Date: January 14th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16414 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


022/09:06:27 407 1 5 3 3 3 3
N/A 2 7 0 0 185 4
000/00:00:54 815 1 1 0 0 179 6

024/09:02:53 473 -4 3 8 2 8 2
N/A -6 7 0 0 187 6
000/00:02:16 945 -1 9 0 0 183 4

Coasting Arc #1 (Orbit 3910)
---------------------------------------

Vector Time (GMT): 2010/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3917700
86                 A    =         6722532
47  meter
 Y    =       -5459891
06  meter          E    =           
0009126
 Z    =         133432
55                 I    =           51
38882
 XDOT =       3831
904096                 Wp   =           80
42879
 YDOT =       2905
063791  meter/sec      RA   =          304
75244  deg
 ZDOT =       6015
907268                 TA   =          281
02701
                                          MA   =          281
12964
                                          Ha   =            186
226  n
mi
                                          Hp   =            178
104

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12853349
29                 X    =         3977814
97
 Y    =      -17913028
42  feet           Y    =        -5415744
92  meter
 Z    =         437770
82                 Z    =          152609
72
 XDOT =      12571
863832                 XDOT =        3769
910695
 YDOT =       9531
049184  feet/sec       YDOT =        2947
567013  meter/sec
 ZDOT =      19737
228568                 ZDOT =        6034
372125

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21430617
29                 X    =         6532052
15
 Y    =        5171233
89  feet           Y    =         1576192
09  meter
 Z    =         513615
74                 Z    =          156550
08
 XDOT =      -3770
882327                 XDOT =       -1149
364933
 YDOT =      13563
183534  feet/sec       YDOT =        4134
058341  meter/sec
 ZDOT =      19810
387018                 ZDOT =        6038
205963


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   10013
56305587  
00016717  00000-0  10270-3 0  9001
2 25544  51
6441 305
0416 0007146 181
5663 178
5481 15
77390747 39118


Satellite: ISS
Catalog Number: 25544
Epoch time:      10013
56305587   =   yrday
fracday
Element set:     900
Inclination:       51
6441  deg
RA of node:       305
0416  deg
Eccentricity:     
0007146     
Arg of perigee:   181
5663  deg
Mean anomaly:     178
5481  deg
Mean motion:   15
77390747  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3911
Checksum:              303


Coasting Arc #2 (Orbit 3925)
---------------------------------------

Vector Time (GMT): 2010/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2730157
62                 A    =         6711107
31  meter
 Y    =       -3439338
37  meter          E    =           
0016284
 Z    =       -5088370
25                 I    =           51
33496
 XDOT =       4702
092271                 Wp   =          126
89683
 YDOT =      -5912
240558  meter/sec      RA   =          299
55700  deg
 ZDOT =       1466
904032                 TA   =          157
27017
                                          MA   =          157
19799
                                          Ha   =            186
037  n
mi
                                          Hp   =            178
137

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8957210
05                 X    =        -2666777
57
 Y    =      -11283918
53  feet           Y    =        -3469513
63  meter
 Z    =      -16694128
12                 Z    =        -5101479
53
 XDOT =      15426
811913                 XDOT =        4760
728716
 YDOT =     -19397
114691  feet/sec       YDOT =       -5859
331300  meter/sec
 ZDOT =       4812
677271                 ZDOT =        1489
888047

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6909402
23                 X    =         2105985
80
 Y    =      -12573016
02  feet           Y    =        -3832255
28  meter
 Z    =      -16746097
21                 Z    =        -5104210
43
 XDOT =      22963
347818                 XDOT =        6999
228415
 YDOT =       6060
302655  feet/sec       YDOT =        1847
180249  meter/sec
 ZDOT =       4903
584821                 ZDOT =        1494
612653


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   10014
51333734  
00016717  00000-0  10270-3 0  9013
2 25544  51
6448 300
1371 0007110 185
2970 174
8121 15
77422348 39263


Satellite: ISS
Catalog Number: 25544
Epoch time:      10014
51333734   =   yrday
fracday
Element set:     901
Inclination:       51
6448  deg
RA of node:       300
1371  deg
Eccentricity:     
0007110     
Arg of perigee:   185
2970  deg
Mean anomaly:     174
8121  deg
Mean motion:   15
77422348  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3926
Checksum:              280


Coasting Arc #3 (Orbit 3941)
---------------------------------------

Vector Time (GMT): 2010/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4201136
96                 A    =         6719848
46  meter
 Y    =        4670296
05  meter          E    =           
0011234
 Z    =       -2370606
94                 I    =           51
35153
 XDOT =      -2473
865057                 Wp   =          164
83678
 YDOT =      -4943
691929  meter/sec      RA   =          294
40833  deg
 ZDOT =      -5371
772434                 TA   =           42
04048
                                          MA   =           41
95433
                                          Ha   =            185
799  n
mi
                                          Hp   =            178
345

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13783257
73                 X    =        -4241533
09
 Y    =       15322493
59  feet           Y    =         4623090
82  meter
 Z    =       -7777581
83                 Z    =        -2391113
23
 XDOT =      -8116
355173                 XDOT =       -2392
305483
 YDOT =     -16219
461709  feet/sec       YDOT =       -4970
899585  meter/sec
 ZDOT =     -17623
925310                 ZDOT =       -5383
592581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19591738
09                 X    =        -5971561
77
 Y    =       -6297021
29  feet           Y    =        -1919332
09  meter
 Z    =       -7858696
09                 Z    =        -2395330
57
 XDOT =      11084
705966                 XDOT =        3378
618378
 YDOT =     -12500
790037  feet/sec       YDOT =       -3810
240803  meter/sec
 ZDOT =     -17670
826290                 ZDOT =       -5386
067853


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   10015
52695061  
00016717  00000-0  10270-3 0  9020
2 25544  51
6453 294
9060 0007119 189
3342 170
7691 15
77456424 39428


Satellite: ISS
Catalog Number: 25544
Epoch time:      10015
52695061   =   yrday
fracday
Element set:     902
Inclination:       51
6453  deg
RA of node:       294
9060  deg
Eccentricity:     
0007119     
Arg of perigee:   189
3342  deg
Mean anomaly:     170
7691  deg
Mean motion:   15
77456424  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3942
Checksum:              312


Coasting Arc #4 (Orbit 3957)
---------------------------------------

Vector Time (GMT): 2010/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1649083
94                 A    =         6715113
04  meter
 Y    =        5097344
50  meter          E    =           
0009931
 Z    =        4037704
17                 I    =           51
32358
 XDOT =      -4851
814430                 Wp   =          116
73361
 YDOT =       4608
471941  meter/sec      RA   =          289
17829  deg
 ZDOT =      -3833
496307                 TA   =           12
82737
                                          MA   =           12
80212
                                          Ha   =            185
650  n
mi
                                          Hp   =            178
500

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5410380
39                 X    =         1572348
03
 Y    =       16723571
20  feet           Y    =         5115356
15  meter
 Z    =       13247060
93                 Z    =         4045529
26
 XDOT =     -15918
026344                 XDOT =       -4884
364613
 YDOT =      15119
658600  feet/sec       YDOT =        4554
034400  meter/sec
 ZDOT =     -12577
087623                 ZDOT =       -3857
144520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12893849
62                 X    =        -3930045
36
 Y    =       11911083
40  feet           Y    =         3630498
22  meter
 Z    =       13278155
27                 Z    =         4047181
73
 XDOT =     -19536
517165                 XDOT =       -5954
730432
 YDOT =      -7013
259879  feet/sec       YDOT =       -2137
641611  meter/sec
 ZDOT =     -12670
640177                 ZDOT =       -3862
011126


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   10016
54054319  
00016717  00000-0  10270-3 0  9039
2 25544  51
6445 289
6749 0007088 192
9313 167
1671 15
77483318 39584


Satellite: ISS
Catalog Number: 25544
Epoch time:      10016
54054319   =   yrday
fracday
Element set:     903
Inclination:       51
6445  deg
RA of node:       289
6749  deg
Eccentricity:     
0007088     
Arg of perigee:   192
9313  deg
Mean anomaly:     167
1671  deg
Mean motion:   15
77483318  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3958
Checksum:              337


Coasting Arc #5 (Orbit 3973)
---------------------------------------

Vector Time (GMT): 2010/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4218654
72                 A    =         6714577
60  meter
 Y    =       -3173144
91  meter          E    =           
0012323
 Z    =        4149219
47                 I    =           51
31359
 XDOT =       1368
181323                 Wp   =          140
53902
 YDOT =       6636
105407  meter/sec      RA   =          284
04405  deg
 ZDOT =       3668
574923                 TA   =          271
80357
                                          MA   =          271
94471
                                          Ha   =            185
482  n
mi
                                          Hp   =            178
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13840730
70                 X    =         4233668
18
 Y    =      -10410580
41  feet           Y    =        -3125885
73  meter
 Z    =       13612924
77                 Z    =         4169749
46
 XDOT =       4488
783867                 XDOT =        1276
052699
 YDOT =      21771
999366  feet/sec       YDOT =        6650
889872  meter/sec
 ZDOT =      12036
006965                 ZDOT =        3674
998026

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15393196
31                 X    =         4691846
24
 Y    =        7795982
42  feet           Y    =         2376215
44  meter
 Z    =       13694155
58                 Z    =         4173978
62
 XDOT =     -17056
148791                 XDOT =       -5198
714151
 YDOT =      12402
471543  feet/sec       YDOT =        3780
273326  meter/sec
 ZDOT =      12061
594556                 ZDOT =        3676
374021


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   10017
55411406  
00016717  00000-0  10270-3 0  9046
2 25544  51
6447 284
4428 0007053 197
1716 162
9211 15
77518224 39745


Satellite: ISS
Catalog Number: 25544
Epoch time:      10017
55411406   =   yrday
fracday
Element set:     904
Inclination:       51
6447  deg
RA of node:       284
4428  deg
Eccentricity:     
0007053     
Arg of perigee:   197
1716  deg
Mean anomaly:     162
9211  deg
Mean motion:   15
77518224  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3974
Checksum:              305


Coasting Arc #6 (Orbit 3988)
---------------------------------------

Vector Time (GMT): 2010/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -787134
23                 A    =         6719948
28  meter
 Y    =       -6309505
93  meter          E    =           
0002542
 Z    =       -2179576
34                 I    =           51
32628
 XDOT =       4815
193903                 Wp   =          141
65882
 YDOT =      -2489
264014  meter/sec      RA   =          278
81308  deg
 ZDOT =       5468
475832                 TA   =          193
80036
                                          MA   =          193
80731
                                          Ha   =            185
303  n
mi
                                          Hp   =            178
738

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2582461
39                 X    =         -705933
97
 Y    =      -20700478
77  feet           Y    =        -6317854
02  meter
 Z    =       -7150841
00                 Z    =        -2183203
20
 XDOT =      15797
880258                 XDOT =        4816
107152
 YDOT =      -8166
876685  feet/sec       YDOT =       -2435
412802  meter/sec
 ZDOT =      17941
193673                 ZDOT =        5491
869623

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17287611
17                 X    =         5269263
88
 Y    =      -11666601
18  feet           Y    =        -3555980
04  meter
 Z    =       -7165359
19                 Z    =        -2184001
48
 XDOT =      13552
825224                 XDOT =        4130
901128
 YDOT =       9009
586359  feet/sec       YDOT =        2746
121922  meter/sec
 ZDOT =      18033
778907                 ZDOT =        5496
695811


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   10018
50431743  
00016717  00000-0  10270-3 0  9059
2 25544  51
6449 279
5376 0007068 201
4416 158
6454 15
77569963 39899


Satellite: ISS
Catalog Number: 25544
Epoch time:      10018
50431743   =   yrday
fracday
Element set:     905
Inclination:       51
6449  deg
RA of node:       279
5376  deg
Eccentricity:     
0007068     
Arg of perigee:   201
4416  deg
Mean anomaly:     158
6454  deg
Mean motion:   15
77569963  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3989
Checksum:              342


Coasting Arc #7 (Orbit 4004)
---------------------------------------

Vector Time (GMT): 2010/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4194784
64                 A    =         6710287
11  meter
 Y    =        1050876
78  meter          E    =           
0011830
 Z    =       -5139902
35                 I    =           51
29057
 XDOT =       -463
051826                 Wp   =          109
83001
 YDOT =      -7594
227151  meter/sec      RA   =          273
65644  deg
 ZDOT =      -1180
928231                 TA   =          148
86939
                                          MA   =          148
79926
                                          Ha   =            184
994  n
mi
                                          Hp   =            178
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13762416
79                 X    =        -4181255
74
 Y    =        3447758
46  feet           Y    =         1004044
01  meter
 Z    =      -16863196
70                 Z    =        -5160247
32
 XDOT =      -1519
198903                 XDOT =        -372
360799
 YDOT =     -24915
443410  feet/sec       YDOT =       -7598
898155  meter/sec
 ZDOT =      -3874
436454                 ZDOT =       -1182
957639

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9458801
19                 X    =        -2883042
60
 Y    =      -10445056
97  feet           Y    =        -3183653
36  meter
 Z    =      -16943742
86                 Z    =        -5164452
82
 XDOT =      20534
317254                 XDOT =        6258
859899
 YDOT =     -12329
643285  feet/sec       YDOT =       -3758
075273  meter/sec
 ZDOT =      -3882
672225                 ZDOT =       -1183
438494


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   10019
51784752  
00016717  00000-0  10270-3 0  9063
2 25544  51
6449 274
3053 0006987 206
0184 154
0631 15
77609546 40055


Satellite: ISS
Catalog Number: 25544
Epoch time:      10019
51784752   =   yrday
fracday
Element set:     906
Inclination:       51
6449  deg
RA of node:       274
3053  deg
Eccentricity:     
0006987     
Arg of perigee:   206
0184  deg
Mean anomaly:     154
0631  deg
Mean motion:   15
77609546  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4005
Checksum:              312


Coasting Arc #8 (Orbit 4020)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          38663
85                 A    =         6721999
13  meter
 Y    =        6709680
07  meter          E    =           
0015583
 Z    =        -176809
05                 I    =           51
32894
 XDOT =      -4821
213500                 Wp   =          162
47883
 YDOT =       -126
793740  meter/sec      RA   =          268
46143  deg
 ZDOT =      -6017
665450                 TA   =           19
45465
                                          MA   =           19
39525
                                          Ha   =            184
979  n
mi
                                          Hp   =            179
134

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         126849
91                 X    =          -35508
96
 Y    =       22013386
05  feet           Y    =         6709697
71  meter
 Z    =        -580082
19                 Z    =         -176801
23
 XDOT =     -15817
629594                 XDOT =       -4790
205087
 YDOT =       -415
989960  feet/sec       YDOT =        -180
533889  meter/sec
 ZDOT =     -19742
996884                 ZDOT =       -6041
011213

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19192395
71                 X    =        -5849842
21
 Y    =       10782274
96  feet           Y    =         3286437
41  meter
 Z    =        -579866
56                 Z    =         -176743
33
 XDOT =      -6458
869349                 XDOT =       -1968
663378
 YDOT =     -12536
718677  feet/sec       YDOT =       -3821
191853  meter/sec
 ZDOT =     -19835
459863                 ZDOT =       -6045
848166


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10020
53135824  
00016717  00000-0  10270-3 0  9078
2 25544  51
6447 269
0730 0007176 209
7428 150
3330 15
77580270 40213


Satellite: ISS
Catalog Number: 25544
Epoch time:      10020
53135824   =   yrday
fracday
Element set:     907
Inclination:       51
6447  deg
RA of node:       269
0730  deg
Eccentricity:     
0007176     
Arg of perigee:   209
7428  deg
Mean anomaly:     150
3330  deg
Mean motion:   15
77580270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4021
Checksum:              285


Coasting Arc #9 (Orbit 4036)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4227747
49                 A    =         6710415
05  meter
 Y    =        1271522
06  meter          E    =           
0002864
 Z    =        5053048
33                 I    =           51
29296
 XDOT =       -383
053874                 Wp   =          182
31898
 YDOT =       7534
589038  meter/sec      RA   =          263
25921  deg
 ZDOT =      -1578
330405                 TA   =          282
87828
                                          MA   =          282
91027
                                          Ha   =            184
479  n
mi
                                          Hp   =            179
252

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13870562
62                 X    =         4188668
40
 Y    =        4171660
31  feet           Y    =         1318580
62  meter
 Z    =       16578242
55                 Z    =         5073491
58
 XDOT =      -1256
738433                 XDOT =        -459
611361
 YDOT =      24719
780309  feet/sec       YDOT =        7529
877484  meter/sec
 ZDOT =      -5178
249360                 ZDOT =       -1580
377040

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3267009
40                 X    =          995784
46
 Y    =       14015333
92  feet           Y    =         4271873
78  meter
 Z    =       16659245
11                 Z    =         5077737
91
 XDOT =     -21004
153551                 XDOT =       -6402
066002
 YDOT =      11049
506306  feet/sec       YDOT =        3367
889522  meter/sec
 ZDOT =      -5186
139568                 ZDOT =       -1580
735340


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10021
54484496  
00016717  00000-0  10270-3 0  9083
2 25544  51
6446 263
8401 0007026 215
7002 144
3694 15
77690871 40370


Satellite: ISS
Catalog Number: 25544
Epoch time:      10021
54484496   =   yrday
fracday
Element set:     908
Inclination:       51
6446  deg
RA of node:       263
8401  deg
Eccentricity:     
0007026     
Arg of perigee:   215
7002  deg
Mean anomaly:     144
3694  deg
Mean motion:   15
77690871  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4037
Checksum:              307


Coasting Arc #10 (Orbit 4050)
---------------------------------------

Vector Time (GMT): 2010/022/09:06:54
815
Vector Time (MET): N/A
Weight (LBS)     : 751525
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3200370
32                 A    =         6713443
01  meter
 Y    =       -3479050
26  meter          E    =           
0009115
 Z    =        4766432
11                 I    =           51
29969
 XDOT =       3328
272637                 Wp   =          151
84310
 YDOT =       6488
222460  meter/sec      RA   =          258
72803  deg
 ZDOT =       2491
191066                 TA   =          273
63326
                                          MA   =          273
73750
                                          Ha   =            185
415  n
mi
                                          Hp   =            179
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10499902
62                 X    =         3215881
57
 Y    =      -11414206
88  feet           Y    =        -3443175
23  meter
 Z    =       15637900
62                 Z    =         4782016
93
 XDOT =      10919
529650                 XDOT =        3243
371183
 YDOT =      21286
819095  feet/sec       YDOT =        6524
966394  meter/sec
 ZDOT =       8173
199037                 ZDOT =        2507
153625

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8905864
81                 X    =         2714507
59
 Y    =       12620875
90  feet           Y    =         3846842
98  meter
 Z    =       15699524
61                 Z    =         4785215
10
 XDOT =     -22207
811748                 XDOT =       -6768
941021
 YDOT =       5384
919602  feet/sec       YDOT =        1641
323495  meter/sec
 ZDOT =       8236
611333                 ZDOT =        2510
519134


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10022
43165763  
00016717  00000-0  10270-3 0  9096
2 25544  51
6430 259
2610 0004809 204
0026 156
0916 15
77073549 40517


Satellite: ISS
Catalog Number: 25544
Epoch time:      10022
43165763   =   yrday
fracday
Element set:     909
Inclination:       51
6430  deg
RA of node:       259
2610  deg
Eccentricity:     
0004809     
Arg of perigee:   204
0026  deg
Mean anomaly:     156
0916  deg
Mean motion:   15
77073549  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4051
Checksum:              287


Coasting Arc #11 (Orbit 4065)
---------------------------------------

Vector Time (GMT): 2010/023/09:06:54
815
Vector Time (MET): N/A
Weight (LBS)     : 751525
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2773347
63                 A    =         6722770
09  meter
 Y    =       -6004754
24  meter          E    =           
0004658
 Z    =       -1194085
64                 I    =           51
33873
 XDOT =       3996
684502                 Wp   =           46
52813
 YDOT =      -3007
114059  meter/sec      RA   =          253
51418  deg
 ZDOT =       5856
860737                 TA   =          300
32074
                                          MA   =          300
36681
                                          Ha   =            185
300  n
mi
                                          Hp   =            179
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9098909
55                 X    =        -2700194
68
 Y    =      -19700637
28  feet           Y    =        -6035358
39  meter
 Z    =       -3917603
81                 Z    =        -1207381
03
 XDOT =      13112
481961                 XDOT =        4001
562184
 YDOT =      -9865
859772  feet/sec       YDOT =       -2962
393739  meter/sec
 ZDOT =      19215
422364                 ZDOT =        5876
288206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21109876
79                 X    =         6434290
45
 Y    =       -4986136
59  feet           Y    =        -1519774
43  meter
 Z    =       -3970444
26                 Z    =        -1210191
41
 XDOT =       6726
168565                 XDOT =        2050
136179
 YDOT =      13159
213565  feet/sec       YDOT =        4010
928295  meter/sec
 ZDOT =      19292
281393                 ZDOT =        5880
287368


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10023
38214307  
00016717  00000-0  10270-3 0  9102
2 25544  51
6433 254
3576 0004697 208
6274 151
4633 15
77083466 40667


Satellite: ISS
Catalog Number: 25544
Epoch time:      10023
38214307   =   yrday
fracday
Element set:     910
Inclination:       51
6433  deg
RA of node:       254
3576  deg
Eccentricity:     
0004697     
Arg of perigee:   208
6274  deg
Mean anomaly:     151
4633  deg
Mean motion:   15
77083466  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4066
Checksum:              303


Coasting Arc #12 (Orbit 4081)
---------------------------------------

Vector Time (GMT): 2010/024/09:04:01
945
Vector Time (MET): N/A
Weight (LBS)     : 750815
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3249337
67                 A    =         6716148
86  meter
 Y    =        2909166
28  meter          E    =           
0006163
 Z    =       -5111181
47                 I    =           51
31255
 XDOT =      -3771
451002                 Wp   =          122
53899
 YDOT =      -6576
610117  meter/sec      RA   =          248
36590  deg
 ZDOT =      -1350
076373                 TA   =          134
50633
                                          MA   =          134
45595
                                          Ha   =            187
595  n
mi
                                          Hp   =            183
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10660556
67                 X    =        -3256797
97
 Y    =        9544508
79  feet           Y    =         2872788
85  meter
 Z    =      -16768968
06                 Z    =        -5126984
58
 XDOT =     -12373
526909                 XDOT =       -3691
071504
 YDOT =     -21576
804845  feet/sec       YDOT =       -6618
335208  meter/sec
 ZDOT =      -4429
384427                 ZDOT =       -1368
203102

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7314739
87                 X    =        -2229532
71
 Y    =      -12212262
15  feet           Y    =        -3722297
50  meter
 Z    =      -16831477
66                 Z    =        -5130234
39
 XDOT =      22671
191184                 XDOT =        6910
179073
 YDOT =      -7395
335683  feet/sec       YDOT =       -2254
098316  meter/sec
 ZDOT =      -4501
385848                 ZDOT =       -1372
022406


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10024
39598009  
00016717  00000-0  10270-3 0  9119
2 25544  51
6440 249
1274 0010452 235
9750 124
0422 15
75602551 40820


Satellite: ISS
Catalog Number: 25544
Epoch time:      10024
39598009   =   yrday
fracday
Element set:     911
Inclination:       51
6440  deg
RA of node:       249
1274  deg
Eccentricity:     
0010452     
Arg of perigee:   235
9750  deg
Mean anomaly:     124
0422  deg
Mean motion:   15
75602551  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4082
Checksum:              283


Coasting Arc #13 (Orbit 4097)
---------------------------------------

Vector Time (GMT): 2010/025/09:08:01
945
Vector Time (MET): N/A
Weight (LBS)     : 750815
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2425473
39                 A    =         6727421
81  meter
 Y    =        6213864
48  meter          E    =           
0013687
 Z    =        -799658
20                 I    =           51
36271
 XDOT =      -4774
940503                 Wp   =          190
89919
 YDOT =       1097
633843  meter/sec      RA   =          243
17875  deg
 ZDOT =      -5950
426522                 TA   =          357
86584
                                          MA   =          357
87168
                                          Ha   =            187
512  n
mi
                                          Hp   =            183
634

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7957589
85                 X    =         2359693
15
 Y    =       20386694
50  feet           Y    =         6240619
83  meter
 Z    =       -2623550
54                 Z    =         -788034
64
 XDOT =     -15665
815300                 XDOT =       -4757
953720
 YDOT =       3601
160903  feet/sec       YDOT =        1044
333084  meter/sec
 ZDOT =     -19522
396727                 ZDOT =       -5973
581628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21398551
36                 X    =        -6522278
45
 Y    =        4613352
77  feet           Y    =         1406149
92  meter
 Z    =       -2577313
04                 Z    =         -785565
01
 XDOT =       -733
495799                 XDOT =        -223
569519
 YDOT =     -14366
074963  feet/sec       YDOT =       -4378
779649  meter/sec
 ZDOT =     -19614
091221                 ZDOT =       -5978
375004


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10025
41078270  
00016717  00000-0  10270-3 0  9127
2 25544  51
6441 243
9041 0010613 239
7090 120
3024 15
75579161 40987


Satellite: ISS
Catalog Number: 25544
Epoch time:      10025
41078270   =   yrday
fracday
Element set:     912
Inclination:       51
6441  deg
RA of node:       243
9041  deg
Eccentricity:     
0010613     
Arg of perigee:   239
7090  deg
Mean anomaly:     120
3024  deg
Mean motion:   15
75579161  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4098
Checksum:              278


Coasting Arc #14 (Orbit 4113)
---------------------------------------

Vector Time (GMT): 2010/026/09:08:01
945
Vector Time (MET): N/A
Weight (LBS)     : 750815
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4352415
60                 A    =         6716086
54  meter
 Y    =        -692819
52  meter          E    =           
0005980
 Z    =        5072310
84                 I    =           51
33992
 XDOT =       2900
244278                 Wp   =          253
40281
 YDOT =       6964
550355  meter/sec      RA   =          237
98975  deg
 ZDOT =      -1540
527207                 TA   =          211
42488
                                          MA   =          211
46062
                                          Ha   =            186
972  n
mi
                                          Hp   =            183
640

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14279578
74                 X    =         4335199
30
 Y    =       -2273029
92  feet           Y    =         -644244
99  meter
 Z    =       16641439
76                 Z    =         5093412
72
 XDOT =       9515
237132                 XDOT =        2829
633398
 YDOT =      22849
574657  feet/sec       YDOT =        6996
587946  meter/sec
 ZDOT =      -5054
223119                 ZDOT =       -1526
608839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         224733
46                 X    =           68498
76
 Y    =       14360838
40  feet           Y    =         4377183
54  meter
 Z    =       16725022
17                 Z    =         5097786
76
 XDOT =     -22930
818834                 XDOT =       -6989
313581
 YDOT =       6168
557062  feet/sec       YDOT =        1880
176193  meter/sec
 ZDOT =      -4998
861382                 ZDOT =       -1523
652949


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10026
42556499  
00016717  00000-0  10270-3 0  9134
2 25544  51
6438 238
6806 0010595 244
9977 115
0087 15
75676918 41141


Satellite: ISS
Catalog Number: 25544
Epoch time:      10026
42556499   =   yrday
fracday
Element set:     913
Inclination:       51
6438  deg
RA of node:       238
6806  deg
Eccentricity:     
0010595     
Arg of perigee:   244
9977  deg
Mean anomaly:     115
0087  deg
Mean motion:   15
75676918  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4114
Checksum:              339


Coasting Arc #15 (Orbit 4129)
---------------------------------------

Vector Time (GMT): 2010/027/09:08:01
945
Vector Time (MET): N/A
Weight (LBS)     : 750815
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2586490
81                 A    =         6725939
71  meter
 Y    =       -5912180
79  meter          E    =           
0003676
 Z    =        1889097
09                 I    =           51
38969
 XDOT =       5246
617128                 Wp   =           60
30615
 YDOT =       -499
358040  meter/sec      RA   =          232
85186  deg
 ZDOT =       5614
321103                 TA   =          320
76579
                                          MA   =          320
79242
                                          Ha   =            186
815  n
mi
                                          Hp   =            183
974

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8485862
23                 X    =        -2529364
24
 Y    =      -19396918
61  feet           Y    =        -5940785
25  meter
 Z    =        6197825
10                 Z    =         1876670
29
 XDOT =      17213
310787                 XDOT =        5224
538257
 YDOT =      -1638
313779  feet/sec       YDOT =        -440
811298  meter/sec
 ZDOT =      18419
688659                 ZDOT =        5639
755012

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20314236
43                 X    =         6191779
26
 Y    =       -6016011
50  feet           Y    =        -1833680
31  meter
 Z    =        6148394
03                 Z    =         1874030
50
 XDOT =       -964
189780                 XDOT =        -293
885045
 YDOT =      15693
753256  feet/sec       YDOT =        4783
455992  meter/sec
 ZDOT =      18520
453083                 ZDOT =        5645
034100


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10027
44033255  
00016717  00000-0  10270-3 0  9148
2 25544  51
6436 233
4562 0010493 249
2561 110
7479 15
75655856 41308


Satellite: ISS
Catalog Number: 25544
Epoch time:      10027
44033255   =   yrday
fracday
Element set:     914
Inclination:       51
6436  deg
RA of node:       233
4562  deg
Eccentricity:     
0010493     
Arg of perigee:   249
2561  deg
Mean anomaly:     110
7479  deg
Mean motion:   15
75655856  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4130
Checksum:              300


Coasting Arc #16 (Orbit 4144)
---------------------------------------

Vector Time (GMT): 2010/028/09:08:01
945
Vector Time (MET): N/A
Weight (LBS)     : 750815
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4837053
57                 A    =         6717755
31  meter
 Y    =         219234
03  meter          E    =           
0006727
 Z    =       -4659768
43                 I    =           51
38160
 XDOT =      -2970
640975                 Wp   =          177
41546
 YDOT =      -6542
268366  meter/sec      RA   =          227
64653  deg
 ZDOT =       2769
388978                 TA   =          120
02460
                                          MA   =          119
95784
                                          Ha   =            186
408  n
mi
                                          Hp   =            183
937

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15869598
34                 X    =        -4816509
85
 Y    =         719271
74  feet           Y    =          165258
55  meter
 Z    =      -15287954
17                 Z    =        -4683216
32
 XDOT =      -9746
197423                 XDOT =       -2910
716238
 YDOT =     -21464
135059  feet/sec       YDOT =       -6575
153042  meter/sec
 ZDOT =       9085
921843                 ZDOT =        2755
102891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         999534
35                 X    =          304658
07
 Y    =      -15764288
46  feet           Y    =        -4804955
12  meter
 Z    =      -15380870
79                 Z    =        -4688089
42
 XDOT =      21251
861939                 XDOT =        6477
567519
 YDOT =      -7482
594918  feet/sec       YDOT =       -2280
694931  meter/sec
 ZDOT =       9029
086634                 ZDOT =        2752
065606


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10028
39165839  
00016717  00000-0  10270-3 0  9158
2 25544  51
6433 228
5587 0010612 253
1695 106
8306 15
75703914 41452


Satellite: ISS
Catalog Number: 25544
Epoch time:      10028
39165839   =   yrday
fracday
Element set:     915
Inclination:       51
6433  deg
RA of node:       228
5587  deg
Eccentricity:     
0010612     
Arg of perigee:   253
1695  deg
Mean anomaly:     106
8306  deg
Mean motion:   15
75703914  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4145
Checksum:              314

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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