Date: August 2nd 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 2421 88 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 1761)
---------------------------------------

Vector Time (GMT): 2007/211/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4233205
46                 A    =         6714951
20  meter
 Y    =        -912641
81  meter          E    =           
0007225
 Z    =        5128276
44                 I    =           51
33623
 XDOT =       3007
213866                 Wp   =          155
80989
 YDOT =       6986
978748  meter/sec      RA   =          239
18911  deg
 ZDOT =      -1244
811478                 TA   =          306
09342
                                          MA   =          306
16030
                                          Ha   =            188
799  n
mi
                                          Hp   =            180
033

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13888469
35                 X    =         4218184
51
 Y    =       -2994231
64  feet           Y    =         -865388
28  meter
 Z    =       16825053
94                 Z    =         5148804
26
 XDOT =       9866
187224                 XDOT =        2934
907856
 YDOT =      22923
158622  feet/sec       YDOT =        7020
202961  meter/sec
 ZDOT =      -4084
027160                 ZDOT =       -1230
377638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10776375
57                 X    =        -3284639
27
 Y    =       -9116291
59  feet           Y    =        -2778645
68  meter
 Z    =       16902674
39                 Z    =         5151935
15
 XDOT =      11492
675286                 XDOT =        3502
967427
 YDOT =     -21019
210940  feet/sec       YDOT =       -6406
655495  meter/sec
 ZDOT =      -4028
525577                 ZDOT =       -1227
894596


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   07211
54692747  
00020000  00000-0  20000-3 0  9004
2 25544  51
6311 239
8336 0008912 182
4954 177
6167 15
75980904 17625


Satellite: ISS
Catalog Number: 25544
Epoch time:      07211
54692747   =   yrday
fracday
Element set:     900
Inclination:       51
6311  deg
RA of node:       239
8336  deg
Eccentricity:     
0008912     
Arg of perigee:   182
4954  deg
Mean anomaly:     177
6167  deg
Mean motion:   15
75980904  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1762
Checksum:              311


Coasting Arc #2 (Orbit 1777)
---------------------------------------

Vector Time (GMT): 2007/212/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2609944
66                 A    =         6725320
59  meter
 Y    =       -5950958
04  meter          E    =           
0012148
 Z    =        1729689
29                 I    =           51
38693
 XDOT =       5164
622860                 Wp   =          102
81020
 YDOT =       -604
043752  meter/sec      RA   =          234
04473  deg
 ZDOT =       5678
617626                 TA   =          276
40973
                                          MA   =          276
54806
                                          Ha   =            188
779  n
mi
                                          Hp   =            180
289

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8562810
58                 X    =        -2551608
51
 Y    =      -19524140
56  feet           Y    =        -5979817
88  meter
 Z    =        5674833
62                 Z    =         1717151
68
 XDOT =      16944
300723                 XDOT =        5143
408484
 YDOT =      -1981
770840  feet/sec       YDOT =        -546
409114  meter/sec
 ZDOT =      18630
635257                 ZDOT =        5703
655191

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9926748
67                 X    =        -3025673
00
 Y    =       18881692
00  feet           Y    =         5755139
72  meter
 Z    =        5626623
70                 Z    =         1714994
91
 XDOT =     -10658
781348                 XDOT =       -3248
796555
 YDOT =     -11219
354431  feet/sec       YDOT =       -3419
659231  meter/sec
 ZDOT =      18725
375490                 ZDOT =        5707
494449


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   07212
56148752  
00020000  00000-0  20000-3 0  9010
2 25544  51
6311 234
6068 0008757 186
1953 173
9104 15
75963651 17784


Satellite: ISS
Catalog Number: 25544
Epoch time:      07212
56148752   =   yrday
fracday
Element set:     901
Inclination:       51
6311  deg
RA of node:       234
6068  deg
Eccentricity:     
0008757     
Arg of perigee:   186
1953  deg
Mean anomaly:     173
9104  deg
Mean motion:   15
75963651  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1778
Checksum:              306


Coasting Arc #3 (Orbit 1792)
---------------------------------------

Vector Time (GMT): 2007/213/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4817488
99                 A    =         6716912
60  meter
 Y    =         182760
09  meter          E    =           
0015223
 Z    =       -4690164
18                 I    =           51
37746
 XDOT =      -2892
872416                 Wp   =          143
90283
 YDOT =      -6594
458866  meter/sec      RA   =          228
83772  deg
 ZDOT =       2706
781467                 TA   =          152
90332
                                          MA   =          152
82378
                                          Ha   =            188
595  n
mi
                                          Hp   =            180
374

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15805410
06                 X    =        -4796391
09
 Y    =         599606
58  feet           Y    =          129006
44  meter
 Z    =      -15387677
74                 Z    =        -4713515
81
 XDOT =      -9491
051232                 XDOT =       -2832
065986
 YDOT =     -21635
363733  feet/sec       YDOT =       -6626
468761  meter/sec
 ZDOT =       8880
516623                 ZDOT =        2692
875501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10459949
13                 X    =         3188192
50
 Y    =       11748669
88  feet           Y    =         3580994
58  meter
 Z    =      -15476090
01                 Z    =        -4717112
23
 XDOT =      -9771
196629                 XDOT =       -2978
260732
 YDOT =      20359
827382  feet/sec       YDOT =        6205
675386  meter/sec
 ZDOT =       8827
032454                 ZDOT =        2690
479492


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   07213
51262995  
00020000  00000-0  20000-3 0  9023
2 25544  51
6318 229
7066 0008771 190
7465 169
3513 15
75966632 17931


Satellite: ISS
Catalog Number: 25544
Epoch time:      07213
51262995   =   yrday
fracday
Element set:     902
Inclination:       51
6318  deg
RA of node:       229
7066  deg
Eccentricity:     
0008771     
Arg of perigee:   190
7465  deg
Mean anomaly:     169
3513  deg
Mean motion:   15
75966632  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1793
Checksum:              316


Coasting Arc #4 (Orbit 1808)
---------------------------------------

Vector Time (GMT): 2007/214/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2381231
55                 A    =         6722754
44  meter
 Y    =        5541611
58  meter          E    =           
0010455
 Z    =       -2957901
16                 I    =           51
41623
 XDOT =      -5879
326732                 Wp   =          169
00508
 YDOT =       -124
649758  meter/sec      RA   =          223
71406  deg
 ZDOT =      -4979
620314                 TA   =           45
27727
                                          MA   =           45
19219
                                          Ha   =            188
484  n
mi
                                          Hp   =            180
681

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7812439
48                 X    =         2333456
19
 Y    =       18181140
36  feet           Y    =         5567972
85  meter
 Z    =       -9704400
14                 Z    =        -2946449
13
 XDOT =     -19289
129698                 XDOT =       -5853
306187
 YDOT =       -408
955899  feet/sec       YDOT =        -190
250010  meter/sec
 ZDOT =     -16337
336987                 ZDOT =       -5008
118455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8722317
16                 X    =         2658562
27
 Y    =      -17786585
57  feet           Y    =        -5421351
28  meter
 Z    =       -9660332
03                 Z    =        -2944469
20
 XDOT =      10854
398175                 XDOT =        3308
420564
 YDOT =      14231
443264  feet/sec       YDOT =        4337
743907  meter/sec
 ZDOT =     -16445
282799                 ZDOT =       -5012
522197


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   07214
52717676  
00020000  00000-0  20000-3 0  9037
2 25544  51
6309 224
4793 0008800 194
3248 165
7668 15
75983456 18094


Satellite: ISS
Catalog Number: 25544
Epoch time:      07214
52717676   =   yrday
fracday
Element set:     903
Inclination:       51
6309  deg
RA of node:       224
4793  deg
Eccentricity:     
0008800     
Arg of perigee:   194
3248  deg
Mean anomaly:     165
7668  deg
Mean motion:   15
75983456  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1809
Checksum:              323


Coasting Arc #5 (Orbit 1824)
---------------------------------------

Vector Time (GMT): 2007/215/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5437384
88                 A    =         6719587
41  meter
 Y    =         327156
94  meter          E    =           
0010106
 Z    =        3922971
47                 I    =           51
42757
 XDOT =       2523
064855                 Wp   =          127
32427
 YDOT =       6086
372650  meter/sec      RA   =          218
49694  deg
 ZDOT =      -4003
636981                 TA   =            4
30261
                                          MA   =            4
29393
                                          Ha   =            188
095  n
mi
                                          Hp   =            180
850

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17839189
23                 X    =         5414265
53
 Y    =        1073349
55  feet           Y    =          387831
42  meter
 Z    =       12870641
29                 Z    =         3949329
89
 XDOT =       8277
771833                 XDOT =        2474
267379
 YDOT =      19968
414207  feet/sec       YDOT =        6114
314299  meter/sec
 ZDOT =     -13135
291932                 ZDOT =       -3991
498336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10960266
41                 X    =        -3340689
20
 Y    =      -14024282
50  feet           Y    =        -4274601
31  meter
 Z    =       12970513
47                 Z    =         3953412
51
 XDOT =       8410
856833                 XDOT =        2563
629163
 YDOT =     -18681
357145  feet/sec       YDOT =       -5694
077658  meter/sec
 ZDOT =     -13088
549119                 ZDOT =       -3989
389771


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   07215
54171647  
00020000  00000-0  20000-3 0  9043
2 25544  51
6305 219
2525 0008641 198
6564 161
4284 15
76027726 18251


Satellite: ISS
Catalog Number: 25544
Epoch time:      07215
54171647   =   yrday
fracday
Element set:     904
Inclination:       51
6305  deg
RA of node:       219
2525  deg
Eccentricity:     
0008641     
Arg of perigee:   198
6564  deg
Mean anomaly:     161
4284  deg
Mean motion:   15
76027726  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1825
Checksum:              296


Coasting Arc #6 (Orbit 1840)
---------------------------------------

Vector Time (GMT): 2007/216/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1940678
13                 A    =         6719614
77  meter
 Y    =       -5065080
89  meter          E    =           
0012552
 Z    =        3967531
54                 I    =           51
45034
 XDOT =       6589
013946                 Wp   =          143
82426
 YDOT =        577
839340  meter/sec      RA   =          213
38350  deg
 ZDOT =       3944
321789                 TA   =          265
19190
                                          MA   =          265
33524
                                          Ha   =            188
090  n
mi
                                          Hp   =            181
102

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6367054
24                 X    =        -1903168
87
 Y    =      -16617719
47  feet           Y    =        -5086573
13  meter
 Z    =       13016835
75                 Z    =         3958194
61
 XDOT =      21617
499824                 XDOT =        6562
902040
 YDOT =       1895
798358  feet/sec       YDOT =         651
375199  meter/sec
 ZDOT =      12940
688285                 ZDOT =        3976
267676

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7914792
00                 X    =        -2412428
60
 Y    =       15968096
15  feet           Y    =         4867075
71  meter
 Z    =       12980830
72                 Z    =         3956557
20
 XDOT =     -11978
520560                 XDOT =       -3651
053067
 YDOT =     -16599
150412  feet/sec       YDOT =       -5059
421046  meter/sec
 ZDOT =      13061
760791                 ZDOT =        3981
224689


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   07216
55625072  
00020000  00000-0  20000-3 0  9052
2 25544  51
6301 214
0258 0008653 203
0355 157
0422 15
76022629 18415


Satellite: ISS
Catalog Number: 25544
Epoch time:      07216
55625072   =   yrday
fracday
Element set:     905
Inclination:       51
6301  deg
RA of node:       214
0258  deg
Eccentricity:     
0008653     
Arg of perigee:   203
0355  deg
Mean anomaly:     157
0422  deg
Mean motion:   15
76022629  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1841
Checksum:              259


Coasting Arc #7 (Orbit 1855)
---------------------------------------

Vector Time (GMT): 2007/217/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6040949
83                 A    =         6722717
10  meter
 Y    =        -625307
26  meter          E    =           
0005855
 Z    =       -2890844
17                 I    =           51
48582
 XDOT =      -1838
038321                 Wp   =          176
01793
 YDOT =      -5526
318636  meter/sec      RA   =          208
17023  deg
 ZDOT =       5031
156119                 TA   =          150
66395
                                          MA   =          150
63107
                                          Ha   =            187
915  n
mi
                                          Hp   =            181
201

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19819389
21                 X    =        -6019465
41
 Y    =       -2051533
02  feet           Y    =         -692740
22  meter
 Z    =       -9484396
87                 Z    =        -2920138
90
 XDOT =      -6030
309453                 XDOT =       -1800
545993
 YDOT =     -18130
966652  feet/sec       YDOT =       -5546
663371  meter/sec
 ZDOT =      16506
417713                 ZDOT =        5022
317593

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12100399
80                 X    =         3688201
86
 Y    =       15763203
45  feet           Y    =         4804624
41  meter
 Z    =       -9595441
74                 Z    =        -2924690
64
 XDOT =      -7806
374904                 XDOT =       -2379
383071
 YDOT =      16029
647610  feet/sec       YDOT =        4885
836592  meter/sec
 ZDOT =      16472
240982                 ZDOT =        5020
739051


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   07217
50737058  
00020000  00000-0  20000-3 0  9067
2 25544  51
6300 209
1260 0008521 206
0868 153
9868 15
76016406 18569


Satellite: ISS
Catalog Number: 25544
Epoch time:      07217
50737058   =   yrday
fracday
Element set:     906
Inclination:       51
6300  deg
RA of node:       209
1260  deg
Eccentricity:     
0008521     
Arg of perigee:   206
0868  deg
Mean anomaly:     153
9868  deg
Mean motion:   15
76016406  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1856
Checksum:              288


Coasting Arc #8 (Orbit 1871)
---------------------------------------

Vector Time (GMT): 2007/218/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1202721
17                 A    =         6716663
14  meter
 Y    =        4609670
99  meter          E    =           
0007468
 Z    =       -4738756
27                 I    =           51
49063
 XDOT =      -7198
368292                 Wp   =          120
11910
 YDOT =       -802
475020  meter/sec      RA   =          203
05201  deg
 ZDOT =      -2614
346157                 TA   =          124
20254
                                          MA   =          124
13174
                                          Ha   =            187
736  n
mi
                                          Hp   =            181
537

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3945935
60                 X    =         1174105
72
 Y    =       15123592
49  feet           Y    =         4622960
99  meter
 Z    =      -15547100
63                 Z    =        -4732982
49
 XDOT =     -23616
693870                 XDOT =       -7176
159914
 YDOT =      -2632
792059  feet/sec       YDOT =        -882
846781  meter/sec
 ZDOT =      -8577
251172                 ZDOT =       -2649
261879

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7978413
48                 X    =         2431820
43
 Y    =      -13466106
00  feet           Y    =        -4104469
11  meter
 Z    =      -15524648
24                 Z    =        -4731912
78
 XDOT =      13634
058545                 XDOT =        4155
661044
 YDOT =      18093
413596  feet/sec       YDOT =        5514
872464  meter/sec
 ZDOT =      -8709
622700                 ZDOT =       -2654
692999


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   07218
52189205  
00020000  00000-0  20000-3 0  9076
2 25544  51
6294 203
8983 0008520 210
4266 149
6405 15
76023861 18724


Satellite: ISS
Catalog Number: 25544
Epoch time:      07218
52189205   =   yrday
fracday
Element set:     907
Inclination:       51
6294  deg
RA of node:       203
8983  deg
Eccentricity:     
0008520     
Arg of perigee:   210
4266  deg
Mean anomaly:     149
6405  deg
Mean motion:   15
76023861  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1872
Checksum:              292


Coasting Arc #9 (Orbit 1887)
---------------------------------------

Vector Time (GMT): 2007/219/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6472581
18                 A    =         6725102
27  meter
 Y    =         718864
86  meter          E    =           
0015200
 Z    =        1637606
62                 I    =           51
54657
 XDOT =        890
675944                 Wp   =          149
40902
 YDOT =       5073
380770  meter/sec      RA   =          197
85615  deg
 ZDOT =      -5737
098445                 TA   =           12
44682
                                          MA   =           12
40932
                                          Ha   =            187
380  n
mi
                                          Hp   =            181
738

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21235502
56                 X    =         6456106
52
 Y    =        2358480
52  feet           Y    =          791152
59  meter
 Z    =        5372725
12                 Z    =         1669010
30
 XDOT =       2922
165169                 XDOT =         861
748069
 YDOT =      16644
950032  feet/sec       YDOT =        5083
179788  meter/sec
 ZDOT =     -18822
501459                 ZDOT =       -5732
841193

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13444798
03                 X    =        -4097974
44
 Y    =      -16566615
89  feet           Y    =        -5049504
52  meter
 Z    =        5491795
57                 Z    =         1673899
29
 XDOT =       8321
574324                 XDOT =        2536
415854
 YDOT =     -12998
517704  feet/sec       YDOT =       -3961
948196  meter/sec
 ZDOT =     -18805
735306                 ZDOT =       -5731
988121


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   07219
53640591  
00020000  00000-0  20000-3 0  9089
2 25544  51
6292 198
6716 0008406 215
5679 144
4926 15
76061359 18886


Satellite: ISS
Catalog Number: 25544
Epoch time:      07219
53640591   =   yrday
fracday
Element set:     908
Inclination:       51
6292  deg
RA of node:       198
6716  deg
Eccentricity:     
0008406     
Arg of perigee:   215
5679  deg
Mean anomaly:     144
4926  deg
Mean motion:   15
76061359  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1888
Checksum:              327


Coasting Arc #10 (Orbit 1903)
---------------------------------------

Vector Time (GMT): 2007/220/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -302996
44                 A    =         6714700
75  meter
 Y    =       -4278243
72  meter          E    =           
0008983
 Z    =        5169717
06                 I    =           51
53887
 XDOT =       7578
723753                 Wp   =          194
19785
 YDOT =        810
161353  meter/sec      RA   =          192
72344  deg
 ZDOT =       1106
481642                 TA   =          245
18327
                                          MA   =          245
27673
                                          Ha   =            187
321  n
mi
                                          Hp   =            181
983

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -994082
81                 X    =         -280247
23
 Y    =      -14036232
68  feet           Y    =        -4281505
50  meter
 Z    =       16961013
99                 Z    =         5168299
80
 XDOT =      24864
579241                 XDOT =        7563
726116
 YDOT =       2658
009687  feet/sec       YDOT =         894
826901  meter/sec
 ZDOT =       3630
189113                 ZDOT =        1143
262355

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8892165
21                 X    =        -2710331
96
 Y    =       10914841
69  feet           Y    =         3326843
75  meter
 Z    =       16955106
98                 Z    =         5167916
61
 XDOT =     -15360
087875                 XDOT =       -4681
754784
 YDOT =     -18411
047259  feet/sec       YDOT =       -5611
687204  meter/sec
 ZDOT =       3769
661977                 ZDOT =        1148
992970


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   07220
55091387  
00020000  00000-0  20000-3 0  9097
2 25544  51
6290 193
4449 0008451 219
7855 140
2690 15
76053034 19044


Satellite: ISS
Catalog Number: 25544
Epoch time:      07220
55091387   =   yrday
fracday
Element set:     909
Inclination:       51
6290  deg
RA of node:       193
4449  deg
Eccentricity:     
0008451     
Arg of perigee:   219
7855  deg
Mean anomaly:     140
2690  deg
Mean motion:   15
76053034  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1904
Checksum:              293


Coasting Arc #11 (Orbit 1918)
---------------------------------------

Vector Time (GMT): 2007/221/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6685573
59                 A    =         6726195
78  meter
 Y    =        -674168
33  meter          E    =           
0003171
 Z    =        -265824
98                 I    =           51
60641
 XDOT =        244
695319                 Wp   =           43
89956
 YDOT =      -4785
365251  meter/sec      RA   =          187
55460  deg
 ZDOT =       6027
195363                 TA   =          313
20948
                                          MA   =          313
23596
                                          Ha   =            187
132  n
mi
                                          Hp   =            182
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21934296
55                 X    =        -6676246
75
 Y    =       -2211838
34  feet           Y    =         -748877
99  meter
 Z    =        -872129
20                 Z    =         -298280
38
 XDOT =        802
806165                 XDOT =         268
909269
 YDOT =     -15700
017229  feet/sec       YDOT =       -4782
494330  meter/sec
 ZDOT =      19774
263002                 ZDOT =        6028
442263

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14638757
00                 X    =         4461893
13
 Y    =       16476727
46  feet           Y    =         5022106
53  meter
 Z    =        -995212
94                 Z    =         -303340
90
 XDOT =      -9938
826226                 XDOT =       -3029
354234
 YDOT =      10016
975026  feet/sec       YDOT =        3053
173988  meter/sec
 ZDOT =      19778
386477                 ZDOT =        6028
452198


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   07221
50200799  
00020000  00000-0  20000-3 0  9104
2 25544  51
6288 188
5445 0008466 222
3718 137
6793 15
76087283 19199


Satellite: ISS
Catalog Number: 25544
Epoch time:      07221
50200799   =   yrday
fracday
Element set:     910
Inclination:       51
6288  deg
RA of node:       188
5445  deg
Eccentricity:     
0008466     
Arg of perigee:   222
3718  deg
Mean anomaly:     137
6793  deg
Mean motion:   15
76087283  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1919
Checksum:              315


Coasting Arc #12 (Orbit 1934)
---------------------------------------

Vector Time (GMT): 2007/222/12:02:02
980
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -748575
02                 A    =         6714287
29  meter
 Y    =        4131784
16  meter          E    =           
0010942
 Z    =       -5247158
75                 I    =           51
59568
 XDOT =      -7646
283946                 Wp   =          127
61184
 YDOT =       -726
950816  meter/sec      RA   =          182
39843  deg
 ZDOT =        512
582225                 TA   =          147
29646
                                          MA   =          147
22867
                                          Ha   =            186
889  n
mi
                                          Hp   =            182
406

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2455954
78                 X    =         -769232
41
 Y    =       13555722
32  feet           Y    =         4123298
27  meter
 Z    =      -17215087
77                 Z    =        -5250844
96
 XDOT =     -25086
233420                 XDOT =       -7640
076768
 YDOT =      -2385
009239  feet/sec       YDOT =        -812
421220  meter/sec
 ZDOT =       1681
700214                 ZDOT =         475
452377

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10769616
86                 X    =         3282579
22
 Y    =       -8563961
49  feet           Y    =        -2610295
46  meter
 Z    =      -17228536
93                 Z    =        -5251258
06
 XDOT =      16546
854696                 XDOT =        5043
481311
 YDOT =      17670
180736  feet/sec       YDOT =        5385
871088  meter/sec
 ZDOT =       1540
875062                 ZDOT =         469
658719


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   07222
51650188  
00020000  00000-0  20000-3 0  9118
2 25544  51
6297 183
3169 0008400 227
6682 132
3771 15
76068428 19357


Satellite: ISS
Catalog Number: 25544
Epoch time:      07222
51650188   =   yrday
fracday
Element set:     911
Inclination:       51
6297  deg
RA of node:       183
3169  deg
Eccentricity:     
0008400     
Arg of perigee:   227
6682  deg
Mean anomaly:     132
3771  deg
Mean motion:   15
76068428  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1935
Checksum:              297

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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