Date: January 14th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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


014/18:07:10 671 6 6 9 7 9 7
N/A 5 3 0 0 193 5
000/00:02:17 342 4 8 -0 0 192 8

Coasting Arc #1 (Orbit 2068)
---------------------------------------

Vector Time (GMT): 2009/007/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3251511
52                 A    =         6736551
95  meter
 Y    =        5663570
69  meter          E    =           
0013855
 Z    =        1641560
75                 I    =           51
90608
 XDOT =      -4971
069374                 Wp   =           90
50386
 YDOT =       1173
525565  meter/sec      RA   =           48
77478  deg
 ZDOT =       5755
934399                 TA   =          287
54095
                                          MA   =          287
69229
                                          Ha   =            194
548  n
mi
                                          Hp   =            185
967

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10667688
71                 X    =         3179964
46
 Y    =       18581268
67  feet           Y    =         5699530
71  meter
 Z    =        5385698
01                 Z    =         1657183
63
 XDOT =     -16309
282724                 XDOT =       -5011
783808
 YDOT =       3850
149492  feet/sec       YDOT =        1117
707739  meter/sec
 ZDOT =      18884
299210                 ZDOT =        5731
686161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12664516
74                 X    =        -3860144
70
 Y    =       17262989
49  feet           Y    =         5261759
20  meter
 Z    =        5446841
34                 Z    =         1660197
24
 XDOT =      -8924
010614                 XDOT =       -2720
038435
 YDOT =     -12518
166473  feet/sec       YDOT =       -3815
537141  meter/sec
 ZDOT =      18789
998048                 ZDOT =        5727
191405


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   09007
58116526  
00010596  00000-0  82463-4 0  9000
2 25544  51
6413  49
0351 0006508 169
5856 190
5442 15
72045418 20692


Satellite: ISS
Catalog Number: 25544
Epoch time:      09007
58116526   =   yrday
fracday
Element set:     900
Inclination:       51
6413  deg
RA of node:        49
0351  deg
Eccentricity:     
0006508     
Arg of perigee:   169
5856  deg
Mean anomaly:     190
5442  deg
Mean motion:   15
72045418  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2069
Checksum:              302


Coasting Arc #2 (Orbit 2083)
---------------------------------------

Vector Time (GMT): 2009/008/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3789018
76                 A    =         6726088
40  meter
 Y    =       -2020670
83  meter          E    =           
0017130
 Z    =       -5191032
40                 I    =           51
85173
 XDOT =       4796
509089                 Wp   =          120
88643
 YDOT =       5883
148210  meter/sec      RA   =           43
64513  deg
 ZDOT =       1205
293775                 TA   =          160
64882
                                          MA   =          160
58370
                                          Ha   =            194
397  n
mi
                                          Hp   =            186
212

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12431163
90                 X    =         3836549
64
 Y    =       -6629497
47  feet           Y    =        -1978033
22  meter
 Z    =      -17030946
20                 Z    =        -5172510
28
 XDOT =      15736
578375                 XDOT =        4724
511190
 YDOT =      19301
667357  feet/sec       YDOT =        5936
382795  meter/sec
 ZDOT =       3954
375903                 ZDOT =        1228
421229

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11293539
06                 X    =         3442270
70
 Y    =        8566585
11  feet           Y    =         2611095
14  meter
 Z    =      -16958973
92                 Z    =        -5169095
25
 XDOT =     -10253
990068                 XDOT =       -3125
416173
 YDOT =      21562
302997  feet/sec       YDOT =        6572
189954  meter/sec
 ZDOT =       4044
737616                 ZDOT =        1232
836025


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   09008
53466622  
00010596  00000-0  82463-4 0  9012
2 25544  51
6424  44
1524 0006559 174
7184 185
4048 15
72080415 20848


Satellite: ISS
Catalog Number: 25544
Epoch time:      09008
53466622   =   yrday
fracday
Element set:     901
Inclination:       51
6424  deg
RA of node:        44
1524  deg
Eccentricity:     
0006559     
Arg of perigee:   174
7184  deg
Mean anomaly:     185
4048  deg
Mean motion:   15
72080415  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2084
Checksum:              300


Coasting Arc #3 (Orbit 2099)
---------------------------------------

Vector Time (GMT): 2009/009/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5016957
20                 A    =         6737447
11  meter
 Y    =       -4459129
82  meter          E    =           
0016837
 Z    =        -458954
23                 I    =           51
86709
 XDOT =       3470
400010                 Wp   =          152
44502
 YDOT =      -3293
755517  meter/sec      RA   =           38
55411  deg
 ZDOT =      -6036
370388                 TA   =           32
53025
                                          MA   =           32
42662
                                          Ha   =            194
260  n
mi
                                          Hp   =            186
157

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16459833
34                 X    =        -4964492
11
 Y    =      -14629691
02  feet           Y    =        -4514938
92  meter
 Z    =       -1505755
36                 Z    =         -483199
70
 XDOT =      11385
826804                 XDOT =        3536
296688
 YDOT =     -10806
284504  feet/sec       YDOT =       -3254
577999  meter/sec
 ZDOT =     -19804
364790                 ZDOT =       -6019
351865

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5967632
61                 X    =         1818934
42
 Y    =      -21190738
29  feet           Y    =        -6458937
03  meter
 Z    =       -1600388
63                 Z    =         -487798
45
 XDOT =      13200
759257                 XDOT =        4023
591421
 YDOT =       5184
431469  feet/sec       YDOT =        1580
214712  meter/sec
 ZDOT =     -19738
311479                 ZDOT =       -6016
237339


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   09009
55171987  
00010596  00000-0  82463-4 0  9023
2 25544  51
6413  38
9438 0006584 177
3254 182
7945 15
72114852 21004


Satellite: ISS
Catalog Number: 25544
Epoch time:      09009
55171987   =   yrday
fracday
Element set:     902
Inclination:       51
6413  deg
RA of node:        38
9438  deg
Eccentricity:     
0006584     
Arg of perigee:   177
3254  deg
Mean anomaly:     182
7945  deg
Mean motion:   15
72114852  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2100
Checksum:              317


Coasting Arc #4 (Orbit 2115)
---------------------------------------

Vector Time (GMT): 2009/010/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2120977
64                 A    =         6725376
40  meter
 Y    =        3579861
76  meter          E    =           
0007147
 Z    =        5281791
19                 I    =           51
80210
 XDOT =      -6500
000254                 Wp   =          160
83357
 YDOT =      -4124
522069  meter/sec      RA   =           33
44312  deg
 ZDOT =        178
644986                 TA   =          287
43569
                                          MA   =          287
51382
                                          Ha   =            194
138  n
mi
                                          Hp   =            186
258

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6958588
07                 X    =        -2186508
13
 Y    =       11744953
30  feet           Y    =         3555776
49  meter
 Z    =       17328711
25                 Z    =         5271329
08
 XDOT =     -21325
460152                 XDOT =       -6454
263887
 YDOT =     -13531
896552  feet/sec       YDOT =       -4196
953141  meter/sec
 ZDOT =        586
105598                 ZDOT =         147
178962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13667800
60                 X    =        -4165945
62
 Y    =        -979683
44  feet           Y    =         -298607
51  meter
 Z    =       17288191
24                 Z    =         5269440
69
 XDOT =       2344
694396                 XDOT =         714
662852
 YDOT =     -24146
489790  feet/sec       YDOT =       -7359
850088  meter/sec
 ZDOT =        463
377185                 ZDOT =         141
237366


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   09010
56875692  
00010596  00000-0  82463-4 0  9031
2 25544  51
6404  33
7349 0006472 180
9289 179
1862 15
72150365 21166


Satellite: ISS
Catalog Number: 25544
Epoch time:      09010
56875692   =   yrday
fracday
Element set:     903
Inclination:       51
6404  deg
RA of node:        33
7349  deg
Eccentricity:     
0006472     
Arg of perigee:   180
9289  deg
Mean anomaly:     179
1862  deg
Mean motion:   15
72150365  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2116
Checksum:              317


Coasting Arc #5 (Orbit 2130)
---------------------------------------

Vector Time (GMT): 2009/011/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6150407
87                 A    =         6737014
89  meter
 Y    =        2643497
22  meter          E    =           
0006476
 Z    =        -751834
72                 I    =           51
81713
 XDOT =      -1276
518353                 Wp   =           75
50677
 YDOT =       4659
798780  meter/sec      RA   =           28
32556  deg
 ZDOT =       5985
903524                 TA   =          276
33054
                                          MA   =          276
40430
                                          Ha   =            193
919  n
mi
                                          Hp   =            186
295

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20178503
51                 X    =         6124042
93
 Y    =        8672891
13  feet           Y    =         2712127
33  meter
 Z    =       -2466649
34                 Z    =         -722020
43
 XDOT =      -4188
052338                 XDOT =       -1357
607848
 YDOT =      15288
053741  feet/sec       YDOT =        4645
069782  meter/sec
 ZDOT =      19638
791090                 ZDOT =        5979
506036

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1779929
81                 X    =          542522
61
 Y    =       21903943
52  feet           Y    =         6676321
98  meter
 Z    =       -2350428
03                 Z    =         -716410
46
 XDOT =     -13927
229798                 XDOT =       -4245
019642
 YDOT =       3220
065792  feet/sec       YDOT =         981
476053  meter/sec
 ZDOT =      19614
155936                 ZDOT =        5978
394729


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   09011
52221458  
00010596  00000-0  82463-4 0  9044
2 25544  51
6409  28
8523 0006587 184
4305 175
6800 15
72220337 21312


Satellite: ISS
Catalog Number: 25544
Epoch time:      09011
52221458   =   yrday
fracday
Element set:     904
Inclination:       51
6409  deg
RA of node:        28
8523  deg
Eccentricity:     
0006587     
Arg of perigee:   184
4305  deg
Mean anomaly:     175
6800  deg
Mean motion:   15
72220337  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2131
Checksum:              286


Coasting Arc #6 (Orbit 2146)
---------------------------------------

Vector Time (GMT): 2009/012/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          61205
54                 A    =         6725974
80  meter
 Y    =       -4368910
29  meter          E    =           
0013203
 Z    =       -5123592
03                 I    =           51
75226
 XDOT =       7310
869488                 Wp   =          105
56196
 YDOT =       1852
495860  meter/sec      RA   =           23
23247  deg
 ZDOT =      -1498
955394                 TA   =          150
10362
                                          MA   =          150
02814
                                          Ha   =            193
794  n
mi
                                          Hp   =            186
522

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         200805
58                 X    =          134943
68
 Y    =      -14333695
18  feet           Y    =        -4367813
02  meter
 Z    =      -16809685
14                 Z    =        -5123116
06
 XDOT =      23985
792284                 XDOT =        7296
892678
 YDOT =       6077
742324  feet/sec       YDOT =        1934
172250  meter/sec
 ZDOT =      -4917
832659                 ZDOT =       -1463
473887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12695530
64                 X    =         3869597
74
 Y    =       -6661254
68  feet           Y    =        -2030350
43  meter
 Z    =      -16808088
61                 Z    =        -5123105
41
 XDOT =       5788
574789                 XDOT =        1764
357596
 YDOT =      23037
338344  feet/sec       YDOT =        7021
780727  meter/sec
 ZDOT =      -4779
588256                 ZDOT =       -1456
818501


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   09012
53922041  
00010596  00000-0  82463-4 0  9053
2 25544  51
6400  23
6425 0006381 188
9109 171
1941 15
72186037 21472


Satellite: ISS
Catalog Number: 25544
Epoch time:      09012
53922041   =   yrday
fracday
Element set:     905
Inclination:       51
6400  deg
RA of node:        23
6425  deg
Eccentricity:     
0006381     
Arg of perigee:   188
9109  deg
Mean anomaly:     171
1941  deg
Mean motion:   15
72186037  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2147
Checksum:              285


Coasting Arc #7 (Orbit 2162)
---------------------------------------

Vector Time (GMT): 2009/013/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6439163
77                 A    =         6735755
99  meter
 Y    =        -562162
95  meter          E    =           
0016477
 Z    =        1858816
57                 I    =           51
75765
 XDOT =      -1196
040952                 Wp   =          135
23714
 YDOT =      -5085
402601  meter/sec      RA   =           18
08925  deg
 ZDOT =      -5662
440855                 TA   =           24
15959
                                          MA   =           24
08240
                                          Ha   =            193
594  n
mi
                                          Hp   =            186
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21125865
38                 X    =        -6441428
56
 Y    =       -1844366
63  feet           Y    =         -634182
21  meter
 Z    =        6098479
58                 Z    =         1827530
37
 XDOT =      -3924
018872                 XDOT =       -1111
579842
 YDOT =     -16684
391734  feet/sec       YDOT =       -5098
304764  meter/sec
 ZDOT =     -18577
561861                 ZDOT =       -5668
046294

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8936397
37                 X    =        -2723813
92
 Y    =      -19269558
26  feet           Y    =        -5873361
36  meter
 Z    =        5976642
52                 Z    =         1821680
64
 XDOT =      11163
902547                 XDOT =        3402
757496
 YDOT =     -10965
705382  feet/sec       YDOT =       -3342
347000  meter/sec
 ZDOT =     -18599
687157                 ZDOT =       -5669
184645


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   09013
55620955  
00010596  00000-0  82463-4 0  9066
2 25544  51
6397  18
4331 0006194 192
8879 167
2126 15
72239161 21631


Satellite: ISS
Catalog Number: 25544
Epoch time:      09013
55620955   =   yrday
fracday
Element set:     906
Inclination:       51
6397  deg
RA of node:        18
4331  deg
Eccentricity:     
0006194     
Arg of perigee:   192
8879  deg
Mean anomaly:     167
2126  deg
Mean motion:   15
72239161  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2163
Checksum:              317


Coasting Arc #8 (Orbit 2178)
---------------------------------------

Vector Time (GMT): 2009/014/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2130901
44                 A    =         6727503
65  meter
 Y    =        4307872
82  meter          E    =           
0010756
 Z    =        4707424
56                 I    =           51
70139
 XDOT =      -7175
923528                 Wp   =          152
57996
 YDOT =        554
083594  meter/sec      RA   =           13
01126  deg
 ZDOT =       2729
426581                 TA   =          270
49755
                                          MA   =          270
62080
                                          Ha   =            193
351  n
mi
                                          Hp   =            186
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6991146
47                 X    =         2059704
41
 Y    =       14133441
00  feet           Y    =         4331303
47  meter
 Z    =       15444306
30                 Z    =         4717603
53
 XDOT =     -23543
056195                 XDOT =       -7194
844823
 YDOT =       1817
859562  feet/sec       YDOT =         473
732324  meter/sec
 ZDOT =       8954
811619                 ZDOT =        2694
520780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8595359
46                 X    =        -2619865
56
 Y    =       13172564
15  feet           Y    =         4014997
55  meter
 Z    =       15484192
90                 Z    =         4719582
00
 XDOT =     -12697
997713                 XDOT =       -3870
349703
 YDOT =     -18697
778552  feet/sec       YDOT =       -5699
082903  meter/sec
 ZDOT =       8818
951275                 ZDOT =        2688
016349


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   09014
57318267  
00010596  00000-0  82463-4 0  9070
2 25544  51
6394  13
2240 0006242 197
7919 162
3026 15
72246459 21793


Satellite: ISS
Catalog Number: 25544
Epoch time:      09014
57318267   =   yrday
fracday
Element set:     907
Inclination:       51
6394  deg
RA of node:        13
2240  deg
Eccentricity:     
0006242     
Arg of perigee:   197
7919  deg
Mean anomaly:     162
3026  deg
Mean motion:   15
72246459  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2179
Checksum:              313


Coasting Arc #9 (Orbit 2181)
---------------------------------------

Vector Time (GMT): 2009/014/18:08:19
342
Vector Time (MET): N/A
Weight (LBS)     : 639553
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5185869
89                 A    =         6736196
04  meter
 Y    =       -1992404
45  meter          E    =           
0003079
 Z    =       -3809820
60                 I    =           51
70970
 XDOT =       4754
529509                 Wp   =          221
17743
 YDOT =       4364
853428  meter/sec      RA   =           11
76293  deg
 ZDOT =       4184
942339                 TA   =           92
72055
                                          MA   =           92
68530
                                          Ha   =            193
480  n
mi
                                          Hp   =            192
776

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17014008
82                 X    =         5226270
89
 Y    =       -6536760
00  feet           Y    =        -1934186
97  meter
 Z    =      -12499411
42                 Z    =        -3784530
13
 XDOT =      15598
850095                 XDOT =        4685
038367
 YDOT =      14320
385262  feet/sec       YDOT =        4417
632595  meter/sec
 ZDOT =      13730
125784                 ZDOT =        4207
870772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12570377
62                 X    =         3831451
10
 Y    =      -13290599
40  feet           Y    =        -4050974
70  meter
 Z    =      -12401072
02                 Z    =        -3779846
75
 XDOT =      19220
840252                 XDOT =        5858
512109
 YDOT =       5271
633591  feet/sec       YDOT =        1606
793919  meter/sec
 ZDOT =      13819
651159                 ZDOT =        4212
229673


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   09014
76386230  
00010596  00000-0  82463-4 0  9087
2 25544  51
6430  12
2481 0008028 264
0696  95
9550 15
70420874 21824


Satellite: ISS
Catalog Number: 25544
Epoch time:      09014
76386230   =   yrday
fracday
Element set:     908
Inclination:       51
6430  deg
RA of node:        12
2481  deg
Eccentricity:     
0008028     
Arg of perigee:   264
0696  deg
Mean anomaly:      95
9550  deg
Mean motion:   15
70420874  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2182
Checksum:              301


Coasting Arc #10 (Orbit 2197)
---------------------------------------

Vector Time (GMT): 2009/015/18:08:19
342
Vector Time (MET): N/A
Weight (LBS)     : 639553
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5469008
72                 A    =         6739056
51  meter
 Y    =       -2821834
00  meter          E    =           
0004915
 Z    =       -2738857
44                 I    =           51
69110
 XDOT =       4437
368167                 Wp   =          235
32191
 YDOT =      -3585
112023  meter/sec      RA   =            6
70775  deg
 ZDOT =      -5163
106620                 TA   =          335
88770
                                          MA   =          335
91070
                                          Ha   =            192
819  n
mi
                                          Hp   =            192
349

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17942942
00                 X    =        -5423743
39
 Y    =       -9257985
55  feet           Y    =        -2882738
43  meter
 Z    =       -8985752
75                 Z    =        -2765315
61
 XDOT =      14558
294511                 XDOT =        4502
208710
 YDOT =     -11762
178553  feet/sec       YDOT =       -3535
128054  meter/sec
 ZDOT =     -16939
326181                 ZDOT =       -5141
392886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20142772
47                 X    =        -6139517
05
 Y    =        -251758
40  feet           Y    =          -76735
96  meter
 Z    =       -9088924
66                 Z    =        -2770304
24
 XDOT =       7806
151690                 XDOT =        2379
315035
 YDOT =     -15616
809891  feet/sec       YDOT =       -4760
003655  meter/sec
 ZDOT =     -16855
010004                 ZDOT =       -5137
407049


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   09015
78200955  
00010596  00000-0  82463-4 0  9090
2 25544  51
6435   7
0474 0008149 267
6899  92
3330 15
70421279 21985


Satellite: ISS
Catalog Number: 25544
Epoch time:      09015
78200955   =   yrday
fracday
Element set:     909
Inclination:       51
6435  deg
RA of node:         7
0474  deg
Eccentricity:     
0008149     
Arg of perigee:   267
6899  deg
Mean anomaly:      92
3330  deg
Mean motion:   15
70421279  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2198
Checksum:              325


Coasting Arc #11 (Orbit 2213)
---------------------------------------

Vector Time (GMT): 2009/016/18:08:19
342
Vector Time (MET): N/A
Weight (LBS)     : 639553
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2259544
69                 A    =         6731374
81  meter
 Y    =        3900248
79  meter          E    =           
0004910
 Z    =        5003310
14                 I    =           51
63637
 XDOT =      -7244
663845                 Wp   =          316
92415
 YDOT =      -1722
926705  meter/sec      RA   =            1
56240  deg
 ZDOT =      -1926
273080                 TA   =          151
71535
                                          MA   =          151
68868
                                          Ha   =            192
865  n
mi
                                          Hp   =            192
353

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7413204
37                 X    =        -2327294
85
 Y    =       12796091
81  feet           Y    =         3874602
22  meter
 Z    =       16415059
50                 Z    =         4992169
01
 XDOT =     -23768
582167                 XDOT =       -7215
501987
 YDOT =      -5652
646670  feet/sec       YDOT =       -1803
777604  meter/sec
 ZDOT =      -6319
793569                 ZDOT =       -1961
396455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -717130
87                 X    =         -218581
49
 Y    =       14818759
25  feet           Y    =         4516757
82  meter
 Z    =       16371922
33                 Z    =         4990161
93
 XDOT =     -22566
314058                 XDOT =       -6878
212525
 YDOT =       6050
048295  feet/sec       YDOT =        1844
054720  meter/sec
 ZDOT =      -6456
628819                 ZDOT =       -1967
980464


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   09016
80014009  
00010596  00000-0  82463-4 0  9109
2 25544  51
6435   1
8465 0008163 272
4549  87
5677 15
70500627 22143


Satellite: ISS
Catalog Number: 25544
Epoch time:      09016
80014009   =   yrday
fracday
Element set:     910
Inclination:       51
6435  deg
RA of node:         1
8465  deg
Eccentricity:     
0008163     
Arg of perigee:   272
4549  deg
Mean anomaly:      87
5677  deg
Mean motion:   15
70500627  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2214
Checksum:              292


Coasting Arc #12 (Orbit 2229)
---------------------------------------

Vector Time (GMT): 2009/017/18:08:19
342
Vector Time (MET): N/A
Weight (LBS)     : 639553
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6712048
89                 A    =         6742029
09  meter
 Y    =          33253
85  meter          E    =           
0009404
 Z    =         563468
77                 I    =           51
64299
 XDOT =       -528
400879                 Wp   =           13
47171
 YDOT =       4790
216957  meter/sec      RA   =          356
47468  deg
 ZDOT =       6000
563809                 TA   =          352
65221
                                          MA   =          352
66599
                                          Ha   =            193
383  n
mi
                                          Hp   =            192
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22021157
77                 X    =         6708440
98
 Y    =         109100
55  feet           Y    =          108291
67  meter
 Z    =        1848650
83                 Z    =          596066
83
 XDOT =      -1733
598685                 XDOT =        -611
075969
 YDOT =      15715
934898  feet/sec       YDOT =        4783
845485  meter/sec
 ZDOT =      19686
889137                 ZDOT =        5997
796307

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19373915
96                 X    =         5905169
59
 Y    =      -10445543
58  feet           Y    =        -3183801
68  meter
 Z    =        1975551
07                 Z    =          602147
96
 XDOT =       5143
812945                 XDOT =        1567
834186
 YDOT =      13268
297982  feet/sec       YDOT =        4044
177225  meter/sec
 ZDOT =      19676
401507                 ZDOT =        5997
367179


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   09017
81825698  
00010596  00000-0  82463-4 0  9116
2 25544  51
6436 356
6449 0008123 276
3025  83
7211 15
70490133 22305


Satellite: ISS
Catalog Number: 25544
Epoch time:      09017
81825698   =   yrday
fracday
Element set:     911
Inclination:       51
6436  deg
RA of node:       356
6449  deg
Eccentricity:     
0008123     
Arg of perigee:   276
3025  deg
Mean anomaly:      83
7211  deg
Mean motion:   15
70490133  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2230
Checksum:              301


Coasting Arc #13 (Orbit 2244)
---------------------------------------

Vector Time (GMT): 2009/018/18:08:19
342
Vector Time (MET): N/A
Weight (LBS)     : 639553
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1354232
89                 A    =         6730124
19  meter
 Y    =       -4002563
29  meter          E    =           
0007263
 Z    =       -5244376
78                 I    =           51
57387
 XDOT =       7479
185828                 Wp   =           68
07721
 YDOT =      -1664
703197  meter/sec      RA   =          351
36339  deg
 ZDOT =       -658
864904                 TA   =          195
63322
                                          MA   =          195
65566
                                          Ha   =            193
677  n
mi
                                          Hp   =            192
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4443021
29                 X    =        -1283898
91
 Y    =      -13131769
32  feet           Y    =        -4017313
48  meter
 Z    =      -17205960
56                 Z    =        -5250785
03
 XDOT =      24538
011246                 XDOT =        7500
445563
 YDOT =      -5461
624661  feet/sec       YDOT =       -1580
947687  meter/sec
 ZDOT =      -2161
630261                 ZDOT =        -622
479810

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10263502
98                 X    =        -3128315
71
 Y    =       -9272382
70  feet           Y    =        -2826222
25  meter
 Z    =      -17231143
54                 Z    =        -5252052
55
 XDOT =      17971
908416                 XDOT =        5477
837685
 YDOT =     -16127
148645  feet/sec       YDOT =       -4915
554907  meter/sec
 ZDOT =      -2020
089671                 ZDOT =        -615
723332


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   09018
77272607  
00010596  00000-0  82463-4 0  9129
2 25544  51
6434 351
7689 0008148 280
1514  79
8728 15
70532885 22454


Satellite: ISS
Catalog Number: 25544
Epoch time:      09018
77272607   =   yrday
fracday
Element set:     912
Inclination:       51
6434  deg
RA of node:       351
7689  deg
Eccentricity:     
0008148     
Arg of perigee:   280
1514  deg
Mean anomaly:      79
8728  deg
Mean motion:   15
70532885  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2245
Checksum:              333

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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