Date: August 21st 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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


There are no maneuvers



Coasting Arc #1 (Orbit 3833)
---------------------------------------

Vector Time (GMT): 2008/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4430621
09                 A    =         6740171
33  meter
 Y    =        4938900
24  meter          E    =           
0017768
 Z    =       -1137145
27                 I    =           51
92812
 XDOT =      -2914
676197                 Wp   =           32
88686
 YDOT =       3964
978016  meter/sec      RA   =           55
82029  deg
 ZDOT =       5921
986048                 TA   =          314
72243
                                          MA   =          314
86696
                                          Ha   =            197
171  n
mi
                                          Hp   =            186
532

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14536158
42                 X    =         4380588
19
 Y    =       16203740
94  feet           Y    =         4988166
23  meter
 Z    =       -3730791
56                 Z    =        -1115743
22
 XDOT =      -9562
585947                 XDOT =       -2987
564127
 YDOT =      13008
458059  feet/sec       YDOT =        3931
976988  meter/sec
 ZDOT =      19429
088083                 ZDOT =        5907
649643

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3184317
79                 X    =         -970580
06
 Y    =      -21548431
39  feet           Y    =        -6567961
89  meter
 Z    =       -3647622
91                 Z    =        -1111795
46
 XDOT =      13678
098865                 XDOT =        4169
084534
 YDOT =      -5268
184068  feet/sec       YDOT =       -1605
742504  meter/sec
 ZDOT =      19374
027661                 ZDOT =        5905
203631


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   08231
50214911  
00020000  00000-0  20000-3 0  9006
2 25544  51
6385  56
4260 0008331  27
6831 332
4772 15
71006828 38349


Satellite: ISS
Catalog Number: 25544
Epoch time:      08231
50214911   =   yrday
fracday
Element set:     900
Inclination:       51
6385  deg
RA of node:        56
4260  deg
Eccentricity:     
0008331     
Arg of perigee:    27
6831  deg
Mean anomaly:     332
4772  deg
Mean motion:   15
71006828  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3834
Checksum:              267


Coasting Arc #2 (Orbit 3849)
---------------------------------------

Vector Time (GMT): 2008/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1318521
02                 A    =         6730335
34  meter
 Y    =       -4451712
76  meter          E    =           
0019406
 Z    =       -4890202
62                 I    =           51
87786
 XDOT =       5902
297093                 Wp   =           56
51433
 YDOT =       4322
793438  meter/sec      RA   =           50
75470  deg
 ZDOT =      -2339
957290                 TA   =          190
68226
                                          MA   =          190
72354
                                          Ha   =            197
200  n
mi
                                          Hp   =            186
331

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4325856
36                 X    =         1391958
30
 Y    =      -14605356
83  feet           Y    =        -4436557
82  meter
 Z    =      -16043971
85                 Z    =        -4883618
81
 XDOT =      19364
491775                 XDOT =        5864
887245
 YDOT =      14182
393170  feet/sec       YDOT =        4388
587093  meter/sec
 ZDOT =      -7677
025230                 ZDOT =       -2311
375160

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11580943
25                 X    =        -3529871
50
 Y    =        9935514
88  feet           Y    =         3028344
94  meter
 Z    =      -16018920
43                 Z    =        -4882566
95
 XDOT =      -8006
520256                 XDOT =       -2440
387374
 YDOT =     -21551
549504  feet/sec       YDOT =       -6568
912289  meter/sec
 ZDOT =      -7566
162666                 ZDOT =       -2306
166381


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   08232
51991005  
00020000  00000-0  20000-3 0  9015
2 25544  51
6385  51
2220 0008415  32
6115 327
5565 15
71037413 38509


Satellite: ISS
Catalog Number: 25544
Epoch time:      08232
51991005   =   yrday
fracday
Element set:     901
Inclination:       51
6385  deg
RA of node:        51
2220  deg
Eccentricity:     
0008415     
Arg of perigee:    32
6115  deg
Mean anomaly:     327
5565  deg
Mean motion:   15
71037413  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3850
Checksum:              256


Coasting Arc #3 (Orbit 3865)
---------------------------------------

Vector Time (GMT): 2008/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5567478
99                 A    =         6737030
57  meter
 Y    =       -2445547
66  meter          E    =           
0018639
 Z    =        2890943
88                 I    =           51
88126
 XDOT =       -104
142728                 Wp   =           74
90411
 YDOT =      -5791
346299  meter/sec      RA   =           45
61590  deg
 ZDOT =      -5067
897443                 TA   =           72
01985
                                          MA   =           71
81678
                                          Ha   =            197
224  n
mi
                                          Hp   =            186
265

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18266007
19                 X    =        -5553762
34
 Y    =       -8023450
32  feet           Y    =        -2507729
65  meter
 Z    =        9484724
03                 Z    =         2863930
53
 XDOT =       -341
675616                 XDOT =         -14
756374
 YDOT =     -19000
479985  feet/sec       YDOT =       -5792
011217  meter/sec
 ZDOT =     -16626
960114                 ZDOT =       -5068
186112

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11411226
60                 X    =         3478141
87
 Y    =       16424994
51  feet           Y    =         5006338
33  meter
 Z    =        9380097
37                 Z    =         2859053
68
 XDOT =      -8536
588669                 XDOT =       -2601
952226
 YDOT =      15487
313862  feet/sec       YDOT =        4720
533265  meter/sec
 ZDOT =     -16628
587419                 ZDOT =       -5068
393445


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   08233
53765933  
00020000  00000-0  20000-3 0  9028
2 25544  51
6388  46
0171 0008324  34
8676 325
3030 15
71057178 38664


Satellite: ISS
Catalog Number: 25544
Epoch time:      08233
53765933   =   yrday
fracday
Element set:     902
Inclination:       51
6388  deg
RA of node:        46
0171  deg
Eccentricity:     
0008324     
Arg of perigee:    34
8676  deg
Mean anomaly:     325
3030  deg
Mean motion:   15
71057178  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3866
Checksum:              294


Coasting Arc #4 (Orbit 3881)
---------------------------------------

Vector Time (GMT): 2008/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1581468
51                 A    =         6734136
32  meter
 Y    =        5303099
89  meter          E    =           
0017227
 Z    =        3819198
71                 I    =           51
85062
 XDOT =      -6369
968022                 Wp   =           73
85267
 YDOT =      -1123
728274  meter/sec      RA   =           40
56748  deg
 ZDOT =       4187
225975                 TA   =          332
39084
                                          MA   =          332
48222
                                          Ha   =            197
208  n
mi
                                          Hp   =            186
031

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5188544
99                 X    =         1503497
86
 Y    =       17398621
69  feet           Y    =         5320348
86  meter
 Z    =       12530179
51                 Z    =         3826692
06
 XDOT =     -20898
845217                 XDOT =       -6377
269692
 YDOT =      -3686
772552  feet/sec       YDOT =       -1195
001712  meter/sec
 ZDOT =      13737
618027                 ZDOT =        4156
262910

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4444225
02                 X    =         1354599
78
 Y    =      -17582480
90  feet           Y    =        -5359140
18  meter
 Z    =       12559604
44                 Z    =         3828167
43
 XDOT =      14903
482013                 XDOT =        4542
581318
 YDOT =      13519
919275  feet/sec       YDOT =        4120
871395  meter/sec
 ZDOT =      13617
845699                 ZDOT =        4150
719369


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   08234
55540000  
00020000  00000-0  20000-3 0  9038
2 25544  51
6388  40
8128 0008276  39
9556 320
2213 15
71080775 38821


Satellite: ISS
Catalog Number: 25544
Epoch time:      08234
55540000   =   yrday
fracday
Element set:     903
Inclination:       51
6388  deg
RA of node:        40
8128  deg
Eccentricity:     
0008276     
Arg of perigee:    39
9556  deg
Mean anomaly:     320
2213  deg
Mean motion:   15
71080775  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3882
Checksum:              281


Coasting Arc #5 (Orbit 3896)
---------------------------------------

Vector Time (GMT): 2008/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5170377
53                 A    =         6732633
75  meter
 Y    =        -468534
62  meter          E    =           
0014158
 Z    =       -4296625
65                 I    =           51
82343
 XDOT =       3463
989076                 Wp   =           77
28736
 YDOT =       5878
915736  meter/sec      RA   =           35
41815  deg
 ZDOT =       3540
138287                 TA   =          228
51306
                                          MA   =          228
63468
                                          Ha   =            197
379  n
mi
                                          Hp   =            185
964

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16963180
88                 X    =         5196104
78
 Y    =       -1537187
08  feet           Y    =         -410572
57  meter
 Z    =      -14096540
83                 Z    =        -4271445
39
 XDOT =      11364
793558                 XDOT =        3380
795239
 YDOT =      19287
781286  feet/sec       YDOT =        5917
186843  meter/sec
 ZDOT =      11614
626926                 ZDOT =        3556
764409

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15580103
16                 X    =        -4748815
44
 Y    =       -7078563
47  feet           Y    =        -2157546
15  meter
 Z    =      -13999258
47                 Z    =        -4266973
98
 XDOT =       -817
605696                 XDOT =        -249
206216
 YDOT =     -21215
111827  feet/sec       YDOT =       -6466
366085  meter/sec
 ZDOT =      11679
392821                 ZDOT =        3559
878932


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   08235
50952342  
00020000  00000-0  20000-3 0  9041
2 25544  51
6400  35
9343 0008403  44
4519 315
7315 15
71075336 38977


Satellite: ISS
Catalog Number: 25544
Epoch time:      08235
50952342   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:        35
9343  deg
Eccentricity:     
0008403     
Arg of perigee:    44
4519  deg
Mean anomaly:     315
7315  deg
Mean motion:   15
71075336  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3897
Checksum:              280


Coasting Arc #6 (Orbit 3912)
---------------------------------------

Vector Time (GMT): 2008/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4324392
78                 A    =         6738048
98  meter
 Y    =       -4631882
14  meter          E    =           
0010489
 Z    =       -2302573
02                 I    =           51
81781
 XDOT =       5040
644629                 Wp   =           80
26477
 YDOT =      -2009
166176  meter/sec      RA   =           30
36213  deg
 ZDOT =      -5444
255925                 TA   =          125
48716
                                          MA   =          125
38924
                                          Ha   =            197
352  n
mi
                                          Hp   =            185
669

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14187640
36                 X    =        -4261091
42
 Y    =      -15196463
72  feet           Y    =        -4679885
96  meter
 Z    =       -7554373
43                 Z    =        -2323427
41
 XDOT =      16537
547997                 XDOT =        5089
184092
 YDOT =      -6591
752545  feet/sec       YDOT =       -1952
527163  meter/sec
 ZDOT =     -17861
732036                 ZDOT =       -5419
650591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5143185
64                 X    =         1567642
98
 Y    =       20113154
35  feet           Y    =         6130489
45  meter
 Z    =       -7635369
67                 Z    =        -2327260
68
 XDOT =     -16297
865004                 XDOT =       -4967
589253
 YDOT =      -2553
374003  feet/sec       YDOT =        -778
268396  meter/sec
 ZDOT =     -17766
800469                 ZDOT =       -5415
320783


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   08236
52724315  
00020000  00000-0  20000-3 0  9052
2 25544  51
6401  30
7301 0008539  47
4003 312
7877 15
71115408 39130


Satellite: ISS
Catalog Number: 25544
Epoch time:      08236
52724315   =   yrday
fracday
Element set:     905
Inclination:       51
6401  deg
RA of node:        30
7301  deg
Eccentricity:     
0008539     
Arg of perigee:    47
4003  deg
Mean anomaly:     312
7877  deg
Mean motion:   15
71115408  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3913
Checksum:              264


Coasting Arc #7 (Orbit 3928)
---------------------------------------

Vector Time (GMT): 2008/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3334517
37                 A    =         6729368
04  meter
 Y    =        2862081
38  meter          E    =           
0013566
 Z    =        5089167
56                 I    =           51
76194
 XDOT =      -6175
867313                 Wp   =           52
63535
 YDOT =      -4312
255461  meter/sec      RA   =           25
22550  deg
 ZDOT =      -1610
390009                 TA   =           52
86369
                                          MA   =           52
73984
                                          Ha   =            197
591  n
mi
                                          Hp   =            185
655

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10940017
61                 X    =        -3390996
02
 Y    =        9390030
77  feet           Y    =         2824476
78  meter
 Z    =       16696743
95                 Z    =         5072831
48
 XDOT =     -20262
031868                 XDOT =       -6119
365002
 YDOT =     -14147
819754  feet/sec       YDOT =       -4381
001541  meter/sec
 ZDOT =      -5283
431788                 ZDOT =       -1640
255373

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14130900
74                 X    =         4307098
54
 Y    =       -3204823
43  feet           Y    =         -976830
18  meter
 Z    =       16633841
20                 Z    =         5069994
80
 XDOT =      11134
561702                 XDOT =        3393
814407
 YDOT =      20883
854327  feet/sec       YDOT =        6365
398799  meter/sec
 ZDOT =      -5399
228272                 ZDOT =       -1645
684777


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   08237
54495477  
00020000  00000-0  20000-3 0  9060
2 25544  51
6399  25
5259 0008515  52
2588 307
9344 15
71067673 39298


Satellite: ISS
Catalog Number: 25544
Epoch time:      08237
54495477   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:        25
5259  deg
Eccentricity:     
0008515     
Arg of perigee:    52
2588  deg
Mean anomaly:     307
9344  deg
Mean motion:   15
71067673  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3929
Checksum:              330


Coasting Arc #8 (Orbit 3944)
---------------------------------------

Vector Time (GMT): 2008/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6168951
93                 A    =         6740241
77  meter
 Y    =        2650805
72  meter          E    =           
0021529
 Z    =         463034
80                 I    =           51
77366
 XDOT =      -2278
769554                 Wp   =           51
94980
 YDOT =       4219
852002  meter/sec      RA   =           20
13947  deg
 ZDOT =       6025
939380                 TA   =          313
07445
                                          MA   =          313
25446
                                          Ha   =            197
408  n
mi
                                          Hp   =            185
468

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20239343
59                 X    =         6136602
38
 Y    =        8696869
16  feet           Y    =         2719609
58  meter
 Z    =        1519143
04                 Z    =          492924
99
 XDOT =      -7476
278065                 XDOT =       -2355
059990
 YDOT =      13844
658800  feet/sec       YDOT =        4193
942494  meter/sec
 ZDOT =      19770
142324                 ZDOT =        6014
684183

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14185849
80                 X    =        -4323847
02
 Y    =      -16842301
67  feet           Y    =        -5133533
55  meter
 Z    =        1634899
96                 Z    =          498317
51
 XDOT =      11761
771126                 XDOT =        3584
987839
 YDOT =      -7939
708599  feet/sec       YDOT =       -2420
023181  meter/sec
 ZDOT =      19726
987387                 ZDOT =        6012
785756


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   08238
56265202  
00020000  00000-0  20000-3 0  9075
2 25544  51
6413  20
3222 0008448  55
8284 304
3678 15
71137131 39451


Satellite: ISS
Catalog Number: 25544
Epoch time:      08238
56265202   =   yrday
fracday
Element set:     907
Inclination:       51
6413  deg
RA of node:        20
3222  deg
Eccentricity:     
0008448     
Arg of perigee:    55
8284  deg
Mean anomaly:     304
3678  deg
Mean motion:   15
71137131  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3945
Checksum:              278


Coasting Arc #9 (Orbit 3959)
---------------------------------------

Vector Time (GMT): 2008/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         516358
10                 A    =         6728304
75  meter
 Y    =       -4172085
11  meter          E    =           
0022816
 Z    =       -5272696
17                 I    =           51
70599
 XDOT =       7495
531259                 Wp   =           75
87090
 YDOT =       1588
522923  meter/sec      RA   =           15
03336  deg
 ZDOT =       -519
318957                 TA   =          189
16540
                                          MA   =          189
20712
                                          Ha   =            197
429  n
mi
                                          Hp   =            185
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1694088
26                 X    =          588586
14
 Y    =      -13687943
27  feet           Y    =        -4165906
71  meter
 Z    =      -17298871
94                 Z    =        -5270012
56
 XDOT =      24591
637990                 XDOT =        7479
733785
 YDOT =       5211
689380  feet/sec       YDOT =        1672
253972  meter/sec
 ZDOT =      -1703
802353                 ZDOT =        -482
944375

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7540564
42                 X    =        -2298364
03
 Y    =       11563582
03  feet           Y    =         3524579
80  meter
 Z    =      -17288844
82                 Z    =        -5269639
90
 XDOT =     -19078
730922                 XDOT =       -5815
197185
 YDOT =     -14795
674303  feet/sec       YDOT =       -4509
721528  meter/sec
 ZDOT =      -1563
062751                 ZDOT =        -476
421526


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   08239
51673533  
00020000  00000-0  20000-3 0  9082
2 25544  51
6415  15
4443 0008538  58
6841 301
5155 15
71156530 39603


Satellite: ISS
Catalog Number: 25544
Epoch time:      08239
51673533   =   yrday
fracday
Element set:     908
Inclination:       51
6415  deg
RA of node:        15
4443  deg
Eccentricity:     
0008538     
Arg of perigee:    58
6841  deg
Mean anomaly:     301
5155  deg
Mean motion:   15
71156530  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3960
Checksum:              287


Coasting Arc #10 (Orbit 3975)
---------------------------------------

Vector Time (GMT): 2008/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6597242
11                 A    =         6739547
58  meter
 Y    =         -70844
33  meter          E    =           
0019737
 Z    =        1349493
41                 I    =           51
71504
 XDOT =      -1156
062307                 Wp   =           98
70255
 YDOT =      -4879
999485  meter/sec      RA   =            9
90635  deg
 ZDOT =      -5838
337802                 TA   =           66
50621
                                          MA   =           66
29890
                                          Ha   =            197
454  n
mi
                                          Hp   =            185
369

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21644495
11                 X    =        -6602515
08
 Y    =        -232428
89  feet           Y    =         -144648
03  meter
 Z    =        4427471
83                 Z    =         1317431
74
 XDOT =      -3792
855339                 XDOT =       -1073
046340
 YDOT =     -16010
496999  feet/sec       YDOT =       -4892
462820  meter/sec
 ZDOT =     -19154
651580                 ZDOT =       -5843
752427

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19596303
37                 X    =         5972953
27
 Y    =        9252311
19  feet           Y    =         2820104
45  meter
 Z    =        4303525
39                 Z    =         1311714
54
 XDOT =      -2658
078393                 XDOT =        -810
182294
 YDOT =      14658
168115  feet/sec       YDOT =        4467
809641  meter/sec
 ZDOT =     -19175
990396                 ZDOT =       -5844
841873


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   08240
53441332  
00020000  00000-0  20000-3 0  9097
2 25544  51
6414  10
2387 0008460  62
2461 297
9557 15
71154360 39765


Satellite: ISS
Catalog Number: 25544
Epoch time:      08240
53441332   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:        10
2387  deg
Eccentricity:     
0008460     
Arg of perigee:    62
2461  deg
Mean anomaly:     297
9557  deg
Mean motion:   15
71154360  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3976
Checksum:              284


Coasting Arc #11 (Orbit 3991)
---------------------------------------

Vector Time (GMT): 2008/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2516763
80                 A    =         6730152
38  meter
 Y    =        4004113
42  meter          E    =           
0013880
 Z    =        4776407
19                 I    =           51
65649
 XDOT =      -7128
576748                 Wp   =           90
01803
 YDOT =       1425
712260  meter/sec      RA   =            4
82822  deg
 ZDOT =       2554
602651                 TA   =          334
94297
                                          MA   =          335
01027
                                          Ha   =            197
314  n
mi
                                          Hp   =            185
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8257099
08                 X    =         2448599
63
 Y    =       13136855
04  feet           Y    =         4031876
12  meter
 Z    =       15670627
25                 Z    =         4788467
88
 XDOT =     -23387
718990                 XDOT =       -7156
399042
 YDOT =       4677
533660  feet/sec       YDOT =        1345
840811  meter/sec
 ZDOT =       8381
242293                 ZDOT =        2519
905132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2205056
73                 X    =         -672101
29
 Y    =      -15310791
19  feet           Y    =        -4666729
15  meter
 Z    =       15717588
93                 Z    =         4790721
11
 XDOT =      22224
813303                 XDOT =        6774
123095
 YDOT =       5286
918594  feet/sec       YDOT =        1611
452787  meter/sec
 ZDOT =       8247
230161                 ZDOT =        2513
755753


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   08241
55207910  
00020000  00000-0  20000-3 0  9104
2 25544  51
6427   5
0347 0008402  65
5185 294
6853 15
71209258 39920


Satellite: ISS
Catalog Number: 25544
Epoch time:      08241
55207910   =   yrday
fracday
Element set:     910
Inclination:       51
6427  deg
RA of node:         5
0347  deg
Eccentricity:     
0008402     
Arg of perigee:    65
5185  deg
Mean anomaly:     294
6853  deg
Mean motion:   15
71209258  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3992
Checksum:              286


Coasting Arc #12 (Orbit 4006)
---------------------------------------

Vector Time (GMT): 2008/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5499688
74                 A    =         6736324
05  meter
 Y    =       -2435204
76  meter          E    =           
0013044
 Z    =       -3037899
93                 I    =           51
64785
 XDOT =       4435
212371                 Wp   =           68
44678
 YDOT =       3882
404634  meter/sec      RA   =          359
67200  deg
 ZDOT =       4938
797476                 TA   =          256
46126
                                          MA   =          256
60661
                                          Ha   =            197
522  n
mi
                                          Hp   =            185
246

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18043598
22                 X    =         5541268
14
 Y    =       -7989516
94  feet           Y    =        -2373471
64  meter
 Z    =       -9966863
28                 Z    =        -3011081
91
 XDOT =      14551
221689                 XDOT =        4367
477726
 YDOT =      12737
548013  feet/sec       YDOT =        3931
623087  meter/sec
 ZDOT =      16203
403792                 ZDOT =        4960
178751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19781398
41                 X    =        -6029370
24
 Y    =         389624
05  feet           Y    =          118757
41  meter
 Z    =       -9863399
58                 Z    =        -3006364
19
 XDOT =      -8397
852675                 XDOT =       -2559
665495
 YDOT =     -15886
252335  feet/sec       YDOT =       -4842
129712  meter/sec
 ZDOT =      16286
389935                 ZDOT =        4964
091652


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   08242
50613323  
00020000  00000-0  20000-3 0  9110
2 25544  51
6431    
1566 0008520  67
9804 292
2262 15
71169131 40070


Satellite: ISS
Catalog Number: 25544
Epoch time:      08242
50613323   =   yrday
fracday
Element set:     911
Inclination:       51
6431  deg
RA of node:          
1566  deg
Eccentricity:     
0008520     
Arg of perigee:    67
9804  deg
Mean anomaly:     292
2262  deg
Mean motion:   15
71169131  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4007
Checksum:              252

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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