Date: February 20th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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 2697)
---------------------------------------

Vector Time (GMT): 2009/047/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3195758
48                 A    =         6735001
61  meter
 Y    =        4629514
92  meter          E    =           
0013348
 Z    =       -3719613
74                 I    =           51
50548
 XDOT =      -6320
120763                 Wp   =           50
54962
 YDOT =        936
016235  meter/sec      RA   =          203
65705  deg
 ZDOT =      -4266
897132                 TA   =          174
25596
                                          MA   =          174
24064
                                          Ha   =            197
444  n
mi
                                          Hp   =            186
434

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10484771
92                 X    =         3161821
93
 Y    =       15188697
24  feet           Y    =         4665062
01  meter
 Z    =      -12203457
17                 Z    =        -3704171
37
 XDOT =     -20735
304342                 XDOT =       -6309
390188
 YDOT =       3070
919407  feet/sec       YDOT =         865
400982  meter/sec
 ZDOT =     -13999
006337                 ZDOT =       -4297
573802

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8107069
07                 X    =         2471034
65
 Y    =       16624603
44  feet           Y    =         5067179
13  meter
 Z    =      -12142871
34                 Z    =        -3701147
18
 XDOT =     -19668
512905                 XDOT =       -5994
962733
 YDOT =       -716
442918  feet/sec       YDOT =        -218
371801  meter/sec
 ZDOT =     -14118
503761                 ZDOT =       -4303
319946


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   09047
59421421  
00010596  00000-0  82463-4 0  9008
2 25544  51
6390 204
5060 0008681  31
9070 328
2616 15
70932188 26983


Satellite: ISS
Catalog Number: 25544
Epoch time:      09047
59421421   =   yrday
fracday
Element set:     900
Inclination:       51
6390  deg
RA of node:       204
5060  deg
Eccentricity:     
0008681     
Arg of perigee:    31
9070  deg
Mean anomaly:     328
2616  deg
Mean motion:   15
70932188  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2698
Checksum:              301


Coasting Arc #2 (Orbit 2713)
---------------------------------------

Vector Time (GMT): 2009/048/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4681588
67                 A    =         6732606
75  meter
 Y    =       -2087338
49  meter          E    =           
0017383
 Z    =        4358898
91                 I    =           51
52536
 XDOT =       5197
888047                 Wp   =           54
01163
 YDOT =       4566
996406  meter/sec      RA   =          198
48655  deg
 ZDOT =      -3376
279126                 TA   =           70
14833
                                          MA   =           69
96106
                                          Ha   =            197
485  n
mi
                                          Hp   =            186
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15359542
90                 X    =         4683407
28
 Y    =       -6848223
38  feet           Y    =        -2034976
14  meter
 Z    =       14300849
44                 Z    =         4381646
10
 XDOT =      17053
438476                 XDOT =        5162
833918
 YDOT =      14983
584009  feet/sec       YDOT =        4624
926266  meter/sec
 ZDOT =     -11077
031253                 ZDOT =       -3351
113253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16065982
60                 X    =         4896911
50
 Y    =       -4707315
90  feet           Y    =        -1434789
89  meter
 Z    =       14389350
09                 Z    =         4385873
91
 XDOT =      14577
576074                 XDOT =        4443
245187
 YDOT =      16000
183681  feet/sec       YDOT =        4876
855986  meter/sec
 ZDOT =     -10978
538314                 ZDOT =       -3346
258478


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   09048
61202544  
00010596  00000-0  82463-4 0  9016
2 25544  51
6392 199
3028 0008767  36
4258 323
7497 15
70922763 27147


Satellite: ISS
Catalog Number: 25544
Epoch time:      09048
61202544   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:       199
3028  deg
Eccentricity:     
0008767     
Arg of perigee:    36
4258  deg
Mean anomaly:     323
7497  deg
Mean motion:   15
70922763  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2714
Checksum:              323


Coasting Arc #3 (Orbit 2729)
---------------------------------------

Vector Time (GMT): 2009/049/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5636084
78                 A    =         6738992
77  meter
 Y    =       -3032435
23  meter          E    =           
0022185
 Z    =        2070677
35                 I    =           51
57620
 XDOT =       3974
240338                 Wp   =           58
06296
 YDOT =      -3576
625433  meter/sec      RA   =          193
41046  deg
 ZDOT =       5547
730962                 TA   =          325
07343
                                          MA   =          325
21878
                                          Ha   =            197
585  n
mi
                                          Hp   =            186
040

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18491091
79                 X    =        -5611815
49
 Y    =       -9948934
49  feet           Y    =        -3095325
56  meter
 Z    =        6793560
86                 Z    =         2043356
64
 XDOT =      13038
846253                 XDOT =        3986
990008
 YDOT =     -11734
335410  feet/sec       YDOT =       -3532
111993  meter/sec
 ZDOT =      18201
217068                 ZDOT =        5567
068360

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17215541
54                 X    =        -5247297
06
 Y    =      -12081650
66  feet           Y    =        -3682487
12  meter
 Z    =        6686784
64                 Z    =         2038131
96
 XDOT =      13356
060663                 XDOT =        4070
927290
 YDOT =      -8857
630251  feet/sec       YDOT =       -2699
805701  meter/sec
 ZDOT =      18276
307157                 ZDOT =        5570
618422


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   09049
62982512  
00010596  00000-0  82463-4 0  9029
2 25544  51
6399 194
0994 0008825  39
6772 320
5034 15
70979633 27307


Satellite: ISS
Catalog Number: 25544
Epoch time:      09049
62982512   =   yrday
fracday
Element set:     902
Inclination:       51
6399  deg
RA of node:       194
0994  deg
Eccentricity:     
0008825     
Arg of perigee:    39
6772  deg
Mean anomaly:     320
5034  deg
Mean motion:   15
70979633  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2730
Checksum:              336


Coasting Arc #4 (Orbit 2744)
---------------------------------------

Vector Time (GMT): 2009/050/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2029632
37                 A    =         6729188
92  meter
 Y    =        3839305
62  meter          E    =           
0020470
 Z    =       -5156739
15                 I    =           51
57260
 XDOT =      -7272
438317                 Wp   =           78
62931
 YDOT =      -2102
744686  meter/sec      RA   =          188
26520  deg
 ZDOT =       1305
134941                 TA   =          203
84842
                                          MA   =          203
94340
                                          Ha   =            197
593  n
mi
                                          Hp   =            185
780

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6658898
86                 X    =        -2047363
32
 Y    =       12596147
06  feet           Y    =         3816510
05  meter
 Z    =      -16918435
54                 Z    =        -5166641
89
 XDOT =     -23859
705764                 XDOT =       -7254
724547
 YDOT =      -6898
768656  feet/sec       YDOT =       -2183
970300  meter/sec
 ZDOT =       4281
938782                 ZDOT =        1269
849194

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7809419
59                 X    =        -2380311
09
 Y    =       11862539
44  feet           Y    =         3615702
02  meter
 Z    =      -16956722
55                 Z    =        -5168409
03
 XDOT =     -22192
527322                 XDOT =       -6764
282328
 YDOT =      -8725
068176  feet/sec       YDOT =       -2659
400780  meter/sec
 ZDOT =       4144
169626                 ZDOT =        1263
142902


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   09050
58400607  
00010596  00000-0  82463-4 0  9037
2 25544  51
6400 189
2222 0008920  42
6850 317
5003 15
71002325 27451


Satellite: ISS
Catalog Number: 25544
Epoch time:      09050
58400607   =   yrday
fracday
Element set:     903
Inclination:       51
6400  deg
RA of node:       189
2222  deg
Eccentricity:     
0008920     
Arg of perigee:    42
6850  deg
Mean anomaly:     317
5003  deg
Mean motion:   15
71002325  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2745
Checksum:              268


Coasting Arc #5 (Orbit 2760)
---------------------------------------

Vector Time (GMT): 2009/051/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6716015
22                 A    =         6740734
78  meter
 Y    =         525612
44  meter          E    =           
0014903
 Z    =        -194997
21                 I    =           51
64075
 XDOT =       -535
186222                 Wp   =           99
81925
 YDOT =       4747
893271  meter/sec      RA   =          183
16229  deg
 ZDOT =      -6027
278913                 TA   =           82
29540
                                          MA   =           82
12620
                                          Ha   =            197
672  n
mi
                                          Hp   =            185
775

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22034170
67                 X    =         6710585
83
 Y    =        1724450
26  feet           Y    =          600684
47  meter
 Z    =        -639754
63                 Z    =         -162384
80
 XDOT =      -1755
860310                 XDOT =        -558
959472
 YDOT =      15577
077660  feet/sec       YDOT =        4741
775637  meter/sec
 ZDOT =     -19774
537116                 ZDOT =       -6029
936485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21812302
52                 X    =         6648389
81
 Y    =        3584475
55  feet           Y    =         1092548
15  meter
 Z    =        -512528
44                 Z    =         -156218
67
 XDOT =      -2693
479991                 XDOT =        -820
972701
 YDOT =      13791
335771  feet/sec       YDOT =        4203
599143  meter/sec
 ZDOT =     -19784
494242                 ZDOT =       -6030
313845


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   09051
60179007  
00010596  00000-0  82463-4 0  9049
2 25544  51
6400 184
0181 0008887  46
3797 313
8100 15
70991824 27616


Satellite: ISS
Catalog Number: 25544
Epoch time:      09051
60179007   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:       184
0181  deg
Eccentricity:     
0008887     
Arg of perigee:    46
3797  deg
Mean anomaly:     313
8100  deg
Mean motion:   15
70991824  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2761
Checksum:              305


Coasting Arc #6 (Orbit 2776)
---------------------------------------

Vector Time (GMT): 2009/052/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1146066
03                 A    =         6728822
77  meter
 Y    =       -4088840
13  meter          E    =           
0010498
 Z    =        5210799
06                 I    =           51
63144
 XDOT =       7588
596865                 Wp   =           68
28136
 YDOT =       -975
373355  meter/sec      RA   =          178
05543  deg
 ZDOT =        906
042063                 TA   =           13
10577
                                          MA   =           13
07851
                                          Ha   =            197
660  n
mi
                                          Hp   =            185
615

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3760059
17                 X    =        -1125571
20
 Y    =      -13414829
81  feet           Y    =        -4101541
48  meter
 Z    =       17095797
43                 Z    =         5205281
43
 XDOT =      24896
971342                 XDOT =        7594
538385
 YDOT =      -3200
043815  feet/sec       YDOT =        -890
480025  meter/sec
 ZDOT =       2972
578948                 ZDOT =         942
920901

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2943990
22                 X    =         -897328
22
 Y    =      -13644633
46  feet           Y    =        -4158884
28  meter
 Z    =       17073924
36                 Z    =         5204132
14
 XDOT =      24043
714693                 XDOT =        7328
524239
 YDOT =      -1297
875760  feet/sec       YDOT =        -395
592532  meter/sec
 ZDOT =       3116
330271                 ZDOT =         949
857467


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   09052
61956352  
00010596  00000-0  82463-4 0  9058
2 25544  51
6408 178
8144 0008915  49
5306 310
6631 15
71043806 27777


Satellite: ISS
Catalog Number: 25544
Epoch time:      09052
61956352   =   yrday
fracday
Element set:     905
Inclination:       51
6408  deg
RA of node:       178
8144  deg
Eccentricity:     
0008915     
Arg of perigee:    49
5306  deg
Mean anomaly:     310
6631  deg
Mean motion:   15
71043806  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2777
Checksum:              315


Coasting Arc #7 (Orbit 2791)
---------------------------------------

Vector Time (GMT): 2009/053/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6134118
59                 A    =         6739374
35  meter
 Y    =        2157491
87  meter          E    =           
0016382
 Z    =       -1753626
63                 I    =           51
69625
 XDOT =      -3078
170220                 Wp   =           46
16892
 YDOT =      -4154
543450  meter/sec      RA   =          172
92124  deg
 ZDOT =       5700
019126                 TA   =          294
45240
                                          MA   =          294
62320
                                          Ha   =            197
762  n
mi
                                          Hp   =            185
561

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20125060
98                 X    =        -6149269
56
 Y    =        7078385
40  feet           Y    =         2088811
83  meter
 Z    =       -5753368
20                 Z    =        -1783462
18
 XDOT =     -10098
983663                 XDOT =       -3059
173530
 YDOT =     -13630
391895  feet/sec       YDOT =       -4188
858981  meter/sec
 ZDOT =      18700
850150                 ZDOT =        5685
112045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20422470
99                 X    =        -6224769
16
 Y    =        6057544
08  feet           Y    =         1846339
44  meter
 Z    =       -5869557
33                 Z    =        -1789041
08
 XDOT =      -9065
720088                 XDOT =       -2763
231483
 YDOT =     -12637
711735  feet/sec       YDOT =       -3851
974537  meter/sec
 ZDOT =      18642
341301                 ZDOT =        5682
185628


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   09053
57372045  
00010596  00000-0  82463-4 0  9066
2 25544  51
6411 173
9370 0009075  51
9420 308
2559 15
70986040 27924


Satellite: ISS
Catalog Number: 25544
Epoch time:      09053
57372045   =   yrday
fracday
Element set:     906
Inclination:       51
6411  deg
RA of node:       173
9370  deg
Eccentricity:     
0009075     
Arg of perigee:    51
9420  deg
Mean anomaly:     308
2559  deg
Mean motion:   15
70986040  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2792
Checksum:              310


Coasting Arc #8 (Orbit 2807)
---------------------------------------

Vector Time (GMT): 2009/054/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4027300
01                 A    =         6731640
71  meter
 Y    =        2848700
83  meter          E    =           
0019123
 Z    =       -4599332
21                 I    =           51
69913
 XDOT =      -6028
203630                 Wp   =           64
03478
 YDOT =       3707
829012  meter/sec      RA   =          167
85130  deg
 ZDOT =      -2983
321281                 TA   =          176
30447
                                          MA   =          176
29033
                                          Ha   =            197
785  n
mi
                                          Hp   =            185
546

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13212926
53                 X    =         4017488
15
 Y    =        9346131
34  feet           Y    =         2893681
37  meter
 Z    =      -15089672
62                 Z    =        -4579792
10
 XDOT =     -19777
570963                 XDOT =       -6054
725130
 YDOT =      12164
793347  feet/sec       YDOT =        3640
269703  meter/sec
 ZDOT =      -9787
799477                 ZDOT =       -3012
670066

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12982496
70                 X    =         3957064
99
 Y    =        9782050
36  feet           Y    =         2981568
95  meter
 Z    =      -15013197
14                 Z    =        -4576022
49
 XDOT =     -19400
082537                 XDOT =       -5913
145157
 YDOT =      10557
117258  feet/sec       YDOT =        3217
809340  meter/sec
 ZDOT =      -9901
962089                 ZDOT =       -3018
118045


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   09054
59147802  
00010596  00000-0  82463-4 0  9071
2 25544  51
6409 168
7336 0008987  56
5761 303
6259 15
71017752 28085


Satellite: ISS
Catalog Number: 25544
Epoch time:      09054
59147802   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:       168
7336  deg
Eccentricity:     
0008987     
Arg of perigee:    56
5761  deg
Mean anomaly:     303
6259  deg
Mean motion:   15
71017752  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2808
Checksum:              336


Coasting Arc #9 (Orbit 2823)
---------------------------------------

Vector Time (GMT): 2009/055/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4128472
86                 A    =         6735498
81  meter
 Y    =       -4088995
28  meter          E    =           
0020956
 Z    =        3393468
66                 I    =           51
74160
 XDOT =       5817
367671                 Wp   =           77
22644
 YDOT =       2009
687128  meter/sec      RA   =          162
69659  deg
 ZDOT =      -4627
344070                 TA   =           62
81456
                                          MA   =           62
60110
                                          Ha   =            197
784  n
mi
                                          Hp   =            185
237

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13544858
45                 X    =         4157405
41
 Y    =      -13415338
86  feet           Y    =        -4042666
30  meter
 Z    =       11133427
35                 Z    =         3413594
82
 XDOT =      19085
851939                 XDOT =        5816
940887
 YDOT =       6593
461707  feet/sec       YDOT =        2074
737620  meter/sec
 ZDOT =     -15181
575032                 ZDOT =       -4599
085196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13692938
06                 X    =         4173607
52
 Y    =      -13198165
52  feet           Y    =        -4022800
85  meter
 Z    =       11211582
67                 Z    =         3417290
40
 XDOT =      18103
002618                 XDOT =        5517
795198
 YDOT =       5900
300559  feet/sec       YDOT =        1798
411611  meter/sec
 ZDOT =     -15071
152574                 ZDOT =       -4593
687304


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   09055
60922628  
00010596  00000-0  82463-4 0  9082
2 25544  51
6411 163
5300 0009201  59
7818 300
4253 15
71059166 28242


Satellite: ISS
Catalog Number: 25544
Epoch time:      09055
60922628   =   yrday
fracday
Element set:     908
Inclination:       51
6411  deg
RA of node:       163
5300  deg
Eccentricity:     
0009201     
Arg of perigee:    59
7818  deg
Mean anomaly:     300
4253  deg
Mean motion:   15
71059166  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2824
Checksum:              294


Coasting Arc #10 (Orbit 2839)
---------------------------------------

Vector Time (GMT): 2009/056/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5814709
78                 A    =         6735752
35  meter
 Y    =        -458962
72  meter          E    =           
0021302
 Z    =        3346513
99                 I    =           51
77007
 XDOT =       3120
159622                 Wp   =           78
57068
 YDOT =      -5268
100103  meter/sec      RA   =          157
64259  deg
 ZDOT =       4678
068925                 TA   =          320
73952
                                          MA   =          320
89381
                                          Ha   =            197
912  n
mi
                                          Hp   =            185
207

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19077131
83                 X    =        -5825401
83
 Y    =       -1505783
21  feet           Y    =         -524045
69  meter
 Z    =       10979376
61                 Z    =         3318240
82
 XDOT =      10236
744167                 XDOT =        3156
111773
 YDOT =     -17283
792990  feet/sec       YDOT =       -5233
007249  meter/sec
 ZDOT =      15347
995160                 ZDOT =        4693
314100

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19142053
99                 X    =        -5834498
06
 Y    =       -1482237
73  feet           Y    =         -451786
06  meter
 Z    =       10869029
08                 Z    =         3312880
06
 XDOT =      10018
661622                 XDOT =        3053
688062
 YDOT =     -15900
223426  feet/sec       YDOT =       -4846
388100  meter/sec
 ZDOT =      15407
006078                 ZDOT =        4696
055453


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   09056
62696493  
00010596  00000-0  82463-4 0  9094
2 25544  51
6411 158
3265 0009139  63
6256 296
5843 15
71075057 28409


Satellite: ISS
Catalog Number: 25544
Epoch time:      09056
62696493   =   yrday
fracday
Element set:     909
Inclination:       51
6411  deg
RA of node:       158
3265  deg
Eccentricity:     
0009139     
Arg of perigee:    63
6256  deg
Mean anomaly:     296
5843  deg
Mean motion:   15
71075057  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2840
Checksum:              333


Coasting Arc #11 (Orbit 2854)
---------------------------------------

Vector Time (GMT): 2009/057/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1209544
72                 A    =         6731162
80  meter
 Y    =        4744709
91  meter          E    =           
0018620
 Z    =       -4634759
57                 I    =           51
78094
 XDOT =      -7023
941593                 Wp   =           90
02471
 YDOT =       1058
817425  meter/sec      RA   =          152
49280  deg
 ZDOT =       2927
074626                 TA   =          208
93210
                                          MA   =          209
03544
                                          Ha   =            197
882  n
mi
                                          Hp   =            185
011

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3968322
58                 X    =        -1239996
51
 Y    =       15566633
58  feet           Y    =         4731013
39  meter
 Z    =      -15205904
09                 Z    =        -4640709
84
 XDOT =     -23044
427797                 XDOT =       -7049
478396
 YDOT =       3473
810450  feet/sec       YDOT =         980
129110  meter/sec
 ZDOT =       9603
263209                 ZDOT =        2892
890765

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3592942
42                 X    =        -1095128
85
 Y    =       15635365
85  feet           Y    =         4765659
51  meter
 Z    =      -15228699
34                 Z    =        -4641707
56
 XDOT =     -21891
423853                 XDOT =       -6672
505990
 YDOT =       4160
942951  feet/sec       YDOT =        1268
255412  meter/sec
 ZDOT =       9469
983565                 ZDOT =        2886
450991


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   09057
58108798  
00010596  00000-0  82463-4 0  9108
2 25544  51
6402 153
4486 0009328  66
5921 293
6221 15
71089922 28551


Satellite: ISS
Catalog Number: 25544
Epoch time:      09057
58108798   =   yrday
fracday
Element set:     910
Inclination:       51
6402  deg
RA of node:       153
4486  deg
Eccentricity:     
0009328     
Arg of perigee:    66
5921  deg
Mean anomaly:     293
6221  deg
Mean motion:   15
71089922  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2855
Checksum:              329


Coasting Arc #12 (Orbit 2870)
---------------------------------------

Vector Time (GMT): 2009/058/13:41:07
008
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6100385
85                 A    =         6739232
13  meter
 Y    =       -2293551
02  meter          E    =           
0013886
 Z    =       -1719315
11                 I    =           51
83327
 XDOT =        326
934703                 Wp   =          102
53590
 YDOT =       5127
226951  meter/sec      RA   =          147
42831  deg
 ZDOT =      -5721
266216                 TA   =           96
39586
                                          MA   =           96
23772
                                          Ha   =            197
960  n
mi
                                          Hp   =            185
009

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20014389
26                 X    =         6133931
35
 Y    =       -7524773
68  feet           Y    =        -2225145
54  meter
 Z    =       -5640797
60                 Z    =        -1689598
08
 XDOT =       1072
620417                 XDOT =         297
369464
 YDOT =      16821
610730  feet/sec       YDOT =        5130
717092  meter/sec
 ZDOT =     -18770
558451                 ZDOT =       -5719
750269

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19765860
36                 X    =         6024634
24
 Y    =       -8234147
82  feet           Y    =        -2509768
25  meter
 Z    =       -5525049
13                 Z    =        -1684034
97
 XDOT =       1179
032927                 XDOT =         359
369236
 YDOT =      15327
357932  feet/sec       YDOT =        4671
778698  meter/sec
 ZDOT =     -18764
191644                 ZDOT =       -5719
325613


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   09058
59881026  
00010596  00000-0  82463-4 0  9113
2 25544  51
6399 148
2443 0009394  70
1290 290
0883 15
71090689 28719


Satellite: ISS
Catalog Number: 25544
Epoch time:      09058
59881026   =   yrday
fracday
Element set:     911
Inclination:       51
6399  deg
RA of node:       148
2443  deg
Eccentricity:     
0009394     
Arg of perigee:    70
1290  deg
Mean anomaly:     290
0883  deg
Mean motion:   15
71090689  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2871
Checksum:              332

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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