Date: February 23rd 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7642 38 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 3250)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6433465
84                 A    =         6717671
19  meter
 Y    =        -616339
60  meter          E    =           
0007838
 Z    =        1851416
46                 I    =           51
54677
 XDOT =      -1133
381800                 Wp   =          209
08948
 YDOT =       5110
500547  meter/sec      RA   =          341
37860  deg
 ZDOT =       5642
910457                 TA   =          171
49939
                                          MA   =          171
48610
                                          Ha   =            186
074  n
mi
                                          Hp   =            175
285

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21107171
39                 X    =         6430885
95
 Y    =       -2022111
53  feet           Y    =         -544411
31  meter
 Z    =        6074200
98                 Z    =         1882663
62
 XDOT =      -3718
444225                 XDOT =       -1217
855819
 YDOT =      16766
734077  feet/sec       YDOT =        5097
354424  meter/sec
 ZDOT =      18513
485751                 ZDOT =        5637
199096

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19306138
46                 X    =         5884511
00
 Y    =        8685402
38  feet           Y    =         2647310
65  meter
 Z    =        6191473
17                 Z    =         1887161
02
 XDOT =     -10993
846542                 XDOT =       -3350
924426
 YDOT =      11262
160623  feet/sec       YDOT =        3432
706558  meter/sec
 ZDOT =      18492
677139                 ZDOT =        5636
567992


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
55960910  
00020000  00000-0  20000-3 0  9008
2 25544  51
6345 341
5457 0020932 233
9551 125
9675 15
78562240 32515


Satellite: ISS
Catalog Number: 25544
Epoch time:      07052
55960910   =   yrday
fracday
Element set:     900
Inclination:       51
6345  deg
RA of node:       341
5457  deg
Eccentricity:     
0020932     
Arg of perigee:   233
9551  deg
Mean anomaly:     125
9675  deg
Mean motion:   15
78562240  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3251
Checksum:              285


Coasting Arc #2 (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    =        2396500
88                 A    =         6711548
72  meter
 Y    =       -4683670
25  meter          E    =           
0017242
 Z    =       -4167702
21                 I    =           51
49981
 XDOT =       6777
457939                 Wp   =          215
60912
 YDOT =        189
770084  meter/sec      RA   =          336
15636  deg
 ZDOT =       3662
503795                 TA   =           91
88388
                                          MA   =           91
68640
                                          Ha   =            185
755  n
mi
                                          Hp   =            175
357

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7862535
70                 X    =         2468941
98
 Y    =      -15366372
22  feet           Y    =        -4656466
32  meter
 Z    =      -13673563
69                 Z    =        -4155884
04
 XDOT =      22235
754394                 XDOT =        6757
040586
 YDOT =        622
605263  feet/sec       YDOT =         265
445349  meter/sec
 ZDOT =      12016
088565                 ZDOT =        3695
378754

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14345395
59                 X    =         4372476
58
 Y    =       -9661797
10  feet           Y    =        -2944915
76  meter
 Z    =      -13629765
55                 Z    =        -4154352
54
 XDOT =      18438
157978                 XDOT =        5619
950552
 YDOT =      10151
697904  feet/sec       YDOT =        3094
237521  meter/sec
 ZDOT =      12139
574074                 ZDOT =        3700
142178


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
50918354  
00020000  00000-0  20000-3 0  9010
2 25544  51
6348 336
6352 0020905 237
5594 122
3550 15
78608697 32660


Satellite: ISS
Catalog Number: 25544
Epoch time:      07053
50918354   =   yrday
fracday
Element set:     901
Inclination:       51
6348  deg
RA of node:       336
6352  deg
Eccentricity:     
0020905     
Arg of perigee:   237
5594  deg
Mean anomaly:     122
3550  deg
Mean motion:   15
78608697  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3266
Checksum:              302


Coasting Arc #3 (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    =       -5068166
71                 A    =         6710905
76  meter
 Y    =       -1065957
12  meter          E    =           
0012251
 Z    =       -4254812
42                 I    =           51
47317
 XDOT =       4116
893754                 Wp   =          235
60340
 YDOT =      -5490
551097  meter/sec      RA   =          331
02514  deg
 ZDOT =      -3527
981876                 TA   =          358
63210
                                          MA   =          358
63545
                                          Ha   =            185
248  n
mi
                                          Hp   =            175
347

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16627843
54                 X    =        -5035201
46
 Y    =       -3497234
65  feet           Y    =        -1122447
89  meter
 Z    =      -13959358
32                 Z    =        -4279353
23
 XDOT =      13506
869271                 XDOT =        4195
122021
 YDOT =     -18013
619084  feet/sec       YDOT =       -5444
076308  meter/sec
 ZDOT =     -11574
743687                 ZDOT =       -3507
792187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13021583
95                 X    =        -3968978
79
 Y    =      -10796705
26  feet           Y    =        -3290835
76  meter
 Z    =      -14051655
52                 Z    =        -4282944
60
 XDOT =      19607
224425                 XDOT =        5976
282005
 YDOT =      -8679
721202  feet/sec       YDOT =       -2645
579022  meter/sec
 ZDOT =     -11499
603415                 ZDOT =       -3505
079121


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
52203852  
00020000  00000-0  20000-3 0  9024
2 25544  51
6353 331
3976 0020845 241
6048 118
3016 15
78657794 32825


Satellite: ISS
Catalog Number: 25544
Epoch time:      07054
52203852   =   yrday
fracday
Element set:     902
Inclination:       51
6353  deg
RA of node:       331
3976  deg
Eccentricity:     
0020845     
Arg of perigee:   241
6048  deg
Mean anomaly:     118
3016  deg
Mean motion:   15
78657794  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3282
Checksum:              291


Coasting Arc #4 (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    =       -4491019
27                 A    =         6717717
56  meter
 Y    =        4686689
20  meter          E    =           
0016231
 Z    =        1698011
98                 I    =           51
47132
 XDOT =      -4613
087069                 Wp   =          202
37504
 YDOT =      -2363
158796  meter/sec      RA   =          325
80095  deg
 ZDOT =      -5711
020994                 TA   =          318
75005
                                          MA   =          318
87257
                                          Ha   =            185
154  n
mi
                                          Hp   =            175
359

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14734315
19                 X    =        -4551341
24
 Y    =       15376276
92  feet           Y    =         4636130
82  meter
 Z    =        5570905
46                 Z    =         1676048
46
 XDOT =     -15134
800096                 XDOT =       -4558
576306
 YDOT =      -7753
145655  feet/sec       YDOT =       -2414
440037  meter/sec
 ZDOT =     -18736
945518                 ZDOT =       -5733
298698

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20105271
29                 X    =        -6128086
69
 Y    =        7086174
96  feet           Y    =         2159866
13  meter
 Z    =        5488999
40                 Z    =         1673047
02
 XDOT =      -9416
307325                 XDOT =       -2870
090473
 YDOT =     -12221
659121  feet/sec       YDOT =       -3725
161700  meter/sec
 ZDOT =     -18820
907547                 ZDOT =       -5736
612620


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
53486910  
00020000  00000-0  20000-3 0  9035
2 25544  51
6351 326
1596 0020909 245
3082 114
5906 15
78663233 32981


Satellite: ISS
Catalog Number: 25544
Epoch time:      07055
53486910   =   yrday
fracday
Element set:     903
Inclination:       51
6351  deg
RA of node:       326
1596  deg
Eccentricity:     
0020909     
Arg of perigee:   245
3082  deg
Mean anomaly:     114
5906  deg
Mean motion:   15
78663233  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3298
Checksum:              298


Coasting Arc #5 (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    =        2804976
41                 A    =         6706619
21  meter
 Y    =        3116643
55  meter          E    =           
0018914
 Z    =        5249232
87                 I    =           51
41184
 XDOT =      -5862
709927                 Wp   =          245
67172
 YDOT =       4982
730077  meter/sec      RA   =          320
63218  deg
 ZDOT =        167
181400                 TA   =          202
69384
                                          MA   =          202
77757
                                          Ha   =            184
764  n
mi
                                          Hp   =            175
113

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9202678
52                 X    =         2744417
83
 Y    =       10225208
51  feet           Y    =         3147671
64  meter
 Z    =       17221892
63                 Z    =         5262712
18
 XDOT =     -19234
612620                 XDOT =       -5918
803922
 YDOT =      16347
539622  feet/sec       YDOT =        4916
856340  meter/sec
 ZDOT =        548
495406                 ZDOT =         138
564738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3757715
03                 X    =         1145351
54
 Y    =       13166776
92  feet           Y    =         4013233
60  meter
 Z    =       17272907
40                 Z    =         5264782
18
 XDOT =     -23470
232839                 XDOT =       -7153
726969
 YDOT =       6087
997941  feet/sec       YDOT =        1855
621773  meter/sec
 ZDOT =        441
634377                 ZDOT =         134
610158


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
54767234  
00020000  00000-0  20000-3 0  9049
2 25544  51
6352 320
9210 0021012 249
5270 110
3639 15
78747998 33145


Satellite: ISS
Catalog Number: 25544
Epoch time:      07056
54767234   =   yrday
fracday
Element set:     904
Inclination:       51
6352  deg
RA of node:       320
9210  deg
Eccentricity:     
0021012     
Arg of perigee:   249
5270  deg
Mean anomaly:     110
3639  deg
Mean motion:   15
78747998  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3314
Checksum:              286


Coasting Arc #6 (Orbit 3329)
---------------------------------------

Vector Time (GMT): 2007/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5409725
35                 A    =         6717756
15  meter
 Y    =       -3716236
43  meter          E    =           
0007726
 Z    =        1437073
49                 I    =           51
42850
 XDOT =       1742
867349                 Wp   =          275
53010
 YDOT =       4766
703910  meter/sec      RA   =          315
45646  deg
 ZDOT =       5793
093599                 TA   =          100
34722
                                          MA   =          100
26011
                                          Ha   =            184
518  n
mi
                                          Hp   =            175
231

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17748442
74                 X    =         5443897
89
 Y    =      -12192376
74  feet           Y    =        -3655550
82  meter
 Z    =        4714808
04                 Z    =         1463436
26
 XDOT =       5718
068729                 XDOT =        1661
294696
 YDOT =      15638
792357  feet/sec       YDOT =        4785
737412  meter/sec
 ZDOT =      19006
212594                 ZDOT =        5801
362216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21200135
97                 X    =         6461801
44
 Y    =       -3643685
34  feet           Y    =        -1110595
29  meter
 Z    =        4813364
45                 Z    =         1467113
49
 XDOT =      -1723
513419                 XDOT =        -525
326890
 YDOT =      15005
154375  feet/sec       YDOT =        4573
571054  meter/sec
 ZDOT =      19037
866714                 ZDOT =        5802
741774


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   07057
56045341  
00020000  00000-0  20000-3 0  9051
2 25544  51
6355 315
6819 0020915 253
6711 106
2154 15
78749485 33308


Satellite: ISS
Catalog Number: 25544
Epoch time:      07057
56045341   =   yrday
fracday
Element set:     905
Inclination:       51
6355  deg
RA of node:       315
6819  deg
Eccentricity:     
0020915     
Arg of perigee:   253
6711  deg
Mean anomaly:     106
2154  deg
Mean motion:   15
78749485  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3330
Checksum:              291


Coasting Arc #7 (Orbit 3344)
---------------------------------------

Vector Time (GMT): 2007/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -285317
30                 A    =         6710155
49  meter
 Y    =       -5074310
48  meter          E    =           
0014221
 Z    =       -4375674
61                 I    =           51
38393
 XDOT =       6180
085067                 Wp   =          236
11116
 YDOT =      -3213
818330  meter/sec      RA   =          310
22931  deg
 ZDOT =       3308
479808                 TA   =           67
26853
                                          MA   =           67
11830
                                          Ha   =            184
288  n
mi
                                          Hp   =            175
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -936080
40                 X    =         -207298
77
 Y    =      -16648000
28  feet           Y    =        -5077064
81  meter
 Z    =      -14355887
82                 Z    =        -4376871
17
 XDOT =      20275
869644                 XDOT =        6199
491569
 YDOT =     -10544
023394  feet/sec       YDOT =       -3144
600684  meter/sec
 ZDOT =      10854
592545                 ZDOT =        3338
548962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5931947
34                 X    =         1808057
55
 Y    =      -15578725
89  feet           Y    =        -4748395
65  meter
 Z    =      -14361022
78                 Z    =        -4377239
74
 XDOT =      21614
801706                 XDOT =        6588
191560
 YDOT =      -1926
420002  feet/sec       YDOT =        -587
172817  meter/sec
 ZDOT =      10967
135818                 ZDOT =        3342
782997


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   07058
50991101  
00020000  00000-0  20000-3 0  9061
2 25544  51
6358 310
7710 0021015 257
3951 102
4864 15
78800839 33459


Satellite: ISS
Catalog Number: 25544
Epoch time:      07058
50991101   =   yrday
fracday
Element set:     906
Inclination:       51
6358  deg
RA of node:       310
7710  deg
Eccentricity:     
0021015     
Arg of perigee:   257
3951  deg
Mean anomaly:     102
4864  deg
Mean motion:   15
78800839  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3345
Checksum:              282


Coasting Arc #8 (Orbit 3360)
---------------------------------------

Vector Time (GMT): 2007/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5089463
46                 A    =         6711127
90  meter
 Y    =        1603334
44  meter          E    =           
0013686
 Z    =       -4057923
66                 I    =           51
37011
 XDOT =        950
007123                 Wp   =          267
23921
 YDOT =      -6643
509141  meter/sec      RA   =          305
08853  deg
 ZDOT =      -3806
081663                 TA   =          323
55384
                                          MA   =          323
64693
                                          Ha   =            184
020  n
mi
                                          Hp   =            175
020

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16697714
77                 X    =        -5087301
84
 Y    =        5260283
58  feet           Y    =         1546433
24  meter
 Z    =      -13313397
82                 Z    =        -4082642
31
 XDOT =       3116
821269                 XDOT =        1042
713896
 YDOT =     -21796
289832  feet/sec       YDOT =       -6632
367335  meter/sec
 ZDOT =     -12487
144565                 ZDOT =       -3801
241393

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17362862
96                 X    =        -5292200
63
 Y    =       -1593641
48  feet           Y    =         -485741
92  meter
 Z    =      -13406047
88                 Z    =        -4086163
40
 XDOT =      11268
734311                 XDOT =        3434
710218
 YDOT =     -17591
464383  feet/sec       YDOT =       -5361
878344  meter/sec
 ZDOT =     -12469
809803                 ZDOT =       -3800
798028


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   07059
52264197  
00020000  00000-0  20000-3 0  9073
2 25544  51
6357 305
5328 0021126 261
4945  98
3826 15
78836574 33611


Satellite: ISS
Catalog Number: 25544
Epoch time:      07059
52264197   =   yrday
fracday
Element set:     907
Inclination:       51
6357  deg
RA of node:       305
5328  deg
Eccentricity:     
0021126     
Arg of perigee:   261
4945  deg
Mean anomaly:      98
3826  deg
Mean motion:   15
78836574  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3361
Checksum:              316


Coasting Arc #9 (Orbit 3376)
---------------------------------------

Vector Time (GMT): 2007/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1776348
97                 A    =         6716805
23  meter
 Y    =        6182600
35  meter          E    =           
0010718
 Z    =        1923430
74                 I    =           51
37354
 XDOT =      -5286
408440                 Wp   =          226
73491
 YDOT =        216
055937  meter/sec      RA   =          299
85294  deg
 ZDOT =      -5603
416062                 TA   =          291
75307
                                          MA   =          291
86712
                                          Ha   =            183
974  n
mi
                                          Hp   =            175
065

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5827916
55                 X    =        -1854695
06
 Y    =       20284121
88  feet           Y    =         6162298
24  meter
 Z    =        6310468
29                 Z    =         1914610
96
 XDOT =     -17343
859710                 XDOT =       -5261
211950
 YDOT =        708
844939  feet/sec       YDOT =         157
081030  meter/sec
 ZDOT =     -18383
910965                 ZDOT =       -5629
035467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12981834
28                 X    =        -3956863
09
 Y    =       16652003
64  feet           Y    =         5075530
71  meter
 Z    =        6278134
70                 Z    =         1913575
46
 XDOT =     -15055
487019                 XDOT =       -4588
912443
 YDOT =      -4803
106883  feet/sec       YDOT =       -1463
986978  meter/sec
 ZDOT =     -18480
123914                 ZDOT =       -5632
741769


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   07060
53534958  
00020000  00000-0  20000-3 0  9082
2 25544  51
6354 300
2942 0020958 265
0958  94
7815 15
78850975 33774


Satellite: ISS
Catalog Number: 25544
Epoch time:      07060
53534958   =   yrday
fracday
Element set:     908
Inclination:       51
6354  deg
RA of node:       300
2942  deg
Eccentricity:     
0020958     
Arg of perigee:   265
0958  deg
Mean anomaly:      94
7815  deg
Mean motion:   15
78850975  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3377
Checksum:              328


Coasting Arc #10 (Orbit 3392)
---------------------------------------

Vector Time (GMT): 2007/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3978292
74                 A    =         6706180
31  meter
 Y    =        1379211
06  meter          E    =           
0018646
 Z    =        5235616
88                 I    =           51
32490
 XDOT =      -2941
849593                 Wp   =          266
70688
 YDOT =       7101
341903  meter/sec      RA   =          294
67929  deg
 ZDOT =        364
733540                 TA   =          179
81284
                                          MA   =          179
81214
                                          Ha   =            183
871  n
mi
                                          Hp   =            174
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13052141
54                 X    =         3937141
58
 Y    =        4524970
68  feet           Y    =         1423468
79  meter
 Z    =       17177220
74                 Z    =         5254842
84
 XDOT =      -9651
737511                 XDOT =       -3022
810931
 YDOT =      23298
365823  feet/sec       YDOT =        7067
991841  meter/sec
 ZDOT =       1196
632348                 ZDOT =         350
245360

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10500102
68                 X    =         3200431
30
 Y    =        8836794
42  feet           Y    =         2693454
94  meter
 Z    =       17249625
47                 Z    =         5257685
84
 XDOT =     -16668
273859                 XDOT =       -5080
489872
 YDOT =      17574
624589  feet/sec       YDOT =        5356
745575  meter/sec
 ZDOT =       1143
134290                 ZDOT =         348
427332


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   07061
54802960  
00020000  00000-0  20000-3 0  9096
2 25544  51
6352 295
0544 0021072 269
3619  90
5132 15
78915015 33931


Satellite: ISS
Catalog Number: 25544
Epoch time:      07061
54802960   =   yrday
fracday
Element set:     909
Inclination:       51
6352  deg
RA of node:       295
0544  deg
Eccentricity:     
0021072     
Arg of perigee:   269
3619  deg
Mean anomaly:      90
5132  deg
Mean motion:   15
78915015  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3393
Checksum:              289


Coasting Arc #11 (Orbit 3408)
---------------------------------------

Vector Time (GMT): 2007/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3169404
73                 A    =         6717275
52  meter
 Y    =       -5766954
77  meter          E    =           
0012238
 Z    =        1329721
87                 I    =           51
35122
 XDOT =       3741
126135                 Wp   =          311
98570
 YDOT =       3389
257593  meter/sec      RA   =          289
49299  deg
 ZDOT =       5824
372710                 TA   =           62
70556
                                          MA   =           62
58099
                                          Ha   =            183
835  n
mi
                                          Hp   =            174
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10398309
48                 X    =         3227196
70
 Y    =      -18920455
29  feet           Y    =        -5731189
48  meter
 Z    =        4362604
56                 Z    =         1345259
27
 XDOT =      12274
035876                 XDOT =        3674
655890
 YDOT =      11119
611524  feet/sec       YDOT =        3430
721763  meter/sec
 ZDOT =      19108
834352                 ZDOT =        5842
384918

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16181411
33                 X    =         4932094
17
 Y    =      -14274608
81  feet           Y    =        -4350900
77  meter
 Z    =        4420210
14                 Z    =         1347280
05
 XDOT =       6628
696459                 XDOT =        2020
426681
 YDOT =      13409
992831  feet/sec       YDOT =        4087
365815  meter/sec
 ZDOT =      19176
947220                 ZDOT =        5845
133513


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   07062
56068465  
00020000  00000-0  20000-3 0  9105
2 25544  51
6342 289
8140 0021241 273
3916  86
4820 15
78972349 34095


Satellite: ISS
Catalog Number: 25544
Epoch time:      07062
56068465   =   yrday
fracday
Element set:     910
Inclination:       51
6342  deg
RA of node:       289
8140  deg
Eccentricity:     
0021241     
Arg of perigee:   273
3916  deg
Mean anomaly:      86
4820  deg
Mean motion:   15
78972349  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3409
Checksum:              302


Coasting Arc #12 (Orbit 3423)
---------------------------------------

Vector Time (GMT): 2007/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2518710
44                 A    =         6709434
74  meter
 Y    =       -4386422
77  meter          E    =           
0012260
 Z    =       -4398060
58                 I    =           51
31570
 XDOT =       4127
056306                 Wp   =          266
50826
 YDOT =      -5645
741710  meter/sec      RA   =          284
25929  deg
 ZDOT =       3258
768473                 TA   =           36
29107
                                          MA   =           36
20798
                                          Ha   =            183
815  n
mi
                                          Hp   =            174
714

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8263485
68                 X    =        -2448109
10
 Y    =      -14391150
83  feet           Y    =        -4414194
04  meter
 Z    =      -14429332
61                 Z    =        -4410124
34
 XDOT =      13540
210978                 XDOT =        4174
050890
 YDOT =     -18522
774640  feet/sec       YDOT =       -5599
327607  meter/sec
 ZDOT =      10691
497616                 ZDOT =        3278
931945

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3091310
33                 X    =         -942231
39
 Y    =      -16263683
12  feet           Y    =        -4957170
61  meter
 Z    =      -14475236
41                 Z    =        -4412052
06
 XDOT =      17558
784382                 XDOT =        5351
917479
 YDOT =     -12944
833354  feet/sec       YDOT =       -3945
585206  meter/sec
 ZDOT =      10766
489942                 ZDOT =        3281
626134


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   07063
51002738  
00020000  00000-0  20000-3 0  9113
2 25544  51
6332 284
9012 0021276 277
1188  82
7559 15
79003246 34246


Satellite: ISS
Catalog Number: 25544
Epoch time:      07063
51002738   =   yrday
fracday
Element set:     911
Inclination:       51
6332  deg
RA of node:       284
9012  deg
Eccentricity:     
0021276     
Arg of perigee:   277
1188  deg
Mean anomaly:      82
7559  deg
Mean motion:   15
79003246  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3424
Checksum:              281

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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