Date: January 18th 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 2666)
---------------------------------------

Vector Time (GMT): 2007/015/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6632001
16                 A    =         6722956
47  meter
 Y    =         -97215
80  meter          E    =           
0030493
 Z    =       -1082012
15                 I    =           51
69394
 XDOT =       -871
071756                 Wp   =          108
85844
 YDOT =       4851
122306  meter/sec      RA   =          171
75632  deg
 ZDOT =      -5919
680675                 TA   =           82
98140
                                          MA   =           82
63469
                                          Ha   =            193
752  n
mi
                                          Hp   =            170
725

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21758533
99                 X    =         6637851
51
 Y    =        -318949
48  feet           Y    =          -23020
21  meter
 Z    =       -3549908
64                 Z    =        -1049779
97
 XDOT =      -2857
846970                 XDOT =        -896
496468
 YDOT =      15915
755596  feet/sec       YDOT =        4841
240173  meter/sec
 ZDOT =     -19421
524525                 ZDOT =       -5923
973379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13915202
42                 X    =         4241353
70
 Y    =       16755471
80  feet           Y    =         5107067
81  meter
 Z    =       -3429094
33                 Z    =        -1045187
95
 XDOT =     -12895
580004                 XDOT =       -3930
572785
 YDOT =       6832
339724  feet/sec       YDOT =        2082
497148  meter/sec
 ZDOT =     -19436
993937                 ZDOT =       -5924
395752


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
57146547  
00020000  00000-0  20000-3 0  9001
2 25544  51
6298 172
5721 0023016  95
0750 265
3042 15
77075813 26673


Satellite: ISS
Catalog Number: 25544
Epoch time:      07015
57146547   =   yrday
fracday
Element set:     900
Inclination:       51
6298  deg
RA of node:       172
5721  deg
Eccentricity:     
0023016     
Arg of perigee:    95
0750  deg
Mean anomaly:     265
3042  deg
Mean motion:   15
77075813  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2667
Checksum:              286


Coasting Arc #2 (Orbit 2682)
---------------------------------------

Vector Time (GMT): 2007/016/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1645792
28                 A    =         6713151
93  meter
 Y    =       -4324012
69  meter          E    =           
0028505
 Z    =        4839783
07                 I    =           51
68976
 XDOT =       7357
434546                 Wp   =           90
41451
 YDOT =        154
269435  meter/sec      RA   =          166
57246  deg
 ZDOT =      -2352
483873                 TA   =           22
48123
                                          MA   =           22
35658
                                          Ha   =            193
751  n
mi
                                          Hp   =            170
740

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5399580
98                 X    =         1670511
22
 Y    =      -14186393
33  feet           Y    =        -4305471
04  meter
 Z    =       15878553
39                 Z    =         4847837
62
 XDOT =      24138
564784                 XDOT =        7366
590451
 YDOT =        506
133318  feet/sec       YDOT =         236
595907  meter/sec
 ZDOT =      -7718
122942                 ZDOT =       -2316
719672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14294221
94                 X    =         4356878
85
 Y    =       -5014195
44  feet           Y    =        -1528326
77  meter
 Z    =       15908197
62                 Z    =         4848818
63
 XDOT =      14742
382927                 XDOT =        4493
478316
 YDOT =      17844
845531  feet/sec       YDOT =        5439
108918  meter/sec
 ZDOT =      -7584
017468                 ZDOT =       -2311
608524


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
58531650  
00020000  00000-0  20000-3 0  9017
2 25544  51
6306 167
3412 0023095  99
0192 261
3587 15
77058889 26835


Satellite: ISS
Catalog Number: 25544
Epoch time:      07016
58531650   =   yrday
fracday
Element set:     901
Inclination:       51
6306  deg
RA of node:       167
3412  deg
Eccentricity:     
0023095     
Arg of perigee:    99
0192  deg
Mean anomaly:     261
3587  deg
Mean motion:   15
77058889  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2683
Checksum:              304


Coasting Arc #3 (Orbit 2698)
---------------------------------------

Vector Time (GMT): 2007/017/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6016757
14                 A    =         6719533
84  meter
 Y    =        -423907
05  meter          E    =           
0035789
 Z    =        2935427
56                 I    =           51
74077
 XDOT =       2837
072029                 Wp   =           95
49756
 YDOT =      -5126
329079  meter/sec      RA   =          161
46169  deg
 ZDOT =       5019
436542                 TA   =          298
37144
                                          MA   =          298
73183
                                          Ha   =            193
602  n
mi
                                          Hp   =            170
732

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19740016
86                 X    =        -6025829
27
 Y    =       -1390771
16  feet           Y    =         -491240
94  meter
 Z    =        9630667
86                 Z    =         2906176
62
 XDOT =       9307
979097                 XDOT =        2869
801469
 YDOT =     -16818
664956  feet/sec       YDOT =       -5094
421105  meter/sec
 ZDOT =      16467
967658                 ZDOT =        5033
297513

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11891899
05                 X    =        -3624650
83
 Y    =      -15883541
20  feet           Y    =        -4841303
36  meter
 Z    =        9520931
11                 Z    =         2901979
80
 XDOT =      17592
766898                 XDOT =        5362
275351
 YDOT =      -3159
320908  feet/sec       YDOT =        -962
961013  meter/sec
 ZDOT =      16519
285660                 ZDOT =        5035
078269


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
59914124  
00020000  00000-0  20000-3 0  9021
2 25544  51
6319 162
1101 0022925 102
9916 257
3810 15
77160463 26999


Satellite: ISS
Catalog Number: 25544
Epoch time:      07017
59914124   =   yrday
fracday
Element set:     902
Inclination:       51
6319  deg
RA of node:       162
1101  deg
Eccentricity:     
0022925     
Arg of perigee:   102
9916  deg
Mean anomaly:     257
3810  deg
Mean motion:   15
77160463  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2699
Checksum:              282


Coasting Arc #4 (Orbit 2713)
---------------------------------------

Vector Time (GMT): 2007/018/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3226293
31                 A    =         6717236
04  meter
 Y    =        4606910
09  meter          E    =           
0028694
 Z    =       -3703125
01                 I    =           51
76034
 XDOT =      -6286
642261                 Wp   =          105
61568
 YDOT =       -950
084775  meter/sec      RA   =          156
26008  deg
 ZDOT =       4315
245708                 TA   =          209
94497
                                          MA   =          210
10941
                                          Ha   =            193
497  n
mi
                                          Hp   =            170
767

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10584951
79                 X    =        -3259579
98
 Y    =       15114534
40  feet           Y    =         4570646
26  meter
 Z    =      -12149360
28                 Z    =        -3718878
19
 XDOT =     -20625
466736                 XDOT =       -6296
513205
 YDOT =      -3117
076032  feet/sec       YDOT =       -1020
441278  meter/sec
 ZDOT =      14157
630275                 ZDOT =        4284
681852

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18276670
03                 X    =        -5570729
03
 Y    =        2242570
61  feet           Y    =          683535
52  meter
 Z    =      -12207846
63                 Z    =        -3720951
65
 XDOT =     -11320
676103                 XDOT =       -3450
542076
 YDOT =     -16173
667894  feet/sec       YDOT =       -4929
733974  meter/sec
 ZDOT =      14042
886304                 ZDOT =        4280
271746


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
54958553  
00020000  00000-0  20000-3 0  9032
2 25544  51
6324 157
2061 0022806 105
9956 254
3723 15
77139120 27144


Satellite: ISS
Catalog Number: 25544
Epoch time:      07018
54958553   =   yrday
fracday
Element set:     903
Inclination:       51
6324  deg
RA of node:       157
2061  deg
Eccentricity:     
0022806     
Arg of perigee:   105
9956  deg
Mean anomaly:     254
3723  deg
Mean motion:   15
77139120  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2714
Checksum:              288


Coasting Arc #5 (Orbit 2729)
---------------------------------------

Vector Time (GMT): 2007/019/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4850926
23                 A    =         6714584
28  meter
 Y    =        1344774
69  meter          E    =           
0030645
 Z    =       -4467032
47                 I    =           51
77797
 XDOT =      -4450
306838                 Wp   =           98
58807
 YDOT =       5364
696051  meter/sec      RA   =          151
15858  deg
 ZDOT =      -3241
057563                 TA   =          139
06900
                                          MA   =          138
83854
                                          Ha   =            193
437  n
mi
                                          Hp   =            170
930

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15915112
29                 X    =         4857227
64
 Y    =        4411990
47  feet           Y    =         1399056
18  meter
 Z    =      -14655618
34                 Z    =        -4443451
90
 XDOT =     -14600
744220                 XDOT =       -4494
220862
 YDOT =      17600
708829  feet/sec       YDOT =        5314
685064  meter/sec
 ZDOT =     -10633
390955                 ZDOT =       -3262
782603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7634475
09                 X    =         2326988
01
 Y    =       14732986
82  feet           Y    =         4490614
38  meter
 Z    =      -14567000
30                 Z    =        -4440021
69
 XDOT =     -21719
666582                 XDOT =       -6620
154374
 YDOT =        737
484378  feet/sec       YDOT =         224
785238  meter/sec
 ZDOT =     -10714
182603                 ZDOT =       -3265
682857


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
56336997  
00020000  00000-0  20000-3 0  9048
2 25544  51
6332 151
9738 0022778 110
0065 250
3555 15
77175726 27300


Satellite: ISS
Catalog Number: 25544
Epoch time:      07019
56336997   =   yrday
fracday
Element set:     904
Inclination:       51
6332  deg
RA of node:       151
9738  deg
Eccentricity:     
0022778     
Arg of perigee:   110
0065  deg
Mean anomaly:     250
3555  deg
Mean motion:   15
77175726  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2730
Checksum:              300


Coasting Arc #6 (Orbit 2745)
---------------------------------------

Vector Time (GMT): 2007/020/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4390004
39                 A    =         6721542
03  meter
 Y    =       -4717756
10  meter          E    =           
0037021
 Z    =        1848195
04                 I    =           51
82666
 XDOT =       4757
998430                 Wp   =          113
76718
 YDOT =       2173
862889  meter/sec      RA   =          145
96948  deg
 ZDOT =      -5678
556388                 TA   =           45
70427
                                          MA   =           45
40122
                                          Ha   =            193
345  n
mi
                                          Hp   =            170
821

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14402901
55                 X    =         4433454
81
 Y    =      -15478202
41  feet           Y    =        -4668421
83  meter
 Z    =        6063632
02                 Z    =         1869626
20
 XDOT =      15610
231071                 XDOT =        4760
920926
 YDOT =       7132
096091  feet/sec       YDOT =        2227
086268  meter/sec
 ZDOT =     -18630
434344                 ZDOT =       -5655
435462

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21117003
36                 X    =         6436462
62
 Y    =        -341530
68  feet           Y    =         -104098
55  meter
 Z    =        6143409
66                 Z    =         1872511
26
 XDOT =       5702
791380                 XDOT =        1738
210813
 YDOT =      14738
151610  feet/sec       YDOT =        4492
188611  meter/sec
 ZDOT =     -18543
422002                 ZDOT =       -5652
035026


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
57713245  
00020000  00000-0  20000-3 0  9057
2 25544  51
6335 146
7425 0022868 113
6635 246
6933 15
77210147 27462


Satellite: ISS
Catalog Number: 25544
Epoch time:      07020
57713245   =   yrday
fracday
Element set:     905
Inclination:       51
6335  deg
RA of node:       146
7425  deg
Eccentricity:     
0022868     
Arg of perigee:   113
6635  deg
Mean anomaly:     246
6933  deg
Mean motion:   15
77210147  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2746
Checksum:              291


Coasting Arc #7 (Orbit 2761)
---------------------------------------

Vector Time (GMT): 2007/021/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3401779
58                 A    =         6711005
04  meter
 Y    =       -2501935
97  meter          E    =           
0026220
 Z    =        5197859
00                 I    =           51
81572
 XDOT =       5443
524926                 Wp   =          118
14284
 YDOT =      -5395
346776  meter/sec      RA   =          140
84790  deg
 ZDOT =        949
809249                 TA   =          322
76469
                                          MA   =          322
94621
                                          Ha   =            193
243  n
mi
                                          Hp   =            170
861

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11160694
16                 X    =        -3398799
28
 Y    =       -8208451
34  feet           Y    =        -2539960
15  meter
 Z    =       17053343
18                 Z    =         5181340
75
 XDOT =      17859
333746                 XDOT =        5498
838019
 YDOT =     -17701
268949  feet/sec       YDOT =       -5334
165024  meter/sec
 ZDOT =       3116
172077                 ZDOT =         976
387216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2102369
18                 X    =         -640802
13
 Y    =      -13771005
27  feet           Y    =        -4197402
41  meter
 Z    =       16991048
79                 Z    =         5178871
67
 XDOT =      24127
977681                 XDOT =        7354
207597
 YDOT =        347
442655  feet/sec       YDOT =         105
900521  meter/sec
 ZDOT =       3215
172105                 ZDOT =         979
984458


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
59087005  
00020000  00000-0  20000-3 0  9069
2 25544  51
6343 141
5110 0022670 117
2572 243
0905 15
77304630 27625


Satellite: ISS
Catalog Number: 25544
Epoch time:      07021
59087005   =   yrday
fracday
Element set:     906
Inclination:       51
6343  deg
RA of node:       141
5110  deg
Eccentricity:     
0022670     
Arg of perigee:   117
2572  deg
Mean anomaly:     243
0905  deg
Mean motion:   15
77304630  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2762
Checksum:              256


Coasting Arc #8 (Orbit 2777)
---------------------------------------

Vector Time (GMT): 2007/022/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4946423
15                 A    =         6722809
49  meter
 Y    =        4547248
84  meter          E    =           
0029099
 Z    =         255652
95                 I    =           51
87686
 XDOT =      -3033
077343                 Wp   =           95
93628
 YDOT =      -3672
476670  meter/sec      RA   =          135
69659  deg
 ZDOT =       6048
643373                 TA   =          266
83400
                                          MA   =          267
16698
                                          Ha   =            193
118  n
mi
                                          Hp   =            171
003

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16228422
40                 X    =        -4998145
39
 Y    =       14918795
42  feet           Y    =         4491645
98  meter
 Z    =         838756
39                 Z    =          231498
31
 XDOT =      -9951
041153                 XDOT =       -3021
168253
 YDOT =     -12048
807973  feet/sec       YDOT =       -3706
327805  meter/sec
 ZDOT =      19844
630490                 ZDOT =        6033
937878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22038013
32                 X    =        -6717186
46
 Y    =        -633269
63  feet           Y    =         -193020
58  meter
 Z    =         748732
89                 Z    =          228213
78
 XDOT =       1149
371336                 XDOT =         350
328383
 YDOT =     -14044
586818  feet/sec       YDOT =       -4280
790062  meter/sec
 ZDOT =      19788
978628                 ZDOT =        6031
680686


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
60458888  
00020000  00000-0  20000-3 0  9074
2 25544  51
6344 136
2797 0022688 120
5828 239
7579 15
77290320 27784


Satellite: ISS
Catalog Number: 25544
Epoch time:      07022
60458888   =   yrday
fracday
Element set:     907
Inclination:       51
6344  deg
RA of node:       136
2797  deg
Eccentricity:     
0022688     
Arg of perigee:   120
5828  deg
Mean anomaly:     239
7579  deg
Mean motion:   15
77290320  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2778
Checksum:              330


Coasting Arc #9 (Orbit 2792)
---------------------------------------

Vector Time (GMT): 2007/023/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1893598
22                 A    =         6711420
83  meter
 Y    =        3958793
04  meter          E    =           
0035762
 Z    =       -5109068
97                 I    =           51
85806
 XDOT =      -5764
261331                 Wp   =          115
91746
 YDOT =       4818
581198  meter/sec      RA   =          130
53638  deg
 ZDOT =       1590
581722                 TA   =          169
38926
                                          MA   =          169
31360
                                          Ha   =            192
959  n
mi
                                          Hp   =            171
071

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6212592
59                 X    =         1874008
15
 Y    =       12988166
14  feet           Y    =         3979858
87  meter
 Z    =      -16762037
31                 Z    =        -5099917
57
 XDOT =     -18911
618540                 XDOT =       -5825
441587
 YDOT =      15808
993432  feet/sec       YDOT =        4753
779912  meter/sec
 ZDOT =       5218
443971                 ZDOT =        1562
430968

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4305332
25                 X    =        -1312265
27
 Y    =       13781150
11  feet           Y    =         4200494
55  meter
 Z    =      -16727183
78                 Z    =        -5098445
62
 XDOT =     -23622
789034                 XDOT =       -7200
226098
 YDOT =      -1146
659939  feet/sec       YDOT =        -349
501949  meter/sec
 ZDOT =       5113
458690                 ZDOT =        1558
582209


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
55492763  
00020000  00000-0  20000-3 0  9080
2 25544  51
6340 131
3748 0022614 124
0572 236
2744 15
77342700 27939


Satellite: ISS
Catalog Number: 25544
Epoch time:      07023
55492763   =   yrday
fracday
Element set:     908
Inclination:       51
6340  deg
RA of node:       131
3748  deg
Eccentricity:     
0022614     
Arg of perigee:   124
0572  deg
Mean anomaly:     236
2744  deg
Mean motion:   15
77342700  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2793
Checksum:              281


Coasting Arc #10 (Orbit 2808)
---------------------------------------

Vector Time (GMT): 2007/024/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5019429
71                 A    =         6720046
09  meter
 Y    =       -3717922
01  meter          E    =           
0028036
 Z    =       -2468158
10                 I    =           51
90398
 XDOT =       1355
870395                 Wp   =          128
97784
 YDOT =       5357
365785  meter/sec      RA   =          125
42652  deg
 ZDOT =      -5370
345350                 TA   =           78
85910
                                          MA   =           78
54401
                                          Ha   =            192
943  n
mi
                                          Hp   =            171
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16467945
25                 X    =         5072620
68
 Y    =      -12197906
84  feet           Y    =        -3661494
48  meter
 Z    =       -8097631
57                 Z    =        -2443644
95
 XDOT =       4448
393684                 XDOT =        1321
950588
 YDOT =      17576
659401  feet/sec       YDOT =        5372
338355  meter/sec
 ZDOT =     -17619
243273                 ZDOT =       -5363
840891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20424061
61                 X    =         6225253
98
 Y    =        2076816
15  feet           Y    =          633013
56  meter
 Z    =       -8006143
33                 Z    =        -2440272
49
 XDOT =      -8304
058198                 XDOT =       -2531
076939
 YDOT =      14576
631507  feet/sec       YDOT =        4442
957283  meter/sec
 ZDOT =     -17594
139506                 ZDOT =       -5362
693721


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   07024
56860154  
00020000  00000-0  20000-3 0  9096
2 25544  51
6331 126
1421 0022598 128
0090 232
3119 15
77351959 28096


Satellite: ISS
Catalog Number: 25544
Epoch time:      07024
56860154   =   yrday
fracday
Element set:     909
Inclination:       51
6331  deg
RA of node:       126
1421  deg
Eccentricity:     
0022598     
Arg of perigee:   128
0090  deg
Mean anomaly:     232
3119  deg
Mean motion:   15
77351959  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2809
Checksum:              284


Coasting Arc #11 (Orbit 2824)
---------------------------------------

Vector Time (GMT): 2007/025/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -570630
81                 A    =         6715304
04  meter
 Y    =       -5309650
11  meter          E    =           
0029980
 Z    =        4039425
45                 I    =           51
90466
 XDOT =       5626
940135                 Wp   =          114
54400
 YDOT =      -3580
401344  meter/sec      RA   =          120
23652  deg
 ZDOT =      -3901
217181                 TA   =           15
41027
                                          MA   =           15
31917
                                          Ha   =            192
719  n
mi
                                          Hp   =            171
238

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1872148
32                 X    =         -530837
72
 Y    =      -17420111
91  feet           Y    =        -5315808
90  meter
 Z    =       13252708
16                 Z    =         4036749
79
 XDOT =      18461
089682                 XDOT =        5685
509683
 YDOT =     -11746
723569  feet/sec       YDOT =       -3517
150121  meter/sec
 ZDOT =     -12799
268968                 ZDOT =       -3873
739697

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10029019
09                 X    =         3056845
02
 Y    =      -14375959
68  feet           Y    =        -4381792
51  meter
 Z    =       13241981
39                 Z    =         4036155
93
 XDOT =      20628
388237                 XDOT =        6287
532735
 YDOT =       2664
975466  feet/sec       YDOT =         812
284522  meter/sec
 ZDOT =     -12696
631262                 ZDOT =       -3869
933209


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   07025
58225200  
00020000  00000-0  20000-3 0  9108
2 25544  51
6335 120
9095 0022427 131
3263 228
9836 15
77421409 28252


Satellite: ISS
Catalog Number: 25544
Epoch time:      07025
58225200   =   yrday
fracday
Element set:     910
Inclination:       51
6335  deg
RA of node:       120
9095  deg
Eccentricity:     
0022427     
Arg of perigee:   131
3263  deg
Mean anomaly:     228
9836  deg
Mean motion:   15
77421409  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2825
Checksum:              272


Coasting Arc #12 (Orbit 2840)
---------------------------------------

Vector Time (GMT): 2007/026/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4706983
73                 A    =         6714889
39  meter
 Y    =        2347015
47  meter          E    =           
0031808
 Z    =        4164730
34                 I    =           51
91637
 XDOT =        -46
421820                 Wp   =          125
91407
 YDOT =      -6756
322234  meter/sec      RA   =          115
14516  deg
 ZDOT =       3717
109216                 TA   =          286
14818
                                          MA   =          286
49806
                                          Ha   =            192
637  n
mi
                                          Hp   =            171
411

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15442860
02                 X    =        -4753109
86
 Y    =        7700182
00  feet           Y    =         2294121
18  meter
 Z    =       13663813
46                 Z    =         4141752
17
 XDOT =       -152
302560                 XDOT =          11
074925
 YDOT =     -22166
411528  feet/sec       YDOT =       -6756
520118  meter/sec
 ZDOT =      12195
240209                 ZDOT =        3717
022905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16816677
89                 X    =        -5125723
42
 Y    =       -4161104
48  feet           Y    =        -1268304
64  meter
 Z    =       13577889
42                 Z    =         4138540
69
 XDOT =      13862
276233                 XDOT =        4225
221796
 YDOT =     -15824
652821  feet/sec       YDOT =       -4823
354180  meter/sec
 ZDOT =      12194
050695                 ZDOT =        3716
746652


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   07026
59588041  
00020000  00000-0  20000-3 0  9116
2 25544  51
6332 115
6771 0022407 135
3834 224
9139 15
77453222 28415


Satellite: ISS
Catalog Number: 25544
Epoch time:      07026
59588041   =   yrday
fracday
Element set:     911
Inclination:       51
6332  deg
RA of node:       115
6771  deg
Eccentricity:     
0022407     
Arg of perigee:   135
3834  deg
Mean anomaly:     224
9139  deg
Mean motion:   15
77453222  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2841
Checksum:              283

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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