Date: October 17th 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) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2976)
---------------------------------------

Vector Time (GMT): 2007/288/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4711972
13                 A    =         6718854
74  meter
 Y    =       -1862051
26  meter          E    =           
0011642
 Z    =        4405000
93                 I    =           51
50628
 XDOT =       5000
907183                 Wp   =           74
08116
 YDOT =       4859
788873  meter/sec      RA   =          202
17986  deg
 ZDOT =      -3284
801661                 TA   =           48
95750
                                          MA   =           48
85694
                                          Ha   =            188
397  n
mi
                                          Hp   =            180
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15459226
15                 X    =         4711044
39
 Y    =       -6109092
06  feet           Y    =        -1809364
53  meter
 Z    =       14452102
78                 Z    =         4427890
03
 XDOT =      16407
175796                 XDOT =        4962
150010
 YDOT =      15944
189217  feet/sec       YDOT =        4915
495161  meter/sec
 ZDOT =     -10776
908336                 ZDOT =       -3260
600727

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8511196
43                 X    =        -2594212
67
 Y    =       14189927
26  feet           Y    =         4325089
83  meter
 Z    =       14538825
72                 Z    =         4431434
08
 XDOT =     -21730
431092                 XDOT =       -6623
435397
 YDOT =      -2052
546914  feet/sec       YDOT =        -625
616299  meter/sec
 ZDOT =     -10684
338936                 ZDOT =       -3256
586508


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   07288
58195589  
00020000  00000-0  20000-3 0  9004
2 25544  51
6369 202
9651 0002664  92
1784 267
9685 15
75671407 29777


Satellite: ISS
Catalog Number: 25544
Epoch time:      07288
58195589   =   yrday
fracday
Element set:     900
Inclination:       51
6369  deg
RA of node:       202
9651  deg
Eccentricity:     
0002664     
Arg of perigee:    92
1784  deg
Mean anomaly:     267
9685  deg
Mean motion:   15
75671407  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2977
Checksum:              343


Coasting Arc #2 (Orbit 2992)
---------------------------------------

Vector Time (GMT): 2007/289/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4208427
90                 A    =         6722685
09  meter
 Y    =       -4048429
36  meter          E    =           
0015395
 Z    =        3317571
54                 I    =           51
54658
 XDOT =       5745
213067                 Wp   =           90
15445
 YDOT =      -2122
576048  meter/sec      RA   =          197
07249  deg
 ZDOT =       4679
116208                 TA   =          308
95279
                                          MA   =          309
08988
                                          Ha   =            188
544  n
mi
                                          Hp   =            180
251

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13807178
15                 X    =        -4178961
52
 Y    =      -13282248
54  feet           Y    =        -4095325
68  meter
 Z    =       10884421
06                 Z    =         3297198
01
 XDOT =      18849
124236                 XDOT =        5745
790188
 YDOT =      -6963
832177  feet/sec       YDOT =       -2058
326681  meter/sec
 ZDOT =      15351
431128                 ZDOT =        4707
028483

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19117542
59                 X    =         5827026
98
 Y    =        1807278
08  feet           Y    =          550858
36  meter
 Z    =       10806490
09                 Z    =         3293818
18
 XDOT =     -10257
543452                 XDOT =       -3126
499244
 YDOT =      15711
104252  feet/sec       YDOT =        4788
744576  meter/sec
 ZDOT =      15457
217079                 ZDOT =        4711
359766


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   07289
59670986  
00020000  00000-0  20000-3 0  9016
2 25544  51
6372 197
7402 0002668  95
9600 264
1868 15
75677226 29933


Satellite: ISS
Catalog Number: 25544
Epoch time:      07289
59670986   =   yrday
fracday
Element set:     901
Inclination:       51
6372  deg
RA of node:       197
7402  deg
Eccentricity:     
0002668     
Arg of perigee:    95
9600  deg
Mean anomaly:     264
1868  deg
Mean motion:   15
75677226  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2993
Checksum:              341


Coasting Arc #3 (Orbit 3007)
---------------------------------------

Vector Time (GMT): 2007/290/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5297844
18                 A    =         6721267
62  meter
 Y    =        1880570
50  meter          E    =           
0008425
 Z    =       -3692587
17                 I    =           51
57067
 XDOT =      -4573
463280                 Wp   =          101
98525
 YDOT =      -4449
103953  meter/sec      RA   =          191
86649  deg
 ZDOT =       4302
333370                 TA   =          213
52214
                                          MA   =          213
57548
                                          Ha   =            188
347  n
mi
                                          Hp   =            180
147

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17381378
53                 X    =        -5300540
96
 Y    =        6169850
72  feet           Y    =         1821312
01  meter
 Z    =      -12114787
30                 Z    =        -3718331
13
 XDOT =     -15004
800788                 XDOT =       -4544
273203
 YDOT =     -14596
797747  feet/sec       YDOT =       -4500
083896  meter/sec
 ZDOT =      14115
266963                 ZDOT =        4280
185834

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9476083
88                 X    =         2888310
37
 Y    =      -15748305
79  feet           Y    =        -4800083
61  meter
 Z    =      -12212376
84                 Z    =        -3722332
46
 XDOT =      19771
073770                 XDOT =        6026
223285
 YDOT =       1032
845909  feet/sec       YDOT =         314
811433  meter/sec
 ZDOT =      14030
534764                 ZDOT =        4276
506996


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   07290
54802385  
00020000  00000-0  20000-3 0  9024
2 25544  51
6373 192
8421 0002508  99
2589 260
8858 15
75714901 30089


Satellite: ISS
Catalog Number: 25544
Epoch time:      07290
54802385   =   yrday
fracday
Element set:     902
Inclination:       51
6373  deg
RA of node:       192
8421  deg
Eccentricity:     
0002508     
Arg of perigee:    99
2589  deg
Mean anomaly:     260
8858  deg
Mean motion:   15
75714901  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3008
Checksum:              305


Coasting Arc #4 (Orbit 3023)
---------------------------------------

Vector Time (GMT): 2007/291/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3713104
93                 A    =         6719774
03  meter
 Y    =        3761144
78  meter          E    =           
0009912
 Z    =       -4159622
16                 I    =           51
59413
 XDOT =      -6374
717328                 Wp   =           78
14495
 YDOT =       2201
651473  meter/sec      RA   =          186
76493  deg
 ZDOT =      -3705
095506                 TA   =          153
96834
                                          MA   =          153
91846
                                          Ha   =            188
281  n
mi
                                          Hp   =            180
322

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12182102
78                 X    =         3690978
31
 Y    =       12339713
85  feet           Y    =         3802543
19  meter
 Z    =      -13647054
34                 Z    =        -4141637
27
 XDOT =     -20914
426930                 XDOT =       -6380
863754
 YDOT =       7223
265989  feet/sec       YDOT =        2130
331484  meter/sec
 ZDOT =     -12155
825152                 ZDOT =       -3736
079290

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17331466
43                 X    =        -5282630
97
 Y    =       -1471892
13  feet           Y    =         -448632
72  meter
 Z    =      -13578220
18                 Z    =        -4138641
51
 XDOT =      11107
577374                 XDOT =        3385
589584
 YDOT =     -17734
718127  feet/sec       YDOT =       -5405
542085  meter/sec
 ZDOT =     -12273
298952                 ZDOT =       -3740
901521


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   07291
56274154  
00020000  00000-0  20000-3 0  9035
2 25544  51
6373 187
6170 0002369 103
6891 256
4537 15
75741180 30245


Satellite: ISS
Catalog Number: 25544
Epoch time:      07291
56274154   =   yrday
fracday
Element set:     903
Inclination:       51
6373  deg
RA of node:       187
6170  deg
Eccentricity:     
0002369     
Arg of perigee:   103
6891  deg
Mean anomaly:     256
4537  deg
Mean motion:   15
75741180  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3024
Checksum:              292


Coasting Arc #5 (Orbit 3039)
---------------------------------------

Vector Time (GMT): 2007/292/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5796443
77                 A    =         6723811
91  meter
 Y    =       -2007470
83  meter          E    =           
0016085
 Z    =        2735315
12                 I    =           51
63713
 XDOT =       3898
102333                 Wp   =          101
56819
 YDOT =       4193
097487  meter/sec      RA   =          181
56571  deg
 ZDOT =      -5160
881940                 TA   =           47
14005
                                          MA   =           47
00505
                                          Ha   =            188
215  n
mi
                                          Hp   =            180
145

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19017203
96                 X    =         5805172
95
 Y    =       -6586190
38  feet           Y    =        -1942602
93  meter
 Z    =        8974130
97                 Z    =         2763495
82
 XDOT =      12789
049650                 XDOT =        3875
995751
 YDOT =      13756
881518  feet/sec       YDOT =        4236
564711  meter/sec
 ZDOT =     -16932
027363                 ZDOT =       -5141
998358

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9895692
75                 X    =        -3016207
15
 Y    =       17469341
90  feet           Y    =         5324655
41  meter
 Z    =        9080987
59                 Z    =         2767885
02
 XDOT =     -17485
773534                 XDOT =       -5329
663773
 YDOT =      -1103
344675  feet/sec       YDOT =        -336
299457  meter/sec
 ZDOT =     -16859
712859                 ZDOT =       -5138
840479


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   07292
57744221  
00020000  00000-0  20000-3 0  9045
2 25544  51
6372 182
3921 0002515 106
1995 253
9446 15
75769355 30409


Satellite: ISS
Catalog Number: 25544
Epoch time:      07292
57744221   =   yrday
fracday
Element set:     904
Inclination:       51
6372  deg
RA of node:       182
3921  deg
Eccentricity:     
0002515     
Arg of perigee:   106
1995  deg
Mean anomaly:     253
9446  deg
Mean motion:   15
75769355  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3040
Checksum:              296


Coasting Arc #6 (Orbit 3055)
---------------------------------------

Vector Time (GMT): 2007/293/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3046595
97                 A    =         6717212
90  meter
 Y    =       -3599648
04  meter          E    =           
0009769
 Z    =        4777834
66                 I    =           51
64380
 XDOT =       6860
972465                 Wp   =          117
40589
 YDOT =      -2433
149358  meter/sec      RA   =          176
45941  deg
 ZDOT =       2533
406208                 TA   =          307
76947
                                          MA   =          307
85792
                                          Ha   =            188
283  n
mi
                                          Hp   =            180
205

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9995393
61                 X    =        -3029327
88
 Y    =      -11809868
91  feet           Y    =        -3633620
21  meter
 Z    =       15675310
56                 Z    =         4763076
09
 XDOT =      22509
752183                 XDOT =        6875
363399
 YDOT =      -7982
773483  feet/sec       YDOT =       -2356
345592  meter/sec
 ZDOT =       8311
700158                 ZDOT =        2566
772209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15406482
45                 X    =         4695895
85
 Y    =        1947149
56  feet           Y    =          593491
19  meter
 Z    =       15618744
04                 Z    =         4760593
18
 XDOT =     -11097
397248                 XDOT =       -3382
486681
 YDOT =      19899
637978  feet/sec       YDOT =        6065
409656  meter/sec
 ZDOT =       8438
222730                 ZDOT =        2571
970288


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   07293
59212390  
00020000  00000-0  20000-3 0  9056
2 25544  51
6373 177
1666 0002417 109
4573 250
6852 15
75784062 30561


Satellite: ISS
Catalog Number: 25544
Epoch time:      07293
59212390   =   yrday
fracday
Element set:     905
Inclination:       51
6373  deg
RA of node:       177
1666  deg
Eccentricity:     
0002417     
Arg of perigee:   109
4573  deg
Mean anomaly:     250
6852  deg
Mean motion:   15
75784062  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3056
Checksum:              299


Coasting Arc #7 (Orbit 3070)
---------------------------------------

Vector Time (GMT): 2007/294/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6120196
59                 A    =         6725775
00  meter
 Y    =        2249809
29  meter          E    =           
0008604
 Z    =       -1640536
40                 I    =           51
70168
 XDOT =      -3048
664719                 Wp   =           52
22973
 YDOT =      -4122
486296  meter/sec      RA   =          171
27636  deg
 ZDOT =       5745
414308                 TA   =          289
65710
                                          MA   =          289
74993
                                          Ha   =            188
028  n
mi
                                          Hp   =            180
219

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20079385
13                 X    =        -6136929
89
 Y    =        7381264
08  feet           Y    =         2181276
18  meter
 Z    =       -5382337
28                 Z    =        -1670309
42
 XDOT =     -10002
180835                 XDOT =       -3030
250424
 YDOT =     -13525
217507  feet/sec       YDOT =       -4156
475050  meter/sec
 ZDOT =      18849
784475                 ZDOT =        5730
648561

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9531591
00                 X    =         2905228
94
 Y    =      -19120290
34  feet           Y    =        -5827864
50  meter
 Z    =       -5495233
55                 Z    =        -1674947
19
 XDOT =      15237
614621                 XDOT =        4644
424936
 YDOT =       2218
460266  feet/sec       YDOT =         676
186689  meter/sec
 ZDOT =      18793
116575                 ZDOT =        5728
141932


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   07294
54337078  
00020000  00000-0  20000-3 0  9064
2 25544  51
6369 172
2675 0002188 113
2192 246
9203 15
75819389 30713


Satellite: ISS
Catalog Number: 25544
Epoch time:      07294
54337078   =   yrday
fracday
Element set:     906
Inclination:       51
6369  deg
RA of node:       172
2675  deg
Eccentricity:     
0002188     
Arg of perigee:   113
2192  deg
Mean anomaly:     246
9203  deg
Mean motion:   15
75819389  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3071
Checksum:              309


Coasting Arc #8 (Orbit 3086)
---------------------------------------

Vector Time (GMT): 2007/295/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2239781
41                 A    =         6715278
82  meter
 Y    =        3661144
71  meter          E    =           
0016075
 Z    =       -5178650
26                 I    =           51
69403
 XDOT =      -7107
304959                 Wp   =           85
75369
 YDOT =       2700
624983  meter/sec      RA   =          166
15584  deg
 ZDOT =      -1166
601025                 TA   =          173
11360
                                          MA   =          173
09148
                                          Ha   =            187
954  n
mi
                                          Hp   =            180
259

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7348364
19                 X    =         2223832
82
 Y    =       12011629
62  feet           Y    =         3686101
77  meter
 Z    =      -16990322
37                 Z    =        -5167808
16
 XDOT =     -23317
929655                 XDOT =       -7131
308293
 YDOT =       8860
318186  feet/sec       YDOT =        2621
012804  meter/sec
 ZDOT =      -3827
431186                 ZDOT =       -1201
187308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13715337
67                 X    =        -4180434
92
 Y    =       -3403279
94  feet           Y    =        -1037319
73  meter
 Z    =      -16948626
94                 Z    =        -5165941
49
 XDOT =      10245
489980                 XDOT =        3122
825346
 YDOT =     -21607
229402  feet/sec       YDOT =       -6585
883522  meter/sec
 ZDOT =      -3958
575240                 ZDOT =       -1206
573733


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   07295
55801741  
00020000  00000-0  20000-3 0  9070
2 25544  51
6360 167
0415 0002152 117
8009 242
3374 15
75864209 30873


Satellite: ISS
Catalog Number: 25544
Epoch time:      07295
55801741   =   yrday
fracday
Element set:     907
Inclination:       51
6360  deg
RA of node:       167
0415  deg
Eccentricity:     
0002152     
Arg of perigee:   117
8009  deg
Mean anomaly:     242
3374  deg
Mean motion:   15
75864209  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3087
Checksum:              285


Coasting Arc #9 (Orbit 3102)
---------------------------------------

Vector Time (GMT): 2007/296/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6240277
01                 A    =         6726811
75  meter
 Y    =       -2463791
70  meter          E    =           
0015206
 Z    =         377912
27                 I    =           51
76097
 XDOT =       2078
408768                 Wp   =          130
00975
 YDOT =       4315
345537  meter/sec      RA   =          160
99897  deg
 ZDOT =      -6036
492035                 TA   =           45
88418
                                          MA   =           45
75918
                                          Ha   =            187
960  n
mi
                                          Hp   =            180
211

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20473349
76                 X    =         6265527
83
 Y    =       -8083306
09  feet           Y    =        -2393868
17  meter
 Z    =        1239869
64                 Z    =          408289
66
 XDOT =       6818
926404                 XDOT =        2059
324259
 YDOT =      14157
957799  feet/sec       YDOT =        4338
480388  meter/sec
 ZDOT =     -19804
763895                 ZDOT =       -6026
441547

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8663287
32                 X    =        -2640569
97
 Y    =       20227369
10  feet           Y    =         6165302
10  meter
 Z    =        1355048
52                 Z    =          413018
79
 XDOT =     -13459
989395                 XDOT =       -4102
604768
 YDOT =      -4410
659824  feet/sec       YDOT =       -1344
369114  meter/sec
 ZDOT =     -19765
991892                 ZDOT =       -6024
674329


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   07296
57264725  
00020000  00000-0  20000-3 0  9089
2 25544  51
6362 161
8165 0002214 123
3914 236
7462 15
75862982 31035


Satellite: ISS
Catalog Number: 25544
Epoch time:      07296
57264725   =   yrday
fracday
Element set:     908
Inclination:       51
6362  deg
RA of node:       161
8165  deg
Eccentricity:     
0002214     
Arg of perigee:   123
3914  deg
Mean anomaly:     236
7462  deg
Mean motion:   15
75862982  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3103
Checksum:              296


Coasting Arc #10 (Orbit 3118)
---------------------------------------

Vector Time (GMT): 2007/297/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1398458
14                 A    =         6714720
82  meter
 Y    =       -3921737
33  meter          E    =           
0004178
 Z    =        5264453
36                 I    =           51
74645
 XDOT =       7120
734376                 Wp   =          100
87651
 YDOT =      -2935
789002  meter/sec      RA   =          155
85781  deg
 ZDOT =       -296
019381                 TA   =          351
92335
                                          MA   =          351
93008
                                          Ha   =            187
905  n
mi
                                          Hp   =            180
234

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4588117
27                 X    =        -1380075
21
 Y    =      -12866592
28  feet           Y    =        -3937272
57  meter
 Z    =       17271828
61                 Z    =         5257704
36
 XDOT =      23361
989422                 XDOT =        7154
471625
 YDOT =      -9631
853682  feet/sec       YDOT =       -2855
972301  meter/sec
 ZDOT =       -971
192194                 ZDOT =        -261
343780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12534181
30                 X    =         3820418
46
 Y    =        5513395
15  feet           Y    =         1680482
84  meter
 Z    =       17245661
88                 Z    =         5256477
74
 XDOT =      -8799
621940                 XDOT =       -2682
124767
 YDOT =      22625
801733  feet/sec       YDOT =        6896
344368  meter/sec
 ZDOT =       -839
724612                 ZDOT =        -255
948062


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   07297
58725784  
00020000  00000-0  20000-3 0  9099
2 25544  51
6352 156
5901 0002125 127
2199 232
9160 15
75895031 31193


Satellite: ISS
Catalog Number: 25544
Epoch time:      07297
58725784   =   yrday
fracday
Element set:     909
Inclination:       51
6352  deg
RA of node:       156
5901  deg
Eccentricity:     
0002125     
Arg of perigee:   127
2199  deg
Mean anomaly:     232
9160  deg
Mean motion:   15
75895031  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3119
Checksum:              304


Coasting Arc #11 (Orbit 3134)
---------------------------------------

Vector Time (GMT): 2007/298/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6122943
91                 A    =         6726339
96  meter
 Y    =        2620055
53  meter          E    =           
0014190
 Z    =         900598
05                 I    =           51
81038
 XDOT =      -1141
274024                 Wp   =           62
77094
 YDOT =      -4740
090660  meter/sec      RA   =          150
72730  deg
 ZDOT =       5965
757017                 TA   =          307
04583
                                          MA   =          307
17553
                                          Ha   =            187
738  n
mi
                                          Hp   =            180
252

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20088398
67                 X    =        -6156161
78
 Y    =        8595982
71  feet           Y    =         2551399
61  meter
 Z    =        2954718
01                 Z    =          870771
01
 XDOT =      -3744
337348                 XDOT =       -1117
166325
 YDOT =     -15551
478543  feet/sec       YDOT =       -4752
718006  meter/sec
 ZDOT =      19572
693624                 ZDOT =        5960
271269

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7340683
49                 X    =         2237440
33
 Y    =      -20596225
55  feet           Y    =        -6277729
55  meter
 Z    =        2841636
37                 Z    =          866130
77
 XDOT =      12532
199301                 XDOT =        3819
814347
 YDOT =       7194
672757  feet/sec       YDOT =        2192
936256  meter/sec
 ZDOT =      19551
229753                 ZDOT =        5959
214829


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   07298
60184998  
00020000  00000-0  20000-3 0  9101
2 25544  51
6337 151
3631 0002070 132
3916 227
7424 15
75941707 31357


Satellite: ISS
Catalog Number: 25544
Epoch time:      07298
60184998   =   yrday
fracday
Element set:     910
Inclination:       51
6337  deg
RA of node:       151
3631  deg
Eccentricity:     
0002070     
Arg of perigee:   132
3916  deg
Mean anomaly:     227
7424  deg
Mean motion:   15
75941707  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3135
Checksum:              290


Coasting Arc #12 (Orbit 3149)
---------------------------------------

Vector Time (GMT): 2007/299/12:57:44
867
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         611155
15                 A    =         6715514
39  meter
 Y    =        4399865
11  meter          E    =           
0015312
 Z    =       -5050150
37                 I    =           51
79756
 XDOT =      -6855
651108                 Wp   =          107
70155
 YDOT =       2999
060888  meter/sec      RA   =          145
56398  deg
 ZDOT =       1783
083983                 TA   =          179
45505
                                          MA   =          179
45338
                                          Ha   =            187
683  n
mi
                                          Hp   =            180
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2005102
20                 X    =          586443
38
 Y    =       14435252
98  feet           Y    =         4406561
20  meter
 Z    =      -16568734
81                 Z    =        -5047241
32
 XDOT =     -22492
293661                 XDOT =       -6897
339738
 YDOT =       9839
438609  feet/sec       YDOT =        2922
164031  meter/sec
 ZDOT =       5850
013067                 ZDOT =        1749
676751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12162539
44                 X    =        -3707142
02
 Y    =       -8053221
63  feet           Y    =        -2454621
95  meter
 Z    =      -16557119
08                 Z    =        -5046609
90
 XDOT =       7083
324747                 XDOT =        2158
997383
 YDOT =     -22465
737933  feet/sec       YDOT =       -6847
556922  meter/sec
 ZDOT =       5723
352407                 ZDOT =        1744
477814


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
55301459  
00020000  00000-0  20000-3 0  9110
2 25544  51
6324 146
4623 0002127 135
2586 224
8750 15
75966730 31507


Satellite: ISS
Catalog Number: 25544
Epoch time:      07299
55301459   =   yrday
fracday
Element set:     911
Inclination:       51
6324  deg
RA of node:       146
4623  deg
Eccentricity:     
0002127     
Arg of perigee:   135
2586  deg
Mean anomaly:     224
8750  deg
Mean motion:   15
75966730  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3150
Checksum:              289

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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