Date: June 24th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4305 56 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


There are no maneuvers



Coasting Arc #1 (Orbit 1161)
---------------------------------------

Vector Time (GMT): 2007/173/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1656716
37                 A    =         6714048
44  meter
 Y    =       -5332541
93  meter          E    =           
0009893
 Z    =       -3738989
43                 I    =           51
94539
 XDOT =       4600
702831                 Wp   =           22
26301
 YDOT =       4439
459274  meter/sec      RA   =           75
64646  deg
 ZDOT =      -4287
730684                 TA   =          202
69483
                                          MA   =          202
73860
                                          Ha   =            184
772  n
mi
                                          Hp   =            177
383

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5435421
16                 X    =         1734385
79
 Y    =      -17495216
29  feet           Y    =        -5313580
83  meter
 Z    =      -12267025
70                 Z    =        -3730753
17
 XDOT =      15094
169393                 XDOT =        4571
547173
 YDOT =      14565
155099  feet/sec       YDOT =        4490
744461  meter/sec
 ZDOT =     -14067
357886                 ZDOT =       -4265
450765

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18227069
84                 X    =        -5555610
89
 Y    =       -2036832
81  feet           Y    =         -620826
64  meter
 Z    =      -12236484
50                 Z    =        -3729680
47
 XDOT =      11227
044764                 XDOT =        3422
003244
 YDOT =     -16361
273241  feet/sec       YDOT =       -4986
916084  meter/sec
 ZDOT =     -13982
628796                 ZDOT =       -4261
905257


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   07173
55569111  
00020000  00000-0  20000-3 0  9000
2 25544  51
6348  76
1711 0008078 345
4358  14
6574 15
78247670 11621


Satellite: ISS
Catalog Number: 25544
Epoch time:      07173
55569111   =   yrday
fracday
Element set:     900
Inclination:       51
6348  deg
RA of node:        76
1711  deg
Eccentricity:     
0008078     
Arg of perigee:   345
4358  deg
Mean anomaly:      14
6574  deg
Mean motion:   15
78247670  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1162
Checksum:              293


Coasting Arc #2 (Orbit 1177)
---------------------------------------

Vector Time (GMT): 2007/174/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3870684
86                 A    =         6717203
07  meter
 Y    =       -4837885
06  meter          E    =           
0012961
 Z    =        2591800
70                 I    =           51
94746
 XDOT =       2631
823100                 Wp   =           68
47007
 YDOT =      -4950
524285  meter/sec      RA   =           70
45123  deg
 ZDOT =      -5284
619528                 TA   =           82
18388
                                          MA   =           82
03677
                                          Ha   =            184
911  n
mi
                                          Hp   =            177
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12699097
31                 X    =        -3828889
76
 Y    =      -15872326
32  feet           Y    =        -4880935
90  meter
 Z    =        8503283
15                 Z    =         2573097
75
 XDOT =       8634
590224                 XDOT =        2712
656736
 YDOT =     -16241
877574  feet/sec       YDOT =       -4920
641075  meter/sec
 ZDOT =     -17337
990576                 ZDOT =       -5271
638447

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12855279
58                 X    =        -3918289
22
 Y    =       15784365
30  feet           Y    =         4811074
54  meter
 Z    =        8432036
43                 Z    =         2570084
70
 XDOT =     -16557
813771                 XDOT =       -5046
821637
 YDOT =      -4203
837701  feet/sec       YDOT =       -1281
329731  meter/sec
 ZDOT =     -17289
462665                 ZDOT =       -5269
828220


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   07174
56878114  
00020000  00000-0  20000-3 0  9019
2 25544  51
6347  70
9345 0008028 350
2782   9
8227 15
78259265 11786


Satellite: ISS
Catalog Number: 25544
Epoch time:      07174
56878114   =   yrday
fracday
Element set:     901
Inclination:       51
6347  deg
RA of node:        70
9345  deg
Eccentricity:     
0008028     
Arg of perigee:   350
2782  deg
Mean anomaly:       9
8227  deg
Mean motion:   15
78259265  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1178
Checksum:              307


Coasting Arc #3 (Orbit 1193)
---------------------------------------

Vector Time (GMT): 2007/175/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2985150
32                 A    =         6708544
79  meter
 Y    =        3127838
97  meter          E    =           
0006060
 Z    =        5125900
38                 I    =           51
90830
 XDOT =      -4156
261185                 Wp   =           26
42080
 YDOT =      -6331
856266  meter/sec      RA   =           65
33712  deg
 ZDOT =       1447
919414                 TA   =           49
80305
                                          MA   =           49
75002
                                          Ha   =            185
067  n
mi
                                          Hp   =            176
854

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9793800
26                 X    =        -3044805
21
 Y    =       10261938
87  feet           Y    =         3094123
03  meter
 Z    =       16817258
48                 Z    =         5111254
03
 XDOT =     -13636
027509                 XDOT =       -4092
182297
 YDOT =     -20773
806647  feet/sec       YDOT =       -6377
975845  meter/sec
 ZDOT =       4750
391778                 ZDOT =        1427
882910

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12230611
13                 X    =         3727890
27
 Y    =        7313410
18  feet           Y    =         2229127
42  meter
 Z    =       16762227
73                 Z    =         5109127
01
 XDOT =     -16616
327225                 XDOT =       -5064
656538
 YDOT =      17110
989702  feet/sec       YDOT =        5215
429661  meter/sec
 ZDOT =       4673
943945                 ZDOT =        1424
618114


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   07175
58185454  
00020000  00000-0  20000-3 0  9021
2 25544  51
6352  65
6977 0008116 353
3882   6
7175 15
78296589 11943


Satellite: ISS
Catalog Number: 25544
Epoch time:      07175
58185454   =   yrday
fracday
Element set:     902
Inclination:       51
6352  deg
RA of node:        65
6977  deg
Eccentricity:     
0008116     
Arg of perigee:   353
3882  deg
Mean anomaly:       6
7175  deg
Mean motion:   15
78296589  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1194
Checksum:              326


Coasting Arc #4 (Orbit 1209)
---------------------------------------

Vector Time (GMT): 2007/176/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3222756
77                 A    =         6719867
75  meter
 Y    =        5881263
85  meter          E    =           
0018891
 Z    =         164506
98                 I    =           51
93354
 XDOT =      -4247
377655                 Wp   =           27
11492
 YDOT =       2150
527051  meter/sec      RA   =           60
17781  deg
 ZDOT =       6070
810702                 TA   =          334
67001
                                          MA   =          334
76251
                                          Ha   =            185
034  n
mi
                                          Hp   =            176
645

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10573348
97                 X    =         3155952
94
 Y    =       19295485
07  feet           Y    =         5916928
98  meter
 Z    =         539721
06                 Z    =          180001
95
 XDOT =     -13934
966061                 XDOT =       -4300
600566
 YDOT =       7055
534945  feet/sec       YDOT =        2102
731891  meter/sec
 ZDOT =      19917
357946                 ZDOT =        6050
047892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16153660
27                 X    =         4923635
65
 Y    =      -14936642
16  feet           Y    =        -4552688
53  meter
 Z    =         598942
47                 Z    =          182557
66
 XDOT =       9163
968411                 XDOT =        2793
177572
 YDOT =      10736
253607  feet/sec       YDOT =        3272
410099  meter/sec
 ZDOT =      19839
090282                 ZDOT =        6046
954718


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   07176
59491318  
00020000  00000-0  20000-3 0  9033
2 25544  51
6352  60
4608 0008177 356
1998   3
9104 15
78336174 12108


Satellite: ISS
Catalog Number: 25544
Epoch time:      07176
59491318   =   yrday
fracday
Element set:     903
Inclination:       51
6352  deg
RA of node:        60
4608  deg
Eccentricity:     
0008177     
Arg of perigee:   356
1998  deg
Mean anomaly:       3
9104  deg
Mean motion:   15
78336174  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1210
Checksum:              293


Coasting Arc #5 (Orbit 1224)
---------------------------------------

Vector Time (GMT): 2007/177/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4400137
23                 A    =         6708845
12  meter
 Y    =        -606443
07  meter          E    =           
0013767
 Z    =       -5037411
97                 I    =           51
88052
 XDOT =       3030
222197                 Wp   =           68
26957
 YDOT =       6837
154916  meter/sec      RA   =           55
01072  deg
 ZDOT =       1832
723018                 TA   =          219
29099
                                          MA   =          219
39098
                                          Ha   =            185
144  n
mi
                                          Hp   =            176
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14436145
78                 X    =         4431062
53
 Y    =       -1989642
61  feet           Y    =         -557064
41  meter
 Z    =      -16526942
15                 Z    =        -5015960
96
 XDOT =       9941
673874                 XDOT =        2944
639823
 YDOT =      22431
610616  feet/sec       YDOT =        6870
561703  meter/sec
 ZDOT =       6012
870794                 ZDOT =        1847
237332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5689054
42                 X    =        -1734023
79
 Y    =      -13515464
66  feet           Y    =        -4119513
63  meter
 Z    =      -16445901
44                 Z    =        -5012710
76
 XDOT =      18109
350247                 XDOT =        5519
729955
 YDOT =     -14971
065606  feet/sec       YDOT =       -4563
180797  meter/sec
 ZDOT =       6068
480474                 ZDOT =        1849
672849


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   07177
54464368  
00020000  00000-0  20000-3 0  9045
2 25544  51
6347  55
5512 0008226 359
2830    
8322 15
78353378 12254


Satellite: ISS
Catalog Number: 25544
Epoch time:      07177
54464368   =   yrday
fracday
Element set:     904
Inclination:       51
6347  deg
RA of node:        55
5512  deg
Eccentricity:     
0008226     
Arg of perigee:   359
2830  deg
Mean anomaly:        
8322  deg
Mean motion:   15
78353378  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1225
Checksum:              291


Coasting Arc #6 (Orbit 1240)
---------------------------------------

Vector Time (GMT): 2007/178/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1852116
98                 A    =         6716075
69  meter
 Y    =       -5761259
09  meter          E    =           
0007840
 Z    =       -2924715
91                 I    =           51
88697
 XDOT =       5770
145745                 Wp   =           34
94068
 YDOT =        706
540404  meter/sec      RA   =           49
89893  deg
 ZDOT =      -5046
135787                 TA   =          178
63600
                                          MA   =          178
63386
                                          Ha   =            185
174  n
mi
                                          Hp   =            176
343

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6076499
29                 X    =        -1773348
28
 Y    =      -18901768
66  feet           Y    =        -5781529
48  meter
 Z    =       -9595524
64                 Z    =        -2933523
40
 XDOT =      18930
924361                 XDOT =        5786
329585
 YDOT =       2318
045945  feet/sec       YDOT =         771
156940  meter/sec
 ZDOT =     -16555
563606                 ZDOT =       -5018
064822

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16506481
99                 X    =        -5031175
71
 Y    =       11003854
39  feet           Y    =         3353974
82  meter
 Z    =       -9629435
91                 Z    =        -2935052
07
 XDOT =      -2217
905746                 XDOT =        -676
017671
 YDOT =     -17720
823833  feet/sec       YDOT =       -5401
307104  meter/sec
 ZDOT =     -16449
348332                 ZDOT =       -5013
761372


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   07178
55767534  
00020000  00000-0  20000-3 0  9059
2 25544  51
6343  50
3149 0008179   2
3739 357
7464 15
78346222 12419


Satellite: ISS
Catalog Number: 25544
Epoch time:      07178
55767534   =   yrday
fracday
Element set:     905
Inclination:       51
6343  deg
RA of node:        50
3149  deg
Eccentricity:     
0008179     
Arg of perigee:     2
3739  deg
Mean anomaly:     357
7464  deg
Mean motion:   15
78346222  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1241
Checksum:              300


Coasting Arc #7 (Orbit 1256)
---------------------------------------

Vector Time (GMT): 2007/179/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5524938
25                 A    =         6714590
12  meter
 Y    =       -1692424
58  meter          E    =           
0015801
 Z    =        3417084
08                 I    =           51
86323
 XDOT =      -1003
361908                 Wp   =           57
65812
 YDOT =      -6089
864936  meter/sec      RA   =           44
69599  deg
 ZDOT =      -4614
816476                 TA   =           82
01398
                                          MA   =           81
83470
                                          Ha   =            185
252  n
mi
                                          Hp   =            176
071

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18126437
82                 X    =        -5522202
28
 Y    =       -5552574
09  feet           Y    =        -1754193
00  meter
 Z    =       11210905
79                 Z    =         3390250
16
 XDOT =      -3291
869776                 XDOT =        -912
771599
 YDOT =     -19979
871838  feet/sec       YDOT =       -6100
577556  meter/sec
 ZDOT =     -15140
474001                 ZDOT =       -4619
472119

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =           8273
80                 X    =            2521
86
 Y    =       19017558
15  feet           Y    =         5796551
72  meter
 Z    =       11109259
61                 Z    =         3386102
33
 XDOT =     -16782
210221                 XDOT =       -5115
217675
 YDOT =       8908
195343  feet/sec       YDOT =        2715
217941  meter/sec
 ZDOT =     -15158
715559                 ZDOT =       -4620
376502


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   07179
57069094  
00020000  00000-0  20000-3 0  9069
2 25544  51
6346  45
0775 0008391   5
8080 354
3182 15
78431693 12575


Satellite: ISS
Catalog Number: 25544
Epoch time:      07179
57069094   =   yrday
fracday
Element set:     906
Inclination:       51
6346  deg
RA of node:        45
0775  deg
Eccentricity:     
0008391     
Arg of perigee:     5
8080  deg
Mean anomaly:     354
3182  deg
Mean motion:   15
78431693  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1257
Checksum:              306


Coasting Arc #8 (Orbit 1272)
---------------------------------------

Vector Time (GMT): 2007/180/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -269212
11                 A    =         6709677
53  meter
 Y    =        4673259
27  meter          E    =           
0008886
 Z    =        4798807
11                 I    =           51
82357
 XDOT =      -6669
516945                 Wp   =           58
67635
 YDOT =      -2957
206275  meter/sec      RA   =           39
58588  deg
 ZDOT =       2506
832023                 TA   =            6
91300
                                          MA   =            6
90076
                                          Ha   =            185
448  n
mi
                                          Hp   =            175
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -883241
84                 X    =         -344760
84
 Y    =       15332215
46  feet           Y    =         4669825
28  meter
 Z    =       15744117
80                 Z    =         4797316
84
 XDOT =     -21881
617273                 XDOT =       -6648
131036
 YDOT =      -9702
120325  feet/sec       YDOT =       -3031
669556  meter/sec
 ZDOT =       8224
514511                 ZDOT =        2474
482867

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14882820
44                 X    =         4536283
67
 Y    =       -3810611
14  feet           Y    =        -1161474
28  meter
 Z    =       15738967
27                 Z    =         4797237
22
 XDOT =      -2734
816402                 XDOT =        -833
572039
 YDOT =      22766
394422  feet/sec       YDOT =        6939
197020  meter/sec
 ZDOT =       8101
874884                 ZDOT =        2469
451465


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   07180
58369597  
00020000  00000-0  20000-3 0  9074
2 25544  51
6334  39
8397 0008335  10
5614 349
5725 15
78371589 12731


Satellite: ISS
Catalog Number: 25544
Epoch time:      07180
58369597   =   yrday
fracday
Element set:     907
Inclination:       51
6334  deg
RA of node:        39
8397  deg
Eccentricity:     
0008335     
Arg of perigee:    10
5614  deg
Mean anomaly:     349
5725  deg
Mean motion:   15
78371589  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1273
Checksum:              327


Coasting Arc #9 (Orbit 1287)
---------------------------------------

Vector Time (GMT): 2007/181/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5819852
84                 A    =         6719413
62  meter
 Y    =        3247440
85  meter          E    =           
0018360
 Z    =        -774497
29                 I    =           51
83256
 XDOT =      -1736
713791                 Wp   =           27
56800
 YDOT =       4526
124648  meter/sec      RA   =           34
40207  deg
 ZDOT =       5999
613920                 TA   =          323
98909
                                          MA   =          324
11265
                                          Ha   =            185
432  n
mi
                                          Hp   =            175
739

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19094005
39                 X    =         5786869
28
 Y    =       10654333
50  feet           Y    =         3312337
47  meter
 Z    =       -2541001
62                 Z    =         -746304
04
 XDOT =      -5697
879893                 XDOT =       -1816
341303
 YDOT =      14849
490316  feet/sec       YDOT =        4506
257151  meter/sec
 ZDOT =      19683
772702                 ZDOT =        5990
984650

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3863378
43                 X    =         1177557
74
 Y    =      -21533747
96  feet           Y    =        -6563486
38  meter
 Z    =       -2434041
77                 Z    =         -741895
93
 XDOT =      14360
728368                 XDOT =        4377
150007
 YDOT =        383
051030  feet/sec       YDOT =         116
753954  meter/sec
 ZDOT =      19651
605803                 ZDOT =        5989
809449


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   07181
53337131  
00020000  00000-0  20000-3 0  9080
2 25544  51
6324  34
9293 0008280  13
0058 347
1319 15
78411000 12882


Satellite: ISS
Catalog Number: 25544
Epoch time:      07181
53337131   =   yrday
fracday
Element set:     908
Inclination:       51
6324  deg
RA of node:        34
9293  deg
Eccentricity:     
0008280     
Arg of perigee:    13
0058  deg
Mean anomaly:     347
1319  deg
Mean motion:   15
78411000  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1288
Checksum:              264


Coasting Arc #10 (Orbit 1303)
---------------------------------------

Vector Time (GMT): 2007/182/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2807146
78                 A    =         6707678
63  meter
 Y    =       -3149351
01  meter          E    =           
0018146
 Z    =       -5228653
11                 I    =           51
76771
 XDOT =       6335
311027                 Wp   =           69
87895
 YDOT =       4291
615052  meter/sec      RA   =           29
24309  deg
 ZDOT =        824
751937                 TA   =          207
91318
                                          MA   =          208
01065
                                          Ha   =            185
423  n
mi
                                          Hp   =            175
578

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9209799
15                 X    =         2867554
18
 Y    =      -10332516
44  feet           Y    =        -3117621
03  meter
 Z    =      -17154373
71                 Z    =        -5214870
11
 XDOT =      20785
141166                 XDOT =        6282
844262
 YDOT =      14080
101878  feet/sec       YDOT =        4362
166520  meter/sec
 ZDOT =       2705
879057                 ZDOT =         855
401985

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12888243
73                 X    =        -3928336
69
 Y    =       -5220066
25  feet           Y    =        -1591076
19  meter
 Z    =      -17102570
44                 Z    =        -5212863
47
 XDOT =       5764
563704                 XDOT =        1757
039017
 YDOT =     -23388
437419  feet/sec       YDOT =       -7128
795725  meter/sec
 ZDOT =       2822
245940                 ZDOT =         860
220563


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   07182
54634608  
00020000  00000-0  20000-3 0  9092
2 25544  51
6313  29
6908 0008210  17
5725 342
5723 15
78454963 13049


Satellite: ISS
Catalog Number: 25544
Epoch time:      07182
54634608   =   yrday
fracday
Element set:     909
Inclination:       51
6313  deg
RA of node:        29
6908  deg
Eccentricity:     
0008210     
Arg of perigee:    17
5725  deg
Mean anomaly:     342
5723  deg
Mean motion:   15
78454963  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1304
Checksum:              293


Coasting Arc #11 (Orbit 1319)
---------------------------------------

Vector Time (GMT): 2007/183/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4894890
16                 A    =         6717343
83  meter
 Y    =       -4062959
17  meter          E    =           
0007792
 Z    =       -2169822
55                 I    =           51
77495
 XDOT =       4658
787717                 Wp   =           65
32790
 YDOT =      -2673
971545  meter/sec      RA   =           24
10988  deg
 ZDOT =      -5514
975158                 TA   =          138
93595
                                          MA   =          138
87727
                                          Ha   =            185
472  n
mi
                                          Hp   =            175
294

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16059350
92                 X    =        -4838553
32
 Y    =      -13329918
53  feet           Y    =        -4117381
16  meter
 Z    =       -7118840
39                 Z    =        -2193465
51
 XDOT =      15284
736603                 XDOT =        4715
132528
 YDOT =      -8772
872522  feet/sec       YDOT =       -2621
558240  meter/sec
 ZDOT =     -18093
750518                 ZDOT =       -5492
206792

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6723218
26                 X    =        -2049236
93
 Y    =       19725631
06  feet           Y    =         6012372
35  meter
 Z    =       -7208688
11                 Z    =        -2197208
14
 XDOT =     -12254
417457                 XDOT =       -3735
146441
 YDOT =     -10743
244961  feet/sec       YDOT =       -3274
541064  meter/sec
 ZDOT =     -18007
910775                 ZDOT =       -5488
811204


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   07183
55930617  
00020000  00000-0  20000-3 0  9105
2 25544  51
6314  24
4535 0008294  21
0217 339
1288 15
78480467 13201


Satellite: ISS
Catalog Number: 25544
Epoch time:      07183
55930617   =   yrday
fracday
Element set:     910
Inclination:       51
6314  deg
RA of node:        24
4535  deg
Eccentricity:     
0008294     
Arg of perigee:    21
0217  deg
Mean anomaly:     339
1288  deg
Mean motion:   15
78480467  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1320
Checksum:              278


Coasting Arc #12 (Orbit 1335)
---------------------------------------

Vector Time (GMT): 2007/184/12:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5162109
48                 A    =         6712548
59  meter
 Y    =        1560986
83  meter          E    =           
0017066
 Z    =        3991875
16                 I    =           51
73170
 XDOT =      -4527
481923                 Wp   =           55
40180
 YDOT =      -4836
999299  meter/sec      RA   =           18
90110  deg
 ZDOT =      -3941
882642                 TA   =           75
32937
                                          MA   =           75
14024
                                          Ha   =            185
547  n
mi
                                          Hp   =            175
245

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16936054
73                 X    =        -5198572
48
 Y    =        5121347
88  feet           Y    =         1503056
67  meter
 Z    =       13096703
29                 Z    =         3966709
76
 XDOT =     -14853
943317                 XDOT =       -4453
908776
 YDOT =     -15869
420273  feet/sec       YDOT =       -4887
216103  meter/sec
 ZDOT =     -12932
685832                 ZDOT =       -3963
698894

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11102965
81                 X    =         3384183
98
 Y    =       13865867
14  feet           Y    =         4226316
30  meter
 Z    =       13001679
50                 Z    =         3962911
91
 XDOT =      -8189
864911                 XDOT =       -2496
270825
 YDOT =      18828
733191  feet/sec       YDOT =        5738
997877  meter/sec
 ZDOT =     -13015
710528                 ZDOT =       -3967
188569


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   07184
57225152  
00020000  00000-0  20000-3 0  9110
2 25544  51
6314  19
2147 0008153  24
2515 335
9033 15
78495917 13367


Satellite: ISS
Catalog Number: 25544
Epoch time:      07184
57225152   =   yrday
fracday
Element set:     911
Inclination:       51
6314  deg
RA of node:        19
2147  deg
Eccentricity:     
0008153     
Arg of perigee:    24
2515  deg
Mean anomaly:     335
9033  deg
Mean motion:   15
78495917  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1336
Checksum:              279

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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