Date: February 12th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 25833 39 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 351)
---------------------------------------

Vector Time (GMT): 2010/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4216087
76                 A    =         6717671
58  meter
 Y    =        2382850
16  meter          E    =           
0010675
 Z    =       -4661545
18                 I    =           51
74607
 XDOT =      -5635
880796                 Wp   =            7
78628
 YDOT =       4413
822719  meter/sec      RA   =          160
10456  deg
 ZDOT =      -2831
472846                 TA   =          234
23462
                                          MA   =          234
33392
                                          Ha   =            187
812  n
mi
                                          Hp   =            182
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13832308
92                 X    =         4211773
25
 Y    =        7817749
88  feet           Y    =         2429972
97  meter
 Z    =      -15293783
39                 Z    =        -4641074
42
 XDOT =     -18490
422560                 XDOT =       -5671
063687
 YDOT =      14481
045666  feet/sec       YDOT =        4350
602325  meter/sec
 ZDOT =      -9289
609075                 ZDOT =       -2858
936497

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5557966
18                 X    =         1694068
09
 Y    =       14967967
49  feet           Y    =         4562236
49  meter
 Z    =      -15212453
93                 Z    =        -4636755
96
 XDOT =     -22334
546641                 XDOT =       -6807
569816
 YDOT =      -1290
832162  feet/sec       YDOT =        -393
445643  meter/sec
 ZDOT =      -9398
418845                 ZDOT =       -2864
638064


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   10041
52084275  
00016717  00000-0  10270-3 0  9006
2 25544  51
6446 160
9963 0011205 308
5494  51
4666 15
75809537  3522


Satellite: ISS
Catalog Number: 25544
Epoch time:      10041
52084275   =   yrday
fracday
Element set:     900
Inclination:       51
6446  deg
RA of node:       160
9963  deg
Eccentricity:     
0011205     
Arg of perigee:   308
5494  deg
Mean anomaly:      51
4666  deg
Mean motion:   15
75809537  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             352
Checksum:              302


Coasting Arc #2 (Orbit 367)
---------------------------------------

Vector Time (GMT): 2010/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5054864
78                 A    =         6725297
39  meter
 Y    =       -4011184
40  meter          E    =           
0005306
 Z    =        1894734
58                 I    =           51
80078
 XDOT =       4386
282477                 Wp   =           66
98905
 YDOT =       2853
427307  meter/sec      RA   =          154
92587  deg
 ZDOT =      -5646
694891                 TA   =           92
00327
                                          MA   =           91
94251
                                          Ha   =            187
913  n
mi
                                          Hp   =            182
400

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16584202
02                 X    =         5090138
87
 Y    =      -13160053
80  feet           Y    =        -3954460
70  meter
 Z    =        6216320
79                 Z    =         1919375
98
 XDOT =      14390
690541                 XDOT =        4381
478727
 YDOT =       9361
638147  feet/sec       YDOT =        2902
450530  meter/sec
 ZDOT =     -18525
901873                 ZDOT =       -5625
398621

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21140121
94                 X    =         6443509
17
 Y    =         307582
65  feet           Y    =           93751
19  meter
 Z    =        6313957
10                 Z    =         1924494
12
 XDOT =       5305
237995                 XDOT =        1617
036541
 YDOT =      14888
680871  feet/sec       YDOT =        4538
069930  meter/sec
 ZDOT =     -18441
267131                 ZDOT =       -5620
898222


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   10042
53548869  
00016717  00000-0  10270-3 0  9013
2 25544  51
6450 155
7721 0011124 312
8345  47
1883 15
75851699  3680


Satellite: ISS
Catalog Number: 25544
Epoch time:      10042
53548869   =   yrday
fracday
Element set:     901
Inclination:       51
6450  deg
RA of node:       155
7721  deg
Eccentricity:     
0011124     
Arg of perigee:   312
8345  deg
Mean anomaly:      47
1883  deg
Mean motion:   15
75851699  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             368
Checksum:              317


Coasting Arc #3 (Orbit 383)
---------------------------------------

Vector Time (GMT): 2010/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3428915
99                 A    =         6715315
69  meter
 Y    =       -2669204
11  meter          E    =           
0006700
 Z    =        5122003
25                 I    =           51
79563
 XDOT =       5880
341527                 Wp   =          325
08034
 YDOT =      -4754
252091  meter/sec      RA   =          149
81720  deg
 ZDOT =       1465
346171                 TA   =          110
94513
                                          MA   =          110
87342
                                          Ha   =            188
091  n
mi
                                          Hp   =            182
066

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11249724
38                 X    =        -3423694
61
 Y    =       -8757231
32  feet           Y    =        -2707519
05  meter
 Z    =       16804472
59                 Z    =         5105358
80
 XDOT =      19292
459079                 XDOT =        5925
949218
 YDOT =     -15597
939932  feet/sec       YDOT =       -4688
239611  meter/sec
 ZDOT =       4807
566179                 ZDOT =        1494
022772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3468182
69                 X    =        -1057102
09
 Y    =      -13908153
20  feet           Y    =        -4239205
10  meter
 Z    =       16738299
83                 Z    =         5101833
79
 XDOT =      23771
061808                 XDOT =        7245
419639
 YDOT =        -30
085877  feet/sec       YDOT =          -9
170175  meter/sec
 ZDOT =       4921
197616                 ZDOT =        1499
981034


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   10043
55010525  
00016717  00000-0  10270-3 0  9020
2 25544  51
6460 150
5473 0011247 317
0958  42
9328 15
75937757  3846


Satellite: ISS
Catalog Number: 25544
Epoch time:      10043
55010525   =   yrday
fracday
Element set:     902
Inclination:       51
6460  deg
RA of node:       150
5473  deg
Eccentricity:     
0011247     
Arg of perigee:   317
0958  deg
Mean anomaly:      42
9328  deg
Mean motion:   15
75937757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             384
Checksum:              300


Coasting Arc #4 (Orbit 398)
---------------------------------------

Vector Time (GMT): 2010/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5147828
08                 A    =         6726519
43  meter
 Y    =        4264321
93  meter          E    =           
0017167
 Z    =        -638272
97                 I    =           51
85914
 XDOT =      -3493
294365                 Wp   =          359
96651
 YDOT =      -3318
438564  meter/sec      RA   =          144
66256  deg
 ZDOT =       6020
404963                 TA   =          353
09210
                                          MA   =          353
11573
                                          Ha   =            188
319  n
mi
                                          Hp   =            181
730

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16889199
73                 X    =        -5192029
37
 Y    =       13990557
50  feet           Y    =         4206508
70  meter
 Z    =       -2094071
44                 Z    =         -663387
82
 XDOT =     -11460
939519                 XDOT =       -3485
172504
 YDOT =     -10887
265631  feet/sec       YDOT =       -3357
457088  meter/sec
 ZDOT =      19751
984787                 ZDOT =        6003
454878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21903863
65                 X    =        -6676297
64
 Y    =         880232
93  feet           Y    =          268295
00  meter
 Z    =       -2193592
69                 Z    =         -668607
05
 XDOT =      -2531
950791                 XDOT =        -771
738601
 YDOT =     -14080
899236  feet/sec       YDOT =       -4291
858087  meter/sec
 ZDOT =      19684
565961                 ZDOT =        5999
855705


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   10044
50128569  
00016717  00000-0  10270-3 0  9035
2 25544  51
6463 145
6499 0011368 321
8168  38
2190 15
75922805  3991


Satellite: ISS
Catalog Number: 25544
Epoch time:      10044
50128569   =   yrday
fracday
Element set:     903
Inclination:       51
6463  deg
RA of node:       145
6499  deg
Eccentricity:     
0011368     
Arg of perigee:   321
8168  deg
Mean anomaly:      38
2190  deg
Mean motion:   15
75922805  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             399
Checksum:              320


Coasting Arc #5 (Orbit 414)
---------------------------------------

Vector Time (GMT): 2010/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2669955
56                 A    =         6714437
01  meter
 Y    =        3179671
68  meter          E    =           
0012737
 Z    =       -5284169
01                 I    =           51
84269
 XDOT =      -5874
402733                 Wp   =           42
91559
 YDOT =       4975
203538  meter/sec      RA   =          139
53453  deg
 ZDOT =         34
751918                 TA   =          227
35961
                                          MA   =          227
46705
                                          Ha   =            188
460  n
mi
                                          Hp   =            181
459

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8759696
73                 X    =         2659870
28
 Y    =       10431993
71  feet           Y    =         3209472
09  meter
 Z    =      -17336512
49                 Z    =        -5271223
37
 XDOT =     -19272
974846                 XDOT =       -5929
768559
 YDOT =      16322
846253  feet/sec       YDOT =        4909
202917  meter/sec
 ZDOT =        114
015478                 ZDOT =           6
080194

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         948988
99                 X    =          289251
84
 Y    =       13654374
43  feet           Y    =         4161853
33  meter
 Z    =      -17284991
29                 Z    =        -5268465
34
 XDOT =     -24202
711339                 XDOT =       -7376
986416
 YDOT =       1644
362802  feet/sec       YDOT =         501
201782  meter/sec
 ZDOT =           
396574                 ZDOT =            
120876


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   10045
51585020  
00016717  00000-0  10270-3 0  9047
2 25544  51
6461 140
4260 0011381 325
4725  34
5699 15
75987067  4155


Satellite: ISS
Catalog Number: 25544
Epoch time:      10045
51585020   =   yrday
fracday
Element set:     904
Inclination:       51
6461  deg
RA of node:       140
4260  deg
Eccentricity:     
0011381     
Arg of perigee:   325
4725  deg
Mean anomaly:      34
5699  deg
Mean motion:   15
75987067  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             415
Checksum:              296


Coasting Arc #6 (Orbit 430)
---------------------------------------

Vector Time (GMT): 2010/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5068080
24                 A    =         6726203
23  meter
 Y    =       -4364605
73  meter          E    =           
0001919
 Z    =        -722379
77                 I    =           51
90413
 XDOT =       2626
331273                 Wp   =           36
46515
 YDOT =       4041
705533  meter/sec      RA   =          134
40788  deg
 ZDOT =      -6000
658849                 TA   =          151
37706
                                          MA   =          151
36652
                                          Ha   =            188
516  n
mi
                                          Hp   =            181
164

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16627559
85                 X    =         5120018
47
 Y    =      -14319572
61  feet           Y    =        -4307641
09  meter
 Z    =       -2370012
36                 Z    =         -697633
25
 XDOT =       8616
572418                 XDOT =        2610
090392
 YDOT =      13260
188757  feet/sec       YDOT =        4070
983567  meter/sec
 ZDOT =     -19687
200948                 ZDOT =       -5987
940141

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21859289
33                 X    =         6662711
39
 Y    =       -2037793
22  feet           Y    =         -621119
37  meter
 Z    =       -2271944
92                 Z    =         -692488
81
 XDOT =       -708
018581                 XDOT =        -215
804064
 YDOT =      14272
848545  feet/sec       YDOT =        4350
364237  meter/sec
 ZDOT =     -19636
543205                 ZDOT =       -5985
218369


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   10046
53038770  
00016717  00000-0  10270-3 0  9056
2 25544  51
6453 135
2012 0011304 329
7259  30
3251 15
76025262  4314


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
53038770   =   yrday
fracday
Element set:     905
Inclination:       51
6453  deg
RA of node:       135
2012  deg
Eccentricity:     
0011304     
Arg of perigee:   329
7259  deg
Mean anomaly:      30
3251  deg
Mean motion:   15
76025262  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             431
Checksum:              264


Coasting Arc #7 (Orbit 446)
---------------------------------------

Vector Time (GMT): 2010/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1953454
42                 A    =         6714928
67  meter
 Y    =       -3922341
15  meter          E    =           
0013186
 Z    =        5092210
93                 I    =           51
88774
 XDOT =       5678
566694                 Wp   =          355
27121
 YDOT =      -4944
134360  meter/sec      RA   =          129
25432  deg
 ZDOT =      -1617
321175                 TA   =          110
28071
                                          MA   =          110
13893
                                          Ha   =            188
631  n
mi
                                          Hp   =            180
761

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6408971
21                 X    =        -1934185
44
 Y    =      -12868573
33  feet           Y    =        -3944077
75  meter
 Z    =       16706728
78                 Z    =         5082768
32
 XDOT =      18630
468155                 XDOT =        5741
287328
 YDOT =     -16220
913256  feet/sec       YDOT =       -4880
282679  meter/sec
 ZDOT =      -5306
171834                 ZDOT =       -1589
582602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1901128
63                 X    =          579464
01
 Y    =      -14293959
64  feet           Y    =        -4356798
90  meter
 Z    =       16669082
33                 Z    =         5080736
29
 XDOT =      23519
737524                 XDOT =        7168
815997
 YDOT =      -2979
695407  feet/sec       YDOT =        -908
211160  meter/sec
 ZDOT =      -5196
242144                 ZDOT =       -1583
814606


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   10047
54489557  
00016717  00000-0  10270-3 0  9062
2 25544  51
6458 129
9754 0011488 333
5522  26
5055 15
76109666  4478


Satellite: ISS
Catalog Number: 25544
Epoch time:      10047
54489557   =   yrday
fracday
Element set:     906
Inclination:       51
6458  deg
RA of node:       129
9754  deg
Eccentricity:     
0011488     
Arg of perigee:   333
5522  deg
Mean anomaly:      26
5055  deg
Mean motion:   15
76109666  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             447
Checksum:              334


Coasting Arc #8 (Orbit 462)
---------------------------------------

Vector Time (GMT): 2010/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4811694
57                 A    =         6724340
55  meter
 Y    =        4193128
24  meter          E    =           
0018009
 Z    =        2078562
87                 I    =           51
93691
 XDOT =      -1913
648418                 Wp   =           29
87636
 YDOT =      -4965
948166  meter/sec      RA   =          124
15480  deg
 ZDOT =       5582
742739                 TA   =          353
28413
                                          MA   =          353
30823
                                          Ha   =            188
868  n
mi
                                          Hp   =            180
437

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15786399
49                 X    =        -4868322
37
 Y    =       13756982
43  feet           Y    =         4139004
54  meter
 Z    =        6819431
99                 Z    =         2055050
21
 XDOT =      -6278
374075                 XDOT =       -1885
095580
 YDOT =     -16292
480860  feet/sec       YDOT =       -4987
187681  meter/sec
 ZDOT =      18316
085101                 ZDOT =        5573
516093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20786211
18                 X    =        -6335637
17
 Y    =        2767798
34  feet           Y    =          843624
93  meter
 Z    =        6726242
94                 Z    =         2050158
85
 XDOT =       3843
422355                 XDOT =        1171
475134
 YDOT =     -15600
012285  feet/sec       YDOT =       -4754
883745  meter/sec
 ZDOT =      18279
256786                 ZDOT =        5571
517468


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   10048
55937853  
00016717  00000-0  10270-3 0  9072
2 25544  51
6451 124
7502 0011460 338
2941  21
7736 15
76113652  4633


Satellite: ISS
Catalog Number: 25544
Epoch time:      10048
55937853   =   yrday
fracday
Element set:     907
Inclination:       51
6451  deg
RA of node:       124
7502  deg
Eccentricity:     
0011460     
Arg of perigee:   338
2941  deg
Mean anomaly:      21
7736  deg
Mean motion:   15
76113652  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             463
Checksum:              299


Coasting Arc #9 (Orbit 477)
---------------------------------------

Vector Time (GMT): 2010/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1434951
02                 A    =         6717037
65  meter
 Y    =        4742760
60  meter          E    =           
0009586
 Z    =       -4536285
90                 I    =           51
92794
 XDOT =      -5338
663913                 Wp   =           39
06865
 YDOT =       4591
005356  meter/sec      RA   =          118
98273  deg
 ZDOT =       3122
031626                 TA   =          261
86679
                                          MA   =          261
97554
                                          Ha   =            188
937  n
mi
                                          Hp   =            180
074

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4707844
56                 X    =         1403846
16
 Y    =       15560238
17  feet           Y    =         4758632
86  meter
 Z    =      -14882827
76                 Z    =        -4529390
85
 XDOT =     -17515
301551                 XDOT =       -5404
770640
 YDOT =      15062
353530  feet/sec       YDOT =        4530
935824  meter/sec
 ZDOT =      10242
885911                 ZDOT =        3095
935871

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4296630
77                 X    =        -1309613
06
 Y    =       15704881
08  feet           Y    =         4786847
75  meter
 Z    =      -14855270
07                 Z    =        -4527886
32
 XDOT =     -21766
605645                 XDOT =       -6634
461400
 YDOT =       3602
226879  feet/sec       YDOT =        1097
958753  meter/sec
 ZDOT =      10139
447282                 ZDOT =        3090
503532


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   10049
51042999  
00016717  00000-0  10270-3 0  9088
2 25544  51
6440 119
8516 0011515 342
5027  17
5739 15
76178224  4783


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
51042999   =   yrday
fracday
Element set:     908
Inclination:       51
6440  deg
RA of node:       119
8516  deg
Eccentricity:     
0011515     
Arg of perigee:   342
5027  deg
Mean anomaly:      17
5739  deg
Mean motion:   15
76178224  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             478
Checksum:              315


Coasting Arc #10 (Orbit 493)
---------------------------------------

Vector Time (GMT): 2010/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4505322
22                 A    =         6721162
60  meter
 Y    =       -3716539
20  meter          E    =           
0011133
 Z    =       -3339452
85                 I    =           51
95513
 XDOT =       1398
032899                 Wp   =           10
68537
 YDOT =       5926
874160  meter/sec      RA   =          113
90004  deg
 ZDOT =      -4701
802868                 TA   =          208
38607
                                          MA   =          208
44677
                                          Ha   =            189
030  n
mi
                                          Hp   =            179
903

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14781240
86                 X    =         4562768
67
 Y    =      -12193370
06  feet           Y    =        -3665836
98  meter
 Z    =      -10956210
14                 Z    =        -3317426
49
 XDOT =       4586
722110                 XDOT =        1354
493915
 YDOT =      19445
125198  feet/sec       YDOT =        5942
264117  meter/sec
 ZDOT =     -15425
862429                 ZDOT =       -4695
117348

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19026284
33                 X    =         5799211
46
 Y    =       -2658891
46  feet           Y    =         -810430
12  meter
 Z    =      -10868886
62                 Z    =        -3312836
64
 XDOT =      -6346
917312                 XDOT =       -1934
540397
 YDOT =      17641
931018  feet/sec       YDOT =        5377
260574  meter/sec
 ZDOT =     -15399
098928                 ZDOT =       -4693
645353


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   10050
52485870  
00016717  00000-0  10270-3 0  9091
2 25544  51
6437 114
6252 0011543 346
5650  13
5205 15
76194588  4949


Satellite: ISS
Catalog Number: 25544
Epoch time:      10050
52485870   =   yrday
fracday
Element set:     909
Inclination:       51
6437  deg
RA of node:       114
6252  deg
Eccentricity:     
0011543     
Arg of perigee:   346
5650  deg
Mean anomaly:      13
5205  deg
Mean motion:   15
76194588  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             494
Checksum:              304


Coasting Arc #11 (Orbit 509)
---------------------------------------

Vector Time (GMT): 2010/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1061910
94                 A    =         6720145
44  meter
 Y    =       -5589750
71  meter          E    =           
0015903
 Z    =        3578742
94                 I    =           51
96423
 XDOT =       4979
705091                 Wp   =           39
37047
 YDOT =      -3817
743926  meter/sec      RA   =          108
71874  deg
 ZDOT =      -4462
664903                 TA   =           98
09904
                                          MA   =           97
91859
                                          Ha   =            189
105  n
mi
                                          Hp   =            179
446

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3483959
77                 X    =        -1016711
16
 Y    =      -18339077
14  feet           Y    =        -5601372
78  meter
 Z    =       11741282
61                 Z    =         3573694
20
 XDOT =      16337
615127                 XDOT =        5043
704305
 YDOT =     -12525
406581  feet/sec       YDOT =       -3761
700221  meter/sec
 ZDOT =     -14641
289052                 ZDOT =       -4438
318132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6233398
32                 X    =         1899939
81
 Y    =      -17609072
64  feet           Y    =        -5367245
34  meter
 Z    =       11721038
76                 Z    =         3572572
61
 XDOT =      19222
256909                 XDOT =        5858
943906
 YDOT =      -2926
719555  feet/sec       YDOT =        -892
064120  meter/sec
 ZDOT =     -14544
744159                 ZDOT =       -4433
238020


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   10051
53925750  
00016717  00000-0  10270-3 0  9101
2 25544  51
6443 109
3987 0011758 350
1023   9
9908 15
76277972  5102


Satellite: ISS
Catalog Number: 25544
Epoch time:      10051
53925750   =   yrday
fracday
Element set:     910
Inclination:       51
6443  deg
RA of node:       109
3987  deg
Eccentricity:     
0011758     
Arg of perigee:   350
1023  deg
Mean anomaly:       9
9908  deg
Mean motion:   15
76277972  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             510
Checksum:              307


Coasting Arc #12 (Orbit 525)
---------------------------------------

Vector Time (GMT): 2010/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4210935
79                 A    =         6717407
36  meter
 Y    =        2867666
50  meter          E    =           
0011553
 Z    =        4366493
34                 I    =           51
96331
 XDOT =      -1099
958112                 Wp   =           43
38645
 YDOT =      -6822
539917  meter/sec      RA   =          103
63901  deg
 ZDOT =       3422
807375                 TA   =           12
32809
                                          MA   =           12
29985
                                          Ha   =            189
335  n
mi
                                          Hp   =            179
127

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13815406
14                 X    =        -4263901
01
 Y    =        9408354
65  feet           Y    =         2820281
24  meter
 Z    =       14325765
54                 Z    =         4345908
12
 XDOT =      -3608
786458                 XDOT =       -1040
212725
 YDOT =     -22383
661144  feet/sec       YDOT =       -6834
506191  meter/sec
 ZDOT =      11229
682990                 ZDOT =        3417
609062

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16729783
28                 X    =        -5099237
94
 Y    =        1352667
62  feet           Y    =          412293
09  meter
 Z    =       14244114
02                 Z    =         4341605
95
 XDOT =       7912
100766                 XDOT =        2411
608313
 YDOT =     -20074
873881  feet/sec       YDOT =       -6118
821559  meter/sec
 ZDOT =      11208
812033                 ZDOT =        3416
445908


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   10052
55363077  
00016717  00000-0  10270-3 0  9113
2 25544  51
6439 104
1721 0011659 354
8947   5
2097 15
76295491  5263


Satellite: ISS
Catalog Number: 25544
Epoch time:      10052
55363077   =   yrday
fracday
Element set:     911
Inclination:       51
6439  deg
RA of node:       104
1721  deg
Eccentricity:     
0011659     
Arg of perigee:   354
8947  deg
Mean anomaly:       5
2097  deg
Mean motion:   15
76295491  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             526
Checksum:              310


Coasting Arc #13 (Orbit 540)
---------------------------------------

Vector Time (GMT): 2010/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         902197
14                 A    =         6723190
35  meter
 Y    =        6237569
63  meter          E    =           
0016306
 Z    =       -2316589
86                 I    =           51
98959
 XDOT =      -4719
743998                 Wp   =           13
72073
 YDOT =       2703
242635  meter/sec      RA   =           98
46524  deg
 ZDOT =       5463
792256                 TA   =          320
31096
                                          MA   =          320
43018
                                          Ha   =            189
338  n
mi
                                          Hp   =            178
807

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2959964
36                 X    =          843633
91
 Y    =       20464467
28  feet           Y    =         6247331
08  meter
 Z    =       -7600360
44                 Z    =        -2312349
30
 XDOT =     -15484
724404                 XDOT =       -4776
163137
 YDOT =       8868
906283  feet/sec       YDOT =        2650
148207  meter/sec
 ZDOT =      17925
827612                 ZDOT =        5440
726986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7119684
04                 X    =        -2170079
70
 Y    =       19419697
05  feet           Y    =         5919123
66  meter
 Z    =       -7583320
80                 Z    =        -2311396
18
 XDOT =     -16516
470096                 XDOT =       -5034
220085
 YDOT =        879
092435  feet/sec       YDOT =         267
947374  meter/sec
 ZDOT =      17834
310597                 ZDOT =        5435
897870


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   10053
50458029  
00016717  00000-0  10270-3 0  9122
2 25544  51
6443  99
2724 0011721 358
8760   1
2376 15
76339545  5414


Satellite: ISS
Catalog Number: 25544
Epoch time:      10053
50458029   =   yrday
fracday
Element set:     912
Inclination:       51
6443  deg
RA of node:        99
2724  deg
Eccentricity:     
0011721     
Arg of perigee:   358
8760  deg
Mean anomaly:       1
2376  deg
Mean motion:   15
76339545  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             541
Checksum:              300


Coasting Arc #14 (Orbit 556)
---------------------------------------

Vector Time (GMT): 2010/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4067985
01                 A    =         6714457
01  meter
 Y    =       -1761123
05  meter          E    =           
0020127
 Z    =       -5058733
91                 I    =           51
96431
 XDOT =        968
234248                 Wp   =           42
53894
 YDOT =       7416
609979  meter/sec      RA   =           93
37090  deg
 ZDOT =      -1793
008598                 TA   =          210
18703
                                          MA   =          210
30315
                                          Ha   =            189
426  n
mi
                                          Hp   =            178
676

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13346407
51                 X    =         4111949
86
 Y    =       -5777962
76  feet           Y    =        -1715386
57  meter
 Z    =      -16596896
01                 Z    =        -5038865
19
 XDOT =       3176
621547                 XDOT =         893
938400
 YDOT =      24332
709905  feet/sec       YDOT =        7427
021953  meter/sec
 ZDOT =      -5882
574139                 ZDOT =       -1788
485398

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14592852
39                 X    =         4447901
41
 Y    =        1082394
26  feet           Y    =          329913
77  meter
 Z    =      -16518035
18                 Z    =        -5034697
12
 XDOT =      -8308
667023                 XDOT =       -2532
481709
 YDOT =      22001
726370  feet/sec       YDOT =        6706
126198  meter/sec
 ZDOT =      -5864
382370                 ZDOT =       -1787
463746


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   10054
51889876  
00016717  00000-0  10270-3 0  9133
2 25544  51
6451  94
0455 0011731   2
9081 357
2149 15
76358307  5577


Satellite: ISS
Catalog Number: 25544
Epoch time:      10054
51889876   =   yrday
fracday
Element set:     913
Inclination:       51
6451  deg
RA of node:        94
0455  deg
Eccentricity:     
0011731     
Arg of perigee:     2
9081  deg
Mean anomaly:     357
2149  deg
Mean motion:   15
76358307  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             557
Checksum:              314


Coasting Arc #15 (Orbit 572)
---------------------------------------

Vector Time (GMT): 2010/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -798245
95                 A    =         6725013
89  meter
 Y    =       -6635648
15  meter          E    =           
0012764
 Z    =         757297
04                 I    =           52
00073
 XDOT =       4652
678082                 Wp   =           73
39254
 YDOT =      -1254
576285  meter/sec      RA   =           88
21918  deg
 ZDOT =      -6002
339529                 TA   =           98
39321
                                          MA   =           98
24848
                                          Ha   =            189
472  n
mi
                                          Hp   =            178
213

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2618917
14                 X    =         -727664
35
 Y    =      -21770499
18  feet           Y    =        -6644179
97  meter
 Z    =        2484570
35                 Z    =          753590
65
 XDOT =      15264
691870                 XDOT =        4695
518819
 YDOT =      -4116
063926  feet/sec       YDOT =       -1202
307707  meter/sec
 ZDOT =     -19692
714990                 ZDOT =       -5979
633267

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7362663
88                 X    =         2244139
95
 Y    =      -20656196
53  feet           Y    =        -6296008
70  meter
 Z    =        2469651
17                 Z    =          752749
68
 XDOT =      14093
905157                 XDOT =        4295
822292
 YDOT =       2645
856648  feet/sec       YDOT =         806
457106  meter/sec
 ZDOT =     -19602
559634                 ZDOT =       -5974
860177


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   10055
53318806  
00016717  00000-0  10270-3 0  9147
2 25544  51
6446  88
8184 0011864   7
2618 352
8716 15
76431395  5730


Satellite: ISS
Catalog Number: 25544
Epoch time:      10055
53318806   =   yrday
fracday
Element set:     914
Inclination:       51
6446  deg
RA of node:        88
8184  deg
Eccentricity:     
0011864     
Arg of perigee:     7
2618  deg
Mean anomaly:     352
8716  deg
Mean motion:   15
76431395  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             573
Checksum:              321

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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