Date: January 21st 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


022/09:06:27 023 1 5 3 3 3 3
N/A 2 7 0 0 185 4
000/00:00:54 046 1 1 0 0 179 6

024/09:03:00 612 -4 8 9 2 9 2
N/A -7 6 0 0 187 9
000/00:02:31 224 -2 1 0 1 183 7

Coasting Arc #1 (Orbit 20)
---------------------------------------

Vector Time (GMT): 2010/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          36380
37                 A    =         6722037
12  meter
 Y    =        6709774
11  meter          E    =           
0015446
 Z    =        -178707
83                 I    =           51
32893
 XDOT =      -4821
135540                 Wp   =          162
38628
 YDOT =       -130
144281  meter/sec      RA   =          268
46797  deg
 ZDOT =      -6017
490859                 TA   =           19
56793
                                          MA   =           19
50871
                                          Ha   =            184
949  n
mi
                                          Hp   =            179
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         119358
17                 X    =          -37784
10
 Y    =       22013694
57  feet           Y    =         6709766
26  meter
 Z    =        -586311
78                 Z    =         -178711
09
 XDOT =     -15817
373819                 XDOT =       -4790
090515
 YDOT =       -426
982550  feet/sec       YDOT =        -183
883354  meter/sec
 ZDOT =     -19742
424079                 ZDOT =       -6040
836154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19196278
39                 X    =        -5851025
65
 Y    =       10775903
33  feet           Y    =         3284495
33  meter
 Z    =        -586140
01                 Z    =         -178655
48
 XDOT =      -6449
596234                 XDOT =       -1965
836932
 YDOT =     -12541
542093  feet/sec       YDOT =       -3822
662030  meter/sec
 ZDOT =     -19834
885298                 ZDOT =       -6045
673039


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   10020
53135479  
00016717  00000-0  10270-3 0  9007
2 25544  51
6448 269
0797 0007063 210
3784 149
6973 15
77566722   211


Satellite: ISS
Catalog Number: 25544
Epoch time:      10020
53135479   =   yrday
fracday
Element set:     900
Inclination:       51
6448  deg
RA of node:       269
0797  deg
Eccentricity:     
0007063     
Arg of perigee:   210
3784  deg
Mean anomaly:     149
6973  deg
Mean motion:   15
77566722  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              21
Checksum:              312


Coasting Arc #2 (Orbit 36)
---------------------------------------

Vector Time (GMT): 2010/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4227828
48                 A    =         6710457
89  meter
 Y    =        1268427
86  meter          E    =           
0002731
 Z    =        5053854
18                 I    =           51
29295
 XDOT =       -381
201770                 Wp   =          182
59516
 YDOT =       7535
307438  meter/sec      RA   =          263
26587  deg
 ZDOT =      -1575
060337                 TA   =          282
57067
                                          MA   =          282
60122
                                          Ha   =            184
452  n
mi
                                          Hp   =            179
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13870828
33                 X    =         4188780
06
 Y    =        4161508
72  feet           Y    =         1315487
49  meter
 Z    =       16580886
41                 Z    =         5074297
90
 XDOT =      -1250
661974                 XDOT =        -457
783313
 YDOT =      24722
137263  feet/sec       YDOT =        7530
616460  meter/sec
 ZDOT =      -5167
520791                 ZDOT =       -1577
098034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3275928
19                 X    =          998502
91
 Y    =       14010478
91  feet           Y    =         4270393
97  meter
 Z    =       16661890
74                 Z    =         5078544
30
 XDOT =     -21003
545209                 XDOT =       -6401
880580
 YDOT =      11055
242744  feet/sec       YDOT =        3369
637988  meter/sec
 ZDOT =      -5175
375585                 ZDOT =       -1577
454478


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   10021
54485120  
00016717  00000-0  10270-3 0  9011
2 25544  51
6448 263
8470 0006916 216
3721 143
6975 15
77674615   378


Satellite: ISS
Catalog Number: 25544
Epoch time:      10021
54485120   =   yrday
fracday
Element set:     901
Inclination:       51
6448  deg
RA of node:       263
8470  deg
Eccentricity:     
0006916     
Arg of perigee:   216
3721  deg
Mean anomaly:     143
6975  deg
Mean motion:   15
77674615  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              37
Checksum:              303


Coasting Arc #3 (Orbit 50)
---------------------------------------

Vector Time (GMT): 2010/022/09:06:54
046
Vector Time (MET): N/A
Weight (LBS)     : 751544
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3193827
94                 A    =         6713517
85  meter
 Y    =       -3492211
46  meter          E    =           
0009013
 Z    =        4761227
31                 I    =           51
29977
 XDOT =       3336
341644                 Wp   =          151
18470
 YDOT =       6479
014940  meter/sec      RA   =          258
73492  deg
 ZDOT =       2504
372732                 TA   =          274
15430
                                          MA   =          274
25731
                                          Ha   =            185
402  n
mi
                                          Hp   =            179
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10478438
12                 X    =         3209512
13
 Y    =      -11457386
70  feet           Y    =        -3456408
63  meter
 Z    =       15620824
49                 Z    =         4776780
77
 XDOT =      10946
002769                 XDOT =        3251
478517
 YDOT =      21256
610695  feet/sec       YDOT =        6515
849320  meter/sec
 ZDOT =       8216
445970                 ZDOT =        2520
374582

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8951924
41                 X    =         2728546
56
 Y    =       12609809
67  feet           Y    =         3843469
99  meter
 Z    =       15682323
89                 Z    =         4779972
32
 XDOT =     -22185
103472                 XDOT =       -6762
019538
 YDOT =       5412
371838  feet/sec       YDOT =        1649
690936  meter/sec
 ZDOT =       8280
013606                 ZDOT =        2523
748147


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   10022
43167375  
00016717  00000-0  10270-3 0  9020
2 25544  51
6432 259
2679 0004677 204
6412 155
4530 15
77054905   518


Satellite: ISS
Catalog Number: 25544
Epoch time:      10022
43167375   =   yrday
fracday
Element set:     902
Inclination:       51
6432  deg
RA of node:       259
2679  deg
Eccentricity:     
0004677     
Arg of perigee:   204
6412  deg
Mean anomaly:     155
4530  deg
Mean motion:   15
77054905  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              51
Checksum:              292


Coasting Arc #4 (Orbit 65)
---------------------------------------

Vector Time (GMT): 2010/023/09:06:54
046
Vector Time (MET): N/A
Weight (LBS)     : 751544
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2785389
64                 A    =         6722809
39  meter
 Y    =       -5995399
72  meter          E    =           
0004710
 Z    =       -1212802
18                 I    =           51
33866
 XDOT =       3985
408641                 Wp   =           45
44038
 YDOT =      -3031
857645  meter/sec      RA   =          253
52097  deg
 ZDOT =       5851
845543                 TA   =          301
19851
                                          MA   =          301
24467
                                          Ha   =            185
294  n
mi
                                          Hp   =            179
745

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9138417
46                 X    =        -2712249
48
 Y    =      -19669946
59  feet           Y    =        -6026138
60  meter
 Z    =       -3979009
77                 Z    =        -1226156
09
 XDOT =      13075
487666                 XDOT =        3990
588211
 YDOT =      -9947
039519  feet/sec       YDOT =       -2987
261731  meter/sec
 ZDOT =      19198
968316                 ZDOT =        5871
218966

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21087847
74                 X    =         6427575
99
 Y    =       -5029412
09  feet           Y    =        -1532964
80  meter
 Z    =       -4032081
75                 Z    =        -1228978
52
 XDOT =       6809
077050                 XDOT =        2075
406685
 YDOT =      13141
167298  feet/sec       YDOT =        4005
427792  meter/sec
 ZDOT =      19275
612542                 ZDOT =        5875
206703


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   10023
38217115  
00016717  00000-0  10270-3 0  9034
2 25544  51
6435 254
3646 0004567 209
2993 150
7916 15
77062590   665


Satellite: ISS
Catalog Number: 25544
Epoch time:      10023
38217115   =   yrday
fracday
Element set:     903
Inclination:       51
6435  deg
RA of node:       254
3646  deg
Eccentricity:     
0004567     
Arg of perigee:   209
2993  deg
Mean anomaly:     150
7916  deg
Mean motion:   15
77062590  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              66
Checksum:              303


Coasting Arc #5 (Orbit 81)
---------------------------------------

Vector Time (GMT): 2010/024/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3289545
91                 A    =         6716676
40  meter
 Y    =        2838752
85  meter          E    =           
0005769
 Z    =       -5125222
36                 I    =           51
31234
 XDOT =      -3725
228599                 Wp   =          127
24738
 YDOT =      -6617
273103  meter/sec      RA   =          248
37156  deg
 ZDOT =      -1278
617894                 TA   =          130
49613
                                          MA   =          130
44585
                                          Ha   =            187
939  n
mi
                                          Hp   =            183
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10792473
47                 X    =        -3296147
64
 Y    =        9313493
61  feet           Y    =         2801930
59  meter
 Z    =      -16815033
98                 Z    =        -5141218
72
 XDOT =     -12221
878606                 XDOT =       -3644
744965
 YDOT =     -21710
213594  feet/sec       YDOT =       -6658
480731  meter/sec
 ZDOT =      -4194
940596                 ZDOT =       -1296
519825

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7075380
26                 X    =        -2156575
90
 Y    =      -12289248
14  feet           Y    =        -3745762
83  meter
 Z    =      -16878311
20                 Z    =        -5144509
25
 XDOT =      22759
219365                 XDOT =        6937
010062
 YDOT =      -7264
138328  feet/sec       YDOT =       -2214
109362  meter/sec
 ZDOT =      -4266
052795                 ZDOT =       -1300
292892


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   10024
39602317  
00016717  00000-0  10270-3 0  9049
2 25544  51
6441 249
1346 0011095 237
7769 122
2320 15
75394779   828


Satellite: ISS
Catalog Number: 25544
Epoch time:      10024
39602317   =   yrday
fracday
Element set:     904
Inclination:       51
6441  deg
RA of node:       249
1346  deg
Eccentricity:     
0011095     
Arg of perigee:   237
7769  deg
Mean anomaly:     122
2320  deg
Mean motion:   15
75394779  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              82
Checksum:              301


Coasting Arc #6 (Orbit 97)
---------------------------------------

Vector Time (GMT): 2010/025/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3468912
79                 A    =         6728085
57  meter
 Y    =        5717772
40  meter          E    =           
0013629
 Z    =         646449
20                 I    =           51
36273
 XDOT =      -3834
492086                 Wp   =          177
18686
 YDOT =       3000
924014  meter/sec      RA   =          243
18673  deg
 ZDOT =      -5974
669091                 TA   =          355
73782
                                          MA   =          355
74942
                                          Ha   =            187
806  n
mi
                                          Hp   =            183
878

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11380947
48                 X    =         3401577
53
 Y    =       18759095
81  feet           Y    =         5756187
30  meter
 Z    =        2120896
34                 Z    =          663137
93
 XDOT =     -12580
354612                 XDOT =       -3838
740361
 YDOT =       9845
551226  feet/sec       YDOT =        2958
021175  meter/sec
 ZDOT =     -19601
932714                 ZDOT =       -5993
306968

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20467079
14                 X    =        -6238365
72
 Y    =        7889406
80  feet           Y    =         2404691
19  meter
 Z    =        2187184
07                 Z    =          666653
70
 XDOT =      -6922
334459                 XDOT =       -2109
927543
 YDOT =     -12510
703677  feet/sec       YDOT =       -3813
262481  meter/sec
 ZDOT =     -19675
673784                 ZDOT =       -5997
145369


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   10025
41096082  
00016717  00000-0  10270-3 0  9050
2 25544  51
6440 243
9122 0011191 241
4001 118
6037 15
75372107   981


Satellite: ISS
Catalog Number: 25544
Epoch time:      10025
41096082   =   yrday
fracday
Element set:     905
Inclination:       51
6440  deg
RA of node:       243
9122  deg
Eccentricity:     
0011191     
Arg of perigee:   241
4001  deg
Mean anomaly:     118
6037  deg
Mean motion:   15
75372107  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              98
Checksum:              265


Coasting Arc #7 (Orbit 113)
---------------------------------------

Vector Time (GMT): 2010/026/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3450916
47                 A    =         6715982
89  meter
 Y    =       -2397805
77  meter          E    =           
0009304
 Z    =        5245813
72                 I    =           51
33729
 XDOT =       4197
742715                 Wp   =          237
88479
 YDOT =       6449
933986  meter/sec      RA   =          238
02796  deg
 ZDOT =        182
104436                 TA   =          210
35212
                                          MA   =          210
40602
                                          Ha   =            187
364  n
mi
                                          Hp   =            183
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11321904
43                 X    =         3451989
79
 Y    =       -7866816
84  feet           Y    =        -2359210
09  meter
 Z    =       17210674
94                 Z    =         5262580
43
 XDOT =      13772
121767                 XDOT =        4124
421809
 YDOT =      21161
200740  feet/sec       YDOT =        6496
465652  meter/sec
 ZDOT =        597
455498                 ZDOT =         202
319337

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5981810
14                 X    =         1823255
73
 Y    =       12328905
02  feet           Y    =         3757850
25  meter
 Z    =       17277028
31                 Z    =         5266038
23
 XDOT =     -22182
492249                 XDOT =       -6761
223638
 YDOT =       9791
620880  feet/sec       YDOT =        2984
486044  meter/sec
 ZDOT =        677
747448                 ZDOT =         206
577422


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   10026
42587984  
00016717  00000-0  10270-3 0  9069
2 25544  51
6439 238
6894 0011225 246
2696 113
7291 15
75450096  1148


Satellite: ISS
Catalog Number: 25544
Epoch time:      10026
42587984   =   yrday
fracday
Element set:     906
Inclination:       51
6439  deg
RA of node:       238
6894  deg
Eccentricity:     
0011225     
Arg of perigee:   246
2696  deg
Mean anomaly:     113
7291  deg
Mean motion:   15
75450096  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             114
Checksum:              321


Coasting Arc #8 (Orbit 129)
---------------------------------------

Vector Time (GMT): 2010/027/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3832965
56                 A    =         6727991
88  meter
 Y    =       -5514871
82  meter          E    =           
0004891
 Z    =         342940
79                 I    =           51
39474
 XDOT =       4125
111354                 Wp   =          349
09981
 YDOT =      -2494
786896  meter/sec      RA   =          232
86316  deg
 ZDOT =       6005
056604                 TA   =           14
64183
                                          MA   =           14
62767
                                          Ha   =            187
086  n
mi
                                          Hp   =            184
037

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12575346
31                 X    =        -3772678
32
 Y    =      -18093411
48  feet           Y    =        -5557397
26  meter
 Z    =        1125133
83                 Z    =          324466
45
 XDOT =      13533
829901                 XDOT =        4123
530986
 YDOT =      -8184
996379  feet/sec       YDOT =       -2448
666923  meter/sec
 ZDOT =      19701
629278                 ZDOT =        6025
091921

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19696914
22                 X    =         6003619
45
 Y    =       -9884441
65  feet           Y    =        -3012777
82  meter
 Z    =        1051752
54                 Z    =          320574
17
 XDOT =       5475
036046                 XDOT =        1668
790987
 YDOT =      13008
027387  feet/sec       YDOT =        3964
846747  meter/sec
 ZDOT =      19780
937728                 ZDOT =        6029
229820


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   10027
44078468  
00016717  00000-0  10270-3 0  9075
2 25544  51
6438 233
4662 0011197 250
7271 109
2682 15
75456045  1302


Satellite: ISS
Catalog Number: 25544
Epoch time:      10027
44078468   =   yrday
fracday
Element set:     907
Inclination:       51
6438  deg
RA of node:       233
4662  deg
Eccentricity:     
0011197     
Arg of perigee:   250
7271  deg
Mean anomaly:     109
2682  deg
Mean motion:   15
75456045  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             130
Checksum:              301


Coasting Arc #9 (Orbit 144)
---------------------------------------

Vector Time (GMT): 2010/028/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3791129
93                 A    =         6716132
89  meter
 Y    =        1984306
06  meter          E    =           
0006046
 Z    =       -5180320
56                 I    =           51
37399
 XDOT =      -4543
789893                 Wp   =          143
00380
 YDOT =      -6141
117607  meter/sec      RA   =          227
68665  deg
 ZDOT =        968
784508                 TA   =          136
28722
                                          MA   =          136
23933
                                          Ha   =            186
611  n
mi
                                          Hp   =            184
043

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12438090
33                 X    =        -3787872
61
 Y    =        6510190
49  feet           Y    =         1941930
12  meter
 Z    =      -16995802
36                 Z    =        -5198729
30
 XDOT =     -14907
447154                 XDOT =       -4479
487187
 YDOT =     -20148
023644  feet/sec       YDOT =       -6191
569512  meter/sec
 ZDOT =       3178
426865                 ZDOT =         946
866930

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4916719
81                 X    =        -1498616
20
 Y    =      -13054948
12  feet           Y    =        -3979148
19  meter
 Z    =      -17068689
61                 Z    =        -5202536
59
 XDOT =      20903
410071                 XDOT =        6371
359390
 YDOT =     -11932
218210  feet/sec       YDOT =       -3636
940110  meter/sec
 ZDOT =       3091
361615                 ZDOT =         942
247020


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   10028
39224237  
00016717  00000-0  10270-3 0  9088
2 25544  51
6434 228
5696 0011226 254
7546 105
2377 15
75494221  1453


Satellite: ISS
Catalog Number: 25544
Epoch time:      10028
39224237   =   yrday
fracday
Element set:     908
Inclination:       51
6434  deg
RA of node:       228
5696  deg
Eccentricity:     
0011226     
Arg of perigee:   254
7546  deg
Mean anomaly:     105
2377  deg
Mean motion:   15
75494221  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             145
Checksum:              305


Coasting Arc #10 (Orbit 160)
---------------------------------------

Vector Time (GMT): 2010/029/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4060575
07                 A    =         6727255
65  meter
 Y    =        5182829
69  meter          E    =           
0011034
 Z    =       -1345504
84                 I    =           51
43210
 XDOT =      -4595
253612                 Wp   =          211
58078
 YDOT =       2085
246226  meter/sec      RA   =          222
54436  deg
 ZDOT =      -5823
430425                 TA   =          343
25668
                                          MA   =          343
29308
                                          Ha   =            186
434  n
mi
                                          Hp   =            184
012

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13322096
69                 X    =         4008853
98
 Y    =       17004034
43  feet           Y    =         5227948
36  meter
 Z    =       -4414385
95                 Z    =        -1325904
42
 XDOT =     -15076
291378                 XDOT =       -4589
941378
 YDOT =       6841
359009  feet/sec       YDOT =        2033
889504  meter/sec
 ZDOT =     -19105
742864                 ZDOT =       -5845
740426

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18344811
45                 X    =        -5591498
53
 Y    =       11435242
27  feet           Y    =         3485461
84  meter
 Z    =       -4336516
75                 Z    =        -1321770
31
 XDOT =      -4352
567062                 XDOT =       -1326
662441
 YDOT =     -14276
874898  feet/sec       YDOT =       -4351
591469  meter/sec
 ZDOT =     -19194
095502                 ZDOT =       -5850
360309


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   10029
40711556  
00016717  00000-0  10270-3 0  9097
2 25544  51
6432 223
3468 0011356 258
1582 101
8308 15
75463615  1610


Satellite: ISS
Catalog Number: 25544
Epoch time:      10029
40711556   =   yrday
fracday
Element set:     909
Inclination:       51
6432  deg
RA of node:       223
3468  deg
Eccentricity:     
0011356     
Arg of perigee:   258
1582  deg
Mean anomaly:     101
8308  deg
Mean motion:   15
75463615  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             161
Checksum:              291


Coasting Arc #11 (Orbit 176)
---------------------------------------

Vector Time (GMT): 2010/030/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4256658
15                 A    =         6717089
73  meter
 Y    =       -1688357
97  meter          E    =           
0006501
 Z    =        4920188
64                 I    =           51
42192
 XDOT =       4707
736916                 Wp   =          288
78303
 YDOT =       5712
972487  meter/sec      RA   =          217
35156  deg
 ZDOT =      -2112
667368                 TA   =          181
76702
                                          MA   =          181
76932
                                          Ha   =            185
759  n
mi
                                          Hp   =            183
568

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13965413
87                 X    =         4251320
71
 Y    =       -5539232
17  feet           Y    =        -1640787
53  meter
 Z    =       16142351
18                 Z    =         4940853
77
 XDOT =      15445
331089                 XDOT =        4653
766175
 YDOT =      18743
348054  feet/sec       YDOT =        5765
315503  meter/sec
 ZDOT =      -6931
323386                 ZDOT =       -2089
928814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4256851
89                 X    =         1297488
46
 Y    =       14315927
34  feet           Y    =         4363494
65  meter
 Z    =       16224204
63                 Z    =         4945137
57
 XDOT =     -19027
614268                 XDOT =       -5799
616829
 YDOT =      13409
956715  feet/sec       YDOT =        4087
354807  meter/sec
 ZDOT =      -6840
976471                 ZDOT =       -2085
129628


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   10030
42196955  
00016717  00000-0  10270-3 0  9103
2 25544  51
6431 218
1228 0011356 263
3794  96
6078 15
75561550  1777


Satellite: ISS
Catalog Number: 25544
Epoch time:      10030
42196955   =   yrday
fracday
Element set:     910
Inclination:       51
6431  deg
RA of node:       218
1228  deg
Eccentricity:     
0011356     
Arg of perigee:   263
3794  deg
Mean anomaly:      96
6078  deg
Mean motion:   15
75561550  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             177
Checksum:              304


Coasting Arc #12 (Orbit 192)
---------------------------------------

Vector Time (GMT): 2010/031/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4102919
24                 A    =         6725415
90  meter
 Y    =       -4785497
91  meter          E    =           
0004127
 Z    =        2336450
85                 I    =           51
47389
 XDOT =       5186
423314                 Wp   =           29
29203
 YDOT =      -1810
945824  meter/sec      RA   =          212
22732  deg
 ZDOT =       5397
978600                 TA   =          357
08348
                                          MA   =          357
08588
                                          Ha   =            185
570  n
mi
                                          Hp   =            183
620

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13461021
12                 X    =        -4060451
71
 Y    =      -15700452
45  feet           Y    =        -4831141
74  meter
 Z    =        7665521
16                 Z    =         2316622
63
 XDOT =      17015
824520                 XDOT =        5180
066597
 YDOT =      -5941
423306  feet/sec       YDOT =       -1752
983732  meter/sec
 ZDOT =      17709
903544                 ZDOT =        5423
157994

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16652127
17                 X    =         5075568
36
 Y    =      -12313070
54  feet           Y    =        -3753023
90  meter
 Z    =        7586729
60                 Z    =         2312435
18
 XDOT =       3781
727444                 XDOT =        1152
670525
 YDOT =      16088
799630  feet/sec       YDOT =        4903
866127  meter/sec
 ZDOT =      17809
652778                 ZDOT =        5428
382167


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   10031
43680931  
00016717  00000-0  10270-3 0  9118
2 25544  51
6425 212
8982 0011384 267
6265  92
3596 15
75558816  1936


Satellite: ISS
Catalog Number: 25544
Epoch time:      10031
43680931   =   yrday
fracday
Element set:     911
Inclination:       51
6425  deg
RA of node:       212
8982  deg
Eccentricity:     
0011384     
Arg of perigee:   267
6265  deg
Mean anomaly:      92
3596  deg
Mean motion:   15
75558816  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             193
Checksum:              318


Coasting Arc #13 (Orbit 207)
---------------------------------------

Vector Time (GMT): 2010/032/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4803090
39                 A    =         6718934
42  meter
 Y    =        1522122
58  meter          E    =           
0003896
 Z    =       -4444717
98                 I    =           51
47836
 XDOT =      -4640
224704                 Wp   =          215
55124
 YDOT =      -5239
977653  meter/sec      RA   =          207
02317  deg
 ZDOT =       3215
368050                 TA   =           86
71776
                                          MA   =           86
67320
                                          Ha   =            185
353  n
mi
                                          Hp   =            183
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15758170
56                 X    =        -4798163
01
 Y    =        4993840
49  feet           Y    =         1468439
05  meter
 Z    =      -14582408
08                 Z    =        -4468038
81
 XDOT =     -15223
834331                 XDOT =       -4596
904724
 YDOT =     -17191
527734  feet/sec       YDOT =       -5291
625122  meter/sec
 ZDOT =      10549
107777                 ZDOT =        3192
931779

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4100541
46                 X    =        -1249845
04
 Y    =      -15929239
08  feet           Y    =        -4855232
07  meter
 Z    =      -14674805
27                 Z    =        -4472880
65
 XDOT =      16865
409712                 XDOT =        5140
576880
 YDOT =     -13991
353472  feet/sec       YDOT =       -4264
564538  meter/sec
 ZDOT =      10459
945725                 ZDOT =        3188
191457


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   10032
38820569  
00016717  00000-0  10270-3 0  9127
2 25544  51
6421 208
0003 0011397 271
2668  88
7191 15
75589384  2086


Satellite: ISS
Catalog Number: 25544
Epoch time:      10032
38820569   =   yrday
fracday
Element set:     912
Inclination:       51
6421  deg
RA of node:       208
0003  deg
Eccentricity:     
0011397     
Arg of perigee:   271
2668  deg
Mean anomaly:      88
7191  deg
Mean motion:   15
75589384  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             208
Checksum:              307


Coasting Arc #14 (Orbit 223)
---------------------------------------

Vector Time (GMT): 2010/033/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3936725
57                 A    =         6723097
09  meter
 Y    =        4369744
71  meter          E    =           
0006835
 Z    =       -3251610
65                 I    =           51
51922
 XDOT =      -5825
719185                 Wp   =          274
16037
 YDOT =       1715
959453  meter/sec      RA   =          201
91507  deg
 ZDOT =      -4738
155499                 TA   =          304
01471
                                          MA   =          304
07961
                                          Ha   =            185
700  n
mi
                                          Hp   =            183
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12915766
30                 X    =         3903365
11
 Y    =       14336432
76  feet           Y    =         4413580
89  meter
 Z    =      -10668013
96                 Z    =        -3232567
61
 XDOT =     -19113
251919                 XDOT =       -5821
457773
 YDOT =       5629
788231  feet/sec       YDOT =        1650
836511  meter/sec
 ZDOT =     -15545
129590                 ZDOT =       -4766
445909

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14834969
62                 X    =        -4521698
74
 Y    =       12404960
13  feet           Y    =         3781031
85  meter
 Z    =      -10592331
46                 Z    =        -3228542
63
 XDOT =      -3973
207517                 XDOT =       -1211
033651
 YDOT =     -18146
330625  feet/sec       YDOT =       -5531
001575  meter/sec
 ZDOT =     -15657
227162                 ZDOT =       -4772
322839


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   10033
40301231  
00016717  00000-0  10270-3 0  9132
2 25544  51
6417 202
7772 0011453 275
3342  84
6515 15
75595706  2240


Satellite: ISS
Catalog Number: 25544
Epoch time:      10033
40301231   =   yrday
fracday
Element set:     913
Inclination:       51
6417  deg
RA of node:       202
7772  deg
Eccentricity:     
0011453     
Arg of perigee:   275
3342  deg
Mean anomaly:      84
6515  deg
Mean motion:   15
75595706  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             224
Checksum:              276


Coasting Arc #15 (Orbit 239)
---------------------------------------

Vector Time (GMT): 2010/034/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5356749
61                 A    =         6721148
52  meter
 Y    =       -1516895
71  meter          E    =           
0003506
 Z    =        3768296
60                 I    =           51
54276
 XDOT =       4318
703355                 Wp   =             
39759
 YDOT =       4786
453801  meter/sec      RA   =          196
70750  deg
 ZDOT =      -4208
951955                 TA   =          133
89329
                                          MA   =          133
86433
                                          Ha   =            185
952  n
mi
                                          Hp   =            183
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17574637
83                 X    =         5355008
30
 Y    =       -4976691
97  feet           Y    =        -1457003
03  meter
 Z    =       12363177
83                 Z    =         3794315
04
 XDOT =      14168
974263                 XDOT =        4285
305379
 YDOT =      15703
588587  feet/sec       YDOT =        4834
561281  meter/sec
 ZDOT =     -13808
897489                 ZDOT =       -4188
053277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4588535
18                 X    =         1398585
52
 Y    =       17607404
23  feet           Y    =         5366736
81  meter
 Z    =       12466281
93                 Z    =         3799722
73
 XDOT =     -14730
280404                 XDOT =       -4489
789467
 YDOT =      13564
823805  feet/sec       YDOT =        4134
558296  meter/sec
 ZDOT =     -13725
833785                 ZDOT =       -4183
634138


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   10034
41780036  
00016717  00000-0  10270-3 0  9149
2 25544  51
6423 197
5527 0011570 279
7707  80
2150 15
75667534  2403


Satellite: ISS
Catalog Number: 25544
Epoch time:      10034
41780036   =   yrday
fracday
Element set:     914
Inclination:       51
6423  deg
RA of node:       197
5527  deg
Eccentricity:     
0011570     
Arg of perigee:   279
7707  deg
Mean anomaly:      80
2150  deg
Mean motion:   15
75667534  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             240
Checksum:              296


Coasting Arc #16 (Orbit 255)
---------------------------------------

Vector Time (GMT): 2010/035/09:04:16
224
Vector Time (MET): N/A
Weight (LBS)     : 750804
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3541814
31                 A    =         6720387
97  meter
 Y    =       -4016677
71  meter          E    =           
0000770
 Z    =        4060606
20                 I    =           51
56766
 XDOT =       6431
167685                 Wp   =          294
41139
 YDOT =      -1789
900074  meter/sec      RA   =          191
60437  deg
 ZDOT =       3839
853257                 TA   =          116
06045
                                          MA   =          116
05252
                                          Ha   =            186
383  n
mi
                                          Hp   =            183
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11620125
68                 X    =        -3516361
28
 Y    =      -13178076
48  feet           Y    =        -4056142
04  meter
 Z    =       13322198
82                 Z    =         4043462
16
 XDOT =      21099
631511                 XDOT =        6432
051642
 YDOT =      -5872
375570  feet/sec       YDOT =       -1717
977985  meter/sec
 ZDOT =      12597
943757                 ZDOT =        3871
097573

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13234821
19                 X    =         4033973
50
 Y    =      -11633557
86  feet           Y    =        -3545908
44  meter
 Z    =       13254049
99                 Z    =         4039834
44
 XDOT =       4920
824807                 XDOT =        1499
867401
 YDOT =      20088
663283  feet/sec       YDOT =        6123
024569  meter/sec
 ZDOT =      12721
767775                 ZDOT =        3877
594818


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   10035
43257410  
00016717  00000-0  10270-3 0  9158
2 25544  51
6410 192
3277 0011504 283
7328  76
2555 15
75645293  2564


Satellite: ISS
Catalog Number: 25544
Epoch time:      10035
43257410   =   yrday
fracday
Element set:     915
Inclination:       51
6410  deg
RA of node:       192
3277  deg
Eccentricity:     
0011504     
Arg of perigee:   283
7328  deg
Mean anomaly:      76
2555  deg
Mean motion:   15
75645293  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             256
Checksum:              296

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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