Date: March 16th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7104 18 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 3616)
---------------------------------------

Vector Time (GMT): 2007/075/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2882871
67                 A    =         6718605
18  meter
 Y    =       -5407996
81  meter          E    =           
0013060
 Z    =        2733399
56                 I    =           51
43406
 XDOT =       5723
867161                 Wp   =           11
48497
 YDOT =       -453
335578  meter/sec      RA   =          221
10755  deg
 ZDOT =       5148
360654                 TA   =           19
91226
                                          MA   =           19
86134
                                          Ha   =            186
177  n
mi
                                          Hp   =            178
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9458240
40                 X    =        -2835462
51
 Y    =      -17742771
68  feet           Y    =        -5439969
43  meter
 Z    =        8967846
32                 Z    =         2719510
37
 XDOT =      18779
091736                 XDOT =        5703
501725
 YDOT =      -1487
321451  feet/sec       YDOT =        -389
441622  meter/sec
 ZDOT =      16890
947028                 ZDOT =        5176
117189

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19899101
90                 X    =        -6065246
26
 Y    =       -3039296
04  feet           Y    =         -926377
43  meter
 Z    =        8914872
37                 Z    =         2717253
10
 XDOT =       9799
232146                 XDOT =        2986
805958
 YDOT =     -14389
243405  feet/sec       YDOT =       -4385
841390  meter/sec
 ZDOT =      16995
218792                 ZDOT =        5180
142688


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   07075
72455025  
00020000  00000-0  20000-3 0  9008
2 25544  51
6342 221
7093 0014909 313
4224  46
5699 15
77643706 36171


Satellite: ISS
Catalog Number: 25544
Epoch time:      07075
72455025   =   yrday
fracday
Element set:     900
Inclination:       51
6342  deg
RA of node:       221
7093  deg
Eccentricity:     
0014909     
Arg of perigee:   313
4224  deg
Mean anomaly:      46
5699  deg
Mean motion:   15
77643706  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3617
Checksum:              291


Coasting Arc #2 (Orbit 3631)
---------------------------------------

Vector Time (GMT): 2007/076/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5564633
98                 A    =         6715499
84  meter
 Y    =        -355590
79  meter          E    =           
0010424
 Z    =       -3730826
19                 I    =           51
44653
 XDOT =      -2460
050884                 Wp   =          336
45392
 YDOT =      -5951
888785  meter/sec      RA   =          215
88078  deg
 ZDOT =       4241
877697                 TA   =          338
22226
                                          MA   =          338
26654
                                          Ha   =            186
248  n
mi
                                          Hp   =            178
303

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18256673
17                 X    =        -5542120
78
 Y    =       -1166636
44  feet           Y    =         -417692
11  meter
 Z    =      -12240243
41                 Z    =        -3757803
99
 XDOT =      -8071
033084                 XDOT =       -2413
919088
 YDOT =     -19527
194176  feet/sec       YDOT =       -5979
140117  meter/sec
 ZDOT =      13916
921579                 ZDOT =        4230
039592

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11606147
73                 X    =        -3537553
83
 Y    =       14052412
29  feet           Y    =         4283175
27  meter
 Z    =      -12341708
07                 Z    =        -3761752
62
 XDOT =     -19572
558542                 XDOT =       -5965
715844
 YDOT =      -3997
768663  feet/sec       YDOT =       -1218
519888  meter/sec
 ZDOT =      13871
570276                 ZDOT =        4228
054620


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   07076
67468760  
00020000  00000-0  20000-3 0  9014
2 25544  51
6340 216
8035 0014973 317
2946  42
7054 15
77689530 36329


Satellite: ISS
Catalog Number: 25544
Epoch time:      07076
67468760   =   yrday
fracday
Element set:     901
Inclination:       51
6340  deg
RA of node:       216
8035  deg
Eccentricity:     
0014973     
Arg of perigee:   317
2946  deg
Mean anomaly:      42
7054  deg
Mean motion:   15
77689530  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3632
Checksum:              305


Coasting Arc #3 (Orbit 3647)
---------------------------------------

Vector Time (GMT): 2007/077/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1226345
34                 A    =         6713009
34  meter
 Y    =        4867934
45  meter          E    =           
0015182
 Z    =       -4464740
66                 I    =           51
46169
 XDOT =      -6917
417090                 Wp   =          359
06163
 YDOT =      -1178
239210  meter/sec      RA   =          210
75356  deg
 ZDOT =      -3169
565560                 TA   =          239
10946
                                          MA   =          239
25884
                                          Ha   =            186
630  n
mi
                                          Hp   =            178
067

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4023442
72                 X    =         1193508
90
 Y    =       15970913
56  feet           Y    =         4881464
04  meter
 Z    =      -14648099
28                 Z    =        -4458863
45
 XDOT =     -22694
937958                 XDOT =       -6888
330738
 YDOT =      -3865
614206  feet/sec       YDOT =       -1255
431363  meter/sec
 ZDOT =     -10398
837140                 ZDOT =       -3203
099187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15447455
10                 X    =         4708384
31
 Y    =        5770749
90  feet           Y    =         1758924
57  meter
 Z    =      -14625305
48                 Z    =        -4457793
11
 XDOT =     -15700
598121                 XDOT =       -4785
542307
 YDOT =      15227
823096  feet/sec       YDOT =        4641
440480  meter/sec
 ZDOT =     -10525
069136                 ZDOT =       -3208
041073


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   07077
68814244  
00020000  00000-0  20000-3 0  9029
2 25544  51
6337 211
5697 0015065 321
4426  38
5662 15
77697971 36487


Satellite: ISS
Catalog Number: 25544
Epoch time:      07077
68814244   =   yrday
fracday
Element set:     902
Inclination:       51
6337  deg
RA of node:       211
5697  deg
Eccentricity:     
0015065     
Arg of perigee:   321
4426  deg
Mean anomaly:      38
5662  deg
Mean motion:   15
77697971  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3648
Checksum:              318


Coasting Arc #4 (Orbit 3663)
---------------------------------------

Vector Time (GMT): 2007/078/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6327180
93                 A    =         6720258
16  meter
 Y    =        1594389
75  meter          E    =           
0007629
 Z    =        1621553
24                 I    =           51
51312
 XDOT =        179
508054                 Wp   =           33
56386
 YDOT =       5135
918319  meter/sec      RA   =          205
53929  deg
 ZDOT =      -5731
244150                 TA   =          128
49035
                                          MA   =          128
42190
                                          Ha   =            186
806  n
mi
                                          Hp   =            177
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20758467
62                 X    =         6301004
81
 Y    =        5230937
49  feet           Y    =         1664997
65  meter
 Z    =        5320056
56                 Z    =         1652226
77
 XDOT =        588
937185                 XDOT =         149
905353
 YDOT =      16850
125720  feet/sec       YDOT =        5137
759518  meter/sec
 ZDOT =     -18803
294454                 ZDOT =       -5730
444585

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15906183
08                 X    =         4848204
60
 Y    =      -14283811
67  feet           Y    =        -4353705
80  meter
 Z    =        5435600
31                 Z    =         1656770
97
 XDOT =      13329
232388                 XDOT =        4062
750032
 YDOT =       7665
851577  feet/sec       YDOT =        2336
551561  meter/sec
 ZDOT =     -18799
548704                 ZDOT =       -5730
102445


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   07078
70157051  
00020000  00000-0  20000-3 0  9030
2 25544  51
6343 206
3356 0015221 326
1620  33
8573 15
77774246 36648


Satellite: ISS
Catalog Number: 25544
Epoch time:      07078
70157051   =   yrday
fracday
Element set:     903
Inclination:       51
6343  deg
RA of node:       206
3356  deg
Eccentricity:     
0015221     
Arg of perigee:   326
1620  deg
Mean anomaly:      33
8573  deg
Mean motion:   15
77774246  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3664
Checksum:              280


Coasting Arc #5 (Orbit 3679)
---------------------------------------

Vector Time (GMT): 2007/079/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1011895
28                 A    =         6709331
41  meter
 Y    =       -4070365
93  meter          E    =           
0013266
 Z    =        5240375
86                 I    =           51
50307
 XDOT =       7322
591083                 Wp   =          337
25818
 YDOT =       2356
903045  meter/sec      RA   =          200
38459  deg
 ZDOT =        429
121532                 TA   =          108
73287
                                          MA   =          108
58887
                                          Ha   =            186
907  n
mi
                                          Hp   =            177
385

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3319866
41                 X    =         1031878
66
 Y    =      -13354218
93  feet           Y    =        -4058938
12  meter
 Z    =       17192834
19                 Z    =         5245340
58
 XDOT =      24024
248959                 XDOT =        7293
607026
 YDOT =       7732
621540  feet/sec       YDOT =        2438
626340  meter/sec
 ZDOT =       1407
879041                 ZDOT =         464
624085

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9456599
36                 X    =        -2882371
49
 Y    =       -9965309
19  feet           Y    =        -3037426
24  meter
 Z    =       17210914
12                 Z    =         5245886
62
 XDOT =      18818
308040                 XDOT =        5735
820290
 YDOT =     -15265
245663  feet/sec       YDOT =       -4652
846878  meter/sec
 ZDOT =       1541
691156                 ZDOT =         469
907464


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   07079
71497218  
00020000  00000-0  20000-3 0  9045
2 25544  51
6345 201
1012 0015244 329
7569  30
2715 15
77810973 36803


Satellite: ISS
Catalog Number: 25544
Epoch time:      07079
71497218   =   yrday
fracday
Element set:     904
Inclination:       51
6345  deg
RA of node:       201
1012  deg
Eccentricity:     
0015244     
Arg of perigee:   329
7569  deg
Mean anomaly:      30
2715  deg
Mean motion:   15
77810973  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3680
Checksum:              290


Coasting Arc #6 (Orbit 3695)
---------------------------------------

Vector Time (GMT): 2007/080/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6189273
45                 A    =         6721112
01  meter
 Y    =       -2420841
50  meter          E    =           
0022391
 Z    =         896564
03                 I    =           51
56931
 XDOT =       2512
411479                 Wp   =           11
90436
 YDOT =      -4215
317615  meter/sec      RA   =          195
21735  deg
 ZDOT =       5957
403178                 TA   =          357
92228
                                          MA   =          357
93157
                                          Ha   =            187
307  n
mi
                                          Hp   =            177
066

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20306015
27                 X    =        -6166098
62
 Y    =       -7942393
37  feet           Y    =        -2489923
78  meter
 Z    =        2941483
04                 Z    =          866552
87
 XDOT =       8242
819813                 XDOT =        2530
420929
 YDOT =     -13829
782203  feet/sec       YDOT =       -4187
121337  meter/sec
 ZDOT =      19545
286016                 ZDOT =        5969
652543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17491381
41                 X    =        -5331373
05
 Y    =       13043023
98  feet           Y    =         3975513
71  meter
 Z    =        2828302
10                 Z    =          862066
48
 XDOT =      -6481
520435                 XDOT =       -1975
567429
 YDOT =     -12943
654661  feet/sec       YDOT =       -3945
225941  meter/sec
 ZDOT =      19590
737797                 ZDOT =        5971
256881


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   07080
72835094  
00020000  00000-0  20000-3 0  9057
2 25544  51
6338 195
8669 0015430 335
0252  25
0165 15
77788424 36961


Satellite: ISS
Catalog Number: 25544
Epoch time:      07080
72835094   =   yrday
fracday
Element set:     905
Inclination:       51
6338  deg
RA of node:       195
8669  deg
Eccentricity:     
0015430     
Arg of perigee:   335
0252  deg
Mean anomaly:      25
0165  deg
Mean motion:   15
77788424  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3696
Checksum:              310


Coasting Arc #7 (Orbit 3710)
---------------------------------------

Vector Time (GMT): 2007/081/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3331361
35                 A    =         6711005
71  meter
 Y    =        3288013
56  meter          E    =           
0012242
 Z    =       -4810245
60                 I    =           51
56413
 XDOT =      -6602
126883                 Wp   =           29
00332
 YDOT =      -3134
918124  meter/sec      RA   =          190
01932  deg
 ZDOT =       2442
594308                 TA   =          264
79681
                                          MA   =          264
93653
                                          Ha   =            187
309  n
mi
                                          Hp   =            176
670

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10929663
22                 X    =        -3344513
40
 Y    =       10787446
08  feet           Y    =         3250686
71  meter
 Z    =      -15781645
66                 Z    =        -4826461
47
 XDOT =     -21660
521270                 XDOT =       -6578
446822
 YDOT =     -10285
164449  feet/sec       YDOT =       -3208
614314  meter/sec
 ZDOT =       8013
760853                 ZDOT =        2410
578681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3674276
03                 X    =         1119919
33
 Y    =       14846306
15  feet           Y    =         4525154
12  meter
 Z    =      -15842151
36                 Z    =        -4828687
74
 XDOT =     -18902
187314                 XDOT =       -5761
386693
 YDOT =      13054
703480  feet/sec       YDOT =        3979
073621  meter/sec
 ZDOT =       7892
934266                 ZDOT =        2405
766364


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   07081
67836519  
00020000  00000-0  20000-3 0  9066
2 25544  51
6337 190
9598 0015422 338
4828  21
5687 15
77863271 37116


Satellite: ISS
Catalog Number: 25544
Epoch time:      07081
67836519   =   yrday
fracday
Element set:     906
Inclination:       51
6337  deg
RA of node:       190
9598  deg
Eccentricity:     
0015422     
Arg of perigee:   338
4828  deg
Mean anomaly:      21
5687  deg
Mean motion:   15
77863271  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3711
Checksum:              324


Coasting Arc #8 (Orbit 3726)
---------------------------------------

Vector Time (GMT): 2007/082/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5048258
09                 A    =         6716481
69  meter
 Y    =        3021153
02  meter          E    =           
0014126
 Z    =       -3255732
02                 I    =           51
61179
 XDOT =      -5061
832045                 Wp   =             
53215
 YDOT =       3335
454510  meter/sec      RA   =          184
89496  deg
 ZDOT =      -4739
902069                 TA   =          217
61900
                                          MA   =          217
71789
                                          Ha   =            187
472  n
mi
                                          Hp   =            176
440

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16562526
54                 X    =         5029915
70
 Y    =        9911919
37  feet           Y    =         3077502
88  meter
 Z    =      -10681535
50                 Z    =        -3231252
14
 XDOT =     -16607
060515                 XDOT =       -5075
727758
 YDOT =      10943
092223  feet/sec       YDOT =        3278
772527  meter/sec
 ZDOT =     -15550
859808                 ZDOT =       -4764
526262

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16890088
13                 X    =         5148098
86
 Y    =       -9447513
77  feet           Y    =        -2879602
20  meter
 Z    =      -10589052
75                 Z    =        -3227543
28
 XDOT =        538
242891                 XDOT =         164
056433
 YDOT =      18546
271806  feet/sec       YDOT =        5652
903647  meter/sec
 ZDOT =     -15642
987222                 ZDOT =       -4767
982505


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   07082
69168992  
00020000  00000-0  20000-3 0  9073
2 25544  51
6340 185
7250 0015418 342
9580  17
1065 15
77928428 37271


Satellite: ISS
Catalog Number: 25544
Epoch time:      07082
69168992   =   yrday
fracday
Element set:     907
Inclination:       51
6340  deg
RA of node:       185
7250  deg
Eccentricity:     
0015418     
Arg of perigee:   342
9580  deg
Mean anomaly:      17
1065  deg
Mean motion:   15
77928428  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3727
Checksum:              316


Coasting Arc #9 (Orbit 3742)
---------------------------------------

Vector Time (GMT): 2007/083/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5339362
67                 A    =         6716367
59  meter
 Y    =       -2551021
19  meter          E    =           
0017222
 Z    =        3185155
69                 I    =           51
63988
 XDOT =       4685
110988                 Wp   =           33
12168
 YDOT =       3775
509883  meter/sec      RA   =          179
67738  deg
 ZDOT =      -4803
581148                 TA   =          109
68910
                                          MA   =          109
50321
                                          Ha   =            187
578  n
mi
                                          Hp   =            175
942

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17517594
08                 X    =         5352018
87
 Y    =       -8369492
09  feet           Y    =        -2491242
69  meter
 Z    =       10449985
86                 Z    =         3211124
97
 XDOT =      15371
099041                 XDOT =        4665
879340
 YDOT =      12386
843447  feet/sec       YDOT =        3827
793892  meter/sec
 ZDOT =     -15759
780670                 ZDOT =       -4780
867661

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1139081
55                 X    =          347192
06
 Y    =      -19328056
21  feet           Y    =        -5891191
53  meter
 Z    =       10547295
43                 Z    =         3214815
65
 XDOT =      16916
998745                 XDOT =        5156
301217
 YDOT =      -7602
949044  feet/sec       YDOT =       -2317
378869  meter/sec
 ZDOT =     -15673
825449                 ZDOT =       -4777
381997


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   07083
70498716  
00020000  00000-0  20000-3 0  9087
2 25544  51
6330 180
4899 0015565 346
8049  13
2706 15
77981847 37438


Satellite: ISS
Catalog Number: 25544
Epoch time:      07083
70498716   =   yrday
fracday
Element set:     908
Inclination:       51
6330  deg
RA of node:       180
4899  deg
Eccentricity:     
0015565     
Arg of perigee:   346
8049  deg
Mean anomaly:      13
2706  deg
Mean motion:   15
77981847  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3743
Checksum:              327


Coasting Arc #10 (Orbit 3758)
---------------------------------------

Vector Time (GMT): 2007/084/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2936767
82                 A    =         6710571
51  meter
 Y    =       -3576650
06  meter          E    =           
0012258
 Z    =        4852281
25                 I    =           51
64867
 XDOT =       6906
962726                 Wp   =           16
71809
 YDOT =      -2515
278739  meter/sec      RA   =          174
55538  deg
 ZDOT =       2336
392636                 TA   =           50
61414
                                          MA   =           50
50564
                                          Ha   =            187
794  n
mi
                                          Hp   =            175
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9635065
02                 X    =        -2920126
25
 Y    =      -11734416
22  feet           Y    =        -3609397
61  meter
 Z    =       15919557
90                 Z    =         4838054
96
 XDOT =      22660
638864                 XDOT =        6923
225912
 YDOT =      -8252
226835  feet/sec       YDOT =       -2437
950291  meter/sec
 ZDOT =       7665
330170                 ZDOT =        2369
985893

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14925911
04                 X    =        -4549417
68
 Y    =        3076524
88  feet           Y    =          937724
78  meter
 Z    =       15865544
42                 Z    =         4835817
94
 XDOT =       3556
055467                 XDOT =        1083
885706
 YDOT =     -22755
995584  feet/sec       YDOT =       -6936
027454  meter/sec
 ZDOT =       7791
334100                 ZDOT =        2374
798634


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   07084
71825954  
00020000  00000-0  20000-3 0  9098
2 25544  51
6327 175
2542 0015536 351
3113   8
7781 15
78000107 37593


Satellite: ISS
Catalog Number: 25544
Epoch time:      07084
71825954   =   yrday
fracday
Element set:     909
Inclination:       51
6327  deg
RA of node:       175
2542  deg
Eccentricity:     
0015536     
Arg of perigee:   351
3113  deg
Mean anomaly:       8
7781  deg
Mean motion:   15
78000107  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3759
Checksum:              293


Coasting Arc #11 (Orbit 3773)
---------------------------------------

Vector Time (GMT): 2007/085/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6413415
36                 A    =         6720416
78  meter
 Y    =        1806901
16  meter          E    =           
0024212
 Z    =        -750428
62                 I    =           51
71198
 XDOT =      -1948
866447                 Wp   =           12
76234
 YDOT =      -4451
256779  meter/sec      RA   =          169
36622  deg
 ZDOT =       5997
418905                 TA   =          339
04011
                                          MA   =          339
13919
                                          Ha   =            187
794  n
mi
                                          Hp   =            175
378

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21041388
99                 X    =        -6429498
33
 Y    =        5928153
40  feet           Y    =         1735092
83  meter
 Z    =       -2462036
14                 Z    =         -781623
69
 XDOT =      -6393
918789                 XDOT =       -1928
081038
 YDOT =     -14603
860822  feet/sec       YDOT =       -4472
933826  meter/sec
 ZDOT =      19676
571211                 ZDOT =        5988
001950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4269319
05                 X    =        -1301288
45
 Y    =       21425817
72  feet           Y    =         6530589
24  meter
 Z    =       -2579132
68                 Z    =         -786119
64
 XDOT =     -14402
186640                 XDOT =       -4389
786488
 YDOT =       -528
028756  feet/sec       YDOT =        -160
943165  meter/sec
 ZDOT =      19640
519699                 ZDOT =        5986
430404


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   07085
66817796  
00020000  00000-0  20000-3 0  9100
2 25544  51
6337 170
3468 0015622 354
7473   5
3526 15
78048578 37740


Satellite: ISS
Catalog Number: 25544
Epoch time:      07085
66817796   =   yrday
fracday
Element set:     910
Inclination:       51
6337  deg
RA of node:       170
3468  deg
Eccentricity:     
0015622     
Arg of perigee:   354
7473  deg
Mean anomaly:       5
3526  deg
Mean motion:   15
78048578  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3774
Checksum:              322


Coasting Arc #12 (Orbit 3789)
---------------------------------------

Vector Time (GMT): 2007/086/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 478698
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         386454
96                 A    =         6708695
14  meter
 Y    =        4188782
78  meter          E    =           
0020329
 Z    =       -5236970
20                 I    =           51
70055
 XDOT =      -7508
325317                 Wp   =           45
37057
 YDOT =       1548
881008  meter/sec      RA   =          164
20617  deg
 ZDOT =        700
466770                 TA   =          231
19650
                                          MA   =          231
37821
                                          Ha   =            187
999  n
mi
                                          Hp   =            175
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1267896
84                 X    =          365026
55
 Y    =       13742725
64  feet           Y    =         4192984
38  meter
 Z    =      -17181660
77                 Z    =        -5235144
99
 XDOT =     -24633
613246                 XDOT =       -7528
489787
 YDOT =       5081
630603  feet/sec       YDOT =        1464
805986  meter/sec
 ZDOT =       2298
119325                 ZDOT =         663
942844

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12947418
43                 X    =         3946373
14
 Y    =        4805272
95  feet           Y    =         1464647
19  meter
 Z    =      -17174202
90                 Z    =        -5234697
04
 XDOT =      -5898
358839                 XDOT =       -1797
819774
 YDOT =      23432
129718  feet/sec       YDOT =        7142
113138  meter/sec
 ZDOT =       2160
926545                 ZDOT =         658
650411


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   07086
68139866  
00020000  00000-0  20000-3 0  9119
2 25544  51
6338 165
1113 0015693 358
4515   1
6599 15
78059274 37908


Satellite: ISS
Catalog Number: 25544
Epoch time:      07086
68139866   =   yrday
fracday
Element set:     911
Inclination:       51
6338  deg
RA of node:       165
1113  deg
Eccentricity:     
0015693     
Arg of perigee:   358
4515  deg
Mean anomaly:       1
6599  deg
Mean motion:   15
78059274  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3790
Checksum:              319

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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