Date: November 13th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6727 44 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 1186)
---------------------------------------

Vector Time (GMT): 2008/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2722358
82                 A    =         6729512
13  meter
 Y    =       -4704987
30  meter          E    =           
0005366
 Z    =       -3970232
18                 I    =           51
50419
 XDOT =       6579
788393                 Wp   =           71
46388
 YDOT =        470
308139  meter/sec      RA   =          335
56703  deg
 ZDOT =       3960
406950                 TA   =          239
63231
                                          MA   =          239
68537
                                          Ha   =            192
374  n
mi
                                          Hp   =            186
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8931623
43                 X    =         2794055
83
 Y    =      -15436310
05  feet           Y    =        -4674143
23  meter
 Z    =      -13025696
12                 Z    =        -3956832
54
 XDOT =      21587
232260                 XDOT =        6554
800626
 YDOT =       1543
005707  feet/sec       YDOT =         543
747214  meter/sec
 ZDOT =      12993
461122                 ZDOT =        3992
312108

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6396300
39                 X    =         1949592
36
 Y    =       16687793
99  feet           Y    =         5086439
61  meter
 Z    =      -12974097
18                 Z    =        -3954504
82
 XDOT =     -13456
427523                 XDOT =       -4101
519109
 YDOT =      15340
333343  feet/sec       YDOT =        4675
733603  meter/sec
 ZDOT =      13117
146319                 ZDOT =        3998
106198


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   08317
50856934  
00020000  00000-0  20000-3 0  9008
2 25544  51
6430 336
0654 0004034 338
4058  21
6933 15
72552216 11877


Satellite: ISS
Catalog Number: 25544
Epoch time:      08317
50856934   =   yrday
fracday
Element set:     900
Inclination:       51
6430  deg
RA of node:       336
0654  deg
Eccentricity:     
0004034     
Arg of perigee:   338
4058  deg
Mean anomaly:      21
6933  deg
Mean motion:   15
72552216  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1187
Checksum:              277


Coasting Arc #2 (Orbit 1202)
---------------------------------------

Vector Time (GMT): 2008/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5947425
54                 A    =         6731937
60  meter
 Y    =         516188
95  meter          E    =           
0004307
 Z    =       -3117523
09                 I    =           51
48548
 XDOT =       2056
577580                 Wp   =           47
60644
 YDOT =      -5602
222235  meter/sec      RA   =          330
48211  deg
 ZDOT =      -4852
421117                 TA   =          168
66431
                                          MA   =          168
65461
                                          Ha   =            192
404  n
mi
                                          Hp   =            186
237

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19512550
97                 X    =        -5937610
70
 Y    =        1693533
29  feet           Y    =          449736
55  meter
 Z    =      -10228094
13                 Z    =        -3146392
85
 XDOT =       6747
301773                 XDOT =        2142
642730
 YDOT =     -18379
994210  feet/sec       YDOT =       -5578
742750  meter/sec
 ZDOT =     -15920
016787                 ZDOT =       -4842
221336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10579919
40                 X    =         3224759
43
 Y    =      -16412567
55  feet           Y    =        -5002550
59  meter
 Z    =      -10339948
83                 Z    =        -3151616
40
 XDOT =       9140
178723                 XDOT =        2785
926475
 YDOT =      15894
074468  feet/sec       YDOT =        4844
513898  meter/sec
 ZDOT =     -15880
875995                 ZDOT =       -4840
491003


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   08318
52533014  
00020000  00000-0  20000-3 0  9013
2 25544  51
6419 330
8544 0004009 341
9086  18
1933 15
72571509 12032


Satellite: ISS
Catalog Number: 25544
Epoch time:      08318
52533014   =   yrday
fracday
Element set:     901
Inclination:       51
6419  deg
RA of node:       330
8544  deg
Eccentricity:     
0004009     
Arg of perigee:   341
9086  deg
Mean anomaly:      18
1933  deg
Mean motion:   15
72571509  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1203
Checksum:              267


Coasting Arc #3 (Orbit 1218)
---------------------------------------

Vector Time (GMT): 2008/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -851997
98                 A    =         6727405
44  meter
 Y    =        4938703
61  meter          E    =           
0010394
 Z    =        4485590
06                 I    =           51
44459
 XDOT =      -6825
668908                 Wp   =           44
17789
 YDOT =       1683
930813  meter/sec      RA   =          325
29652  deg
 ZDOT =      -3138
805798                 TA   =           77
30146
                                          MA   =           77
18528
                                          Ha   =            192
479  n
mi
                                          Hp   =            186
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2795268
97                 X    =         -928950
91
 Y    =       16203095
84  feet           Y    =         4928745
29  meter
 Z    =       14716502
81                 Z    =         4481264
57
 XDOT =     -22393
926864                 XDOT =       -6828
743367
 YDOT =       5524
707391  feet/sec       YDOT =        1607
585417  meter/sec
 ZDOT =     -10297
919286                 ZDOT =       -3171
973207

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11250193
04                 X    =        -3429058
84
 Y    =      -12011250
91  feet           Y    =        -3661029
28  meter
 Z    =       14700078
45                 Z    =         4480583
91
 XDOT =       8077
864821                 XDOT =        2462
133198
 YDOT =     -20373
469594  feet/sec       YDOT =       -6209
833532  meter/sec
 ZDOT =     -10426
356780                 ZDOT =       -3177
953547


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   08319
54207715  
00020000  00000-0  20000-3 0  9023
2 25544  51
6411 325
6434 0004107 346
3692  13
7359 15
72614718 12195


Satellite: ISS
Catalog Number: 25544
Epoch time:      08319
54207715   =   yrday
fracday
Element set:     902
Inclination:       51
6411  deg
RA of node:       325
6434  deg
Eccentricity:     
0004107     
Arg of perigee:   346
3692  deg
Mean anomaly:      13
7359  deg
Mean motion:   15
72614718  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1219
Checksum:              280


Coasting Arc #4 (Orbit 1234)
---------------------------------------

Vector Time (GMT): 2008/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5821247
02                 A    =         6733613
64  meter
 Y    =       -2412546
19  meter          E    =           
0014880
 Z    =        2349196
38                 I    =           51
44231
 XDOT =        100
666222                 Wp   =           57
62660
 YDOT =       5505
499130  meter/sec      RA   =          320
20207  deg
 ZDOT =       5387
589367                 TA   =          328
90642
                                          MA   =          328
99439
                                          Ha   =            192
423  n
mi
                                          Hp   =            186
005

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19098579
46                 X    =         5836379
61
 Y    =       -7915177
80  feet           Y    =        -2347365
34  meter
 Z    =        7707337
21                 Z    =         2377513
13
 XDOT =        330
269756                 XDOT =          12
922792
 YDOT =      18062
661189  feet/sec       YDOT =        5506
133545  meter/sec
 ZDOT =      17675
818133                 ZDOT =        5387
865991

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4729866
96                 X    =        -1441663
45
 Y    =       20083146
13  feet           Y    =         6121342
94  meter
 Z    =        7816931
87                 Z    =         2382600
84
 XDOT =     -13317
501615                 XDOT =       -4059
174492
 YDOT =     -10038
268854  feet/sec       YDOT =       -3059
664347  meter/sec
 ZDOT =      17677
269134                 ZDOT =        5388
031632


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   08320
55881113  
00020000  00000-0  20000-3 0  9037
2 25544  51
6410 320
4331 0004097 349
4748  10
6328 15
72632859 12353


Satellite: ISS
Catalog Number: 25544
Epoch time:      08320
55881113   =   yrday
fracday
Element set:     903
Inclination:       51
6410  deg
RA of node:       320
4331  deg
Eccentricity:     
0004097     
Arg of perigee:   349
4748  deg
Mean anomaly:      10
6328  deg
Mean motion:   15
72632859  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1235
Checksum:              272


Coasting Arc #5 (Orbit 1249)
---------------------------------------

Vector Time (GMT): 2008/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -985609
93                 A    =         6725768
47  meter
 Y    =       -4528106
90  meter          E    =           
0011370
 Z    =       -4884023
32                 I    =           51
39363
 XDOT =       6311
754176                 Wp   =           86
36186
 YDOT =      -3781
439415  meter/sec      RA   =          315
02214  deg
 ZDOT =       2237
330658                 TA   =          205
46674
                                          MA   =          205
52281
                                          Ha   =            192
631  n
mi
                                          Hp   =            185
901

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3233628
37                 X    =         -911176
54
 Y    =      -14855993
78  feet           Y    =        -4538711
78  meter
 Z    =      -16023698
56                 Z    =        -4888631
25
 XDOT =      20707
854908                 XDOT =        6342
701008
 YDOT =     -12406
297293  feet/sec       YDOT =       -3710
684976  meter/sec
 ZDOT =       7340
323680                 ZDOT =        2268
068393

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13989454
97                 X    =         4263985
87
 Y    =        5905017
70  feet           Y    =         1799849
40  meter
 Z    =      -16041874
42                 Z    =        -4889563
32
 XDOT =      -1186
547766                 XDOT =        -361
659759
 YDOT =      23028
921734  feet/sec       YDOT =        7019
215345  meter/sec
 ZDOT =       7459
215581                 ZDOT =        2273
568909


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   08321
51198773  
00020000  00000-0  20000-3 0  9048
2 25544  51
6408 315
5478 0004210 353
5005   6
6102 15
72611464 12507


Satellite: ISS
Catalog Number: 25544
Epoch time:      08321
51198773   =   yrday
fracday
Element set:     904
Inclination:       51
6408  deg
RA of node:       315
5478  deg
Eccentricity:     
0004210     
Arg of perigee:   353
5005  deg
Mean anomaly:       6
6102  deg
Mean motion:   15
72611464  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1250
Checksum:              257


Coasting Arc #6 (Orbit 1265)
---------------------------------------

Vector Time (GMT): 2008/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5085119
54                 A    =         6734893
24  meter
 Y    =        4127074
90  meter          E    =           
0005232
 Z    =       -1569164
37                 I    =           51
40452
 XDOT =      -2045
271532                 Wp   =          113
75398
 YDOT =      -4696
165455  meter/sec      RA   =          309
91222  deg
 ZDOT =      -5740
578625                 TA   =           83
59092
                                          MA   =           83
53135
                                          Ha   =            192
704  n
mi
                                          Hp   =            185
702

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16683463
07                 X    =        -5123268
42
 Y    =       13540271
98  feet           Y    =         4069997
02  meter
 Z    =       -5148177
08                 Z    =        -1593960
42
 XDOT =      -6710
208439                 XDOT =       -1964
719205
 YDOT =     -15407
366979  feet/sec       YDOT =       -4718
585874  meter/sec
 ZDOT =     -18833
919372                 ZDOT =       -5750
319501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1972671
17                 X    =         -601270
17
 Y    =      -21372634
60  feet           Y    =        -6514379
03  meter
 Z    =       -5244014
83                 Z    =        -1598375
72
 XDOT =      14915
403750                 XDOT =        4546
215063
 YDOT =       3240
217864  feet/sec       YDOT =         987
618405  meter/sec
 ZDOT =     -18872
011209                 ZDOT =       -5752
189017


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   08322
52869593  
00020000  00000-0  20000-3 0  9056
2 25544  51
6403 310
3365 0004250 358
8035   1
3117 15
72655735 12669


Satellite: ISS
Catalog Number: 25544
Epoch time:      08322
52869593   =   yrday
fracday
Element set:     905
Inclination:       51
6403  deg
RA of node:       310
3365  deg
Eccentricity:     
0004250     
Arg of perigee:   358
8035  deg
Mean anomaly:       1
3117  deg
Mean motion:   15
72655735  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1266
Checksum:              277


Coasting Arc #7 (Orbit 1281)
---------------------------------------

Vector Time (GMT): 2008/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2515818
12                 A    =         6724487
44  meter
 Y    =        3557338
05  meter          E    =           
0007730
 Z    =        5120238
13                 I    =           51
35119
 XDOT =      -5152
763946                 Wp   =           27
59286
 YDOT =       5566
415222  meter/sec      RA   =          304
74204  deg
 ZDOT =      -1327
969403                 TA   =           75
20654
                                          MA   =           75
12092
                                          Ha   =            192
670  n
mi
                                          Hp   =            185
642

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8253996
46                 X    =         2450978
97
 Y    =       11671056
59  feet           Y    =         3585108
44  meter
 Z    =       16798681
53                 Z    =         5132302
88
 XDOT =     -16905
393522                 XDOT =       -5208
174441
 YDOT =      18262
517134  feet/sec       YDOT =        5508
484327  meter/sec
 ZDOT =      -4356
854996                 ZDOT =       -1353
135933

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14229837
84                 X    =        -4337254
57
 Y    =         521074
08  feet           Y    =          158823
38  meter
 Z    =       16845709
16                 Z    =         5134572
15
 XDOT =      -6146
123752                 XDOT =       -1873
338520
 YDOT =     -23049
941224  feet/sec       YDOT =       -7025
622085  meter/sec
 ZDOT =      -4454
025866                 ZDOT =       -1357
587084


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   08323
54538980  
00020000  00000-0  20000-3 0  9063
2 25544  51
6398 305
1256 0004303    
6412 359
4755 15
72676208 12824


Satellite: ISS
Catalog Number: 25544
Epoch time:      08323
54538980   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       305
1256  deg
Eccentricity:     
0004303     
Arg of perigee:      
6412  deg
Mean anomaly:     359
4755  deg
Mean motion:   15
72676208  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1282
Checksum:              289


Coasting Arc #8 (Orbit 1297)
---------------------------------------

Vector Time (GMT): 2008/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3808115
79                 A    =         6735508
46  meter
 Y    =       -5494166
66  meter          E    =           
0016532
 Z    =         745207
98                 I    =           51
37314
 XDOT =       3594
360963                 Wp   =           42
30674
 YDOT =       3307
972567  meter/sec      RA   =          299
61613  deg
 ZDOT =       5956
436316                 TA   =          325
84618
                                          MA   =          325
95243
                                          Ha   =            192
656  n
mi
                                          Hp   =            185
407

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12493818
22                 X    =         3865649
31
 Y    =      -18025481
16  feet           Y    =        -5451260
46  meter
 Z    =        2444908
07                 Z    =          763847
44
 XDOT =      11792
522846                 XDOT =        3528
167942
 YDOT =      10852
928371  feet/sec       YDOT =        3347
796350  meter/sec
 ZDOT =      19542
113898                 ZDOT =        5973
737307

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8719584
47                 X    =         2657729
35
 Y    =       20115310
94  feet           Y    =         6131146
77  meter
 Z    =        2516774
30                 Z    =          767112
81
 XDOT =     -13917
021280                 XDOT =       -4241
908086
 YDOT =       3553
570994  feet/sec       YDOT =        1083
128439  meter/sec
 ZDOT =      19609
430180                 ZDOT =        5976
954319


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   08324
56206840  
00020000  00000-0  20000-3 0  9074
2 25544  51
6397 299
9152 0004120   5
7535 354
3674 15
72744656 12981


Satellite: ISS
Catalog Number: 25544
Epoch time:      08324
56206840   =   yrday
fracday
Element set:     907
Inclination:       51
6397  deg
RA of node:       299
9152  deg
Eccentricity:     
0004120     
Arg of perigee:     5
7535  deg
Mean anomaly:     354
3674  deg
Mean motion:   15
72744656  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1298
Checksum:              307


Coasting Arc #9 (Orbit 1312)
---------------------------------------

Vector Time (GMT): 2008/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3637551
58                 A    =         6723856
96  meter
 Y    =       -2145338
83  meter          E    =           
0015977
 Z    =       -5245431
80                 I    =           51
32010
 XDOT =       3467
940478                 Wp   =           77
24613
 YDOT =      -6849
302589  meter/sec      RA   =          294
45806  deg
 ZDOT =        400
895639                 TA   =          196
55799
                                          MA   =          196
61023
                                          Ha   =            192
854  n
mi
                                          Hp   =            185
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11934224
34                 X    =        -3587810
01
 Y    =       -7038513
21  feet           Y    =        -2185737
70  meter
 Z    =      -17209421
90                 Z    =        -5262982
51
 XDOT =      11377
757473                 XDOT =        3542
325245
 YDOT =     -22471
465186  feet/sec       YDOT =       -6810
106182  meter/sec
 ZDOT =       1315
274406                 ZDOT =         417
923523

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12115491
18                 X    =         3692801
71
 Y    =       -6544395
93  feet           Y    =        -1994731
88  meter
 Z    =      -17277625
31                 Z    =        -5266220
19
 XDOT =      12972
236906                 XDOT =        3953
937809
 YDOT =      20408
670024  feet/sec       YDOT =        6220
562623  meter/sec
 ZDOT =       1380
787117                 ZDOT =         420
863913


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   08325
51519536  
00020000  00000-0  20000-3 0  9080
2 25544  51
6397 295
0293 0004378   8
8175 351
3063 15
72704910 13139


Satellite: ISS
Catalog Number: 25544
Epoch time:      08325
51519536   =   yrday
fracday
Element set:     908
Inclination:       51
6397  deg
RA of node:       295
0293  deg
Eccentricity:     
0004378     
Arg of perigee:     8
8175  deg
Mean anomaly:     351
3063  deg
Mean motion:   15
72704910  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1313
Checksum:              291


Coasting Arc #10 (Orbit 1328)
---------------------------------------

Vector Time (GMT): 2008/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2202922
95                 A    =         6735738
30  meter
 Y    =        6362206
92  meter          E    =           
0010555
 Z    =          31591
33                 I    =           51
34984
 XDOT =      -4553
739696                 Wp   =          113
38929
 YDOT =      -1539
029147  meter/sec      RA   =          289
31348  deg
 ZDOT =      -6010
177634                 TA   =           66
26647
                                          MA   =           66
15578
                                          Ha   =            192
893  n
mi
                                          Hp   =            185
202

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7227437
50                 X    =        -2274055
93
 Y    =       20873382
27  feet           Y    =         6337174
83  meter
 Z    =         103646
10                 Z    =           20716
77
 XDOT =     -14940
090867                 XDOT =       -4506
994724
 YDOT =      -5049
308225  feet/sec       YDOT =       -1589
690140  meter/sec
 ZDOT =     -19718
430559                 ZDOT =       -6032
186581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14492918
65                 X    =        -4417441
60
 Y    =      -16670217
54  feet           Y    =        -5081082
31  meter
 Z    =          61959
55                 Z    =           18885
27
 XDOT =      10552
086949                 XDOT =        3216
276102
 YDOT =      -9279
799163  feet/sec       YDOT =       -2828
482785  meter/sec
 ZDOT =     -19803
875653                 ZDOT =       -6036
221299


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   08326
53184812  
00020000  00000-0  20000-3 0  9099
2 25544  51
6400 289
8178 0004492  11
8279 348
2989 15
72749047 13292


Satellite: ISS
Catalog Number: 25544
Epoch time:      08326
53184812   =   yrday
fracday
Element set:     909
Inclination:       51
6400  deg
RA of node:       289
8178  deg
Eccentricity:     
0004492     
Arg of perigee:    11
8279  deg
Mean anomaly:     348
2989  deg
Mean motion:   15
72749047  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1329
Checksum:              323


Coasting Arc #11 (Orbit 1344)
---------------------------------------

Vector Time (GMT): 2008/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4194363
86                 A    =         6723684
04  meter
 Y    =         496761
58  meter          E    =           
0004956
 Z    =        5228113
44                 I    =           51
30104
 XDOT =      -1499
177724                 Wp   =           47
30992
 YDOT =       7539
385979  meter/sec      RA   =          284
16992  deg
 ZDOT =        489
397152                 TA   =           38
03786
                                          MA   =           38
00288
                                          Ha   =            192
788  n
mi
                                          Hp   =            185
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13761036
28                 X    =         4163099
48
 Y    =        1629795
21  feet           Y    =          543490
40  meter
 Z    =       17152603
15                 Z    =         5248414
17
 XDOT =      -4918
562086                 XDOT =       -1585
750397
 YDOT =      24735
518304  feet/sec       YDOT =        7522
137237  meter/sec
 ZDOT =       1605
633702                 ZDOT =         481
903958

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8031914
20                 X    =        -2448127
45
 Y    =       11171532
58  feet           Y    =         3405083
13  meter
 Z    =       17231348
20                 Z    =         5252114
93
 XDOT =     -18455
737628                 XDOT =       -5625
308829
 YDOT =     -15686
405058  feet/sec       YDOT =       -4781
216262  meter/sec
 ZDOT =       1577
148766                 ZDOT =         480
714944


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   08327
54848702  
00020000  00000-0  20000-3 0  9108
2 25544  51
6401 284
6069 0004467  14
7704 345
3588 15
72768189 13451


Satellite: ISS
Catalog Number: 25544
Epoch time:      08327
54848702   =   yrday
fracday
Element set:     910
Inclination:       51
6401  deg
RA of node:       284
6069  deg
Eccentricity:     
0004467     
Arg of perigee:    14
7704  deg
Mean anomaly:     345
3588  deg
Mean motion:   15
72768189  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1345
Checksum:              311


Coasting Arc #12 (Orbit 1359)
---------------------------------------

Vector Time (GMT): 2008/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         393658
66                 A    =         6735343
00  meter
 Y    =       -6666439
98  meter          E    =           
0014609
 Z    =        -818595
54                 I    =           51
33437
 XDOT =       4881
592683                 Wp   =           33
14936
 YDOT =       -433
601852  meter/sec      RA   =          279
00831  deg
 ZDOT =       5940
624098                 TA   =          317
88597
                                          MA   =          317
99815
                                          Ha   =            192
942  n
mi
                                          Hp   =            184
951

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1291531
05                 X    =          472151
31
 Y    =      -21871522
24  feet           Y    =        -6661598
95  meter
 Z    =       -2685680
92                 Z    =         -816492
74
 XDOT =      16015
724027                 XDOT =        4857
219274
 YDOT =      -1422
578253  feet/sec       YDOT =        -379
149603  meter/sec
 ZDOT =      19490
236541                 ZDOT =        5964
280247

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18712642
85                 X    =         5703613
54
 Y    =       11397787
86  feet           Y    =         3474045
74  meter
 Z    =       -2678030
81                 Z    =         -816263
79
 XDOT =      -5360
125658                 XDOT =       -1633
766300
 YDOT =      13353
232141  feet/sec       YDOT =        4070
065157  meter/sec
 ZDOT =      19581
921784                 ZDOT =        5968
569760


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   08328
50157299  
00020000  00000-0  20000-3 0  9110
2 25544  51
6399 279
7210 0004454  19
2038 340
9292 15
72785983 13607


Satellite: ISS
Catalog Number: 25544
Epoch time:      08328
50157299   =   yrday
fracday
Element set:     911
Inclination:       51
6399  deg
RA of node:       279
7210  deg
Eccentricity:     
0004454     
Arg of perigee:    19
2038  deg
Mean anomaly:     340
9292  deg
Mean motion:   15
72785983  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1360
Checksum:              309

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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