Date: February 27th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


064/20:15:11 644 0 3 1 6 1 6
N/A -1 5 0 0 198 7
000/00:00:23 287 0 4 0 0 184 5

Coasting Arc #1 (Orbit 2837)
---------------------------------------

Vector Time (GMT): 2009/056/11:41:12
065
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -490262
43                 A    =         6729456
52  meter
 Y    =        4469454
99  meter          E    =           
0021062
 Z    =       -5024772
89                 I    =           51
74776
 XDOT =      -7320
450371                 Wp   =           88
17452
 YDOT =       1332
069651  meter/sec      RA   =          158
03175  deg
 ZDOT =       1906
618732                 TA   =          200
21037
                                          MA   =          200
29387
                                          Ha   =            197
743  n
mi
                                          Hp   =            185
067

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1608472
55                 X    =         -515795
28
 Y    =       14663566
24  feet           Y    =         4463829
41  meter
 Z    =      -16485475
35                 Z    =        -5027216
92
 XDOT =     -24017
225627                 XDOT =       -7344
063532
 YDOT =       4370
307253  feet/sec       YDOT =        1250
076244  meter/sec
 ZDOT =       6255
310800                 ZDOT =        1870
999306

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8640297
06                 X    =        -2633562
54
 Y    =       11943669
12  feet           Y    =         3640430
35  meter
 Z    =      -16494614
00                 Z    =        -5027558
35
 XDOT =     -22146
023464                 XDOT =       -6750
107952
 YDOT =      -7607
878299  feet/sec       YDOT =       -2318
881305  meter/sec
 ZDOT =       6116
461655                 ZDOT =        1864
297512


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
49968765  
00010596  00000-0  82463-4 0  9004
2 25544  51
6415 158
9825 0009143  64
1039 296
1064 15
71126325 28384


Satellite: ISS
Catalog Number: 25544
Epoch time:      09056
49968765   =   yrday
fracday
Element set:     900
Inclination:       51
6415  deg
RA of node:       158
9825  deg
Eccentricity:     
0009143     
Arg of perigee:    64
1039  deg
Mean anomaly:     296
1064  deg
Mean motion:   15
71126325  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2838
Checksum:              328


Coasting Arc #2 (Orbit 2853)
---------------------------------------

Vector Time (GMT): 2009/057/11:41:12
065
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6214915
72                 A    =         6740131
23  meter
 Y    =       -2484641
29  meter          E    =           
0015846
 Z    =        -779826
08                 I    =           51
81014
 XDOT =       1141
551841                 Wp   =          107
41808
 YDOT =       4700
004703  meter/sec      RA   =          152
95050  deg
 ZDOT =      -5981
194052                 TA   =           81
04909
                                          MA   =           80
86975
                                          Ha   =            197
789  n
mi
                                          Hp   =            185
064

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20390143
42                 X    =         6246025
67
 Y    =       -8151710
26  feet           Y    =        -2414968
61  meter
 Z    =       -2558484
51                 Z    =         -749558
74
 XDOT =       3745
248822                 XDOT =        1117
965831
 YDOT =      15419
962935  feet/sec       YDOT =        4712
637769  meter/sec
 ZDOT =     -19623
340067                 ZDOT =       -5975
706214

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21798034
59                 X    =         6644040
94
 Y    =        2764646
34  feet           Y    =          842664
21  meter
 Z    =       -2440612
74                 Z    =         -743898
76
 XDOT =      -3900
719997                 XDOT =       -1188
939455
 YDOT =      13767
197656  feet/sec       YDOT =        4196
241846  meter/sec
 ZDOT =     -19601
511640                 ZDOT =       -5974
540748


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
51738901  
00010596  00000-0  82463-4 0  9016
2 25544  51
6412 153
7783 0009113  67
7978 292
4149 15
71122745 28548


Satellite: ISS
Catalog Number: 25544
Epoch time:      09057
51738901   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:       153
7783  deg
Eccentricity:     
0009113     
Arg of perigee:    67
7978  deg
Mean anomaly:     292
4149  deg
Mean motion:   15
71122745  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2854
Checksum:              324


Coasting Arc #3 (Orbit 2869)
---------------------------------------

Vector Time (GMT): 2009/058/11:41:12
065
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2390375
64                 A    =         6728125
81  meter
 Y    =       -3404390
60  meter          E    =           
0011279
 Z    =        5278607
73                 I    =           51
79641
 XDOT =       6439
712281                 Wp   =           77
24002
 YDOT =      -4227
117966  meter/sec      RA   =          147
84274  deg
 ZDOT =        192
031473                 TA   =           10
95488
                                          MA   =           10
93033
                                          Ha   =            197
760  n
mi
                                          Hp   =            184
918

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7842439
77                 X    =        -2377771
74
 Y    =      -11169260
49  feet           Y    =        -3431050
21  meter
 Z    =       17318266
82                 Z    =         5267026
35
 XDOT =      21127
664963                 XDOT =        6485
569160
 YDOT =     -13868
497265  feet/sec       YDOT =       -4154
848937  meter/sec
 ZDOT =        630
024519                 ZDOT =         223
426996

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1764434
39                 X    =         -537799
60
 Y    =      -13591045
13  feet           Y    =        -4142550
56  meter
 Z    =       17272778
32                 Z    =         5264742
83
 XDOT =      24171
678557                 XDOT =        7367
527624
 YDOT =      -2190
924452  feet/sec       YDOT =        -667
793773  meter/sec
 ZDOT =        752
151093                 ZDOT =         229
255653


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
53507231  
00010596  00000-0  82463-4 0  9020
2 25544  51
6415 148
5741 0009095  70
7598 289
4547 15
71189206 28709


Satellite: ISS
Catalog Number: 25544
Epoch time:      09058
53507231   =   yrday
fracday
Element set:     902
Inclination:       51
6415  deg
RA of node:       148
5741  deg
Eccentricity:     
0009095     
Arg of perigee:    70
7598  deg
Mean anomaly:     289
4547  deg
Mean motion:   15
71189206  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2870
Checksum:              329


Coasting Arc #4 (Orbit 2884)
---------------------------------------

Vector Time (GMT): 2009/059/11:41:12
065
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4715462
68                 A    =         6739764
21  meter
 Y    =        4680043
08  meter          E    =           
0017800
 Z    =       -1106448
41                 I    =           51
85905
 XDOT =      -4084
943245                 Wp   =           55
56106
 YDOT =      -2734
216565  meter/sec      RA   =          142
73053  deg
 ZDOT =       5921
104232                 TA   =          292
38250
                                          MA   =          292
57100
                                          Ha   =            197
795  n
mi
                                          Hp   =            184
914

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15470678
08                 X    =        -4762070
35
 Y    =       15354472
06  feet           Y    =         4627051
35  meter
 Z    =       -3630080
09                 Z    =        -1129469
55
 XDOT =     -13402
044767                 XDOT =       -4082
828628
 YDOT =      -8970
526789  feet/sec       YDOT =       -2779
884474  meter/sec
 ZDOT =      19426
194987                 ZDOT =        5901
265082

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20740283
51                 X    =        -6321638
41
 Y    =        6654707
50  feet           Y    =         2028354
84  meter
 Z    =       -3719500
23                 Z    =        -1133703
67
 XDOT =      -7474
972279                 XDOT =       -2278
371551
 YDOT =     -12620
202545  feet/sec       YDOT =       -3846
637736  meter/sec
 ZDOT =      19348
544138                 ZDOT =        5897
436253


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   09059
48913815  
00010596  00000-0  82463-4 0  9035
2 25544  51
6411 143
6961 0009228  73
0485 287
1688 15
71140405 28859


Satellite: ISS
Catalog Number: 25544
Epoch time:      09059
48913815   =   yrday
fracday
Element set:     903
Inclination:       51
6411  deg
RA of node:       143
6961  deg
Eccentricity:     
0009228     
Arg of perigee:    73
0485  deg
Mean anomaly:     287
1688  deg
Mean motion:   15
71140405  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2885
Checksum:              324


Coasting Arc #5 (Orbit 2900)
---------------------------------------

Vector Time (GMT): 2009/060/11:41:12
065
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4453785
14                 A    =         6729859
32  meter
 Y    =        1176775
05  meter          E    =           
0021486
 Z    =       -4925776
15                 I    =           51
84759
 XDOT =      -4086
652039                 Wp   =           75
50797
 YDOT =       6104
095179  meter/sec      RA   =          137
65991  deg
 ZDOT =      -2239
650858                 TA   =          172
73881
                                          MA   =          172
70764
                                          Ha   =            197
754  n
mi
                                          Hp   =            184
948

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14612155
98                 X    =         4464223
66
 Y    =        3860810
53  feet           Y    =         1226637
93  meter
 Z    =      -16160682
91                 Z    =        -4904114
47
 XDOT =     -13407
651046                 XDOT =       -4143
725543
 YDOT =      20026
558986  feet/sec       YDOT =        6058
076604  meter/sec
 ZDOT =      -7347
935887                 ZDOT =       -2259
642735

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11516211
57                 X    =         3510141
29
 Y    =        9926027
49  feet           Y    =         3025453
18  meter
 Z    =      -16076053
05                 Z    =        -4899980
97
 XDOT =     -20077
830706                 XDOT =       -6119
722799
 YDOT =      11283
542941  feet/sec       YDOT =        3439
223888  meter/sec
 ZDOT =      -7425
424120                 ZDOT =       -2263
269272


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   09060
50679150  
00010596  00000-0  82463-4 0  9042
2 25544  51
6401 138
4917 0009156  77
6112 282
6074 15
71178600 29014


Satellite: ISS
Catalog Number: 25544
Epoch time:      09060
50679150   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:       138
4917  deg
Eccentricity:     
0009156     
Arg of perigee:    77
6112  deg
Mean anomaly:     282
6074  deg
Mean motion:   15
71178600  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2901
Checksum:              296


Coasting Arc #6 (Orbit 2916)
---------------------------------------

Vector Time (GMT): 2009/061/11:41:12
065
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2281486
53                 A    =         6736710
66  meter
 Y    =       -5694611
78  meter          E    =           
0022547
 Z    =        2763212
98                 I    =           51
89231
 XDOT =       5709
887367                 Wp   =           92
35382
 YDOT =       -234
816932  meter/sec      RA   =          132
52095  deg
 ZDOT =      -5163
291207                 TA   =           56
18375
                                          MA   =           55
96929
                                          Ha   =            197
724  n
mi
                                          Hp   =            184
655

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7485192
03                 X    =         2331571
92
 Y    =      -18683109
50  feet           Y    =        -5668818
72  meter
 Z    =        9065659
39                 Z    =         2774418
27
 XDOT =      18733
226270                 XDOT =        5737
171001
 YDOT =       -770
396757  feet/sec       YDOT =        -170
813290  meter/sec
 ZDOT =     -16939
931782                 ZDOT =       -5135
486398

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14647201
06                 X    =         4464466
88
 Y    =      -13775346
40  feet           Y    =        -4198725
58  meter
 Z    =        9108907
35                 Z    =         2776394
96
 XDOT =      16379
633234                 XDOT =        4992
512210
 YDOT =       6210
818556  feet/sec       YDOT =        1893
057496  meter/sec
 ZDOT =     -16831
442785                 ZDOT =       -5130
223761


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
52442829  
00010596  00000-0  82463-4 0  9057
2 25544  51
6400 133
2870 0009334  80
4023 279
8193 15
71237985 29174


Satellite: ISS
Catalog Number: 25544
Epoch time:      09061
52442829   =   yrday
fracday
Element set:     905
Inclination:       51
6400  deg
RA of node:       133
2870  deg
Eccentricity:     
0009334     
Arg of perigee:    80
4023  deg
Mean anomaly:     279
8193  deg
Mean motion:   15
71237985  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2917
Checksum:              311


Coasting Arc #7 (Orbit 2932)
---------------------------------------

Vector Time (GMT): 2009/062/11:41:12
065
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5177524
29                 A    =         6733269
80  meter
 Y    =        1651915
70  meter          E    =           
0020166
 Z    =        3958751
06                 I    =           51
89969
 XDOT =       1012
286933                 Wp   =           93
32654
 YDOT =      -6497
057052  meter/sec      RA   =          127
47293  deg
 ZDOT =       4016
444340                 TA   =          315
10804
                                          MA   =          315
27096
                                          Ha   =            197
793  n
mi
                                          Hp   =            184
645

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16986628
24                 X    =        -5214842
27
 Y    =        5419670
93  feet           Y    =         1593809
01  meter
 Z    =       12988028
41                 Z    =         3933508
12
 XDOT =       3321
151355                 XDOT =        1065
351822
 YDOT =     -21315
803977  feet/sec       YDOT =       -6485
440314  meter/sec
 ZDOT =      13177
310828                 ZDOT =        4021
490986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17788066
80                 X    =        -5421802
76
 Y    =       -2012206
63  feet           Y    =         -613320
58  meter
 Z    =       12889645
38                 Z    =         3928763
91
 XDOT =      11512
001659                 XDOT =        3508
858106
 YDOT =     -16840
189195  feet/sec       YDOT =       -5132
889667  meter/sec
 ZDOT =      13196
468159                 ZDOT =        4022
283495


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
54204842  
00010596  00000-0  82463-4 0  9062
2 25544  51
6399 128
0823 0009269  84
4848 275
7370 15
71264310 29339


Satellite: ISS
Catalog Number: 25544
Epoch time:      09062
54204842   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       128
0823  deg
Eccentricity:     
0009269     
Arg of perigee:    84
4848  deg
Mean anomaly:     275
7370  deg
Mean motion:   15
71264310  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2933
Checksum:              321


Coasting Arc #8 (Orbit 2947)
---------------------------------------

Vector Time (GMT): 2009/063/11:41:12
065
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         482613
56                 A    =         6732494
81  meter
 Y    =        5301382
32  meter          E    =           
0016916
 Z    =       -4137652
54                 I    =           51
91391
 XDOT =      -5711
685669                 Wp   =           97
61146
 YDOT =       3470
038787  meter/sec      RA   =          122
32674  deg
 ZDOT =       3790
764413                 TA   =          211
15526
                                          MA   =          211
25565
                                          Ha   =            197
715  n
mi
                                          Hp   =            184
512

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1583377
84                 X    =          443396
52
 Y    =       17392986
61  feet           Y    =         5306559
92  meter
 Z    =      -13574975
54                 Z    =        -4135403
28
 XDOT =     -18739
126212                 XDOT =       -5768
478378
 YDOT =      11384
641689  feet/sec       YDOT =        3405
849842  meter/sec
 ZDOT =      12436
891118                 ZDOT =        3762
879384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5292869
56                 X    =        -1613266
64
 Y    =       16651085
24  feet           Y    =         5075250
78  meter
 Z    =      -13565762
84                 Z    =        -4134844
51
 XDOT =     -20554
433329                 XDOT =       -6264
991279
 YDOT =       3481
009949  feet/sec       YDOT =        1061
011832  meter/sec
 ZDOT =      12328
331204                 ZDOT =        3757
675351


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
49605431  
00010596  00000-0  82463-4 0  9077
2 25544  51
6393 123
2032 0009474  87
3881 272
8365 15
71294467 29483


Satellite: ISS
Catalog Number: 25544
Epoch time:      09063
49605431   =   yrday
fracday
Element set:     907
Inclination:       51
6393  deg
RA of node:       123
2032  deg
Eccentricity:     
0009474     
Arg of perigee:    87
3881  deg
Mean anomaly:     272
8365  deg
Mean motion:   15
71294467  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2948
Checksum:              330


Coasting Arc #9 (Orbit 2963)
---------------------------------------

Vector Time (GMT): 2009/064/11:41:12
065
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4505451
49                 A    =         6736976
59  meter
 Y    =       -4279052
60  meter          E    =           
0013928
 Z    =       -2609951
22                 I    =           51
94412
 XDOT =       1941
652875                 Wp   =          103
60850
 YDOT =       5245
916489  meter/sec      RA   =          117
27868  deg
 ZDOT =      -5275
571870                 TA   =          105
85147
                                          MA   =          105
69790
                                          Ha   =            197
753  n
mi
                                          Hp   =            184
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14781664
99                 X    =         4565644
19
 Y    =      -14038886
49  feet           Y    =        -4228333
46  meter
 Z    =       -8562832
10                 Z    =        -2587917
90
 XDOT =       6370
252216                 XDOT =        1908
475232
 YDOT =      17211
012104  feet/sec       YDOT =        5267
443702  meter/sec
 ZDOT =     -17308
306661                 ZDOT =       -5266
220029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19023804
74                 X    =         5798455
69
 Y    =       -7425803
72  feet           Y    =        -2263384
97  meter
 Z    =       -8477165
78                 Z    =        -2583840
13
 XDOT =      -1023
765796                 XDOT =        -312
043815
 YDOT =      16993
282664  feet/sec       YDOT =        5179
552556  meter/sec
 ZDOT =     -17271
375676                 ZDOT =       -5264
315306


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
51364469  
00010596  00000-0  82463-4 0  9085
2 25544  51
6398 117
9978 0009520  90
6403 269
5850 15
71298641 29644


Satellite: ISS
Catalog Number: 25544
Epoch time:      09064
51364469   =   yrday
fracday
Element set:     908
Inclination:       51
6398  deg
RA of node:       117
9978  deg
Eccentricity:     
0009520     
Arg of perigee:    90
6403  deg
Mean anomaly:     269
5850  deg
Mean motion:   15
71298641  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2964
Checksum:              349


Coasting Arc #10 (Orbit 2969)
---------------------------------------

Vector Time (GMT): 2009/064/20:15:23
287
Vector Time (MET): N/A
Weight (LBS)     : 638664
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4494365
53                 A    =         6729953
42  meter
 Y    =         356263
47  meter          E    =           
0015887
 Z    =        4984197
76                 I    =           51
92256
 XDOT =       1685
867444                 Wp   =          101
04598
 YDOT =      -7240
833121  meter/sec      RA   =          115
45505  deg
 ZDOT =       2029
348725                 TA   =          329
36412
                                          MA   =          329
45680
                                          Ha   =            198
684  n
mi
                                          Hp   =            184
498

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14745293
74                 X    =        -4522227
21
 Y    =        1168843
41  feet           Y    =          305849
07  meter
 Z    =       16352354
84                 Z    =         4962296
84
 XDOT =       5531
061169                 XDOT =        1756
852312
 YDOT =     -23756
014177  feet/sec       YDOT =       -7221
583878  meter/sec
 ZDOT =       6657
968258                 ZDOT =        2037
710927

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5406447
86                 X    =         1647885
31
 Y    =       13868964
08  feet           Y    =         4227260
25  meter
 Z    =       16266885
02                 Z    =         4958146
55
 XDOT =     -23318
406352                 XDOT =       -7107
450256
 YDOT =       1210
838818  feet/sec       YDOT =         369
063672  meter/sec
 ZDOT =       6690
029781                 ZDOT =        2039
121077


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
89524861  
00010596  00000-0  82463-4 0  9091
2 25544  51
6398 116
0470 0010612  88
2832 271
9545 15
71027549 29706


Satellite: ISS
Catalog Number: 25544
Epoch time:      09064
89524861   =   yrday
fracday
Element set:     909
Inclination:       51
6398  deg
RA of node:       116
0470  deg
Eccentricity:     
0010612     
Arg of perigee:    88
2832  deg
Mean anomaly:     271
9545  deg
Mean motion:   15
71027549  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2970
Checksum:              327


Coasting Arc #11 (Orbit 2984)
---------------------------------------

Vector Time (GMT): 2009/065/20:15:23
287
Vector Time (MET): N/A
Weight (LBS)     : 638664
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -57118
85                 A    =         6737557
03  meter
 Y    =        6186148
23  meter          E    =           
0014965
 Z    =       -2677786
43                 I    =           51
96000
 XDOT =      -5182
495151                 Wp   =           80
27441
 YDOT =       2205
317933  meter/sec      RA   =          110
32464  deg
 ZDOT =       5232
340730                 TA   =          249
43591
                                          MA   =          249
59654
                                          Ha   =            198
586  n
mi
                                          Hp   =            184
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -187397
80                 X    =         -113281
23
 Y    =       20295761
90  feet           Y    =         6185195
43  meter
 Z    =       -8785388
54                 Z    =        -2678200
41
 XDOT =     -17002
936847                 XDOT =       -5232
187407
 YDOT =       7235
295057  feet/sec       YDOT =        2147
086487  meter/sec
 ZDOT =      17166
472211                 ZDOT =        5207
044003

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19368172
72                 X    =         5903419
04
 Y    =       -6066899
85  feet           Y    =        -1849191
07  meter
 Z    =       -8786508
57                 Z    =        -2678127
81
 XDOT =      11669
324971                 XDOT =        3556
810251
 YDOT =      12663
532731  feet/sec       YDOT =        3859
844776  meter/sec
 ZDOT =      17067
883703                 ZDOT =        5202
290953


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
84940789  
00010596  00000-0  82463-4 0  9100
2 25544  51
6401 111
1686 0010699  91
2030 269
0357 15
71020073 29855


Satellite: ISS
Catalog Number: 25544
Epoch time:      09065
84940789   =   yrday
fracday
Element set:     910
Inclination:       51
6401  deg
RA of node:       111
1686  deg
Eccentricity:     
0010699     
Arg of perigee:    91
2030  deg
Mean anomaly:     269
0357  deg
Mean motion:   15
71020073  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2985
Checksum:              305


Coasting Arc #12 (Orbit 3000)
---------------------------------------

Vector Time (GMT): 2009/066/20:15:23
287
Vector Time (MET): N/A
Weight (LBS)     : 638664
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4202801
88                 A    =         6733595
57  meter
 Y    =       -3389669
24  meter          E    =           
0017565
 Z    =       -4039388
83                 I    =           51
95681
 XDOT =       1429
703979                 Wp   =           85
58301
 YDOT =       6443
407633  meter/sec      RA   =          105
28139  deg
 ZDOT =      -3932
749062                 TA   =          143
93727
                                          MA   =          143
81865
                                          Ha   =            198
560  n
mi
                                          Hp   =            184
489

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13788720
06                 X    =         4260015
49
 Y    =      -11120962
07  feet           Y    =        -3342351
33  meter
 Z    =      -13252588
01                 Z    =        -4018833
02
 XDOT =       4690
629853                 XDOT =        1376
650569
 YDOT =      21139
788821  feet/sec       YDOT =        6459
098618  meter/sec
 ZDOT =     -12902
720020                 ZDOT =       -3925
932861

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14989999
62                 X    =        -4568951
88
 Y    =       -9550825
54  feet           Y    =        -2911091
62  meter
 Z    =      -13172597
70                 Z    =        -4015007
78
 XDOT =      17786
879104                 XDOT =        5421
440751
 YDOT =     -10218
779579  feet/sec       YDOT =       -3114
684016  meter/sec
 ZDOT =     -12875
589078                 ZDOT =       -3924
479551


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
86716093  
00010596  00000-0  82463-4 0  9113
2 25544  51
6409 105
9645 0010751  94
6982 265
5408 15
71057259 30015


Satellite: ISS
Catalog Number: 25544
Epoch time:      09066
86716093   =   yrday
fracday
Element set:     911
Inclination:       51
6409  deg
RA of node:       105
9645  deg
Eccentricity:     
0010751     
Arg of perigee:    94
6982  deg
Mean anomaly:     265
5408  deg
Mean motion:   15
71057259  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3001
Checksum:              318


Coasting Arc #13 (Orbit 3016)
---------------------------------------

Vector Time (GMT): 2009/067/20:15:23
287
Vector Time (MET): N/A
Weight (LBS)     : 638664
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2418728
49                 A    =         6733250
92  meter
 Y    =       -4738752
35  meter          E    =           
0020880
 Z    =        4109651
53                 I    =           51
96157
 XDOT =       3996
453505                 Wp   =           87
38552
 YDOT =      -5368
174021  meter/sec      RA   =          100
14037  deg
 ZDOT =      -3820
338775                 TA   =           41
70369
                                          MA   =           41
54470
                                          Ha   =            198
591  n
mi
                                          Hp   =            184
417

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7935460
94                 X    =        -2385522
66
 Y    =      -15547087
78  feet           Y    =        -4765614
03  meter
 Z    =       13483108
68                 Z    =         4097982
62
 XDOT =      13111
724098                 XDOT =        4074
742351
 YDOT =     -17612
119492  feet/sec       YDOT =       -5323
045882  meter/sec
 ZDOT =     -12533
919865                 ZDOT =       -3800
733956

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11924713
81                 X    =        -3634652
77
 Y    =       12795370
98  feet           Y    =         3900029
08  meter
 Z    =       13437164
14                 Z    =         4095647
63
 XDOT =     -20098
180016                 XDOT =       -6125
925269
 YDOT =      -5587
504281  feet/sec       YDOT =       -1703
071305  meter/sec
 ZDOT =     -12457
797157                 ZDOT =       -3797
136574


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
88489859  
00010596  00000-0  82463-4 0  9124
2 25544  51
6401 100
7608 0010750  98
4284 261
8097 15
71065848 30178


Satellite: ISS
Catalog Number: 25544
Epoch time:      09067
88489859   =   yrday
fracday
Element set:     912
Inclination:       51
6401  deg
RA of node:       100
7608  deg
Eccentricity:     
0010750     
Arg of perigee:    98
4284  deg
Mean anomaly:     261
8097  deg
Mean motion:   15
71065848  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3017
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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