Date: March 5th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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


There are no maneuvers



Coasting Arc #1 (Orbit 682)
---------------------------------------

Vector Time (GMT): 2010/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2334582
12                 A    =         6731191
76  meter
 Y    =       -5914448
52  meter          E    =           
0005984
 Z    =       -2219041
34                 I    =           51
92461
 XDOT =       5376
637737                 Wp   =           56
36566
 YDOT =        -61
683272  meter/sec      RA   =           52
59302  deg
 ZDOT =      -5499
509581                 TA   =          148
37862
                                          MA   =          148
34266
                                          Ha   =            192
468  n
mi
                                          Hp   =            183
549

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7659390
15                 X    =        -2257492
59
 Y    =      -19404358
67  feet           Y    =        -5940124
38  meter
 Z    =       -7280319
37                 Z    =        -2230194
85
 XDOT =      17639
887588                 XDOT =        5403
643270
 YDOT =       -202
372939  feet/sec       YDOT =          -1
408026  meter/sec
 ZDOT =     -18043
010435                 ZDOT =       -5473
324514

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -660027
86                 X    =         -201176
49
 Y    =      -20835317
22  feet           Y    =        -6350604
69  meter
 Z    =       -7324777
30                 Z    =        -2232592
12
 XDOT =      15264
498189                 XDOT =        4652
619048
 YDOT =       5814
604550  feet/sec       YDOT =        1772
291467  meter/sec
 ZDOT =     -17938
994350                 ZDOT =       -5467
805478


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   10062
52737403  
00016717  00000-0  10270-3 0  9007
2 25544  51
6434  53
0429 0007756   6
5608 353
5655 15
73583780  6834


Satellite: ISS
Catalog Number: 25544
Epoch time:      10062
52737403   =   yrday
fracday
Element set:     900
Inclination:       51
6434  deg
RA of node:        53
0429  deg
Eccentricity:     
0007756     
Arg of perigee:     6
5608  deg
Mean anomaly:     353
5655  deg
Mean motion:   15
73583780  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             683
Checksum:              305


Coasting Arc #2 (Orbit 698)
---------------------------------------

Vector Time (GMT): 2010/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4620269
52                 A    =         6723154
28  meter
 Y    =         590969
84  meter          E    =           
0013420
 Z    =        4846222
21                 I    =           51
87837
 XDOT =      -3379
481698                 Wp   =           32
42543
 YDOT =      -6484
569647  meter/sec      RA   =           47
44043  deg
 ZDOT =      -2416
995361                 TA   =           81
16161
                                          MA   =           81
00967
                                          Ha   =            192
587  n
mi
                                          Hp   =            183
400

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15158364
58                 X    =        -4650076
37
 Y    =        1938877
44  feet           Y    =          539136
93  meter
 Z    =       15899679
15                 Z    =         4823704
65
 XDOT =     -11087
538379                 XDOT =       -3294
977670
 YDOT =     -21274
834799  feet/sec       YDOT =       -6521
888702  meter/sec
 ZDOT =      -7929
774805                 ZDOT =       -2433
207047

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15071889
77                 X    =        -4593912
00
 Y    =       -3034685
51  feet           Y    =         -924972
14  meter
 Z    =       15810246
12                 Z    =         4818963
02
 XDOT =      -3886
899659                 XDOT =       -1184
727016
 YDOT =     -22588
225302  feet/sec       YDOT =       -6884
891072  meter/sec
 ZDOT =      -7994
328838                 ZDOT =       -2436
671430


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   10063
54346368  
00016717  00000-0  10270-3 0  9017
2 25544  51
6433  47
8282 0007790   9
0495 351
0807 15
73620520  6994


Satellite: ISS
Catalog Number: 25544
Epoch time:      10063
54346368   =   yrday
fracday
Element set:     901
Inclination:       51
6433  deg
RA of node:        47
8282  deg
Eccentricity:     
0007790     
Arg of perigee:     9
0495  deg
Mean anomaly:     351
0807  deg
Mean motion:   15
73620520  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             699
Checksum:              305


Coasting Arc #3 (Orbit 714)
---------------------------------------

Vector Time (GMT): 2010/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3537615
89                 A    =         6731282
66  meter
 Y    =        5351031
40  meter          E    =           
0019427
 Z    =        2001381
67                 I    =           51
88573
 XDOT =      -5127
180459                 Wp   =           49
54347
 YDOT =       1282
212240  meter/sec      RA   =           42
36303  deg
 ZDOT =       5611
505950                 TA   =          332
70072
                                          MA   =          332
80269
                                          Ha   =            192
410  n
mi
                                          Hp   =            183
122

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11606351
34                 X    =         3467794
50
 Y    =       17555877
29  feet           Y    =         5390200
83  meter
 Z    =        6566212
83                 Z    =         2018397
42
 XDOT =     -16821
458200                 XDOT =       -5168
396805
 YDOT =       4206
733070  feet/sec       YDOT =        1224
646888  meter/sec
 ZDOT =      18410
452591                 ZDOT =        5586
498114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5701833
93                 X    =         1737918
98
 Y    =       20236390
46  feet           Y    =         6168051
81  meter
 Z    =        6633924
98                 Z    =         2022020
33
 XDOT =     -15932
534299                 XDOT =       -4856
236454
 YDOT =      -1538
119812  feet/sec       YDOT =        -468
818919  meter/sec
 ZDOT =      18311
142150                 ZDOT =        5581
236127


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   10064
55953136  
00016717  00000-0  10270-3 0  9027
2 25544  51
6438  42
6142 0007607  13
2273 346
9088 15
73691943  7155


Satellite: ISS
Catalog Number: 25544
Epoch time:      10064
55953136   =   yrday
fracday
Element set:     902
Inclination:       51
6438  deg
RA of node:        42
6142  deg
Eccentricity:     
0007607     
Arg of perigee:    13
2273  deg
Mean anomaly:     346
9088  deg
Mean motion:   15
73691943  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             715
Checksum:              306


Coasting Arc #4 (Orbit 729)
---------------------------------------

Vector Time (GMT): 2010/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4284171
28                 A    =         6722692
42  meter
 Y    =       -1615506
44  meter          E    =           
0014793
 Z    =       -4933241
14                 I    =           51
83342
 XDOT =       4666
201052                 Wp   =           73
84525
 YDOT =       5707
098354  meter/sec      RA   =           37
20977  deg
 ZDOT =       2192
772911                 TA   =          217
36506
                                          MA   =          217
46802
                                          Ha   =            192
676  n
mi
                                          Hp   =            183
087

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14055680
06                 X    =         4325882
32
 Y    =       -5300217
98  feet           Y    =        -1567365
24  meter
 Z    =      -16185174
34                 Z    =        -4912327
46
 XDOT =      15309
058569                 XDOT =        4591
384465
 YDOT =      18724
075966  feet/sec       YDOT =        5758
860336  meter/sec
 ZDOT =       7194
136848                 ZDOT =        2215
259185

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15076217
25                 X    =         4595231
02
 Y    =       -1021440
69  feet           Y    =         -311335
12  meter
 Z    =      -16102131
96                 Z    =        -4907929
82
 XDOT =       9183
389187                 XDOT =        2799
097024
 YDOT =      21215
533041  feet/sec       YDOT =        6466
494471  meter/sec
 ZDOT =       7283
580584                 ZDOT =        2220
035362


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   10065
51207836  
00016717  00000-0  10270-3 0  9034
2 25544  51
6440  37
7250 0007851  16
6668 343
4751 15
73659748  7302


Satellite: ISS
Catalog Number: 25544
Epoch time:      10065
51207836   =   yrday
fracday
Element set:     903
Inclination:       51
6440  deg
RA of node:        37
7250  deg
Eccentricity:     
0007851     
Arg of perigee:    16
6668  deg
Mean anomaly:     343
4751  deg
Mean motion:   15
73659748  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             730
Checksum:              310


Coasting Arc #5 (Orbit 745)
---------------------------------------

Vector Time (GMT): 2010/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4564765
70                 A    =         6731416
27  meter
 Y    =       -4589599
11  meter          E    =           
0007425
 Z    =       -1857296
59                 I    =           51
83951
 XDOT =       4648
403512                 Wp   =           74
99013
 YDOT =      -2337
600932  meter/sec      RA   =           32
12512  deg
 ZDOT =      -5664
970243                 TA   =          125
54360
                                          MA   =          125
47435
                                          Ha   =            192
636  n
mi
                                          Hp   =            182
726

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14976265
43                 X    =        -4504082
43
 Y    =      -15057739
85  feet           Y    =        -4640305
77  meter
 Z    =       -6093492
73                 Z    =        -1879324
43
 XDOT =      15250
667690                 XDOT =        4701
716555
 YDOT =      -7669
294395  feet/sec       YDOT =       -2285
321772  meter/sec
 ZDOT =     -18585
860376                 ZDOT =       -5642
259034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10316657
94                 X    =        -3144517
34
 Y    =      -18534169
11  feet           Y    =        -5649214
74  meter
 Z    =       -6181088
41                 Z    =        -1883995
75
 XDOT =      15509
050852                 XDOT =        4727
158700
 YDOT =      -2482
716142  feet/sec       YDOT =        -756
731880  meter/sec
 ZDOT =     -18495
689094                 ZDOT =       -5637
486036


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   10066
52810532  
00016717  00000-0  10270-3 0  9040
2 25544  51
6446  32
5097 0007920  20
2338 339
9138 15
73723016  7468


Satellite: ISS
Catalog Number: 25544
Epoch time:      10066
52810532   =   yrday
fracday
Element set:     904
Inclination:       51
6446  deg
RA of node:        32
5097  deg
Eccentricity:     
0007920     
Arg of perigee:    20
2338  deg
Mean anomaly:     339
9138  deg
Mean motion:   15
73723016  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             746
Checksum:              292


Coasting Arc #6 (Orbit 761)
---------------------------------------

Vector Time (GMT): 2010/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3804745
86                 A    =         6722253
86  meter
 Y    =        2451668
28  meter          E    =           
0013431
 Z    =        4966380
11                 I    =           51
78256
 XDOT =      -5731
218394                 Wp   =           37
50146
 YDOT =      -4723
704914  meter/sec      RA   =           26
97066  deg
 ZDOT =      -2045
484842                 TA   =           72
32458
                                          MA   =           72
17798
                                          Ha   =            192
759  n
mi
                                          Hp   =            182
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12482762
02                 X    =        -3856003
46
 Y    =        8043531
10  feet           Y    =         2408834
88  meter
 Z    =       16293897
99                 Z    =         4947772
39
 XDOT =     -18803
209955                 XDOT =       -5668
034695
 YDOT =     -15497
719533  feet/sec       YDOT =       -4787
441572  meter/sec
 ZDOT =      -6710
908273                 ZDOT =       -2073
173057

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14206881
84                 X    =        -4330257
59
 Y    =        4591740
03  feet           Y    =         1399562
36  meter
 Z    =       16220027
24                 Z    =         4943864
30
 XDOT =     -13885
851649                 XDOT =       -4232
407583
 YDOT =     -18713
004267  feet/sec       YDOT =       -5703
723701  meter/sec
 ZDOT =      -6820
990503                 ZDOT =       -2079
037905


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   10067
54411056  
00016717  00000-0  10270-3 0  9052
2 25544  51
6447  27
2950 0007867  23
7194 336
4331 15
73747089  7627


Satellite: ISS
Catalog Number: 25544
Epoch time:      10067
54411056   =   yrday
fracday
Element set:     905
Inclination:       51
6447  deg
RA of node:        27
2950  deg
Eccentricity:     
0007867     
Arg of perigee:    23
7194  deg
Mean anomaly:     336
4331  deg
Mean motion:   15
73747089  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             762
Checksum:              313


Coasting Arc #7 (Orbit 777)
---------------------------------------

Vector Time (GMT): 2010/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5394416
55                 A    =         6731435
60  meter
 Y    =        3621172
07  meter          E    =           
0020847
 Z    =        1714726
39                 I    =           51
78693
 XDOT =      -4010
902729                 Wp   =           51
44422
 YDOT =       3247
448369  meter/sec      RA   =           21
88029  deg
 ZDOT =       5726
281284                 TA   =          327
50790
                                          MA   =          327
63606
                                          Ha   =            192
609  n
mi
                                          Hp   =            182
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17698217
01                 X    =         5345193
36
 Y    =       11880485
79  feet           Y    =         3681220
47  meter
 Z    =        5625742
76                 Z    =         1740812
27
 XDOT =     -13159
129689                 XDOT =       -4074
734872
 YDOT =      10654
358166  feet/sec       YDOT =        3202
239357  meter/sec
 ZDOT =      18787
012086                 ZDOT =        5706
641550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14347813
92                 X    =         4373213
68
 Y    =       15726906
28  feet           Y    =         4793561
03  meter
 Z    =        5729438
38                 Z    =         1746332
82
 XDOT =     -14268
789008                 XDOT =       -4349
126890
 YDOT =       6162
067855  feet/sec       YDOT =        1878
198282  meter/sec
 ZDOT =      18709
055551                 ZDOT =        5702
520132


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   10068
56009246  
00016717  00000-0  10270-3 0  9060
2 25544  51
6449  22
0798 0007794  27
6772 332
4805 15
73797559  7782


Satellite: ISS
Catalog Number: 25544
Epoch time:      10068
56009246   =   yrday
fracday
Element set:     906
Inclination:       51
6449  deg
RA of node:        22
0798  deg
Eccentricity:     
0007794     
Arg of perigee:    27
6772  deg
Mean anomaly:     332
4805  deg
Mean motion:   15
73797559  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             778
Checksum:              346


Coasting Arc #8 (Orbit 792)
---------------------------------------

Vector Time (GMT): 2010/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3178566
06                 A    =         6721895
08  meter
 Y    =       -3175024
31  meter          E    =           
0016997
 Z    =       -5013167
78                 I    =           51
72678
 XDOT =       6548
669012                 Wp   =           77
70541
 YDOT =       3545
643113  meter/sec      RA   =           16
72294  deg
 ZDOT =       1915
539017                 TA   =          210
74558
                                          MA   =          210
84526
                                          Ha   =            192
714  n
mi
                                          Hp   =            182
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10428366
33                 X    =         3238186
04
 Y    =      -10416746
42  feet           Y    =        -3139146
58  meter
 Z    =      -16447400
86                 Z    =        -4997581
68
 XDOT =      21485
134554                 XDOT =        6499
229148
 YDOT =      11632
687379  feet/sec       YDOT =        3618
597878  meter/sec
 ZDOT =       6284
576829                 ZDOT =        1947
231501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12559873
51                 X    =         3828249
45
 Y    =       -7844735
39  feet           Y    =        -2391075
35  meter
 Z    =      -16385546
36                 Z    =        -4994314
53
 XDOT =      17788
892806                 XDOT =        5422
054527
 YDOT =      15152
944846  feet/sec       YDOT =        4618
617589  meter/sec
 ZDOT =       6410
543402                 ZDOT =        1953
933629


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   10069
51255595  
00016717  00000-0  10270-3 0  9077
2 25544  51
6454  17
1903 0007865  30
4957 329
6662 15
73811450  7930


Satellite: ISS
Catalog Number: 25544
Epoch time:      10069
51255595   =   yrday
fracday
Element set:     907
Inclination:       51
6454  deg
RA of node:        17
1903  deg
Eccentricity:     
0007865     
Arg of perigee:    30
4957  deg
Mean anomaly:     329
6662  deg
Mean motion:   15
73811450  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             793
Checksum:              321


Coasting Arc #9 (Orbit 808)
---------------------------------------

Vector Time (GMT): 2010/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5997778
08                 A    =         6731321
84  meter
 Y    =       -2571201
07  meter          E    =           
0009159
 Z    =       -1660214
99                 I    =           51
73078
 XDOT =       3272
014471                 Wp   =           87
04164
 YDOT =      -3946
279278  meter/sec      RA   =           11
62647  deg
 ZDOT =      -5735
622960                 TA   =          111
26145
                                          MA   =          111
16361
                                          Ha   =            192
687  n
mi
                                          Hp   =            182
026

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19677749
60                 X    =        -5960515
84
 Y    =       -8435699
05  feet           Y    =        -2638063
55  meter
 Z    =       -5446899
58                 Z    =        -1689260
87
 XDOT =      10734
955615                 XDOT =        3343
761284
 YDOT =     -12947
110493  feet/sec       YDOT =       -3909
288882  meter/sec
 ZDOT =     -18817
660631                 ZDOT =       -5719
553348

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17519862
64                 X    =        -5340054
13
 Y    =      -12253914
76  feet           Y    =        -3734993
22  meter
 Z    =       -5562333
05                 Z    =        -1695399
11
 XDOT =      12357
821470                 XDOT =        3766
663984
 YDOT =      -9194
445456  feet/sec       YDOT =       -2802
466975  meter/sec
 ZDOT =     -18753
902306                 ZDOT =       -5716
189423


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   10070
52849443  
00016717  00000-0  10270-3 0  9082
2 25544  51
6462  11
9747 0007882  34
2779 325
8891 15
73858835  8098


Satellite: ISS
Catalog Number: 25544
Epoch time:      10070
52849443   =   yrday
fracday
Element set:     908
Inclination:       51
6462  deg
RA of node:        11
9747  deg
Eccentricity:     
0007882     
Arg of perigee:    34
2779  deg
Mean anomaly:     325
8891  deg
Mean motion:   15
73858835  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             809
Checksum:              344


Coasting Arc #10 (Orbit 824)
---------------------------------------

Vector Time (GMT): 2010/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2516562
54                 A    =         6721615
48  meter
 Y    =        3700908
99  meter          E    =           
0013404
 Z    =        5009562
18                 I    =           51
66863
 XDOT =      -7115
203417                 Wp   =           44
80012
 YDOT =      -2292
849937  meter/sec      RA   =            6
46607  deg
 ZDOT =      -1868
086842                 TA   =           63
27109
                                          MA   =           63
13397
                                          Ha   =            192
776  n
mi
                                          Hp   =            181
894

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8256438
79                 X    =        -2582094
76
 Y    =       12142089
86  feet           Y    =         3672401
29  meter
 Z    =       16435571
44                 Z    =         4997177
50
 XDOT =     -23343
843233                 XDOT =       -7079
960911
 YDOT =      -7522
473548  feet/sec       YDOT =       -2372
219472  meter/sec
 ZDOT =      -6128
893840                 ZDOT =       -1902
565961

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10470418
84                 X    =        -3191383
66
 Y    =       10372161
38  feet           Y    =         3161434
79  meter
 Z    =       16386449
70                 Z    =         4994589
87
 XDOT =     -20739
774533                 XDOT =       -6321
483278
 YDOT =     -10972
798902  feet/sec       YDOT =       -3344
509105  meter/sec
 ZDOT =      -6265
902416                 ZDOT =       -1909
847056


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   10071
54441006  
00016717  00000-0  10270-3 0  9099
2 25544  51
6464   6
7597 0007856  38
0241 322
1476 15
73891192  8252


Satellite: ISS
Catalog Number: 25544
Epoch time:      10071
54441006   =   yrday
fracday
Element set:     909
Inclination:       51
6464  deg
RA of node:         6
7597  deg
Eccentricity:     
0007856     
Arg of perigee:    38
0241  deg
Mean anomaly:     322
1476  deg
Mean motion:   15
73891192  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             825
Checksum:              305


Coasting Arc #11 (Orbit 840)
---------------------------------------

Vector Time (GMT): 2010/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6369724
42                 A    =         6731251
17  meter
 Y    =        1418921
21  meter          E    =           
0021579
 Z    =        1602497
16                 I    =           51
67151
 XDOT =      -2460
695945                 Wp   =           55
26551
 YDOT =       4495
045370  meter/sec      RA   =            1
36421  deg
 ZDOT =       5758
392842                 TA   =          322
43237
                                          MA   =          322
58294
                                          Ha   =            192
678  n
mi
                                          Hp   =            181
722

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20898045
99                 X    =         6345599
88
 Y    =        4655253
33  feet           Y    =         1490016
53  meter
 Z    =        5257536
60                 Z    =         1633381
94
 XDOT =      -8073
149425                 XDOT =       -2538
750157
 YDOT =      14747
524179  feet/sec       YDOT =        4467
092543  meter/sec
 ZDOT =      18892
364968                 ZDOT =        5746
248984

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19775572
62                 X    =         6027594
53
 Y    =        8125336
12  feet           Y    =         2476602
45  meter
 Z    =        5380245
47                 Z    =         1639898
82
 XDOT =      -9973
236978                 XDOT =       -3039
842631
 YDOT =      11705
073431  feet/sec       YDOT =        3567
706382  meter/sec
 ZDOT =      18844
220002                 ZDOT =        5743
718257


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   10072
56030268  
00016717  00000-0  10270-3 0  9108
2 25544  51
6465   1
5437 0007854  41
5707 318
6052 15
73917605  8419


Satellite: ISS
Catalog Number: 25544
Epoch time:      10072
56030268   =   yrday
fracday
Element set:     910
Inclination:       51
6465  deg
RA of node:         1
5437  deg
Eccentricity:     
0007854     
Arg of perigee:    41
5707  deg
Mean anomaly:     318
6052  deg
Mean motion:   15
73917605  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             841
Checksum:              291


Coasting Arc #12 (Orbit 855)
---------------------------------------

Vector Time (GMT): 2010/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1783892
58                 A    =         6721394
67  meter
 Y    =       -4109398
13  meter          E    =           
0018486
 Z    =       -5025795
78                 I    =           51
60905
 XDOT =       7400
848175                 Wp   =           82
31116
 YDOT =        970
596474  meter/sec      RA   =          356
19904  deg
 ZDOT =       1841
483080                 TA   =          205
43751
                                          MA   =          205
52861
                                          Ha   =            192
701  n
mi
                                          Hp   =            181
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5852665
96                 X    =         1854126
05
 Y    =      -13482277
34  feet           Y    =        -4089057
44  meter
 Z    =      -16488831
29                 Z    =        -5016958
72
 XDOT =      24280
997948                 XDOT =        7380
499291
 YDOT =       3184
371634  feet/sec       YDOT =        1053
243584  meter/sec
 ZDOT =       6041
611156                 ZDOT =        1877
386301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7936593
18                 X    =         2419073
60
 Y    =      -12417304
10  feet           Y    =        -3784794
29  meter
 Z    =      -16453817
36                 Z    =        -5015123
53
 XDOT =      22570
044194                 XDOT =        6879
349470
 YDOT =       6266
904388  feet/sec       YDOT =        1910
152457  meter/sec
 ZDOT =       6184
237830                 ZDOT =        1884
955691


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   10073
51268022  
00016717  00000-0  10270-3 0  9116
2 25544  51
6472 356
6539 0007834  44
9494 315
2302 15
73956941  8565


Satellite: ISS
Catalog Number: 25544
Epoch time:      10073
51268022   =   yrday
fracday
Element set:     911
Inclination:       51
6472  deg
RA of node:       356
6539  deg
Eccentricity:     
0007834     
Arg of perigee:    44
9494  deg
Mean anomaly:     315
2302  deg
Mean motion:   15
73956941  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             856
Checksum:              315


Coasting Arc #13 (Orbit 871)
---------------------------------------

Vector Time (GMT): 2010/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6522442
87                 A    =         6730973
01  meter
 Y    =        -295001
84  meter          E    =           
0010645
 Z    =       -1642622
09                 I    =           51
61241
 XDOT =       1655
169590                 Wp   =           95
20098
 YDOT =      -4856
577287  meter/sec      RA   =          351
09277  deg
 ZDOT =      -5732
787818                 TA   =          102
93475
                                          MA   =          102
81584
                                          Ha   =            192
662  n
mi
                                          Hp   =            181
444

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21399090
79                 X    =        -6510679
87
 Y    =        -967853
79  feet           Y    =         -367874
09  meter
 Z    =       -5389180
09                 Z    =        -1674279
15
 XDOT =       5430
346423                 XDOT =        1737
202230
 YDOT =     -15933
652515  feet/sec       YDOT =       -4837
610200  meter/sec
 ZDOT =     -18808
358983                 ZDOT =       -5724
547270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21038724
94                 X    =        -6412603
36
 Y    =       -3854712
00  feet           Y    =        -1174916
22  meter
 Z    =       -5514919
57                 Z    =        -1680947
48
 XDOT =       7368
052543                 XDOT =        2245
782415
 YDOT =     -13502
013637  feet/sec       YDOT =       -4115
413757  meter/sec
 ZDOT =     -18775
733554                 ZDOT =       -5722
843587


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   10074
52852742  
00016717  00000-0  10270-3 0  9127
2 25544  51
6478 351
4379 0007768  48
9447 311
2387 15
73988746  8729


Satellite: ISS
Catalog Number: 25544
Epoch time:      10074
52852742   =   yrday
fracday
Element set:     912
Inclination:       51
6478  deg
RA of node:       351
4379  deg
Eccentricity:     
0007768     
Arg of perigee:    48
9447  deg
Mean anomaly:     311
2387  deg
Mean motion:   15
73988746  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             872
Checksum:              350


Coasting Arc #14 (Orbit 887)
---------------------------------------

Vector Time (GMT): 2010/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1092183
43                 A    =         6721173
96  meter
 Y    =        4359355
71  meter          E    =           
0013530
 Z    =        4990793
11                 I    =           51
54979
 XDOT =      -7462
642849                 Wp   =           52
89349
 YDOT =        317
162407  meter/sec      RA   =          345
92257  deg
 ZDOT =      -1898
600882                 TA   =           55
50487
                                          MA   =           55
37716
                                          Ha   =            192
638  n
mi
                                          Hp   =            181
301

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3583278
98                 X    =        -1165093
58
 Y    =       14302348
11  feet           Y    =         4346735
19  meter
 Z    =       16373993
16                 Z    =         4985309
71
 XDOT =     -24483
736381                 XDOT =       -7456
411771
 YDOT =       1040
559077  feet/sec       YDOT =         233
745313  meter/sec
 ZDOT =      -6229
005520                 ZDOT =       -1934
839069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5347874
62                 X    =        -1630032
18
 Y    =       13766150
73  feet           Y    =         4195922
74  meter
 Z    =       16352309
71                 Z    =         4984184
00
 XDOT =     -23393
953499                 XDOT =       -7130
477027
 YDOT =      -1472
830015  feet/sec       YDOT =        -448
918589  meter/sec
 ZDOT =      -6372
917929                 ZDOT =       -1942
465385


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   10075
54435011  
00016717  00000-0  10270-3 0  9137
2 25544  51
6473 346
2223 0007757  51
8041 308
3818 15
74059815  8885


Satellite: ISS
Catalog Number: 25544
Epoch time:      10075
54435011   =   yrday
fracday
Element set:     913
Inclination:       51
6473  deg
RA of node:       346
2223  deg
Eccentricity:     
0007757     
Arg of perigee:    51
8041  deg
Mean anomaly:     308
3818  deg
Mean motion:   15
74059815  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             888
Checksum:              306


Coasting Arc #15 (Orbit 903)
---------------------------------------

Vector Time (GMT): 2010/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6453768
25                 A    =         6730755
41  meter
 Y    =        -838810
89  meter          E    =           
0021877
 Z    =        1673894
22                 I    =           51
55353
 XDOT =       -832
859680                 Wp   =           60
95937
 YDOT =       5098
534806  meter/sec      RA   =          340
81216  deg
 ZDOT =       5720
484312                 TA   =          317
58589
                                          MA   =          317
75477
                                          Ha   =            192
631  n
mi
                                          Hp   =            181
172

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21173780
34                 X    =         6454536
86
 Y    =       -2752004
24  feet           Y    =         -766636
54  meter
 Z    =        5491778
93                 Z    =         1705248
52
 XDOT =      -2732
479265                 XDOT =        -917
599536
 YDOT =      16727
476398  feet/sec       YDOT =        5088
748102  meter/sec
 ZDOT =      18767
993150                 ZDOT =        5716
231891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21311164
47                 X    =         6495642
93
 Y    =        -594845
43  feet           Y    =         -181308
89  meter
 Z    =        5616276
81                 Z    =         1711841
17
 XDOT =      -4567
084438                 XDOT =       -1392
047337
 YDOT =      14799
573020  feet/sec       YDOT =        4510
909856  meter/sec
 ZDOT =      18751
214945                 ZDOT =        5715
370315


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   10076
56015147  
00016717  00000-0  10270-3 0  9145
2 25544  51
6476 341
0058 0007819  55
8034 304
3870 15
74054821  9047


Satellite: ISS
Catalog Number: 25544
Epoch time:      10076
56015147   =   yrday
fracday
Element set:     914
Inclination:       51
6476  deg
RA of node:       341
0058  deg
Eccentricity:     
0007819     
Arg of perigee:    55
8034  deg
Mean anomaly:     304
3870  deg
Mean motion:   15
74054821  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             904
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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