Date: July 19th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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


205/16:18:03 319 -11 1 11 8 11 8
N/A 1 6 -0 0 191 9
000/00:22:06 638 -3 9 -0 1 186 9

Coasting Arc #1 (Orbit 3282)
---------------------------------------

Vector Time (GMT): 2008/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3883700
47                 A    =         6729263
43  meter
 Y    =       -5480264
35  meter          E    =           
0020912
 Z    =         -51721
38                 I    =           51
39117
 XDOT =       3903
410805                 Wp   =           29
48542
 YDOT =      -2813
213386  meter/sec      RA   =          235
02824  deg
 ZDOT =       6024
789706                 TA   =          329
94999
                                          MA   =          330
06982
                                          Ha   =            190
957  n
mi
                                          Hp   =            180
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12741799
43                 X    =        -3821879
38
 Y    =      -17979869
93  feet           Y    =        -5523348
45  meter
 Z    =        -169689
58                 Z    =          -70439
15
 XDOT =      12806
465897                 XDOT =        3905
311309
 YDOT =      -9229
702710  feet/sec       YDOT =       -2769
553690  meter/sec
 ZDOT =      19766
370427                 ZDOT =        6043
756481

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11906529
15                 X    =        -3629110
09
 Y    =       18542756
15  feet           Y    =         5651832
07  meter
 Z    =        -242338
53                 Z    =          -73864
78
 XDOT =     -11956
541023                 XDOT =       -3644
353704
 YDOT =      -7449
583442  feet/sec       YDOT =       -2270
633033  meter/sec
 ZDOT =      19839
222024                 ZDOT =        6046
994873


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   08196
50014429  
00020000  00000-0  20000-3 0  9008
2 25544  51
6394 235
9268 0009767   9
9943 350
1413 15
75025317 32837


Satellite: ISS
Catalog Number: 25544
Epoch time:      08196
50014429   =   yrday
fracday
Element set:     900
Inclination:       51
6394  deg
RA of node:       235
9268  deg
Eccentricity:     
0009767     
Arg of perigee:     9
9943  deg
Mean anomaly:     350
1413  deg
Mean motion:   15
75025317  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3283
Checksum:              297


Coasting Arc #2 (Orbit 3298)
---------------------------------------

Vector Time (GMT): 2008/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3475315
91                 A    =         6717111
95  meter
 Y    =        2381981
06  meter          E    =           
0019290
 Z    =       -5245850
64                 I    =           51
36893
 XDOT =      -4715
222583                 Wp   =           63
71756
 YDOT =      -6063
431569  meter/sec      RA   =          229
86341  deg
 ZDOT =        380
048590                 TA   =          209
85434
                                          MA   =          209
96451
                                          Ha   =            190
961  n
mi
                                          Hp   =            180
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11401955
08                 X    =        -3476210
14
 Y    =        7814898
50  feet           Y    =         2343114
08  meter
 Z    =      -17210796
06                 Z    =        -5262735
30
 XDOT =     -15469
890365                 XDOT =       -4648
916074
 YDOT =     -19893
148192  feet/sec       YDOT =       -6115
789225  meter/sec
 ZDOT =       1246
878577                 ZDOT =         357
302142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11604928
35                 X    =         3537182
16
 Y    =        7359732
86  feet           Y    =         2243246
57  meter
 Z    =      -17275667
55                 Z    =        -5265623
47
 XDOT =     -11743
544013                 XDOT =       -3579
432215
 YDOT =      21164
280467  feet/sec       YDOT =        6450
872686  meter/sec
 ZDOT =       1158
633974                 ZDOT =         353
151635


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   08197
51528476  
00020000  00000-0  20000-3 0  9013
2 25544  51
6399 230
7050 0009603  13
7426 346
3997 15
75064603 32994


Satellite: ISS
Catalog Number: 25544
Epoch time:      08197
51528476   =   yrday
fracday
Element set:     901
Inclination:       51
6399  deg
RA of node:       230
7050  deg
Eccentricity:     
0009603     
Arg of perigee:    13
7426  deg
Mean anomaly:     346
3997  deg
Mean motion:   15
75064603  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3299
Checksum:              309


Coasting Arc #3 (Orbit 3314)
---------------------------------------

Vector Time (GMT): 2008/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4326247
33                 A    =         6728813
01  meter
 Y    =        5103605
31  meter          E    =           
0009890
 Z    =        -731240
81                 I    =           51
42787
 XDOT =      -4097
828585                 Wp   =           84
37936
 YDOT =       2629
703362  meter/sec      RA   =          224
71221  deg
 ZDOT =      -5958
430116                 TA   =          103
60873
                                          MA   =          103
49856
                                          Ha   =            191
072  n
mi
                                          Hp   =            180
231

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14193724
85                 X    =         4272408
66
 Y    =       16744111
93  feet           Y    =         5151683
00  meter
 Z    =       -2399084
04                 Z    =         -710353
98
 XDOT =     -13444
319504                 XDOT =       -4097
985185
 YDOT =       8627
635703  feet/sec       YDOT =        2583
879338  meter/sec
 ZDOT =     -19548
655235                 ZDOT =       -5978
337003

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9537024
61                 X    =         2906885
10
 Y    =      -19780150
89  feet           Y    =        -6028989
99  meter
 Z    =       -2318082
38                 Z    =         -706551
51
 XDOT =      11853
663207                 XDOT =        3612
996545
 YDOT =       7988
079945  feet/sec       YDOT =        2434
766767  meter/sec
 ZDOT =     -19625
161712                 ZDOT =       -5981
749290


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   08198
53041407  
00020000  00000-0  20000-3 0  9021
2 25544  51
6391 225
4830 0009682  18
3100 341
8410 15
75104151 33152


Satellite: ISS
Catalog Number: 25544
Epoch time:      08198
53041407   =   yrday
fracday
Element set:     902
Inclination:       51
6391  deg
RA of node:       225
4830  deg
Eccentricity:     
0009682     
Arg of perigee:    18
3100  deg
Mean anomaly:     341
8410  deg
Mean motion:   15
75104151  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3315
Checksum:              255


Coasting Arc #4 (Orbit 3330)
---------------------------------------

Vector Time (GMT): 2008/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3704009
30                 A    =         6717396
35  meter
 Y    =       -2249424
38  meter          E    =           
0013397
 Z    =        5128615
40                 I    =           51
41028
 XDOT =       5164
355374                 Wp   =           32
06866
 YDOT =       5577
366554  meter/sec      RA   =          219
53465  deg
 ZDOT =      -1270
862949                 TA   =           70
18299
                                          MA   =           70
03861
                                          Ha   =            191
045  n
mi
                                          Hp   =            180
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12152261
49                 X    =         3703973
97
 Y    =       -7380001
24  feet           Y    =        -2208005
14  meter
 Z    =       16826166
00                 Z    =         5146608
69
 XDOT =      16943
423144                 XDOT =        5107
778070
 YDOT =      18298
446700  feet/sec       YDOT =        5634
801226  meter/sec
 ZDOT =      -4169
497865                 ZDOT =       -1245
911347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11774027
17                 X    =        -3588723
48
 Y    =       -7821869
56  feet           Y    =        -2384105
84  meter
 Z    =       16895336
07                 Z    =         5149698
43
 XDOT =       8871
202871                 XDOT =        2703
942635
 YDOT =     -22240
484365  feet/sec       YDOT =       -6778
899634  meter/sec
 ZDOT =      -4072
762907                 ZDOT =       -1241
378134


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   08199
54553241  
00020000  00000-0  20000-3 0  9038
2 25544  51
6379 220
2610 0009751  22
2645 337
8941 15
75128912 33315


Satellite: ISS
Catalog Number: 25544
Epoch time:      08199
54553241   =   yrday
fracday
Element set:     903
Inclination:       51
6379  deg
RA of node:       220
2610  deg
Eccentricity:     
0009751     
Arg of perigee:    22
2645  deg
Mean anomaly:     337
8941  deg
Mean motion:   15
75128912  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3331
Checksum:              285


Coasting Arc #5 (Orbit 3346)
---------------------------------------

Vector Time (GMT): 2008/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4654719
86                 A    =         6728065
53  meter
 Y    =       -4609834
39  meter          E    =           
0022771
 Z    =        1473961
22                 I    =           51
46968
 XDOT =       4396
944253                 Wp   =           46
94098
 YDOT =      -2575
846565  meter/sec      RA   =          214
40140  deg
 ZDOT =       5788
705366                 TA   =          329
35500
                                          MA   =          329
48781
                                          Ha   =            191
243  n
mi
                                          Hp   =            179
856

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15271390
60                 X    =        -4609986
10
 Y    =      -15124128
57  feet           Y    =        -4661636
26  meter
 Z    =        4835830
76                 Z    =         1451456
93
 XDOT =      14425
670122                 XDOT =        4397
301058
 YDOT =      -8450
940173  feet/sec       YDOT =       -2526
676359  meter/sec
 ZDOT =      18991
815504                 ZDOT =        5810
065755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6916837
40                 X    =        -2108252
04
 Y    =       20370272
09  feet           Y    =         6208858
93  meter
 Z    =        4748607
22                 Z    =         1447375
48
 XDOT =     -12372
812326                 XDOT =       -3771
233197
 YDOT =      -8679
370257  feet/sec       YDOT =       -2645
472054  meter/sec
 ZDOT =      19073
944561                 ZDOT =        5813
738302


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   08200
56064058  
00020000  00000-0  20000-3 0  9047
2 25544  51
6380 215
0394 0009829  25
7471 334
4181 15
75130446 33470


Satellite: ISS
Catalog Number: 25544
Epoch time:      08200
56064058   =   yrday
fracday
Element set:     904
Inclination:       51
6380  deg
RA of node:       215
0394  deg
Eccentricity:     
0009829     
Arg of perigee:    25
7471  deg
Mean anomaly:     334
4181  deg
Mean motion:   15
75130446  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3347
Checksum:              279


Coasting Arc #6 (Orbit 3361)
---------------------------------------

Vector Time (GMT): 2008/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3984327
28                 A    =         6718336
99  meter
 Y    =        2266278
78  meter          E    =           
0017790
 Z    =       -4924737
29                 I    =           51
46207
 XDOT =      -5453
168605                 Wp   =           73
42003
 YDOT =      -4990
228971  meter/sec      RA   =          209
21355  deg
 ZDOT =       2126
757308                 TA   =          217
21925
                                          MA   =          217
34269
                                          Ha   =            191
267  n
mi
                                          Hp   =            179
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13071939
91                 X    =        -3985450
07
 Y    =        7435297
84  feet           Y    =         2221718
16  meter
 Z    =      -16157274
58                 Z    =        -4944095
16
 XDOT =     -17890
973113                 XDOT =       -5407
292968
 YDOT =     -16372
142293  feet/sec       YDOT =       -5050
953226  meter/sec
 ZDOT =       6977
550222                 ZDOT =        2100
377093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12503266
70                 X    =         3810995
69
 Y    =        8210756
56  feet           Y    =         2502638
60  meter
 Z    =      -16231715
48                 Z    =        -4947426
88
 XDOT =      -5888
865878                 XDOT =       -1794
926320
 YDOT =      22486
133301  feet/sec       YDOT =        6853
773430  meter/sec
 ZDOT =       6875
325639                 ZDOT =        2095
599255


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   08201
51229356  
00020000  00000-0  20000-3 0  9058
2 25544  51
6381 210
1436 0009794  28
7657 331
4045 15
75126988 33623


Satellite: ISS
Catalog Number: 25544
Epoch time:      08201
51229356   =   yrday
fracday
Element set:     905
Inclination:       51
6381  deg
RA of node:       210
1436  deg
Eccentricity:     
0009794     
Arg of perigee:    28
7657  deg
Mean anomaly:     331
4045  deg
Mean motion:   15
75126988  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3362
Checksum:              293


Coasting Arc #7 (Orbit 3377)
---------------------------------------

Vector Time (GMT): 2008/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4825485
20                 A    =         6726732
15  meter
 Y    =        4118567
44  meter          E    =           
0010217
 Z    =       -2251270
07                 I    =           51
51568
 XDOT =      -4762
964191                 Wp   =           68
66089
 YDOT =       2612
541266  meter/sec      RA   =          204
09474  deg
 ZDOT =      -5445
834006                 TA   =          136
63104
                                          MA   =          136
55060
                                          Ha   =            191
362  n
mi
                                          Hp   =            179
549

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15831644
37                 X    =         4790008
13
 Y    =       13512360
36  feet           Y    =         4172330
68  meter
 Z    =       -7386056
66                 Z    =        -2227914
04
 XDOT =     -15626
522936                 XDOT =       -4765
369715
 YDOT =       8571
329614  feet/sec       YDOT =        2559
266244  meter/sec
 ZDOT =     -17866
909468                 ZDOT =       -5468
977559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4518593
57                 X    =         1377267
32
 Y    =      -20350324
57  feet           Y    =        -6202778
93  meter
 Z    =       -7295565
85                 Z    =        -2223688
47
 XDOT =      13353
052897                 XDOT =        4070
010523
 YDOT =       9382
861969  feet/sec       YDOT =        2859
896328  meter/sec
 ZDOT =     -17955
922345                 ZDOT =       -5472
965131


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   08202
52737994  
00020000  00000-0  20000-3 0  9063
2 25544  51
6370 204
9205 0009823  33
2033 326
9745 15
75156385 33785


Satellite: ISS
Catalog Number: 25544
Epoch time:      08202
52737994   =   yrday
fracday
Element set:     906
Inclination:       51
6370  deg
RA of node:       204
9205  deg
Eccentricity:     
0009823     
Arg of perigee:    33
2033  deg
Mean anomaly:     326
9745  deg
Mean motion:   15
75156385  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3378
Checksum:              300


Coasting Arc #8 (Orbit 3393)
---------------------------------------

Vector Time (GMT): 2008/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4335647
85                 A    =         6719614
47  meter
 Y    =       -2346862
15  meter          E    =           
0017683
 Z    =        4559973
78                 I    =           51
51936
 XDOT =       5559
618827                 Wp   =           49
61421
 YDOT =       4418
260787  meter/sec      RA   =          198
89877  deg
 ZDOT =      -2993
313088                 TA   =           70
22822
                                          MA   =           70
03761
                                          Ha   =            191
278  n
mi
                                          Hp   =            179
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14224566
44                 X    =         4339417
47
 Y    =       -7699678
98  feet           Y    =        -2298357
79  meter
 Z    =       14960543
91                 Z    =         4581044
92
 XDOT =      18240
219250                 XDOT =        5524
340643
 YDOT =      14495
606255  feet/sec       YDOT =        4480
234661  meter/sec
 ZDOT =      -9820
580997                 ZDOT =       -2966
390225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13569677
68                 X    =        -4136037
76
 Y    =       -8663460
65  feet           Y    =        -2640622
81  meter
 Z    =       15041592
93                 Z    =         4584677
52
 XDOT =       3227
423542                 XDOT =         983
718696
 YDOT =     -22031
615302  feet/sec       YDOT =       -6715
236344  meter/sec
 ZDOT =      -9716
289566                 ZDOT =       -2961
525060


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   08203
54245405  
00020000  00000-0  20000-3 0  9078
2 25544  51
6368 199
6978 0009861  36
1170 324
0658 15
75195208 33942


Satellite: ISS
Catalog Number: 25544
Epoch time:      08203
54245405   =   yrday
fracday
Element set:     907
Inclination:       51
6368  deg
RA of node:       199
6978  deg
Eccentricity:     
0009861     
Arg of perigee:    36
1170  deg
Mean anomaly:     324
0658  deg
Mean motion:   15
75195208  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3394
Checksum:              312


Coasting Arc #9 (Orbit 3409)
---------------------------------------

Vector Time (GMT): 2008/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4840201
64                 A    =         6724971
28  meter
 Y    =       -3597197
72  meter          E    =           
0021597
 Z    =        2947879
38                 I    =           51
56570
 XDOT =       5152
376010                 Wp   =           64
83310
 YDOT =      -2820
043881  meter/sec      RA   =          193
79461  deg
 ZDOT =       4999
271042                 TA   =          329
26720
                                          MA   =          329
39350
                                          Ha   =            191
392  n
mi
                                          Hp   =            179
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15879926
63                 X    =        -4813937
53
 Y    =      -11801829
79  feet           Y    =        -3651177
01  meter
 Z    =        9671520
26                 Z    =         2924429
53
 XDOT =      16904
120768                 XDOT =        5159
242038
 YDOT =      -9252
112470  feet/sec       YDOT =       -2762
389040  meter/sec
 ZDOT =      16401
807880                 ZDOT =        5024
317404

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2301899
48                 X    =         -701618
96
 Y    =       19695305
18  feet           Y    =         6003129
02  meter
 Z    =        9580697
94                 Z    =         2920196
73
 XDOT =     -14956
760035                 XDOT =       -4558
820459
 YDOT =      -9804
705138  feet/sec       YDOT =       -2988
474126  meter/sec
 ZDOT =      16498
148571                 ZDOT =        5028
635685


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   08204
55751675  
00020000  00000-0  20000-3 0  9082
2 25544  51
6369 194
4762 0009758  39
8766 320
3113 15
75228925 34100


Satellite: ISS
Catalog Number: 25544
Epoch time:      08204
55751675   =   yrday
fracday
Element set:     908
Inclination:       51
6369  deg
RA of node:       194
4762  deg
Eccentricity:     
0009758     
Arg of perigee:    39
8766  deg
Mean anomaly:     320
3113  deg
Mean motion:   15
75228925  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3410
Checksum:              314


Coasting Arc #10 (Orbit 3424)
---------------------------------------

Vector Time (GMT): 2008/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4641177
24                 A    =         6721316
09  meter
 Y    =        2600556
65  meter          E    =           
0014946
 Z    =       -4116772
81                 I    =           51
58213
 XDOT =      -5489
817210                 Wp   =           72
50936
 YDOT =      -3853
932303  meter/sec      RA   =          188
59547  deg
 ZDOT =       3770
217741                 TA   =          236
12987
                                          MA   =          236
27216
                                          Ha   =            191
479  n
mi
                                          Hp   =            178
978

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15226959
45                 X    =        -4649913
78
 Y    =        8532010
01  feet           Y    =         2548607
78  meter
 Z    =      -13506472
48                 Z    =        -4139340
49
 XDOT =     -18011
211318                 XDOT =       -5464
628783
 YDOT =     -12644
134854  feet/sec       YDOT =       -3915
182019  meter/sec
 ZDOT =      12369
480779                 ZDOT =        3743
609360

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15092446
28                 X    =         4600177
62
 Y    =        8632563
87  feet           Y    =         2631205
47  meter
 Z    =      -13593277
53                 Z    =        -4143230
99
 XDOT =       -955
845405                 XDOT =        -291
341679
 YDOT =      20906
328449  feet/sec       YDOT =        6372
248911  meter/sec
 ZDOT =      12266
439959                 ZDOT =        3738
810900


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   08205
50912919  
00020000  00000-0  20000-3 0  9099
2 25544  51
6368 189
5800 0009963  43
2219 316
9725 15
75192152 34255


Satellite: ISS
Catalog Number: 25544
Epoch time:      08205
50912919   =   yrday
fracday
Element set:     909
Inclination:       51
6368  deg
RA of node:       189
5800  deg
Eccentricity:     
0009963     
Arg of perigee:    43
2219  deg
Mean anomaly:     316
9725  deg
Mean motion:   15
75192152  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3425
Checksum:              306


Coasting Arc #11 (Orbit 3427)
---------------------------------------

Vector Time (GMT): 2008/205/16:29:06
638
Vector Time (MET): N/A
Weight (LBS)     : 660953
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2715883
36                 A    =         6725621
05  meter
 Y    =        3622681
90  meter          E    =           
0010008
 Z    =       -4982063
17                 I    =           51
57893
 XDOT =      -6990
750377                 Wp   =           92
61513
 YDOT =      -2522
449811  meter/sec      RA   =          187
64318  deg
 ZDOT =       1979
662246                 TA   =          196
54857
                                          MA   =          196
58125
                                          Ha   =            191
859  n
mi
                                          Hp   =            186
920

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8910378
49                 X    =        -2731989
15
 Y    =       11885439
30  feet           Y    =         3592221
63  meter
 Z    =      -16345351
62                 Z    =        -4995295
70
 XDOT =     -22935
532732                 XDOT =       -6971
641138
 YDOT =      -8275
753972  feet/sec       YDOT =       -2600
517689  meter/sec
 ZDOT =       6494
954874                 ZDOT =        1945
747689

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7007464
24                 X    =         2135875
10
 Y    =      -13034352
72  feet           Y    =        -3972870
71  meter
 Z    =      -16396039
95                 Z    =        -4997512
98
 XDOT =      22976
310402                 XDOT =        7003
179411
 YDOT =       4359
449718  feet/sec       YDOT =        1328
760274  meter/sec
 ZDOT =       6363
858806                 ZDOT =        1939
704164


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   08205
69946698  
00020000  00000-0  20000-3 0  9102
2 25544  51
6396 188
6013 0003919 317
2749  42
8109 15
72500751 34288


Satellite: ISS
Catalog Number: 25544
Epoch time:      08205
69946698   =   yrday
fracday
Element set:     910
Inclination:       51
6396  deg
RA of node:       188
6013  deg
Eccentricity:     
0003919     
Arg of perigee:   317
2749  deg
Mean anomaly:      42
8109  deg
Mean motion:   15
72500751  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3428
Checksum:              312


Coasting Arc #12 (Orbit 3443)
---------------------------------------

Vector Time (GMT): 2008/206/16:29:06
638
Vector Time (MET): N/A
Weight (LBS)     : 660953
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6478409
14                 A    =         6735769
11  meter
 Y    =        1308148
76  meter          E    =           
0005223
 Z    =       -1287852
58                 I    =           51
64255
 XDOT =      -2077
807787                 Wp   =          144
93102
 YDOT =       4543
869497  meter/sec      RA   =          182
54507  deg
 ZDOT =      -5852
615176                 TA   =           49
18628
                                          MA   =           49
14099
                                          Ha   =            191
958  n
mi
                                          Hp   =            186
960

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21254623
15                 X    =         6469555
85
 Y    =        4291826
65  feet           Y    =         1380544
66  meter
 Z    =       -4225238
13                 Z    =        -1256401
98
 XDOT =      -6816
954682                 XDOT =       -2100
032783
 YDOT =      14907
708323  feet/sec       YDOT =        4520
510451  meter/sec
 ZDOT =     -19201
493360                 ZDOT =       -5862
762760

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21692178
04                 X    =        -6611775
87
 Y    =        -799981
34  feet           Y    =         -243834
31  meter
 Z    =       -4103761
75                 Z    =        -1250826
58
 XDOT =       4153
894235                 XDOT =        1266
106963
 YDOT =     -14213
122325  feet/sec       YDOT =       -4332
159685  meter/sec
 ZDOT =     -19240
190934                 ZDOT =       -5864
410197


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   08206
71626427  
00020000  00000-0  20000-3 0  9112
2 25544  51
6400 183
3911 0003883 320
0296  40
0580 15
72499758 34447


Satellite: ISS
Catalog Number: 25544
Epoch time:      08206
71626427   =   yrday
fracday
Element set:     911
Inclination:       51
6400  deg
RA of node:       183
3911  deg
Eccentricity:     
0003883     
Arg of perigee:   320
0296  deg
Mean anomaly:      40
0580  deg
Mean motion:   15
72499758  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3444
Checksum:              281


Coasting Arc #13 (Orbit 3459)
---------------------------------------

Vector Time (GMT): 2008/207/16:29:06
638
Vector Time (MET): N/A
Weight (LBS)     : 660953
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         865730
21                 A    =         6724444
69  meter
 Y    =       -4165826
21  meter          E    =           
0005045
 Z    =        5207382
38                 I    =           51
63405
 XDOT =       7630
443184                 Wp   =            6
13250
 YDOT =        400
826486  meter/sec      RA   =          177
40099  deg
 ZDOT =       -942
901109                 TA   =           92
88287
                                          MA   =           92
82513
                                          Ha   =            191
906  n
mi
                                          Hp   =            186
784

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2840322
20                 X    =          886952
29
 Y    =      -13667408
82  feet           Y    =        -4156026
97  meter
 Z    =       17084587
86                 Z    =         5211639
23
 XDOT =      25034
262416                 XDOT =        7629
974407
 YDOT =       1315
047526  feet/sec       YDOT =         486
151956  meter/sec
 ZDOT =      -3093
507575                 ZDOT =        -905
833528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -260315
75                 X    =          -79344
24
 Y    =       13937373
78  feet           Y    =         4248111
53  meter
 Z    =       17100598
94                 Z    =         5212262
56
 XDOT =     -23867
901186                 XDOT =       -7274
936281
 YDOT =       3194
422090  feet/sec       YDOT =         973
659853  meter/sec
 ZDOT =      -2950
438662                 ZDOT =        -899
293704


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   08207
73304983  
00020000  00000-0  20000-3 0  9126
2 25544  51
6396 178
1808 0004046 323
6962  36
3925 15
72570953 34605


Satellite: ISS
Catalog Number: 25544
Epoch time:      08207
73304983   =   yrday
fracday
Element set:     912
Inclination:       51
6396  deg
RA of node:       178
1808  deg
Eccentricity:     
0004046     
Arg of perigee:   323
6962  deg
Mean anomaly:      36
3925  deg
Mean motion:   15
72570953  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3460
Checksum:              303

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics 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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