          Hp   =            180
270

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15638602
79                 X    =        -4799361
54
 Y    =        3099608
08  feet           Y    =          891274
03  meter
 Z    =       15199205
28                 Z    =         4609481
66
 XDOT =       4771
633472                 XDOT =        1518
261826
 YDOT =     -22920
354122  feet/sec       YDOT =       -6969
503141  meter/sec
 ZDOT =       9552
240587                 ZDOT =        2918
743222

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13831965
99                 X    =         4215983
23
 Y    =       -8094844
29  feet           Y    =        -2467308
54  meter
 Z    =       15110907
37                 Z    =         4605804
57
 XDOT =       2486
443751                 XDOT =         757
868055
 YDOT =      22189
098815  feet/sec       YDOT =        6763
237319  meter/sec
 ZDOT =       9578
879745                 ZDOT =        2919
642546


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   07304
49868326  
00020000  00000-0  20000-3 0  9054
2 25544  51
6346 120
9930 0001851 153
2409 206
8851 15
76078021 32282


Satellite: ISS
Catalog Number: 25544
Epoch time:      07304
49868326   =   yrday
fracday
Element set:     905
Inclination:       51
6346  deg
RA of node:       120
9930  deg
Eccentricity:     
0001851     
Arg of perigee:   153
2409  deg
Mean anomaly:     206
8851  deg
Mean motion:   15
76078021  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3228
Checksum:              288


Coasting Arc #7 (Orbit 3242)
---------------------------------------

Vector Time (GMT): 2007/305/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1341524
93                 A    =         6724536
26  meter
 Y    =        6311825
12  meter          E    =           
0006301
 Z    =       -1888371
51                 I    =           51
94089
 XDOT =      -5181
733014                 Wp   =           54
27371
 YDOT =        588
673673  meter/sec      RA   =          115
24470  deg
 ZDOT =       5665
494473                 TA   =          284
82810
                                          MA   =          284
89788
                                          Ha   =            187
162  n
mi
                                          Hp   =            180
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4401328
51                 X    =        -1402831
53
 Y    =       20708087
67  feet           Y    =         6296480
72  meter
 Z    =       -6195444
58                 Z    =        -1895037
40
 XDOT =     -17000
436396                 XDOT =       -5215
452801
 YDOT =       1931
344073  feet/sec       YDOT =         530
539858  meter/sec
 ZDOT =      18587
580292                 ZDOT =        5640
239435

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3042284
64                 X    =         -927288
36
 Y    =      -20943626
43  feet           Y    =        -6383617
34  meter
 Z    =       -6220059
24                 Z    =        -1895874
06
 XDOT =      13862
506665                 XDOT =        4225
292032
 YDOT =      -7489
287704  feet/sec       YDOT =       -2282
734892  meter/sec
 ZDOT =      18491
548716                 ZDOT =        5636
224049


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   07305
44974091  
00020000  00000-0  20000-3 0  9068
2 25544  51
6340 116
0921 0001949 160
1338 199
9903 15
76134424 32435


Satellite: ISS
Catalog Number: 25544
Epoch time:      07305
44974091   =   yrday
fracday
Element set:     906
Inclination:       51
6340  deg
RA of node:       116
0921  deg
Eccentricity:     
0001949     
Arg of perigee:   160
1338  deg
Mean anomaly:     199
9903  deg
Mean motion:   15
76134424  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3243
Checksum:              285


Coasting Arc #8 (Orbit 3258)
---------------------------------------

Vector Time (GMT): 2007/306/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4310642
33                 A    =         6714545
81  meter
 Y    =          -9129
69  meter          E    =           
0014560
 Z    =       -5160683
41                 I    =           51
91799
 XDOT =      -1592
725008                 Wp   =           87
49446
 YDOT =       7405
753025  meter/sec      RA   =          110
14167  deg
 ZDOT =      -1346
100084                 TA   =          169
67775
                                          MA   =          169
64782
                                          Ha   =            187
131  n
mi
                                          Hp   =            180
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14142527
33                 X    =         4335493
99
 Y    =         -29953
06  feet           Y    =           39213
39  meter
 Z    =      -16931376
01                 Z    =        -5139681
71
 XDOT =      -5225
475747                 XDOT =       -1668
879695
 YDOT =      24297
089976  feet/sec       YDOT =        7387
516491  meter/sec
 ZDOT =      -4416
338858                 ZDOT =       -1354
022491

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13267165
77                 X    =        -4043832
13
 Y    =        5166648
13  feet           Y    =         1574794
35  meter
 Z    =      -16851454
82                 Z    =        -5136323
43
 XDOT =      -3542
779240                 XDOT =       -1079
839112
 YDOT =     -23568
883731  feet/sec       YDOT =       -7183
795761  meter/sec
 ZDOT =      -4445
608916                 ZDOT =       -1355
021597


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   07306
46418608  
00020000  00000-0  20000-3 0  9079
2 25544  51
6334 110
8650 0001980 160
3998 199
7243 15
76165796 32596


Satellite: ISS
Catalog Number: 25544
Epoch time:      07306
46418608   =   yrday
fracday
Element set:     907
Inclination:       51
6334  deg
RA of node:       110
8650  deg
Eccentricity:     
0001980     
Arg of perigee:   160
3998  deg
Mean anomaly:     199
7243  deg
Mean motion:   15
76165796  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3259
Checksum:              317


Coasting Arc #9 (Orbit 3274)
---------------------------------------

Vector Time (GMT): 2007/307/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1403864
60                 A    =         6725724
37  meter
 Y    =       -6555670
14  meter          E    =           
0014446
 Z    =         434767
08                 I    =           51
96566
 XDOT =       4736
567162                 Wp   =          134
31179
 YDOT =        605
661402  meter/sec      RA   =          104
99481  deg
 ZDOT =      -6049
191297                 TA   =           40
97545
                                          MA   =           40
86699
                                          Ha   =            186
905  n
mi
                                          Hp   =            180
163

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4605855
00                 X    =         1474954
71
 Y    =      -21508104
13  feet           Y    =        -6539573
84  meter
 Z    =        1426401
19                 Z    =          441759
83
 XDOT =      15539
918512                 XDOT =        4758
828792
 YDOT =       1987
078089  feet/sec       YDOT =         658
752842  meter/sec
 ZDOT =     -19846
428139                 ZDOT =       -6026
126682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3848111
29                 X    =         1172904
32
 Y    =       21654794
11  feet           Y    =         6600381
24  meter
 Z    =        1452238
08                 Z    =          442642
17
 XDOT =     -13667
014473                 XDOT =       -4165
706011
 YDOT =       3778
087841  feet/sec       YDOT =        1151
561174  meter/sec
 ZDOT =     -19758
579413                 ZDOT =       -6022
415005


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   07307
47861058  
00020000  00000-0  20000-3 0  9083
2 25544  51
6339 105
6376 0001662 165
7420 194
3791 15
76242092 32756


Satellite: ISS
Catalog Number: 25544
Epoch time:      07307
47861058   =   yrday
fracday
Element set:     908
Inclination:       51
6339  deg
RA of node:       105
6376  deg
Eccentricity:     
0001662     
Arg of perigee:   165
7420  deg
Mean anomaly:     194
3791  deg
Mean motion:   15
76242092  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3275
Checksum:              301


Coasting Arc #10 (Orbit 3290)
---------------------------------------

Vector Time (GMT): 2007/308/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4004027
67                 A    =         6713934
65  meter
 Y    =       -1090835
72  meter          E    =           
0003185
 Z    =        5275186
02                 I    =           51
93070
 XDOT =       1589
889046                 Wp   =          112
15203
 YDOT =      -7533
476670  meter/sec      RA   =           99
86464  deg
 ZDOT =       -352
052423                 TA   =          341
16823
                                          MA   =          341
18000
                                          Ha   =            187
185  n
mi
                                          Hp   =            180
218

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13136573
73                 X    =        -4017158
52
 Y    =       -3578857
35  feet           Y    =        -1135684
38  meter
 Z    =       17307040
73                 Z    =         5255702
25
 XDOT =       5216
171411                 XDOT =        1675
721589
 YDOT =     -24716
130806  feet/sec       YDOT =       -7515
217720  meter/sec
 ZDOT =      -1155
027635                 ZDOT =        -344
120027

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13575977
27                 X    =         4137957
87
 Y    =       -1906894
59  feet           Y    =         -581221
47  meter
 Z    =       17232760
73                 Z    =         5252545
47
 XDOT =       4766
442883                 XDOT =        1452
811791
 YDOT =      23791
035163  feet/sec       YDOT =        7251
507518  meter/sec
 ZDOT =      -1125
724922                 ZDOT =        -343
120956


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   07308
49302051  
00020000  00000-0  20000-3 0  9090
2 25544  51
6330 100
4095 0001957 165
2770 194
8452 15
76178006 32918


Satellite: ISS
Catalog Number: 25544
Epoch time:      07308
49302051   =   yrday
fracday
Element set:     909
Inclination:       51
6330  deg
RA of node:       100
4095  deg
Eccentricity:     
0001957     
Arg of perigee:   165
2770  deg
Mean anomaly:     194
8452  deg
Mean motion:   15
76178006  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3291
Checksum:              280


Coasting Arc #11 (Orbit 3306)
---------------------------------------

Vector Time (GMT): 2007/309/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1366011
44                 A    =         6725294
41  meter
 Y    =        6494754
15  meter          E    =           
0013093
 Z    =        1053565
58                 I    =           51
97369
 XDOT =      -4506
869337                 Wp   =           64
22700
 YDOT =      -1920
848025  meter/sec      RA   =           94
74640  deg
 ZDOT =       5946
553751                 TA   =          307
25325
                                          MA   =          307
37260
                                          Ha   =            186
884  n
mi
                                          Hp   =            180
181

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4481664
81                 X    =        -1443653
37
 Y    =       21308248
53  feet           Y    =         6479044
54  meter
 Z    =        3456580
00                 Z    =         1046740
65
 XDOT =     -14786
316723                 XDOT =       -4513
943047
 YDOT =      -6301
994834  feet/sec       YDOT =       -1971
285841  meter/sec
 ZDOT =      19509
690785                 ZDOT =        5924
641776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4597294
43                 X    =        -1401255
34
 Y    =      -21287680
67  feet           Y    =        -6488485
07  meter
 Z    =        3431363
53                 Z    =         1045879
60
 XDOT =      14618
475821                 XDOT =        4455
711430
 YDOT =          1
542087  feet/sec       YDOT =            
470028  meter/sec
 ZDOT =      19426
071994                 ZDOT =        5921
066744


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   07309
50740702  
00020000  00000-0  20000-3 0  9104
2 25544  51
6333  95
1814 0001982 171
0805 189
0395 15
76257010 33075


Satellite: ISS
Catalog Number: 25544
Epoch time:      07309
50740702   =   yrday
fracday
Element set:     910
Inclination:       51
6333  deg
RA of node:        95
1814  deg
Eccentricity:     
0001982     
Arg of perigee:   171
0805  deg
Mean anomaly:     189
0395  deg
Mean motion:   15
76257010  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3307
Checksum:              271


Coasting Arc #12 (Orbit 3321)
---------------------------------------

Vector Time (GMT): 2007/310/10:42:16
349
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3912974
86                 A    =         6715016
74  meter
 Y    =        2266046
96  meter          E    =           
0013769
 Z    =       -4976867
69                 I    =           51
94100
 XDOT =      -1565
923549                 Wp   =          112
81802
 YDOT =       7243
929613  meter/sec      RA   =           89
58888  deg
 ZDOT =       2066
378653                 TA   =          177
12973
                                          MA   =          177
12182
                                          Ha   =            186
828  n
mi
                                          Hp   =            180
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12837844
03                 X    =         3911522
10
 Y    =        7434537
26  feet           Y    =         2309795
87  meter
 Z    =      -16328306
06                 Z    =        -4957861
53
 XDOT =      -5137
544452                 XDOT =       -1656
848228
 YDOT =      23766
173272  feet/sec       YDOT =        7225
910209  meter/sec
 ZDOT =       6779
457523                 ZDOT =        2058
550251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14862397
89                 X    =        -4530058
88
 Y    =       -1247895
38  feet           Y    =         -380358
51  meter
 Z    =      -16255708
19                 Z    =        -4954739
86
 XDOT =      -5485
534510                 XDOT =       -1671
990919
 YDOT =     -22633
639164  feet/sec       YDOT =       -6898
733217  meter/sec
 ZDOT =       6750
500185                 ZDOT =        2057
552456


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   07310
45837846  
00020000  00000-0  20000-3 0  9117
2 25544  51
6340  90
2806 0001986 171
4985 188
6213 15
76279884 33221


Satellite: ISS
Catalog Number: 25544
Epoch time:      07310
45837846   =   yrday
fracday
Element set:     911
Inclination:       51
6340  deg
RA of node:        90
2806  deg
Eccentricity:     
0001986     
Arg of perigee:   171
4985  deg
Mean anomaly:     188
6213  deg
Mean motion:   15
76279884  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3322
Checksum:              310

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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