Date: April 26th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 3750)
---------------------------------------

Vector Time (GMT): 2009/114/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5629482
42                 A    =         6735883
68  meter
 Y    =        3404204
77  meter          E    =           
0006467
 Z    =        1427029
39                 I    =           51
43950
 XDOT =      -1463
913825                 Wp   =          147
02518
 YDOT =       4852
262562  meter/sec      RA   =          221
11923  deg
 ZDOT =      -5793
216211                 TA   =           17
24516
                                          MA   =           17
22320
                                          Ha   =            191
008  n
mi
                                          Hp   =            189
974

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18469430
51                 X    =         5584065
22
 Y    =       11168650
81  feet           Y    =         3466903
00  meter
 Z    =        4681854
95                 Z    =         1454267
67
 XDOT =      -4802
866881                 XDOT =       -1489
920810
 YDOT =      15919
496596  feet/sec       YDOT =        4835
746754  meter/sec
 ZDOT =     -19006
614867                 ZDOT =       -5800
391284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21428650
91                 X    =         6531452
80
 Y    =       -2379339
94  feet           Y    =         -725222
81  meter
 Z    =        4788533
34                 Z    =         1459544
96
 XDOT =       5804
088239                 XDOT =        1769
086095
 YDOT =      13920
100105  feet/sec       YDOT =        4242
846512  meter/sec
 ZDOT =     -19034
275348                 ZDOT =       -5801
647126


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   09114
55026191  
00010596  00000-0  82463-4 0  9004
2 25544  51
6414 221
9132 0008853 278
7812  81
2347 15
72373648 37519


Satellite: ISS
Catalog Number: 25544
Epoch time:      09114
55026191   =   yrday
fracday
Element set:     900
Inclination:       51
6414  deg
RA of node:       221
9132  deg
Eccentricity:     
0008853     
Arg of perigee:   278
7812  deg
Mean anomaly:      81
2347  deg
Mean motion:   15
72373648  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3751
Checksum:              303


Coasting Arc #2 (Orbit 3766)
---------------------------------------

Vector Time (GMT): 2009/115/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         326171
18                 A    =         6726184
82  meter
 Y    =       -4596388
91  meter          E    =           
0003540
 Z    =        4903100
29                 I    =           51
43100
 XDOT =       6823
888313                 Wp   =          246
31618
 YDOT =       2810
481533  meter/sec      RA   =          216
01229  deg
 ZDOT =       2180
565575                 TA   =          182
43416
                                          MA   =          182
43588
                                          Ha   =            191
134  n
mi
                                          Hp   =            189
684

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1070115
40                 X    =          353725
57
 Y    =      -15080016
12  feet           Y    =        -4592587
51  meter
 Z    =       16086287
03                 Z    =         4904751
71
 XDOT =      22388
085016                 XDOT =        6781
360814
 YDOT =       9220
739937  feet/sec       YDOT =        2886
552407  meter/sec
 ZDOT =       7154
086532                 ZDOT =        2213
613580

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8627374
42                 X    =        -2629623
72
 Y    =      -12406613
11  feet           Y    =        -3781535
68  meter
 Z    =       16092390
29                 Z    =         4904960
56
 XDOT =      22321
329067                 XDOT =        6803
541100
 YDOT =      -6074
047718  feet/sec       YDOT =       -1851
369745  meter/sec
 ZDOT =       7283
425170                 ZDOT =        2219
987992


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   09115
56712812  
00010596  00000-0  82463-4 0  9019
2 25544  51
6419 216
7031 0008925 283
4604  76
5564 15
72437930 37676


Satellite: ISS
Catalog Number: 25544
Epoch time:      09115
56712812   =   yrday
fracday
Element set:     901
Inclination:       51
6419  deg
RA of node:       216
7031  deg
Eccentricity:     
0008925     
Arg of perigee:   283
4604  deg
Mean anomaly:      76
5564  deg
Mean motion:   15
72437930  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3767
Checksum:              315


Coasting Arc #3 (Orbit 3781)
---------------------------------------

Vector Time (GMT): 2009/116/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6126466
38                 A    =         6734212
38  meter
 Y    =       -1463830
85  meter          E    =           
0008069
 Z    =       -2366567
98                 I    =           51
48220
 XDOT =       -776
803386                 Wp   =          326
10885
 YDOT =      -5452
096429  meter/sec      RA   =          210
83824  deg
 ZDOT =       5381
120283                 TA   =            7
17866
                                          MA   =            7
16711
                                          Ha   =            191
419  n
mi
                                          Hp   =            189
424

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20099955
33                 X    =        -6098145
62
 Y    =       -4802594
65  feet           Y    =        -1532182
10  meter
 Z    =       -7764330
65                 Z    =        -2396262
32
 XDOT =      -2548
567539                 XDOT =        -741
920507
 YDOT =     -17887
455475  feet/sec       YDOT =       -5460
588328  meter/sec
 ZDOT =      17654
594103                 ZDOT =        5377
430943

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18528510
70                 X    =        -5647490
06
 Y    =        9052644
35  feet           Y    =         2759246
00  meter
 Z    =       -7880474
06                 Z    =        -2401968
49
 XDOT =     -12764
323425                 XDOT =       -3890
565780
 YDOT =     -10763
483316  feet/sec       YDOT =       -3280
709715  meter/sec
 ZDOT =      17639
767616                 ZDOT =        5376
601169


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   09116
52042837  
00010596  00000-0  82463-4 0  9020
2 25544  51
6415 211
8200 0009053 288
4615  71
5563 15
72405079 37826


Satellite: ISS
Catalog Number: 25544
Epoch time:      09116
52042837   =   yrday
fracday
Element set:     902
Inclination:       51
6415  deg
RA of node:       211
8200  deg
Eccentricity:     
0009053     
Arg of perigee:   288
4615  deg
Mean anomaly:      71
5563  deg
Mean motion:   15
72405079  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3782
Checksum:              296


Coasting Arc #4 (Orbit 3797)
---------------------------------------

Vector Time (GMT): 2009/117/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1679954
46                 A    =         6728014
14  meter
 Y    =        4751858
45  meter          E    =           
0006743
 Z    =       -4461089
74                 I    =           51
48647
 XDOT =      -6977
291045                 Wp   =            5
87660
 YDOT =       -540
483305  meter/sec      RA   =          205
74857  deg
 ZDOT =      -3197
043185                 TA   =          232
01611
                                          MA   =          232
07703
                                          Ha   =            191
639  n
mi
                                          Hp   =            189
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5511661
63                 X    =         1648365
11
 Y    =       15590086
78  feet           Y    =         4770468
40  meter
 Z    =      -14636121
20                 Z    =        -4453004
74
 XDOT =     -22891
374819                 XDOT =       -6955
197743
 YDOT =      -1773
239189  feet/sec       YDOT =        -618
383668  meter/sec
 ZDOT =     -10488
986826                 ZDOT =       -3230
885892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14379180
33                 X    =         4382774
16
 Y    =        8222083
18  feet           Y    =         2506090
95  meter
 Z    =      -14604170
11                 Z    =        -4451351
05
 XDOT =     -17914
234365                 XDOT =       -5460
258635
 YDOT =      12427
573420  feet/sec       YDOT =        3787
924378  meter/sec
 ZDOT =     -10621
286946                 ZDOT =       -3237
368261


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   09117
53726647  
00010596  00000-0  82463-4 0  9031
2 25544  51
6404 206
6108 0008965 291
9574  68
0635 15
72443961 37987


Satellite: ISS
Catalog Number: 25544
Epoch time:      09117
53726647   =   yrday
fracday
Element set:     903
Inclination:       51
6404  deg
RA of node:       206
6108  deg
Eccentricity:     
0008965     
Arg of perigee:   291
9574  deg
Mean anomaly:      68
0635  deg
Mean motion:   15
72443961  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3798
Checksum:              338


Coasting Arc #5 (Orbit 3813)
---------------------------------------

Vector Time (GMT): 2009/118/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5905194
72                 A    =         6731937
60  meter
 Y    =        -495016
02  meter          E    =           
0005976
 Z    =        3193825
47                 I    =           51
52755
 XDOT =       3032
136903                 Wp   =           54
88430
 YDOT =       5203
298099  meter/sec      RA   =          200
56703  deg
 ZDOT =      -4790
090107                 TA   =           87
81505
                                          MA   =           87
74663
                                          Ha   =            191
798  n
mi
                                          Hp   =            188
703

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19373998
43                 X    =         5894775
95
 Y    =       -1624068
30  feet           Y    =         -429039
23  meter
 Z    =       10478430
02                 Z    =         3222487
94
 XDOT =       9947
955718                 XDOT =        2996
997096
 YDOT =      17071
187990  feet/sec       YDOT =        5237
009182  meter/sec
 ZDOT =     -15715
518723                 ZDOT =       -4775
444668

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13393938
32                 X    =         4082472
40
 Y    =      -14008291
87  feet           Y    =        -4269727
36  meter
 Z    =       10590424
15                 Z    =         3227961
28
 XDOT =      17806
302396                 XDOT =        5427
360970
 YDOT =       5164
076509  feet/sec       YDOT =        1574
010520  meter/sec
 ZDOT =     -15657
888923                 ZDOT =       -4772
524544


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   09118
55408886  
00010596  00000-0  82463-4 0  9047
2 25544  51
6403 201
4008 0008971 297
2810  62
7439 15
72496953 38148


Satellite: ISS
Catalog Number: 25544
Epoch time:      09118
55408886   =   yrday
fracday
Element set:     904
Inclination:       51
6403  deg
RA of node:       201
4008  deg
Eccentricity:     
0008971     
Arg of perigee:   297
2810  deg
Mean anomaly:      62
7439  deg
Mean motion:   15
72496953  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3814
Checksum:              325


Coasting Arc #6 (Orbit 3829)
---------------------------------------

Vector Time (GMT): 2009/119/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3558765
98                 A    =         6729919
08  meter
 Y    =       -4184985
52  meter          E    =           
0004440
 Z    =        3882366
57                 I    =           51
54838
 XDOT =       6332
373847                 Wp   =           51
18492
 YDOT =      -1603
638743  meter/sec      RA   =          195
48634  deg
 ZDOT =       4075
540899                 TA   =          356
28809
                                          MA   =          356
29138
                                          Ha   =            192
002  n
mi
                                          Hp   =            188
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11675741
40                 X    =        -3530564
25
 Y    =      -13730267
46  feet           Y    =        -4224624
39  meter
 Z    =       12737423
13                 Z    =         3865146
07
 XDOT =      20775
504749                 XDOT =        6330
036978
 YDOT =      -5261
281965  feet/sec       YDOT =       -1532
839884  meter/sec
 ZDOT =      13371
197176                 ZDOT =        4106
297983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17937011
67                 X    =        -5467201
16
 Y    =       -2196602
35  feet           Y    =         -669524
40  meter
 Z    =       12669794
00                 Z    =         3861753
21
 XDOT =      11556
808029                 XDOT =        3522
515087
 YDOT =     -16546
655611  feet/sec       YDOT =       -5043
420630  meter/sec
 ZDOT =      13491
313408                 ZDOT =        4112
152327


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   09119
57089600  
00010596  00000-0  82463-4 0  9050
2 25544  51
6398 196
1902 0008995 300
8522  59
1755 15
72518064 38308


Satellite: ISS
Catalog Number: 25544
Epoch time:      09119
57089600   =   yrday
fracday
Element set:     905
Inclination:       51
6398  deg
RA of node:       196
1902  deg
Eccentricity:     
0008995     
Arg of perigee:   300
8522  deg
Mean anomaly:      59
1755  deg
Mean motion:   15
72518064  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3830
Checksum:              328


Coasting Arc #7 (Orbit 3844)
---------------------------------------

Vector Time (GMT): 2009/120/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5007046
61                 A    =         6729600
13  meter
 Y    =        2233473
70  meter          E    =           
0003270
 Z    =       -3899270
98                 I    =           51
57593
 XDOT =      -5026
255014                 Wp   =          347
22266
 YDOT =      -4186
418957  meter/sec      RA   =          190
30557  deg
 ZDOT =       4058
741671                 TA   =          325
06372
                                          MA   =          325
08518
                                          Ha   =            192
033  n
mi
                                          Hp   =            188
158

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16427318
26                 X    =        -5012707
54
 Y    =        7327669
61  feet           Y    =         2177450
63  meter
 Z    =      -12792883
81                 Z    =        -3923608
86
 XDOT =     -16490
337972                 XDOT =       -4998
784897
 YDOT =     -13734
970332  feet/sec       YDOT =       -4242
472194  meter/sec
 ZDOT =      13316
081599                 ZDOT =        4034
390455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6832808
79                 X    =        -2082640
12
 Y    =       16565774
73  feet           Y    =         5049248
14  meter
 Z    =      -12887871
62                 Z    =        -3928223
27
 XDOT =     -20265
078306                 XDOT =       -6176
795868
 YDOT =       1920
412661  feet/sec       YDOT =         585
341779  meter/sec
 ZDOT =      13220
562160                 ZDOT =        4029
627346


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   09120
52414070  
00010596  00000-0  82463-4 0  9061
2 25544  51
6389 191
3060 0008903 305
6327  54
4006 15
72550325 38454


Satellite: ISS
Catalog Number: 25544
Epoch time:      09120
52414070   =   yrday
fracday
Element set:     906
Inclination:       51
6389  deg
RA of node:       191
3060  deg
Eccentricity:     
0008903     
Arg of perigee:   305
6327  deg
Mean anomaly:      54
4006  deg
Mean motion:   15
72550325  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3845
Checksum:              285


Coasting Arc #8 (Orbit 3860)
---------------------------------------

Vector Time (GMT): 2009/121/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5107218
74                 A    =         6731974
31  meter
 Y    =        3008779
47  meter          E    =           
0005431
 Z    =       -3194642
27                 I    =           51
61313
 XDOT =      -4986
199892                 Wp   =          334
72804
 YDOT =       3360
839909  meter/sec      RA   =          185
22850  deg
 ZDOT =      -4798
227483                 TA   =          242
51992
                                          MA   =          242
57514
                                          Ha   =            192
366  n
mi
                                          Hp   =            188
030

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16755967
00                 X    =         5088713
48
 Y    =        9871323
72  feet           Y    =         3065788
07  meter
 Z    =      -10481109
82                 Z    =        -3169876
18
 XDOT =     -16358
923530                 XDOT =       -5000
101853
 YDOT =      11026
377653  feet/sec       YDOT =        3305
003844  meter/sec
 ZDOT =     -15742
216153                 ZDOT =       -4822
484037

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18918484
32                 X    =         5766354
02
 Y    =       -4724587
84  feet           Y    =        -1440054
37  meter
 Z    =      -10384042
86                 Z    =        -3165056
26
 XDOT =      -4240
904752                 XDOT =       -1292
627769
 YDOT =      17882
487010  feet/sec       YDOT =        5450
582041  meter/sec
 ZDOT =     -15836
811301                 ZDOT =       -4827
060085


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   09121
54092074  
00010596  00000-0  82463-4 0  9071
2 25544  51
6391 186
0953 0008936 310
2786  49
7594 15
72545370 38617


Satellite: ISS
Catalog Number: 25544
Epoch time:      09121
54092074   =   yrday
fracday
Element set:     907
Inclination:       51
6391  deg
RA of node:       186
0953  deg
Eccentricity:     
0008936     
Arg of perigee:   310
2786  deg
Mean anomaly:      49
7594  deg
Mean motion:   15
72545370  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3861
Checksum:              328


Coasting Arc #9 (Orbit 3876)
---------------------------------------

Vector Time (GMT): 2009/122/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3609292
62                 A    =         6727473
50  meter
 Y    =       -3523930
55  meter          E    =           
0009920
 Z    =        4455015
57                 I    =           51
62873
 XDOT =       6498
190137                 Wp   =           10
55266
 YDOT =       2561
701180  meter/sec      RA   =          180
05455  deg
 ZDOT =      -3227
578527                 TA   =          111
84580
                                          MA   =          111
74026
                                          Ha   =            192
465  n
mi
                                          Hp   =            187
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11841511
21                 X    =         3626787
88
 Y    =      -11561451
92  feet           Y    =        -3483471
64  meter
 Z    =       14616192
81                 Z    =         4472591
92
 XDOT =      21319
521446                 XDOT =        6484
740805
 YDOT =       8404
531430  feet/sec       YDOT =        2634
292630  meter/sec
 ZDOT =     -10589
168397                 ZDOT =       -3196
042891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          17197
60                 X    =            5241
83
 Y    =      -16488848
44  feet           Y    =        -5025801
00  meter
 Z    =       14684659
75                 Z    =         4475884
29
 XDOT =      19790
813904                 XDOT =        6032
240078
 YDOT =      -9331
009960  feet/sec       YDOT =       -2844
091836  meter/sec
 ZDOT =     -10465
651015                 ZDOT =       -3189
930429


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   09122
55768432  
00010596  00000-0  82463-4 0  9082
2 25544  51
6395 180
8848 0009139 314
2089  45
8322 15
72600269 38774


Satellite: ISS
Catalog Number: 25544
Epoch time:      09122
55768432   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:       180
8848  deg
Eccentricity:     
0009139     
Arg of perigee:   314
2089  deg
Mean anomaly:      45
8322  deg
Mean motion:   15
72600269  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3877
Checksum:              336


Coasting Arc #10 (Orbit 3892)
---------------------------------------

Vector Time (GMT): 2009/123/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6115054
11                 A    =         6733776
36  meter
 Y    =       -1389647
79  meter          E    =           
0013128
 Z    =        2429198
16                 I    =           51
67866
 XDOT =       3163
212075                 Wp   =           35
73256
 YDOT =      -4534
544493  meter/sec      RA   =          174
97493  deg
 ZDOT =       5364
719041                 TA   =          351
68141
                                          MA   =          351
70316
                                          Ha   =            192
851  n
mi
                                          Hp   =            187
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20062513
47                 X    =        -6110860
99
 Y    =       -4559211
92  feet           Y    =        -1458006
48  meter
 Z    =        7969810
24                 Z    =         2399501
29
 XDOT =      10377
992372                 XDOT =        3187
622088
 YDOT =     -14877
114478  feet/sec       YDOT =       -4499
035181  meter/sec
 ZDOT =      17600
784255                 ZDOT =        5380
145225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17167479
11                 X    =        -5232647
63
 Y    =       11419630
01  feet           Y    =         3480703
23  meter
 Z    =        7853562
70                 Z    =         2393765
91
 XDOT =      -2856
087142                 XDOT =        -870
535361
 YDOT =     -16448
655651  feet/sec       YDOT =       -5013
550242  meter/sec
 ZDOT =      17660
769663                 ZDOT =        5383
002593


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   09123
57443761  
00010596  00000-0  82463-4 0  9091
2 25544  51
6391 175
6738 0008993 320
1548  39
8953 15
72565152 38935


Satellite: ISS
Catalog Number: 25544
Epoch time:      09123
57443761   =   yrday
fracday
Element set:     909
Inclination:       51
6391  deg
RA of node:       175
6738  deg
Eccentricity:     
0008993     
Arg of perigee:   320
1548  deg
Mean anomaly:      39
8953  deg
Mean motion:   15
72565152  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3893
Checksum:              346


Coasting Arc #11 (Orbit 3907)
---------------------------------------

Vector Time (GMT): 2009/124/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1854032
71                 A    =         6725801
76  meter
 Y    =        4248957
84  meter          E    =           
0007423
 Z    =       -4877097
08                 I    =           51
68255
 XDOT =      -7318
299756                 Wp   =           59
88961
 YDOT =       -543
583842  meter/sec      RA   =          169
81393  deg
 ZDOT =       2314
749251                 TA   =          232
62152
                                          MA   =          232
68913
                                          Ha   =            192
880  n
mi
                                          Hp   =            187
047

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6082784
47                 X    =        -1877715
22
 Y    =       13940150
40  feet           Y    =         4228092
56  meter
 Z    =      -16000974
68                 Z    =        -4886161
56
 XDOT =     -24010
169802                 XDOT =       -7322
922121
 YDOT =      -1783
411556  feet/sec       YDOT =        -625
447192  meter/sec
 ZDOT =       7594
321688                 ZDOT =        2279
185430

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6204624
30                 X    =         1891169
49
 Y    =       13845765
93  feet           Y    =         4220189
46  meter
 Z    =      -16036104
69                 Z    =        -4887804
71
 XDOT =     -16586
859580                 XDOT =       -5055
674800
 YDOT =      16043
782729  feet/sec       YDOT =        4890
144976  meter/sec
 ZDOT =       7455
184222                 ZDOT =        2272
340151


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   09124
52762788  
00010596  00000-0  82463-4 0  9102
2 25544  51
6399 170
7889 0009100 323
2757  36
7781 15
72596648 39089


Satellite: ISS
Catalog Number: 25544
Epoch time:      09124
52762788   =   yrday
fracday
Element set:     910
Inclination:       51
6399  deg
RA of node:       170
7889  deg
Eccentricity:     
0009100     
Arg of perigee:   323
2757  deg
Mean anomaly:      36
7781  deg
Mean motion:   15
72596648  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3908
Checksum:              351


Coasting Arc #12 (Orbit 3923)
---------------------------------------

Vector Time (GMT): 2009/125/12:22:31
864
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6521706
96                 A    =         6734952
73  meter
 Y    =        -455043
06  meter          E    =           
0001220
 Z    =       -1621902
27                 I    =           51
74256
 XDOT =      -1081
515219                 Wp   =            3
09710
 YDOT =       4994
759090  meter/sec      RA   =          164
72718  deg
 ZDOT =      -5749
141056                 TA   =          194
76017
                                          MA   =          194
76373
                                          Ha   =            192
998  n
mi
                                          Hp   =            186
837

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21396676
37                 X    =         6534189
63
 Y    =       -1492923
42  feet           Y    =         -382043
72  meter
 Z    =       -5321201
66                 Z    =        -1590189
07
 XDOT =      -3548
278277                 XDOT =       -1109
358413
 YDOT =      16387
004888  feet/sec       YDOT =        4982
509311  meter/sec
 ZDOT =     -18862
011337                 ZDOT =       -5754
462728

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13116339
67                 X    =         3997860
33
 Y    =      -17009191
27  feet           Y    =        -5184401
50  meter
 Z    =       -5197192
81                 Z    =        -1584104
37
 XDOT =       8725
076188                 XDOT =        2659
403222
 YDOT =      12498
779800  feet/sec       YDOT =        3809
628083  meter/sec
 ZDOT =     -18882
450124                 ZDOT =       -5755
370798


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   09125
54435123  
00010596  00000-0  82463-4 0  9116
2 25544  51
6399 165
5780 0009043 327
7312  32
3296 15
72641036 39246


Satellite: ISS
Catalog Number: 25544
Epoch time:      09125
54435123   =   yrday
fracday
Element set:     911
Inclination:       51
6399  deg
RA of node:       165
5780  deg
Eccentricity:     
0009043     
Arg of perigee:   327
7312  deg
Mean anomaly:      32
3296  deg
Mean motion:   15
72641036  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3924
Checksum:              302

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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