Date: November 21st 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8718 77 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 3527)
---------------------------------------

Vector Time (GMT): 2007/323/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5658645
99                 A    =         6719897
16  meter
 Y    =        -692047
70  meter          E    =           
0005230
 Z    =       -3563786
44                 I    =           51
76587
 XDOT =       3449
503617                 Wp   =          112
40954
 YDOT =       5238
457642  meter/sec      RA   =           22
53492  deg
 ZDOT =       4463
164454                 TA   =          205
14838
                                          MA   =          205
17386
                                          Ha   =            186
342  n
mi
                                          Hp   =            180
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18565111
53                 X    =         5683276
57
 Y    =       -2270497
71  feet           Y    =         -628631
70  meter
 Z    =      -11692212
71                 Z    =        -3536236
40
 XDOT =      11317
269086                 XDOT =        3368
988355
 YDOT =      17186
540821  feet/sec       YDOT =        5276
581643  meter/sec
 ZDOT =      14642
928000                 ZDOT =        4479
727028

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6615950
76                 X    =        -2016541
79
 Y    =       17563827
69  feet           Y    =         5353454
68  meter
 Z    =      -11587386
09                 Z    =        -3531835
28
 XDOT =     -19154
496335                 XDOT =       -5838
290483
 YDOT =       2480
161611  feet/sec       YDOT =         755
953259  meter/sec
 ZDOT =      14706
526749                 ZDOT =        4482
549353


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   07323
52130675  
00020000  00000-0  20000-3 0  9003
2 25544  51
6406  23
0283 0001500 196
0205 164
0912 15
76407082 35282


Satellite: ISS
Catalog Number: 25544
Epoch time:      07323
52130675   =   yrday
fracday
Element set:     900
Inclination:       51
6406  deg
RA of node:        23
0283  deg
Eccentricity:     
0001500     
Arg of perigee:   196
0205  deg
Mean anomaly:     164
0912  deg
Mean motion:   15
76407082  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3528
Checksum:              247


Coasting Arc #2 (Orbit 3543)
---------------------------------------

Vector Time (GMT): 2007/324/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2496286
49                 A    =         6716834
70  meter
 Y    =       -4424573
96  meter          E    =           
0008574
 Z    =       -4402331
92                 I    =           51
72905
 XDOT =       6912
783248                 Wp   =           76
00659
 YDOT =       -585
862868  meter/sec      RA   =           17
43843  deg
 ZDOT =      -3334
346318                 TA   =          160
52151
                                          MA   =          160
48873
                                          Ha   =            186
280  n
mi
                                          Hp   =            180
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8189916
30                 X    =        -2425238
46
 Y    =      -14516318
78  feet           Y    =        -4452091
50  meter
 Z    =      -14443346
20                 Z    =        -4414286
70
 XDOT =      22679
735066                 XDOT =        6935
018719
 YDOT =      -1922
122269  feet/sec       YDOT =        -508
435805  meter/sec
 ZDOT =     -10939
456425                 ZDOT =       -3300
709213

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16610435
62                 X    =         5062860
78
 Y    =        -749464
24  feet           Y    =         -228436
70  meter
 Z    =      -14489314
04                 Z    =        -4416342
92
 XDOT =      -8519
617710                 XDOT =       -2596
779478
 YDOT =      19982
937016  feet/sec       YDOT =        6090
799202  meter/sec
 ZDOT =     -10811
445033                 ZDOT =       -3295
328446


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   07324
53559079  
00020000  00000-0  20000-3 0  9019
2 25544  51
6412  17
8005 0001402 200
0042 160
1067 15
76409068 35440


Satellite: ISS
Catalog Number: 25544
Epoch time:      07324
53559079   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:        17
8005  deg
Eccentricity:     
0001402     
Arg of perigee:   200
0042  deg
Mean anomaly:     160
1067  deg
Mean motion:   15
76409068  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3544
Checksum:              251


Coasting Arc #3 (Orbit 3559)
---------------------------------------

Vector Time (GMT): 2007/325/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6340822
37                 A    =         6723111
21  meter
 Y    =         383889
38  meter          E    =           
0013980
 Z    =        2179981
26                 I    =           51
72276
 XDOT =      -2199
047056                 Wp   =          113
95803
 YDOT =      -4924
254240  meter/sec      RA   =           12
24728  deg
 ZDOT =      -5507
103735                 TA   =           41
61832
                                          MA   =           41
51201
                                          Ha   =            186
179  n
mi
                                          Hp   =            180
171

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20803223
00                 X    =        -6355234
08
 Y    =        1259479
59  feet           Y    =          312902
05  meter
 Z    =        7152169
48                 Z    =         2149141
65
 XDOT =      -7214
721313                 XDOT =       -2117
066564
 YDOT =     -16155
689764  feet/sec       YDOT =       -4948
386662  meter/sec
 ZDOT =     -18067
925641                 ZDOT =       -5517
588054

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7876097
55                 X    =         2400634
53
 Y    =      -19338890
97  feet           Y    =        -5894493
97  meter
 Z    =        7034791
23                 Z    =         2144204
37
 XDOT =      16232
628352                 XDOT =        4947
705122
 YDOT =         -2
867639  feet/sec       YDOT =           -
874056  meter/sec
 ZDOT =     -18108
340210                 ZDOT =       -5519
422096


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   07325
54984845  
00020000  00000-0  20000-3 0  9025
2 25544  51
6413  12
5732 0001180 206
9938 153
1166 15
76486275 35607


Satellite: ISS
Catalog Number: 25544
Epoch time:      07325
54984845   =   yrday
fracday
Element set:     902
Inclination:       51
6413  deg
RA of node:        12
5732  deg
Eccentricity:     
0001180     
Arg of perigee:   206
9938  deg
Mean anomaly:     153
1166  deg
Mean motion:   15
76486275  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3560
Checksum:              294


Coasting Arc #4 (Orbit 3575)
---------------------------------------

Vector Time (GMT): 2007/326/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1271023
85                 A    =         6713771
10  meter
 Y    =        4204200
98  meter          E    =           
0005221
 Z    =        5075686
80                 I    =           51
66247
 XDOT =      -7531
006779                 Wp   =          137
68383
 YDOT =        335
642670  meter/sec      RA   =            7
12973  deg
 ZDOT =       1603
113796                 TA   =          296
91135
                                          MA   =          296
96468
                                          Ha   =            186
097  n
mi
                                          Hp   =            180
078

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4170025
75                 X    =         1199259
79
 Y    =       13793310
30  feet           Y    =         4218012
72  meter
 Z    =       16652515
74                 Z    =         5081687
58
 XDOT =     -24708
027489                 XDOT =       -7541
988153
 YDOT =       1101
189863  feet/sec       YDOT =         251
365185  meter/sec
 ZDOT =       5259
559699                 ZDOT =        1566
500299

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14237015
24                 X    =        -4339442
25
 Y    =       -2043650
85  feet           Y    =         -622904
78  meter
 Z    =       16675781
61                 Z    =         5082778
24
 XDOT =       9160
125628                 XDOT =        2792
006292
 YDOT =     -21907
092895  feet/sec       YDOT =       -6677
281915  meter/sec
 ZDOT =       5120
194334                 ZDOT =        1560
635233


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   07326
56408298  
00020000  00000-0  20000-3 0  9032
2 25544  51
6408   7
3457 0001145 203
5193 156
5920 15
76506212 35760


Satellite: ISS
Catalog Number: 25544
Epoch time:      07326
56408298   =   yrday
fracday
Element set:     903
Inclination:       51
6408  deg
RA of node:         7
3457  deg
Eccentricity:     
0001145     
Arg of perigee:   203
5193  deg
Mean anomaly:     156
5920  deg
Mean motion:   15
76506212  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3576
Checksum:              284


Coasting Arc #5 (Orbit 3590)
---------------------------------------

Vector Time (GMT): 2007/327/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6692823
41                 A    =         6724878
24  meter
 Y    =        -219021
23  meter          E    =           
0010130
 Z    =        -566211
68                 I    =           51
67149
 XDOT =        658
859247                 Wp   =           41
66853
 YDOT =       4775
905782  meter/sec      RA   =            1
95850  deg
 ZDOT =       6009
151908                 TA   =          312
16586
                                          MA   =          312
25185
                                          Ha   =            186
093  n
mi
                                          Hp   =            180
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21958082
05                 X    =         6697525
75
 Y    =        -718573
58  feet           Y    =         -144151
94  meter
 Z    =       -1857649
87                 Z    =         -533685
44
 XDOT =       2161
611703                 XDOT =         576
213019
 YDOT =      15668
982226  feet/sec       YDOT =        4782
810826  meter/sec
 ZDOT =      19715
065315                 ZDOT =        6012
152474

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8152928
21                 X    =        -2485012
52
 Y    =       20411961
34  feet           Y    =         6221565
82  meter
 Z    =       -1733832
25                 Z    =         -528472
07
 XDOT =     -13687
327494                 XDOT =       -4171
897420
 YDOT =      -3811
819864  feet/sec       YDOT =       -1161
842694  meter/sec
 ZDOT =      19726
958493                 ZDOT =        6012
776949


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   07327
51490559  
00020000  00000-0  20000-3 0  9040
2 25544  51
6412   2
4447 0001000 209
7143 150
3965 15
76523748 35914


Satellite: ISS
Catalog Number: 25544
Epoch time:      07327
51490559   =   yrday
fracday
Element set:     904
Inclination:       51
6412  deg
RA of node:         2
4447  deg
Eccentricity:     
0001000     
Arg of perigee:   209
7143  deg
Mean anomaly:     150
3965  deg
Mean motion:   15
76523748  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3591
Checksum:              276


Coasting Arc #6 (Orbit 3606)
---------------------------------------

Vector Time (GMT): 2007/328/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         160856
25                 A    =         6712882
33  meter
 Y    =       -4183787
23  meter          E    =           
0014493
 Z    =       -5259599
31                 I    =           51
60259
 XDOT =       7685
062097                 Wp   =           96
22285
 YDOT =       -148
928380  meter/sec      RA   =          356
80526  deg
 ZDOT =        352
787818                 TA   =          177
13510
                                          MA   =          177
12679
                                          Ha   =            185
996  n
mi
                                          Hp   =            180
037

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         527743
60                 X    =          233179
00
 Y    =      -13726336
06  feet           Y    =        -4181583
36  meter
 Z    =      -17255903
24                 Z    =        -5258642
73
 XDOT =      25213
458324                 XDOT =        7684
442429
 YDOT =       -488
610169  feet/sec       YDOT =         -62
993175  meter/sec
 ZDOT =       1157
440348                 ZDOT =         390
121471

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12425893
42                 X    =         3787412
31
 Y    =        5865125
15  feet           Y    =         1787690
14  meter
 Z    =      -17252666
22                 Z    =        -5258612
66
 XDOT =      -8832
757956                 XDOT =       -2692
224625
 YDOT =      22542
814190  feet/sec       YDOT =        6871
049765  meter/sec
 ZDOT =       1299
574636                 ZDOT =         396
110349


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   07328
52909211  
00020000  00000-0  20000-3 0  9053
2 25544  51
6416 357
2163 0001046 213
6707 146
4391 15
76554653 36070


Satellite: ISS
Catalog Number: 25544
Epoch time:      07328
52909211   =   yrday
fracday
Element set:     905
Inclination:       51
6416  deg
RA of node:       357
2163  deg
Eccentricity:     
0001046     
Arg of perigee:   213
6707  deg
Mean anomaly:     146
4391  deg
Mean motion:   15
76554653  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3607
Checksum:              285


Coasting Arc #7 (Orbit 3622)
---------------------------------------

Vector Time (GMT): 2007/329/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6614172
67                 A    =         6724131
99  meter
 Y    =          20107
82  meter          E    =           
0009597
 Z    =       -1185476
39                 I    =           51
61119
 XDOT =       1034
624061                 Wp   =          147
56599
 YDOT =      -4863
851019  meter/sec      RA   =          351
66219  deg
 ZDOT =      -5884
859382                 TA   =           45
44157
                                          MA   =           45
36325
                                          Ha   =            185
911  n
mi
                                          Hp   =            179
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21700041
57                 X    =        -6608146
97
 Y    =          65970
52  feet           Y    =          -53821
73  meter
 Z    =       -3889358
24                 Z    =        -1217594
18
 XDOT =       3394
435896                 XDOT =        1117
523751
 YDOT =     -15957
516465  feet/sec       YDOT =       -4851
816818  meter/sec
 ZDOT =     -19307
281436                 ZDOT =       -5879
632459

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7945166
37                 X    =         2421686
71
 Y    =      -20169388
46  feet           Y    =        -6147629
60  meter
 Z    =       -4011653
51                 Z    =        -1222751
99
 XDOT =      12064
550061                 XDOT =        3677
274859
 YDOT =       8569
927628  feet/sec       YDOT =        2612
113941  meter/sec
 ZDOT =     -19287
844834                 ZDOT =       -5878
935105


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   07329
54325434  
00020000  00000-0  20000-3 0  9066
2 25544  51
6406 351
9876 0000971 211
4868 148
6239 15
76601468 36231


Satellite: ISS
Catalog Number: 25544
Epoch time:      07329
54325434   =   yrday
fracday
Element set:     906
Inclination:       51
6406  deg
RA of node:       351
9876  deg
Eccentricity:     
0000971     
Arg of perigee:   211
4868  deg
Mean anomaly:     148
6239  deg
Mean motion:   15
76601468  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3623
Checksum:              309


Coasting Arc #8 (Orbit 3638)
---------------------------------------

Vector Time (GMT): 2007/330/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1613140
65                 A    =         6714375
03  meter
 Y    =        4349545
88  meter          E    =           
0006054
 Z    =        4850584
39                 I    =           51
54933
 XDOT =      -7348
278955                 Wp   =           61
02215
 YDOT =       -129
129722  meter/sec      RA   =          346
47180  deg
 ZDOT =      -2322
937364                 TA   =           51
63809
                                          MA   =           51
58371
                                          Ha   =            185
879  n
mi
                                          Hp   =            179
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5292456
19                 X    =        -1685221
68
 Y    =       14270163
63  feet           Y    =         4331103
00  meter
 Z    =       15913990
79                 Z    =         4842573
25
 XDOT =     -24108
526755                 XDOT =       -7335
004270
 YDOT =       -423
653945  feet/sec       YDOT =        -211
227735  meter/sec
 ZDOT =      -7621
185578                 ZDOT =       -2358
603673

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11448366
84                 X    =        -3489462
21
 Y    =      -10076676
20  feet           Y    =        -3071370
90  meter
 Z    =       15883899
37                 Z    =         4841412
53
 XDOT =       8163
765029                 XDOT =        2488
315581
 YDOT =     -21528
695479  feet/sec       YDOT =       -6561
946382  meter/sec
 ZDOT =      -7757
017345                 ZDOT =       -2364
338887


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   07330
55739168  
00020000  00000-0  20000-3 0  9073
2 25544  51
6398 346
7588 0000854 217
6909 142
4196 15
76661043 36393


Satellite: ISS
Catalog Number: 25544
Epoch time:      07330
55739168   =   yrday
fracday
Element set:     907
Inclination:       51
6398  deg
RA of node:       346
7588  deg
Eccentricity:     
0000854     
Arg of perigee:   217
6909  deg
Mean anomaly:     142
4196  deg
Mean motion:   15
76661043  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3639
Checksum:              328


Coasting Arc #9 (Orbit 3654)
---------------------------------------

Vector Time (GMT): 2007/331/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6089191
16                 A    =         6721001
81  meter
 Y    =         304974
85  meter          E    =           
0012824
 Z    =        2815474
13                 I    =           51
54405
 XDOT =      -2622
144672                 Wp   =           82
89614
 YDOT =       5155
016305  meter/sec      RA   =          341
35205  deg
 ZDOT =       5094
486274                 TA   =          309
47357
                                          MA   =          309
58694
                                          Ha   =            185
717  n
mi
                                          Hp   =            179
821

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19977661
29                 X    =         6071651
13
 Y    =        1000573
67  feet           Y    =          372969
14  meter
 Z    =        9237119
84                 Z    =         2845013
16
 XDOT =      -8602
836850                 XDOT =       -2704
342294
 YDOT =      16912
783154  feet/sec       YDOT =        5125
233632  meter/sec
 ZDOT =      16714
193811                 ZDOT =        5081
548893

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7659908
87                 X    =        -2334740
22
 Y    =       18421249
76  feet           Y    =         5614796
93  meter
 Z    =        9349643
56                 Z    =         2849771
36
 XDOT =     -11646
973944                 XDOT =       -3549
997658
 YDOT =     -13331
426470  feet/sec       YDOT =       -4063
418788  meter/sec
 ZDOT =      16665
417533                 ZDOT =        5079
619264


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   07331
57150543  
00020000  00000-0  20000-3 0  9081
2 25544  51
6396 341
5303 0000835 224
8703 135
2394 15
76688418 36553


Satellite: ISS
Catalog Number: 25544
Epoch time:      07331
57150543   =   yrday
fracday
Element set:     908
Inclination:       51
6396  deg
RA of node:       341
5303  deg
Eccentricity:     
0000835     
Arg of perigee:   224
8703  deg
Mean anomaly:     135
2394  deg
Mean motion:   15
76688418  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3655
Checksum:              296


Coasting Arc #10 (Orbit 3669)
---------------------------------------

Vector Time (GMT): 2007/332/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2894765
55                 A    =         6717974
16  meter
 Y    =       -4659080
70  meter          E    =           
0006120
 Z    =       -3885366
19                 I    =           51
50686
 XDOT =       6505
640225                 Wp   =          111
44186
 YDOT =        655
779003  meter/sec      RA   =          336
13801  deg
 ZDOT =       4063
531145                 TA   =          200
95300
                                          MA   =          200
97809
                                          Ha   =            185
747  n
mi
                                          Hp   =            179
878

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9497262
30                 X    =         2965523
46
 Y    =      -15285697
83  feet           Y    =        -4626313
66  meter
 Z    =      -12747264
41                 Z    =        -3871132
08
 XDOT =      21343
963992                 XDOT =        6478
083681
 YDOT =       2151
505916  feet/sec       YDOT =         728
374150  meter/sec
 ZDOT =      13331
795095                 ZDOT =        4095
068878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11406400
69                 X    =         3476670
93
 Y    =       13968261
10  feet           Y    =         4257525
98  meter
 Z    =      -12693502
44                 Z    =        -3868979
54
 XDOT =      -7844
422226                 XDOT =       -2390
979895
 YDOT =      18621
308075  feet/sec       YDOT =        5675
774701  meter/sec
 ZDOT =      13451
971414                 ZDOT =        4100
160887


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   07332
52221469  
00020000  00000-0  20000-3 0  9094
2 25544  51
6398 336
6284 0000760 233
1896 126
9199 15
76701123 36707


Satellite: ISS
Catalog Number: 25544
Epoch time:      07332
52221469   =   yrday
fracday
Element set:     909
Inclination:       51
6398  deg
RA of node:       336
6284  deg
Eccentricity:     
0000760     
Arg of perigee:   233
1896  deg
Mean anomaly:     126
9199  deg
Mean motion:   15
76701123  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3670
Checksum:              303


Coasting Arc #11 (Orbit 3685)
---------------------------------------

Vector Time (GMT): 2007/333/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5182174
31                 A    =         6716658
81  meter
 Y    =        -932077
30  meter          E    =           
0007512
 Z    =       -4177818
71                 I    =           51
47607
 XDOT =       3938
248692                 Wp   =           70
92616
 YDOT =      -5510
520754  meter/sec      RA   =          331
02168  deg
 ZDOT =      -3658
532558                 TA   =          161
68064
                                          MA   =          161
65357
                                          Ha   =            185
648  n
mi
                                          Hp   =            179
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17001884
23                 X    =        -5151071
36
 Y    =       -3057996
40  feet           Y    =         -989852
96  meter
 Z    =      -13706754
29                 Z    =        -4202918
37
 XDOT =      12920
763426                 XDOT =        4017
348033
 YDOT =     -18079
136332  feet/sec       YDOT =       -5466
038370  meter/sec
 ZDOT =     -12003
059574                 ZDOT =       -3639
208917

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8067387
38                 X    =         2458939
67
 Y    =      -15188824
16  feet           Y    =        -4629553
60  meter
 Z    =      -13802441
96                 Z    =        -4206984
31
 XDOT =      12156
703615                 XDOT =        3705
363262
 YDOT =      17289
314001  feet/sec       YDOT =        5269
782907  meter/sec
 ZDOT =     -11929
998441                 ZDOT =       -3636
263525


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   07333
53628117  
00020000  00000-0  20000-3 0  9109
2 25544  51
6388 331
3986 0000754 233
8223 126
2872 15
76746728 36869


Satellite: ISS
Catalog Number: 25544
Epoch time:      07333
53628117   =   yrday
fracday
Element set:     910
Inclination:       51
6388  deg
RA of node:       331
3986  deg
Eccentricity:     
0000754     
Arg of perigee:   233
8223  deg
Mean anomaly:     126
2872  deg
Mean motion:   15
76746728  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3686
Checksum:              310


Coasting Arc #12 (Orbit 3701)
---------------------------------------

Vector Time (GMT): 2007/334/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3874120
41                 A    =         6721718
35  meter
 Y    =        4935811
51  meter          E    =           
0013365
 Z    =        2392771
69                 I    =           51
46866
 XDOT =      -5310
468090                 Wp   =          107
67440
 YDOT =      -1557
287583  meter/sec      RA   =          325
80670  deg
 ZDOT =      -5365
262269                 TA   =           45
22939
                                          MA   =           45
12074
                                          Ha   =            185
544  n
mi
                                          Hp   =            179
711

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12710368
79                 X    =        -3940649
18
 Y    =       16193607
31  feet           Y    =         4892116
71  meter
 Z    =        7850300
82                 Z    =         2373789
94
 XDOT =     -17422
795572                 XDOT =       -5266
595977
 YDOT =      -5109
211230  feet/sec       YDOT =       -1616
426489  meter/sec
 ZDOT =     -17602
566499                 ZDOT =       -5390
954219

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11831661
76                 X    =        -3606290
50
 Y    =      -16879588
20  feet           Y    =        -5144898
48  meter
 Z    =        7778489
42                 Z    =         2370883
57
 XDOT =       8653
206081                 XDOT =        2637
497214
 YDOT =     -14253
528422  feet/sec       YDOT =       -4344
475463  meter/sec
 ZDOT =     -17700
574068                 ZDOT =       -5395
134976


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   07334
55032208  
00020000  00000-0  20000-3 0  9113
2 25544  51
6386 326
1694 0000724 252
7563 107
3523 15
76819250 37022


Satellite: ISS
Catalog Number: 25544
Epoch time:      07334
55032208   =   yrday
fracday
Element set:     911
Inclination:       51
6386  deg
RA of node:       326
1694  deg
Eccentricity:     
0000724     
Arg of perigee:   252
7563  deg
Mean anomaly:     107
3523  deg
Mean motion:   15
76819250  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3702
Checksum:              277

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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