Date: April 2nd 2009

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) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 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 3388)
---------------------------------------

Vector Time (GMT): 2009/091/12:23:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5350011
20                 A    =         6731697
46  meter
 Y    =       -1280280
97  meter          E    =           
0008985
 Z    =       -3878850
08                 I    =           51
52487
 XDOT =       4154
608771                 Wp   =          143
36276
 YDOT =      -5029
838244  meter/sec      RA   =          339
37671  deg
 ZDOT =      -4082
108035                 TA   =           84
03580
                                          MA   =           83
93340
                                          Ha   =            195
150  n
mi
                                          Hp   =            186
492

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17552530
17                 X    =        -5316454
48
 Y    =       -4200396
88  feet           Y    =        -1339920
25  meter
 Z    =      -12725886
07                 Z    =        -3904758
96
 XDOT =      13630
606203                 XDOT =        4230
374646
 YDOT =     -16502
093978  feet/sec       YDOT =       -4982
955319  meter/sec
 ZDOT =     -13392
742897                 ZDOT =       -4061
740939

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17970219
48                 X    =        -5477322
90
 Y    =         467778
93  feet           Y    =          142579
02  meter
 Z    =      -12827128
29                 Z    =        -3909708
70
 XDOT =       9002
275974                 XDOT =        2743
893717
 YDOT =     -18178
046431  feet/sec       YDOT =       -5540
668552  meter/sec
 ZDOT =     -13313
534887                 ZDOT =       -4057
965434


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   09091
53941688  
00010596  00000-0  82463-4 0  9003
2 25544  51
6437 339
7443 0009246 186
9335 173
1700 15
71839154 33893


Satellite: ISS
Catalog Number: 25544
Epoch time:      09091
53941688   =   yrday
fracday
Element set:     900
Inclination:       51
6437  deg
RA of node:       339
7443  deg
Eccentricity:     
0009246     
Arg of perigee:   186
9335  deg
Mean anomaly:     173
1700  deg
Mean motion:   15
71839154  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3389
Checksum:              336


Coasting Arc #2 (Orbit 3404)
---------------------------------------

Vector Time (GMT): 2009/092/12:23:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2472227
54                 A    =         6731079
95  meter
 Y    =        4768792
56  meter          E    =           
0011046
 Z    =        4044043
53                 I    =           51
49605
 XDOT =      -6666
426820                 Wp   =          126
31152
 YDOT =       -184
798226  meter/sec      RA   =          334
19720  deg
 ZDOT =      -3856
587675                 TA   =            3
46184
                                          MA   =            3
45421
                                          Ha   =            194
988  n
mi
                                          Hp   =            186
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8110982
76                 X    =        -2545014
39
 Y    =       15645644
87  feet           Y    =         4740739
68  meter
 Z    =       13267859
35                 Z    =         4031856
72
 XDOT =     -21871
479068                 XDOT =       -6645
130386
 YDOT =       -606
293392  feet/sec       YDOT =        -259
227006  meter/sec
 ZDOT =     -12652
846703                 ZDOT =       -3888
921308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3560867
68                 X    =        -1085352
47
 Y    =       17295864
96  feet           Y    =         5271779
64  meter
 Z    =       13220575
37                 Z    =         4029631
37
 XDOT =     -19860
394802                 XDOT =       -6053
448336
 YDOT =       5681
363666  feet/sec       YDOT =        1731
679646  meter/sec
 ZDOT =     -12779
110124                 ZDOT =       -3895
072766


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   09092
55663294  
00010596  00000-0  82463-4 0  9011
2 25544  51
6438 334
5372 0009082 190
6387 169
4585 15
71906706 34051


Satellite: ISS
Catalog Number: 25544
Epoch time:      09092
55663294   =   yrday
fracday
Element set:     901
Inclination:       51
6438  deg
RA of node:       334
5372  deg
Eccentricity:     
0009082     
Arg of perigee:   190
6387  deg
Mean anomaly:     169
4585  deg
Mean motion:   15
71906706  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3405
Checksum:              332


Coasting Arc #3 (Orbit 3420)
---------------------------------------

Vector Time (GMT): 2009/093/12:23:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6036517
14                 A    =         6734700
84  meter
 Y    =       -1002236
20  meter          E    =           
0012851
 Z    =        2812313
59                 I    =           51
48159
 XDOT =      -1453
100873                 Wp   =          120
82229
 YDOT =       5586
486037  meter/sec      RA   =          329
11535  deg
 ZDOT =       5086
233757                 TA   =          271
43597
                                          MA   =          271
58319
                                          Ha   =            194
836  n
mi
                                          Hp   =            186
882

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19804846
25                 X    =         6033614
06
 Y    =       -3288176
51  feet           Y    =         -934748
54  meter
 Z    =        9226750
61                 Z    =         2841631
71
 XDOT =      -4767
391316                 XDOT =       -1540
169698
 YDOT =      18328
366264  feet/sec       YDOT =        5569
749866  meter/sec
 ZDOT =      16687
118624                 ZDOT =        5078
963078

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17930578
70                 X    =         5465240
39
 Y    =       -8911448
77  feet           Y    =        -2716209
58  meter
 Z    =        9341166
69                 Z    =         2847187
61
 XDOT =         49
543249                 XDOT =          15
100782
 YDOT =      17642
486311  feet/sec       YDOT =        5377
429827  meter/sec
 ZDOT =      16659
086119                 ZDOT =        5077
689449


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   09093
57383650  
00010596  00000-0  82463-4 0  9020
2 25544  51
6433 329
3292 0009077 194
9181 165
1715 15
71882015 34214


Satellite: ISS
Catalog Number: 25544
Epoch time:      09093
57383650   =   yrday
fracday
Element set:     902
Inclination:       51
6433  deg
RA of node:       329
3292  deg
Eccentricity:     
0009077     
Arg of perigee:   194
9181  deg
Mean anomaly:     165
1715  deg
Mean motion:   15
71882015  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3421
Checksum:              314


Coasting Arc #4 (Orbit 3435)
---------------------------------------

Vector Time (GMT): 2009/094/12:23:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          74794
10                 A    =         6728252
85  meter
 Y    =       -4757733
75  meter          E    =           
0014622
 Z    =       -4768705
54                 I    =           51
43477
 XDOT =       6824
229887                 Wp   =          146
71999
 YDOT =      -2455
575307  meter/sec      RA   =          323
93882  deg
 ZDOT =       2548
631112                 TA   =          148
41216
                                          MA   =          148
32431
                                          Ha   =            194
656  n
mi
                                          Hp   =            187
082

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         245387
46                 X    =          151155
60
 Y    =      -15609362
71  feet           Y    =        -4756470
60  meter
 Z    =      -15645359
40                 Z    =        -4768156
52
 XDOT =      22389
205665                 XDOT =        6838
800679
 YDOT =      -8056
349432  feet/sec       YDOT =       -2379
181214  meter/sec
 ZDOT =       8361
650630                 ZDOT =        2581
818391

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4494048
86                 X    =        -1369786
09
 Y    =      -14952368
21  feet           Y    =        -4557481
83  meter
 Z    =      -15643525
81                 Z    =        -4768146
67
 XDOT =      17677
043016                 XDOT =        5387
962711
 YDOT =     -14225
131874  feet/sec       YDOT =       -4335
820195  meter/sec
 ZDOT =       8491
080248                 ZDOT =        2588
081259


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   09094
52745042  
00010596  00000-0  82463-4 0  9034
2 25544  51
6427 324
4467 0009145 199
0856 160
9965 15
71924450 34364


Satellite: ISS
Catalog Number: 25544
Epoch time:      09094
52745042   =   yrday
fracday
Element set:     903
Inclination:       51
6427  deg
RA of node:       324
4467  deg
Eccentricity:     
0009145     
Arg of perigee:   199
0856  deg
Mean anomaly:     160
9965  deg
Mean motion:   15
71924450  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3436
Checksum:              328


Coasting Arc #5 (Orbit 3451)
---------------------------------------

Vector Time (GMT): 2009/095/12:23:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5668269
84                 A    =         6736972
28  meter
 Y    =        3243539
09  meter          E    =           
0014795
 Z    =       -1616500
49                 I    =           51
44048
 XDOT =      -1228
833527                 Wp   =          175
24800
 YDOT =      -4995
405627  meter/sec      RA   =          318
84096  deg
 ZDOT =      -5732
701618                 TA   =           22
64675
                                          MA   =           22
58154
                                          Ha   =            194
482  n
mi
                                          Hp   =            187
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18596685
83                 X    =        -5696265
76
 Y    =       10641532
45  feet           Y    =         3179996
55  meter
 Z    =       -5303479
31                 Z    =        -1644104
94
 XDOT =      -4031
606061                 XDOT =       -1145
034533
 YDOT =     -16389
126074  feet/sec       YDOT =       -5008
678996  meter/sec
 ZDOT =     -18808
076174                 ZDOT =       -5738
467365

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14104633
52                 X    =        -4299092
30
 Y    =       16093031
10  feet           Y    =         4905155
88  meter
 Z    =       -5411052
84                 Z    =        -1649288
91
 XDOT =      -7858
148679                 XDOT =       -2395
163717
 YDOT =     -13199
134595  feet/sec       YDOT =       -4023
096224  meter/sec
 ZDOT =     -18830
921889                 ZDOT =       -5739
664992


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   09095
54462649  
00010596  00000-0  82463-4 0  9047
2 25544  51
6423 319
2401 0009266 203
3015 156
7728 15
71902680 34529


Satellite: ISS
Catalog Number: 25544
Epoch time:      09095
54462649   =   yrday
fracday
Element set:     904
Inclination:       51
6423  deg
RA of node:       319
2401  deg
Eccentricity:     
0009266     
Arg of perigee:   203
3015  deg
Mean anomaly:     156
7728  deg
Mean motion:   15
71902680  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3452
Checksum:              306


Coasting Arc #6 (Orbit 3467)
---------------------------------------

Vector Time (GMT): 2009/096/12:23:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2131984
80                 A    =         6726356
41  meter
 Y    =        3742598
32  meter          E    =           
0006038
 Z    =        5166223
77                 I    =           51
38328
 XDOT =      -5865
347014                 Wp   =          188
92930
 YDOT =       4861
394748  meter/sec      RA   =          313
67962  deg
 ZDOT =      -1107
321512                 TA   =          271
64464
                                          MA   =          271
71380
                                          Ha   =            194
223  n
mi
                                          Hp   =            187
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6994700
78                 X    =         2064879
51
 Y    =       12278865
89  feet           Y    =         3766064
65  meter
 Z    =       16949553
04                 Z    =         5176417
59
 XDOT =     -19243
264480                 XDOT =       -5913
892872
 YDOT =      15949
457836  feet/sec       YDOT =        4795
533490  meter/sec
 ZDOT =      -3632
944594                 ZDOT =       -1135
933568

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10669476
46                 X    =         3252056
42
 Y    =        9192343
67  feet           Y    =         2801826
35  meter
 Z    =       16989609
31                 Z    =         5178432
92
 XDOT =     -11962
788400                 XDOT =       -3646
257904
 YDOT =      20768
925776  feet/sec       YDOT =        6330
368577  meter/sec
 ZDOT =      -3744
337113                 ZDOT =       -1141
273952


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   09096
56178735  
00010596  00000-0  82463-4 0  9051
2 25544  51
6418 314
0319 0009155 207
3868 152
6813 15
71954858 34682


Satellite: ISS
Catalog Number: 25544
Epoch time:      09096
56178735   =   yrday
fracday
Element set:     905
Inclination:       51
6418  deg
RA of node:       314
0319  deg
Eccentricity:     
0009155     
Arg of perigee:   207
3868  deg
Mean anomaly:     152
6813  deg
Mean motion:   15
71954858  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3468
Checksum:              343


Coasting Arc #7 (Orbit 3483)
---------------------------------------

Vector Time (GMT): 2009/097/12:23:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4392461
18                 A    =         6737874
69  meter
 Y    =       -5098234
84  meter          E    =           
0004959
 Z    =         322664
75                 I    =           51
40136
 XDOT =       3449
565751                 Wp   =           81
84160
 YDOT =       3356
714330  meter/sec      RA   =          308
55353  deg
 ZDOT =       6000
256481                 TA   =          281
67172
                                          MA   =          281
72736
                                          Ha   =            194
095  n
mi
                                          Hp   =            187
692

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14410961
87                 X    =         4447576
59
 Y    =      -16726492
24  feet           Y    =        -5048807
58  meter
 Z    =        1058611
38                 Z    =          344137
68
 XDOT =      11317
472936                 XDOT =        3382
625828
 YDOT =      11012
842291  feet/sec       YDOT =        3394
915645  meter/sec
 ZDOT =      19685
880844                 ZDOT =        6016
851592

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7483332
15                 X    =         2280919
64
 Y    =      -20766977
60  feet           Y    =        -6329774
77  meter
 Z    =        1142105
14                 Z    =          348113
65
 XDOT =      12882
680650                 XDOT =        3926
641062
 YDOT =       5741
511600  feet/sec       YDOT =        1750
012736  meter/sec
 ZDOT =      19750
906375                 ZDOT =        6020
076263


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   09097
57893449  
00010596  00000-0  82463-4 0  9060
2 25544  51
6403 308
8228 0009149 211
5643 148
4971 15
71980102 34844


Satellite: ISS
Catalog Number: 25544
Epoch time:      09097
57893449   =   yrday
fracday
Element set:     906
Inclination:       51
6403  deg
RA of node:       308
8228  deg
Eccentricity:     
0009149     
Arg of perigee:   211
5643  deg
Mean anomaly:     148
4971  deg
Mean motion:   15
71980102  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3484
Checksum:              334


Coasting Arc #8 (Orbit 3498)
---------------------------------------

Vector Time (GMT): 2009/098/12:27:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2636716
16                 A    =         6726366
37  meter
 Y    =       -3465222
11  meter          E    =           
0013231
 Z    =       -5136195
58                 I    =           51
34398
 XDOT =       4990
006825                 Wp   =          138
63118
 YDOT =      -5708
736917  meter/sec      RA   =          303
38430  deg
 ZDOT =       1281
930422                 TA   =          143
73981
                                          MA   =          143
65006
                                          Ha   =            193
878  n
mi
                                          Hp   =            187
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8650643
56                 X    =        -2572820
61
 Y    =      -11368838
96  feet           Y    =        -3494350
59  meter
 Z    =      -16851035
37                 Z    =        -5148849
34
 XDOT =      16371
413469                 XDOT =        5047
244578
 YDOT =     -18729
451826  feet/sec       YDOT =       -5652
615607  meter/sec
 ZDOT =       4205
808471                 ZDOT =        1306
311554

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12303676
15                 X    =        -3750160
49
 Y    =       -7143397
52  feet           Y    =        -2177307
56  meter
 Z    =      -16900679
01                 Z    =        -5151326
96
 XDOT =       7246
847747                 XDOT =        2208
839193
 YDOT =     -22717
863556  feet/sec       YDOT =       -6924
404812  meter/sec
 ZDOT =       4300
610085                 ZDOT =        1310
825954


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   09098
53249747  
00010596  00000-0  82463-4 0  9074
2 25544  51
6390 303
9390 0009134 214
8396 145
2169 15
72005496 34995


Satellite: ISS
Catalog Number: 25544
Epoch time:      09098
53249747   =   yrday
fracday
Element set:     907
Inclination:       51
6390  deg
RA of node:       303
9390  deg
Eccentricity:     
0009134     
Arg of perigee:   214
8396  deg
Mean anomaly:     145
2169  deg
Mean motion:   15
72005496  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3499
Checksum:              339


Coasting Arc #9 (Orbit 3514)
---------------------------------------

Vector Time (GMT): 2009/099/12:27:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3519577
19                 A    =         6737666
72  meter
 Y    =        5711957
38  meter          E    =           
0015433
 Z    =        -494973
61                 I    =           51
36739
 XDOT =      -3874
932754                 Wp   =          174
02450
 YDOT =      -2904
031302  meter/sec      RA   =          298
26016  deg
 ZDOT =      -5990
896421                 TA   =           11
37998
                                          MA   =           11
34513
                                          Ha   =            193
584  n
mi
                                          Hp   =            188
125

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11547169
26                 X    =        -3580783
15
 Y    =       18740017
66  feet           Y    =         5672257
16  meter
 Z    =       -1623929
17                 Z    =         -512220
99
 XDOT =     -12713
033969                 XDOT =       -3813
068364
 YDOT =      -9527
661752  feet/sec       YDOT =       -2947
017584  meter/sec
 ZDOT =     -19655
171986                 ZDOT =       -6009
570583

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2958973
65                 X    =         -901895
17
 Y    =       21807061
74  feet           Y    =         6646792
42  meter
 Z    =       -1690875
28                 Z    =         -515378
78
 XDOT =     -13788
240348                 XDOT =       -4202
655658
 YDOT =      -3392
822548  feet/sec       YDOT =       -1034
132313  meter/sec
 ZDOT =     -19728
281677                 ZDOT =       -6013
180255


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   09099
54961704  
00010596  00000-0  82463-4 0  9081
2 25544  51
6393 298
7315 0009049 219
5916 140
4586 15
72034034 35150


Satellite: ISS
Catalog Number: 25544
Epoch time:      09099
54961704   =   yrday
fracday
Element set:     908
Inclination:       51
6393  deg
RA of node:       298
7315  deg
Eccentricity:     
0009049     
Arg of perigee:   219
5916  deg
Mean anomaly:     140
4586  deg
Mean motion:   15
72034034  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3515
Checksum:              331


Coasting Arc #10 (Orbit 3530)
---------------------------------------

Vector Time (GMT): 2009/100/12:27:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3938426
07                 A    =         6725821
61  meter
 Y    =        1482169
76  meter          E    =           
0007926
 Z    =        5250124
60                 I    =           51
31347
 XDOT =      -2902
596627                 Wp   =          207
83752
 YDOT =       7125
154092  meter/sec      RA   =          293
11338  deg
 ZDOT =        159
083096                 TA   =          240
60531
                                          MA   =          240
68446
                                          Ha   =            193
489  n
mi
                                          Hp   =            188
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12921345
36                 X    =         3896054
95
 Y    =        4862761
67  feet           Y    =         1525974
89  meter
 Z    =       17224818
23                 Z    =         5269154
75
 XDOT =      -9522
954812                 XDOT =       -2982
828373
 YDOT =      23376
489804  feet/sec       YDOT =        7092
246973  meter/sec
 ZDOT =        521
926167                 ZDOT =         144
786832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13677519
31                 X    =         4168907
89
 Y    =        -982067
47  feet           Y    =         -299334
17  meter
 Z    =       17299219
32                 Z    =         5272802
05
 XDOT =       1120
541116                 XDOT =         341
540932
 YDOT =      24217
305810  feet/sec       YDOT =        7381
434811  meter/sec
 ZDOT =        466
599068                 ZDOT =         142
219396


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   09100
56672430  
00010596  00000-0  82463-4 0  9092
2 25544  51
6385 293
5220 0009072 222
5607 137
4852 15
71996488 35315


Satellite: ISS
Catalog Number: 25544
Epoch time:      09100
56672430   =   yrday
fracday
Element set:     909
Inclination:       51
6385  deg
RA of node:       293
5220  deg
Eccentricity:     
0009072     
Arg of perigee:   222
5607  deg
Mean anomaly:     137
4852  deg
Mean motion:   15
71996488  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3531
Checksum:              317


Coasting Arc #11 (Orbit 3545)
---------------------------------------

Vector Time (GMT): 2009/101/12:27:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1480944
74                 A    =         6737449
61  meter
 Y    =       -6527922
27  meter          E    =           
0001775
 Z    =        -755280
38                 I    =           51
34259
 XDOT =       4864
546188                 Wp   =            2
90927
 YDOT =        415
996610  meter/sec      RA   =          287
96043  deg
 ZDOT =       5945
224856                 TA   =          348
83564
                                          MA   =          348
83958
                                          Ha   =            193
323  n
mi
                                          Hp   =            188
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4858742
57                 X    =         1557500
06
 Y    =      -21417067
82  feet           Y    =        -6510933
46  meter
 Z    =       -2477954
02                 Z    =         -747899
71
 XDOT =      15959
797204                 XDOT =        4830
651623
 YDOT =       1364
818275  feet/sec       YDOT =         470
205448  meter/sec
 ZDOT =      19505
330894                 ZDOT =        5968
774842

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4957750
14                 X    =        -1511122
24
 Y    =      -21397632
51  feet           Y    =        -6521998
39  meter
 Z    =       -2449584
88                 Z    =         -746633
47
 XDOT =      13294
583696                 XDOT =        4052
189111
 YDOT =      -5322
893423  feet/sec       YDOT =       -1622
417915  meter/sec
 ZDOT =      19597
306444                 ZDOT =        5973
259004


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   09101
52024636  
00010596  00000-0  82463-4 0  9100
2 25544  51
6382 288
6378 0009159 226
2437 133
7968 15
72061682 35462


Satellite: ISS
Catalog Number: 25544
Epoch time:      09101
52024636   =   yrday
fracday
Element set:     910
Inclination:       51
6382  deg
RA of node:       288
6378  deg
Eccentricity:     
0009159     
Arg of perigee:   226
2437  deg
Mean anomaly:     133
7968  deg
Mean motion:   15
72061682  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3546
Checksum:              322


Coasting Arc #12 (Orbit 3561)
---------------------------------------

Vector Time (GMT): 2009/102/12:27:04
881
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4349288
40                 A    =         6726314
44  meter
 Y    =         779743
05  meter          E    =           
0007345
 Z    =       -5076452
25                 I    =           51
29771
 XDOT =        446
553467                 Wp   =          114
50615
 YDOT =      -7524
111780  meter/sec      RA   =          282
83710  deg
 ZDOT =      -1543
046340                 TA   =          140
62873
                                          MA   =          140
57532
                                          Ha   =            192
985  n
mi
                                          Hp   =            188
514

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14269318
91                 X    =        -4333023
53
 Y    =        2558212
10  feet           Y    =          731197
69  meter
 Z    =      -16655027
07                 Z    =        -5097541
89
 XDOT =       1465
070429                 XDOT =         538
152105
 YDOT =     -24685
406102  feet/sec       YDOT =       -7518
606010  meter/sec
 ZDOT =      -5062
487992                 ZDOT =       -1540
654427

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11489629
18                 X    =        -3502038
97
 Y    =        8683228
92  feet           Y    =         2646648
17  meter
 Z    =      -16737317
43                 Z    =        -5101534
35
 XDOT =      -9182
460877                 XDOT =       -2798
814075
 YDOT =     -21861
457010  feet/sec       YDOT =       -6663
372097  meter/sec
 ZDOT =      -5053
663980                 ZDOT =       -1540
356781


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   09102
53732427  
00010596  00000-0  82463-4 0  9117
2 25544  51
6384 283
4296 0009001 229
5289 130
5089 15
72095101 35623


Satellite: ISS
Catalog Number: 25544
Epoch time:      09102
53732427   =   yrday
fracday
Element set:     911
Inclination:       51
6384  deg
RA of node:       283
4296  deg
Eccentricity:     
0009001     
Arg of perigee:   229
5289  deg
Mean anomaly:     130
5089  deg
Mean motion:   15
72095101  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3562
Checksum:              300

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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