Date: May 28th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 2510)
---------------------------------------

Vector Time (GMT): 2008/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -349081
28                 A    =         6716966
92  meter
 Y    =       -5133013
80  meter          E    =           
0004289
 Z    =        4316856
63                 I    =           51
88658
 XDOT =       5994
074916                 Wp   =           54
36039
 YDOT =      -3350
068737  meter/sec      RA   =          127
27410  deg
 ZDOT =      -3493
876828                 TA   =           70
85879
                                          MA   =           70
81236
                                          Ha   =            184
306  n
mi
                                          Hp   =            182
033

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1145279
80                 X    =         -312627
71
 Y    =      -16840596
45  feet           Y    =        -5136714
15  meter
 Z    =       14162915
45                 Z    =         4315248
69
 XDOT =      19665
600118                 XDOT =        6048
063061
 YDOT =     -10991
039163  feet/sec       YDOT =       -3282
737256  meter/sec
 ZDOT =     -11462
850486                 ZDOT =       -3464
626856

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15638079
21                 X    =        -4766486
54
 Y    =       -6368461
49  feet           Y    =        -1941107
06  meter
 Z    =       14156224
97                 Z    =         4314817
37
 XDOT =      -1567
218172                 XDOT =        -477
688099
 YDOT =     -21418
059055  feet/sec       YDOT =       -6528
224400  meter/sec
 ZDOT =     -11350
674925                 ZDOT =       -3459
685717


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   08147
54139827  
00020000  00000-0  20000-3 0  9008
2 25544  51
6344 127
9894 0005720 264
0314  96
0198 15
76494201 25110


Satellite: ISS
Catalog Number: 25544
Epoch time:      08147
54139827   =   yrday
fracday
Element set:     900
Inclination:       51
6344  deg
RA of node:       127
9894  deg
Eccentricity:     
0005720     
Arg of perigee:   264
0314  deg
Mean anomaly:      96
0198  deg
Mean motion:   15
76494201  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2511
Checksum:              290


Coasting Arc #2 (Orbit 2526)
---------------------------------------

Vector Time (GMT): 2008/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5010029
38                 A    =         6719085
13  meter
 Y    =        2520979
94  meter          E    =           
0006198
 Z    =        3696187
85                 I    =           51
91113
 XDOT =         -3
177535                 Wp   =          103
68919
 YDOT =      -6370
559180  meter/sec      RA   =          122
18878  deg
 ZDOT =       4333
262994                 TA   =          300
67043
                                          MA   =          300
73150
                                          Ha   =            184
194  n
mi
                                          Hp   =            181
997

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16437104
26                 X    =        -5055802
48
 Y    =        8270931
57  feet           Y    =         2464698
59  meter
 Z    =       12126600
57                 Z    =         3671738
16
 XDOT =        -10
424985                 XDOT =          47
009031
 YDOT =     -20900
784711  feet/sec       YDOT =       -6370
314583  meter/sec
 ZDOT =      14216
742105                 ZDOT =        4333
368758

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         412138
15                 X    =          125619
71
 Y    =       18457600
85  feet           Y    =         5625876
74  meter
 Z    =       12032799
34                 Z    =         3667597
24
 XDOT =     -17583
525929                 XDOT =       -5359
458703
 YDOT =      -8891
436052  feet/sec       YDOT =       -2710
109709  meter/sec
 ZDOT =      14216
523022                 ZDOT =        4333
196217


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   08148
55561753  
00020000  00000-0  20000-3 0  9018
2 25544  51
6348 122
7614 0005811 266
9112  93
1387 15
76543799 25277


Satellite: ISS
Catalog Number: 25544
Epoch time:      08148
55561753   =   yrday
fracday
Element set:     901
Inclination:       51
6348  deg
RA of node:       122
7614  deg
Eccentricity:     
0005811     
Arg of perigee:   266
9112  deg
Mean anomaly:      93
1387  deg
Mean motion:   15
76543799  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2527
Checksum:              307


Coasting Arc #3 (Orbit 2541)
---------------------------------------

Vector Time (GMT): 2008/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -269479
41                 A    =         6720750
26  meter
 Y    =        5937264
81  meter          E    =           
0001697
 Z    =       -3135217
18                 I    =           51
93092
 XDOT =      -5481
080157                 Wp   =          315
32968
 YDOT =       2330
562033  meter/sec      RA   =          117
00253  deg
 ZDOT =       4884
169119                 TA   =            8
32485
                                          MA   =            8
32203
                                          Ha   =            184
215  n
mi
                                          Hp   =            181
975

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -884118
80                 X    =         -320620
40
 Y    =       19479215
25  feet           Y    =         5933965
70  meter
 Z    =      -10286145
60                 Z    =        -3136649
96
 XDOT =     -17982
546448                 XDOT =       -5530
460052
 YDOT =       7646
200895  feet/sec       YDOT =        2268
992880  meter/sec
 ZDOT =      16024
176901                 ZDOT =        4857
422155

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17405953
02                 X    =         5305334
48
 Y    =        8783667
73  feet           Y    =         2677261
92  meter
 Z    =      -10291076
96                 Z    =        -3136720
26
 XDOT =        154
594045                 XDOT =          47
120265
 YDOT =      18349
094153  feet/sec       YDOT =        5592
803898  meter/sec
 ZDOT =      15921
513351                 ZDOT =        4852
877269


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   08149
50643881  
00020000  00000-0  20000-3 0  9028
2 25544  51
6346 117
8594 0005644 272
4513  87
6005 15
76509513 25426


Satellite: ISS
Catalog Number: 25544
Epoch time:      08149
50643881   =   yrday
fracday
Element set:     902
Inclination:       51
6346  deg
RA of node:       117
8594  deg
Eccentricity:     
0005644     
Arg of perigee:   272
4513  deg
Mean anomaly:      87
6005  deg
Mean motion:   15
76509513  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2542
Checksum:              296


Coasting Arc #4 (Orbit 2557)
---------------------------------------

Vector Time (GMT): 2008/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4563784
80                 A    =         6715366
50  meter
 Y    =       -1450384
66  meter          E    =           
0006442
 Z    =       -4713882
06                 I    =           51
92567
 XDOT =       -562
848006                 Wp   =           48
60323
 YDOT =       7169
898454  meter/sec      RA   =          111
91358  deg
 ZDOT =      -2749
225954                 TA   =          194
41384
                                          MA   =          194
43222
                                          Ha   =            184
196  n
mi
                                          Hp   =            182
056

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14973047
24                 X    =         4602563
46
 Y    =       -4758479
86  feet           Y    =        -1399132
55  meter
 Z    =      -15465492
33                 Z    =        -4691616
90
 XDOT =      -1846
614192                 XDOT =        -629
625726
 YDOT =      23523
288890  feet/sec       YDOT =        7163
231248  meter/sec
 ZDOT =      -9019
770189                 ZDOT =       -2752
121834

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1604555
37                 X    =          489068
48
 Y    =      -15713000
41  feet           Y    =        -4789322
52  meter
 Z    =      -15379978
79                 Z    =        -4687817
53
 XDOT =      19736
554880                 XDOT =        6015
701927
 YDOT =      10859
942188  feet/sec       YDOT =        3310
110379  meter/sec
 ZDOT =      -9030
215941                 ZDOT =       -2752
409819


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   08150
52063421  
00020000  00000-0  20000-3 0  9039
2 25544  51
6351 112
6305 0005706 276
4036  83
6479 15
76544890 25583


Satellite: ISS
Catalog Number: 25544
Epoch time:      08150
52063421   =   yrday
fracday
Element set:     903
Inclination:       51
6351  deg
RA of node:       112
6305  deg
Eccentricity:     
0005706     
Arg of perigee:   276
4036  deg
Mean anomaly:      83
6479  deg
Mean motion:   15
76544890  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2558
Checksum:              284


Coasting Arc #5 (Orbit 2573)
---------------------------------------

Vector Time (GMT): 2008/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         652216
13                 A    =         6723774
58  meter
 Y    =       -6494615
44  meter          E    =           
0008721
 Z    =        1593414
85                 I    =           51
96427
 XDOT =       5003
952010                 Wp   =          127
68805
 YDOT =       -921
040745  meter/sec      RA   =          106
74403  deg
 ZDOT =      -5786
141121                 TA   =           34
78844
                                          MA   =           34
73145
                                          Ha   =            184
286  n
mi
                                          Hp   =            181
938

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2139816
70                 X    =          717050
83
 Y    =      -21307793
45  feet           Y    =        -6486959
64  meter
 Z    =        5227739
01                 Z    =         1596740
21
 XDOT =      16417
165388                 XDOT =        5041
987782
 YDOT =      -3021
787221  feet/sec       YDOT =        -864
870447  meter/sec
 ZDOT =     -18983
402627                 ZDOT =       -5761
739248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18899619
87                 X    =        -5760604
14
 Y    =      -10063688
70  feet           Y    =        -3067412
32  meter
 Z    =        5239911
36                 Z    =         1597124
98
 XDOT =       2763
499763                 XDOT =         842
314728
 YDOT =     -15052
737274  feet/sec       YDOT =       -4588
074321  meter/sec
 ZDOT =     -18889
613214                 ZDOT =       -5757
554107


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   08151
53481646  
00020000  00000-0  20000-3 0  9045
2 25544  51
6353 107
4020 0005766 280
9249  79
1266 15
76566433 25742


Satellite: ISS
Catalog Number: 25544
Epoch time:      08151
53481646   =   yrday
fracday
Element set:     904
Inclination:       51
6353  deg
RA of node:       107
4020  deg
Eccentricity:     
0005766     
Arg of perigee:   280
9249  deg
Mean anomaly:      79
1266  deg
Mean motion:   15
76566433  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2574
Checksum:              299


Coasting Arc #6 (Orbit 2589)
---------------------------------------

Vector Time (GMT): 2008/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4204878
84                 A    =         6712915
12  meter
 Y    =          96802
83  meter          E    =           
0002871
 Z    =        5234374
53                 I    =           51
93589
 XDOT =        884
820165                 Wp   =          265
64528
 YDOT =      -7604
997938  meter/sec      RA   =          101
63340  deg
 ZDOT =        851
622224                 TA   =          176
28407
                                          MA   =          176
28194
                                          Ha   =            184
470  n
mi
                                          Hp   =            181
914

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13795534
27                 X    =        -4231076
93
 Y    =         317594
59  feet           Y    =           49634
37  meter
 Z    =       17173144
78                 Z    =         5213883
20
 XDOT =       2902
953298                 XDOT =         965
657580
 YDOT =     -24950
780635  feet/sec       YDOT =       -7594
651487  meter/sec
 ZDOT =       2794
036168                 ZDOT =         856
116226

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4772032
65                 X    =        -1454515
55
 Y    =       13051687
31  feet           Y    =         3978154
29  meter
 Z    =       17094317
66                 Z    =         5210348
02
 XDOT =     -21226
750032                 XDOT =       -6469
913410
 YDOT =     -11441
423611  feet/sec       YDOT =       -3487
345916  meter/sec
 ZDOT =       2810
612460                 ZDOT =         856
674678


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   08152
54898460  
00020000  00000-0  20000-3 0  9054
2 25544  51
6360 102
1737 0005901 284
6329  75
4182 15
76609819 25908


Satellite: ISS
Catalog Number: 25544
Epoch time:      08152
54898460   =   yrday
fracday
Element set:     905
Inclination:       51
6360  deg
RA of node:       102
1737  deg
Eccentricity:     
0005901     
Arg of perigee:   284
6329  deg
Mean anomaly:      75
4182  deg
Mean motion:   15
76609819  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2590
Checksum:              304


Coasting Arc #7 (Orbit 2605)
---------------------------------------

Vector Time (GMT): 2008/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -863283
65                 A    =         6724753
01  meter
 Y    =        6660608
38  meter          E    =           
0011059
 Z    =         133589
39                 I    =           51
98049
 XDOT =      -4692
728947                 Wp   =           18
68064
 YDOT =       -732
507320  meter/sec      RA   =           96
49392  deg
 ZDOT =       6069
657338                 TA   =          342
76582
                                          MA   =          342
80334
                                          Ha   =            184
565  n
mi
                                          Hp   =            181
883

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2832295
45                 X    =         -938348
43
 Y    =       21852389
69  feet           Y    =         6650534
92  meter
 Z    =         438285
38                 Z    =          129214
11
 XDOT =     -15396
092345                 XDOT =       -4713
675092
 YDOT =      -2403
239240  feet/sec       YDOT =        -785
102118  meter/sec
 ZDOT =      19913
573942                 ZDOT =        6046
808574

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19492321
33                 X    =         5941259
54
 Y    =       10276779
63  feet           Y    =         3132362
43  meter
 Z    =         422062
27                 Z    =          128644
58
 XDOT =      -6911
018005                 XDOT =       -2106
478288
 YDOT =      12276
388359  feet/sec       YDOT =        3741
843172  meter/sec
 ZDOT =      19825
595812                 ZDOT =        6042
841603


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   08153
56314086  
00020000  00000-0  20000-3 0  9065
2 25544  51
6360  96
9444 0005853 288
6837  71
3692 15
76613608 26067


Satellite: ISS
Catalog Number: 25544
Epoch time:      08153
56314086   =   yrday
fracday
Element set:     906
Inclination:       51
6360  deg
RA of node:        96
9444  deg
Eccentricity:     
0005853     
Arg of perigee:   288
6837  deg
Mean anomaly:      71
3692  deg
Mean motion:   15
76613608  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2606
Checksum:              314


Coasting Arc #8 (Orbit 2620)
---------------------------------------

Vector Time (GMT): 2008/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4032784
46                 A    =         6713071
46  meter
 Y    =        1387529
98  meter          E    =           
0008745
 Z    =       -5191724
64                 I    =           51
94430
 XDOT =      -1091
261714                 Wp   =           89
59412
 YDOT =       7531
439270  meter/sec      RA   =           91
34999  deg
 ZDOT =       1166
913935                 TA   =          191
49383
                                          MA   =          191
51381
                                          Ha   =            184
768  n
mi
                                          Hp   =            181
950

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13230920
14                 X    =         4042190
12
 Y    =        4552263
71  feet           Y    =         1432680
43  meter
 Z    =      -17033217
34                 Z    =        -5172109
87
 XDOT =      -3580
254966                 XDOT =       -1181
067119
 YDOT =      24709
446424  feet/sec       YDOT =        7518
733815  meter/sec
 ZDOT =       3828
457791                 ZDOT =        1161
395719

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8724974
35                 X    =         2659372
18
 Y    =      -11055533
49  feet           Y    =        -3369726
61  meter
 Z    =      -16957619
15                 Z    =        -5168682
32
 XDOT =      21299
381726                 XDOT =        6492
051550
 YDOT =      10977
377815  feet/sec       YDOT =        3345
904758  meter/sec
 ZDOT =       3807
898717                 ZDOT =        1160
647529


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   08154
51390000  
00020000  00000-0  20000-3 0  9072
2 25544  51
6370  92
0425 0005915 292
7847  67
2692 15
76625164 26211


Satellite: ISS
Catalog Number: 25544
Epoch time:      08154
51390000   =   yrday
fracday
Element set:     907
Inclination:       51
6370  deg
RA of node:        92
0425  deg
Eccentricity:     
0005915     
Arg of perigee:   292
7847  deg
Mean anomaly:      67
2692  deg
Mean motion:   15
76625164  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2621
Checksum:              285


Coasting Arc #9 (Orbit 2636)
---------------------------------------

Vector Time (GMT): 2008/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1058292
13                 A    =         6723098
88  meter
 Y    =       -6364294
11  meter          E    =           
0003035
 Z    =       -1883751
26                 I    =           51
97891
 XDOT =       4603
774507                 Wp   =          195
70310
 YDOT =       2443
788198  meter/sec      RA   =           86
24458  deg
 ZDOT =      -5670
735351                 TA   =            5
13799
                                          MA   =            5
13487
                                          Ha   =            184
836  n
mi
                                          Hp   =            181
717

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3472087
04                 X    =         1138531
08
 Y    =      -20880230
03  feet           Y    =        -6352010
64  meter
 Z    =       -6180286
30                 Z    =        -1878416
46
 XDOT =      15104
247071                 XDOT =        4603
653343
 YDOT =       8017
677814  feet/sec       YDOT =        2495
270771  meter/sec
 ZDOT =     -18604
774773                 ZDOT =       -5648
369638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18699369
53                 X    =        -5699567
83
 Y    =       -9930732
50  feet           Y    =        -3026887
27  meter
 Z    =       -6160313
68                 Z    =        -1877663
61
 XDOT =      11692
164086                 XDOT =        3563
771613
 YDOT =     -10530
090153  feet/sec       YDOT =       -3209
571479  meter/sec
 ZDOT =     -18518
493117                 ZDOT =       -5644
436702


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   08155
52803029  
00020000  00000-0  20000-3 0  9085
2 25544  51
6381  86
8142 0005912 296
8592  63
1968 15
76653261 26376


Satellite: ISS
Catalog Number: 25544
Epoch time:      08155
52803029   =   yrday
fracday
Element set:     908
Inclination:       51
6381  deg
RA of node:        86
8142  deg
Eccentricity:     
0005912     
Arg of perigee:   296
8592  deg
Mean anomaly:      63
1968  deg
Mean motion:   15
76653261  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2637
Checksum:              313


Coasting Arc #10 (Orbit 2652)
---------------------------------------

Vector Time (GMT): 2008/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4049090
55                 A    =         6715663
85  meter
 Y    =       -2831194
72  meter          E    =           
0007121
 Z    =        4549392
09                 I    =           51
95083
 XDOT =       1360
492291                 Wp   =           23
80505
 YDOT =      -6924
152733  meter/sec      RA   =           81
07226  deg
 ZDOT =      -3090
146571                 TA   =           96
85867
                                          MA   =           96
77766
                                          Ha   =            185
033  n
mi
                                          Hp   =            181
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13284417
83                 X    =        -4039231
04
 Y    =       -9288696
60  feet           Y    =        -2876419
88  meter
 Z    =       14925827
05                 Z    =         4529744
75
 XDOT =       4463
557386                 XDOT =        1452
829631
 YDOT =     -22717
036526  feet/sec       YDOT =       -6908
421941  meter/sec
 ZDOT =     -10138
276153                 ZDOT =       -3083
314536

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12870410
17                 X    =        -3922901
02
 Y    =        9968296
80  feet           Y    =         3038336
86  meter
 Z    =       14849968
21                 Z    =         4526270
31
 XDOT =     -19588
719081                 XDOT =       -5970
641576
 YDOT =     -10187
262660  feet/sec       YDOT =       -3105
077659  meter/sec
 ZDOT =     -10112
577159                 ZDOT =       -3082
313518


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   08156
54214762  
00020000  00000-0  20000-3 0  9099
2 25544  51
6383  81
5861 0005907 300
7055  59
3527 15
76666596 26532


Satellite: ISS
Catalog Number: 25544
Epoch time:      08156
54214762   =   yrday
fracday
Element set:     909
Inclination:       51
6383  deg
RA of node:        81
5861  deg
Eccentricity:     
0005907     
Arg of perigee:   300
7055  deg
Mean anomaly:      59
3527  deg
Mean motion:   15
76666596  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2653
Checksum:              313


Coasting Arc #11 (Orbit 2668)
---------------------------------------

Vector Time (GMT): 2008/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1366424
80                 A    =         6719440
65  meter
 Y    =        5608279
84  meter          E    =           
0008237
 Z    =        3429935
05                 I    =           51
95830
 XDOT =      -4717
490314                 Wp   =           67
02215
 YDOT =      -3977
524243  meter/sec      RA   =           75
98677  deg
 ZDOT =       4618
719808                 TA   =          333
41521
                                          MA   =          333
45743
                                          Ha   =            185
209  n
mi
                                          Hp   =            181
442

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4483020
99                 X    =        -1445697
92
 Y    =       18399868
25  feet           Y    =         5592555
69  meter
 Z    =       11253067
76                 Z    =         3423105
66
 XDOT =     -15477
330427                 XDOT =       -4695
099307
 YDOT =     -13049
620219  feet/sec       YDOT =       -4030
153759  meter/sec
 ZDOT =      15153
280211                 ZDOT =        4595
855722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16356554
17                 X    =         4985477
71
 Y    =        9575802
22  feet           Y    =         2918704
52  meter
 Z    =       11227257
48                 Z    =         3422068
08
 XDOT =     -16227
362008                 XDOT =       -4946
099940
 YDOT =      10033
686296  feet/sec       YDOT =        3058
267583  meter/sec
 ZDOT =      15064
936744                 ZDOT =        4591
792720


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   08157
55625152  
00020000  00000-0  20000-3 0  9102
2 25544  51
6386  76
3570 0005940 304
8885  55
1721 15
76684675 26692


Satellite: ISS
Catalog Number: 25544
Epoch time:      08157
55625152   =   yrday
fracday
Element set:     910
Inclination:       51
6386  deg
RA of node:        76
3570  deg
Eccentricity:     
0005940     
Arg of perigee:   304
8885  deg
Mean anomaly:      55
1721  deg
Mean motion:   15
76684675  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2669
Checksum:              316


Coasting Arc #12 (Orbit 2683)
---------------------------------------

Vector Time (GMT): 2008/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4196294
57                 A    =         6719535
98  meter
 Y    =        4014416
03  meter          E    =           
0003796
 Z    =       -3376693
13                 I    =           51
95102
 XDOT =      -1835
949242                 Wp   =            1
81570
 YDOT =       5844
952482  meter/sec      RA   =           70
80155  deg
 ZDOT =       4671
107416                 TA   =          318
51813
                                          MA   =          318
54693
                                          Ha   =            185
328  n
mi
                                          Hp   =            181
336

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13767370
65                 X    =         4167496
14
 Y    =       13170656
27  feet           Y    =         4061181
07  meter
 Z    =      -11078389
53                 Z    =        -3356376
76
 XDOT =      -6023
455518                 XDOT =       -1923
863245
 YDOT =      19176
353286  feet/sec       YDOT =        5823
929336  meter/sec
 ZDOT =      15325
155565                 ZDOT =        4661
976076

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16384119
37                 X    =         4993879
58
 Y    =       -9813331
02  feet           Y    =        -2991103
30  meter
 Z    =      -10999843
75                 Z    =        -3352752
38
 XDOT =      16134
259212                 XDOT =        4917
722208
 YDOT =       9812
423518  feet/sec       YDOT =        2990
826688  meter/sec
 ZDOT =      15290
498884                 ZDOT =        4660
544060


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   08158
50696147  
00020000  00000-0  20000-3 0  9111
2 25544  51
6391  71
4549 0005974 308
1890  51
8736 15
76720608 26843


Satellite: ISS
Catalog Number: 25544
Epoch time:      08158
50696147   =   yrday
fracday
Element set:     911
Inclination:       51
6391  deg
RA of node:        71
4549  deg
Eccentricity:     
0005974     
Arg of perigee:   308
1890  deg
Mean anomaly:      51
8736  deg
Mean motion:   15
76720608  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2684
Checksum:              316

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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