Date: January 13th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 65 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 2618)
---------------------------------------

Vector Time (GMT): 2007/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6410964
73                 A    =         6723159
11  meter
 Y    =        1709236
22  meter          E    =           
0029357
 Z    =       -1090100
29                 I    =           51
60649
 XDOT =      -2163
991737                 Wp   =           99
73864
 YDOT =       4437
967382  meter/sec      RA   =          187
44786  deg
 ZDOT =      -5907
363867                 TA   =           92
19938
                                          MA   =           91
86319
                                          Ha   =            193
914  n
mi
                                          Hp   =            170
797

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21033348
86                 X    =         6396670
82
 Y    =        5607730
37  feet           Y    =         1780847
37  meter
 Z    =       -3576444
52                 Z    =        -1058990
54
 XDOT =      -7099
710424                 XDOT =       -2184
760121
 YDOT =      14560
260439  feet/sec       YDOT =        4413
652812  meter/sec
 ZDOT =     -19381
115049                 ZDOT =       -5917
926549

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2261085
59                 X    =          689178
89
 Y    =       21669280
73  feet           Y    =         6604796
77  meter
 Z    =       -3459642
18                 Z    =        -1054498
94
 XDOT =     -14515
907904                 XDOT =       -4424
448729
 YDOT =      -1510
440076  feet/sec       YDOT =        -460
382135  meter/sec
 ZDOT =     -19420
121490                 ZDOT =       -5919
253030


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   07012
52978138  
00020000  00000-0  20000-3 0  9002
2 25544  51
6293 188
2643 0023174  82
9664 277
4135 15
77000317 26190


Satellite: ISS
Catalog Number: 25544
Epoch time:      07012
52978138   =   yrday
fracday
Element set:     900
Inclination:       51
6293  deg
RA of node:       188
2643  deg
Eccentricity:     
0023174     
Arg of perigee:    82
9664  deg
Mean anomaly:     277
4135  deg
Mean motion:   15
77000317  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2619
Checksum:              294


Coasting Arc #2 (Orbit 2634)
---------------------------------------

Vector Time (GMT): 2007/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2735243
52                 A    =         6713377
12  meter
 Y    =       -3732004
84  meter          E    =           
0029129
 Z    =        4841088
95                 I    =           51
60107
 XDOT =       7051
658442                 Wp   =           81
24592
 YDOT =       2125
601703  meter/sec      RA   =          182
25753  deg
 ZDOT =      -2329
388246                 TA   =           31
47098
                                          MA   =           31
29704
                                          Ha   =            193
883  n
mi
                                          Hp   =            170
816

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8973896
08                 X    =         2753255
01
 Y    =      -12244110
38  feet           Y    =        -3701317
63  meter
 Z    =       15882837
75                 Z    =         4854420
06
 XDOT =      23135
362341                 XDOT =        7038
681267
 YDOT =       6973
758868  feet/sec       YDOT =        2204
384956  meter/sec
 ZDOT =      -7642
349888                 ZDOT =       -2295
162730

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14672140
44                 X    =         4472068
41
 Y    =        3688246
94  feet           Y    =         1124177
67  meter
 Z    =       15932316
67                 Z    =         4856170
12
 XDOT =       2425
575417                 XDOT =         739
315387
 YDOT =      23037
672356  feet/sec       YDOT =        7021
882534  meter/sec
 ZDOT =      -7513
806648                 ZDOT =       -2290
208266


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   07013
54369497  
00020000  00000-0  20000-3 0  9018
2 25544  51
6285 183
0328 0023147  87
4316 272
9498 15
76970599 26355


Satellite: ISS
Catalog Number: 25544
Epoch time:      07013
54369497   =   yrday
fracday
Element set:     901
Inclination:       51
6285  deg
RA of node:       183
0328  deg
Eccentricity:     
0023147     
Arg of perigee:    87
4316  deg
Mean anomaly:     272
9498  deg
Mean motion:   15
76970599  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2635
Checksum:              325


Coasting Arc #3 (Orbit 2650)
---------------------------------------

Vector Time (GMT): 2007/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5710701
20                 A    =         6719998
56  meter
 Y    =       -2002735
17  meter          E    =           
0036498
 Z    =        2888567
49                 I    =           51
65261
 XDOT =       4053
758301                 Wp   =           87
92510
 YDOT =      -4201
151467  meter/sec      RA   =          177
14046  deg
 ZDOT =       5048
296274                 TA   =          305
39083
                                          MA   =          305
73124
                                          Ha   =            193
896  n
mi
                                          Hp   =            170
747

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18735896
32                 X    =        -5701913
96
 Y    =       -6570653
44  feet           Y    =        -2066546
63  meter
 Z    =        9476927
47                 Z    =         2860846
15
 XDOT =      13299
731958                 XDOT =        4075
911313
 YDOT =     -13783
305338  feet/sec       YDOT =       -4155
696848  meter/sec
 ZDOT =      16562
651816                 ZDOT =        5068
042616

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1238507
59                 X    =         -377497
11
 Y    =      -19865467
80  feet           Y    =        -6054994
58  meter
 Z    =        9372765
88                 Z    =         2856819
04
 XDOT =      16381
138105                 XDOT =        4992
970895
 YDOT =       6911
105716  feet/sec       YDOT =        2106
505022  meter/sec
 ZDOT =      16636
122946                 ZDOT =        5070
690274


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   07014
55758515  
00020000  00000-0  20000-3 0  9024
2 25544  51
6287 177
8015 0023146  91
3949 268
9867 15
77036227 26511


Satellite: ISS
Catalog Number: 25544
Epoch time:      07014
55758515   =   yrday
fracday
Element set:     902
Inclination:       51
6287  deg
RA of node:       177
8015  deg
Eccentricity:     
0023146     
Arg of perigee:    91
3949  deg
Mean anomaly:     268
9867  deg
Mean motion:   15
77036227  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2651
Checksum:              317


Coasting Arc #4 (Orbit 2665)
---------------------------------------

Vector Time (GMT): 2007/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4263785
49                 A    =         6717258
63  meter
 Y    =        3606853
28  meter          E    =           
0029318
 Z    =       -3760648
36                 I    =           51
67341
 XDOT =      -5878
691636                 Wp   =           97
21404
 YDOT =      -2552
976478  meter/sec      RA   =          171
93294  deg
 ZDOT =       4241
183783                 TA   =          217
38877
                                          MA   =          217
59312
                                          Ha   =            193
809  n
mi
                                          Hp   =            170
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13988797
54                 X    =        -4285532
55
 Y    =       11833508
14  feet           Y    =         3559052
19  meter
 Z    =      -12338085
18                 Z    =        -3781413
98
 XDOT =     -19287
046051                 XDOT =       -5870
309702
 YDOT =      -8375
907081  feet/sec       YDOT =       -2618
669008  meter/sec
 ZDOT =      13914
644957                 ZDOT =        4212
645341

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16448684
27                 X    =        -5013558
97
 Y    =       -7952593
16  feet           Y    =        -2423950
39  meter
 Z    =      -12415464
76                 Z    =        -3784233
66
 XDOT =       -741
181442                 XDOT =        -225
912104
 YDOT =     -19897
811256  feet/sec       YDOT =       -6064
852871  meter/sec
 ZDOT =      13807
337672                 ZDOT =        4208
476522


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   07015
50808865  
00020000  00000-0  20000-3 0  9035
2 25544  51
6297 172
8971 0023229  94
9107 265
4710 15
77057623 26663


Satellite: ISS
Catalog Number: 25544
Epoch time:      07015
50808865   =   yrday
fracday
Element set:     903
Inclination:       51
6297  deg
RA of node:       172
8971  deg
Eccentricity:     
0023229     
Arg of perigee:    94
9107  deg
Mean anomaly:     265
4710  deg
Mean motion:   15
77057623  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2666
Checksum:              310


Coasting Arc #5 (Orbit 2681)
---------------------------------------

Vector Time (GMT): 2007/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4422771
17                 A    =         6715064
86  meter
 Y    =        2533273
26  meter          E    =           
0031477
 Z    =       -4398656
16                 I    =           51
69455
 XDOT =      -5619
431368                 Wp   =           90
68865
 YDOT =       4032
115833  meter/sec      RA   =          166
82700  deg
 ZDOT =      -3348
993230                 TA   =          145
67691
                                          MA   =          145
47313
                                          Ha   =            193
754  n
mi
                                          Hp   =            170
719

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14510404
09                 X    =         4415482
63
 Y    =        8311263
97  feet           Y    =         2582691
05  meter
 Z    =      -14431286
63                 Z    =        -4377187
95
 XDOT =     -18436
454618                 XDOT =       -5647
832826
 YDOT =      13228
726486  feet/sec       YDOT =        3969
117926  meter/sec
 ZDOT =     -10987
510597                 ZDOT =       -3376
360451

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1420630
33                 X    =         -433008
12
 Y    =       16731307
34  feet           Y    =         5099702
48  meter
 Z    =      -14350475
02                 Z    =        -4374024
79
 XDOT =     -18499
100578                 XDOT =       -5638
525856
 YDOT =     -11023
073700  feet/sec       YDOT =       -3359
832864  meter/sec
 ZDOT =     -11089
597832                 ZDOT =       -3380
109419


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   07016
52193714  
00020000  00000-0  20000-3 0  9049
2 25544  51
6300 167
6653 0023190  98
5231 261
8563 15
77097885 26820


Satellite: ISS
Catalog Number: 25544
Epoch time:      07016
52193714   =   yrday
fracday
Element set:     904
Inclination:       51
6300  deg
RA of node:       167
6653  deg
Eccentricity:     
0023190     
Arg of perigee:    98
5231  deg
Mean anomaly:     261
8563  deg
Mean motion:   15
77097885  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2682
Checksum:              301


Coasting Arc #6 (Orbit 2697)
---------------------------------------

Vector Time (GMT): 2007/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5403533
56                 A    =         6721576
35  meter
 Y    =       -3441421
32  meter          E    =           
0037141
 Z    =        1982332
05                 I    =           51
74402
 XDOT =       4170
994383                 Wp   =          106
15779
 YDOT =       3274
696455  meter/sec      RA   =          161
62967  deg
 ZDOT =      -5608
503442                 TA   =           51
72865
                                          MA   =           51
39509
                                          Ha   =            193
645  n
mi
                                          Hp   =            170
664

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17728128
48                 X    =         5431984
80
 Y    =      -11290752
37  feet           Y    =        -3380837
22  meter
 Z    =        6503714
07                 Z    =         2008650
51
 XDOT =      13684
364772                 XDOT =        4161
310841
 YDOT =      10743
754772  feet/sec       YDOT =        3321
285524  meter/sec
 ZDOT =     -18400
601843                 ZDOT =       -5588
264169

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17865376
03                 X    =         5445366
61
 Y    =       11014009
18  feet           Y    =         3357070
00  meter
 Z    =        6601959
29                 Z    =         2012277
19
 XDOT =      -2869
420976                 XDOT =        -874
599513
 YDOT =      15785
383678  feet/sec       YDOT =        4811
384945  meter/sec
 ZDOT =     -18324
291566                 ZDOT =       -5585
244069


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   07017
53576399  
00020000  00000-0  20000-3 0  9056
2 25544  51
6296 162
4326 0023117 102
4923 257
8830 15
77114188 26981


Satellite: ISS
Catalog Number: 25544
Epoch time:      07017
53576399   =   yrday
fracday
Element set:     905
Inclination:       51
6296  deg
RA of node:       162
4326  deg
Eccentricity:     
0023117     
Arg of perigee:   102
4923  deg
Mean anomaly:     257
8830  deg
Mean motion:   15
77114188  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2698
Checksum:              309


Coasting Arc #7 (Orbit 2713)
---------------------------------------

Vector Time (GMT): 2007/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2797565
94                 A    =         6711488
61  meter
 Y    =       -3221619
77  meter          E    =           
0026783
 Z    =        5160442
79                 I    =           51
73875
 XDOT =       6592
593690                 Wp   =          109
05197
 YDOT =      -3856
936316  meter/sec      RA   =          156
50617  deg
 ZDOT =       1152
682689                 TA   =          329
91565
                                          MA   =          330
06923
                                          Ha   =            193
597  n
mi
                                          Hp   =            170
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9178365
93                 X    =        -2786401
28
 Y    =      -10569618
67  feet           Y    =        -3252841
98  meter
 Z    =       16930586
58                 Z    =         5146879
23
 XDOT =      21629
244389                 XDOT =        6629
633141
 YDOT =     -12653
990537  feet/sec       YDOT =       -3783
007323  meter/sec
 ZDOT =       3781
767353                 ZDOT =        1184
798168

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5256946
42                 X    =         1602317
27
 Y    =      -13040610
85  feet           Y    =        -3974778
19  meter
 Z    =       16879306
41                 Z    =         5144812
59
 XDOT =      20083
049072                 XDOT =        6121
313357
 YDOT =      13203
325645  feet/sec       YDOT =        4024
373657  meter/sec
 ZDOT =       3901
712048                 ZDOT =        1189
241832


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   07018
54956762  
00020000  00000-0  20000-3 0  9065
2 25544  51
6310 157
2015 0022961 106
1175 254
2520 15
77187021 27143


Satellite: ISS
Catalog Number: 25544
Epoch time:      07018
54956762   =   yrday
fracday
Element set:     906
Inclination:       51
6310  deg
RA of node:       157
2015  deg
Eccentricity:     
0022961     
Arg of perigee:   106
1175  deg
Mean anomaly:     254
2520  deg
Mean motion:   15
77187021  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2714
Checksum:              270


Coasting Arc #8 (Orbit 2729)
---------------------------------------

Vector Time (GMT): 2007/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5913886
11                 A    =         6723092
57  meter
 Y    =        3196072
12  meter          E    =           
0030525
 Z    =          39540
02                 I    =           51
80510
 XDOT =      -2211
943679                 Wp   =           88
63382
 YDOT =      -4217
174082  meter/sec      RA   =          151
34650  deg
 ZDOT =       6051
733402                 TA   =          271
79499
                                          MA   =          272
14458
                                          Ha   =            193
492  n
mi
                                          Hp   =            170
720

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19402513
47                 X    =        -5949377
58
 Y    =       10485800
93  feet           Y    =         3129741
31  meter
 Z    =         129724
47                 Z    =           10725
33
 XDOT =      -7257
033069                 XDOT =       -2194
019623
 YDOT =     -13835
872973  feet/sec       YDOT =       -4241
809723  meter/sec
 ZDOT =      19854
768380                 ZDOT =        6041
031156

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18318714
83                 X    =        -5583544
28
 Y    =      -12282124
36  feet           Y    =        -3743591
51  meter
 Z    =          22061
74                 Z    =            6724
42
 XDOT =       7913
926309                 XDOT =        2412
164739
 YDOT =     -11629
579969  feet/sec       YDOT =       -3544
695974  meter/sec
 ZDOT =      19814
082655                 ZDOT =        6039
332393


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   07019
56335067  
00020000  00000-0  20000-3 0  9078
2 25544  51
6324 151
9703 0023079 109
8076 250
5580 15
77198896 27309


Satellite: ISS
Catalog Number: 25544
Epoch time:      07019
56335067   =   yrday
fracday
Element set:     907
Inclination:       51
6324  deg
RA of node:       151
9703  deg
Eccentricity:     
0023079     
Arg of perigee:   109
8076  deg
Mean anomaly:     250
5580  deg
Mean motion:   15
77198896  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2730
Checksum:              309


Coasting Arc #9 (Orbit 2744)
---------------------------------------

Vector Time (GMT): 2007/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1042261
10                 A    =         6711432
94  meter
 Y    =        4195928
61  meter          E    =           
0036987
 Z    =       -5165587
79                 I    =           51
79104
 XDOT =      -6801
914046                 Wp   =          108
40627
 YDOT =       3311
266764  meter/sec      RA   =          146
18703  deg
 ZDOT =       1313
506042                 TA   =          174
18983
                                          MA   =          174
14681
                                          Ha   =            193
368  n
mi
                                          Hp   =            170
733

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3419491
78                 X    =         1020356
89
 Y    =       13766169
97  feet           Y    =         4207461
69  meter
 Z    =      -16947466
49                 Z    =        -5160577
50
 XDOT =     -22315
990966                 XDOT =       -6844
816153
 YDOT =      10863
736101  feet/sec       YDOT =        3234
963990  meter/sec
 ZDOT =       4309
403024                 ZDOT =        1280
359408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10378079
48                 X    =        -3163238
63
 Y    =        9703142
10  feet           Y    =         2957517
71  meter
 Z    =      -16928126
88                 Z    =        -5159693
07
 XDOT =     -19563
821437                 XDOT =       -5963
052774
 YDOT =     -13601
063326  feet/sec       YDOT =       -4145
604102  meter/sec
 ZDOT =       4185
496578                 ZDOT =        1275
739357


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   07020
51375126  
00020000  00000-0  20000-3 0  9086
2 25544  51
6328 147
0663 0023017 113
2162 247
1430 15
77244454 27455


Satellite: ISS
Catalog Number: 25544
Epoch time:      07020
51375126   =   yrday
fracday
Element set:     908
Inclination:       51
6328  deg
RA of node:       147
0663  deg
Eccentricity:     
0023017     
Arg of perigee:   113
2162  deg
Mean anomaly:     247
1430  deg
Mean motion:   15
77244454  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2745
Checksum:              263


Coasting Arc #10 (Orbit 2760)
---------------------------------------

Vector Time (GMT): 2007/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5838339
31                 A    =         6720811
57  meter
 Y    =       -2477149
76  meter          E    =           
0028826
 Z    =       -2217040
98                 I    =           51
84635
 XDOT =        218
824606                 Wp   =          121
61071
 YDOT =       5383
833233  meter/sec      RA   =          141
06900  deg
 ZDOT =      -5506
026322                 TA   =           83
20159
                                          MA   =           82
87367
                                          Ha   =            193
337  n
mi
                                          Hp   =            170
841

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19154656
54                 X    =         5876374
91
 Y    =       -8127131
75  feet           Y    =        -2411649
42  meter
 Z    =       -7273756
49                 Z    =        -2188586
89
 XDOT =        717
928498                 XDOT =         185
352061
 YDOT =      17663
494859  feet/sec       YDOT =        5386
093375  meter/sec
 ZDOT =     -18064
390819                 ZDOT =       -5505
044333

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16579084
21                 X    =         5053304
87
 Y    =       12634156
86  feet           Y    =         3850891
01  meter
 Z    =       -7167336
91                 Z    =        -2184604
29
 XDOT =     -14009
412540                 XDOT =       -4270
068942
 YDOT =       8264
517310  feet/sec       YDOT =        2519
024876  meter/sec
 ZDOT =     -18060
002990                 ZDOT =       -5504
688911


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   07021
52749019  
00020000  00000-0  20000-3 0  9095
2 25544  51
6332 141
8332 0022961 117
0252 243
3260 15
77264366 27615


Satellite: ISS
Catalog Number: 25544
Epoch time:      07021
52749019   =   yrday
fracday
Element set:     909
Inclination:       51
6332  deg
RA of node:       141
8332  deg
Eccentricity:     
0022961     
Arg of perigee:   117
0252  deg
Mean anomaly:     243
3260  deg
Mean motion:   15
77264366  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2761
Checksum:              272


Coasting Arc #11 (Orbit 2776)
---------------------------------------

Vector Time (GMT): 2007/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         553181
84                 A    =         6715012
60  meter
 Y    =       -5162633
20  meter          E    =           
0030628
 Z    =        4227653
98                 I    =           51
84879
 XDOT =       6435
071678                 Wp   =          106
75388
 YDOT =      -2282
710048  meter/sec      RA   =          135
87923  deg
 ZDOT =      -3616
886474                 TA   =           19
83634
                                          MA   =           19
71750
                                          Ha   =            193
271  n
mi
                                          Hp   =            170
877

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1814901
03                 X    =          590333
35
 Y    =      -16937772
95  feet           Y    =        -5156239
60  meter
 Z    =       13870255
83                 Z    =         4230431
37
 XDOT =      21112
439888                 XDOT =        6477
688742
 YDOT =      -7489
206195  feet/sec       YDOT =       -2210
511108  meter/sec
 ZDOT =     -11866
425441                 ZDOT =       -3585
522226

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15447768
58                 X    =         4708479
86
 Y    =       -7160873
19  feet           Y    =        -2182634
15  meter
 Z    =       13879998
42                 Z    =         4230623
52
 XDOT =      16736
769711                 XDOT =        5101
367408
 YDOT =      13251
421035  feet/sec       YDOT =        4039
033132  meter/sec
 ZDOT =     -11749
057049                 ZDOT =       -3581
112589


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   07022
54120747  
00020000  00000-0  20000-3 0  9101
2 25544  51
6336 136
6021 0023005 120
5357 239
8082 15
77274638 27773


Satellite: ISS
Catalog Number: 25544
Epoch time:      07022
54120747   =   yrday
fracday
Element set:     910
Inclination:       51
6336  deg
RA of node:       136
6021  deg
Eccentricity:     
0023005     
Arg of perigee:   120
5357  deg
Mean anomaly:     239
8082  deg
Mean motion:   15
77274638  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2777
Checksum:              276


Coasting Arc #12 (Orbit 2792)
---------------------------------------

Vector Time (GMT): 2007/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5255785
36                 A    =         6715936
54  meter
 Y    =        1357780
65  meter          E    =           
0033356
 Z    =        3940217
77                 I    =           51
87251
 XDOT =       1382
991443                 Wp   =          116
69429
 YDOT =      -6435
248916  meter/sec      RA   =          130
78487  deg
 ZDOT =       4021
634538                 TA   =          291
61551
                                          MA   =          291
97053
                                          Ha   =            193
100  n
mi
                                          Hp   =            170
964

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17243390
28                 X    =        -5289718
12
 Y    =        4454660
94  feet           Y    =         1298817
74  meter
 Z    =       12927223
66                 Z    =         3914603
27
 XDOT =       4537
373500                 XDOT =        1435
312535
 YDOT =     -21113
021377  feet/sec       YDOT =       -6419
491063  meter/sec
 ZDOT =      13194
339036                 ZDOT =        4028
479951

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12891519
54                 X    =        -3929335
16
 Y    =      -12387819
64  feet           Y    =        -3775807
43  meter
 Z    =       12831300
50                 Z    =         3910980
39
 XDOT =      19403
879482                 XDOT =        5914
302466
 YDOT =      -6361
197145  feet/sec       YDOT =       -1938
892890  meter/sec
 ZDOT =      13219
178089                 ZDOT =        4029
205482


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   07023
55489887  
00020000  00000-0  20000-3 0  9117
2 25544  51
6339 131
3700 0022850 124
4653 235
8675 15
77366077 27932


Satellite: ISS
Catalog Number: 25544
Epoch time:      07023
55489887   =   yrday
fracday
Element set:     911
Inclination:       51
6339  deg
RA of node:       131
3700  deg
Eccentricity:     
0022850     
Arg of perigee:   124
4653  deg
Mean anomaly:     235
8675  deg
Mean motion:   15
77366077  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2793
Checksum:              311

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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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