Date: May 18th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5920 15 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 2321)
---------------------------------------

Vector Time (GMT): 2008/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6018553
53                 A    =         6724443
35  meter
 Y    =       -2397170
89  meter          E    =           
0009828
 Z    =        1791992
14                 I    =           51
60197
 XDOT =       3301
560771                 Wp   =           84
98763
 YDOT =      -4027
947038  meter/sec      RA   =          189
05379  deg
 ZDOT =       5674
582748                 TA   =          294
89988
                                          MA   =          295
00201
                                          Ha   =            186
719  n
mi
                                          Hp   =            181
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19745910
53                 X    =        -6000005
92
 Y    =       -7864733
89  feet           Y    =        -2464370
18  meter
 Z    =        5879239
32                 Z    =         1762798
72
 XDOT =      10831
892294                 XDOT =        3318
790213
 YDOT =     -13215
049337  feet/sec       YDOT =       -3990
931032  meter/sec
 ZDOT =      18617
397466                 ZDOT =        5690
663515

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18402542
96                 X    =        -5609095
10
 Y    =       10696288
59  feet           Y    =         3260228
76  meter
 Z    =        5766827
53                 Z    =         1757729
03
 XDOT =      -2986
991420                 XDOT =        -910
434985
 YDOT =     -15255
938166  feet/sec       YDOT =       -4650
009953  meter/sec
 ZDOT =      18678
742208                 ZDOT =        5693
280625


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   08135
55996770  
00020000  00000-0  20000-3 0  9004
2 25544  51
6383 189
7309 0005866 211
5317 148
5497 15
76249809 23228


Satellite: ISS
Catalog Number: 25544
Epoch time:      08135
55996770   =   yrday
fracday
Element set:     900
Inclination:       51
6383  deg
RA of node:       189
7309  deg
Eccentricity:     
0005866     
Arg of perigee:   211
5317  deg
Mean anomaly:     148
5497  deg
Mean motion:   15
76249809  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2322
Checksum:              324


Coasting Arc #2 (Orbit 2336)
---------------------------------------

Vector Time (GMT): 2008/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3443649
52                 A    =         6716253
74  meter
 Y    =        3446945
66  meter          E    =           
0010809
 Z    =       -4632269
07                 I    =           51
60420
 XDOT =      -6599
001277                 Wp   =          141
13191
 YDOT =      -2726
540296  meter/sec      RA   =          183
85982  deg
 ZDOT =       2872
206386                 TA   =          157
32824
                                          MA   =          157
28046
                                          Ha   =            186
479  n
mi
                                          Hp   =            181
230

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11298062
73                 X    =        -3459434
86
 Y    =       11308876
85  feet           Y    =         3408348
78  meter
 Z    =      -15197733
19                 Z    =        -4649036
70
 XDOT =     -21650
266658                 XDOT =       -6581
975054
 YDOT =      -8945
342179  feet/sec       YDOT =       -2800
239055  meter/sec
 ZDOT =       9423
249297                 ZDOT =        2840
189253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2239513
27                 X    =          682603
64
 Y    =       15766119
89  feet           Y    =         4805513
34  meter
 Z    =      -15261784
13                 Z    =        -4651791
80
 XDOT =     -19089
856883                 XDOT =       -5818
588378
 YDOT =      11728
823995  feet/sec       YDOT =        3574
945554  meter/sec
 ZDOT =       9299
947315                 ZDOT =        2834
623941


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   08136
51092923  
00020000  00000-0  20000-3 0  9019
2 25544  51
6384 184
8304 0005833 215
6321 144
4454 15
76287898 23378


Satellite: ISS
Catalog Number: 25544
Epoch time:      08136
51092923   =   yrday
fracday
Element set:     901
Inclination:       51
6384  deg
RA of node:       184
8304  deg
Eccentricity:     
0005833     
Arg of perigee:   215
6321  deg
Mean anomaly:     144
4454  deg
Mean motion:   15
76287898  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2337
Checksum:              299


Coasting Arc #3 (Orbit 2352)
---------------------------------------

Vector Time (GMT): 2008/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5418191
48                 A    =         6721282
06  meter
 Y    =        2392147
47  meter          E    =           
0005490
 Z    =       -3172002
85                 I    =           51
65097
 XDOT =      -4551
155722                 Wp   =          171
65134
 YDOT =       3917
825758  meter/sec      RA   =          178
75286  deg
 ZDOT =      -4825
730169                 TA   =           45
36198
                                          MA   =           45
31722
                                          Ha   =            186
391  n
mi
                                          Hp   =            181
442

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17776218
77                 X    =         5406448
69
 Y    =        7848252
86  feet           Y    =         2452671
34  meter
 Z    =      -10406833
49                 Z    =        -3145709
21
 XDOT =     -14931
613262                 XDOT =       -4571
184302
 YDOT =      12853
759048  feet/sec       YDOT =        3866
820460  meter/sec
 ZDOT =     -15832
448062                 ZDOT =       -4847
888442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16862945
32                 X    =         5139825
73
 Y    =       -9763599
92  feet           Y    =        -2975945
25  meter
 Z    =      -10305551
99                 Z    =        -3141132
25
 XDOT =        902
729995                 XDOT =         275
152102
 YDOT =      18337
529762  feet/sec       YDOT =        5589
279071  meter/sec
 ZDOT =     -15917
167342                 ZDOT =       -4851
552606


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   08137
52527809  
00020000  00000-0  20000-3 0  9028
2 25544  51
6389 179
6033 0005758 218
9328 141
1422 15
76318461 23531


Satellite: ISS
Catalog Number: 25544
Epoch time:      08137
52527809   =   yrday
fracday
Element set:     902
Inclination:       51
6389  deg
RA of node:       179
6033  deg
Eccentricity:     
0005758     
Arg of perigee:   218
9328  deg
Mean anomaly:     141
1422  deg
Mean motion:   15
76318461  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2353
Checksum:              301


Coasting Arc #4 (Orbit 2368)
---------------------------------------

Vector Time (GMT): 2008/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4434684
32                 A    =         6719472
45  meter
 Y    =       -3436196
30  meter          E    =           
0008237
 Z    =        3689180
49                 I    =           51
67351
 XDOT =       5749
147188                 Wp   =          110
51572
 YDOT =       2782
399897  meter/sec      RA   =          173
55046  deg
 ZDOT =      -4314
443080                 TA   =           25
02704
                                          MA   =           24
98713
                                          Ha   =            186
007  n
mi
                                          Hp   =            181
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14549489
23                 X    =         4454857
09
 Y    =      -11273609
89  feet           Y    =        -3386492
64  meter
 Z    =       12103610
53                 Z    =         3710773
31
 XDOT =      18862
031456                 XDOT =        5738
565848
 YDOT =       9128
608586  feet/sec       YDOT =        2846
631353  meter/sec
 ZDOT =     -14154
996981                 ZDOT =       -4286
538651

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -867710
85                 X    =         -264478
27
 Y    =      -18330915
67  feet           Y    =        -5587263
10  meter
 Z    =       12186218
17                 Z    =         3714359
30
 XDOT =      17040
175813                 XDOT =        5193
845588
 YDOT =     -10155
825231  feet/sec       YDOT =       -3095
495530  meter/sec
 ZDOT =     -14047
479475                 ZDOT =       -4281
671744


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   08138
53961455  
00020000  00000-0  20000-3 0  9030
2 25544  51
6377 174
3763 0005694 223
9090 136
1623 15
76351552 23693


Satellite: ISS
Catalog Number: 25544
Epoch time:      08138
53961455   =   yrday
fracday
Element set:     903
Inclination:       51
6377  deg
RA of node:       174
3763  deg
Eccentricity:     
0005694     
Arg of perigee:   223
9090  deg
Mean anomaly:     136
1623  deg
Mean motion:   15
76351552  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2369
Checksum:              305


Coasting Arc #5 (Orbit 2384)
---------------------------------------

Vector Time (GMT): 2008/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4535718
82                 A    =         6717682
37  meter
 Y    =       -2514953
72  meter          E    =           
0008751
 Z    =        4269145
12                 I    =           51
69541
 XDOT =       5556
253136                 Wp   =          141
29036
 YDOT =      -3990
713266  meter/sec      RA   =          168
45085  deg
 ZDOT =       3541
672973                 TA   =          272
79407
                                          MA   =          272
89422
                                          Ha   =            186
038  n
mi
                                          Hp   =            181
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14880967
25                 X    =        -4527998
26
 Y    =       -8251160
49  feet           Y    =        -2565632
01  meter
 Z    =       14006381
64                 Z    =         4247128
63
 XDOT =      18229
176957                 XDOT =        5583
259805
 YDOT =     -13092
891292  feet/sec       YDOT =       -3928
429440  meter/sec
 ZDOT =      11619
661984                 ZDOT =        3568
730981

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15234218
86                 X    =        -4643389
91
 Y    =        7733926
99  feet           Y    =         2357300
95  meter
 Z    =       13921512
54                 Z    =         4243277
02
 XDOT =        -53
358014                 XDOT =         -16
263523
 YDOT =     -21270
527433  feet/sec       YDOT =       -6483
256761  meter/sec
 ZDOT =      11723
224800                 ZDOT =        3573
238919


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   08139
55394143  
00020000  00000-0  20000-3 0  9048
2 25544  51
6371 169
1484 0005552 226
5399 133
5304 15
76339108 23851


Satellite: ISS
Catalog Number: 25544
Epoch time:      08139
55394143   =   yrday
fracday
Element set:     904
Inclination:       51
6371  deg
RA of node:       169
1484  deg
Eccentricity:     
0005552     
Arg of perigee:   226
5399  deg
Mean anomaly:     133
5304  deg
Mean motion:   15
76339108  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2385
Checksum:              301


Coasting Arc #6 (Orbit 2399)
---------------------------------------

Vector Time (GMT): 2008/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5180583
91                 A    =         6722765
42  meter
 Y    =        3542568
02  meter          E    =           
0000258
 Z    =       -2409494
22                 I    =           51
74274
 XDOT =      -4587
902579                 Wp   =          288
81150
 YDOT =      -3049
866323  meter/sec      RA   =          163
25719  deg
 ZDOT =       5379
854477                 TA   =           44
03083
                                          MA   =           44
02877
                                          Ha   =            185
758  n
mi
                                          Hp   =            181
578

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16996666
37                 X    =        -5208107
31
 Y    =       11622598
49  feet           Y    =         3484482
18  meter
 Z    =       -7905164
78                 Z    =        -2434728
41
 XDOT =     -15052
173817                 XDOT =       -4579
592392
 YDOT =     -10006
123106  feet/sec       YDOT =       -3101
125094  meter/sec
 ZDOT =      17650
441197                 ZDOT =        5357
585793

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         435900
30                 X    =          132862
41
 Y    =       20548591
22  feet           Y    =         6263210
60  meter
 Z    =       -8001780
02                 Z    =        -2438942
55
 XDOT =     -15173
790251                 XDOT =       -4624
971269
 YDOT =       7162
137778  feet/sec       YDOT =        2183
019595  meter/sec
 ZDOT =      17564
542137                 ZDOT =        5353
672443


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   08140
50486132  
00020000  00000-0  20000-3 0  9056
2 25544  51
6380 164
2480 0005587 229
9918 130
0757 15
76397426 24004


Satellite: ISS
Catalog Number: 25544
Epoch time:      08140
50486132   =   yrday
fracday
Element set:     905
Inclination:       51
6380  deg
RA of node:       164
2480  deg
Eccentricity:     
0005587     
Arg of perigee:   229
9918  deg
Mean anomaly:     130
0757  deg
Mean motion:   15
76397426  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2400
Checksum:              292


Coasting Arc #7 (Orbit 2415)
---------------------------------------

Vector Time (GMT): 2008/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3432776
54                 A    =         6714587
88  meter
 Y    =        2878616
29  meter          E    =           
0008081
 Z    =       -5008447
99                 I    =           51
74177
 XDOT =      -6223
226631                 Wp   =           89
84875
 YDOT =       4113
272018  meter/sec      RA   =          158
14771  deg
 ZDOT =      -1903
878441                 TA   =          161
80898
                                          MA   =          161
78005
                                          Ha   =            185
630  n
mi
                                          Hp   =            181
911

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11262390
23                 X    =         3424662
84
 Y    =        9444279
16  feet           Y    =         2916958
92  meter
 Z    =      -16431915
99                 Z    =        -4991790
55
 XDOT =     -20417
410208                 XDOT =       -6259
510494
 YDOT =      13494
986936  feet/sec       YDOT =        4043
477742  meter/sec
 ZDOT =      -6246
320344                 ZDOT =       -1934
198967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14045639
72                 X    =         4281110
99
 Y    =       -4567877
26  feet           Y    =        -1392288
99  meter
 Z    =      -16367596
27                 Z    =        -4988843
34
 XDOT =        210
377115                 XDOT =          64
122945
 YDOT =      23413
979248  feet/sec       YDOT =        7136
580875  meter/sec
 ZDOT =      -6362
442868                 ZDOT =       -1939
272586


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   08141
51916514  
00020000  00000-0  20000-3 0  9061
2 25544  51
6374 159
0202 0005611 235
3284 124
7352 15
76372623 24166


Satellite: ISS
Catalog Number: 25544
Epoch time:      08141
51916514   =   yrday
fracday
Element set:     906
Inclination:       51
6374  deg
RA of node:       159
0202  deg
Eccentricity:     
0005611     
Arg of perigee:   235
3284  deg
Mean anomaly:     124
7352  deg
Mean motion:   15
76372623  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2416
Checksum:              269


Coasting Arc #8 (Orbit 2431)
---------------------------------------

Vector Time (GMT): 2008/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5589089
37                 A    =         6725017
44  meter
 Y    =       -3622061
38  meter          E    =           
0012492
 Z    =         873646
51                 I    =           51
80278
 XDOT =       3274
796209                 Wp   =          149
33999
 YDOT =       3605
999674  meter/sec      RA   =          152
97869  deg
 ZDOT =      -5973
450095                 TA   =           21
13394
                                          MA   =           21
08237
                                          Ha   =            185
389  n
mi
                                          Hp   =            181
817

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18336907
40                 X    =         5624932
36
 Y    =      -11883403
46  feet           Y    =        -3559360
71  meter
 Z    =        2866294
33                 Z    =          900885
21
 XDOT =      10744
082052                 XDOT =        3263
248336
 YDOT =      11830
707593  feet/sec       YDOT =        3642
556700  meter/sec
 ZDOT =     -19597
933384                 ZDOT =       -5957
568371

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -655307
26                 X    =         -199737
65
 Y    =      -21827023
96  feet           Y    =        -6652876
90  meter
 Z    =        2970638
23                 Z    =          905450
53
 XDOT =      14153
990268                 XDOT =        4314
136234
 YDOT =      -3095
330764  feet/sec       YDOT =        -943
456817  meter/sec
 ZDOT =     -19536
517374                 ZDOT =       -5954
730496


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   08142
53345797  
00020000  00000-0  20000-3 0  9074
2 25544  51
6362 153
7922 0005466 239
2867 120
7760 15
76395421 24329


Satellite: ISS
Catalog Number: 25544
Epoch time:      08142
53345797   =   yrday
fracday
Element set:     907
Inclination:       51
6362  deg
RA of node:       153
7922  deg
Eccentricity:     
0005466     
Arg of perigee:   239
2867  deg
Mean anomaly:     120
7760  deg
Mean motion:   15
76395421  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2432
Checksum:              305


Coasting Arc #9 (Orbit 2447)
---------------------------------------

Vector Time (GMT): 2008/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2282170
18                 A    =         6713237
94  meter
 Y    =       -3471209
40  meter          E    =           
0003686
 Z    =        5275756
57                 I    =           51
78825
 XDOT =       6490
057909                 Wp   =          224
63576
 YDOT =      -4149
426941  meter/sec      RA   =          147
84497  deg
 ZDOT =         74
772895                 TA   =          224
64159
                                          MA   =          224
67128
                                          Ha   =            185
246  n
mi
                                          Hp   =            181
925

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7487434
97                 X    =        -2268813
91
 Y    =      -11388482
30  feet           Y    =        -3496656
14  meter
 Z    =       17308912
64                 Z    =         5264701
53
 XDOT =      21292
840908                 XDOT =        6535
611858
 YDOT =     -13613
605449  feet/sec       YDOT =       -4076
596709  meter/sec
 ZDOT =        245
317896                 ZDOT =         106
411916

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13659458
88                 X    =        -4163403
07
 Y    =         812366
16  feet           Y    =          247609
20  meter
 Z    =       17266062
45                 Z    =         5262695
83
 XDOT =       -968
589306                 XDOT =        -295
226021
 YDOT =     -24254
376602  feet/sec       YDOT =       -7392
733988  meter/sec
 ZDOT =        366
543216                 ZDOT =         111
722372


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   08143
54773898  
00020000  00000-0  20000-3 0  9084
2 25544  51
6358 148
5639 0005506 244
2746 115
7850 15
76412216 24481


Satellite: ISS
Catalog Number: 25544
Epoch time:      08143
54773898   =   yrday
fracday
Element set:     908
Inclination:       51
6358  deg
RA of node:       148
5639  deg
Eccentricity:     
0005506     
Arg of perigee:   244
2746  deg
Mean anomaly:     115
7850  deg
Mean motion:   15
76412216  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2448
Checksum:              317


Coasting Arc #10 (Orbit 2463)
---------------------------------------

Vector Time (GMT): 2008/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5650547
67                 A    =         6724916
33  meter
 Y    =        3559213
82  meter          E    =           
0008130
 Z    =         753254
18                 I    =           51
85269
 XDOT =      -1976
966501                 Wp   =           42
95146
 YDOT =      -4414
376502  meter/sec      RA   =          142
71098  deg
 ZDOT =       5996
361672                 TA   =          325
24246
                                          MA   =          325
29555
                                          Ha   =            184
941  n
mi
                                          Hp   =            181
956

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18538542
22                 X    =        -5693586
59
 Y    =       11677210
70  feet           Y    =         3495785
40  meter
 Z    =        2471306
36                 Z    =          725699
66
 XDOT =      -6486
110569                 XDOT =       -1956
586767
 YDOT =     -14482
862541  feet/sec       YDOT =       -4436
371122  meter/sec
 ZDOT =      19673
102598                 ZDOT =        5986
806264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1112416
11                 X    =          339064
43
 Y    =       21893106
23  feet           Y    =         6673018
78  meter
 Z    =        2365709
70                 Z    =          721068
32
 XDOT =     -14262
960136                 XDOT =       -4347
350249
 YDOT =      -1408
876509  feet/sec       YDOT =        -429
425560  meter/sec
 ZDOT =      19635
921726                 ZDOT =        5985
028942


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   08144
56200698  
00020000  00000-0  20000-3 0  9091
2 25544  51
6362 143
3367 0005616 247
3204 112
7367 15
76477708 24647


Satellite: ISS
Catalog Number: 25544
Epoch time:      08144
56200698   =   yrday
fracday
Element set:     909
Inclination:       51
6362  deg
RA of node:       143
3367  deg
Eccentricity:     
0005616     
Arg of perigee:   247
3204  deg
Mean anomaly:     112
7367  deg
Mean motion:   15
76477708  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2464
Checksum:              300


Coasting Arc #11 (Orbit 2478)
---------------------------------------

Vector Time (GMT): 2008/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1206184
94                 A    =         6714225
89  meter
 Y    =        4270985
50  meter          E    =           
0009079
 Z    =       -5046197
44                 I    =           51
83837
 XDOT =      -6376
386088                 Wp   =          121
19790
 YDOT =       3922
591783  meter/sec      RA   =          137
54910  deg
 ZDOT =       1793
607912                 TA   =          166
05161
                                          MA   =          166
02651
                                          Ha   =            184
765  n
mi
                                          Hp   =            182
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3957299
66                 X    =         1182850
07
 Y    =       14012419
63  feet           Y    =         4284344
08  meter
 Z    =      -16555765
89                 Z    =        -5040393
78
 XDOT =     -20919
901864                 XDOT =       -6428
488274
 YDOT =      12869
395615  feet/sec       YDOT =        3850
995785  meter/sec
 ZDOT =       5884
540393                 ZDOT =        1762
505363

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14258705
03                 X    =         4346053
29
 Y    =        3074075
78  feet           Y    =          936978
30  meter
 Z    =      -16533024
46                 Z    =        -5039265
86
 XDOT =       1624
878905                 XDOT =         495
263090
 YDOT =      23509
994925  feet/sec       YDOT =        7165
846453  meter/sec
 ZDOT =       5765
321225                 ZDOT =        1757
269909


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   08145
51287660  
00020000  00000-0  20000-3 0  9103
2 25544  51
6358 138
4351 0005537 253
4109 106
6447 15
76423229 24790


Satellite: ISS
Catalog Number: 25544
Epoch time:      08145
51287660   =   yrday
fracday
Element set:     910
Inclination:       51
6358  deg
RA of node:       138
4351  deg
Eccentricity:     
0005537     
Arg of perigee:   253
4109  deg
Mean anomaly:     106
6447  deg
Mean motion:   15
76423229  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2479
Checksum:              295


Coasting Arc #12 (Orbit 2494)
---------------------------------------

Vector Time (GMT): 2008/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5421579
73                 A    =         6722845
51  meter
 Y    =       -3202933
31  meter          E    =           
0005438
 Z    =       -2344441
85                 I    =           51
88834
 XDOT =        839
934259                 Wp   =          193
60405
 YDOT =       5396
874140  meter/sec      RA   =          132
44568  deg
 ZDOT =      -5433
383770                 TA   =           12
72033
                                          MA   =           12
70662
                                          Ha   =            184
648  n
mi
                                          Hp   =            182
028

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17787335
06                 X    =         5468381
38
 Y    =      -10508311
37  feet           Y    =        -3142044
08  meter
 Z    =       -7691738
36                 Z    =        -2317990
54
 XDOT =       2755
689825                 XDOT =         805
917579
 YDOT =      17706
279987  feet/sec       YDOT =        5406
077350  meter/sec
 ZDOT =     -17826
062239                 ZDOT =       -5429
385213

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1157192
52                 X    =         -352712
28
 Y    =      -20664574
49  feet           Y    =        -6298562
30  meter
 Z    =       -7590322
91                 Z    =        -2313530
42
 XDOT =      15536
878729                 XDOT =        4735
640637
 YDOT =       5668
587768  feet/sec       YDOT =        1727
785552  meter/sec
 ZDOT =     -17810
150792                 ZDOT =       -5428
533961


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   08146
52712459  
00020000  00000-0  20000-3 0  9115
2 25544  51
6357 133
2068 0005452 257
7410 102
3144 15
76461938 24959


Satellite: ISS
Catalog Number: 25544
Epoch time:      08146
52712459   =   yrday
fracday
Element set:     911
Inclination:       51
6357  deg
RA of node:       133
2068  deg
Eccentricity:     
0005452     
Arg of perigee:   257
7410  deg
Mean anomaly:     102
3144  deg
Mean motion:   15
76461938  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2495
Checksum:              286

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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