Date: October 2nd 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 3875 01 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2754)
---------------------------------------

Vector Time (GMT): 2007/274/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3313017
95                 A    =         6719337
95  meter
 Y    =        3704049
03  meter          E    =           
0011345
 Z    =        4516451
35                 I    =           51
30240
 XDOT =      -3000
529949                 Wp   =           62
98101
 YDOT =       6411
711481  meter/sec      RA   =          274
91263  deg
 ZDOT =      -3046
417008                 TA   =           57
50400
                                          MA   =           57
39441
                                          Ha   =            188
800  n
mi
                                          Hp   =            180
851

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10869481
45                 X    =         3249412
01
 Y    =       12152391
84  feet           Y    =         3740741
39  meter
 Z    =       14817753
78                 Z    =         4532391
80
 XDOT =      -9844
258364                 XDOT =       -3057
204466
 YDOT =      21035
798821  feet/sec       YDOT =        6377
841006  meter/sec
 ZDOT =      -9994
806456                 ZDOT =       -3061
131429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9470836
33                 X    =        -2886710
91
 Y    =      -13202994
83  feet           Y    =        -4024272
83  meter
 Z    =       14878718
63                 Z    =         4535033
44
 XDOT =      10948
936342                 XDOT =        3337
235797
 YDOT =     -19219
707221  feet/sec       YDOT =       -5858
166761  meter/sec
 ZDOT =     -10049
884640                 ZDOT =       -3063
204838


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   07274
50057236  
00020000  00000-0  20000-3 0  9007
2 25544  51
6335 275
4361 0002743  53
6295 306
5122 15
75360614 27555


Satellite: ISS
Catalog Number: 25544
Epoch time:      07274
50057236   =   yrday
fracday
Element set:     900
Inclination:       51
6335  deg
RA of node:       275
4361  deg
Eccentricity:     
0002743     
Arg of perigee:    53
6295  deg
Mean anomaly:     306
5122  deg
Mean motion:   15
75360614  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2755
Checksum:              274


Coasting Arc #2 (Orbit 2770)
---------------------------------------

Vector Time (GMT): 2007/275/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2412633
25                 A    =         6724268
02  meter
 Y    =       -5482859
10  meter          E    =           
0015694
 Z    =        3038333
65                 I    =           51
31752
 XDOT =       3939
418201                 Wp   =           79
63089
 YDOT =       4459
084053  meter/sec      RA   =          269
79077  deg
 ZDOT =       4899
909909                 TA   =          315
78315
                                          MA   =          315
90846
                                          Ha   =            188
872  n
mi
                                          Hp   =            180
814

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7915463
43                 X    =         2459004
24
 Y    =      -17988382
88  feet           Y    =        -5455620
45  meter
 Z    =        9968286
26                 Z    =         3050166
92
 XDOT =      12924
600397                 XDOT =        3865
460108
 YDOT =      14629
540855  feet/sec       YDOT =        4502
723257  meter/sec
 ZDOT =      16075
819912                 ZDOT =        4918
868253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9382951
52                 X    =        -2859923
62
 Y    =       17242750
24  feet           Y    =         5255590
27  meter
 Z    =       10012541
92                 Z    =         3051822
78
 XDOT =     -10265
677479                 XDOT =       -3128
978495
 YDOT =     -14998
622447  feet/sec       YDOT =       -4571
580122  meter/sec
 ZDOT =      16148
340978                 ZDOT =        4922
014330


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   07275
51553519  
00020000  00000-0  20000-3 0  9015
2 25544  51
6332 270
2128 0002781  56
8079 303
3351 15
75356405 27713


Satellite: ISS
Catalog Number: 25544
Epoch time:      07275
51553519   =   yrday
fracday
Element set:     901
Inclination:       51
6332  deg
RA of node:       270
2128  deg
Eccentricity:     
0002781     
Arg of perigee:    56
8079  deg
Mean anomaly:     303
3351  deg
Mean motion:   15
75356405  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2771
Checksum:              280


Coasting Arc #3 (Orbit 2785)
---------------------------------------

Vector Time (GMT): 2007/276/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3590814
03                 A    =         6721324
50  meter
 Y    =       -4059358
94  meter          E    =           
0009197
 Z    =       -3983898
19                 I    =           51
30939
 XDOT =       2568
665201                 Wp   =           95
06055
 YDOT =      -6106
957635  meter/sec      RA   =          264
57088  deg
 ZDOT =       3914
370052                 TA   =          215
57936
                                          MA   =          215
64071
                                          Ha   =            188
891  n
mi
                                          Hp   =            180
720

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11780885
93                 X    =        -3525801
60
 Y    =      -13318106
76  feet           Y    =        -4099149
92  meter
 Z    =      -13070532
12                 Z    =        -4001184
61
 XDOT =       8427
379267                 XDOT =        2617
747770
 YDOT =     -20035
950246  feet/sec       YDOT =       -6077
958967  meter/sec
 ZDOT =      12842
421432                 ZDOT =        3926
967888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10757729
16                 X    =         3278955
85
 Y    =       14096074
81  feet           Y    =         4296483
60  meter
 Z    =      -13136665
83                 Z    =        -4004055
74
 XDOT =      -8693
273614                 XDOT =       -2649
709798
 YDOT =      18625
512782  feet/sec       YDOT =        5677
056296  meter/sec
 ZDOT =      12889
502711                 ZDOT =        3928
720426


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   07276
46704841  
00020000  00000-0  20000-3 0  9027
2 25544  51
6334 265
3160 0002770  58
5549 301
5885 15
75362691 27867


Satellite: ISS
Catalog Number: 25544
Epoch time:      07276
46704841   =   yrday
fracday
Element set:     902
Inclination:       51
6334  deg
RA of node:       265
3160  deg
Eccentricity:     
0002770     
Arg of perigee:    58
5549  deg
Mean anomaly:     301
5885  deg
Mean motion:   15
75362691  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2786
Checksum:              306


Coasting Arc #4 (Orbit 2801)
---------------------------------------

Vector Time (GMT): 2007/277/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2123128
03                 A    =         6721955
07  meter
 Y    =        5142388
81  meter          E    =           
0008919
 Z    =       -3782251
04                 I    =           51
31440
 XDOT =      -4295
332723                 Wp   =           71
88002
 YDOT =      -4835
225541  meter/sec      RA   =          259
45223  deg
 ZDOT =      -4168
200644                 TA   =          154
19529
                                          MA   =          154
15077
                                          Ha   =            188
886  n
mi
                                          Hp   =            180
670

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6965643
14                 X    =        -2162099
64
 Y    =       16871354
36  feet           Y    =         5118428
86  meter
 Z    =      -12408960
09                 Z    =        -3792659
93
 XDOT =     -14092
298961                 XDOT =       -4220
696831
 YDOT =     -15863
600855  feet/sec       YDOT =       -4882
841102  meter/sec
 ZDOT =     -13675
198962                 ZDOT =       -4188
886113

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7763951
42                 X    =         2366452
39
 Y    =      -16489913
92  feet           Y    =        -5026125
76  meter
 Z    =      -12447846
00                 Z    =        -3794103
46
 XDOT =      11968
589539                 XDOT =        3648
026092
 YDOT =      16004
876358  feet/sec       YDOT =        4878
286314  meter/sec
 ZDOT =     -13754
345774                 ZDOT =       -4192
324592


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   07277
48198201  
00020000  00000-0  20000-3 0  9038
2 25544  51
6320 260
0915 0002761  63
4316 296
7130 15
75392742 28026


Satellite: ISS
Catalog Number: 25544
Epoch time:      07277
48198201   =   yrday
fracday
Element set:     903
Inclination:       51
6320  deg
RA of node:       260
0915  deg
Eccentricity:     
0002761     
Arg of perigee:    63
4316  deg
Mean anomaly:     296
7130  deg
Mean motion:   15
75392742  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2802
Checksum:              276


Coasting Arc #5 (Orbit 2817)
---------------------------------------

Vector Time (GMT): 2007/278/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3943523
56                 A    =         6723346
70  meter
 Y    =        4348910
19  meter          E    =           
0015225
 Z    =        3264870
43                 I    =           51
32580
 XDOT =      -2317
432568                 Wp   =           86
78297
 YDOT =       5647
499709  meter/sec      RA   =          254
23089  deg
 ZDOT =      -4703
812727                 TA   =           54
71463
                                          MA   =           54
57231
                                          Ha   =            188
744  n
mi
                                          Hp   =            180
617

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12938069
43                 X    =         3878740
13
 Y    =       14268078
04  feet           Y    =         4392646
77  meter
 Z    =       10711517
16                 Z    =         3283870
62
 XDOT =      -7603
125224                 XDOT =       -2357
561204
 YDOT =      18528
542352  feet/sec       YDOT =        5621
360361  meter/sec
 ZDOT =     -15432
456454                 ZDOT =       -4715
168471

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12372863
50                 X    =        -3771248
80
 Y    =      -14707863
39  feet           Y    =        -4482956
76  meter
 Z    =       10784215
08                 Z    =         3287028
75
 XDOT =       7084
441469                 XDOT =        2159
337760
 YDOT =     -17353
374246  feet/sec       YDOT =       -5289
308470  meter/sec
 ZDOT =     -15474
870000                 ZDOT =       -4716
740376


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   07278
49689932  
00020000  00000-0  20000-3 0  9047
2 25544  51
6315 254
8673 0002751  63
1609 296
9836 15
75450830 28188


Satellite: ISS
Catalog Number: 25544
Epoch time:      07278
49689932   =   yrday
fracday
Element set:     904
Inclination:       51
6315  deg
RA of node:       254
8673  deg
Eccentricity:     
0002751     
Arg of perigee:    63
1609  deg
Mean anomaly:     296
9836  deg
Mean motion:   15
75450830  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2818
Checksum:              327


Coasting Arc #6 (Orbit 2833)
---------------------------------------

Vector Time (GMT): 2007/279/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1966387
90                 A    =         6719591
53  meter
 Y    =       -4689926
26  meter          E    =           
0011397
 Z    =        4383811
10                 I    =           51
32177
 XDOT =       4763
920875                 Wp   =          101
59000
 YDOT =       5085
843646  meter/sec      RA   =          249
11124  deg
 ZDOT =       3294
613237                 TA   =          315
16788
                                          MA   =          315
25991
                                          Ha   =            188
712  n
mi
                                          Hp   =            180
622

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6451403
86                 X    =         1997389
39
 Y    =      -15386897
18  feet           Y    =        -4667763
44  meter
 Z    =       14382582
35                 Z    =         4393439
38
 XDOT =      15629
661665                 XDOT =        4690
691466
 YDOT =      16685
838735  feet/sec       YDOT =        5138
707226  meter/sec
 ZDOT =      10809
098546                 ZDOT =        3317
578289

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6640711
03                 X    =        -2024088
72
 Y    =       15272269
70  feet           Y    =         4654987
81  meter
 Z    =       14418551
48                 Z    =         4394774
49
 XDOT =     -14158
305406                 XDOT =       -4315
451488
 YDOT =     -16473
440312  feet/sec       YDOT =       -5021
104607  meter/sec
 ZDOT =      10896
956830                 ZDOT =        3321
392442


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   07279
51180218  
00020000  00000-0  20000-3 0  9055
2 25544  51
6309 249
6434 0002659  67
3144 292
8300 15
75463048 28349


Satellite: ISS
Catalog Number: 25544
Epoch time:      07279
51180218   =   yrday
fracday
Element set:     905
Inclination:       51
6309  deg
RA of node:       249
6434  deg
Eccentricity:     
0002659     
Arg of perigee:    67
3144  deg
Mean anomaly:     292
8300  deg
Mean motion:   15
75463048  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2834
Checksum:              296


Coasting Arc #7 (Orbit 2848)
---------------------------------------

Vector Time (GMT): 2007/280/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4374260
53                 A    =         6725346
10  meter
 Y    =       -4484643
32  meter          E    =           
0008092
 Z    =       -2444744
08                 I    =           51
35281
 XDOT =       2248
798300                 Wp   =           56
56086
 YDOT =      -5086
591001  meter/sec      RA   =          243
89688  deg
 ZDOT =       5324
238830                 TA   =          275
69797
                                          MA   =          275
79023
                                          Ha   =            188
816  n
mi
                                          Hp   =            180
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14351248
44                 X    =        -4311911
28
 Y    =      -14713396
73  feet           Y    =        -4533210
34  meter
 Z    =       -8020813
91                 Z    =        -2465842
59
 XDOT =       7377
947177                 XDOT =        2279
645856
 YDOT =     -16688
290685  feet/sec       YDOT =       -5061
270819  meter/sec
 ZDOT =      17467
975163                 ZDOT =        5335
238831

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14299554
26                 X    =         4358504
14
 Y    =       14719511
40  feet           Y    =         4486507
07  meter
 Z    =       -8101516
11                 Z    =        -2469342
11
 XDOT =      -6213
391876                 XDOT =       -1893
841844
 YDOT =      15642
522366  feet/sec       YDOT =        4767
840817  meter/sec
 ZDOT =      17509
098228                 ZDOT =        5336
773140


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   07280
46325957  
00020000  00000-0  20000-3 0  9063
2 25544  51
6308 244
7457 0002859  71
3166 288
8308 15
75465961 28495


Satellite: ISS
Catalog Number: 25544
Epoch time:      07280
46325957   =   yrday
fracday
Element set:     906
Inclination:       51
6308  deg
RA of node:       244
7457  deg
Eccentricity:     
0002859     
Arg of perigee:    71
3166  deg
Mean anomaly:     288
8308  deg
Mean motion:   15
75465961  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2849
Checksum:              330


Coasting Arc #8 (Orbit 2864)
---------------------------------------

Vector Time (GMT): 2007/281/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2027228
77                 A    =         6717590
46  meter
 Y    =        4173401
59  meter          E    =           
0015121
 Z    =       -4871855
77                 I    =           51
34094
 XDOT =      -5236
038432                 Wp   =           73
71333
 YDOT =      -5166
035173  meter/sec      RA   =          238
76756  deg
 ZDOT =      -2248
231001                 TA   =          174
31263
                                          MA   =          174
29544
                                          Ha   =            188
797  n
mi
                                          Hp   =            180
433

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6651013
04                 X    =        -2050078
88
 Y    =       13692262
43  feet           Y    =         4150603
81  meter
 Z    =      -15983778
78                 Z    =        -4881759
98
 XDOT =     -17178
603778                 XDOT =       -5166
960289
 YDOT =     -16948
934295  feet/sec       YDOT =       -5224
201465  meter/sec
 ZDOT =      -7376
085960                 ZDOT =       -2273
499708

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6330440
18                 X    =         1929518
17
 Y    =      -13800469
73  feet           Y    =        -4206383
18  meter
 Z    =      -16020854
26                 Z    =        -4883156
38
 XDOT =      16412
317312                 XDOT =        5002
474317
 YDOT =      16197
490272  feet/sec       YDOT =        4936
995035  meter/sec
 ZDOT =      -7472
720683                 ZDOT =       -2277
685264


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   07281
47813175  
00020000  00000-0  20000-3 0  9070
2 25544  51
6311 239
5203 0002781  74
1704 285
9766 15
75486865 28653


Satellite: ISS
Catalog Number: 25544
Epoch time:      07281
47813175   =   yrday
fracday
Element set:     907
Inclination:       51
6311  deg
RA of node:       239
5203  deg
Eccentricity:     
0002781     
Arg of perigee:    74
1704  deg
Mean anomaly:     285
9766  deg
Mean motion:   15
75486865  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2865
Checksum:              315


Coasting Arc #9 (Orbit 2880)
---------------------------------------

Vector Time (GMT): 2007/282/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4772286
82                 A    =         6726859
24  meter
 Y    =        4499929
80  meter          E    =           
0016156
 Z    =        1461642
19                 I    =           51
38929
 XDOT =      -2435
091759                 Wp   =          111
85173
 YDOT =       4474
844611  meter/sec      RA   =          233
56822  deg
 ZDOT =      -5780
952012                 TA   =           51
98671
                                          MA   =           51
84096
                                          Ha   =            188
694  n
mi
                                          Hp   =            180
424

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15657108
99                 X    =         4714512
74
 Y    =       14763549
22  feet           Y    =         4552973
30  meter
 Z    =        4795414
02                 Z    =         1484685
59
 XDOT =      -7989
146190                 XDOT =       -2456
865926
 YDOT =      14681
248725  feet/sec       YDOT =        4447
491806  meter/sec
 ZDOT =     -18966
377993                 ZDOT =       -5792
835126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16122332
39                 X    =        -4914086
91
 Y    =      -14224103
17  feet           Y    =        -4335506
65  meter
 Z    =        4883516
18                 Z    =         1488495
73
 XDOT =       6341
855752                 XDOT =        1932
997633
 YDOT =     -13764
976927  feet/sec       YDOT =       -4195
564967  meter/sec
 ZDOT =     -19010
928111                 ZDOT =       -5794
530888


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   07282
49298712  
00020000  00000-0  20000-3 0  9088
2 25544  51
6315 234
2958 0002738  74
6879 285
4587 15
75533052 28811


Satellite: ISS
Catalog Number: 25544
Epoch time:      07282
49298712   =   yrday
fracday
Element set:     908
Inclination:       51
6315  deg
RA of node:       234
2958  deg
Eccentricity:     
0002738     
Arg of perigee:    74
6879  deg
Mean anomaly:     285
4587  deg
Mean motion:   15
75533052  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2881
Checksum:              331


Coasting Arc #10 (Orbit 2896)
---------------------------------------

Vector Time (GMT): 2007/283/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2268993
23                 A    =         6716072
28  meter
 Y    =       -3650612
59  meter          E    =           
0006014
 Z    =        5155758
99                 I    =           51
37196
 XDOT =       5685
411257                 Wp   =          106
14486
 YDOT =       5087
760825  meter/sec      RA   =          228
42644  deg
 ZDOT =       1097
671407                 TA   =          333
33665
                                          MA   =          333
36756
                                          Ha   =            188
572  n
mi
                                          Hp   =            180
434

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7444203
50                 X    =         2284600
05
 Y    =      -11977075
44  feet           Y    =        -3625151
76  meter
 Z    =       16915219
77                 Z    =         5166820
17
 XDOT =      18652
924073                 XDOT =        5622
764203
 YDOT =      16692
128691  feet/sec       YDOT =        5150
988121  meter/sec
 ZDOT =       3601
284145                 ZDOT =        1125
139099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6726633
97                 X    =        -2050278
03
 Y    =       12337422
98  feet           Y    =         3760446
53  meter
 Z    =       16956755
33                 Z    =         5168419
02
 XDOT =     -18562
169332                 XDOT =       -5657
749212
 YDOT =     -15226
635383  feet/sec       YDOT =       -4641
078465  meter/sec
 ZDOT =       3706
269990                 ZDOT =        1129
671093


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   07283
50782635  
00020000  00000-0  20000-3 0  9094
2 25544  51
6321 229
0719 0002633  78
6002 281
5458 15
75561619 28972


Satellite: ISS
Catalog Number: 25544
Epoch time:      07283
50782635   =   yrday
fracday
Element set:     909
Inclination:       51
6321  deg
RA of node:       229
0719  deg
Eccentricity:     
0002633     
Arg of perigee:    78
6002  deg
Mean anomaly:     281
5458  deg
Mean motion:   15
75561619  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2897
Checksum:              308


Coasting Arc #11 (Orbit 2911)
---------------------------------------

Vector Time (GMT): 2007/284/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5116802
73                 A    =         6727582
55  meter
 Y    =       -4338169
45  meter          E    =           
0013399
 Z    =        -433757
45                 I    =           51
43127
 XDOT =       2822
647888                 Wp   =           49
57822
 YDOT =      -3916
499413  meter/sec      RA   =          223
24767  deg
 ZDOT =       6002
936646                 TA   =          305
68792
                                          MA   =          305
81255
                                          Ha   =            188
624  n
mi
                                          Hp   =            180
356

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16787410
54                 X    =        -5065805
21
 Y    =      -14232839
39  feet           Y    =        -4395103
32  meter
 Z    =       -1423088
74                 Z    =         -458491
29
 XDOT =       9260
655801                 XDOT =        2837
071108
 YDOT =     -12849
407522  feet/sec       YDOT =       -3884
853916  meter/sec
 ZDOT =      19694
674037                 ZDOT =        6016
684695

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17712377
18                 X    =         5398732
57
 Y    =       13053146
98  feet           Y    =         3978599
20  meter
 Z    =       -1517596
66                 Z    =         -462563
46
 XDOT =      -7298
543743                 XDOT =       -2224
596133
 YDOT =      12153
042990  feet/sec       YDOT =        3704
247503  meter/sec
 ZDOT =      19746
381642                 ZDOT =        6018
697124


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   07284
45922344  
00020000  00000-0  20000-3 0  9104
2 25544  51
6322 224
1738 0002713  83
6575 276
4898 15
75581709 29121


Satellite: ISS
Catalog Number: 25544
Epoch time:      07284
45922344   =   yrday
fracday
Element set:     910
Inclination:       51
6322  deg
RA of node:       224
1738  deg
Eccentricity:     
0002713     
Arg of perigee:    83
6575  deg
Mean anomaly:     276
4898  deg
Mean motion:   15
75581709  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2912
Checksum:              307


Coasting Arc #12 (Orbit 2927)
---------------------------------------

Vector Time (GMT): 2007/285/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2714023
44                 A    =         6715579
45  meter
 Y    =        3202353
50  meter          E    =           
0017660
 Z    =       -5257130
44                 I    =           51
41367
 XDOT =      -5980
532197                 Wp   =           90
31748
 YDOT =      -4833
004699  meter/sec      RA   =          218
08746  deg
 ZDOT =        143
803652                 TA   =          181
05138
                                          MA   =          181
05510
                                          Ha   =            188
601  n
mi
                                          Hp   =            180
273

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8904276
36                 X    =        -2724092
04
 Y    =       10506409
11  feet           Y    =         3171947
18  meter
 Z    =      -17247803
29                 Z    =        -5270340
15
 XDOT =     -19621
168625                 XDOT =       -5926
742913
 YDOT =     -15856
314628  feet/sec       YDOT =       -4899
581636  meter/sec
 ZDOT =        471
796758                 ZDOT =         114
880359

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7876822
00                 X    =         2400855
35
 Y    =      -11220850
94  feet           Y    =        -3420115
37  meter
 Z    =      -17297562
48                 Z    =        -5272297
04
 XDOT =      20088
782717                 XDOT =        6123
060972
 YDOT =      13546
573769  feet/sec       YDOT =        4128
995685  meter/sec
 ZDOT =        361
308646                 ZDOT =         110
126875


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   07285
47403054  
00020000  00000-0  20000-3 0  9110
2 25544  51
6330 218
9490 0002615  85
1360 275
0102 15
75591522 29280


Satellite: ISS
Catalog Number: 25544
Epoch time:      07285
47403054   =   yrday
fracday
Element set:     911
Inclination:       51
6330  deg
RA of node:       218
9490  deg
Eccentricity:     
0002615     
Arg of perigee:    85
1360  deg
Mean anomaly:     275
0102  deg
Mean motion:   15
75591522  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2928
Checksum:              272

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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