Date: March 14th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


075/02:53:16 439 -2 3 8 7 8 7
N/A 5 4 -0 3 186 2
000/00:12:32 877 -6 4 0 0 178 5

Coasting Arc #1 (Orbit 3549)
---------------------------------------

Vector Time (GMT): 2007/071/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         644443
12                 A    =         6714010
14  meter
 Y    =        6094266
54  meter          E    =           
0016591
 Z    =       -2747062
89                 I    =           51
35504
 XDOT =      -5485
277660                 Wp   =          310
83578
 YDOT =      -1741
788140  meter/sec      RA   =          242
96048  deg
 ZDOT =      -5120
062648                 TA   =          260
74671
                                          MA   =          260
93439
                                          Ha   =            185
319  n
mi
                                          Hp   =            174
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2114314
70                 X    =          589592
87
 Y    =       19994312
79  feet           Y    =         6101166
36  meter
 Z    =       -9012673
53                 Z    =        -2744065
49
 XDOT =     -17996
317783                 XDOT =       -5440
520951
 YDOT =      -5714
528017  feet/sec       YDOT =       -1802
877367  meter/sec
 ZDOT =     -16798
105802                 ZDOT =       -5146
601154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6825410
93                 X    =        -2080385
25
 Y    =       18917570
99  feet           Y    =         5766075
64  meter
 Z    =       -9000579
32                 Z    =        -2743376
58
 XDOT =     -12202
188848                 XDOT =       -3719
227161
 YDOT =     -12490
472913  feet/sec       YDOT =       -3807
096144  meter/sec
 ZDOT =     -16898
063231                 ZDOT =       -5150
529673


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   07071
48441143  
00020000  00000-0  20000-3 0  9003
2 25544  51
6297 243
6505 0021320 308
7749  51
1512 15
79243643 35505


Satellite: ISS
Catalog Number: 25544
Epoch time:      07071
48441143   =   yrday
fracday
Element set:     900
Inclination:       51
6297  deg
RA of node:       243
6505  deg
Eccentricity:     
0021320     
Arg of perigee:   308
7749  deg
Mean anomaly:      51
1512  deg
Mean motion:   15
79243643  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3550
Checksum:              270


Coasting Arc #2 (Orbit 3565)
---------------------------------------

Vector Time (GMT): 2007/072/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5022680
57                 A    =         6712351
29  meter
 Y    =        3004019
37  meter          E    =           
0014520
 Z    =        3304751
67                 I    =           51
36406
 XDOT =       -565
084548                 Wp   =          347
45001
 YDOT =       6092
044882  meter/sec      RA   =          237
71392  deg
 ZDOT =      -4668
692834                 TA   =          153
53871
                                          MA   =          153
46449
                                          Ha   =            185
521  n
mi
                                          Hp   =            173
799

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16478610
80                 X    =         4972662
23
 Y    =        9855706
59  feet           Y    =         3059906
15  meter
 Z    =       10842361
11                 Z    =         3329030
01
 XDOT =      -1853
951929                 XDOT =        -610
485305
 YDOT =      19987
023892  feet/sec       YDOT =        6085
471914  meter/sec
 ZDOT =     -15317
233708                 ZDOT =       -4671
548293

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10705725
49                 X    =         3263105
13
 Y    =       15876751
72  feet           Y    =         4839233
93  meter
 Z    =       10934009
21                 Z    =         3332686
01
 XDOT =      -8901
860347                 XDOT =       -2713
287034
 YDOT =      16580
756295  feet/sec       YDOT =        5053
814519  meter/sec
 ZDOT =     -15327
128678                 ZDOT =       -4671
708821


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   07072
49686494  
00020000  00000-0  20000-3 0  9016
2 25544  51
6295 238
4083 0021417 312
2159  47
7189 15
79279270 35661


Satellite: ISS
Catalog Number: 25544
Epoch time:      07072
49686494   =   yrday
fracday
Element set:     901
Inclination:       51
6295  deg
RA of node:       238
4083  deg
Eccentricity:     
0021417     
Arg of perigee:   312
2159  deg
Mean anomaly:      47
7189  deg
Mean motion:   15
79279270  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3566
Checksum:              319


Coasting Arc #3 (Orbit 3581)
---------------------------------------

Vector Time (GMT): 2007/073/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1768730
31                 A    =         6706476
93  meter
 Y    =       -4183956
03  meter          E    =           
0015430
 Z    =        4938391
71                 I    =           51
35985
 XDOT =       5696
269381                 Wp   =          321
53861
 YDOT =       4778
461808  meter/sec      RA   =          232
55931  deg
 ZDOT =       2023
578578                 TA   =          108
89863
                                          MA   =          108
73129
                                          Ha   =            185
718  n
mi
                                          Hp   =            173
766

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5802920
96                 X    =         1791395
05
 Y    =      -13726889
88  feet           Y    =        -4164050
31  meter
 Z    =       16202072
53                 Z    =         4947039
16
 XDOT =      18688
547839                 XDOT =        5632
582569
 YDOT =      15677
368135  feet/sec       YDOT =        4841
804615  meter/sec
 ZDOT =       6639
037330                 ZDOT =        2051
095814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10810326
62                 X    =         3294987
55
 Y    =      -10207979
03  feet           Y    =        -3111392
01  meter
 Z    =       16233993
78                 Z    =         4948121
30
 XDOT =       9900
137214                 XDOT =        3017
561823
 YDOT =      21128
431967  feet/sec       YDOT =        6439
946063  meter/sec
 ZDOT =       6743
115676                 ZDOT =        2055
301658


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   07073
50929628  
00020000  00000-0  20000-3 0  9029
2 25544  51
6288 233
1659 0021283 316
6331  43
3159 15
79281514 35826


Satellite: ISS
Catalog Number: 25544
Epoch time:      07073
50929628   =   yrday
fracday
Element set:     902
Inclination:       51
6288  deg
RA of node:       233
1659  deg
Eccentricity:     
0021283     
Arg of perigee:   316
6331  deg
Mean anomaly:      43
3159  deg
Mean motion:   15
79281514  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3582
Checksum:              297


Coasting Arc #4 (Orbit 3596)
---------------------------------------

Vector Time (GMT): 2007/074/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4552136
74                 A    =         6717028
88  meter
 Y    =       -4916420
41  meter          E    =           
0025397
 Z    =         -21083
17                 I    =           51
41511
 XDOT =       3518
746128                 Wp   =          349
02170
 YDOT =      -3288
882561  meter/sec      RA   =          227
34710  deg
 ZDOT =       6036
587297                 TA   =           10
74766
                                          MA   =           10
69349
                                          Ha   =            185
836  n
mi
                                          Hp   =            173
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14934831
83                 X    =        -4496719
89
 Y    =      -16129988
22  feet           Y    =        -4967015
10  meter
 Z    =         -69170
50                 Z    =          -43062
23
 XDOT =      11544
442678                 XDOT =        3525
937302
 YDOT =     -10790
297117  feet/sec       YDOT =       -3249
493565  meter/sec
 ZDOT =      19805
076433                 ZDOT =        6053
698598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7422565
73                 X    =        -2262398
04
 Y    =      -20690886
35  feet           Y    =        -6306582
16  meter
 Z    =        -152468
19                 Z    =          -46472
31
 XDOT =      13238
232415                 XDOT =        4035
013240
 YDOT =      -4908
158944  feet/sec       YDOT =       -1496
006846  meter/sec
 ZDOT =      19868
932305                 ZDOT =        6056
050567


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   07074
45842505  
00020000  00000-0  20000-3 0  9033
2 25544  51
6292 228
2516 0021161 320
1425  39
8186 15
79341415 35970


Satellite: ISS
Catalog Number: 25544
Epoch time:      07074
45842505   =   yrday
fracday
Element set:     903
Inclination:       51
6292  deg
RA of node:       228
2516  deg
Eccentricity:     
0021161     
Arg of perigee:   320
1425  deg
Mean anomaly:      39
8186  deg
Mean motion:   15
79341415  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3597
Checksum:              285


Coasting Arc #5 (Orbit 3607)
---------------------------------------

Vector Time (GMT): 2007/075/02:59:32
877
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4207073
16                 A    =         6721402
18  meter
 Y    =        5148333
67  meter          E    =           
0005587
 Z    =        -993547
95                 I    =           51
42951
 XDOT =      -4320
058077                 Wp   =          297
84980
 YDOT =       2384
178048  meter/sec      RA   =          223
90125  deg
 ZDOT =      -5910
728073                 TA   =          253
04660
                                          MA   =          253
10785
                                          Ha   =            186
236  n
mi
                                          Hp   =            178
518

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13802733
45                 X    =         4154017
45
 Y    =       16890858
49  feet           Y    =         5195082
81  meter
 Z    =       -3259671
75                 Z    =         -973239
55
 XDOT =     -14173
418889                 XDOT =       -4317
684573
 YDOT =       7822
106458  feet/sec       YDOT =        2335
881715  meter/sec
 ZDOT =     -19392
152470                 ZDOT =       -5931
708831

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21245706
84                 X    =        -6475691
45
 Y    =       -4993288
83  feet           Y    =        -1521954
44  meter
 Z    =       -3182611
89                 Z    =         -970060
10
 XDOT =       6037
076806                 XDOT =        1840
101011
 YDOT =     -13217
053822  feet/sec       YDOT =       -4028
558005  meter/sec
 ZDOT =     -19470
680274                 ZDOT =       -5934
663348


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   07075
15448061  
00020000  00000-0  20000-3 0  9041
2 25544  51
6316 224
6532 0015207 313
1832  46
8061 15
77647762 36088


Satellite: ISS
Catalog Number: 25544
Epoch time:      07075
15448061   =   yrday
fracday
Element set:     904
Inclination:       51
6316  deg
RA of node:       224
6532  deg
Eccentricity:     
0015207     
Arg of perigee:   313
1832  deg
Mean anomaly:      46
8061  deg
Mean motion:   15
77647762  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3608
Checksum:              281


Coasting Arc #6 (Orbit 3623)
---------------------------------------

Vector Time (GMT): 2007/076/02:59:32
877
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4561601
87                 A    =         6711630
87  meter
 Y    =       -1228764
36  meter          E    =           
0015430
 Z    =        4776763
41                 I    =           51
41855
 XDOT =       4224
168807                 Wp   =          344
40702
 YDOT =       5933
275087  meter/sec      RA   =          218
69252  deg
 ZDOT =      -2494
852131                 TA   =          130
15111
                                          MA   =          130
01586
                                          Ha   =            186
399  n
mi
                                          Hp   =            178
113

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14965885
40                 X    =         4551798
87
 Y    =       -4031379
15  feet           Y    =        -1177808
41  meter
 Z    =       15671795
95                 Z    =         4798899
52
 XDOT =      13858
821546                 XDOT =        4169
627430
 YDOT =      19466
125615  feet/sec       YDOT =        5980
206952  meter/sec
 ZDOT =      -8185
210405                 ZDOT =       -2474
464474

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9141085
67                 X    =        -2786202
91
 Y    =       12412120
67  feet           Y    =         3783214
38  meter
 Z    =       15754832
45                 Z    =         4802072
93
 XDOT =     -22090
798724                 XDOT =       -6733
275451
 YDOT =      -5924
911900  feet/sec       YDOT =       -1805
913147  meter/sec
 ZDOT =      -8107
728706                 ZDOT =       -2471
235710


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   07076
16794712  
00020000  00000-0  20000-3 0  9051
2 25544  51
6315 219
4192 0015293 317
3756  42
6222 15
77695785 36246


Satellite: ISS
Catalog Number: 25544
Epoch time:      07076
16794712   =   yrday
fracday
Element set:     905
Inclination:       51
6315  deg
RA of node:       219
4192  deg
Eccentricity:     
0015293     
Arg of perigee:   317
3756  deg
Mean anomaly:      42
6222  deg
Mean motion:   15
77695785  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3624
Checksum:              309


Coasting Arc #7 (Orbit 3639)
---------------------------------------

Vector Time (GMT): 2007/077/02:59:32
877
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2970240
32                 A    =         6717075
03  meter
 Y    =       -5068142
16  meter          E    =           
0012993
 Z    =        3240821
51                 I    =           51
46093
 XDOT =       6056
627194                 Wp   =           15
00592
 YDOT =       -519
507859  meter/sec      RA   =          213
55854  deg
 ZDOT =       4746
660754                 TA   =           23
13292
                                          MA   =           23
07448
                                          Ha   =            186
685  n
mi
                                          Hp   =            177
971

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9744882
95                 X    =        -2929089
96
 Y    =      -16627762
98  feet           Y    =        -5101126
63  meter
 Z    =       10632616
50                 Z    =         3226492
78
 XDOT =      19870
824127                 XDOT =        6038
928195
 YDOT =      -1704
422109  feet/sec       YDOT =        -451
877732  meter/sec
 ZDOT =      15573
033970                 ZDOT =        4776
040459

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18136296
23                 X    =         5527943
09
 Y    =        6608927
13  feet           Y    =         2014400
99  meter
 Z    =       10578025
35                 Z    =         3224182
13
 XDOT =     -13710
617223                 XDOT =       -4178
996130
 YDOT =      12565
478980  feet/sec       YDOT =        3829
957993  meter/sec
 ZDOT =      15683
404462                 ZDOT =        4780
301680


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   07077
18139077  
00020000  00000-0  20000-3 0  9062
2 25544  51
6322 214
1841 0015335 321
5610  38
4461 15
77717372 36403


Satellite: ISS
Catalog Number: 25544
Epoch time:      07077
18139077   =   yrday
fracday
Element set:     906
Inclination:       51
6322  deg
RA of node:       214
1841  deg
Eccentricity:     
0015335     
Arg of perigee:   321
5610  deg
Mean anomaly:      38
4461  deg
Mean motion:   15
77717372  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3640
Checksum:              277


Coasting Arc #8 (Orbit 3654)
---------------------------------------

Vector Time (GMT): 2007/078/02:59:32
877
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5863490
04                 A    =         6716739
74  meter
 Y    =        -221790
46  meter          E    =           
0013627
 Z    =       -3251186
50                 I    =           51
48619
 XDOT =      -2412
616104                 Wp   =          342
81589
 YDOT =      -5586
323141  meter/sec      RA   =          208
33111  deg
 ZDOT =       4740
017960                 TA   =          338
91139
                                          MA   =          338
96752
                                          Ha   =            186
704  n
mi
                                          Hp   =            177
634

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19237172
04                 X    =        -5844780
62
 Y    =        -727659
00  feet           Y    =         -287255
05  meter
 Z    =      -10666622
38                 Z    =        -3279625
61
 XDOT =      -7915
407165                 XDOT =       -2372
995680
 YDOT =     -18327
831829  feet/sec       YDOT =       -5613
080295  meter/sec
 ZDOT =      15551
240026                 ZDOT =        4728
394450

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15067685
45                 X    =         4592630
52
 Y    =      -11885715
21  feet           Y    =        -3622766
00  meter
 Z    =      -10773566
63                 Z    =        -3283783
11
 XDOT =      17111
826283                 XDOT =        5215
684651
 YDOT =       7660
075248  feet/sec       YDOT =        2334
790936  meter/sec
 ZDOT =      15506
739078                 ZDOT =        4726
454071


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   07078
13147177  
00020000  00000-0  20000-3 0  9079
2 25544  51
6331 209
2770 0015402 325
1447  34
8708 15
77771874 36559


Satellite: ISS
Catalog Number: 25544
Epoch time:      07078
13147177   =   yrday
fracday
Element set:     907
Inclination:       51
6331  deg
RA of node:       209
2770  deg
Eccentricity:     
0015402     
Arg of perigee:   325
1447  deg
Mean anomaly:      34
8708  deg
Mean motion:   15
77771874  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3655
Checksum:              300


Coasting Arc #9 (Orbit 3670)
---------------------------------------

Vector Time (GMT): 2007/079/02:59:32
877
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1057051
74                 A    =         6711359
85  meter
 Y    =        4595210
76  meter          E    =           
0017266
 Z    =       -4785315
91                 I    =           51
49478
 XDOT =      -7224
705163                 Wp   =           11
05052
 YDOT =       -943
928751  meter/sec      RA   =          203
20165  deg
 ZDOT =      -2487
124213                 TA   =          234
48708
                                          MA   =          234
64825
                                          Ha   =            187
007  n
mi
                                          Hp   =            177
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3468017
52                 X    =         1028835
03
 Y    =       15076150
80  feet           Y    =         4606873
03  meter
 Z    =      -15699855
34                 Z    =        -4780249
79
 XDOT =     -23703
100929                 XDOT =       -7201
531082
 YDOT =      -3096
879105  feet/sec       YDOT =       -1024
590140  meter/sec
 ZDOT =      -8159
856341                 ZDOT =       -2522
165368

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12641033
73                 X    =        -3852987
08
 Y    =       -8952103
43  feet           Y    =        -2728601
13  meter
 Z    =      -15680147
85                 Z    =        -4779309
06
 XDOT =      19134
853419                 XDOT =        5832
303322
 YDOT =     -12408
880926  feet/sec       YDOT =       -3782
226906  meter/sec
 ZDOT =      -8291
727969                 ZDOT =       -2527
318685


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   07079
14486875  
00020000  00000-0  20000-3 0  9083
2 25544  51
6337 204
0429 0015515 329
3157  30
7099 15
77823189 36711


Satellite: ISS
Catalog Number: 25544
Epoch time:      07079
14486875   =   yrday
fracday
Element set:     908
Inclination:       51
6337  deg
RA of node:       204
0429  deg
Eccentricity:     
0015515     
Arg of perigee:   329
3157  deg
Mean anomaly:      30
7099  deg
Mean motion:   15
77823189  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3671
Checksum:              316


Coasting Arc #10 (Orbit 3686)
---------------------------------------

Vector Time (GMT): 2007/080/02:59:32
877
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6523106
23                 A    =         6720929
88  meter
 Y    =        1336273
08  meter          E    =           
0007322
 Z    =         938114
12                 I    =           51
55391
 XDOT =       -147
255388                 Wp   =           36
02138
 YDOT =       4903
440278  meter/sec      RA   =          197
99905  deg
 ZDOT =      -5931
441402                 TA   =          133
71775
                                          MA   =          133
65708
                                          Ha   =            187
176  n
mi
                                          Hp   =            177
104

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21401267
16                 X    =         6503121
82
 Y    =        4384098
02  feet           Y    =         1409106
44  meter
 Z    =        3077802
25                 Z    =          969754
81
 XDOT =       -483
121351                 XDOT =        -173
261461
 YDOT =      16087
402486  feet/sec       YDOT =        4901
647689  meter/sec
 ZDOT =     -19460
109588                 ZDOT =       -5932
220344

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18745023
56                 X    =        -5713483
18
 Y    =       11185303
44  feet           Y    =         3409280
49  meter
 Z    =        3196951
19                 Z    =          974430
72
 XDOT =      -9757
836681                 XDOT =       -2974
188620
 YDOT =     -10763
746716  feet/sec       YDOT =       -3280
789999  meter/sec
 ZDOT =     -19462
334651                 ZDOT =       -5932
119602


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   07080
15824302  
00020000  00000-0  20000-3 0  9098
2 25544  51
6335 198
8082 0015442 333
0113  27
0247 15
77812515 36879


Satellite: ISS
Catalog Number: 25544
Epoch time:      07080
15824302   =   yrday
fracday
Element set:     909
Inclination:       51
6335  deg
RA of node:       198
8082  deg
Eccentricity:     
0015442     
Arg of perigee:   333
0113  deg
Mean anomaly:      27
0247  deg
Mean motion:   15
77812515  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3687
Checksum:              279


Coasting Arc #11 (Orbit 3702)
---------------------------------------

Vector Time (GMT): 2007/081/02:59:32
877
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1380565
95                 A    =         6709042
33  meter
 Y    =       -3956602
63  meter          E    =           
0015600
 Z    =        5243350
16                 I    =           51
54245
 XDOT =       7421
933471                 Wp   =          346
44961
 YDOT =       2025
540217  meter/sec      RA   =          192
83297  deg
 ZDOT =       -411
045532                 TA   =          107
54238
                                          MA   =          107
37187
                                          Ha   =            187
246  n
mi
                                          Hp   =            176
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4529415
83                 X    =         1399235
28
 Y    =      -12980979
76  feet           Y    =        -3941059
72  meter
 Z    =       17202592
38                 Z    =         5250102
53
 XDOT =      24350
175431                 XDOT =        7400
728769
 YDOT =       6645
473154  feet/sec       YDOT =        2108
417847  meter/sec
 ZDOT =      -1348
574579                 ZDOT =        -375
041234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5697126
63                 X    =         1736484
20
 Y    =       12478361
32  feet           Y    =         3803404
53  meter
 Z    =       17227416
38                 Z    =         5250916
51
 XDOT =     -21354
203141                 XDOT =       -6508
761118
 YDOT =      11490
395280  feet/sec       YDOT =        3502
272481  meter/sec
 ZDOT =      -1212
913496                 ZDOT =        -369
696034


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   07081
17159040  
00020000  00000-0  20000-3 0  9103
2 25544  51
6337 193
5732 0015668 336
7723  23
2733 15
77905249 37036


Satellite: ISS
Catalog Number: 25544
Epoch time:      07081
17159040   =   yrday
fracday
Element set:     910
Inclination:       51
6337  deg
RA of node:       193
5732  deg
Eccentricity:     
0015668     
Arg of perigee:   336
7723  deg
Mean anomaly:      23
2733  deg
Mean motion:   15
77905249  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3703
Checksum:              291


Coasting Arc #12 (Orbit 3718)
---------------------------------------

Vector Time (GMT): 2007/082/02:59:32
877
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6142990
27                 A    =         6719984
12  meter
 Y    =       -2133824
15  meter          E    =           
0022574
 Z    =        1632501
88                 I    =           51
60719
 XDOT =       2985
903526                 Wp   =           19
47568
 YDOT =      -4195
187572  meter/sec      RA   =          187
68145  deg
 ZDOT =       5750
549279                 TA   =          358
62298
                                          MA   =          358
62918
                                          Ha   =            187
566  n
mi
                                          Hp   =            176
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20154167
55                 X    =        -6126603
40
 Y    =       -7000735
41  feet           Y    =        -2202426
85  meter
 Z    =        5355977
28                 Z    =         1602699
00
 XDOT =       9796
271412                 XDOT =        3004
657588
 YDOT =     -13763
738754  feet/sec       YDOT =       -4161
692541  meter/sec
 ZDOT =      18866
631494                 ZDOT =        5765
100487

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19321710
36                 X    =         5889257
32
 Y    =       -9113908
86  feet           Y    =        -2777919
42  meter
 Z    =        5243608
71                 Z    =         1598251
94
 XDOT =       2036
348560                 XDOT =         620
679041
 YDOT =      15206
309172  feet/sec       YDOT =        4634
883035  meter/sec
 ZDOT =      18920
753194                 ZDOT =        5767
045574


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   07082
18491665  
00020000  00000-0  20000-3 0  9118
2 25544  51
6333 188
3381 0015825 340
9731  19
0841 15
77905647 37197


Satellite: ISS
Catalog Number: 25544
Epoch time:      07082
18491665   =   yrday
fracday
Element set:     911
Inclination:       51
6333  deg
RA of node:       188
3381  deg
Eccentricity:     
0015825     
Arg of perigee:   340
9731  deg
Mean anomaly:      19
0841  deg
Mean motion:   15
77905647  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3719
Checksum:              307


Coasting Arc #13 (Orbit 3733)
---------------------------------------

Vector Time (GMT): 2007/083/02:59:32
877
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3737167
59                 A    =         6712209
58  meter
 Y    =        3363371
39  meter          E    =           
0012777
 Z    =       -4444718
73                 I    =           51
60992
 XDOT =      -6391
255035                 Wp   =           22
62295
 YDOT =      -2843
262770  meter/sec      RA   =          182
47452  deg
 ZDOT =       3236
958469                 TA   =          279
70294
                                          MA   =          279
84723
                                          Ha   =            187
564  n
mi
                                          Hp   =            176
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12261048
51                 X    =        -3752907
91
 Y    =       11034683
05  feet           Y    =         3321492
27  meter
 Z    =      -14582410
54                 Z    =        -4462912
12
 XDOT =     -20968
684497                 XDOT =       -6374
710797
 YDOT =      -9328
289927  feet/sec       YDOT =       -2914
640843  meter/sec
 ZDOT =      10619
942482                 ZDOT =        3205
949973

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         704127
49                 X    =          214618
06
 Y    =      -16419973
07  feet           Y    =        -5004807
79  meter
 Z    =      -14650355
85                 Z    =        -4465428
46
 XDOT =      20213
939248                 XDOT =        6161
208683
 YDOT =      -8461
489232  feet/sec       YDOT =       -2579
061918  meter/sec
 ZDOT =      10502
928612                 ZDOT =        3201
292641


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   07083
13488632  
00020000  00000-0  20000-3 0  9125
2 25544  51
6328 183
4303 0015860 344
2454  15
8215 15
77957210 37348


Satellite: ISS
Catalog Number: 25544
Epoch time:      07083
13488632   =   yrday
fracday
Element set:     912
Inclination:       51
6328  deg
RA of node:       183
4303  deg
Eccentricity:     
0015860     
Arg of perigee:   344
2454  deg
Mean anomaly:      15
8215  deg
Mean motion:   15
77957210  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3734
Checksum:              285

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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