Date: February 16th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7104 18 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


There are no maneuvers



Coasting Arc #1 (Orbit 3139)
---------------------------------------

Vector Time (GMT): 2007/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6438841
56                 A    =         6720065
87  meter
 Y    =       -1843786
37  meter          E    =           
0027435
 Z    =         231946
18                 I    =           51
74772
 XDOT =       1116
138125                 Wp   =          179
74703
 YDOT =      -4656
899281  meter/sec      RA   =           17
54381  deg
 ZDOT =      -6058
763712                 TA   =          357
72694
                                          MA   =          357
73938
                                          Ha   =            188
294  n
mi
                                          Hp   =            174
654

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21124808
27                 X    =        -6418872
26
 Y    =       -6049167
87  feet           Y    =        -1915677
44  meter
 Z    =         760978
29                 Z    =          200715
53
 XDOT =       3661
870490                 XDOT =        1197
560880
 YDOT =     -15278
540947  feet/sec       YDOT =       -4643
962441  meter/sec
 ZDOT =     -19877
833700                 ZDOT =       -6053
144119

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13355064
05                 X    =        -4070623
52
 Y    =      -17454433
88  feet           Y    =        -5320111
45  meter
 Z    =         643464
47                 Z    =          196127
97
 XDOT =      10865
489331                 XDOT =        3311
801148
 YDOT =      -9042
190366  feet/sec       YDOT =       -2756
059624  meter/sec
 ZDOT =     -19857
290305                 ZDOT =       -6052
502085


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   07045
53203413  
00020000  00000-0  20000-3 0  9006
2 25544  51
6324  17
8717 0021000 206
5229 153
4863 15
78266123 31402


Satellite: ISS
Catalog Number: 25544
Epoch time:      07045
53203413   =   yrday
fracday
Element set:     900
Inclination:       51
6324  deg
RA of node:        17
8717  deg
Eccentricity:     
0021000     
Arg of perigee:   206
5229  deg
Mean anomaly:     153
4863  deg
Mean motion:   15
78266123  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3140
Checksum:              250


Coasting Arc #2 (Orbit 3155)
---------------------------------------

Vector Time (GMT): 2007/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2337306
43                 A    =         6708539
17  meter
 Y    =        3638812
34  meter          E    =           
0017032
 Z    =        5131193
74                 I    =           51
68134
 XDOT =      -7101
691699                 Wp   =          203
79524
 YDOT =      -2661
541994  meter/sec      RA   =           12
37166  deg
 ZDOT =      -1364
303304                 TA   =          259
15074
                                          MA   =          259
34247
                                          Ha   =            188
065  n
mi
                                          Hp   =            174
863

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7668328
19                 X    =        -2402748
08
 Y    =       11938360
71  feet           Y    =         3612309
21  meter
 Z    =       16834625
13                 Z    =         5119680
62
 XDOT =     -23299
513447                 XDOT =       -7064
774816
 YDOT =      -8732
093155  feet/sec       YDOT =       -2740
750617  meter/sec
 ZDOT =      -4476
060709                 ZDOT =       -1398
712670

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13262182
53                 X    =        -4042313
24
 Y    =        5184730
41  feet           Y    =         1580305
83  meter
 Z    =       16791825
45                 Z    =         5118148
40
 XDOT =     -13457
021415                 XDOT =       -4101
700127
 YDOT =     -19685
514801  feet/sec       YDOT =       -6000
144911  meter/sec
 ZDOT =      -4605
619172                 ZDOT =       -1403
792724


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   07046
54510433  
00020000  00000-0  20000-3 0  9012
2 25544  51
6325  12
6355 0021008 210
5004 149
4941 15
78290762 31563


Satellite: ISS
Catalog Number: 25544
Epoch time:      07046
54510433   =   yrday
fracday
Element set:     901
Inclination:       51
6325  deg
RA of node:        12
6355  deg
Eccentricity:     
0021008     
Arg of perigee:   210
5004  deg
Mean anomaly:     149
4941  deg
Mean motion:   15
78290762  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3156
Checksum:              257


Coasting Arc #3 (Orbit 3171)
---------------------------------------

Vector Time (GMT): 2007/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5588824
52                 A    =         6716875
90  meter
 Y    =        2738775
60  meter          E    =           
0014424
 Z    =        2546858
77                 I    =           51
68271
 XDOT =      -4216
443764                 Wp   =          173
33283
 YDOT =       3674
051498  meter/sec      RA   =            7
23968  deg
 ZDOT =       5284
603426                 TA   =          215
52970
                                          MA   =          215
62583
                                          Ha   =            187
729  n
mi
                                          Hp   =            174
796

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18336038
45                 X    =         5545412
01
 Y    =        8985484
24  feet           Y    =         2801030
21  meter
 Z    =        8355835
85                 Z    =         2573902
93
 XDOT =     -13833
476916                 XDOT =       -4282
884949
 YDOT =      12053
974730  feet/sec       YDOT =        3626
529363  meter/sec
 ZDOT =      17337
937749                 ZDOT =        5263
959259

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9942555
72                 X    =         3030490
98
 Y    =       17787111
19  feet           Y    =         5421511
49  meter
 Z    =        8457747
16                 Z    =         2577921
33
 XDOT =     -17014
751394                 XDOT =       -5186
096225
 YDOT =       1277
037738  feet/sec       YDOT =         389
241102  meter/sec
 ZDOT =      17260
849256                 ZDOT =        5261
106853


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   07047
55814958  
00020000  00000-0  20000-3 0  9024
2 25544  51
6331   7
3984 0021145 214
3854 145
5944 15
78370177 31723


Satellite: ISS
Catalog Number: 25544
Epoch time:      07047
55814958   =   yrday
fracday
Element set:     902
Inclination:       51
6331  deg
RA of node:         7
3984  deg
Eccentricity:     
0021145     
Arg of perigee:   214
3854  deg
Mean anomaly:     145
5944  deg
Mean motion:   15
78370177  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3172
Checksum:              299


Coasting Arc #4 (Orbit 3186)
---------------------------------------

Vector Time (GMT): 2007/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4855362
65                 A    =         6713855
55  meter
 Y    =       -2776399
70  meter          E    =           
0019087
 Z    =       -3722892
39                 I    =           51
64367
 XDOT =       5327
490414                 Wp   =          202
02878
 YDOT =       3565
272125  meter/sec      RA   =            2
02353  deg
 ZDOT =       4264
782711                 TA   =          113
01176
                                          MA   =          112
81033
                                          Ha   =            187
454  n
mi
                                          Hp   =            175
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15929667
50                 X    =         4904132
44
 Y    =       -9108922
90  feet           Y    =        -2721831
75  meter
 Z    =      -12214213
88                 Z    =        -3699187
28
 XDOT =      17478
643092                 XDOT =        5266
510224
 YDOT =      11697
087024  feet/sec       YDOT =        3624
506265  meter/sec
 ZDOT =      13992
069262                 ZDOT =        4290
514586

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18364253
66                 X    =         5597424
52
 Y    =        1280514
35  feet           Y    =          390300
77  meter
 Z    =      -12125521
60                 Z    =        -3695858
98
 XDOT =       8098
226800                 XDOT =        2468
339529
 YDOT =      18039
217097  feet/sec       YDOT =        5498
353371  meter/sec
 ZDOT =      14089
157634                 ZDOT =        4294
375247


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   07048
50786147  
00020000  00000-0  20000-3 0  9039
2 25544  51
6333   2
4887 0020949 218
3497 141
6180 15
78354273 31875


Satellite: ISS
Catalog Number: 25544
Epoch time:      07048
50786147   =   yrday
fracday
Element set:     903
Inclination:       51
6333  deg
RA of node:         2
4887  deg
Eccentricity:     
0020949     
Arg of perigee:   218
3497  deg
Mean anomaly:     141
6180  deg
Mean motion:   15
78354273  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3187
Checksum:              306


Coasting Arc #5 (Orbit 3202)
---------------------------------------

Vector Time (GMT): 2007/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3439135
18                 A    =         6710289
95  meter
 Y    =       -3462076
81  meter          E    =           
0012518
 Z    =       -4596960
34                 I    =           51
60470
 XDOT =       6610
465367                 Wp   =          197
91838
 YDOT =      -2685
290063  meter/sec      RA   =          356
90183  deg
 ZDOT =      -2932
765780                 TA   =           43
11332
                                          MA   =           43
01535
                                          Ha   =            187
014  n
mi
                                          Hp   =            175
178

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11283251
91                 X    =        -3377835
59
 Y    =      -11358519
72  feet           Y    =        -3500192
66  meter
 Z    =      -15081890
88                 Z    =        -4613518
08
 XDOT =      21687
878501                 XDOT =        6654
247797
 YDOT =      -8810
006769  feet/sec       YDOT =       -2611
123515  meter/sec
 ZDOT =      -9621
934974                 ZDOT =       -2900
546578

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3298872
96                 X    =        -1005496
48
 Y    =      -15606165
01  feet           Y    =        -4756759
09  meter
 Z    =      -15144511
46                 Z    =        -4616047
09
 XDOT =      21919
796726                 XDOT =        6681
154042
 YDOT =       4556
242414  feet/sec       YDOT =        1388
742688  meter/sec
 ZDOT =      -9501
257831                 ZDOT =       -2895
983387


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   07049
52086381  
00020000  00000-0  20000-3 0  9046
2 25544  51
6343 357
2518 0020916 222
2417 137
7138 15
78416746 32030


Satellite: ISS
Catalog Number: 25544
Epoch time:      07049
52086381   =   yrday
fracday
Element set:     904
Inclination:       51
6343  deg
RA of node:       357
2518  deg
Eccentricity:     
0020916     
Arg of perigee:   222
2417  deg
Mean anomaly:     137
7138  deg
Mean motion:   15
78416746  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3203
Checksum:              288


Coasting Arc #6 (Orbit 3218)
---------------------------------------

Vector Time (GMT): 2007/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6329406
09                 A    =         6719035
20  meter
 Y    =        1870469
48  meter          E    =           
0022301
 Z    =        1182287
44                 I    =           51
60612
 XDOT =      -2386
825872                 Wp   =          188
20172
 YDOT =      -4372
668170  meter/sec      RA   =          351
69715  deg
 ZDOT =      -5895
269660                 TA   =          338
79677
                                          MA   =          338
88906
                                          Ha   =            186
838  n
mi
                                          Hp   =            175
299

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20765768
02                 X    =        -6355594
74
 Y    =        6136710
89  feet           Y    =         1799544
18  meter
 Z    =        3878895
82                 Z    =         1151476
16
 XDOT =      -7830
793544                 XDOT =       -2309
115185
 YDOT =     -14346
024181  feet/sec       YDOT =       -4398
924914  meter/sec
 ZDOT =     -19341
435891                 ZDOT =       -5906
675520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20913014
56                 X    =        -6374286
84
 Y    =       -5692516
08  feet           Y    =        -1735078
90  meter
 Z    =        3763410
33                 Z    =         1147087
47
 XDOT =        545
070397                 XDOT =         166
137457
 YDOT =     -14739
304437  feet/sec       YDOT =       -4492
539992  meter/sec
 ZDOT =     -19384
821601                 ZDOT =       -5908
493624


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   07050
53384363  
00020000  00000-0  20000-3 0  9051
2 25544  51
6349 352
0155 0020945 226
0288 133
9151 15
78429734 32197


Satellite: ISS
Catalog Number: 25544
Epoch time:      07050
53384363   =   yrday
fracday
Element set:     905
Inclination:       51
6349  deg
RA of node:       352
0155  deg
Eccentricity:     
0020945     
Arg of perigee:   226
0288  deg
Mean anomaly:     133
9151  deg
Mean motion:   15
78429734  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3219
Checksum:              290


Coasting Arc #7 (Orbit 3234)
---------------------------------------

Vector Time (GMT): 2007/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         599681
04                 A    =         6707366
72  meter
 Y    =        4144712
98  meter          E    =           
0018605
 Z    =        5250288
52                 I    =           51
53925
 XDOT =      -7539
587353                 Wp   =          226
70778
 YDOT =       1518
859693  meter/sec      RA   =          346
53158  deg
 ZDOT =       -351
184768                 TA   =          226
55426
                                          MA   =          226
70919
                                          Ha   =            186
410  n
mi
                                          Hp   =            175
303

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1967457
47                 X    =          527785
17
 Y    =       13598139
70  feet           Y    =         4151017
33  meter
 Z    =       17225356
03                 Z    =         5253026
79
 XDOT =     -24736
178979                 XDOT =       -7554
305140
 YDOT =       4983
135476  feet/sec       YDOT =        1434
465500  meter/sec
 ZDOT =      -1152
180997                 ZDOT =        -387
847317

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5330561
79                 X    =        -1624755
23
 Y    =       12648836
70  feet           Y    =         3855365
43  meter
 Z    =       17236160
36                 Z    =         5253581
68
 XDOT =     -22886
987116                 XDOT =       -6975
953673
 YDOT =      -7947
298830  feet/sec       YDOT =       -2422
336683  meter/sec
 ZDOT =      -1289
681059                 ZDOT =        -393
094787


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   07051
54679847  
00020000  00000-0  20000-3 0  9068
2 25544  51
6349 346
7791 0020976 230
3025 129
6291 15
78497887 32353


Satellite: ISS
Catalog Number: 25544
Epoch time:      07051
54679847   =   yrday
fracday
Element set:     906
Inclination:       51
6349  deg
RA of node:       346
7791  deg
Eccentricity:     
0020976     
Arg of perigee:   230
3025  deg
Mean anomaly:     129
6291  deg
Mean motion:   15
78497887  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3235
Checksum:              333


Coasting Arc #8 (Orbit 3250)
---------------------------------------

Vector Time (GMT): 2007/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6444862
54                 A    =         6717895
64  meter
 Y    =        -670098
96  meter          E    =           
0007700
 Z    =        1792515
40                 I    =           51
54724
 XDOT =      -1044
802423                 Wp   =          210
78585
 YDOT =       5101
739095  meter/sec      RA   =          341
37399  deg
 ZDOT =       5667
903979                 TA   =          169
11936
                                          MA   =          169
10269
                                          Ha   =            186
133  n
mi
                                          Hp   =            175
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21144562
15                 X    =         6443169
08
 Y    =       -2198487
41  feet           Y    =         -598038
28  meter
 Z    =        5880956
04                 Z    =         1823820
08
 XDOT =      -3427
829473                 XDOT =       -1129
306466
 YDOT =      16737
989158  feet/sec       YDOT =        5089
583350  meter/sec
 ZDOT =      18595
485496                 ZDOT =        5662
622859

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19426943
92                 X    =         5921332
51
 Y    =        8551262
89  feet           Y    =         2606424
93  meter
 Z    =        5998437
50                 Z    =         1828323
75
 XDOT =     -10737
355445                 XDOT =       -3272
745940
 YDOT =      11372
156392  feet/sec       YDOT =        3466
233268  meter/sec
 ZDOT =      18576
291567                 ZDOT =        5662
053670


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   07052
55973149  
00020000  00000-0  20000-3 0  9073
2 25544  51
6346 341
5409 0020941 234
1617 125
7603 15
78516631 32511


Satellite: ISS
Catalog Number: 25544
Epoch time:      07052
55973149   =   yrday
fracday
Element set:     907
Inclination:       51
6346  deg
RA of node:       341
5409  deg
Eccentricity:     
0020941     
Arg of perigee:   234
1617  deg
Mean anomaly:     125
7603  deg
Mean motion:   15
78516631  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3251
Checksum:              286


Coasting Arc #9 (Orbit 3265)
---------------------------------------

Vector Time (GMT): 2007/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2307663
55                 A    =         6711512
12  meter
 Y    =       -4685850
85  meter          E    =           
0017191
 Z    =       -4214982
06                 I    =           51
49940
 XDOT =       6817
754258                 Wp   =          214
98791
 YDOT =        108
936679  meter/sec      RA   =          336
15282  deg
 ZDOT =       3590
462977                 TA   =           91
64801
                                          MA   =           91
45109
                                          Ha   =            185
817  n
mi
                                          Hp   =            175
432

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7571074
65                 X    =         2380365
31
 Y    =      -15373526
41  feet           Y    =        -4659638
89  meter
 Z    =      -13828681
31                 Z    =        -4203594
82
 XDOT =      22367
960165                 XDOT =        6798
587758
 YDOT =        357
403801  feet/sec       YDOT =         185
069552  meter/sec
 ZDOT =      11779
734177                 ZDOT =        3623
536735

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14093982
10                 X    =         4295845
74
 Y    =       -9807698
44  feet           Y    =        -2989386
48  meter
 Z    =      -13786501
82                 Z    =        -4202125
75
 XDOT =      18672
040436                 XDOT =        5691
237925
 YDOT =      10001
606516  feet/sec       YDOT =        3048
489666  meter/sec
 ZDOT =      11903
956173                 ZDOT =        3628
325841


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   07053
50933441  
00020000  00000-0  20000-3 0  9081
2 25544  51
6349 336
6305 0020911 237
7728 122
1411 15
78559957 32665


Satellite: ISS
Catalog Number: 25544
Epoch time:      07053
50933441   =   yrday
fracday
Element set:     908
Inclination:       51
6349  deg
RA of node:       336
6305  deg
Eccentricity:     
0020911     
Arg of perigee:   237
7728  deg
Mean anomaly:     122
1411  deg
Mean motion:   15
78559957  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3266
Checksum:              298


Coasting Arc #10 (Orbit 3281)
---------------------------------------

Vector Time (GMT): 2007/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5132428
05                 A    =         6711261
88  meter
 Y    =        -978834
73  meter          E    =           
0012566
 Z    =       -4198586
59                 I    =           51
47406
 XDOT =       4010
187040                 Wp   =          236
17295
 YDOT =      -5512
084269  meter/sec      RA   =          331
02208  deg
 ZDOT =      -3616
265617                 TA   =          357
02168
                                          MA   =          357
02915
                                          Ha   =            185
315  n
mi
                                          Hp   =            175
425

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16838674
72                 X    =        -5100705
37
 Y    =       -3211400
03  feet           Y    =        -1036051
05  meter
 Z    =      -13774890
39                 Z    =        -4223442
60
 XDOT =      13156
781628                 XDOT =        4089
092887
 YDOT =     -18084
265975  feet/sec       YDOT =       -5466
798946  meter/sec
 ZDOT =     -11864
388506                 ZDOT =       -3596
592658

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13342111
55                 X    =        -4066675
60
 Y    =      -10642288
22  feet           Y    =        -3243769
45  meter
 Z    =      -13868360
49                 Z    =        -4227076
28
 XDOT =      19342
914372                 XDOT =        5895
720301
 YDOT =      -8881
034039  feet/sec       YDOT =       -2706
939175  meter/sec
 ZDOT =     -11791
191526                 ZDOT =       -3593
955177


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   07054
52222153  
00020000  00000-0  20000-3 0  9096
2 25544  51
6354 331
3932 0020854 241
8225 118
0834 15
78605992 32825


Satellite: ISS
Catalog Number: 25544
Epoch time:      07054
52222153   =   yrday
fracday
Element set:     909
Inclination:       51
6354  deg
RA of node:       331
3932  deg
Eccentricity:     
0020854     
Arg of perigee:   241
8225  deg
Mean anomaly:     118
0834  deg
Mean motion:   15
78605992  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3282
Checksum:              283


Coasting Arc #11 (Orbit 3297)
---------------------------------------

Vector Time (GMT): 2007/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4403755
26                 A    =         6717708
53  meter
 Y    =        4730138
74  meter          E    =           
0015832
 Z    =        1804193
86                 I    =           51
47093
 XDOT =      -4722
719166                 Wp   =          202
50136
 YDOT =      -2246
771879  meter/sec      RA   =          325
79716  deg
 ZDOT =      -5667
656845                 TA   =          317
39520
                                          MA   =          317
51791
                                          Ha   =            185
226  n
mi
                                          Hp   =            175
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14448015
94                 X    =        -4465085
38
 Y    =       15518827
88  feet           Y    =         4680550
54  meter
 Z    =        5919271
18                 Z    =         1782651
81
 XDOT =     -15494
485452                 XDOT =       -4669
712362
 YDOT =      -7371
298816  feet/sec       YDOT =       -2299
287497  meter/sec
 ZDOT =     -18594
674689                 ZDOT =       -5690
470786

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19915490
89                 X    =        -6070241
62
 Y    =        7341443
98  feet           Y    =         2237672
12  meter
 Z    =        5838953
45                 Z    =         1779713
01
 XDOT =      -9891
442824                 XDOT =       -3014
911773
 YDOT =     -12056
734512  feet/sec       YDOT =       -3674
892679  meter/sec
 ZDOT =     -18680
636200                 ZDOT =       -5693
857914


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   07055
53508611  
00020000  00000-0  20000-3 0  9106
2 25544  51
6352 326
1554 0020914 245
5297 114
3687 15
78609338 32982


Satellite: ISS
Catalog Number: 25544
Epoch time:      07055
53508611   =   yrday
fracday
Element set:     910
Inclination:       51
6352  deg
RA of node:       326
1554  deg
Eccentricity:     
0020914     
Arg of perigee:   245
5297  deg
Mean anomaly:     114
3687  deg
Mean motion:   15
78609338  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3298
Checksum:              300


Coasting Arc #12 (Orbit 3313)
---------------------------------------

Vector Time (GMT): 2007/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2931513
75                 A    =         6706806
84  meter
 Y    =        3007505
72  meter          E    =           
0018997
 Z    =        5244141
09                 I    =           51
41211
 XDOT =      -5780
744891                 Wp   =          245
00024
 YDOT =       5070
095152  meter/sec      RA   =          320
63096  deg
 ZDOT =        316
777806                 TA   =          201
94032
                                          MA   =          202
02177
                                          Ha   =            184
843  n
mi
                                          Hp   =            175
199

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9617827
26                 X    =         2872190
89
 Y    =        9867144
77  feet           Y    =         3039955
73  meter
 Z    =       17205187
29                 Z    =         5258238
10
 XDOT =     -18965
698462                 XDOT =       -5838
548606
 YDOT =      16634
170445  feet/sec       YDOT =        5005
128431  meter/sec
 ZDOT =       1039
297264                 ZDOT =         288
555173

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4287302
46                 X    =         1306769
79
 Y    =       13024766
33  feet           Y    =         3969948
78  meter
 Z    =       17258508
52                 Z    =         5260393
40
 XDOT =     -23365
434618                 XDOT =       -7121
784472
 YDOT =       6423
206053  feet/sec       YDOT =        1957
793205  meter/sec
 ZDOT =        933
927039                 ZDOT =         284
660961


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   07056
54792524  
00020000  00000-0  20000-3 0  9117
2 25544  51
6354 320
9170 0021013 249
7294 110
1613 15
78689441 33149


Satellite: ISS
Catalog Number: 25544
Epoch time:      07056
54792524   =   yrday
fracday
Element set:     911
Inclination:       51
6354  deg
RA of node:       320
9170  deg
Eccentricity:     
0021013     
Arg of perigee:   249
7294  deg
Mean anomaly:     110
1613  deg
Mean motion:   15
78689441  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3314
Checksum:              278

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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