Date: March 21st 2007

ISS TRAJECTORY DATA

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

Maneuvers contained within the current ephemeris are as follows:

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


There are no maneuvers



Coasting Arc #1 (Orbit 3659)
---------------------------------------

Vector Time (GMT): 2007/078/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6150007
04                 A    =         6718675
69  meter
 Y    =        -820667
19  meter          E    =           
0015720
 Z    =       -2550760
31                 I    =           51
49989
 XDOT =      -1460
997447                 Wp   =          344
01898
 YDOT =      -5433
197012  meter/sec      RA   =          206
68847  deg
 ZDOT =       5277
792776                 TA   =          346
91243
                                          MA   =          346
95318
                                          Ha   =            186
545  n
mi
                                          Hp   =            177
955

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20177188
44                 X    =        -6127982
08
 Y    =       -2692477
64  feet           Y    =         -889317
15  meter
 Z    =       -8368636
20                 Z    =        -2580583
26
 XDOT =      -4793
298712                 XDOT =       -1425
772476
 YDOT =     -17825
449513  feet/sec       YDOT =       -5449
337150  meter/sec
 ZDOT =      17315
593098                 ZDOT =        5270
781476

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17176068
17                 X    =        -5235265
58
 Y    =      -10837894
93  feet           Y    =        -3303390
38  meter
 Z    =       -8480870
05                 Z    =        -2584969
19
 XDOT =       2194
976539                 XDOT =         669
028849
 YDOT =     -16988
926569  feet/sec       YDOT =       -5178
224818  meter/sec
 ZDOT =      17288
452395                 ZDOT =        5269
520290


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07078
44822690  
00020000  00000-0  20000-3 0  9006
2 25544  51
6327 207
6431 0014653 324
7980  35
2215 15
77723459 36604


Satellite: ISS
Catalog Number: 25544
Epoch time:      07078
44822690   =   yrday
fracday
Element set:     900
Inclination:       51
6327  deg
RA of node:       207
6431  deg
Eccentricity:     
0014653     
Arg of perigee:   324
7980  deg
Mean anomaly:      35
2215  deg
Mean motion:   15
77723459  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3660
Checksum:              292


Coasting Arc #2 (Orbit 3675)
---------------------------------------

Vector Time (GMT): 2007/079/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         178795
44                 A    =         6710246
87  meter
 Y    =        4404842
52  meter          E    =           
0016615
 Z    =       -5067638
40                 I    =           51
49838
 XDOT =      -7372
123509                 Wp   =           20
74745
 YDOT =      -1549
176044  meter/sec      RA   =          201
55136  deg
 ZDOT =      -1592
956783                 TA   =          233
84673
                                          MA   =          234
00057
                                          Ha   =            186
822  n
mi
                                          Hp   =            177
586

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         586599
23                 X    =          154144
25
 Y    =       14451583
08  feet           Y    =         4406703
57  meter
 Z    =      -16626110
22                 Z    =        -5066830
13
 XDOT =     -24186
756920                 XDOT =       -7346
514192
 YDOT =      -5082
598569  feet/sec       YDOT =       -1631
472226  meter/sec
 ZDOT =      -5226
236166                 ZDOT =       -1628
708191

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5174673
26                 X    =        -1577240
41
 Y    =       13510633
25  feet           Y    =         4118041
01  meter
 Z    =      -16622437
82                 Z    =        -5066519
05
 XDOT =     -19104
865086                 XDOT =       -5823
162878
 YDOT =     -13968
231723  feet/sec       YDOT =       -4257
517029  meter/sec
 ZDOT =      -5360
866591                 ZDOT =       -1633
992137


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07079
46164728  
00020000  00000-0  20000-3 0  9011
2 25544  51
6331 202
4102 0014730 329
1621  30
8677 15
77779084 36769


Satellite: ISS
Catalog Number: 25544
Epoch time:      07079
46164728   =   yrday
fracday
Element set:     901
Inclination:       51
6331  deg
RA of node:       202
4102  deg
Eccentricity:     
0014730     
Arg of perigee:   329
1621  deg
Mean anomaly:      30
8677  deg
Mean motion:   15
77779084  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3676
Checksum:              292


Coasting Arc #3 (Orbit 3691)
---------------------------------------

Vector Time (GMT): 2007/080/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6478140
00                 A    =         6721316
82  meter
 Y    =        1798551
37  meter          E    =           
0005158
 Z    =         125143
37                 I    =           51
56292
 XDOT =      -1170
342414                 Wp   =           27
93439
 YDOT =       4642
083680  meter/sec      RA   =          196
36290  deg
 ZDOT =      -6027
602100                 TA   =          150
70417
                                          MA   =          150
67524
                                          Ha   =            186
977  n
mi
                                          Hp   =            177
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21253740
17                 X    =         6456938
95
 Y    =        5900759
07  feet           Y    =         1870875
02  meter
 Z    =         410575
37                 Z    =          156562
66
 XDOT =      -3839
706084                 XDOT =       -1192
882765
 YDOT =      15229
933332  feet/sec       YDOT =        4628
869788  meter/sec
 ZDOT =     -19775
597441                 ZDOT =       -6033
342732

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17336829
55                 X    =         5284265
65
 Y    =       13633178
03  feet           Y    =         4155392
66  meter
 Z    =         528960
10                 Z    =          161227
04
 XDOT =      -8315
581629                 XDOT =       -2534
589281
 YDOT =      11353
043757  feet/sec       YDOT =        3460
407737  meter/sec
 ZDOT =     -19796
515702                 ZDOT =       -6033
977986


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07080
47504341  
00020000  00000-0  20000-3 0  9024
2 25544  51
6326 197
1747 0014842 332
9002  27
1387 15
77817531 36922


Satellite: ISS
Catalog Number: 25544
Epoch time:      07080
47504341   =   yrday
fracday
Element set:     902
Inclination:       51
6326  deg
RA of node:       197
1747  deg
Eccentricity:     
0014842     
Arg of perigee:   332
9002  deg
Mean anomaly:      27
1387  deg
Mean motion:   15
77817531  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3692
Checksum:              288


Coasting Arc #4 (Orbit 3707)
---------------------------------------

Vector Time (GMT): 2007/081/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2246435
97                 A    =         6709808
40  meter
 Y    =       -3705749
08  meter          E    =           
0016257
 Z    =        5127726
46                 I    =           51
55283
 XDOT =       7168
108546                 Wp   =          352
26688
 YDOT =       2489
860852  meter/sec      RA   =          191
18281  deg
 ZDOT =      -1325
560098                 TA   =          110
51298
                                          MA   =          110
33843
                                          Ha   =            187
138  n
mi
                                          Hp   =            177
031

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7370196
74                 X    =         2262797
55
 Y    =      -12157969
41  feet           Y    =        -3680536
48  meter
 Z    =       16823249
56                 Z    =         5138679
59
 XDOT =      23517
416489                 XDOT =        7146
173173
 YDOT =       8168
834816  feet/sec       YDOT =        2569
895950  meter/sec
 ZDOT =      -4348
950452                 ZDOT =       -1290
790667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11252668
94                 X    =         3429813
49
 Y    =       -8610683
11  feet           Y    =        -2624536
21  meter
 Z    =       16863905
95                 Z    =         5140118
53
 XDOT =      18231
292454                 XDOT =        5556
897940
 YDOT =      15466
018652  feet/sec       YDOT =        4714
042485  meter/sec
 ZDOT =      -4217
863247                 ZDOT =       -1285
604718


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07081
48841740  
00020000  00000-0  20000-3 0  9034
2 25544  51
6334 191
9405 0014823 337
3076  22
7432 15
77815046 37082


Satellite: ISS
Catalog Number: 25544
Epoch time:      07081
48841740   =   yrday
fracday
Element set:     903
Inclination:       51
6334  deg
RA of node:       191
9405  deg
Eccentricity:     
0014823     
Arg of perigee:   337
3076  deg
Mean anomaly:      22
7432  deg
Mean motion:   15
77815046  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3708
Checksum:              288


Coasting Arc #5 (Orbit 3723)
---------------------------------------

Vector Time (GMT): 2007/082/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5755585
29                 A    =         6718725
35  meter
 Y    =       -2495826
79  meter          E    =           
0019922
 Z    =        2367637
79                 I    =           51
61254
 XDOT =       3907
741180                 Wp   =           25
66228
 YDOT =      -3888
842311  meter/sec      RA   =          186
04603  deg
 ZDOT =       5400
934943                 TA   =            1
11202
                                          MA   =            1
10759
                                          Ha   =            187
269  n
mi
                                          Hp   =            176
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18883153
84                 X    =        -5738750
41
 Y    =       -8188408
09  feet           Y    =        -2560094
80  meter
 Z    =        7767840
53                 Z    =         2339718
04
 XDOT =      12820
673164                 XDOT =        3924
699527
 YDOT =     -12758
668999  feet/sec       YDOT =       -3845
048863  meter/sec
 ZDOT =      17719
602832                 ZDOT =        5419
960034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14812153
63                 X    =        -4514744
43
 Y    =      -14347441
99  feet           Y    =        -4373100
32  meter
 Z    =        7662498
68                 Z    =         2335529
60
 XDOT =      15363
067252                 XDOT =        4682
662899
 YDOT =      -6360
799414  feet/sec       YDOT =       -1938
771661  meter/sec
 ZDOT =      17790
594330                 ZDOT =        5422
573152


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07082
50176373  
00020000  00000-0  20000-3 0  9042
2 25544  51
6339 186
7061 0014814 340
9221  19
1387 15
77899830 37249


Satellite: ISS
Catalog Number: 25544
Epoch time:      07082
50176373   =   yrday
fracday
Element set:     904
Inclination:       51
6339  deg
RA of node:       186
7061  deg
Eccentricity:     
0014814     
Arg of perigee:   340
9221  deg
Mean anomaly:      19
1387  deg
Mean motion:   15
77899830  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3724
Checksum:              303


Coasting Arc #6 (Orbit 3738)
---------------------------------------

Vector Time (GMT): 2007/083/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4435894
99                 A    =         6714089
73  meter
 Y    =        3086012
49  meter          E    =           
0012505
 Z    =       -3978213
31                 I    =           51
62565
 XDOT =      -5778
331784                 Wp   =           13
35163
 YDOT =      -3219
931396  meter/sec      RA   =          180
83324  deg
 ZDOT =       3959
733779                 TA   =          297
51567
                                          MA   =          297
64270
                                          Ha   =            187
378  n
mi
                                          Hp   =            176
375

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14553461
25                 X    =        -4450748
14
 Y    =       10124712
90  feet           Y    =         3036324
79  meter
 Z    =      -13051880
93                 Z    =        -3999798
92
 XDOT =     -18957
781444                 XDOT =       -5761
132219
 YDOT =     -10564
079383  feet/sec       YDOT =       -3284
451766  meter/sec
 ZDOT =      12991
252555                 ZDOT =        3931
704484

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17046487
16                 X    =        -5195769
29
 Y    =        4649306
49  feet           Y    =         1417108
62  meter
 Z    =      -13132626
02                 Z    =        -4002824
41
 XDOT =     -14014
313638                 XDOT =       -4271
562797
 YDOT =     -15119
046140  feet/sec       YDOT =       -4608
285263  meter/sec
 ZDOT =      12885
385796                 ZDOT =        3927
465591


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07083
45175684  
00020000  00000-0  20000-3 0  9052
2 25544  51
6337 181
7996 0015024 344
4275  15
6426 15
77897723 37391


Satellite: ISS
Catalog Number: 25544
Epoch time:      07083
45175684   =   yrday
fracday
Element set:     905
Inclination:       51
6337  deg
RA of node:       181
7996  deg
Eccentricity:     
0015024     
Arg of perigee:   344
4275  deg
Mean anomaly:      15
6426  deg
Mean motion:   15
77897723  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3739
Checksum:              325


Coasting Arc #7 (Orbit 3754)
---------------------------------------

Vector Time (GMT): 2007/084/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4072309
86                 A    =         6712902
82  meter
 Y    =        3133961
75  meter          E    =           
0018546
 Z    =       -4334549
64                 I    =           51
65073
 XDOT =      -6110
948156                 Wp   =           16
74437
 YDOT =       3178
338912  meter/sec      RA   =          175
71796  deg
 ZDOT =      -3429
422251                 TA   =          218
55681
                                          MA   =          218
68941
                                          Ha   =            187
564  n
mi
                                          Hp   =            176
205

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13360596
66                 X    =         4058019
10
 Y    =       10282026
75  feet           Y    =         3179420
71  meter
 Z    =      -14220963
39                 Z    =        -4314801
20
 XDOT =     -20049
042508                 XDOT =       -6129
375222
 YDOT =      10427
621102  feet/sec       YDOT =        3109
899850  meter/sec
 ZDOT =     -11251
385339                 ZDOT =       -3459
153783

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9428673
15                 X    =         2873859
58
 Y    =       14051524
61  feet           Y    =         4282904
70  meter
 Z    =      -14146243
16                 Z    =        -4311774
92
 XDOT =     -21250
820333                 XDOT =       -6477
250038
 YDOT =       2774
219602  feet/sec       YDOT =         845
582135  meter/sec
 ZDOT =     -11362
767473                 ZDOT =       -3463
371526


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   07084
46505873  
00020000  00000-0  20000-3 0  9062
2 25544  51
6340 176
5645 0014989 348
4340  11
6478 15
77936435 37559


Satellite: ISS
Catalog Number: 25544
Epoch time:      07084
46505873   =   yrday
fracday
Element set:     906
Inclination:       51
6340  deg
RA of node:       176
5645  deg
Eccentricity:     
0014989     
Arg of perigee:   348
4340  deg
Mean anomaly:      11
6478  deg
Mean motion:   15
77936435  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3755
Checksum:              323


Coasting Arc #8 (Orbit 3770)
---------------------------------------

Vector Time (GMT): 2007/085/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5999883
79                 A    =         6719420
49  meter
 Y    =       -2441940
26  meter          E    =           
0014340
 Z    =        1797719
59                 I    =           51
70186
 XDOT =       3335
873709                 Wp   =           50
67564
 YDOT =       3988
080610  meter/sec      RA   =          170
51337  deg
 ZDOT =      -5677
285732                 TA   =          109
40221
                                          MA   =          109
24716
                                          Ha   =            187
664  n
mi
                                          Hp   =            175
753

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19684658
12                 X    =         6018011
10
 Y    =       -8011615
02  feet           Y    =        -2374744
84  meter
 Z    =        5898030
15                 Z    =         1826910
74
 XDOT =      10944
467549                 XDOT =        3318
609410
 YDOT =      13084
253970  feet/sec       YDOT =        4025
287656  meter/sec
 ZDOT =     -18626
265526                 ZDOT =       -5661
122196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21158028
42                 X    =         6448967
06
 Y    =       -1645090
35  feet           Y    =         -501423
54  meter
 Z    =        6007496
25                 Z    =         1831084
86
 XDOT =       6417
543084                 XDOT =        1956
067132
 YDOT =      14285
028574  feet/sec       YDOT =        4354
076709  meter/sec
 ZDOT =     -18564
901418                 ZDOT =       -5658
581952


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   07085
47833683  
00020000  00000-0  20000-3 0  9078
2 25544  51
6339 171
3297 0015020 352
8134   7
2814 15
77977086 37710


Satellite: ISS
Catalog Number: 25544
Epoch time:      07085
47833683   =   yrday
fracday
Element set:     907
Inclination:       51
6339  deg
RA of node:       171
3297  deg
Eccentricity:     
0015020     
Arg of perigee:   352
8134  deg
Mean anomaly:       7
2814  deg
Mean motion:   15
77977086  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3771
Checksum:              310


Coasting Arc #9 (Orbit 3786)
---------------------------------------

Vector Time (GMT): 2007/086/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1638809
13                 A    =         6708663
41  meter
 Y    =       -3850620
52  meter          E    =           
0014025
 Z    =        5240811
19                 I    =           51
69514
 XDOT =       7316
367803                 Wp   =            7
06760
 YDOT =      -2367
908965  meter/sec      RA   =          165
37282  deg
 ZDOT =        561
563034                 TA   =           77
68554
                                          MA   =           77
52856
                                          Ha   =            187
751  n
mi
                                          Hp   =            175
419

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5376670
39                 X    =        -1621087
69
 Y    =      -12633269
41  feet           Y    =        -3868847
40  meter
 Z    =       17194262
45                 Z    =         5232893
10
 XDOT =      24003
831376                 XDOT =        7339
574403
 YDOT =      -7768
730199  feet/sec       YDOT =       -2285
963480  meter/sec
 ZDOT =       1842
398405                 ZDOT =         597
161860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1599610
44                 X    =         -487561
26
 Y    =      -13674482
73  feet           Y    =        -4167982
34  meter
 Z    =       17163930
49                 Z    =         5231566
01
 XDOT =      24216
950649                 XDOT =        7381
326558
 YDOT =       -408
376917  feet/sec       YDOT =        -124
473284  meter/sec
 ZDOT =       1975
992494                 ZDOT =         602
282512


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   07086
49158935  
00020000  00000-0  20000-3 0  9082
2 25544  51
6347 166
0940 0015164 356
5218   3
5839 15
78060316 37871


Satellite: ISS
Catalog Number: 25544
Epoch time:      07086
49158935   =   yrday
fracday
Element set:     908
Inclination:       51
6347  deg
RA of node:       166
0940  deg
Eccentricity:     
0015164     
Arg of perigee:   356
5218  deg
Mean anomaly:       3
5839  deg
Mean motion:   15
78060316  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3787
Checksum:              315


Coasting Arc #10 (Orbit 3802)
---------------------------------------

Vector Time (GMT): 2007/087/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6452088
05                 A    =         6720414
95  meter
 Y    =        1608468
89  meter          E    =           
0025877
 Z    =         850600
89                 I    =           51
76227
 XDOT =       -417
034323                 Wp   =           25
83412
 YDOT =      -4860
859605  meter/sec      RA   =          160
21667  deg
 ZDOT =       5983
735932                 TA   =          343
46239
                                          MA   =          343
54664
                                          Ha   =            187
974  n
mi
                                          Hp   =            175
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21168267
89                 X    =        -6473726
66
 Y    =        5277128
90  feet           Y    =         1536197
08  meter
 Z    =        2790685
33                 Z    =          819204
50
 XDOT =      -1368
222845                 XDOT =        -391
715961
 YDOT =     -15947
702117  feet/sec       YDOT =       -4865
381304  meter/sec
 ZDOT =      19631
679567                 ZDOT =        5981
771711

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21820422
14                 X    =        -6650864
67
 Y    =        -676003
27  feet           Y    =         -206045
80  meter
 Z    =        2672784
45                 Z    =          814664
70
 XDOT =       2861
085517                 XDOT =         872
058865
 YDOT =     -14158
370091  feet/sec       YDOT =       -4315
471204  meter/sec
 ZDOT =      19623
601658                 ZDOT =        5981
273785


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   07087
50482154  
00020000  00000-0  20000-3 0  9099
2 25544  51
6350 160
8595 0015313    
9521 359
1671 15
78047609 38039


Satellite: ISS
Catalog Number: 25544
Epoch time:      07087
50482154   =   yrday
fracday
Element set:     909
Inclination:       51
6350  deg
RA of node:       160
8595  deg
Eccentricity:     
0015313     
Arg of perigee:      
9521  deg
Mean anomaly:     359
1671  deg
Mean motion:   15
78047609  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3803
Checksum:              290


Coasting Arc #11 (Orbit 3817)
---------------------------------------

Vector Time (GMT): 2007/088/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -882463
80                 A    =         6710326
45  meter
 Y    =        4596914
34  meter          E    =           
0017228
 Z    =       -4814599
41                 I    =           51
75534
 XDOT =      -7193
888856                 Wp   =           47
82247
 YDOT =       1195
844226  meter/sec      RA   =          155
03182  deg
 ZDOT =       2477
289913                 TA   =          246
26344
                                          MA   =          246
44425
                                          Ha   =            187
979  n
mi
                                          Hp   =            174
731

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2895222
43                 X    =         -910413
45
 Y    =       15081739
95  feet           Y    =         4586889
56  meter
 Z    =      -15795929
81                 Z    =        -4818954
53
 XDOT =     -23601
997560                 XDOT =       -7218
760351
 YDOT =       3923
373444  feet/sec       YDOT =        1115
259225  meter/sec
 ZDOT =       8127
591577                 ZDOT =        2442
282019

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6561174
47                 X    =        -1999845
98
 Y    =       13867041
13  feet           Y    =         4226674
14  meter
 Z    =      -15811665
04                 Z    =        -4819395
51
 XDOT =     -22854
256162                 XDOT =       -6965
977278
 YDOT =      -1759
471694  feet/sec       YDOT =        -536
286972  meter/sec
 ZDOT =       7996
035251                 ZDOT =        2437
191544


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   07088
45470291  
00020000  00000-0  20000-3 0  9105
2 25544  51
6346 155
9523 0015309   4
7234 355
4073 15
78120569 38186


Satellite: ISS
Catalog Number: 25544
Epoch time:      07088
45470291   =   yrday
fracday
Element set:     910
Inclination:       51
6346  deg
RA of node:       155
9523  deg
Eccentricity:     
0015309     
Arg of perigee:     4
7234  deg
Mean anomaly:     355
4073  deg
Mean motion:   15
78120569  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3818
Checksum:              293


Coasting Arc #12 (Orbit 3833)
---------------------------------------

Vector Time (GMT): 2007/089/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5824824
62                 A    =         6715680
40  meter
 Y    =        -329233
79  meter          E    =           
0016427
 Z    =       -3347736
23                 I    =           51
79797
 XDOT =      -2373
007677                 Wp   =           25
42022
 YDOT =       5627
329056  meter/sec      RA   =          149
91953  deg
 ZDOT =      -4676
187895                 TA   =          193
87686
                                          MA   =          193
92206
                                          Ha   =            188
097  n
mi
                                          Hp   =            174
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19110316
99                 X    =         5844335
76
 Y    =       -1080163
34  feet           Y    =         -263988
51  meter
 Z    =      -10983386
58                 Z    =        -3319392
14
 XDOT =      -7785
458257                 XDOT =       -2413
041097
 YDOT =      18462
365668  feet/sec       YDOT =        5600
568548  meter/sec
 ZDOT =     -15341
823802                 ZDOT =       -4687
813517

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18875950
46                 X    =         5753389
70
 Y    =        3521361
51  feet           Y    =         1073310
99  meter
 Z    =      -10876776
02                 Z    =        -3315241
33
 XDOT =     -11622
432775                 XDOT =       -3542
517510
 YDOT =      14718
168796  feet/sec       YDOT =        4486
097849  meter/sec
 ZDOT =     -15384
770970                 ZDOT =       -4689
278192


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   07089
46788784  
00020000  00000-0  20000-3 0  9117
2 25544  51
6338 150
7166 0015306   8
4627 351
6794 15
78123288 38344


Satellite: ISS
Catalog Number: 25544
Epoch time:      07089
46788784   =   yrday
fracday
Element set:     911
Inclination:       51
6338  deg
RA of node:       150
7166  deg
Eccentricity:     
0015306     
Arg of perigee:     8
4627  deg
Mean anomaly:     351
6794  deg
Mean motion:   15
78123288  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3834
Checksum:              323

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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