Date: November 23rd 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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


326/18:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 187 1
000/00:00:00 000 0 0 0 0 179 1

328/09:45:33 979 -0 5 0 6 0 6
N/A 0 0 -0 0 187 4
000/00:00:07 958 -0 3 -0 0 179 2

328/10:20:30 409 0 8 1 9 1 9
N/A -1 1 0 2 188 5
000/00:27:00 819 1 3 -0 0 179 6

328/10:45:32 231 0 3 0 3 0 3
N/A 0 2 0 0 188 5
000/00:00:04 462 -0 1 -0 0 179 6

Coasting Arc #1 (Orbit 3058)
---------------------------------------

Vector Time (GMT): 2009/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4724883
78                 A    =         6724995
08  meter
 Y    =       -4757783
05  meter          E    =           
0017468
 Z    =         355127
31                 I    =           51
43765
 XDOT =       3644
325720                 Wp   =           32
67631
 YDOT =      -3161
015287  meter/sec      RA   =          222
77891  deg
 ZDOT =       6014
998762                 TA   =          331
20202
                                          MA   =          331
29833
                                          Ha   =            187
226  n
mi
                                          Hp   =            179
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15501587
19                 X    =        -4673055
42
 Y    =      -15609524
43  feet           Y    =        -4810329
73  meter
 Z    =        1165115
86                 Z    =          332298
83
 XDOT =      11956
449214                 XDOT =        3650
181618
 YDOT =     -10370
785061  feet/sec       YDOT =       -3120
230177  meter/sec
 ZDOT =      19734
247907                 ZDOT =        6032
717091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21379471
16                 X    =         6516462
81
 Y    =       -5203549
85  feet           Y    =        -1586041
99  meter
 Z    =        1074818
69                 Z    =          327604
74
 XDOT =       2374
900456                 XDOT =         723
869659
 YDOT =      13938
198198  feet/sec       YDOT =        4248
362811  meter/sec
 ZDOT =      19804
048166                 ZDOT =        6036
273881


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   09324
56276393  
00016717  00000-0  10270-3 0  9006
2 25544  51
6464 223
4136 0006217 357
5893   2
5240 15
76513791 30590


Satellite: ISS
Catalog Number: 25544
Epoch time:      09324
56276393   =   yrday
fracday
Element set:     900
Inclination:       51
6464  deg
RA of node:       223
4136  deg
Eccentricity:     
0006217     
Arg of perigee:   357
5893  deg
Mean anomaly:       2
5240  deg
Mean motion:   15
76513791  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3059
Checksum:              310


Coasting Arc #2 (Orbit 3073)
---------------------------------------

Vector Time (GMT): 2009/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3714272
62                 A    =         6713381
04  meter
 Y    =        2288371
19  meter          E    =           
0014425
 Z    =       -5113929
81                 I    =           51
42226
 XDOT =      -5257
376426                 Wp   =           75
69642
 YDOT =      -5445
617016  meter/sec      RA   =          217
59428  deg
 ZDOT =       1388
435655                 TA   =          207
60851
                                          MA   =          207
68519
                                          Ha   =            187
207  n
mi
                                          Hp   =            179
311

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12185933
78                 X    =        -3714742
63
 Y    =        7507779
50  feet           Y    =         2246833
87  meter
 Z    =      -16777984
94                 Z    =        -5131974
92
 XDOT =     -17248
610322                 XDOT =       -5202
836707
 YDOT =     -17866
197558  feet/sec       YDOT =       -5504
103284  meter/sec
 ZDOT =       4555
235090                 ZDOT =        1363
026917

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -420923
19                 X    =         -128297
39
 Y    =      -14223029
44  feet           Y    =        -4335179
37  meter
 Z    =      -16849117
81                 Z    =        -5135611
11
 XDOT =      23088
350088                 XDOT =        7037
329107
 YDOT =      -5934
293710  feet/sec       YDOT =       -1808
772723  meter/sec
 ZDOT =       4454
709574                 ZDOT =        1357
795478


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   09325
51356871  
00016717  00000-0  10270-3 0  9013
2 25544  51
6466 218
5131 0006184    
6471 359
4701 15
76572533 30745


Satellite: ISS
Catalog Number: 25544
Epoch time:      09325
51356871   =   yrday
fracday
Element set:     901
Inclination:       51
6466  deg
RA of node:       218
5131  deg
Eccentricity:     
0006184     
Arg of perigee:      
6471  deg
Mean anomaly:     359
4701  deg
Mean motion:   15
76572533  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3074
Checksum:              302


Coasting Arc #3 (Orbit 3089)
---------------------------------------

Vector Time (GMT): 2009/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4344756
01                 A    =         6723060
20  meter
 Y    =        4703038
31  meter          E    =           
0004725
 Z    =       -2056242
08                 I    =           51
47939
 XDOT =      -4904
788868                 Wp   =           78
69699
 YDOT =       2111
243698  meter/sec      RA   =          212
45603  deg
 ZDOT =      -5544
611073                 TA   =          124
30826
                                          MA   =          124
26352
                                          Ha   =            187
276  n
mi
                                          Hp   =            179
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14254448
84                 X    =         4301831
87
 Y    =       15429915
72  feet           Y    =         4751384
10  meter
 Z    =       -6746201
04                 Z    =        -2035238
86
 XDOT =     -16091
826995                 XDOT =       -4901
097574
 YDOT =       6926
652552  feet/sec       YDOT =        2056
416552  meter/sec
 ZDOT =     -18190
981211                 ZDOT =       -5568
429696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20439068
92                 X    =        -6229828
21
 Y    =        4962924
34  feet           Y    =         1512699
34  meter
 Z    =       -6663083
58                 Z    =        -2030907
88
 XDOT =       2103
132951                 XDOT =         641
034923
 YDOT =     -15843
544480  feet/sec       YDOT =       -4829
112357  meter/sec
 ZDOT =     -18284
919774                 ZDOT =       -5573
243547


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   09326
52773759  
00016717  00000-0  10270-3 0  9024
2 25544  51
6465 213
2853 0006061   3
3113 356
8091 15
76573281 30906


Satellite: ISS
Catalog Number: 25544
Epoch time:      09326
52773759   =   yrday
fracday
Element set:     902
Inclination:       51
6465  deg
RA of node:       213
2853  deg
Eccentricity:     
0006061     
Arg of perigee:     3
3113  deg
Mean anomaly:     356
8091  deg
Mean motion:   15
76573281  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3090
Checksum:              304


Coasting Arc #4 (Orbit 3093)
---------------------------------------

Vector Time (GMT): 2009/326/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4821365
76                 A    =         6715830
17  meter
 Y    =        1286487
11  meter          E    =           
0010375
 Z    =       -4502309
82                 I    =           51
45938
 XDOT =      -4371
334401                 Wp   =           78
62917
 YDOT =      -5519
880291  meter/sec      RA   =          211
00977  deg
 ZDOT =       3111
914860                 TA   =          222
45004
                                          MA   =          222
53033
                                          Ha   =            187
139  n
mi
                                          Hp   =            179
126

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15818129
12                 X    =        -4813521
47
 Y    =        4220758
23  feet           Y    =         1232615
97  meter
 Z    =      -14771357
67                 Z    =        -4525713
15
 XDOT =     -14341
648298                 XDOT =       -4324
402551
 YDOT =     -18109
843476  feet/sec       YDOT =       -5568
500965  meter/sec
 ZDOT =      10209
694421                 ZDOT =        3090
792220

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16186953
15                 X    =        -4933783
32
 Y    =       -1809459
88  feet           Y    =         -551523
37  meter
 Z    =      -14863694
66                 Z    =        -4530454
13
 XDOT =      -6933
963158                 XDOT =       -2113
471971
 YDOT =     -20934
839105  feet/sec       YDOT =       -6380
938959  meter/sec
 ZDOT =      10126
066642                 ZDOT =        3086
425112


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   09326
78127601  
00016717  00000-0  10270-3 0  9032
2 25544  51
6435 211
9733 0005666   6
8395 353
2846 15
76603458 30948


Satellite: ISS
Catalog Number: 25544
Epoch time:      09326
78127601   =   yrday
fracday
Element set:     903
Inclination:       51
6435  deg
RA of node:       211
9733  deg
Eccentricity:     
0005666     
Arg of perigee:     6
8395  deg
Mean anomaly:     353
2846  deg
Mean motion:   15
76603458  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3094
Checksum:              324


Coasting Arc #5 (Orbit 3109)
---------------------------------------

Vector Time (GMT): 2009/327/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3373075
87                 A    =         6719519
77  meter
 Y    =        4686177
44  meter          E    =           
0008350
 Z    =       -3448064
64                 I    =           51
49851
 XDOT =      -6115
832176                 Wp   =           46
31009
 YDOT =       1054
929038  meter/sec      RA   =          205
89167  deg
 ZDOT =      -4550
273089                 TA   =          174
62094
                                          MA   =          174
61197
                                          Ha   =            187
218  n
mi
                                          Hp   =            179
091

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11066521
87                 X    =         3337173
80
 Y    =       15374597
92  feet           Y    =         4723696
65  meter
 Z    =      -11312548
04                 Z    =        -3431764
94
 XDOT =     -20065
066194                 XDOT =       -6105
069350
 YDOT =       3461
053273  feet/sec       YDOT =         986
598661  meter/sec
 ZDOT =     -14928
717485                 ZDOT =       -4579
957967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5071909
68                 X    =         1545918
07
 Y    =       18291485
54  feet           Y    =         5575244
79  meter
 Z    =      -11247986
47                 Z    =        -3428386
28
 XDOT =     -18596
281662                 XDOT =       -5668
146651
 YDOT =      -4093
351471  feet/sec       YDOT =       -1247
653528  meter/sec
 ZDOT =     -15045
873601                 ZDOT =       -4585
982274


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   09327
79541388  
00016717  00000-0  10270-3 0  9047
2 25544  51
6435 206
7450 0005717  10
3740 349
7541 15
76651705 31106


Satellite: ISS
Catalog Number: 25544
Epoch time:      09327
79541388   =   yrday
fracday
Element set:     904
Inclination:       51
6435  deg
RA of node:       206
7450  deg
Eccentricity:     
0005717     
Arg of perigee:    10
3740  deg
Mean anomaly:     349
7541  deg
Mean motion:   15
76651705  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3110
Checksum:              307


Coasting Arc #6 (Orbit 3119)
---------------------------------------

Vector Time (GMT): 2009/328/09:45:37
958
Vector Time (MET): N/A
Weight (LBS)     : 731746
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2507445
42                 A    =         6717338
76  meter
 Y    =        4639319
97  meter          E    =           
0011950
 Z    =       -4173604
89                 I    =           51
51024
 XDOT =      -6753
840519                 Wp   =           44
68305
 YDOT =        347
554696  meter/sec      RA   =          202
61189  deg
 ZDOT =      -3669
273869                 TA   =          187
77013
                                          MA   =          187
78866
                                          Ha   =            187
350  n
mi
                                          Hp   =            179
239

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8226526
96                 X    =         2475656
26
 Y    =       15220866
05  feet           Y    =         4667182
19  meter
 Z    =      -13692929
42                 Z    =        -4161500
51
 XDOT =     -22158
269420                 XDOT =       -6739
400064
 YDOT =       1140
271313  feet/sec       YDOT =         272
110208  meter/sec
 ZDOT =     -12038
300095                 ZDOT =       -3702
049374

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14664213
36                 X    =        -4469652
23
 Y    =       -9253300
86  feet           Y    =        -2820406
10  meter
 Z    =      -13644929
26                 Z    =        -4158974
44
 XDOT =      18065
228256                 XDOT =        5506
281572
 YDOT =     -10676
720243  feet/sec       YDOT =       -3254
264330  meter/sec
 ZDOT =     -12167
697134                 ZDOT =       -3708
714087


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   09328
42923894  
00016717  00000-0  10270-3 0  9055
2 25544  51
6459 203
4825 0005895   8
4948 351
6316 15
76572109 31200


Satellite: ISS
Catalog Number: 25544
Epoch time:      09328
42923894   =   yrday
fracday
Element set:     905
Inclination:       51
6459  deg
RA of node:       203
4825  deg
Eccentricity:     
0005895     
Arg of perigee:     8
4948  deg
Mean anomaly:     351
6316  deg
Mean motion:   15
76572109  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3120
Checksum:              329


Coasting Arc #7 (Orbit 3120)
---------------------------------------

Vector Time (GMT): 2009/328/10:34:00
819
Vector Time (MET): N/A
Weight (LBS)     : 731742
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1366322
84                 A    =         6716544
39  meter
 Y    =       -4600206
27  meter          E    =           
0008931
 Z    =        4690709
39                 I    =           51
50381
 XDOT =       7189
211731                 Wp   =           65
51459
 YDOT =        632
721729  meter/sec      RA   =          202
43394  deg
 ZDOT =       2714
221772                 TA   =          357
75422
                                          MA   =          357
75823
                                          Ha   =            188
549  n
mi
                                          Hp   =            179
578

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4482686
49                 X    =        -1337567
91
 Y    =      -15092540
27  feet           Y    =        -4615324
78  meter
 Z    =       15389466
50                 Z    =         4684141
30
 XDOT =      23586
652660                 XDOT =        7168
416827
 YDOT =       2075
858692  feet/sec       YDOT =         712
999319  meter/sec
 ZDOT =       8904
927074                 ZDOT =        2749
096959

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13389263
50                 X    =         4081047
52
 Y    =        8331309
32  feet           Y    =         2539383
08  meter
 Z    =       15363327
67                 Z    =         4682742
27
 XDOT =     -18454
537916                 XDOT =       -5624
943157
 YDOT =      12980
897115  feet/sec       YDOT =        3956
577441  meter/sec
 ZDOT =       9042
658694                 ZDOT =        2756
202370


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   09328
49264297  
00016717  00000-0  10270-3 0  9068
2 25544  51
6455 203
1555 0007492   9
0784 351
0515 15
76126549 31212


Satellite: ISS
Catalog Number: 25544
Epoch time:      09328
49264297   =   yrday
fracday
Element set:     906
Inclination:       51
6455  deg
RA of node:       203
1555  deg
Eccentricity:     
0007492     
Arg of perigee:     9
0784  deg
Mean anomaly:     351
0515  deg
Mean motion:   15
76126549  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3121
Checksum:              314


Coasting Arc #8 (Orbit 3120)
---------------------------------------

Vector Time (GMT): 2009/328/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3520996
94                 A    =         6715328
07  meter
 Y    =       -2825807
58  meter          E    =           
0012209
 Z    =        4969145
86                 I    =           51
49989
 XDOT =       6152
133256                 Wp   =           29
68336
 YDOT =       4209
731938  meter/sec      RA   =          202
35575  deg
 ZDOT =      -1952
790783                 TA   =           79
27827
                                          MA   =           79
14084
                                          Ha   =            188
511  n
mi
                                          Hp   =            179
564

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11551827
24                 X    =         3528194
39
 Y    =       -9271022
24  feet           Y    =        -2786393
74  meter
 Z    =       16302971
98                 Z    =         4986268
42
 XDOT =      20184
164227                 XDOT =        6114
088487
 YDOT =      13811
456488  feet/sec       YDOT =        4278
316108  meter/sec
 ZDOT =      -6406
793906                 ZDOT =       -1922
995498

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1762477
48                 X    =         -537203
14
 Y    =       14631656
49  feet           Y    =         4459728
90  meter
 Z    =       16370453
96                 Z    =         4989714
37
 XDOT =     -23062
244242                 XDOT =       -7029
372045
 YDOT =       4303
978140  feet/sec       YDOT =        1311
852537  meter/sec
 ZDOT =      -6288
960565                 ZDOT =       -1916
875180


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   09328
49264394  
00016717  00000-0  10270-3 0  9077
2 25544  51
6455 203
1557 0007504   9
8343 350
2966 15
76103453 31217


Satellite: ISS
Catalog Number: 25544
Epoch time:      09328
49264394   =   yrday
fracday
Element set:     907
Inclination:       51
6455  deg
RA of node:       203
1557  deg
Eccentricity:     
0007504     
Arg of perigee:     9
8343  deg
Mean anomaly:     350
2966  deg
Mean motion:   15
76103453  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3121
Checksum:              308


Coasting Arc #9 (Orbit 3136)
---------------------------------------

Vector Time (GMT): 2009/329/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5186232
41                 A    =         6723923
76  meter
 Y    =       -3558027
67  meter          E    =           
0019052
 Z    =        2345434
95                 I    =           51
55711
 XDOT =       4562
769195                 Wp   =           53
43160
 YDOT =      -3075
995233  meter/sec      RA   =          197
23307  deg
 ZDOT =       5403
901894                 TA   =          333
06336
                                          MA   =          333
16213
                                          Ha   =            188
798  n
mi
                                          Hp   =            179
430

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17015198
20                 X    =        -5157454
35
 Y    =      -11673319
12  feet           Y    =        -3615862
37  meter
 Z    =        7694996
55                 Z    =         2320309
58
 XDOT =      14969
715206                 XDOT =        4570
574795
 YDOT =     -10091
847877  feet/sec       YDOT =       -3024
928244  meter/sec
 ZDOT =      17729
336922                 ZDOT =        5426
087010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20308200
33                 X    =         6189939
46
 Y    =       -3857441
59  feet           Y    =        -1175748
20  meter
 Z    =        7595621
42                 Z    =         2315145
41
 XDOT =      -3615
166477                 XDOT =       -1101
902742
 YDOT =      16174
525515  feet/sec       YDOT =        4929
995377  meter/sec
 ZDOT =      17816
802730                 ZDOT =        5430
561472


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   09329
50713650  
00016717  00000-0  10270-3 0  9085
2 25544  51
6458 197
9299 0007577  14
2980 345
8397 15
76082797 31372


Satellite: ISS
Catalog Number: 25544
Epoch time:      09329
50713650   =   yrday
fracday
Element set:     908
Inclination:       51
6458  deg
RA of node:       197
9299  deg
Eccentricity:     
0007577     
Arg of perigee:    14
2980  deg
Mean anomaly:     345
8397  deg
Mean motion:   15
76082797  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3137
Checksum:              361


Coasting Arc #10 (Orbit 3151)
---------------------------------------

Vector Time (GMT): 2009/330/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4425327
77                 A    =         6717759
23  meter
 Y    =        2585901
86  meter          E    =           
0011432
 Z    =       -4349514
94                 I    =           51
56642
 XDOT =      -5651
827762                 Wp   =           70
18295
 YDOT =      -3966
013172  meter/sec      RA   =          192
03120  deg
 ZDOT =       3403
468349                 TA   =          234
12675
                                          MA   =          234
23295
                                          Ha   =            188
661  n
mi
                                          Hp   =            179
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14518791
90                 X    =        -4432785
31
 Y    =        8483929
99  feet           Y    =         2536373
70  meter
 Z    =      -14270062
13                 Z    =        -4371031
62
 XDOT =     -18542
742000                 XDOT =       -5623
592803
 YDOT =     -13011
854238  feet/sec       YDOT =       -4029
057501  meter/sec
 ZDOT =      11166
234742                 ZDOT =        3376
079674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3890131
71                 X    =         1185712
15
 Y    =      -16285278
70  feet           Y    =        -4963752
95  meter
 Z    =      -14354916
67                 Z    =        -4375378
60
 XDOT =      21088
915862                 XDOT =        6427
901555
 YDOT =      -4677
856036  feet/sec       YDOT =       -1425
810520  meter/sec
 ZDOT =      11057
894997                 ZDOT =        3370
446395


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   09330
45819974  
00016717  00000-0  10270-3 0  9098
2 25544  51
6460 193
0310 0007517  16
5633 343
5776 15
76136865 31529


Satellite: ISS
Catalog Number: 25544
Epoch time:      09330
45819974   =   yrday
fracday
Element set:     909
Inclination:       51
6460  deg
RA of node:       193
0310  deg
Eccentricity:     
0007517     
Arg of perigee:    16
5633  deg
Mean anomaly:     343
5776  deg
Mean motion:   15
76136865  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3152
Checksum:              321


Coasting Arc #11 (Orbit 3167)
---------------------------------------

Vector Time (GMT): 2009/331/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4588024
97                 A    =         6720629
56  meter
 Y    =        3398283
41  meter          E    =           
0010810
 Z    =       -3558945
10                 I    =           51
60544
 XDOT =      -5579
198921                 Wp   =           45
81448
 YDOT =       2873
903093  meter/sec      RA   =          186
92591  deg
 ZDOT =      -4449
198845                 TA   =          176
63487
                                          MA   =          176
62760
                                          Ha   =            188
728  n
mi
                                          Hp   =            179
212

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15052575
37                 X    =         4566972
89
 Y    =       11149223
79  feet           Y    =         3449471
85  meter
 Z    =      -11676329
06                 Z    =        -3536706
96
 XDOT =     -18304
458401                 XDOT =       -5589
306839
 YDOT =       9428
815923  feet/sec       YDOT =        2811
456856  meter/sec
 ZDOT =     -14597
109070                 ZDOT =       -4476
327664

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18459527
77                 X    =        -5626464
07
 Y    =        3489681
18  feet           Y    =         1063654
83  meter
 Z    =      -11588349
17                 Z    =        -3532128
83
 XDOT =       5746
905315                 XDOT =        1751
656740
 YDOT =     -18418
861866  feet/sec       YDOT =       -5614
069097  meter/sec
 ZDOT =     -14704
122168                 ZDOT =       -4481
816437


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   09331
47264622  
00016717  00000-0  10270-3 0  9107
2 25544  51
6458 187
8052 0007435  19
4872 340
6575 15
76152102 31680


Satellite: ISS
Catalog Number: 25544
Epoch time:      09331
47264622   =   yrday
fracday
Element set:     910
Inclination:       51
6458  deg
RA of node:       187
8052  deg
Eccentricity:     
0007435     
Arg of perigee:    19
4872  deg
Mean anomaly:     340
6575  deg
Mean motion:   15
76152102  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3168
Checksum:              311


Coasting Arc #12 (Orbit 3183)
---------------------------------------

Vector Time (GMT): 2009/332/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5274583
91                 A    =         6720888
27  meter
 Y    =       -2484123
72  meter          E    =           
0017118
 Z    =        3337090
00                 I    =           51
63730
 XDOT =       4777
898227                 Wp   =           66
38082
 YDOT =       3839
994957  meter/sec      RA   =          181
72097  deg
 ZDOT =      -4667
882408                 TA   =           74
30746
                                          MA   =           74
11868
                                          Ha   =            188
711  n
mi
                                          Hp   =            178
779

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17305065
32                 X    =         5285758
38
 Y    =       -8150012
22  feet           Y    =        -2425077
91  meter
 Z    =       10948457
99                 Z    =         3362741
63
 XDOT =      15675
519119                 XDOT =        4757
279961
 YDOT =      12598
408652  feet/sec       YDOT =        3893
309193  meter/sec
 ZDOT =     -15314
574831                 ZDOT =       -4644
720640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5450058
60                 X    =        -1661177
86
 Y    =       18274531
28  feet           Y    =         5570077
14  meter
 Z    =       11049664
47                 Z    =         3367937
73
 XDOT =     -18572
921649                 XDOT =       -5661
026519
 YDOT =       3715
684475  feet/sec       YDOT =        1132
540628  meter/sec
 ZDOT =     -15222
922415                 ZDOT =       -4639
946752


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   09332
48706974  
00016717  00000-0  10270-3 0  9111
2 25544  51
6457 182
5791 0007647  23
5390 336
6123 15
76232530 31843


Satellite: ISS
Catalog Number: 25544
Epoch time:      09332
48706974   =   yrday
fracday
Element set:     911
Inclination:       51
6457  deg
RA of node:       182
5791  deg
Eccentricity:     
0007647     
Arg of perigee:    23
5390  deg
Mean anomaly:     336
6123  deg
Mean motion:   15
76232530  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3184
Checksum:              318


Coasting Arc #13 (Orbit 3199)
---------------------------------------

Vector Time (GMT): 2009/333/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3686352
20                 A    =         6717123
50  meter
 Y    =       -3346188
67  meter          E    =           
0012215
 Z    =        4497504
40                 I    =           51
65342
 XDOT =       6435
430577                 Wp   =           74
49719
 YDOT =      -2866
983636  meter/sec      RA   =          176
61756  deg
 ZDOT =       3137
882670                 TA   =          344
23346
                                          MA   =          344
27146
                                          Ha   =            188
952  n
mi
                                          Hp   =            178
715

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12094331
36                 X    =        -3670509
25
 Y    =      -10978309
30  feet           Y    =        -3387323
39  meter
 Z    =       14755591
85                 Z    =         4479633
81
 XDOT =      21113
617380                 XDOT =        6451
767676
 YDOT =      -9406
114291  feet/sec       YDOT =       -2794
927741  meter/sec
 ZDOT =      10294
890650                 ZDOT =        3169
186381

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16273495
69                 X    =         4960161
49
 Y    =       -2012941
00  feet           Y    =         -613544
42  meter
 Z    =       14684856
95                 Z    =         4475944
40
 XDOT =      -6829
681513                 XDOT =       -2081
686925
 YDOT =      20882
302077  feet/sec       YDOT =        6364
925673  meter/sec
 ZDOT =      10418
418572                 ZDOT =        3175
533981


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   09333
50147236  
00016717  00000-0  10270-3 0  9126
2 25544  51
6449 177
3525 0007650  27
4713 332
6854 15
76213100 32005


Satellite: ISS
Catalog Number: 25544
Epoch time:      09333
50147236   =   yrday
fracday
Element set:     912
Inclination:       51
6449  deg
RA of node:       177
3525  deg
Eccentricity:     
0007650     
Arg of perigee:    27
4713  deg
Mean anomaly:     332
6854  deg
Mean motion:   15
76213100  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3200
Checksum:              285


Coasting Arc #14 (Orbit 3214)
---------------------------------------

Vector Time (GMT): 2009/334/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5869829
04                 A    =         6723824
75  meter
 Y    =        2534286
01  meter          E    =           
0013944
 Z    =       -2065342
85                 I    =           51
70565
 XDOT =      -3631
200141                 Wp   =           35
06809
 YDOT =      -3897
788549  meter/sec      RA   =          171
42534  deg
 ZDOT =       5566
955335                 TA   =          301
87367
                                          MA   =          302
00929
                                          Ha   =            188
750  n
mi
                                          Hp   =            178
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19257969
29                 X    =        -5887698
25
 Y    =        8314586
66  feet           Y    =         2468546
43  meter
 Z    =       -6776059
23                 Z    =        -2093902
47
 XDOT =     -11913
386290                 XDOT =       -3614
388569
 YDOT =     -12788
020173  feet/sec       YDOT =       -3938
301349  meter/sec
 ZDOT =      18264
289157                 ZDOT =        5549
354872

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5961227
61                 X    =         1816982
18
 Y    =      -20072997
16  feet           Y    =        -6118249
53  meter
 Z    =       -6888777
96                 Z    =        -2099699
52
 XDOT =      16057
306743                 XDOT =        4894
267095
 YDOT =      -1442
628775  feet/sec       YDOT =        -439
713251  meter/sec
 ZDOT =      18194
594759                 ZDOT =        5545
712483


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   09334
45245187  
00016717  00000-0  10270-3 0  9136
2 25544  51
6438 172
4524 0007572  29
2579 330
9008 15
76259615 32150


Satellite: ISS
Catalog Number: 25544
Epoch time:      09334
45245187   =   yrday
fracday
Element set:     913
Inclination:       51
6438  deg
RA of node:       172
4524  deg
Eccentricity:     
0007572     
Arg of perigee:    29
2579  deg
Mean anomaly:     330
9008  deg
Mean motion:   15
76259615  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3215
Checksum:              320


Coasting Arc #15 (Orbit 3230)
---------------------------------------

Vector Time (GMT): 2009/335/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2589555
54                 A    =         6714327
01  meter
 Y    =        3524094
47  meter          E    =           
0019874
 Z    =       -5111971
39                 I    =           51
70203
 XDOT =      -6953
465677                 Wp   =           63
03528
 YDOT =       2918
278722  meter/sec      RA   =          166
30815  deg
 ZDOT =      -1506
233322                 TA   =          192
48742
                                          MA   =          192
53674
                                          Ha   =            188
798  n
mi
                                          Hp   =            178
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8495917
13                 X    =         2574789
75
 Y    =       11561989
74  feet           Y    =         3552970
53  meter
 Z    =      -16771559
68                 Z    =        -5099426
38
 XDOT =     -22813
207603                 XDOT =       -6978
264368
 YDOT =       9574
405257  feet/sec       YDOT =        2840
382512  meter/sec
 ZDOT =      -4941
710374                 ZDOT =       -1540
074037

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14393864
87                 X    =        -4387250
01
 Y    =        -584620
52  feet           Y    =         -178192
33  meter
 Z    =      -16721851
02                 Z    =        -5096820
19
 XDOT =       6834
306133                 XDOT =        2083
096509
 YDOT =     -22688
143146  feet/sec       YDOT =       -6915
346031  meter/sec
 ZDOT =      -5075
297550                 ZDOT =       -1546
950693


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   09335
46680945  
00016717  00000-0  10270-3 0  9144
2 25544  51
6424 167
2250 0007548  33
1868 326
9769 15
76309410 32317


Satellite: ISS
Catalog Number: 25544
Epoch time:      09335
46680945   =   yrday
fracday
Element set:     914
Inclination:       51
6424  deg
RA of node:       167
2250  deg
Eccentricity:     
0007548     
Arg of perigee:    33
1868  deg
Mean anomaly:     326
9769  deg
Mean motion:   15
76309410  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3231
Checksum:              325


Coasting Arc #16 (Orbit 3246)
---------------------------------------

Vector Time (GMT): 2009/336/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6197229
77                 A    =         6725375
45  meter
 Y    =       -2552562
31  meter          E    =           
0014992
 Z    =         523856
58                 I    =           51
76901
 XDOT =       2265
985594                 Wp   =           99
19107
 YDOT =       4236
815415  meter/sec      RA   =          161
14404  deg
 ZDOT =      -6019
034709                 TA   =           75
11591
                                          MA   =           74
94993
                                          Ha   =            188
822  n
mi
                                          Hp   =            178
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20332118
68                 X    =         6222767
52
 Y    =       -8374548
26  feet           Y    =        -2483118
53  meter
 Z    =        1718689
56                 Z    =          554025
03
 XDOT =       7434
335938                 XDOT =        2247
680401
 YDOT =      13900
313042  feet/sec       YDOT =        4262
053586  meter/sec
 ZDOT =     -19747
489203                 ZDOT =       -6008
070110

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5898838
42                 X    =        -1797965
95
 Y    =       21173289
45  feet           Y    =         6453618
62  meter
 Z    =        1837803
50                 Z    =          560162
51
 XDOT =     -14058
951641                 XDOT =       -4285
168460
 YDOT =      -2168
404641  feet/sec       YDOT =        -660
929735  meter/sec
 ZDOT =     -19703
994535                 ZDOT =       -6005
777534


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   09336
48114501  
00016717  00000-0  10270-3 0  9158
2 25544  51
6427 161
9984 0007584  37
0324 323
1362 15
76344207 32473


Satellite: ISS
Catalog Number: 25544
Epoch time:      09336
48114501   =   yrday
fracday
Element set:     915
Inclination:       51
6427  deg
RA of node:       161
9984  deg
Eccentricity:     
0007584     
Arg of perigee:    37
0324  deg
Mean anomaly:     323
1362  deg
Mean motion:   15
76344207  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3247
Checksum:              305


Coasting Arc #17 (Orbit 3262)
---------------------------------------

Vector Time (GMT): 2009/337/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1373795
82                 A    =         6713408
64  meter
 Y    =       -3928150
36  meter          E    =           
0009620
 Z    =        5262007
58                 I    =           51
75609
 XDOT =       7133
213395                 Wp   =           49
94380
 YDOT =      -2912
308951  meter/sec      RA   =          156
00137  deg
 ZDOT =       -305
302582                 TA   =           42
98346
                                          MA   =           42
90834
                                          Ha   =            188
879  n
mi
                                          Hp   =            178
120

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4507204
14                 X    =        -1355330
73
 Y    =      -12887632
43  feet           Y    =        -3943410
58  meter
 Z    =       17263804
39                 Z    =         5255377
78
 XDOT =      23402
931086                 XDOT =        7166
732310
 YDOT =      -9554
819392  feet/sec       YDOT =       -2832
353688  meter/sec
 ZDOT =      -1001
648892                 ZDOT =        -270
567940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13066958
19                 X    =         3982808
86
 Y    =        4070601
09  feet           Y    =         1240719
21  meter
 Z    =       17237450
83                 Z    =         5253975
01
 XDOT =      -6150
680997                 XDOT =       -1874
727568
 YDOT =      23494
581811  feet/sec       YDOT =        7161
148536  meter/sec
 ZDOT =       -864
480332                 ZDOT =        -263
493605


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   09337
49545828  
00016717  00000-0  10270-3 0  9161
2 25544  51
6420 156
7704 0007522  40
9097 319
2631 15
76354098 32632


Satellite: ISS
Catalog Number: 25544
Epoch time:      09337
49545828   =   yrday
fracday
Element set:     916
Inclination:       51
6420  deg
RA of node:       156
7704  deg
Eccentricity:     
0007522     
Arg of perigee:    40
9097  deg
Mean anomaly:     319
2631  deg
Mean motion:   15
76354098  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3263
Checksum:              327


Coasting Arc #18 (Orbit 3278)
---------------------------------------

Vector Time (GMT): 2009/338/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6150331
02                 A    =         6724896
67  meter
 Y    =        2477758
19  meter          E    =           
0021179
 Z    =        1055005
64                 I    =           51
82151
 XDOT =       -917
235981                 Wp   =           52
20546
 YDOT =      -4833
796236  meter/sec      RA   =          150
87005  deg
 ZDOT =       5937
711909                 TA   =          319
32521
                                          MA   =          319
48320
                                          Ha   =            188
828  n
mi
                                          Hp   =            177
972

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20178251
37                 X    =        -6182705
71
 Y    =        8129127
90  feet           Y    =         2408800
38  meter
 Z    =        3461304
58                 Z    =         1025048
80
 XDOT =      -3009
304401                 XDOT =        -891
960042
 YDOT =     -15858
911537  feet/sec       YDOT =       -4843
912916  meter/sec
 ZDOT =      19480
682116                 ZDOT =        5933
316573

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5292890
76                 X    =         1613273
10
 Y    =      -21119539
68  feet           Y    =        -6437235
70  meter
 Z    =        3342982
07                 Z    =         1018940
94
 XDOT =      13126
322766                 XDOT =        4000
903179
 YDOT =       6406
821203  feet/sec       YDOT =        1952
799103  meter/sec
 ZDOT =      19463
124621                 ZDOT =        5932
360384


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   09338
50974837  
00016717  00000-0  10270-3 0  9171
2 25544  51
6412 151
5423 0007510  44
4532 315
7234 15
76405795 32792


Satellite: ISS
Catalog Number: 25544
Epoch time:      09338
50974837   =   yrday
fracday
Element set:     917
Inclination:       51
6412  deg
RA of node:       151
5423  deg
Eccentricity:     
0007510     
Arg of perigee:    44
4532  deg
Mean anomaly:     315
7234  deg
Mean motion:   15
76405795  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3279
Checksum:              317


Coasting Arc #19 (Orbit 3293)
---------------------------------------

Vector Time (GMT): 2009/339/10:45:34
462
Vector Time (MET): N/A
Weight (LBS)     : 731713
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         246422
62                 A    =         6714575
43  meter
 Y    =        4545646
96  meter          E    =           
0018085
 Z    =       -4950711
44                 I    =           51
81268
 XDOT =      -6890
966080                 Wp   =           85
35105
 YDOT =       2678
144737  meter/sec      RA   =          145
70086  deg
 ZDOT =       2124
072713                 TA   =          205
17279
                                          MA   =          205
26104
                                          Ha   =            188
824  n
mi
                                          Hp   =            177
765

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         808473
18                 X    =          219623
85
 Y    =       14913539
88  feet           Y    =         4548253
44  meter
 Z    =      -16242491
59                 Z    =        -4949578
78
 XDOT =     -22608
156429                 XDOT =       -6930
719810
 YDOT =       8786
564099  feet/sec       YDOT =        2600
863324  meter/sec
 ZDOT =       6968
742497                 ZDOT =        2090
500064

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12733372
91                 X    =        -3881132
06
 Y    =       -7815338
94  feet           Y    =        -2382115
31  meter
 Z    =      -16237842
38                 Z    =        -4949294
36
 XDOT =       5226
099649                 XDOT =        1592
915173
 YDOT =     -22663
197365  feet/sec       YDOT =       -6907
742557  meter/sec
 ZDOT =       6836
114431                 ZDOT =        2083
647679


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   09339
46062550  
00016717  00000-0  10270-3 0  9188
2 25544  51
6410 146
6409 0007544  48
7561 311
4252 15
76444230 32942


Satellite: ISS
Catalog Number: 25544
Epoch time:      09339
46062550   =   yrday
fracday
Element set:     918
Inclination:       51
6410  deg
RA of node:       146
6409  deg
Eccentricity:     
0007544     
Arg of perigee:    48
7561  deg
Mean anomaly:     311
4252  deg
Mean motion:   15
76444230  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3294
Checksum:              304

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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