Date: June 29th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5381 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 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 1239)
---------------------------------------

Vector Time (GMT): 2007/178/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5227037
68                 A    =         6717693
12  meter
 Y    =       -3610416
57  meter          E    =           
0014215
 Z    =        2178947
02                 I    =           51
89499
 XDOT =       1289
553197                 Wp   =           75
69846
 YDOT =      -5218
445385  meter/sec      RA   =           50
23779  deg
 ZDOT =      -5520
008633                 TA   =           79
95138
                                          MA   =           79
79102
                                          Ha   =            185
152  n
mi
                                          Hp   =            176
274

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17149073
74                 X    =        -5196861
96
 Y    =      -11845198
72  feet           Y    =        -3668699
96  meter
 Z    =        7148776
30                 Z    =         2153626
49
 XDOT =       4230
817574                 XDOT =        1374
626108
 YDOT =     -17120
883810  feet/sec       YDOT =       -5203
548081  meter/sec
 ZDOT =     -18110
264543                 ZDOT =       -5513
538376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14793980
90                 X    =        -4509205
38
 Y    =       14727615
73  feet           Y    =         4488977
27  meter
 Z    =        7052654
08                 Z    =         2149648
96
 XDOT =     -14963
354364                 XDOT =       -4560
830410
 YDOT =      -6316
797025  feet/sec       YDOT =       -1925
359733  meter/sec
 ZDOT =     -18086
351519                 ZDOT =       -5512
719943


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   07178
49427289  
00020000  00000-0  20000-3 0  9007
2 25544  51
6351  50
6458 0008166   3
6630 356
4593 15
78392080 12405


Satellite: ISS
Catalog Number: 25544
Epoch time:      07178
49427289   =   yrday
fracday
Element set:     900
Inclination:       51
6351  deg
RA of node:        50
6458  deg
Eccentricity:     
0008166     
Arg of perigee:     3
6630  deg
Mean anomaly:     356
4593  deg
Mean motion:   15
78392080  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1240
Checksum:              294


Coasting Arc #2 (Orbit 1255)
---------------------------------------

Vector Time (GMT): 2007/179/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2224419
38                 A    =         6707666
52  meter
 Y    =        3575447
96  meter          E    =           
0007534
 Z    =        5217233
85                 I    =           51
84272
 XDOT =      -5872
881015                 Wp   =           29
34140
 YDOT =      -4921
707958  meter/sec      RA   =           45
11125  deg
 ZDOT =        874
871993                 TA   =           52
39802
                                          MA   =           52
32964
                                          Ha   =            185
237  n
mi
                                          Hp   =            175
981

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7297963
86                 X    =        -2289579
66
 Y    =       11730472
30  feet           Y    =         3550207
77  meter
 Z    =       17116908
96                 Z    =         5206270
11
 XDOT =     -19267
982332                 XDOT =       -5821
659246
 YDOT =     -16147
335821  feet/sec       YDOT =       -4987
095606  meter/sec
 ZDOT =       2870
314938                 ZDOT =         846
464812

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10337714
46                 X    =         3150935
37
 Y    =        9241248
80  feet           Y    =         2816732
64  meter
 Z    =       17075825
29                 Z    =         5204711
55
 XDOT =     -18455
151654                 XDOT =       -5625
130224
 YDOT =      15576
489643  feet/sec       YDOT =        4747
714043  meter/sec
 ZDOT =       2762
382125                 ZDOT =         841
974072


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   07179
50725348  
00020000  00000-0  20000-3 0  9018
2 25544  51
6355  45
4085 0008262   6
4303 353
6967 15
78452016 12569


Satellite: ISS
Catalog Number: 25544
Epoch time:      07179
50725348   =   yrday
fracday
Element set:     901
Inclination:       51
6355  deg
RA of node:        45
4085  deg
Eccentricity:     
0008262     
Arg of perigee:     6
4303  deg
Mean anomaly:     353
6967  deg
Mean motion:   15
78452016  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1256
Checksum:              289


Coasting Arc #3 (Orbit 1271)
---------------------------------------

Vector Time (GMT): 2007/180/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4731479
03                 A    =         6719224
78  meter
 Y    =        4699365
94  meter          E    =           
0020342
 Z    =         717853
50                 I    =           51
86038
 XDOT =      -3841
828110                 Wp   =           36
07322
 YDOT =       2939
224125  meter/sec      RA   =           39
95616  deg
 ZDOT =       6011
390598                 TA   =          331
74782
                                          MA   =          331
85801
                                          Ha   =            185
207  n
mi
                                          Hp   =            175
783

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15523225
18                 X    =         4675091
19
 Y    =       15417867
25  feet           Y    =         4751960
55  meter
 Z    =        2355162
39                 Z    =          740703
08
 XDOT =     -12604
422933                 XDOT =       -3903
611577
 YDOT =       9643
123769  feet/sec       YDOT =        2895
915822  meter/sec
 ZDOT =      19722
410099                 ZDOT =        5992
577644

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17560571
24                 X    =         5352462
11
 Y    =      -13034209
90  feet           Y    =        -3972827
18  meter
 Z    =        2442058
70                 Z    =          744339
49
 XDOT =       6686
334928                 XDOT =        2037
994886
 YDOT =      12731
233346  feet/sec       YDOT =        3880
479924  meter/sec
 ZDOT =      19651
571946                 ZDOT =        5989
799129


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   07180
52021685  
00020000  00000-0  20000-3 0  9026
2 25544  51
6353  40
1711 0008326   9
3080 350
8238 15
78483011 12727


Satellite: ISS
Catalog Number: 25544
Epoch time:      07180
52021685   =   yrday
fracday
Element set:     902
Inclination:       51
6353  deg
RA of node:        40
1711  deg
Eccentricity:     
0008326     
Arg of perigee:     9
3080  deg
Mean anomaly:     350
8238  deg
Mean motion:   15
78483011  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1272
Checksum:              255


Coasting Arc #4 (Orbit 1286)
---------------------------------------

Vector Time (GMT): 2007/181/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4419060
39                 A    =         6709352
96  meter
 Y    =       -1544642
56  meter          E    =           
0013761
 Z    =       -4815697
27                 I    =           51
80366
 XDOT =       4654
589536                 Wp   =           70
46513
 YDOT =       5609
372047  meter/sec      RA   =           34
77252  deg
 ZDOT =       2482
226200                 TA   =          223
69676
                                          MA   =          223
80578
                                          Ha   =            185
291  n
mi
                                          Hp   =            175
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14498229
64                 X    =         4459397
98
 Y    =       -5067724
93  feet           Y    =        -1494999
51  meter
 Z    =      -15799531
74                 Z    =        -4794132
01
 XDOT =      15270
963046                 XDOT =        4579
460667
 YDOT =      18403
451597  feet/sec       YDOT =        5661
001644  meter/sec
 ZDOT =       8143
786747                 ZDOT =        2504
656824

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3093931
20                 X    =         -943030
23
 Y    =      -15128567
15  feet           Y    =        -4611187
27  meter
 Z    =      -15718134
36                 Z    =        -4790887
35
 XDOT =      19152
264632                 XDOT =        5837
610260
 YDOT =     -12431
692349  feet/sec       YDOT =       -3789
179828  meter/sec
 ZDOT =       8229
196874                 ZDOT =        2508
259207


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   07181
46985408  
00020000  00000-0  20000-3 0  9033
2 25544  51
6347  35
2607 0008345  12
2318 347
9049 15
78508125 12874


Satellite: ISS
Catalog Number: 25544
Epoch time:      07181
46985408   =   yrday
fracday
Element set:     903
Inclination:       51
6347  deg
RA of node:        35
2607  deg
Eccentricity:     
0008345     
Arg of perigee:    12
2318  deg
Mean anomaly:     347
9049  deg
Mean motion:   15
78508125  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1287
Checksum:              299


Coasting Arc #5 (Orbit 1302)
---------------------------------------

Vector Time (GMT): 2007/182/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3079629
47                 A    =         6714129
55  meter
 Y    =       -4878076
03  meter          E    =           
0011050
 Z    =       -3449561
32                 I    =           51
79488
 XDOT =       6151
813607                 Wp   =           40
60400
 YDOT =       -645
024717  meter/sec      RA   =           29
65932  deg
 ZDOT =      -4579
902675                 TA   =          180
17196
                                          MA   =          180
17234
                                          Ha   =            185
299  n
mi
                                          Hp   =            175
468

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10103771
22                 X    =        -3008096
09
 Y    =      -16004186
44  feet           Y    =        -4912113
46  meter
 Z    =      -11317458
39                 Z    =        -3464349
29
 XDOT =      20183
115508                 XDOT =        6180
817212
 YDOT =      -2116
222825  feet/sec       YDOT =        -576
068518  meter/sec
 ZDOT =     -15025
927410                 ZDOT =       -4549
947220

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17054176
67                 X    =        -5198113
05
 Y    =        8129861
97  feet           Y    =         2477981
93  meter
 Z    =      -11373893
06                 Z    =        -3466762
60
 XDOT =        825
334076                 XDOT =         251
561826
 YDOT =     -19132
169608  feet/sec       YDOT =       -5831
485296  meter/sec
 ZDOT =     -14912
698897                 ZDOT =       -4545
390624


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   07182
48278287  
00020000  00000-0  20000-3 0  9047
2 25544  51
6341  30
0231 0008295  15
2913 344
8502 15
78509884 13034


Satellite: ISS
Catalog Number: 25544
Epoch time:      07182
48278287   =   yrday
fracday
Element set:     904
Inclination:       51
6341  deg
RA of node:        30
0231  deg
Eccentricity:     
0008295     
Arg of perigee:    15
2913  deg
Mean anomaly:     344
8502  deg
Mean motion:   15
78509884  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1303
Checksum:              283


Coasting Arc #6 (Orbit 1318)
---------------------------------------

Vector Time (GMT): 2007/183/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6077651
98                 A    =         6715725
75  meter
 Y    =        -311027
75  meter          E    =           
0017106
 Z    =        2834230
39                 I    =           51
77530
 XDOT =      -2117
638662                 Wp   =           69
94516
 YDOT =      -5375
721239  meter/sec      RA   =           24
44899  deg
 ZDOT =      -5100
459406                 TA   =           77
54719
                                          MA   =           77
35583
                                          Ha   =            185
370  n
mi
                                          Hp   =            175
237

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19939803
07                 X    =        -6087490
27
 Y    =       -1020432
24  feet           Y    =         -379047
04  meter
 Z    =        9298656
14                 Z    =         2804681
66
 XDOT =      -6947
633407                 XDOT =       -2032
592459
 YDOT =     -17636
880707  feet/sec       YDOT =       -5398
925333  meter/sec
 ZDOT =     -16733
790703                 ZDOT =       -5110
541228

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2976475
11                 X    =         -907229
61
 Y    =       19795055
30  feet           Y    =         6033532
86  meter
 Z    =        9186861
05                 Z    =         2800155
25
 XDOT =     -16780
583053                 XDOT =       -5114
721715
 YDOT =       5307
860348  feet/sec       YDOT =        1617
835834  meter/sec
 ZDOT =     -16772
481700                 ZDOT =       -5112
252422


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   07183
49569272  
00020000  00000-0  20000-3 0  9057
2 25544  51
6344  24
7848 0008505  18
9262 341
2218 15
78590101 13196


Satellite: ISS
Catalog Number: 25544
Epoch time:      07183
49569272   =   yrday
fracday
Element set:     905
Inclination:       51
6344  deg
RA of node:        24
7848  deg
Eccentricity:     
0008505     
Arg of perigee:    18
9262  deg
Mean anomaly:     341
2218  deg
Mean motion:   15
78590101  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1319
Checksum:              295


Coasting Arc #7 (Orbit 1334)
---------------------------------------

Vector Time (GMT): 2007/184/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         418568
36                 A    =         6708019
28  meter
 Y    =        4376988
41  meter          E    =           
0008807
 Z    =        5058540
84                 I    =           51
72136
 XDOT =      -7434
469751                 Wp   =           56
29672
 YDOT =      -1212
643555  meter/sec      RA   =           19
32266  deg
 ZDOT =       1667
165409                 TA   =           17
74016
                                          MA   =           17
70943
                                          Ha   =            185
478  n
mi
                                          Hp   =            175
085

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1373255
79                 X    =          345020
08
 Y    =       14360198
18  feet           Y    =         4381256
97  meter
 Z    =       16596262
61                 Z    =         5060396
32
 XDOT =     -24391
304957                 XDOT =       -7428
455897
 YDOT =      -3978
489354  feet/sec       YDOT =       -1295
746633  meter/sec
 ZDOT =       5469
702786                 ZDOT =        1631
063768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14416658
17                 X    =         4394197
41
 Y    =        -113569
50  feet           Y    =          -34615
98  meter
 Z    =       16603738
28                 Z    =         5060819
43
 XDOT =      -5950
784764                 XDOT =       -1813
799196
 YDOT =      22968
031690  feet/sec       YDOT =        7000
656059  meter/sec
 ZDOT =       5333
023425                 ZDOT =        1625
505540


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   07184
50858692  
00020000  00000-0  20000-3 0  9068
2 25544  51
6335  19
5461 0008428  23
2509 336
9036 15
78552569 13359


Satellite: ISS
Catalog Number: 25544
Epoch time:      07184
50858692   =   yrday
fracday
Element set:     906
Inclination:       51
6335  deg
RA of node:        19
5461  deg
Eccentricity:     
0008428     
Arg of perigee:    23
2509  deg
Mean anomaly:     336
9036  deg
Mean motion:   15
78552569  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1335
Checksum:              309


Coasting Arc #8 (Orbit 1350)
---------------------------------------

Vector Time (GMT): 2007/185/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6493175
64                 A    =         6719120
13  meter
 Y    =        1683328
48  meter          E    =           
0020555
 Z    =          57798
32                 I    =           51
73067
 XDOT =      -1258
877698                 Wp   =           37
59294
 YDOT =       4610
031131  meter/sec      RA   =           14
14426  deg
 ZDOT =       6056
528863                 TA   =          323
03587
                                          MA   =          323
17733
                                          Ha   =            185
440  n
mi
                                          Hp   =            174
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21303069
70                 X    =         6473589
06
 Y    =        5522731
23  feet           Y    =         1755829
29  meter
 Z    =         189627
05                 Z    =           89294
34
 XDOT =      -4130
176176                 XDOT =       -1339
755227
 YDOT =      15124
774053  feet/sec       YDOT =        4595
500564  meter/sec
 ZDOT =      19870
501518                 ZDOT =        6050
217554

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6870494
10                 X    =         2094126
60
 Y    =      -20905936
13  feet           Y    =        -6372129
33  meter
 Z    =         308937
73                 Z    =           94164
22
 XDOT =      13298
814375                 XDOT =        4053
478622
 YDOT =       4696
672361  feet/sec       YDOT =        1431
545736  meter/sec
 ZDOT =      19847
113907                 ZDOT =        6049
400319


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   07185
52146046  
00020000  00000-0  20000-3 0  9075
2 25544  51
6327  14
3073 0008384  26
0391 334
1195 15
78603774 13512


Satellite: ISS
Catalog Number: 25544
Epoch time:      07185
52146046   =   yrday
fracday
Element set:     907
Inclination:       51
6327  deg
RA of node:        14
3073  deg
Eccentricity:     
0008384     
Arg of perigee:    26
0391  deg
Mean anomaly:     334
1195  deg
Mean motion:   15
78603774  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1351
Checksum:              279


Coasting Arc #9 (Orbit 1365)
---------------------------------------

Vector Time (GMT): 2007/186/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2617709
31                 A    =         6708051
58  meter
 Y    =       -3609829
53  meter          E    =           
0017526
 Z    =       -5024893
41                 I    =           51
66445
 XDOT =       7023
253541                 Wp   =           76
27956
 YDOT =       2567
361592  meter/sec      RA   =            8
96033  deg
 ZDOT =       1823
756897                 TA   =          211
25049
                                          MA   =          211
35480
                                          Ha   =            185
447  n
mi
                                          Hp   =            174
775

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8588285
15                 X    =         2682290
12
 Y    =      -11843272
74  feet           Y    =        -3580195
13  meter
 Z    =      -16485870
78                 Z    =        -5012020
32
 XDOT =      23042
170411                 XDOT =        6985
163577
 YDOT =       8423
102335  feet/sec       YDOT =        2645
686362  meter/sec
 ZDOT =       5983
454385                 ZDOT =        1857
783234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11425626
28                 X    =        -3482530
89
 Y    =       -9223196
87  feet           Y    =        -2811230
41  meter
 Z    =      -16437560
34                 Z    =        -5010168
39
 XDOT =       8814
065124                 XDOT =        2686
527050
 YDOT =     -21757
404049  feet/sec       YDOT =       -6631
656754  meter/sec
 ZDOT =       6112
429627                 ZDOT =        1863
068550


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   07186
47101364  
00020000  00000-0  20000-3 0  9085
2 25544  51
6319   9
3955 0008347  30
0032 330
1610 15
78640389 13669


Satellite: ISS
Catalog Number: 25544
Epoch time:      07186
47101364   =   yrday
fracday
Element set:     908
Inclination:       51
6319  deg
RA of node:         9
3955  deg
Eccentricity:     
0008347     
Arg of perigee:    30
0032  deg
Mean anomaly:     330
1610  deg
Mean motion:   15
78640389  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1366
Checksum:              276


Coasting Arc #10 (Orbit 1381)
---------------------------------------

Vector Time (GMT): 2007/187/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5355203
28                 A    =         6714906
16  meter
 Y    =       -2737458
12  meter          E    =           
0010566
 Z    =       -3001017
42                 I    =           51
65922
 XDOT =       4631
573741                 Wp   =           57
26422
 YDOT =      -3625
396605  meter/sec      RA   =            3
83109  deg
 ZDOT =      -4964
864891                 TA   =          157
43376
                                          MA   =          157
38726
                                          Ha   =            185
475  n
mi
                                          Hp   =            174
478

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17569564
58                 X    =        -5309616
33
 Y    =       -8981161
82  feet           Y    =        -2797087
79  meter
 Z    =       -9845857
67                 Z    =        -3026922
38
 XDOT =      15195
451905                 XDOT =        4695
887461
 YDOT =     -11894
345816  feet/sec       YDOT =       -3573
243589  meter/sec
 ZDOT =     -16288
926809                 ZDOT =       -4942
209066

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9492731
87                 X    =        -2893384
67
 Y    =       17242218
03  feet           Y    =         5255428
05  meter
 Z    =       -9944130
92                 Z    =        -3030971
11
 XDOT =     -10181
880147                 XDOT =       -3103
437069
 YDOT =     -14937
679417  feet/sec       YDOT =       -4553
004686  meter/sec
 ZDOT =     -16203
617427                 ZDOT =       -4938
862592


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   07187
48385287  
00020000  00000-0  20000-3 0  9096
2 25544  51
6318   4
1577 0008424  33
4564 326
7132 15
78670346 13828


Satellite: ISS
Catalog Number: 25544
Epoch time:      07187
48385287   =   yrday
fracday
Element set:     909
Inclination:       51
6318  deg
RA of node:         4
1577  deg
Eccentricity:     
0008424     
Arg of perigee:    33
4564  deg
Mean anomaly:     326
7132  deg
Mean motion:   15
78670346  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1382
Checksum:              306


Coasting Arc #11 (Orbit 1397)
---------------------------------------

Vector Time (GMT): 2007/188/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5216662
82                 A    =         6714271
59  meter
 Y    =        2697542
19  meter          E    =           
0018779
 Z    =        3245994
72                 I    =           51
62859
 XDOT =      -4857
607232                 Wp   =           70
63863
 YDOT =      -3644
093537  meter/sec      RA   =          358
60896  deg
 ZDOT =      -4749
995008                 TA   =           71
26302
                                          MA   =           71
05933
                                          Ha   =            185
466  n
mi
                                          Hp   =            174
459

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17115035
50                 X    =        -5262207
83
 Y    =        8850204
03  feet           Y    =         2638951
50  meter
 Z    =       10649588
98                 Z    =         3220541
92
 XDOT =     -15937
031602                 XDOT =       -4793
422856
 YDOT =     -11955
687458  feet/sec       YDOT =       -3698
054601  meter/sec
 ZDOT =     -15583
973123                 ZDOT =       -4773
437734

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8639373
34                 X    =         2633280
99
 Y    =       17281405
58  feet           Y    =         5267372
42  meter
 Z    =       10553603
48                 Z    =         3216738
34
 XDOT =     -10888
473450                 XDOT =       -3318
806707
 YDOT =      15072
048277  feet/sec       YDOT =        4593
960315  meter/sec
 ZDOT =     -15673
026982                 ZDOT =       -4777
138624


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   07188
49667254  
00020000  00000-0  20000-3 0  9107
2 25544  51
6321 358
9184 0008306  36
0324 324
1400 15
78715700 13989


Satellite: ISS
Catalog Number: 25544
Epoch time:      07188
49667254   =   yrday
fracday
Element set:     910
Inclination:       51
6321  deg
RA of node:       358
9184  deg
Eccentricity:     
0008306     
Arg of perigee:    36
0324  deg
Mean anomaly:     324
1400  deg
Mean motion:   15
78715700  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1398
Checksum:              288


Coasting Arc #12 (Orbit 1413)
---------------------------------------

Vector Time (GMT): 2007/189/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2836576
87                 A    =         6708260
97  meter
 Y    =        3586316
31  meter          E    =           
0011132
 Z    =        4898289
93                 I    =           51
57849
 XDOT =      -6957
935104                 Wp   =           74
34463
 YDOT =       2531
693266  meter/sec      RA   =          353
47722  deg
 ZDOT =       2174
600220                 TA   =          354
56875
                                          MA   =          354
58081
                                          Ha   =            185
519  n
mi
                                          Hp   =            174
266

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9306354
55                 X    =         2772468
29
 Y    =       11766129
64  feet           Y    =         3617677
39  meter
 Z    =       16070505
00                 Z    =         4911914
81
 XDOT =     -22827
871077                 XDOT =       -6996
291571
 YDOT =       8306
080270  feet/sec       YDOT =        2453
670967  meter/sec
 ZDOT =       7134
515159                 ZDOT =        2140
705694

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11720151
74                 X    =         3572302
25
 Y    =       -9274530
35  feet           Y    =        -2826876
85  meter
 Z    =       16122416
16                 Z    =         4914112
45
 XDOT =       7743
222497                 XDOT =        2360
134217
 YDOT =      21971
286881  feet/sec       YDOT =        6696
848241  meter/sec
 ZDOT =       7006
582638                 ZDOT =        2135
606388


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   07189
50947729  
00020000  00000-0  20000-3 0  9119
2 25544  51
6312 353
6793 0008426  41
0622 319
1177 15
78691883 14146


Satellite: ISS
Catalog Number: 25544
Epoch time:      07189
50947729   =   yrday
fracday
Element set:     911
Inclination:       51
6312  deg
RA of node:       353
6793  deg
Eccentricity:     
0008426     
Arg of perigee:    41
0622  deg
Mean anomaly:     319
1177  deg
Mean motion:   15
78691883  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1414
Checksum:              307

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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