Date: June 24th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 678)
---------------------------------------

Vector Time (GMT): 2009/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -357740
72                 A    =         6731258
21  meter
 Y    =       -6506111
97  meter          E    =           
0010045
 Z    =       -1698748
36                 I    =           51
33059
 XDOT =       4878
589949                 Wp   =           92
70969
 YDOT =      -1745
320832  meter/sec      RA   =          278
89523  deg
 ZDOT =       5685
593949                 TA   =          248
43908
                                          MA   =          248
54617
                                          Ha   =            192
950  n
mi
                                          Hp   =            181
673

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1173690
03                 X    =         -276709
48
 Y    =      -21345511
70  feet           Y    =        -6509658
96  meter
 Z    =       -5573321
40                 Z    =        -1700290
98
 XDOT =      16005
872535                 XDOT =        4870
124257
 YDOT =      -5726
118216  feet/sec       YDOT =       -1690
814269  meter/sec
 ZDOT =      18653
523455                 ZDOT =        5709
273165

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21344842
72                 X    =        -6505908
06
 Y    =        1155627
03  feet           Y    =          352235
12  meter
 Z    =       -5579654
55                 Z    =        -1700678
71
 XDOT =      -5652
170115                 XDOT =       -1722
781451
 YDOT =     -14336
958080  feet/sec       YDOT =       -4369
904823  meter/sec
 ZDOT =      18746
249583                 ZDOT =        5713
856873


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   09173
50332302  
00010596  00000-0  82463-4 0  9008
2 25544  51
6432 279
6143 0008466 141
1119 219
0654 15
73877565  6790


Satellite: ISS
Catalog Number: 25544
Epoch time:      09173
50332302   =   yrday
fracday
Element set:     900
Inclination:       51
6432  deg
RA of node:       279
6143  deg
Eccentricity:     
0008466     
Arg of perigee:   141
1119  deg
Mean anomaly:     219
0654  deg
Mean motion:   15
73877565  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             679
Checksum:              308


Coasting Arc #2 (Orbit 694)
---------------------------------------

Vector Time (GMT): 2009/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4121055
84                 A    =         6721596
64  meter
 Y    =        1888372
67  meter          E    =           
0017862
 Z    =       -4976909
81                 I    =           51
29475
 XDOT =      -1061
381373                 Wp   =          102
02022
 YDOT =      -7367
708991  meter/sec      RA   =          273
76920  deg
 ZDOT =      -1926
141442                 TA   =          149
30803
                                          MA   =          149
20343
                                          Ha   =            192
788  n
mi
                                          Hp   =            181
659

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13520524
42                 X    =        -4117688
92
 Y    =        6195448
39  feet           Y    =         1842308
58  meter
 Z    =      -16328444
26                 Z    =        -4996921
14
 XDOT =      -3482
222351                 XDOT =        -969
558742
 YDOT =     -24172
273592  feet/sec       YDOT =       -7379
064129  meter/sec
 ZDOT =      -6319
361687                 ZDOT =       -1931
076246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6434101
52                 X    =         1961114
14
 Y    =       13312612
49  feet           Y    =         4057684
29  meter
 Z    =      -16406795
53                 Z    =        -5000791
28
 XDOT =     -23136
179389                 XDOT =       -7051
907478
 YDOT =       3407
743328  feet/sec       YDOT =        1038
680166  meter/sec
 ZDOT =      -6339
038249                 ZDOT =       -1932
138858


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   09174
51921234  
00010596  00000-0  82463-4 0  9019
2 25544  51
6430 274
3986 0008463 145
7570 214
4141 15
73906760  6951


Satellite: ISS
Catalog Number: 25544
Epoch time:      09174
51921234   =   yrday
fracday
Element set:     901
Inclination:       51
6430  deg
RA of node:       274
3986  deg
Eccentricity:     
0008463     
Arg of perigee:   145
7570  deg
Mean anomaly:     214
4141  deg
Mean motion:   15
73906760  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             695
Checksum:              310


Coasting Arc #3 (Orbit 710)
---------------------------------------

Vector Time (GMT): 2009/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1499374
69                 A    =         6731149
41  meter
 Y    =        6331208
28  meter          E    =           
0021803
 Z    =        1676624
94                 I    =           51
32560
 XDOT =      -4500
250649                 Wp   =          127
98889
 YDOT =       2585
210077  meter/sec      RA   =          268
57983  deg
 ZDOT =      -5700
699039                 TA   =           33
37049
                                          MA   =           33
23325
                                          Ha   =            192
726  n
mi
                                          Hp   =            181
815

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4919208
31                 X    =         1420321
98
 Y    =       20771680
71  feet           Y    =         6347532
81  meter
 Z    =        5500738
00                 Z    =         1683718
10
 XDOT =     -14764
601868                 XDOT =       -4501
131836
 YDOT =       8481
660356  feet/sec       YDOT =        2534
881892  meter/sec
 ZDOT =     -18703
080835                 ZDOT =       -5722
562587

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20587620
70                 X    =         6275106
79
 Y    =       -5612596
70  feet           Y    =        -1710719
48  meter
 Z    =        5528840
77                 Z    =         1685190
67
 XDOT =       8580
775357                 XDOT =        2615
420329
 YDOT =      12848
022740  feet/sec       YDOT =        3916
077331  meter/sec
 ZDOT =     -18788
665023                 ZDOT =       -5726
785099


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   09175
53508682  
00010596  00000-0  82463-4 0  9021
2 25544  51
6422 269
1831 0008546 148
5228 211
6448 15
73929388  7115


Satellite: ISS
Catalog Number: 25544
Epoch time:      09175
53508682   =   yrday
fracday
Element set:     902
Inclination:       51
6422  deg
RA of node:       269
1831  deg
Eccentricity:     
0008546     
Arg of perigee:   148
5228  deg
Mean anomaly:     211
6448  deg
Mean motion:   15
73929388  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             711
Checksum:              326


Coasting Arc #4 (Orbit 726)
---------------------------------------

Vector Time (GMT): 2009/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3704467
48                 A    =         6721359
06  meter
 Y    =       -2602927
72  meter          E    =           
0013752
 Z    =        4963416
22                 I    =           51
29537
 XDOT =       2367
612162                 Wp   =          141
10723
 YDOT =       7073
436905  meter/sec      RA   =          263
45261  deg
 ZDOT =       1928
931516                 TA   =          290
10616
                                          MA   =          290
25410
                                          Ha   =            192
443  n
mi
                                          Hp   =            181
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12153764
71                 X    =         3709187
52
 Y    =       -8539789
11  feet           Y    =        -2561476
68  meter
 Z    =       16284173
95                 Z    =         4981423
26
 XDOT =       7767
756437                 XDOT =        2278
969565
 YDOT =      23206
813992  feet/sec       YDOT =        7099
416961  meter/sec
 ZDOT =       6328
515471                 ZDOT =        1940
219142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9157956
52                 X    =        -2791345
15
 Y    =      -11596286
90  feet           Y    =        -3534548
25  meter
 Z    =       16354640
88                 Z    =         4984894
54
 XDOT =      21925
643479                 XDOT =        6682
936132
 YDOT =      -8265
141834  feet/sec       YDOT =       -2519
215231  meter/sec
 ZDOT =       6373
112563                 ZDOT =        1942
524709


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   09176
55094344  
00010596  00000-0  82463-4 0  9030
2 25544  51
6423 263
9664 0008372 152
6816 207
4789 15
73996935  7278


Satellite: ISS
Catalog Number: 25544
Epoch time:      09176
55094344   =   yrday
fracday
Element set:     903
Inclination:       51
6423  deg
RA of node:       263
9664  deg
Eccentricity:     
0008372     
Arg of perigee:   152
6816  deg
Mean anomaly:     207
4789  deg
Mean motion:   15
73996935  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             727
Checksum:              348


Coasting Arc #5 (Orbit 741)
---------------------------------------

Vector Time (GMT): 2009/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2609412
59                 A    =         6731044
63  meter
 Y    =       -5977706
89  meter          E    =           
0008187
 Z    =       -1673049
28                 I    =           51
33167
 XDOT =       3965
390992                 Wp   =           98
88361
 YDOT =      -3318
679657  meter/sec      RA   =          258
26278  deg
 ZDOT =       5695
232935                 TA   =          242
56069
                                          MA   =          242
64398
                                          Ha   =            192
433  n
mi
                                          Hp   =            182
125

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8561064
93                 X    =        -2534247
66
 Y    =      -19611899
25  feet           Y    =        -6006466
35  meter
 Z    =       -5489006
82                 Z    =        -1685543
94
 XDOT =      13009
812967                 XDOT =        3974
540288
 YDOT =     -10888
056619  feet/sec       YDOT =       -3274
286025  meter/sec
 ZDOT =      18685
147423                 ZDOT =        5714
518273

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18972561
39                 X    =        -5782836
71
 Y    =        9869995
26  feet           Y    =         3008374
55  meter
 Z    =       -5538296
55                 Z    =        -1688072
79
 XDOT =     -11037
365355                 XDOT =       -3364
188960
 YDOT =     -10730
569439  feet/sec       YDOT =       -3270
677565  meter/sec
 ZDOT =      18760
589460                 ZDOT =        5718
227667


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   09177
50329778  
00010596  00000-0  82463-4 0  9049
2 25544  51
6416 259
0765 0008117 155
5925 204
5624 15
73959243  7422


Satellite: ISS
Catalog Number: 25544
Epoch time:      09177
50329778   =   yrday
fracday
Element set:     904
Inclination:       51
6416  deg
RA of node:       259
0765  deg
Eccentricity:     
0008117     
Arg of perigee:   155
5925  deg
Mean anomaly:     204
5624  deg
Mean motion:   15
73959243  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             742
Checksum:              331


Coasting Arc #6 (Orbit 757)
---------------------------------------

Vector Time (GMT): 2009/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3222576
01                 A    =         6721292
47  meter
 Y    =        3157993
75  meter          E    =           
0016275
 Z    =       -4993958
86                 I    =           51
30531
 XDOT =      -3551
423754                 Wp   =          106
03189
 YDOT =      -6561
050464  meter/sec      RA   =          253
13528  deg
 ZDOT =      -1866
718228                 TA   =          145
90120
                                          MA   =          145
79653
                                          Ha   =            192
278  n
mi
                                          Hp   =            182
132

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10572755
93                 X    =        -3233390
23
 Y    =       10360871
89  feet           Y    =         3121897
20  meter
 Z    =      -16384379
46                 Z    =        -5009639
83
 XDOT =     -11651
652737                 XDOT =       -3468
724939
 YDOT =     -21525
756117  feet/sec       YDOT =       -6600
301927  meter/sec
 ZDOT =      -6124
403634                 ZDOT =       -1883
770842

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11228749
28                 X    =         3422522
78
 Y    =        9541120
54  feet           Y    =         2908133
54  meter
 Z    =      -16445696
49                 Z    =        -5012648
29
 XDOT =     -19743
671766                 XDOT =       -6017
871154
 YDOT =      12617
018546  feet/sec       YDOT =        3845
667253  meter/sec
 ZDOT =      -6191
606264                 ZDOT =       -1887
201589


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   09178
51912734  
00010596  00000-0  82463-4 0  9052
2 25544  51
6406 253
8596 0008189 159
7073 200
4417 15
73993255  7587


Satellite: ISS
Catalog Number: 25544
Epoch time:      09178
51912734   =   yrday
fracday
Element set:     905
Inclination:       51
6406  deg
RA of node:       253
8596  deg
Eccentricity:     
0008189     
Arg of perigee:   159
7073  deg
Mean anomaly:     200
4417  deg
Mean motion:   15
73993255  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             758
Checksum:              339


Coasting Arc #7 (Orbit 773)
---------------------------------------

Vector Time (GMT): 2009/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3587364
08                 A    =         6730910
88  meter
 Y    =        5451606
68  meter          E    =           
0020581
 Z    =        1597923
95                 I    =           51
34823
 XDOT =      -3365
167562                 Wp   =          132
98988
 YDOT =       3904
291393  meter/sec      RA   =          247
94658  deg
 ZDOT =      -5732
773621                 TA   =           29
27998
                                          MA   =           29
16479
                                          Ha   =            192
084  n
mi
                                          Hp   =            182
265

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11769567
18                 X    =         3518374
29
 Y    =       17885848
68  feet           Y    =         5491336
74  meter
 Z    =        5242532
66                 Z    =         1615184
35
 XDOT =     -11040
575992                 XDOT =       -3380
727300
 YDOT =      12809
354965  feet/sec       YDOT =        3866
573818  meter/sec
 ZDOT =     -18808
312406                 ZDOT =       -5749
158828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16572224
83                 X    =         5051214
13
 Y    =      -13530350
55  feet           Y    =        -4124050
85  meter
 Z    =        5310501
04                 Z    =         1618640
72
 XDOT =      12886
851490                 XDOT =        3927
912334
 YDOT =       8335
480660  feet/sec       YDOT =        2540
654505  meter/sec
 ZDOT =     -18872
349808                 ZDOT =       -5752
292222


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   09179
53494207  
00010596  00000-0  82463-4 0  9066
2 25544  51
6407 248
6427 0008062 162
1216 198
0232 15
74046642  7745


Satellite: ISS
Catalog Number: 25544
Epoch time:      09179
53494207   =   yrday
fracday
Element set:     906
Inclination:       51
6407  deg
RA of node:       248
6427  deg
Eccentricity:     
0008062     
Arg of perigee:   162
1216  deg
Mean anomaly:     198
0232  deg
Mean motion:   15
74046642  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             774
Checksum:              311


Coasting Arc #8 (Orbit 789)
---------------------------------------

Vector Time (GMT): 2009/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2637156
88                 A    =         6721001
95  meter
 Y    =       -3628983
43  meter          E    =           
0012696
 Z    =        5002277
82                 I    =           51
32740
 XDOT =       4641
283548                 Wp   =          149
96936
 YDOT =       5877
335805  meter/sec      RA   =          242
81918  deg
 ZDOT =       1804
143085                 TA   =          282
50298
                                          MA   =          282
64499
                                          Ha   =            191
932  n
mi
                                          Hp   =            182
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8652089
49                 X    =         2653240
67
 Y    =      -11906113
62  feet           Y    =        -3599403
89  meter
 Z    =       16411672
65                 Z    =         5015127
72
 XDOT =      15227
308229                 XDOT =        4566
453046
 YDOT =      19282
597784  feet/sec       YDOT =        5928
818729  meter/sec
 ZDOT =       5919
104611                 ZDOT =        1826
509367

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12852208
75                 X    =        -3917353
23
 Y    =       -7055848
57  feet           Y    =        -2150622
64  meter
 Z    =       16461862
73                 Z    =         5017575
76
 XDOT =      16791
866943                 XDOT =        5118
161044
 YDOT =     -16473
393936  feet/sec       YDOT =       -5021
090472  meter/sec
 ZDOT =       6007
123772                 ZDOT =        1830
971326


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   09180
55074150  
00010596  00000-0  82463-4 0  9072
2 25544  51
6407 243
4255 0008033 166
7341 193
4035 15
74073720  7909


Satellite: ISS
Catalog Number: 25544
Epoch time:      09180
55074150   =   yrday
fracday
Element set:     907
Inclination:       51
6407  deg
RA of node:       243
4255  deg
Eccentricity:     
0008033     
Arg of perigee:   166
7341  deg
Mean anomaly:     193
4035  deg
Mean motion:   15
74073720  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             790
Checksum:              291


Coasting Arc #9 (Orbit 804)
---------------------------------------

Vector Time (GMT): 2009/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4483632
55                 A    =         6730953
21  meter
 Y    =       -4782596
70  meter          E    =           
0006483
 Z    =       -1535273
46                 I    =           51
37503
 XDOT =       2680
346664                 Wp   =          101
00044
 YDOT =      -4352
253540  meter/sec      RA   =          237
63270  deg
 ZDOT =       5749
497060                 TA   =          242
02967
                                          MA   =          242
09530
                                          Ha   =            191
872  n
mi
                                          Hp   =            182
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14710080
55                 X    =        -4422361
42
 Y    =      -15690934
07  feet           Y    =        -4832392
51  meter
 Z    =       -5036986
41                 Z    =        -1556906
80
 XDOT =       8793
788268                 XDOT =        2700
885041
 YDOT =     -14279
047048  feet/sec       YDOT =       -4322
166278  meter/sec
 ZDOT =      18863
179330                 ZDOT =        5762
567502

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13517542
87                 X    =        -4120147
07
 Y    =       16703396
55  feet           Y    =         5091195
27  meter
 Z    =       -5122078
88                 Z    =        -1561209
64
 XDOT =     -14121
450142                 XDOT =       -4304
218003
 YDOT =      -5647
152520  feet/sec       YDOT =       -1721
252088  meter/sec
 ZDOT =      18914
196347                 ZDOT =        5765
047046


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   09181
50304217  
00010596  00000-0  82463-4 0  9089
2 25544  51
6401 238
5344 0007828 169
5143 190
6185 15
74054369  8059


Satellite: ISS
Catalog Number: 25544
Epoch time:      09181
50304217   =   yrday
fracday
Element set:     908
Inclination:       51
6401  deg
RA of node:       238
5344  deg
Eccentricity:     
0007828     
Arg of perigee:   169
5143  deg
Mean anomaly:     190
6185  deg
Mean motion:   15
74054369  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             805
Checksum:              308


Coasting Arc #10 (Orbit 820)
---------------------------------------

Vector Time (GMT): 2009/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2058958
75                 A    =         6720829
27  meter
 Y    =        3945439
94  meter          E    =           
0014963
 Z    =       -5047194
30                 I    =           51
35830
 XDOT =      -5561
124980                 Wp   =          109
02122
 YDOT =      -5041
038226  meter/sec      RA   =          232
50529  deg
 ZDOT =      -1680
875392                 TA   =          144
78106
                                          MA   =          144
68208
                                          Ha   =            191
728  n
mi
                                          Hp   =            182
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6755114
01                 X    =        -2078405
87
 Y    =       12944356
77  feet           Y    =         3922307
50  meter
 Z    =      -16559036
42                 Z    =        -5057243
39
 XDOT =     -18245
160697                 XDOT =       -5496
176505
 YDOT =     -16538
839323  feet/sec       YDOT =       -5102
862576  meter/sec
 ZDOT =      -5514
683045                 ZDOT =       -1707
734430

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13819113
47                 X    =         4212065
79
 Y    =        4573891
28  feet           Y    =         1394122
06  meter
 Z    =      -16598230
21                 Z    =        -5059140
57
 XDOT =     -13185
354944                 XDOT =       -4018
896187
 YDOT =      19546
681345  feet/sec       YDOT =        5957
828474  meter/sec
 ZDOT =      -5620
289681                 ZDOT =       -1713
064295


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   09182
51881553  
00010596  00000-0  82463-4 0  9095
2 25544  51
6404 233
3168 0007895 172
9350 187
1926 15
74082893  8216


Satellite: ISS
Catalog Number: 25544
Epoch time:      09182
51881553   =   yrday
fracday
Element set:     909
Inclination:       51
6404  deg
RA of node:       233
3168  deg
Eccentricity:     
0007895     
Arg of perigee:   172
9350  deg
Mean anomaly:     187
1926  deg
Mean motion:   15
74082893  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             821
Checksum:              331


Coasting Arc #11 (Orbit 836)
---------------------------------------

Vector Time (GMT): 2009/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5214346
35                 A    =         6730869
29  meter
 Y    =        3996399
91  meter          E    =           
0019342
 Z    =        1409295
39                 I    =           51
41206
 XDOT =      -1998
066481                 Wp   =          138
75474
 YDOT =       4664
330612  meter/sec      RA   =          227
32335  deg
 ZDOT =      -5803
312312                 TA   =           25
68011
                                          MA   =           25
58419
                                          Ha   =            191
466  n
mi
                                          Hp   =            182
771

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17107435
53                 X    =         5162424
26
 Y    =       13111548
25  feet           Y    =         4054419
22  meter
 Z    =        4623672
55                 Z    =         1434501
33
 XDOT =      -6555
336225                 XDOT =       -2021
883803
 YDOT =      15302
921954  feet/sec       YDOT =        4641
854886  meter/sec
 ZDOT =     -19039
738556                 ZDOT =       -5813
076003

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9981607
33                 X    =         3042393
91
 Y    =      -19079270
38  feet           Y    =        -5815361
61  meter
 Z    =        4722748
44                 Z    =         1439493
73
 XDOT =      14791
093451                 XDOT =        4508
325284
 YDOT =       2991
354078  feet/sec       YDOT =         911
764723  meter/sec
 ZDOT =     -19077
777140                 ZDOT =       -5814
906472


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   09183
53457366  
00010596  00000-0  82463-4 0  9101
2 25544  51
6405 228
0997 0007705 176
1115 184
0109 15
74144949  8370


Satellite: ISS
Catalog Number: 25544
Epoch time:      09183
53457366   =   yrday
fracday
Element set:     910
Inclination:       51
6405  deg
RA of node:       228
0997  deg
Eccentricity:     
0007705     
Arg of perigee:   176
1115  deg
Mean anomaly:     184
0109  deg
Mean motion:   15
74144949  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             837
Checksum:              321


Coasting Arc #12 (Orbit 852)
---------------------------------------

Vector Time (GMT): 2009/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1428421
34                 A    =         6720505
49  meter
 Y    =       -4170403
36  meter          E    =           
0011383
 Z    =        5071667
58                 I    =           51
39738
 XDOT =       6346
229435                 Wp   =          159
04111
 YDOT =       4078
414600  meter/sec      RA   =          222
19721  deg
 ZDOT =       1554
705703                 TA   =          275
92553
                                          MA   =          276
05526
                                          Ha   =            191
417  n
mi
                                          Hp   =            182
899

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4686421
72                 X    =         1450312
08
 Y    =      -13682425
72  feet           Y    =        -4154308
47  meter
 Z    =       16639329
32                 Z    =         5078659
25
 XDOT =      20820
962713                 XDOT =        6292
599759
 YDOT =      13380
625327  feet/sec       YDOT =        4149
081697  meter/sec
 ZDOT =       5100
740495                 ZDOT =        1585
406212

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14302499
45                 X    =        -4359401
83
 Y    =       -1924586
15  feet           Y    =         -586613
86  meter
 Z    =       16666525
73                 Z    =         5079957
04
 XDOT =       9075
435127                 XDOT =        2766
192627
 YDOT =     -21899
969212  feet/sec       YDOT =       -6675
110616  meter/sec
 ZDOT =       5221
383907                 ZDOT =        1591
477815


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   09184
55031877  
00010596  00000-0  82463-4 0  9110
2 25544  51
6396 222
8826 0007737 179
3325 180
7850 15
74152485  8533


Satellite: ISS
Catalog Number: 25544
Epoch time:      09184
55031877   =   yrday
fracday
Element set:     911
Inclination:       51
6396  deg
RA of node:       222
8826  deg
Eccentricity:     
0007737     
Arg of perigee:   179
3325  deg
Mean anomaly:     180
7850  deg
Mean motion:   15
74152485  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             853
Checksum:              333


Coasting Arc #13 (Orbit 867)
---------------------------------------

Vector Time (GMT): 2009/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5829941
10                 A    =         6730898
25  meter
 Y    =       -3109832
78  meter          E    =           
0005033
 Z    =       -1289293
40                 I    =           51
45611
 XDOT =       1297
605018                 Wp   =           97
14115
 YDOT =      -4843
987438  meter/sec      RA   =          217
01967  deg
 ZDOT =       5835
229128                 TA   =          248
68522
                                          MA   =          248
73896
                                          Ha   =            191
270  n
mi
                                          Hp   =            183
023

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19127103
35                 X    =        -5788469
99
 Y    =      -10202863
45  feet           Y    =        -3174794
46  meter
 Z    =       -4229965
21                 Z    =        -1317515
07
 XDOT =       4257
234310                 XDOT =        1323
328456
 YDOT =     -15892
347239  feet/sec       YDOT =       -4829
334188  meter/sec
 ZDOT =      19144
452520                 ZDOT =        5841
594402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6057136
49                 X    =        -1846215
20
 Y    =       20791951
74  feet           Y    =         6337386
89  meter
 Z    =       -4340846
84                 Z    =        -1323090
12
 XDOT =     -14888
726158                 XDOT =       -4538
083733
 YDOT =       -347
930381  feet/sec       YDOT =        -106
049180  meter/sec
 ZDOT =      19169
157075                 ZDOT =        5842
759076


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   09185
50256731  
00010596  00000-0  82463-4 0  9125
2 25544  51
6400 217
9912 0007679 182
9280 177
1839 15
74178616  8682


Satellite: ISS
Catalog Number: 25544
Epoch time:      09185
50256731   =   yrday
fracday
Element set:     912
Inclination:       51
6400  deg
RA of node:       217
9912  deg
Eccentricity:     
0007679     
Arg of perigee:   182
9280  deg
Mean anomaly:     177
1839  deg
Mean motion:   15
74178616  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             868
Checksum:              337


Coasting Arc #14 (Orbit 883)
---------------------------------------

Vector Time (GMT): 2009/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -860355
20                 A    =         6720256
12  meter
 Y    =        4274457
90  meter          E    =           
0013781
 Z    =       -5123766
30                 I    =           51
44464
 XDOT =      -6936
849902                 Wp   =          111
57102
 YDOT =      -3029
882072  meter/sec      RA   =          211
89330  deg
 ZDOT =      -1370
787537                 TA   =          145
30264
                                          MA   =          145
21267
                                          Ha   =            191
122  n
mi
                                          Hp   =            183
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2822687
67                 X    =         -883198
81
 Y    =       14023812
00  feet           Y    =         4264710
21  meter
 Z    =      -16810256
88                 Z    =        -5128000
50
 XDOT =     -22758
693905                 XDOT =       -6895
794689
 YDOT =      -9940
557979  feet/sec       YDOT =       -3107
224156  meter/sec
 ZDOT =      -4497
334438                 ZDOT =       -1404
387432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14278310
66                 X    =         4352029
09
 Y    =        -462455
80  feet           Y    =         -140956
53  meter
 Z    =      -16826633
18                 Z    =        -5128757
79
 XDOT =      -4669
194616                 XDOT =       -1423
170519
 YDOT =      23332
577360  feet/sec       YDOT =        7111
769579  meter/sec
 ZDOT =      -4629
328503                 ZDOT =       -1411
019328


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   09186
51828507  
00010596  00000-0  82463-4 0  9134
2 25544  51
6400 212
7734 0007656 187
0424 173
0633 15
74174657  8844


Satellite: ISS
Catalog Number: 25544
Epoch time:      09186
51828507   =   yrday
fracday
Element set:     913
Inclination:       51
6400  deg
RA of node:       212
7734  deg
Eccentricity:     
0007656     
Arg of perigee:   187
0424  deg
Mean anomaly:     173
0633  deg
Mean motion:   15
74174657  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             884
Checksum:              318


Coasting Arc #15 (Orbit 899)
---------------------------------------

Vector Time (GMT): 2009/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6263942
81                 A    =         6731018
56  meter
 Y    =        2163794
31  meter          E    =           
0018167
 Z    =        1111509
32                 I    =           51
50586
 XDOT =       -648
655464                 Wp   =          145
45354
 YDOT =       4922
936511  meter/sec      RA   =          206
72192  deg
 ZDOT =      -5895
915204                 TA   =           22
34553
                                          MA   =           22
26648
                                          Ha   =            190
932  n
mi
                                          Hp   =            183
325

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20550993
49                 X    =         6233881
89
 Y    =        7099062
69  feet           Y    =         2233673
08  meter
 Z    =        3646684
13                 Z    =         1141866
66
 XDOT =      -2128
134724                 XDOT =        -675
015380
 YDOT =      16151
366505  feet/sec       YDOT =        4915
536644  meter/sec
 ZDOT =     -19343
553820                 ZDOT =       -5899
129396

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1983278
37                 X    =          604503
25
 Y    =      -21631521
88  feet           Y    =        -6593287
87  meter
 Z    =        3765925
83                 Z    =         1147854
19
 XDOT =      14586
986293                 XDOT =        4446
113422
 YDOT =      -2050
121347  feet/sec       YDOT =        -624
876987  meter/sec
 ZDOT =     -19355
890819                 ZDOT =       -5899
675522


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   09187
53398895  
00010596  00000-0  82463-4 0  9140
2 25544  51
6386 207
5555 0007557 189
9194 170
1821 15
74207851  9004


Satellite: ISS
Catalog Number: 25544
Epoch time:      09187
53398895   =   yrday
fracday
Element set:     914
Inclination:       51
6386  deg
RA of node:       207
5555  deg
Eccentricity:     
0007557     
Arg of perigee:   189
9194  deg
Mean anomaly:     170
1821  deg
Mean motion:   15
74207851  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             900
Checksum:              344

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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