Date: May 4th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5812 51 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 355)
---------------------------------------

Vector Time (GMT): 2007/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -106239
78                 A    =         6710782
16  meter
 Y    =       -4330968
38  meter          E    =           
0023199
 Z    =       -5144866
08                 I    =           51
50201
 XDOT =       7392
011364                 Wp   =          115
42293
 YDOT =      -1695
813549  meter/sec      RA   =          339
42787  deg
 ZDOT =       1269
556854                 TA   =          166
78596
                                          MA   =          166
72509
                                          Ha   =            188
117  n
mi
                                          Hp   =            175
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -348555
70                 X    =          -32809
01
 Y    =      -14209213
86  feet           Y    =        -4331745
59  meter
 Z    =      -16879481
89                 Z    =        -5145204
05
 XDOT =      24252
005786                 XDOT =        7404
257394
 YDOT =      -5563
692745  feet/sec       YDOT =       -1613
083529  meter/sec
 ZDOT =       4165
212774                 ZDOT =        1305
497669

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9194676
96                 X    =        -2802537
54
 Y    =      -10836099
84  feet           Y    =        -3302843
23  meter
 Z    =      -16881262
22                 Z    =        -5145408
73
 XDOT =      14438
330121                 XDOT =        4400
803021
 YDOT =     -18977
991768  feet/sec       YDOT =       -5784
491891  meter/sec
 ZDOT =       4300
373967                 ZDOT =        1310
753985


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   07122
51366528  
00020000  00000-0  20000-3 0  9007
2 25544  51
6338 339
8656 0010307 137
7825 222
4136 15
77480189  3566


Satellite: ISS
Catalog Number: 25544
Epoch time:      07122
51366528   =   yrday
fracday
Element set:     900
Inclination:       51
6338  deg
RA of node:       339
8656  deg
Eccentricity:     
0010307     
Arg of perigee:   137
7825  deg
Mean anomaly:     222
4136  deg
Mean motion:   15
77480189  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             356
Checksum:              295


Coasting Arc #2 (Orbit 371)
---------------------------------------

Vector Time (GMT): 2007/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6247695
03                 A    =         6720029
56  meter
 Y    =        1036970
12  meter          E    =           
0016157
 Z    =       -2233626
31                 I    =           51
50650
 XDOT =       1056
371923                 Wp   =          139
65726
 YDOT =      -5331
438842  meter/sec      RA   =          334
28762  deg
 ZDOT =      -5463
970306                 TA   =           65
49086
                                          MA   =           65
32248
                                          Ha   =            187
944  n
mi
                                          Hp   =            175
607

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20497687
12                 X    =        -6247975
46
 Y    =        3402132
94  feet           Y    =          967103
49  meter
 Z    =       -7328170
30                 Z    =        -2263978
86
 XDOT =       3465
787148                 XDOT =        1142
453869
 YDOT =     -17491
597251  feet/sec       YDOT =       -5319
144195  meter/sec
 ZDOT =     -17926
411765                 ZDOT =       -5458
629632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13407861
77                 X    =        -4086716
27
 Y    =       15819994
28  feet           Y    =         4821934
26  meter
 Z    =       -7442364
50                 Z    =        -2268432
70
 XDOT =      -7433
470389                 XDOT =       -2265
721774
 YDOT =     -14672
465203  feet/sec       YDOT =       -4472
167394  meter/sec
 ZDOT =     -17906
917997                 ZDOT =       -5458
028606


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   07123
52725057  
00020000  00000-0  20000-3 0  9016
2 25544  51
6333 334
6330 0010248 142
3074 217
8810 15
77483920  3726


Satellite: ISS
Catalog Number: 25544
Epoch time:      07123
52725057   =   yrday
fracday
Element set:     901
Inclination:       51
6333  deg
RA of node:       334
6330  deg
Eccentricity:     
0010248     
Arg of perigee:   142
3074  deg
Mean anomaly:     217
8810  deg
Mean motion:   15
77483920  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             372
Checksum:              264


Coasting Arc #3 (Orbit 387)
---------------------------------------

Vector Time (GMT): 2007/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1841421
77                 A    =         6714586
30  meter
 Y    =        4944115
74  meter          E    =           
0016674
 Z    =        4136169
62                 I    =           51
46347
 XDOT =      -6741
354569                 Wp   =          109
62493
 YDOT =        596
773832  meter/sec      RA   =          329
06717  deg
 ZDOT =      -3708
055175                 TA   =           18
30556
                                          MA   =           18
24562
                                          Ha   =            187
772  n
mi
                                          Hp   =            175
717

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6041409
99                 X    =        -1916663
87
 Y    =       16220852
18  feet           Y    =         4923102
85  meter
 Z    =       13570110
32                 Z    =         4127041
52
 XDOT =     -22117
305018                 XDOT =       -6729
513341
 YDOT =       1957
919396  feet/sec       YDOT =         521
454784  meter/sec
 ZDOT =     -12165
535351                 ZDOT =       -3740
776487

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6099154
07                 X    =         1859022
16
 Y    =       16227488
81  feet           Y    =         4946138
59  meter
 Z    =       13536303
06                 Z    =         4125865
17
 XDOT =     -14100
034904                 XDOT =       -4297
690639
 YDOT =      15568
219467  feet/sec       YDOT =        4745
193294  meter/sec
 ZDOT =     -12288
706098                 ZDOT =       -3745
597619


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   07124
54081213  
00020000  00000-0  20000-3 0  9029
2 25544  51
6334 329
3988 0010066 146
2682 213
9126 15
77567405  3888


Satellite: ISS
Catalog Number: 25544
Epoch time:      07124
54081213   =   yrday
fracday
Element set:     902
Inclination:       51
6334  deg
RA of node:       329
3988  deg
Eccentricity:     
0010066     
Arg of perigee:   146
2682  deg
Mean anomaly:     213
9126  deg
Mean motion:   15
77567405  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             388
Checksum:              289


Coasting Arc #4 (Orbit 403)
---------------------------------------

Vector Time (GMT): 2007/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5339467
89                 A    =         6714747
15  meter
 Y    =         120227
19  meter          E    =           
0018980
 Z    =        4064438
90                 I    =           51
43888
 XDOT =      -3048
232483                 Wp   =          126
03341
 YDOT =       5971
078801  meter/sec      RA   =          323
94119  deg
 ZDOT =       3804
493403                 TA   =          284
72391
                                          MA   =          284
93418
                                          Ha   =            187
618  n
mi
                                          Hp   =            175
830

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17517939
28                 X    =         5317982
03
 Y    =         394446
15  feet           Y    =          179815
53  meter
 Z    =       13334773
29                 Z    =         4090326
27
 XDOT =     -10000
762740                 XDOT =       -3133
257232
 YDOT =      19590
153545  feet/sec       YDOT =        5936
515944  meter/sec
 ZDOT =      12481
933738                 ZDOT =        3789
478980

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13177694
15                 X    =         4016561
18
 Y    =      -11435552
54  feet           Y    =        -3485556
42  meter
 Z    =       13432292
36                 Z    =         4094162
71
 XDOT =       4882
337307                 XDOT =        1488
136411
 YDOT =      20311
244246  feet/sec       YDOT =        6190
867246  meter/sec
 ZDOT =      12426
070803                 ZDOT =        3787
466381


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   07125
55435441  
00020000  00000-0  20000-3 0  9038
2 25544  51
6321 324
1646 0010057 150
0455 210
1287 15
77560245  4040


Satellite: ISS
Catalog Number: 25544
Epoch time:      07125
55435441   =   yrday
fracday
Element set:     903
Inclination:       51
6321  deg
RA of node:       324
1646  deg
Eccentricity:     
0010057     
Arg of perigee:   150
0455  deg
Mean anomaly:     210
1287  deg
Mean motion:   15
77560245  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             404
Checksum:              250


Coasting Arc #5 (Orbit 418)
---------------------------------------

Vector Time (GMT): 2007/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3333045
60                 A    =         6719653
04  meter
 Y    =       -5368549
77  meter          E    =           
0009869
 Z    =       -2301426
69                 I    =           51
43261
 XDOT =       5375
104072                 Wp   =          119
42527
 YDOT =       1022
666657  meter/sec      RA   =          318
71590  deg
 ZDOT =       5411
543559                 TA   =          214
61856
                                          MA   =          214
68284
                                          Ha   =            187
577  n
mi
                                          Hp   =            175
944

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10935188
98                 X    =         3404009
83
 Y    =      -17613352
26  feet           Y    =        -5330880
73  meter
 Z    =       -7550612
49                 Z    =        -2285062
82
 XDOT =      17634
855880                 XDOT =        5336
980372
 YDOT =       3355
205568  feet/sec       YDOT =        1082
560287  meter/sec
 ZDOT =      17754
408003                 ZDOT =        5437
563637

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4066538
30                 X    =        -1239480
87
 Y    =      -20351646
92  feet           Y    =        -6203181
98  meter
 Z    =       -7489594
03                 Z    =        -2282828
26
 XDOT =      13590
155466                 XDOT =        4142
279386
 YDOT =      -9270
038310  feet/sec       YDOT =       -2825
507677  meter/sec
 ZDOT =      17852
536367                 ZDOT =        5441
453085


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   07126
50452843  
00020000  00000-0  20000-3 0  9040
2 25544  51
6315 319
2570 0010177 153
9191 206
2489 15
77605702  4190


Satellite: ISS
Catalog Number: 25544
Epoch time:      07126
50452843   =   yrday
fracday
Element set:     904
Inclination:       51
6315  deg
RA of node:       319
2570  deg
Eccentricity:     
0010177     
Arg of perigee:   153
9191  deg
Mean anomaly:     206
2489  deg
Mean motion:   15
77605702  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             419
Checksum:              282


Coasting Arc #6 (Orbit 434)
---------------------------------------

Vector Time (GMT): 2007/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3966007
92                 A    =         6710293
10  meter
 Y    =       -1774285
65  meter          E    =           
0019269
 Z    =       -5127928
87                 I    =           51
38010
 XDOT =       4424
368425                 Wp   =          110
93491
 YDOT =      -6159
730467  meter/sec      RA   =          313
56698  deg
 ZDOT =      -1301
279499                 TA   =          146
62551
                                          MA   =          146
50390
                                          Ha   =            187
417  n
mi
                                          Hp   =            175
888

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13011837
02                 X    =        -3920962
11
 Y    =       -5821147
15  feet           Y    =        -1818383
32  meter
 Z    =      -16823913
60                 Z    =        -5147086
66
 XDOT =      14515
644438                 XDOT =        4499
240021
 YDOT =     -20209
089458  feet/sec       YDOT =       -6109
835924  meter/sec
 ZDOT =      -4269
289695                 ZDOT =       -1279
604602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13317621
54                 X    =        -4059211
04
 Y    =        4836757
35  feet           Y    =         1474243
64  meter
 Z    =      -16896285
40                 Z    =        -5149987
79
 XDOT =      -3320
618621                 XDOT =       -1012
124556
 YDOT =     -23652
073533  feet/sec       YDOT =       -7209
152013  meter/sec
 ZDOT =      -4188
355112                 ZDOT =       -1276
610638


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   07127
51802660  
00020000  00000-0  20000-3 0  9059
2 25544  51
6309 314
0228 0010179 157
3189 202
8427 15
77637021  4354


Satellite: ISS
Catalog Number: 25544
Epoch time:      07127
51802660   =   yrday
fracday
Element set:     905
Inclination:       51
6309  deg
RA of node:       314
0228  deg
Eccentricity:     
0010179     
Arg of perigee:   157
3189  deg
Mean anomaly:     202
8427  deg
Mean motion:   15
77637021  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             435
Checksum:              275


Coasting Arc #7 (Orbit 450)
---------------------------------------

Vector Time (GMT): 2007/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4222077
73                 A    =         6721639
18  meter
 Y    =        5214003
70  meter          E    =           
0021415
 Z    =         -91476
47                 I    =           51
40073
 XDOT =      -3694
718074                 Wp   =          146
93446
 YDOT =      -3085
699516  meter/sec      RA   =          308
37545  deg
 ZDOT =      -6028
231258                 TA   =           34
06509
                                          MA   =           33
92782
                                          Ha   =            187
101  n
mi
                                          Hp   =            176
156

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13851961
06                 X    =        -4279623
31
 Y    =       17106311
35  feet           Y    =         5166468
32  meter
 Z    =        -300119
65                 Z    =         -112126
64
 XDOT =     -12121
778459                 XDOT =       -3630
654570
 YDOT =     -10123
686076  feet/sec       YDOT =       -3126
657099  meter/sec
 ZDOT =     -19777
661609                 ZDOT =       -6046
024978

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2380165
27                 X    =          725474
37
 Y    =       21881161
76  feet           Y    =         6669378
11  meter
 Z    =        -377303
93                 Z    =         -115002
24
 XDOT =     -14051
232291                 XDOT =       -4282
815602
 YDOT =       1216
744383  feet/sec       YDOT =         370
863688  meter/sec
 ZDOT =     -19845
052975                 ZDOT =       -6048
772147


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   07128
53150095  
00020000  00000-0  20000-3 0  9061
2 25544  51
6314 308
7888 0009887 161
2780 198
8750 15
77711924  4513


Satellite: ISS
Catalog Number: 25544
Epoch time:      07128
53150095   =   yrday
fracday
Element set:     906
Inclination:       51
6314  deg
RA of node:       308
7888  deg
Eccentricity:     
0009887     
Arg of perigee:   161
2780  deg
Mean anomaly:     198
8750  deg
Mean motion:   15
77711924  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             451
Checksum:              316


Coasting Arc #8 (Orbit 466)
---------------------------------------

Vector Time (GMT): 2007/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2486795
48                 A    =         6710404
44  meter
 Y    =        3611109
74  meter          E    =           
0009553
 Z    =        5072760
90                 I    =           51
34479
 XDOT =      -5090
193618                 Wp   =          137
08760
 YDOT =       5599
010647  meter/sec      RA   =          303
17821  deg
 ZDOT =      -1495
649043                 TA   =          327
25987
                                          MA   =          327
31903
                                          Ha   =            187
109  n
mi
                                          Hp   =            176
323

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8158777
83                 X    =         2421588
11
 Y    =       11847472
91  feet           Y    =         3638553
45  meter
 Z    =       16642916
32                 Z    =         5084683
70
 XDOT =     -16700
110294                 XDOT =       -5145
158647
 YDOT =      18369
457503  feet/sec       YDOT =        5541
782055  meter/sec
 ZDOT =      -4906
985050                 ZDOT =       -1520
510277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14133173
79                 X    =         4307791
37
 Y    =        2381253
50  feet           Y    =          725806
07  meter
 Z    =       16688258
28                 Z    =         5086581
12
 XDOT =       1887
484727                 XDOT =         575
305345
 YDOT =      23717
565139  feet/sec       YDOT =        7229
113854  meter/sec
 ZDOT =      -4999
986480                 ZDOT =       -1523
995879


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   07129
54495597  
00020000  00000-0  20000-3 0  9073
2 25544  51
6306 303
5544 0010139 165
1964 194
9499 15
77674350  4670


Satellite: ISS
Catalog Number: 25544
Epoch time:      07129
54495597   =   yrday
fracday
Element set:     907
Inclination:       51
6306  deg
RA of node:       303
5544  deg
Eccentricity:     
0010139     
Arg of perigee:   165
1964  deg
Mean anomaly:     194
9499  deg
Mean motion:   15
77674350  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             467
Checksum:              325


Coasting Arc #9 (Orbit 482)
---------------------------------------

Vector Time (GMT): 2007/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4523262
31                 A    =         6718849
23  meter
 Y    =       -4316187
11  meter          E    =           
0016667
 Z    =        2457486
09                 I    =           51
35931
 XDOT =       2047
749508                 Wp   =          112
55985
 YDOT =       5190
152740  meter/sec      RA   =          298
02734  deg
 ZDOT =       5311
647193                 TA   =          275
36744
                                          MA   =          275
55757
                                          Ha   =            186
965  n
mi
                                          Hp   =            176
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14840099
44                 X    =         4559252
31
 Y    =      -14160718
86  feet           Y    =        -4265404
39  meter
 Z    =        8062618
42                 Z    =         2479547
28
 XDOT =       6718
338280                 XDOT =        1963
757193
 YDOT =      17028
060172  feet/sec       YDOT =        5212
581841  meter/sec
 ZDOT =      17426
664018                 ZDOT =        5321
391515

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -328825
71                 X    =         -100226
08
 Y    =      -20477001
64  feet           Y    =        -6241390
10  meter
 Z    =        8145219
64                 Z    =         2482662
95
 XDOT =      15496
292371                 XDOT =        4723
269915
 YDOT =       6743
013270  feet/sec       YDOT =        2055
270445  meter/sec
 ZDOT =      17463
992035                 ZDOT =        5323
024772


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   07130
55838560  
00020000  00000-0  20000-3 0  9088
2 25544  51
6305 298
3195 0010139 169
2664 190
8719 15
77748939  4837


Satellite: ISS
Catalog Number: 25544
Epoch time:      07130
55838560   =   yrday
fracday
Element set:     908
Inclination:       51
6305  deg
RA of node:       298
3195  deg
Eccentricity:     
0010139     
Arg of perigee:   169
2664  deg
Mean anomaly:     190
8719  deg
Mean motion:   15
77748939  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             483
Checksum:              327


Coasting Arc #10 (Orbit 497)
---------------------------------------

Vector Time (GMT): 2007/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1140818
94                 A    =         6714780
27  meter
 Y    =       -5352988
11  meter          E    =           
0014321
 Z    =       -3906048
31                 I    =           51
33407
 XDOT =       5178
344502                 Wp   =          146
79974
 YDOT =      -4035
083621  meter/sec      RA   =          292
79335  deg
 ZDOT =       4012
535990                 TA   =          165
12826
                                          MA   =          165
08610
                                          Ha   =            186
841  n
mi
                                          Hp   =            176
461

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3742844
30                 X    =        -1061901
29
 Y    =      -17562296
95  feet           Y    =        -5365303
94  meter
 Z    =      -12815119
12                 Z    =        -3911399
01
 XDOT =      16989
319231                 XDOT =        5203
588255
 YDOT =     -13238
463324  feet/sec       YDOT =       -3977
035524  meter/sec
 ZDOT =      13164
488157                 ZDOT =        4037
753632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15532984
56                 X    =        -4734453
69
 Y    =       -8979753
93  feet           Y    =        -2737029
00  meter
 Z    =      -12835920
13                 Z    =        -3912388
46
 XDOT =        765
866915                 XDOT =         233
436236
 YDOT =     -20300
419934  feet/sec       YDOT =       -6187
567996  meter/sec
 ZDOT =      13259
011531                 ZDOT =        4041
346715


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   07131
50845666  
00020000  00000-0  20000-3 0  9090
2 25544  51
6311 293
4119 0010138 172
2926 187
8397 15
77777064  4985


Satellite: ISS
Catalog Number: 25544
Epoch time:      07131
50845666   =   yrday
fracday
Element set:     909
Inclination:       51
6311  deg
RA of node:       293
4119  deg
Eccentricity:     
0010138     
Arg of perigee:   172
2926  deg
Mean anomaly:     187
8397  deg
Mean motion:   15
77777064  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             498
Checksum:              317


Coasting Arc #11 (Orbit 513)
---------------------------------------

Vector Time (GMT): 2007/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4454657
78                 A    =         6712975
99  meter
 Y    =        2524118
57  meter          E    =           
0011454
 Z    =       -4345650
76                 I    =           51
31875
 XDOT =       -634
692520                 Wp   =          125
65069
 YDOT =      -6897
801657  meter/sec      RA   =          287
65695  deg
 ZDOT =      -3368
680833                 TA   =          110
33859
                                          MA   =          110
21548
                                          Ha   =            186
531  n
mi
                                          Hp   =            176
580

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14615018
97                 X    =        -4461441
17
 Y    =        8281228
91  feet           Y    =         2474266
33  meter
 Z    =      -14257384
37                 Z    =        -4367308
07
 XDOT =      -2082
324540                 XDOT =        -541
148529
 YDOT =     -22630
582864  feet/sec       YDOT =       -6904
375983  meter/sec
 ZDOT =     -11052
102471                 ZDOT =       -3371
537247

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3244235
75                 X    =         -988843
06
 Y    =       16411212
90  feet           Y    =         5002137
69  meter
 Z    =      -14338673
80                 Z    =        -4370427
77
 XDOT =     -17242
208174                 XDOT =       -5255
425052
 YDOT =     -13038
541904  feet/sec       YDOT =       -3974
147572  meter/sec
 ZDOT =     -11063
697351                 ZDOT =       -3372
214952


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   07132
52184304  
00020000  00000-0  20000-3 0  9100
2 25544  51
6313 288
1777 0009978 176
0213 184
1033 15
77822409  5149


Satellite: ISS
Catalog Number: 25544
Epoch time:      07132
52184304   =   yrday
fracday
Element set:     910
Inclination:       51
6313  deg
RA of node:       288
1777  deg
Eccentricity:     
0009978     
Arg of perigee:   176
0213  deg
Mean anomaly:     184
1033  deg
Mean motion:   15
77822409  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             514
Checksum:              281


Coasting Arc #12 (Orbit 529)
---------------------------------------

Vector Time (GMT): 2007/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          45484
96                 A    =         6719874
13  meter
 Y    =        6462540
31  meter          E    =           
0020344
 Z    =        1793497
26                 I    =           51
33385
 XDOT =      -4992
157530                 Wp   =          140
95310
 YDOT =       1611
030798  meter/sec      RA   =          282
42695  deg
 ZDOT =      -5659
354632                 TA   =           19
01880
                                          MA   =           18
94294
                                          Ha   =            186
403  n
mi
                                          Hp   =            176
878

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         149228
87                 X    =          -35496
10
 Y    =       21202560
06  feet           Y    =         6462596
08  meter
 Z    =        5884177
35                 Z    =         1793521
79
 XDOT =     -16378
469586                 XDOT =       -4982
308740
 YDOT =       5285
534113  feet/sec       YDOT =        1555
260995  meter/sec
 ZDOT =     -18567
436457                 ZDOT =       -5683
582914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16347885
42                 X    =         4982835
48
 Y    =       13502116
85  feet           Y    =         4115445
22  meter
 Z    =        5885052
94                 Z    =         1793764
14
 XDOT =      -5391
081335                 XDOT =       -1643
201591
 YDOT =      14687
163215  feet/sec       YDOT =        4476
647348  meter/sec
 ZDOT =     -18658
521883                 ZDOT =       -5687
117470


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   07133
53520673  
00020000  00000-0  20000-3 0  9116
2 25544  51
6305 282
9419 0009983 180
7132 179
4021 15
77840066  5304


Satellite: ISS
Catalog Number: 25544
Epoch time:      07133
53520673   =   yrday
fracday
Element set:     911
Inclination:       51
6305  deg
RA of node:       282
9419  deg
Eccentricity:     
0009983     
Arg of perigee:   180
7132  deg
Mean anomaly:     179
4021  deg
Mean motion:   15
77840066  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             530
Checksum:              282

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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