Date: March 5th 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 2916)
---------------------------------------

Vector Time (GMT): 2009/061/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3220490
26                 A    =         6738696
51  meter
 Y    =        5635011
66  meter          E    =           
0015484
 Z    =       -1806968
77                 I    =           51
89921
 XDOT =      -5058
454575                 Wp   =           61
99094
 YDOT =      -1079
108030  meter/sec      RA   =          132
35812  deg
 ZDOT =       5694
260166                 TA   =          278
08169
                                          MA   =          278
25733
                                          Ha   =            197
738  n
mi
                                          Hp   =            184
750

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10565912
94                 X    =        -3274484
65
 Y    =       18487571
06  feet           Y    =         5598696
30  meter
 Z    =       -5928375
22                 Z    =        -1822745
21
 XDOT =     -16595
979578                 XDOT =       -5073
673439
 YDOT =      -3540
380675  feet/sec       YDOT =       -1135
759498  meter/sec
 ZDOT =      18681
955926                 ZDOT =        5669
649360

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14373771
90                 X    =        -4381125
67
 Y    =       15687427
81  feet           Y    =         4781528
00  meter
 Z    =       -5989467
67                 Z    =        -1825589
75
 XDOT =     -14356
537651                 XDOT =       -4375
872676
 YDOT =      -6112
757090  feet/sec       YDOT =       -1863
168361  meter/sec
 ZDOT =      18585
820403                 ZDOT =        5664
958059


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   09061
52440963  
00010596  00000-0  82463-4 0  9009
2 25544  51
6398 133
2909 0009235  79
9705 280
2498 15
71202711 29176


Satellite: ISS
Catalog Number: 25544
Epoch time:      09061
52440963   =   yrday
fracday
Element set:     900
Inclination:       51
6398  deg
RA of node:       133
2909  deg
Eccentricity:     
0009235     
Arg of perigee:    79
9705  deg
Mean anomaly:     280
2498  deg
Mean motion:   15
71202711  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2917
Checksum:              315


Coasting Arc #2 (Orbit 2932)
---------------------------------------

Vector Time (GMT): 2009/062/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4890588
00                 A    =         6730949
35  meter
 Y    =        -437106
07  meter          E    =           
0019567
 Z    =       -4622442
51                 I    =           51
89217
 XDOT =      -2200
095294                 Wp   =           77
00081
 YDOT =       6732
927818  meter/sec      RA   =          127
29955  deg
 ZDOT =      -2970
604484                 TA   =          163
59072
                                          MA   =          163
52729
                                          Ha   =            197
761  n
mi
                                          Hp   =            184
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16045236
23                 X    =         4917567
17
 Y    =       -1434075
04  feet           Y    =         -382265
88  meter
 Z    =      -15165493
80                 Z    =        -4598618
64
 XDOT =      -7218
160415                 XDOT =       -2260
789922
 YDOT =      22089
658195  feet/sec       YDOT =        6707
985671  meter/sec
 ZDOT =      -9746
077702                 ZDOT =       -2981
439998

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16083474
15                 X    =         4902242
92
 Y    =        1907493
94  feet           Y    =          581404
15  meter
 Z    =      -15072548
06                 Z    =        -4594112
65
 XDOT =     -11404
008103                 XDOT =       -3475
941670
 YDOT =      18976
526730  feet/sec       YDOT =        5784
045347  meter/sec
 ZDOT =      -9787
809185                 ZDOT =       -2983
324240


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   09062
54202856  
00010596  00000-0  82463-4 0  9010
2 25544  51
6398 128
0855 0009337  84
3669 275
8557 15
71233233 29337


Satellite: ISS
Catalog Number: 25544
Epoch time:      09062
54202856   =   yrday
fracday
Element set:     901
Inclination:       51
6398  deg
RA of node:       128
0855  deg
Eccentricity:     
0009337     
Arg of perigee:    84
3669  deg
Mean anomaly:     275
8557  deg
Mean motion:   15
71233233  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2933
Checksum:              327


Coasting Arc #3 (Orbit 2948)
---------------------------------------

Vector Time (GMT): 2009/063/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         572837
15                 A    =         6735037
76  meter
 Y    =       -5814733
56  meter          E    =           
0021956
 Z    =        3331336
96                 I    =           51
92405
 XDOT =       5707
006474                 Wp   =           89
31641
 YDOT =      -2149
681069  meter/sec      RA   =          122
15661  deg
 ZDOT =      -4706
777369                 TA   =           51
69238
                                          MA   =           51
49515
                                          Ha   =            197
653  n
mi
                                          Hp   =            184
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1879386
96                 X    =          621633
02
 Y    =      -19077209
83  feet           Y    =        -5808054
93  meter
 Z    =       10929583
21                 Z    =         3334238
29
 XDOT =      18723
774520                 XDOT =        5753
484847
 YDOT =      -7052
759413  feet/sec       YDOT =       -2085
602117  meter/sec
 ZDOT =     -15442
182969                 ZDOT =       -4678
940128

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5377489
72                 X    =         1639058
87
 Y    =      -18393405
01  feet           Y    =        -5606309
85  meter
 Z    =       10940433
08                 Z    =         3334644
00
 XDOT =      18463
211711                 XDOT =        5627
586930
 YDOT =      -3774
785901  feet/sec       YDOT =       -1150
554742  meter/sec
 ZDOT =     -15333
701205                 ZDOT =       -4673
712127


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   09063
55963109  
00010596  00000-0  82463-4 0  9028
2 25544  51
6402 122
8808 0009331  86
8357 273
3873 15
71303793 29498


Satellite: ISS
Catalog Number: 25544
Epoch time:      09063
55963109   =   yrday
fracday
Element set:     902
Inclination:       51
6402  deg
RA of node:       122
8808  deg
Eccentricity:     
0009331     
Arg of perigee:    86
8357  deg
Mean anomaly:     273
3873  deg
Mean motion:   15
71303793  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2949
Checksum:              326


Coasting Arc #4 (Orbit 2964)
---------------------------------------

Vector Time (GMT): 2009/064/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4735317
59                 A    =         6734739
88  meter
 Y    =        3272141
25  meter          E    =           
0021983
 Z    =        3478283
35                 I    =           51
93708
 XDOT =       -872
105623                 Wp   =           91
14786
 YDOT =      -6143
129284  meter/sec      RA   =          117
11293  deg
 ZDOT =       4566
693611                 TA   =          309
91602
                                          MA   =          310
10902
                                          Ha   =            197
853  n
mi
                                          Hp   =            184
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15535818
88                 X    =        -4788451
89
 Y    =       10735371
56  feet           Y    =         3218891
07  meter
 Z    =       11411690
79                 Z    =         3455150
50
 XDOT =      -2861
238920                 XDOT =        -825
531135
 YDOT =     -20154
623635  feet/sec       YDOT =       -6152
621287  meter/sec
 ZDOT =      14982
590587                 ZDOT =        4562
570087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17211156
60                 X    =        -5245960
53
 Y    =        7901447
79  feet           Y    =         2408361
29  meter
 Z    =       11321650
44                 Z    =         3450839
06
 XDOT =       1127
797562                 XDOT =         343
752697
 YDOT =     -19106
382035  feet/sec       YDOT =       -5823
625244  meter/sec
 ZDOT =      14965
997113                 ZDOT =        4561
635920


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   09064
57722191  
00010596  00000-0  82463-4 0  9036
2 25544  51
6399 117
6761 0009594  90
8255 269
4006 15
71288104 29656


Satellite: ISS
Catalog Number: 25544
Epoch time:      09064
57722191   =   yrday
fracday
Element set:     903
Inclination:       51
6399  deg
RA of node:       117
6761  deg
Eccentricity:     
0009594     
Arg of perigee:    90
8255  deg
Mean anomaly:     269
4006  deg
Mean motion:   15
71288104  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2965
Checksum:              332


Coasting Arc #5 (Orbit 2979)
---------------------------------------

Vector Time (GMT): 2009/065/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1960526
42                 A    =         6731057
65  meter
 Y    =        4602856
36  meter          E    =           
0019200
 Z    =       -4521231
32                 I    =           51
93841
 XDOT =      -4751
009999                 Wp   =          102
34756
 YDOT =       5134
052268  meter/sec      RA   =          111
97046  deg
 ZDOT =       3173
848834                 TA   =          199
26964
                                          MA   =          199
34234
                                          Ha   =            197
714  n
mi
                                          Hp   =            184
500

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6432173
30                 X    =         1930873
67
 Y    =       15101234
77  feet           Y    =         4624614
27  meter
 Z    =      -14833436
08                 Z    =        -4511779
34
 XDOT =     -15587
303147                 XDOT =       -4823
484382
 YDOT =      16844
003504  feet/sec       YDOT =        5080
518508  meter/sec
 ZDOT =      10412
889876                 ZDOT =        3150
592839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4106563
05                 X    =         1251680
42
 Y    =       15926726
81  feet           Y    =         4854466
33  meter
 Z    =      -14796164
50                 Z    =        -4509870
94
 XDOT =     -16900
183416                 XDOT =       -5151
175905
 YDOT =      13925
099921  feet/sec       YDOT =        4244
370456  meter/sec
 ZDOT =      10322
507127                 ZDOT =        3146
300172


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   09065
53119879  
00010596  00000-0  82463-4 0  9047
2 25544  51
6409 112
7966 0009537  93
6626 266
5627 15
71310163 29806


Satellite: ISS
Catalog Number: 25544
Epoch time:      09065
53119879   =   yrday
fracday
Element set:     904
Inclination:       51
6409  deg
RA of node:       112
7966  deg
Eccentricity:     
0009537     
Arg of perigee:    93
6626  deg
Mean anomaly:     266
5627  deg
Mean motion:   15
71310163  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2980
Checksum:              333


Coasting Arc #6 (Orbit 2995)
---------------------------------------

Vector Time (GMT): 2009/066/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3328740
65                 A    =         6737995
76  meter
 Y    =       -5495848
10  meter          E    =           
0015237
 Z    =       -2027144
87                 I    =           51
97207
 XDOT =       3340
570658                 Wp   =          115
02338
 YDOT =       4075
683405  meter/sec      RA   =          106
91802  deg
 ZDOT =      -5603
114983                 TA   =           87
43177
                                          MA   =           87
25734
                                          Ha   =            197
697  n
mi
                                          Hp   =            184
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10921065
13                 X    =         3399796
00
 Y    =      -18030997
70  feet           Y    =        -5458226
96  meter
 Z    =       -6650737
76                 Z    =        -2010801
48
 XDOT =      10959
877488                 XDOT =        3321
965663
 YDOT =      13371
664716  feet/sec       YDOT =        4112
935409  meter/sec
 ZDOT =     -18382
923171                 ZDOT =       -5586
932209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13334012
60                 X    =         4064207
04
 Y    =      -16353274
22  feet           Y    =        -4984477
98  meter
 Z    =       -6587365
53                 Z    =        -2007829
01
 XDOT =       7930
148571                 XDOT =        2417
109284
 YDOT =      13793
462515  feet/sec       YDOT =        4204
247375  meter/sec
 ZDOT =     -18319
410807                 ZDOT =       -5583
756414


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   09066
54876013  
00010596  00000-0  82463-4 0  9050
2 25544  51
6411 107
5912 0009582  97
6206 262
6045 15
71342492 29968


Satellite: ISS
Catalog Number: 25544
Epoch time:      09066
54876013   =   yrday
fracday
Element set:     905
Inclination:       51
6411  deg
RA of node:       107
5912  deg
Eccentricity:     
0009582     
Arg of perigee:    97
6206  deg
Mean anomaly:     262
6045  deg
Mean motion:   15
71342492  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2996
Checksum:              318


Coasting Arc #7 (Orbit 3011)
---------------------------------------

Vector Time (GMT): 2009/067/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3644510
81                 A    =         6728169
96  meter
 Y    =       -2297047
32  meter          E    =           
0013006
 Z    =        5157148
84                 I    =           51
94542
 XDOT =       2574
452186                 Wp   =           87
05751
 YDOT =      -7136
270518  meter/sec      RA   =          101
79596  deg
 ZDOT =      -1355
659080                 TA   =           15
87150
                                          MA   =           15
83078
                                          Ha   =            197
754  n
mi
                                          Hp   =            184
355

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11957056
47                 X    =        -3643605
84
 Y    =       -7536244
48  feet           Y    =        -2337796
99  meter
 Z    =       16919779
66                 Z    =         5139446
60
 XDOT =       8446
365441                 XDOT =        2660
645194
 YDOT =     -23412
961018  feet/sec       YDOT =       -7106
999647  meter/sec
 ZDOT =      -4447
700393                 ZDOT =       -1342
942920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11059467
16                 X    =        -3370925
59
 Y    =       -8932797
80  feet           Y    =        -2722716
77  meter
 Z    =       16850472
80                 Z    =         5136024
11
 XDOT =      10578
119970                 XDOT =        3224
210967
 YDOT =     -21416
044963  feet/sec       YDOT =       -6527
610505  meter/sec
 ZDOT =      -4398
619012                 ZDOT =       -1340
699075


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   09067
56630662  
00010596  00000-0  82463-4 0  9062
2 25544  51
6398 102
3863 0009623 101
0409 259
1836 15
71376343 30122


Satellite: ISS
Catalog Number: 25544
Epoch time:      09067
56630662   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       102
3863  deg
Eccentricity:     
0009623     
Arg of perigee:   101
0409  deg
Mean anomaly:     259
1836  deg
Mean motion:   15
71376343  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3012
Checksum:              304


Coasting Arc #8 (Orbit 3027)
---------------------------------------

Vector Time (GMT): 2009/068/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1030764
31                 A    =         6739572
71  meter
 Y    =        6647881
12  meter          E    =           
0019834
 Z    =         314761
61                 I    =           51
98907
 XDOT =      -4642
909018                 Wp   =           72
02136
 YDOT =      -1020
842216  meter/sec      RA   =           96
71787  deg
 ZDOT =       6052
319879                 TA   =          291
37940
                                          MA   =          291
59092
                                          Ha   =            197
583  n
mi
                                          Hp   =            184
389

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3381772
67                 X    =        -1106554
43
 Y    =       21810633
60  feet           Y    =         6635930
78  meter
 Z    =        1032682
45                 Z    =          309569
60
 XDOT =     -15232
641136                 XDOT =       -4660
549121
 YDOT =      -3349
219868  feet/sec       YDOT =       -1072
860030  meter/sec
 ZDOT =      19856
692517                 ZDOT =        6029
722394

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5623006
63                 X    =        -1713892
42
 Y    =       21343905
57  feet           Y    =         6505622
42  meter
 Z    =        1012940
57                 Z    =          308744
29
 XDOT =     -13362
548550                 XDOT =       -4072
904798
 YDOT =      -4506
743298  feet/sec       YDOT =       -1373
655357  meter/sec
 ZDOT =      19768
370196                 ZDOT =        6025
399236


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   09068
58383894  
00010596  00000-0  82463-4 0  9078
2 25544  51
6402  97
1813 0009594 104
5976 255
6250 15
71390761 30286


Satellite: ISS
Catalog Number: 25544
Epoch time:      09068
58383894   =   yrday
fracday
Element set:     907
Inclination:       51
6402  deg
RA of node:        97
1813  deg
Eccentricity:     
0009594     
Arg of perigee:   104
5976  deg
Mean anomaly:     255
6250  deg
Mean motion:   15
71390761  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3028
Checksum:              334


Coasting Arc #9 (Orbit 3042)
---------------------------------------

Vector Time (GMT): 2009/069/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4153669
78                 A    =         6727681
55  meter
 Y    =        -533897
86  meter          E    =           
0023914
 Z    =       -5285561
64                 I    =           51
95083
 XDOT =        242
141900                 Wp   =           94
36167
 YDOT =       7652
871667  meter/sec      RA   =           91
62640  deg
 ZDOT =       -586
773796                 TA   =          170
09365
                                          MA   =          170
04642
                                          Ha   =            197
536  n
mi
                                          Hp   =            184
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13627525
51                 X    =         4185007
04
 Y    =       -1751633
39  feet           Y    =         -487274
45  meter
 Z    =      -17341081
50                 Z    =        -5265307
31
 XDOT =        794
428805                 XDOT =         159
398606
 YDOT =      25107
846676  feet/sec       YDOT =        7655
116734  meter/sec
 ZDOT =      -1925
110878                 ZDOT =        -585
799288

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13827405
59                 X    =         4214593
22
 Y    =        -562022
49  feet           Y    =         -171304
46  meter
 Z    =      -17262032
44                 Z    =        -5261467
49
 XDOT =      -1402
596492                 XDOT =        -427
511411
 YDOT =      24075
510577  feet/sec       YDOT =        7338
215624  meter/sec
 ZDOT =      -1920
695607                 ZDOT =        -585
428021


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   09069
53776179  
00010596  00000-0  82463-4 0  9087
2 25544  51
6399  92
3006 0009522 108
3529 251
8669 15
71387135 30439


Satellite: ISS
Catalog Number: 25544
Epoch time:      09069
53776179   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:        92
3006  deg
Eccentricity:     
0009522     
Arg of perigee:   108
3529  deg
Mean anomaly:     251
8669  deg
Mean motion:   15
71387135  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3043
Checksum:              336


Coasting Arc #10 (Orbit 3058)
---------------------------------------

Vector Time (GMT): 2009/070/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1433549
38                 A    =         6738742
88  meter
 Y    =       -6437858
84  meter          E    =           
0023521
 Z    =        1329985
34                 I    =           51
98681
 XDOT =       4463
164325                 Wp   =          116
60416
 YDOT =      -2221
168439  meter/sec      RA   =           86
51529  deg
 ZDOT =      -5872
041608                 TA   =           48
86550
                                          MA   =           48
66273
                                          Ha   =            197
506  n
mi
                                          Hp   =            184
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4703246
01                 X    =        -1367914
38
 Y    =      -21121584
13  feet           Y    =        -6453522
49  meter
 Z    =        4363468
97                 Z    =         1323181
41
 XDOT =      14642
927575                 XDOT =        4516
195052
 YDOT =      -7287
298029  feet/sec       YDOT =       -2170
962898  meter/sec
 ZDOT =     -19265
228374                 ZDOT =       -5850
230767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3258773
93                 X    =         -993274
29
 Y    =      -21397611
90  feet           Y    =        -6521992
11  meter
 Z    =        4336392
33                 Z    =         1321732
38
 XDOT =      13661
615270                 XDOT =        4164
060334
 YDOT =      -6013
750441  feet/sec       YDOT =       -1832
991134  meter/sec
 ZDOT =     -19180
234267                 ZDOT =       -5846
135405


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   09070
55526499  
00010596  00000-0  82463-4 0  9090
2 25544  51
6386  87
0942 0009641 111
3038 248
9154 15
71432642 30593


Satellite: ISS
Catalog Number: 25544
Epoch time:      09070
55526499   =   yrday
fracday
Element set:     909
Inclination:       51
6386  deg
RA of node:        87
0942  deg
Eccentricity:     
0009641     
Arg of perigee:   111
3038  deg
Mean anomaly:     248
9154  deg
Mean motion:   15
71432642  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3059
Checksum:              323


Coasting Arc #11 (Orbit 3074)
---------------------------------------

Vector Time (GMT): 2009/071/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3341325
09                 A    =         6729358
39  meter
 Y    =        3255696
38  meter          E    =           
0016521
 Z    =        4840083
47                 I    =           51
95172
 XDOT =      -2943
909178                 Wp   =          117
31194
 YDOT =      -6684
682779  meter/sec      RA   =           81
45343  deg
 ZDOT =       2450
395691                 TA   =          308
79308
                                          MA   =          308
94052
                                          Ha   =            197
498  n
mi
                                          Hp   =            184
469

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10962352
65                 X    =        -3400994
58
 Y    =       10681418
57  feet           Y    =         3217998
64  meter
 Z    =       15879538
95                 Z    =         4823706
13
 XDOT =      -9658
494678                 XDOT =       -2880
844641
 YDOT =     -21931
373946  feet/sec       YDOT =       -6717
250402  meter/sec
 ZDOT =       8039
355940                 ZDOT =        2436
248209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11593138
63                 X    =        -3533588
65
 Y    =       10093758
54  feet           Y    =         3076577
60  meter
 Z    =       15815840
50                 Z    =         4820668
19
 XDOT =      -7818
012082                 XDOT =       -2382
930083
 YDOT =     -21559
820246  feet/sec       YDOT =       -6571
433211  meter/sec
 ZDOT =       7983
592629                 ZDOT =        2433
399033


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   09071
57275277  
00010596  00000-0  82463-4 0  9100
2 25544  51
6380  81
8881 0009521 115
0993 245
1149 15
71443499 30752


Satellite: ISS
Catalog Number: 25544
Epoch time:      09071
57275277   =   yrday
fracday
Element set:     910
Inclination:       51
6380  deg
RA of node:        81
8881  deg
Eccentricity:     
0009521     
Arg of perigee:   115
0993  deg
Mean anomaly:     245
1149  deg
Mean motion:   15
71443499  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3075
Checksum:              322


Coasting Arc #12 (Orbit 3089)
---------------------------------------

Vector Time (GMT): 2009/072/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3528746
86                 A    =         6735838
96  meter
 Y    =        4970202
68  meter          E    =           
0012786
 Z    =       -2880398
24                 I    =           51
96849
 XDOT =      -2882
805307                 Wp   =          100
86714
 YDOT =       4986
325610  meter/sec      RA   =           76
31768  deg
 ZDOT =       5088
978690                 TA   =          226
28463
                                          MA   =          226
39060
                                          Ha   =            197
351  n
mi
                                          Hp   =            184
525

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11577253
49                 X    =         3486899
38
 Y    =       16306439
25  feet           Y    =         5009428
92  meter
 Z    =       -9450125
45                 Z    =        -2863357
77
 XDOT =      -9458
022662                 XDOT =       -2963
070246
 YDOT =      16359
335991  feet/sec       YDOT =        4953
640114  meter/sec
 ZDOT =      16696
124310                 ZDOT =        5074
778613

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11059032
15                 X    =         3370793
00
 Y    =       16700026
03  feet           Y    =         5090167
93  meter
 Z    =       -9383206
75                 Z    =        -2860001
42
 XDOT =      -8898
285062                 XDOT =       -2712
197287
 YDOT =      15211
772749  feet/sec       YDOT =        4636
548334  meter/sec
 ZDOT =      16641
054732                 ZDOT =        5072
193482


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   09072
52663349  
00010596  00000-0  82463-4 0  9118
2 25544  51
6383  77
0082 0009553 118
2504 241
9623 15
71469838 30906


Satellite: ISS
Catalog Number: 25544
Epoch time:      09072
52663349   =   yrday
fracday
Element set:     911
Inclination:       51
6383  deg
RA of node:        77
0082  deg
Eccentricity:     
0009553     
Arg of perigee:   118
2504  deg
Mean anomaly:     241
9623  deg
Mean motion:   15
71469838  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3090
Checksum:              314

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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