Date: April 22nd 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 3686)
---------------------------------------

Vector Time (GMT): 2009/110/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4228443
05                 A    =         6735694
32  meter
 Y    =       -4936047
08  meter          E    =           
0006268
 Z    =       -1752852
47                 I    =           51
36280
 XDOT =       2784
619886                 Wp   =          318
72666
 YDOT =      -4400
657846  meter/sec      RA   =          241
86444  deg
 ZDOT =       5668
014631                 TA   =           21
80110
                                          MA   =           21
77444
                                          Ha   =            191
089  n
mi
                                          Hp   =            190
163

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13872844
66                 X    =        -4164418
00
 Y    =      -16194380
20  feet           Y    =        -4982974
08  meter
 Z    =       -5750828
30                 Z    =        -1773238
64
 XDOT =       9135
892013                 XDOT =        2806
087520
 YDOT =     -14437
853826  feet/sec       YDOT =       -4369
398382  meter/sec
 ZDOT =      18595
848528                 ZDOT =        5681
594658

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18620682
51                 X    =        -5675584
03
 Y    =      -10346851
82  feet           Y    =        -3153720
43  meter
 Z    =       -5830834
88                 Z    =        -1777238
47
 XDOT =       2667
754311                 XDOT =         813
131514
 YDOT =     -15322
714229  feet/sec       YDOT =       -4670
363297  meter/sec
 ZDOT =      18648
563779                 ZDOT =        5684
082240


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   09110
48264461  
00010596  00000-0  82463-4 0  9006
2 25544  51
6400 242
7464 0008829 262
3492  97
6668 15
72282945 36873


Satellite: ISS
Catalog Number: 25544
Epoch time:      09110
48264461   =   yrday
fracday
Element set:     900
Inclination:       51
6400  deg
RA of node:       242
7464  deg
Eccentricity:     
0008829     
Arg of perigee:   262
3492  deg
Mean anomaly:      97
6668  deg
Mean motion:   15
72282945  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3687
Checksum:              329


Coasting Arc #2 (Orbit 3702)
---------------------------------------

Vector Time (GMT): 2009/111/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1595487
99                 A    =         6727167
62  meter
 Y    =        4493347
74  meter          E    =           
0003765
 Z    =       -4748480
98                 I    =           51
34953
 XDOT =      -5533
374130                 Wp   =           33
09518
 YDOT =      -4687
257263  meter/sec      RA   =          236
75876  deg
 ZDOT =      -2574
054004                 TA   =          211
53248
                                          MA   =          211
55505
                                          Ha   =            190
694  n
mi
                                          Hp   =            190
399

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5234540
66                 X    =        -1622547
34
 Y    =       14741954
54  feet           Y    =         4475354
57  meter
 Z    =      -15579005
84                 Z    =        -4756297
84
 XDOT =     -18154
114601                 XDOT =       -5468
044790
 YDOT =     -15378
140626  feet/sec       YDOT =       -4748
769515  meter/sec
 ZDOT =      -8445
059067                 ZDOT =       -2600
776461

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         592011
89                 X    =          180445
22
 Y    =       15602355
65  feet           Y    =         4755598
00  meter
 Z    =      -15609198
65                 Z    =        -4757683
75
 XDOT =     -21331
465271                 XDOT =       -6501
830615
 YDOT =      -7751
195909  feet/sec       YDOT =       -2362
564513  meter/sec
 ZDOT =      -8549
806109                 ZDOT =       -2605
980902


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   09111
49957811  
00010596  00000-0  82463-4 0  9017
2 25544  51
6402 237
5376 0008872 267
0396  92
9751 15
72310078 37031


Satellite: ISS
Catalog Number: 25544
Epoch time:      09111
49957811   =   yrday
fracday
Element set:     901
Inclination:       51
6402  deg
RA of node:       237
5376  deg
Eccentricity:     
0008872     
Arg of perigee:   267
0396  deg
Mean anomaly:      92
9751  deg
Mean motion:   15
72310078  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3703
Checksum:              318


Coasting Arc #3 (Orbit 3718)
---------------------------------------

Vector Time (GMT): 2009/112/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5282179
84                 A    =         6733679
68  meter
 Y    =        3161915
67  meter          E    =           
0005123
 Z    =        2720890
78                 I    =           51
38931
 XDOT =       -743
721297                 Wp   =          118
43578
 YDOT =       5675
271176  meter/sec      RA   =          231
57311  deg
 ZDOT =      -5146
414311                 TA   =           30
41032
                                          MA   =           30
38062
                                          Ha   =            190
228  n
mi
                                          Hp   =            190
038

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17329986
35                 X    =         5233212
42
 Y    =       10373739
09  feet           Y    =         3220710
42  meter
 Z    =        8926807
02                 Z    =         2746432
86
 XDOT =      -2440
030501                 XDOT =        -782
127183
 YDOT =      18619
656088  feet/sec       YDOT =        5666
739493  meter/sec
 ZDOT =     -16884
561387                 ZDOT =       -5150
120885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19927269
33                 X    =         6073831
69
 Y    =        3008491
59  feet           Y    =          916988
24  meter
 Z    =        9026831
59                 Z    =         2751378
27
 XDOT =       5147
759818                 XDOT =        1569
037193
 YDOT =      16654
393043  feet/sec       YDOT =        5076
258999  meter/sec
 ZDOT =     -16898
604849                 ZDOT =       -5150
694758


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   09112
51649625  
00010596  00000-0  82463-4 0  9023
2 25544  51
6405 232
3277 0008835 270
6315  89
3835 15
72318841 37193


Satellite: ISS
Catalog Number: 25544
Epoch time:      09112
51649625   =   yrday
fracday
Element set:     902
Inclination:       51
6405  deg
RA of node:       232
3277  deg
Eccentricity:     
0008835     
Arg of perigee:   270
6315  deg
Mean anomaly:      89
3835  deg
Mean motion:   15
72318841  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3719
Checksum:              316


Coasting Arc #4 (Orbit 3734)
---------------------------------------

Vector Time (GMT): 2009/113/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -345274
41                 A    =         6729093
64  meter
 Y    =       -5241219
02  meter          E    =           
0002239
 Z    =        4206670
98                 I    =           51
39499
 XDOT =       6328
877563                 Wp   =          157
32733
 YDOT =       2481
115781  meter/sec      RA   =          226
48042  deg
 ZDOT =       3608
085911                 TA   =          255
79541
                                          MA   =          255
82028
                                          Ha   =            190
709  n
mi
                                          Hp   =            190
167

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1132790
08                 X    =         -307076
18
 Y    =      -17195600
47  feet           Y    =        -5244866
37  meter
 Z    =       13801413
98                 Z    =         4205086
56
 XDOT =      20764
034000                 XDOT =        6283
135183
 YDOT =       8140
143637  feet/sec       YDOT =        2551
633340  meter/sec
 ZDOT =      11837
552203                 ZDOT =        3638
720962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7937010
60                 X    =        -2419200
83
 Y    =      -15302212
37  feet           Y    =        -4664114
33  meter
 Z    =       13794820
63                 Z    =         4204661
33
 XDOT =      21110
382885                 XDOT =        6434
444703
 YDOT =       -162
186148  feet/sec       YDOT =         -49
434338  meter/sec
 ZDOT =      11957
425123                 ZDOT =        3644
623178


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   09113
53339633  
00010596  00000-0  82463-4 0  9032
2 25544  51
6418 227
1181 0008906 275
1416  84
8730 15
72388938 37350


Satellite: ISS
Catalog Number: 25544
Epoch time:      09113
53339633   =   yrday
fracday
Element set:     903
Inclination:       51
6418  deg
RA of node:       227
1181  deg
Eccentricity:     
0008906     
Arg of perigee:   275
1416  deg
Mean anomaly:      84
8730  deg
Mean motion:   15
72388938  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3735
Checksum:              322


Coasting Arc #5 (Orbit 3749)
---------------------------------------

Vector Time (GMT): 2009/114/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5598477
22                 A    =         6731253
78  meter
 Y    =       -1143951
27  meter          E    =           
0003542
 Z    =       -3554113
90                 I    =           51
42367
 XDOT =      -1573
402395                 Wp   =          283
09927
 YDOT =      -6090
795155  meter/sec      RA   =          221
29092  deg
 ZDOT =       4435
949224                 TA   =           34
40129
                                          MA   =           34
37836
                                          Ha   =            190
993  n
mi
                                          Hp   =            189
955

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18367707
41                 X    =        -5568003
64
 Y    =       -3753120
97  feet           Y    =        -1206386
36  meter
 Z    =      -11660478
69                 Z    =        -3581237
88
 XDOT =      -5162
081350                 XDOT =       -1526
726681
 YDOT =     -19982
923736  feet/sec       YDOT =       -6108
128833  meter/sec
 ZDOT =      14553
639186                 ZDOT =        4428
418909

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18218322
70                 X    =        -5552944
76
 Y    =        4131183
73  feet           Y    =         1259184
80  meter
 Z    =      -11766537
07                 Z    =        -3586440
50
 XDOT =     -12722
062018                 XDOT =       -3877
684503
 YDOT =     -14709
787190  feet/sec       YDOT =       -4483
543135  meter/sec
 ZDOT =      14523
752088                 ZDOT =        4426
839636


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   09114
48672843  
00010596  00000-0  82463-4 0  9041
2 25544  51
6419 222
2350 0008960 280
0532  79
9619 15
72362891 37507


Satellite: ISS
Catalog Number: 25544
Epoch time:      09114
48672843   =   yrday
fracday
Element set:     904
Inclination:       51
6419  deg
RA of node:       222
2350  deg
Eccentricity:     
0008960     
Arg of perigee:   280
0532  deg
Mean anomaly:      79
9619  deg
Mean motion:   15
72362891  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3750
Checksum:              318


Coasting Arc #6 (Orbit 3765)
---------------------------------------

Vector Time (GMT): 2009/115/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2384904
30                 A    =         6731408
12  meter
 Y    =        5219877
94  meter          E    =           
0004302
 Z    =       -3517559
52                 I    =           51
44765
 XDOT =      -6258
101643                 Wp   =          306
45570
 YDOT =       -160
938912  meter/sec      RA   =          216
20517  deg
 ZDOT =      -4475
510153                 TA   =          275
47479
                                          MA   =          275
52386
                                          Ha   =            191
248  n
mi
                                          Hp   =            189
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7824489
16                 X    =         2343445
57
 Y    =       17125583
78  feet           Y    =         5246315
58  meter
 Z    =      -11540549
59                 Z    =        -3506073
98
 XDOT =     -20531
829539                 XDOT =       -6234
095131
 YDOT =       -528
014804  feet/sec       YDOT =        -230
786347  meter/sec
 ZDOT =     -14683
432261                 ZDOT =       -4505
854437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14464009
88                 X    =         4408630
21
 Y    =       12097254
45  feet           Y    =         3687243
16  meter
 Z    =      -11495276
77                 Z    =        -3503760
36
 XDOT =     -17821
350828                 XDOT =       -5431
947732
 YDOT =       7222
819569  feet/sec       YDOT =        2201
515405  meter/sec
 ZDOT =     -14802
005247                 ZDOT =       -4511
651199


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   09115
50359990  
00010596  00000-0  82463-4 0  9051
2 25544  51
6422 217
0258 0008871 283
6294  76
3880 15
72399588 37666


Satellite: ISS
Catalog Number: 25544
Epoch time:      09115
50359990   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:       217
0258  deg
Eccentricity:     
0008871     
Arg of perigee:   283
6294  deg
Mean anomaly:      76
3880  deg
Mean motion:   15
72399588  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3766
Checksum:              347


Coasting Arc #7 (Orbit 3781)
---------------------------------------

Vector Time (GMT): 2009/116/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5170089
56                 A    =         6728814
22  meter
 Y    =        -822404
04  meter          E    =           
0005868
 Z    =        4229990
71                 I    =           51
46384
 XDOT =       3830
793778                 Wp   =           11
98822
 YDOT =       5631
348397  meter/sec      RA   =          211
01883  deg
 ZDOT =      -3580
776702                 TA   =          114
54916
                                          MA   =          114
48798
                                          Ha   =            191
429  n
mi
                                          Hp   =            189
326

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16962236
08                 X    =         5158352
55
 Y    =       -2698176
00  feet           Y    =         -764654
92  meter
 Z    =       13877922
29                 Z    =         4255079
04
 XDOT =      12568
221055                 XDOT =        3784
933547
 YDOT =      18475
552485  feet/sec       YDOT =        5673
930326  meter/sec
 ZDOT =     -11747
955058                 ZDOT =       -3562
277393

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13932177
29                 X    =         4246527
64
 Y    =       -9907730
84  feet           Y    =        -3019876
36  meter
 Z    =       13975894
94                 Z    =         4259852
78
 XDOT =      18798
711748                 XDOT =        5729
847341
 YDOT =       9935
410085  feet/sec       YDOT =        3028
312994  meter/sec
 ZDOT =     -11675
243962                 ZDOT =       -3558
614360


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   09116
52045630  
00010596  00000-0  82463-4 0  9068
2 25544  51
6420 211
8167 0008751 288
6983  71
3229 15
72416964 37820


Satellite: ISS
Catalog Number: 25544
Epoch time:      09116
52045630   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:       211
8167  deg
Eccentricity:     
0008751     
Arg of perigee:   288
6983  deg
Mean anomaly:      71
3229  deg
Mean motion:   15
72416964  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3782
Checksum:              318


Coasting Arc #8 (Orbit 3797)
---------------------------------------

Vector Time (GMT): 2009/117/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4232925
03                 A    =         6733390
37  meter
 Y    =       -4465408
35  meter          E    =           
0008028
 Z    =        2722006
06                 I    =           51
50532
 XDOT =       5374
400230                 Wp   =           40
95135
 YDOT =      -1948
477058  meter/sec      RA   =          205
93159  deg
 ZDOT =       5158
546788                 TA   =          350
17446
                                          MA   =          350
19015
                                          Ha   =            191
645  n
mi
                                          Hp   =            189
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13887549
30                 X    =        -4195900
75
 Y    =      -14650289
86  feet           Y    =        -4512536
58  meter
 Z    =        8930466
06                 Z    =         2701531
70
 XDOT =      17632
546686                 XDOT =        5370
729215
 YDOT =      -6392
641265  feet/sec       YDOT =       -1888
398295  meter/sec
 ZDOT =      16924
366101                 ZDOT =        5184
647067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19108468
37                 X    =        -5824261
16
 Y    =       -6617407
98  feet           Y    =        -2016985
95  meter
 Z    =        8850118
13                 Z    =         2697516
00
 XDOT =      12161
184654                 XDOT =        3706
729082
 YDOT =     -12334
315641  feet/sec       YDOT =       -3759
499407  meter/sec
 ZDOT =      17026
222102                 ZDOT =        5189
592497


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   09117
53729541  
00010596  00000-0  82463-4 0  9071
2 25544  51
6419 206
6067 0008833 292
8662  67
1567 15
72464841 37983


Satellite: ISS
Catalog Number: 25544
Epoch time:      09117
53729541   =   yrday
fracday
Element set:     907
Inclination:       51
6419  deg
RA of node:       206
6067  deg
Eccentricity:     
0008833     
Arg of perigee:   292
8662  deg
Mean anomaly:      67
1567  deg
Mean motion:   15
72464841  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3798
Checksum:              344


Coasting Arc #9 (Orbit 3812)
---------------------------------------

Vector Time (GMT): 2009/118/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4073376
56                 A    =         6726572
71  meter
 Y    =        2488493
52  meter          E    =           
0003126
 Z    =       -4741894
26                 I    =           51
50959
 XDOT =      -5740
442096                 Wp   =           82
99587
 YDOT =      -4404
762553  meter/sec      RA   =          200
75662  deg
 ZDOT =       2621
426362                 TA   =          212
79172
                                          MA   =          212
81112
                                          Ha   =            191
687  n
mi
                                          Hp   =            188
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13364096
32                 X    =        -4077864
99
 Y    =        8164348
81  feet           Y    =         2442917
98  meter
 Z    =      -15557395
88                 Z    =        -4761693
68
 XDOT =     -18833
471443                 XDOT =       -5703
495245
 YDOT =     -14451
320713  feet/sec       YDOT =       -4468
749182  meter/sec
 ZDOT =       8600
480191                 ZDOT =        2593
628255

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7814598
17                 X    =        -2381889
52
 Y    =       13482566
16  feet           Y    =         4109486
17  meter
 Z    =      -15634599
25                 Z    =        -4765425
85
 XDOT =     -22494
593516                 XDOT =       -6856
352104
 YDOT =      -3198
156749  feet/sec       YDOT =        -974
798177  meter/sec
 ZDOT =       8491
501382                 ZDOT =        2588
209621


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   09118
49056982  
00010596  00000-0  82463-4 0  9080
2 25544  51
6413 201
7236 0008837 297
1961  62
8300 15
72505574 38139


Satellite: ISS
Catalog Number: 25544
Epoch time:      09118
49056982   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:       201
7236  deg
Eccentricity:     
0008837     
Arg of perigee:   297
1961  deg
Mean anomaly:      62
8300  deg
Mean motion:   15
72505574  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3813
Checksum:              319


Coasting Arc #10 (Orbit 3828)
---------------------------------------

Vector Time (GMT): 2009/119/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5671907
74                 A    =         6735031
06  meter
 Y    =        3119218
67  meter          E    =           
0003291
 Z    =       -1855020
03                 I    =           51
56487
 XDOT =      -3816
183846                 Wp   =          249
87045
 YDOT =       3579
908662  meter/sec      RA   =          195
66275  deg
 ZDOT =      -5641
773974                 TA   =          310
72063
                                          MA   =          310
74921
                                          Ha   =            191
998  n
mi
                                          Hp   =            188
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18608621
20                 X    =         5645617
98
 Y    =       10233657
06  feet           Y    =         3182498
43  meter
 Z    =       -6086023
73                 Z    =        -1827529
26
 XDOT =     -12520
288209                 XDOT =       -3828
524430
 YDOT =      11745
107158  feet/sec       YDOT =        3537
165386  meter/sec
 ZDOT =     -18509
757134                 ZDOT =       -5660
342788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21266612
62                 X    =         6482063
53
 Y    =        -197514
63  feet           Y    =          -60202
46  meter
 Z    =       -5978325
87                 Z    =        -1822193
72
 XDOT =      -5093
070416                 XDOT =       -1552
367863
 YDOT =      14765
761316  feet/sec       YDOT =        4500
604049  meter/sec
 ZDOT =     -18582
079888                 ZDOT =       -5663
817950


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   09119
50738149  
00010596  00000-0  82463-4 0  9096
2 25544  51
6403 196
5137 0008892 301
1628  58
8662 15
72491010 38298


Satellite: ISS
Catalog Number: 25544
Epoch time:      09119
50738149   =   yrday
fracday
Element set:     909
Inclination:       51
6403  deg
RA of node:       196
5137  deg
Eccentricity:     
0008892     
Arg of perigee:   301
1628  deg
Mean anomaly:      58
8662  deg
Mean motion:   15
72491010  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3829
Checksum:              324


Coasting Arc #11 (Orbit 3844)
---------------------------------------

Vector Time (GMT): 2009/120/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2506451
43                 A    =         6725040
47  meter
 Y    =       -3634257
60  meter          E    =           
0008774
 Z    =        5077893
50                 I    =           51
56149
 XDOT =       7057
799051                 Wp   =          337
41646
 YDOT =       2608
087346  meter/sec      RA   =          190
50261  deg
 ZDOT =      -1610
078968                 TA   =          128
11752
                                          MA   =          128
03838
                                          Ha   =            192
098  n
mi
                                          Hp   =            188
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8223265
85                 X    =         2522236
46
 Y    =      -11923417
32  feet           Y    =        -3606141
14  meter
 Z    =       16659755
57                 Z    =         5090107
93
 XDOT =      23155
508699                 XDOT =        7035
931922
 YDOT =       8556
717016  feet/sec       YDOT =        2686
889632  meter/sec
 ZDOT =      -5282
411313                 ZDOT =       -1575
844989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1005861
84                 X    =          306586
69
 Y    =      -14394229
34  feet           Y    =        -4387361
10  meter
 Z    =       16707239
19                 Z    =         5092366
50
 XDOT =      23287
325758                 XDOT =        7097
976891
 YDOT =      -4375
097467  feet/sec       YDOT =       -1333
529708  meter/sec
 ZDOT =      -5148
371493                 ZDOT =       -1569
223631


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   09120
52417650  
00010596  00000-0  82463-4 0  9103
2 25544  51
6409 191
3029 0009066 305
4839  54
5477 15
72555079 38453


Satellite: ISS
Catalog Number: 25544
Epoch time:      09120
52417650   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:       191
3029  deg
Eccentricity:     
0009066     
Arg of perigee:   305
4839  deg
Mean anomaly:      54
5477  deg
Mean motion:   15
72555079  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3845
Checksum:              316


Coasting Arc #12 (Orbit 3860)
---------------------------------------

Vector Time (GMT): 2009/121/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6515966
54                 A    =         6736040
97  meter
 Y    =       -1372064
93  meter          E    =           
0014391
 Z    =         951022
38                 I    =           51
62696
 XDOT =       1826
949841                 Wp   =           17
77748
 YDOT =      -4551
912047  meter/sec      RA   =          185
39763  deg
 ZDOT =       5940
186603                 TA   =          352
61223
                                          MA   =          352
63341
                                          Ha   =            192
460  n
mi
                                          Hp   =            187
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21377842
99                 X    =        -6504759
50
 Y    =       -4501525
37  feet           Y    =        -1444867
66  meter
 Z    =        3120152
16                 Z    =          919394
95
 XDOT =       5993
929926                 XDOT =        1848
857941
 YDOT =     -14934
094641  feet/sec       YDOT =       -4531
359862  meter/sec
 ZDOT =      19488
801192                 ZDOT =        5949
114892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20624527
85                 X    =        -6286356
09
 Y    =        7256845
81  feet           Y    =         2211886
60  meter
 Z    =        2996379
65                 Z    =          913296
52
 XDOT =      -2194
808126                 XDOT =        -668
977517
 YDOT =     -14313
294535  feet/sec       YDOT =       -4362
692174  meter/sec
 ZDOT =      19523
369970                 ZDOT =        5950
723167


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   09121
54096071  
00010596  00000-0  82463-4 0  9117
2 25544  51
6405 186
0929 0009012 310
8837  49
1544 15
72518190 38614


Satellite: ISS
Catalog Number: 25544
Epoch time:      09121
54096071   =   yrday
fracday
Element set:     911
Inclination:       51
6405  deg
RA of node:       186
0929  deg
Eccentricity:     
0009012     
Arg of perigee:   310
8837  deg
Mean anomaly:      49
1544  deg
Mean motion:   15
72518190  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3861
Checksum:              301

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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