Date: April 29th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17222 26 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 1533)
---------------------------------------

Vector Time (GMT): 2010/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3669773
55                 A    =         6722242
50  meter
 Y    =       -2125211
81  meter          E    =           
0008696
 Z    =        5221591
15                 I    =           51
86222
 XDOT =       4819
371407                 Wp   =          220
76490
 YDOT =      -5919
922259  meter/sec      RA   =          134
88732  deg
 ZDOT =        972
114112                 TA   =          219
96060
                                          MA   =          220
02463
                                          Ha   =            190
757  n
mi
                                          Hp   =            187
367

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12039939
46                 X    =        -3671102
23
 Y    =       -6972479
68  feet           Y    =        -2166256
67  meter
 Z    =       17131204
54                 Z    =         5203759
95
 XDOT =      15811
585982                 XDOT =        4880
488425
 YDOT =     -19422
317124  feet/sec       YDOT =       -5865
687425  meter/sec
 ZDOT =       3189
350760                 ZDOT =         995
675611

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13970340
83                 X    =        -4258159
88
 Y    =         913081
23  feet           Y    =          278307
16  meter
 Z    =       17060177
14                 Z    =         5199941
99
 XDOT =       2469
364233                 XDOT =         752
662218
 YDOT =     -23898
200502  feet/sec       YDOT =       -7284
171513  meter/sec
 ZDOT =       3282
934968                 ZDOT =        1000
638578


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   10116
54931956  
00016717  00000-0  10270-3 0  9008
2 25544  51
6438 135
5875 0009852 241
9344 118
0823 15
73365358 15346


Satellite: ISS
Catalog Number: 25544
Epoch time:      10116
54931956   =   yrday
fracday
Element set:     900
Inclination:       51
6438  deg
RA of node:       135
5875  deg
Eccentricity:     
0009852     
Arg of perigee:   241
9344  deg
Mean anomaly:     118
0823  deg
Mean motion:   15
73365358  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1534
Checksum:              318


Coasting Arc #2 (Orbit 1548)
---------------------------------------

Vector Time (GMT): 2010/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3599902
17                 A    =         6733283
36  meter
 Y    =        5592438
58  meter          E    =           
0004600
 Z    =       -1032558
71                 I    =           51
92116
 XDOT =      -4539
803073                 Wp   =          319
15158
 YDOT =      -1823
023789  meter/sec      RA   =          129
75647  deg
 ZDOT =       5942
449351                 TA   =           29
60992
                                          MA   =           29
58389
                                          Ha   =            190
391  n
mi
                                          Hp   =            187
376

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11810702
64                 X    =        -3657154
18
 Y    =       18347895
62  feet           Y    =         5551862
21  meter
 Z    =       -3387659
80                 Z    =        -1050186
49
 XDOT =     -14894
367036                 XDOT =       -4547
948181
 YDOT =      -5981
049176  feet/sec       YDOT =       -1873
836052  meter/sec
 ZDOT =      19496
224904                 ZDOT =        5920
374798

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         710655
22                 X    =          216607
71
 Y    =       21798022
97  feet           Y    =         6644037
40  meter
 Z    =       -3457654
26                 Z    =        -1053893
02
 XDOT =     -14161
339397                 XDOT =       -4316
376248
 YDOT =       3546
091366  feet/sec       YDOT =        1080
848648  meter/sec
 ZDOT =      19408
318314                 ZDOT =        5915
655422


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   10117
50203694  
00016717  00000-0  10270-3 0  9017
2 25544  51
6443 130
7002 0009909 245
1816 114
8316 15
73440076 15492


Satellite: ISS
Catalog Number: 25544
Epoch time:      10117
50203694   =   yrday
fracday
Element set:     901
Inclination:       51
6443  deg
RA of node:       130
7002  deg
Eccentricity:     
0009909     
Arg of perigee:   245
1816  deg
Mean anomaly:     114
8316  deg
Mean motion:   15
73440076  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1549
Checksum:              283


Coasting Arc #3 (Orbit 1564)
---------------------------------------

Vector Time (GMT): 2010/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4193736
35                 A    =         6722396
88  meter
 Y    =        1039827
50  meter          E    =           
0004551
 Z    =       -5153614
84                 I    =           51
90156
 XDOT =      -3373
600882                 Wp   =          100
12481
 YDOT =       6779
492967  meter/sec      RA   =          124
66575  deg
 ZDOT =      -1379
187838                 TA   =          156
72420
                                          MA   =          156
70359
                                          Ha   =            190
202  n
mi
                                          Hp   =            187
667

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13758977
53                 X    =         4206832
97
 Y    =        3411507
55  feet           Y    =         1086797
67  meter
 Z    =      -16908185
17                 Z    =        -5133209
41
 XDOT =     -11068
244362                 XDOT =       -3442
459669
 YDOT =      22242
430995  feet/sec       YDOT =        6741
382366  meter/sec
 ZDOT =      -4524
894482                 ZDOT =       -1395
744287

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13255881
66                 X    =         4040392
73
 Y    =       -5288688
76  feet           Y    =        -1611992
33  meter
 Z    =      -16826941
04                 Z    =        -5128851
63
 XDOT =       3575
020688                 XDOT =        1089
666306
 YDOT =      23547
561154  feet/sec       YDOT =        7177
296640  meter/sec
 ZDOT =      -4590
609803                 ZDOT =       -1399
217868


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   10118
51824905  
00016717  00000-0  10270-3 0  9024
2 25544  51
6432 125
4858 0009901 250
1256 109
8840 15
73419235 15653


Satellite: ISS
Catalog Number: 25544
Epoch time:      10118
51824905   =   yrday
fracday
Element set:     902
Inclination:       51
6432  deg
RA of node:       125
4858  deg
Eccentricity:     
0009901     
Arg of perigee:   250
1256  deg
Mean anomaly:     109
8840  deg
Mean motion:   15
73419235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1565
Checksum:              301


Coasting Arc #4 (Orbit 1580)
---------------------------------------

Vector Time (GMT): 2010/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2268121
52                 A    =         6732852
35  meter
 Y    =       -6181893
87  meter          E    =           
0009912
 Z    =        1371605
77                 I    =           51
95286
 XDOT =       4972
312308                 Wp   =          164
21349
 YDOT =        524
383799  meter/sec      RA   =          119
52995  deg
 ZDOT =      -5858
407915                 TA   =             
77902
                                          MA   =             
77748
                                          Ha   =            189
757  n
mi
                                          Hp   =            187
780

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7441343
56                 X    =         2330416
85
 Y    =      -20281804
04  feet           Y    =        -6156182
13  meter
 Z    =        4500018
93                 Z    =         1382775
58
 XDOT =      16313
360589                 XDOT =        4994
538652
 YDOT =       1720
419289  feet/sec       YDOT =         580
111673  meter/sec
 ZDOT =     -19220
498410                 ZDOT =       -5834
197927

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6126723
06                 X    =        -1867425
19
 Y    =      -20707189
25  feet           Y    =        -6311551
28  meter
 Z    =        4544328
04                 Z    =         1385111
19
 XDOT =      12708
074755                 XDOT =        3873
421185
 YDOT =      -7957
266852  feet/sec       YDOT =       -2425
374936  meter/sec
 ZDOT =     -19124
118646                 ZDOT =       -5829
031363


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   10119
53444054  
00016717  00000-0  10270-3 0  9031
2 25544  51
6426 120
2714 0009790 254
6980 105
3101 15
73470228 15817


Satellite: ISS
Catalog Number: 25544
Epoch time:      10119
53444054   =   yrday
fracday
Element set:     903
Inclination:       51
6426  deg
RA of node:       120
2714  deg
Eccentricity:     
0009790     
Arg of perigee:   254
6980  deg
Mean anomaly:     105
3101  deg
Mean motion:   15
73470228  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1581
Checksum:              282


Coasting Arc #5 (Orbit 1596)
---------------------------------------

Vector Time (GMT): 2010/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4417389
42                 A    =         6722605
81  meter
 Y    =         118189
28  meter          E    =           
0007323
 Z    =        5072033
13                 I    =           51
93178
 XDOT =       1808
623982                 Wp   =          227
05042
 YDOT =      -7274
009237  meter/sec      RA   =          114
44677  deg
 ZDOT =       1741
381094                 TA   =          206
22611
                                          MA   =          206
26321
                                          Ha   =            189
479  n
mi
                                          Hp   =            187
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14492747
44                 X    =        -4443022
16
 Y    =         387760
09  feet           Y    =           68647
76  meter
 Z    =       16640528
66                 Z    =         5050510
83
 XDOT =       5933
805715                 XDOT =        1881
369379
 YDOT =     -23864
859702  feet/sec       YDOT =       -7253
377497  meter/sec
 ZDOT =       5713
192564                 ZDOT =        1750
343778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11331169
58                 X    =        -3453740
49
 Y    =        9199927
15  feet           Y    =         2804137
79  meter
 Z    =       16554854
78                 Z    =         5045919
74
 XDOT =      -9195
660886                 XDOT =       -2802
837438
 YDOT =     -21690
069639  feet/sec       YDOT =       -6611
133226  meter/sec
 ZDOT =       5748
707898                 ZDOT =        1752
206167


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   10120
55061168  
00016717  00000-0  10270-3 0  9047
2 25544  51
6422 115
0567 0009879 258
8777 101
1276 15
73478430 15976


Satellite: ISS
Catalog Number: 25544
Epoch time:      10120
55061168   =   yrday
fracday
Element set:     904
Inclination:       51
6422  deg
RA of node:       115
0567  deg
Eccentricity:     
0009879     
Arg of perigee:   258
8777  deg
Mean anomaly:     101
1276  deg
Mean motion:   15
73478430  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1597
Checksum:              317


Coasting Arc #6 (Orbit 1611)
---------------------------------------

Vector Time (GMT): 2010/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -886793
64                 A    =         6732282
16  meter
 Y    =        6459291
30  meter          E    =           
0006892
 Z    =       -1661046
61                 I    =           51
97668
 XDOT =      -5048
582560                 Wp   =          314
82142
 YDOT =        790
372420  meter/sec      RA   =          109
30815  deg
 ZDOT =       5759
106970                 TA   =           26
91461
                                          MA   =           26
87888
                                          Ha   =            188
948  n
mi
                                          Hp   =            187
772

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2909427
97                 X    =         -950887
52
 Y    =       21191900
60  feet           Y    =         6449016
41  meter
 Z    =       -5449627
99                 Z    =        -1665509
89
 XDOT =     -16563
591077                 XDOT =       -5085
022483
 YDOT =       2593
085368  feet/sec       YDOT =         733
711972  meter/sec
 ZDOT =      18894
707906                 ZDOT =        5734
492185

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10951644
97                 X    =         3338061
39
 Y    =       18369277
77  feet           Y    =         5598955
86  meter
 Z    =       -5467263
87                 Z    =        -1666422
03
 XDOT =     -10088
023195                 XDOT =       -3074
829470
 YDOT =      11618
364805  feet/sec       YDOT =        3541
277593  meter/sec
 ZDOT =      18796
727389                 ZDOT =        5729
242508


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   10121
50325233  
00016717  00000-0  10270-3 0  9050
2 25544  51
6424 110
1690 0009759 262
0682  97
9374 15
73538105 16125


Satellite: ISS
Catalog Number: 25544
Epoch time:      10121
50325233   =   yrday
fracday
Element set:     905
Inclination:       51
6424  deg
RA of node:       110
1690  deg
Eccentricity:     
0009759     
Arg of perigee:   262
0682  deg
Mean anomaly:      97
9374  deg
Mean motion:   15
73538105  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1612
Checksum:              289


Coasting Arc #7 (Orbit 1627)
---------------------------------------

Vector Time (GMT): 2010/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4339836
85                 A    =         6722786
37  meter
 Y    =       -1245782
11  meter          E    =           
0003803
 Z    =       -4983995
81                 I    =           51
95363
 XDOT =       -226
438117                 Wp   =           42
81768
 YDOT =       7416
259900  meter/sec      RA   =          104
23051  deg
 ZDOT =      -2049
095174                 TA   =          207
41530
                                          MA   =          207
43537
                                          Ha   =            188
444  n
mi
                                          Hp   =            187
402

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14238309
88                 X    =         4377656
42
 Y    =       -4087211
64  feet           Y    =        -1197039
60  meter
 Z    =      -16351692
30                 Z    =        -4962820
94
 XDOT =       -742
907207                 XDOT =        -299
397020
 YDOT =      24331
561352  feet/sec       YDOT =        7413
319968  meter/sec
 ZDOT =      -6722
753195                 ZDOT =       -2050
371829

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8456268
87                 X    =         2577470
75
 Y    =      -12274999
57  feet           Y    =        -3741419
87  meter
 Z    =      -16267406
39                 Z    =        -4958305
47
 XDOT =      14045
817068                 XDOT =        4281
165042
 YDOT =      18599
995481  feet/sec       YDOT =        5669
278622  meter/sec
 ZDOT =      -6727
694405                 ZDOT =       -2050
601255


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   10122
51938278  
00016717  00000-0  10270-3 0  9062
2 25544  51
6425 104
9539 0009842 266
7342  93
2695 15
73544583 16285


Satellite: ISS
Catalog Number: 25544
Epoch time:      10122
51938278   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:       104
9539  deg
Eccentricity:     
0009842     
Arg of perigee:   266
7342  deg
Mean anomaly:      93
2695  deg
Mean motion:   15
73544583  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1628
Checksum:              331


Coasting Arc #8 (Orbit 1643)
---------------------------------------

Vector Time (GMT): 2010/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -482984
12                 A    =         6731728
50  meter
 Y    =       -6432675
97  meter          E    =           
0006058
 Z    =        1910331
85                 I    =           51
99090
 XDOT =       4805
410369                 Wp   =          149
81267
 YDOT =      -2042
060787  meter/sec      RA   =           99
08830  deg
 ZDOT =      -5658
722441                 TA   =            9
06363
                                          MA   =            9
05270
                                          Ha   =            188
037  n
mi
                                          Hp   =            187
136

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1584593
56                 X    =         -420296
97
 Y    =      -21104579
94  feet           Y    =        -6437726
62  meter
 Z    =        6267492
95                 Z    =         1908137
28
 XDOT =      15765
782049                 XDOT =        4855
377093
 YDOT =      -6699
674497  feet/sec       YDOT =       -1988
044018  meter/sec
 ZDOT =     -18565
362338                 ZDOT =       -5635
256427

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14940857
97                 X    =        -4553973
51
 Y    =      -14993195
03  feet           Y    =        -4569925
85  meter
 Z    =        6258639
22                 Z    =         1907633
24
 XDOT =       6624
924171                 XDOT =        2019
276887
 YDOT =     -14316
131904  feet/sec       YDOT =       -4363
557004  meter/sec
 ZDOT =     -18471
958652                 ZDOT =       -5630
252997


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   10123
53549117  
00016717  00000-0  10270-3 0  9076
2 25544  51
6428  99
7396 0009955 271
5690  88
4333 15
73601689 16449


Satellite: ISS
Catalog Number: 25544
Epoch time:      10123
53549117   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:        99
7396  deg
Eccentricity:     
0009955     
Arg of perigee:   271
5690  deg
Mean anomaly:      88
4333  deg
Mean motion:   15
73601689  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1644
Checksum:              339


Coasting Arc #9 (Orbit 1659)
---------------------------------------

Vector Time (GMT): 2010/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4002644
61                 A    =         6722882
67  meter
 Y    =        2283385
46  meter          E    =           
0005124
 Z    =        4899781
54                 I    =           51
96532
 XDOT =      -1300
113272                 Wp   =          238
35920
 YDOT =      -7226
849011  meter/sec      RA   =           94
01583  deg
 ZDOT =       2304
900224                 TA   =          189
28773
                                          MA   =          189
29721
                                          Ha   =            188
529  n
mi
                                          Hp   =            187
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13132036
13                 X    =        -4051682
67
 Y    =        7491422
12  feet           Y    =         2238351
01  meter
 Z    =       16075398
76                 Z    =         4880217
67
 XDOT =      -4265
463491                 XDOT =       -1230
401536
 YDOT =     -23710
134549  feet/sec       YDOT =       -7240
998017  meter/sec
 ZDOT =       7562
008609                 ZDOT =        2298
753132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4943851
63                 X    =        -1506885
98
 Y    =       14374546
90  feet           Y    =         4381361
89  meter
 Z    =       15997529
69                 Z    =         4876047
05
 XDOT =     -17888
319482                 XDOT =       -5452
359778
 YDOT =     -14543
985518  feet/sec       YDOT =       -4433
006786  meter/sec
 ZDOT =       7537
407636                 ZDOT =        2297
401848


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   10124
55157838  
00016717  00000-0  10270-3 0  9085
2 25544  51
6431  94
5254 0010056 275
0340  84
9675 15
73636568 16606


Satellite: ISS
Catalog Number: 25544
Epoch time:      10124
55157838   =   yrday
fracday
Element set:     908
Inclination:       51
6431  deg
RA of node:        94
5254  deg
Eccentricity:     
0010056     
Arg of perigee:   275
0340  deg
Mean anomaly:      84
9675  deg
Mean motion:   15
73636568  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1660
Checksum:              315


Coasting Arc #10 (Orbit 1674)
---------------------------------------

Vector Time (GMT): 2010/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1770390
79                 A    =         6731265
29  meter
 Y    =        6135900
35  meter          E    =           
0008475
 Z    =       -2110248
05                 I    =           51
99448
 XDOT =      -4288
069030                 Wp   =          319
04356
 YDOT =       3153
603445  meter/sec      RA   =           88
86994  deg
 ZDOT =       5565
911585                 TA   =           17
49146
                                          MA   =           17
46229
                                          Ha   =            188
968  n
mi
                                          Hp   =            187
554

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5808368
74                 X    =         1711897
69
 Y    =       20130906
65  feet           Y    =         6155370
96  meter
 Z    =       -6923386
00                 Z    =        -2101789
27
 XDOT =     -14068
467946                 XDOT =       -4350
052734
 YDOT =      10346
467996  feet/sec       YDOT =        3105
304875  meter/sec
 ZDOT =      18260
864781                 ZDOT =        5544
929694

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17908224
01                 X    =         5458426
68
 Y    =       10897372
47  feet           Y    =         3321519
13  meter
 Z    =       -6889601
58                 Z    =        -2099950
56
 XDOT =      -2673
301923                 XDOT =        -814
822426
 YDOT =      15898
396441  feet/sec       YDOT =        4845
831235  meter/sec
 ZDOT =      18177
356124                 ZDOT =        5540
458147


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   10125
50414108  
00016717  00000-0  10270-3 0  9098
2 25544  51
6430  89
6364 0009900 278
9703  81
0340 15
73646041 16753


Satellite: ISS
Catalog Number: 25544
Epoch time:      10125
50414108   =   yrday
fracday
Element set:     909
Inclination:       51
6430  deg
RA of node:        89
6364  deg
Eccentricity:     
0009900     
Arg of perigee:   278
9703  deg
Mean anomaly:      81
0340  deg
Mean motion:   15
73646041  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1675
Checksum:              295


Coasting Arc #11 (Orbit 1690)
---------------------------------------

Vector Time (GMT): 2010/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3446803
51                 A    =         6723056
50  meter
 Y    =       -3181503
05  meter          E    =           
0006032
 Z    =       -4819871
07                 I    =           51
96620
 XDOT =       2710
750470                 Wp   =           14
18954
 YDOT =       6751
384789  meter/sec      RA   =           83
79930  deg
 ZDOT =      -2512
878117                 TA   =          231
29606
                                          MA   =          231
35002
                                          Ha   =            189
204  n
mi
                                          Hp   =            187
437

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11308410
46                 X    =         3505537
60
 Y    =      -10438002
14  feet           Y    =        -3142630
29  meter
 Z    =      -15813225
28                 Z    =        -4802983
88
 XDOT =       8893
538289                 XDOT =        2647
260944
 YDOT =      22150
212562  feet/sec       YDOT =        6781
343106  meter/sec
 ZDOT =      -8244
350776                 ZDOT =       -2499
863253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1094855
21                 X    =          333711
87
 Y    =      -15419283
77  feet           Y    =        -4699797
69  meter
 Z    =      -15746018
85                 Z    =        -4799386
55
 XDOT =      20602
543948                 XDOT =        6279
655395
 YDOT =       9845
927839  feet/sec       YDOT =        3001
038805  meter/sec
 ZDOT =      -8192
416463                 ZDOT =       -2497
048538


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   10126
52018624  
00016717  00000-0  10270-3 0  9106
2 25544  51
6438  84
4214 0009989 282
9738  77
0309 15
73687067 16919


Satellite: ISS
Catalog Number: 25544
Epoch time:      10126
52018624   =   yrday
fracday
Element set:     910
Inclination:       51
6438  deg
RA of node:        84
4214  deg
Eccentricity:     
0009989     
Arg of perigee:   282
9738  deg
Mean anomaly:      77
0309  deg
Mean motion:   15
73687067  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1691
Checksum:              329


Coasting Arc #12 (Orbit 1706)
---------------------------------------

Vector Time (GMT): 2010/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2935606
36                 A    =         6730765
40  meter
 Y    =       -5613436
16  meter          E    =           
0003988
 Z    =        2269079
38                 I    =           51
98831
 XDOT =       3551
233095                 Wp   =          110
73546
 YDOT =      -4075
095382  meter/sec      RA   =           78
65079  deg
 ZDOT =      -5480
609865                 TA   =           43
92363
                                          MA   =           43
89193
                                          Ha   =            189
469  n
mi
                                          Hp   =            187
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9631254
45                 X    =        -2883640
56
 Y    =      -18416785
30  feet           Y    =        -5645973
35  meter
 Z    =        7444486
15                 Z    =         2254944
24
 XDOT =      11651
027213                 XDOT =        3623
161562
 YDOT =     -13369
735504  feet/sec       YDOT =       -4034
981090  meter/sec
 ZDOT =     -17981
003493                 ZDOT =       -5463
183253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19803328
13                 X    =        -6036054
42
 Y    =       -6372080
81  feet           Y    =        -1942210
23  meter
 Z    =        7388111
95                 Z    =         2251896
52
 XDOT =      -1434
544589                 XDOT =        -437
249191
 YDOT =     -16333
562256  feet/sec       YDOT =       -4978
469776  meter/sec
 ZDOT =     -17911
656954                 ZDOT =       -5459
473040


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   10127
53620943  
00016717  00000-0  10270-3 0  9112
2 25544  51
6441  79
2066 0010029 287
1021  72
9044 15
73721354 17075


Satellite: ISS
Catalog Number: 25544
Epoch time:      10127
53620943   =   yrday
fracday
Element set:     911
Inclination:       51
6441  deg
RA of node:        79
2066  deg
Eccentricity:     
0010029     
Arg of perigee:   287
1021  deg
Mean anomaly:      72
9044  deg
Mean motion:   15
73721354  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1707
Checksum:              281


Coasting Arc #13 (Orbit 1722)
---------------------------------------

Vector Time (GMT): 2010/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2735019
94                 A    =         6723004
92  meter
 Y    =        3887729
03  meter          E    =           
0002928
 Z    =        4756943
37                 I    =           51
95638
 XDOT =      -3954
976250                 Wp   =          266
24015
 YDOT =      -6042
350154  meter/sec      RA   =           73
58146  deg
 ZDOT =       2665
543225                 TA   =          157
68238
                                          MA   =          157
66964
                                          Ha   =            189
668  n
mi
                                          Hp   =            187
044

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8973162
54                 X    =        -2801398
53
 Y    =       12755016
50  feet           Y    =         3856773
19  meter
 Z    =       15606769
60                 Z    =         4743495
35
 XDOT =     -12975
643865                 XDOT =       -3900
064499
 YDOT =     -19823
983444  feet/sec       YDOT =       -6086
270066  meter/sec
 ZDOT =       8745
220555                 ZDOT =        2646
463072

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2726450
76                 X    =          831022
19
 Y    =       15409149
29  feet           Y    =         4696708
70  meter
 Z    =       15553261
20                 Z    =         4740634
01
 XDOT =     -22141
065710                 XDOT =       -6748
596829
 YDOT =      -4828
631578  feet/sec       YDOT =       -1471
766905  meter/sec
 ZDOT =       8669
152811                 ZDOT =        2642
357777


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   10128
55220872  
00016717  00000-0  10270-3 0  9123
2 25544  51
6447  73
9917 0010147 290
1099  69
8972 15
73789911 17233


Satellite: ISS
Catalog Number: 25544
Epoch time:      10128
55220872   =   yrday
fracday
Element set:     912
Inclination:       51
6447  deg
RA of node:        73
9917  deg
Eccentricity:     
0010147     
Arg of perigee:   290
1099  deg
Mean anomaly:      69
8972  deg
Mean motion:   15
73789911  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1723
Checksum:              330


Coasting Arc #14 (Orbit 1737)
---------------------------------------

Vector Time (GMT): 2010/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3941173
40                 A    =         6730394
50  meter
 Y    =        4898661
05  meter          E    =           
0009692
 Z    =       -2383516
28                 I    =           51
97109
 XDOT =      -2666
146307                 Wp   =          327
58379
 YDOT =       4782
413266  meter/sec      RA   =           68
42912  deg
 ZDOT =       5418
348160                 TA   =            5
67097
                                          MA   =            5
66001
                                          Ha   =            189
988  n
mi
                                          Hp   =            186
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12930358
94                 X    =         3897681
61
 Y    =       16071722
60  feet           Y    =         4942490
46  meter
 Z    =       -7819935
32                 Z    =        -2364475
39
 XDOT =      -8747
199169                 XDOT =       -2745
747650
 YDOT =      15690
332238  feet/sec       YDOT =        4752
153672  meter/sec
 ZDOT =      17776
732807                 ZDOT =        5405
202575

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20587773
97                 X    =         6275153
51
 Y    =        1679033
05  feet           Y    =          511769
27  meter
 Z    =       -7744046
04                 Z    =        -2360385
23
 XDOT =       5386
918112                 XDOT =        1641
932640
 YDOT =      15727
816714  feet/sec       YDOT =        4793
838534  meter/sec
 ZDOT =      17724
434249                 ZDOT =        5402
407559


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   10129
50469051  
00016717  00000-0  10270-3 0  9134
2 25544  51
6445  69
1019 0010161 294
6928  65
3177 15
73774083 17385


Satellite: ISS
Catalog Number: 25544
Epoch time:      10129
50469051   =   yrday
fracday
Element set:     913
Inclination:       51
6445  deg
RA of node:        69
1019  deg
Eccentricity:     
0010161     
Arg of perigee:   294
6928  deg
Mean anomaly:      65
3177  deg
Mean motion:   15
73774083  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1738
Checksum:              313


Coasting Arc #15 (Orbit 1753)
---------------------------------------

Vector Time (GMT): 2010/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 793683
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1910367
59                 A    =         6723064
22  meter
 Y    =       -4410438
86  meter          E    =           
0008626
 Z    =       -4705961
09                 I    =           51
93592
 XDOT =       5010
264163                 Wp   =           10
66879
 YDOT =       5139
874747  meter/sec      RA   =           63
35905  deg
 ZDOT =      -2775
721138                 TA   =          232
02709
                                          MA   =          232
10505
                                          Ha   =            190
042  n
mi
                                          Hp   =            186
581

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6267610
19                 X    =         1982405
02
 Y    =      -14469943
76  feet           Y    =        -4388673
10  meter
 Z    =      -15439504
89                 Z    =        -4696505
49
 XDOT =      16437
874552                 XDOT =        4965
900960
 YDOT =      16863
106124  feet/sec       YDOT =        5195
654520  meter/sec
 ZDOT =      -9106
696648                 ZDOT =       -2751
488507

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6349103
18                 X    =        -1935206
65
 Y    =      -14474500
23  feet           Y    =        -4411827
67  meter
 Z    =      -15401891
21                 Z    =        -4694496
44
 XDOT =      22519
665420                 XDOT =        6863
994020
 YDOT =       -264
423885  feet/sec       YDOT =         -80
596400  meter/sec
 ZDOT =      -9010
137400                 ZDOT =       -2746
289880


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   10130
52064823  
00016717  00000-0  10270-3 0  9147
2 25544  51
6455  63
8864 0010100 298
6836  61
3311 15
73837647 17540


Satellite: ISS
Catalog Number: 25544
Epoch time:      10130
52064823   =   yrday
fracday
Element set:     914
Inclination:       51
6455  deg
RA of node:        63
8864  deg
Eccentricity:     
0010100     
Arg of perigee:   298
6836  deg
Mean anomaly:      61
3311  deg
Mean motion:   15
73837647  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1754
Checksum:              301

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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