Date: January 22nd 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11474 33 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 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 523)
---------------------------------------

Vector Time (GMT): 2008/021/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -67460
55                 A    =         6716538
45  meter
 Y    =       -5547068
72  meter          E    =           
0005713
 Z    =       -3792501
74                 I    =           51
90794
 XDOT =       5788
838329                 Wp   =           18
26373
 YDOT =       2818
929401  meter/sec      RA   =           56
89877  deg
 ZDOT =      -4222
446094                 TA   =          207
55111
                                          MA   =          207
58140
                                          Ha   =            184
483  n
mi
                                          Hp   =            180
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -221327
25                 X    =           12995
43
 Y    =      -18199044
34  feet           Y    =        -5547372
75  meter
 Z    =      -12442591
03                 Z    =        -3792634
76
 XDOT =      18992
251735                 XDOT =        5777
397721
 YDOT =       9248
456039  feet/sec       YDOT =        2883
600063  meter/sec
 ZDOT =     -13853
169600                 ZDOT =       -4194
352087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8103146
11                 X    =         2469838
93
 Y    =      -16296232
23  feet           Y    =        -4967091
58  meter
 Z    =      -12443637
34                 Z    =        -3792820
66
 XDOT =      11630
269376                 XDOT =        3544
906106
 YDOT =      16287
962749  feet/sec       YDOT =        4964
571046  meter/sec
 ZDOT =     -13745
451282                 ZDOT =       -4189
613551


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   08021
61665162  
00020000  00000-0  20000-3 0  9003
2 25544  51
6372  57
3549 0005708 312
6203  47
4480 15
77296667  5240


Satellite: ISS
Catalog Number: 25544
Epoch time:      08021
61665162   =   yrday
fracday
Element set:     900
Inclination:       51
6372  deg
RA of node:        57
3549  deg
Eccentricity:     
0005708     
Arg of perigee:   312
6203  deg
Mean anomaly:      47
4480  deg
Mean motion:   15
77296667  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             524
Checksum:              285


Coasting Arc #2 (Orbit 539)
---------------------------------------

Vector Time (GMT): 2008/022/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5252776
52                 A    =         6719259
32  meter
 Y    =       -3118280
87  meter          E    =           
0009596
 Z    =        2793393
40                 I    =           51
90022
 XDOT =        639
062039                 Wp   =           78
34983
 YDOT =      -5699
858368  meter/sec      RA   =           51
70676  deg
 ZDOT =      -5144
399283                 TA   =           69
74845
                                          MA   =           69
64531
                                          Ha   =            184
595  n
mi
                                          Hp   =            179
970

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17233518
77                 X    =        -5231086
41
 Y    =      -10230580
28  feet           Y    =        -3176899
42  meter
 Z    =        9164676
51                 Z    =         2767928
55
 XDOT =       2096
660234                 XDOT =         727
741027
 YDOT =     -18700
322730  feet/sec       YDOT =       -5692
215648  meter/sec
 ZDOT =     -16877
950403                 ZDOT =       -5141
080013

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11072081
07                 X    =        -3374770
31
 Y    =      -16758555
55  feet           Y    =        -5108007
73  meter
 Z    =        9066977
12                 Z    =         2763614
63
 XDOT =       8925
977762                 XDOT =        2720
638022
 YDOT =     -15052
157574  feet/sec       YDOT =       -4587
897628  meter/sec
 ZDOT =     -16865
809143                 ZDOT =       -5140
698627


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   08022
63033830  
00020000  00000-0  20000-3 0  9018
2 25544  51
6368  52
1227 0005877 317
6324  42
4387 15
77375306  5404


Satellite: ISS
Catalog Number: 25544
Epoch time:      08022
63033830   =   yrday
fracday
Element set:     901
Inclination:       51
6368  deg
RA of node:        52
1227  deg
Eccentricity:     
0005877     
Arg of perigee:   317
6324  deg
Mean anomaly:      42
4387  deg
Mean motion:   15
77375306  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             540
Checksum:              274


Coasting Arc #3 (Orbit 555)
---------------------------------------

Vector Time (GMT): 2008/023/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1288817
06                 A    =         6711795
93  meter
 Y    =        4319574
78  meter          E    =           
0001730
 Z    =        4971357
07                 I    =           51
85553
 XDOT =      -6149
650697                 Wp   =           44
62876
 YDOT =      -4176
691846  meter/sec      RA   =           46
60183  deg
 ZDOT =       2035
590136                 TA   =           25
75351
                                          MA   =           25
74490
                                          Ha   =            184
762  n
mi
                                          Hp   =            179
767

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4228402
42                 X    =        -1361172
61
 Y    =       14171833
28  feet           Y    =         4304757
57  meter
 Z    =       16310226
59                 Z    =         4964920
76
 XDOT =     -20176
019348                 XDOT =       -6112
377453
 YDOT =     -13703
057236  feet/sec       YDOT =       -4245
252481  meter/sec
 ZDOT =       6678
445328                 ZDOT =        2005
806301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9894019
54                 X    =        -3015697
15
 Y    =       11028024
45  feet           Y    =         3361341
85  meter
 Z    =       16286030
55                 Z    =         4963982
11
 XDOT =     -11745
437220                 XDOT =       -3580
009265
 YDOT =     -20227
662953  feet/sec       YDOT =       -6165
391668  meter/sec
 ZDOT =       6564
117585                 ZDOT =        2000
743040


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   08023
64399977  
00020000  00000-0  20000-3 0  9028
2 25544  51
6362  46
8902 0005855 321
3010  38
7734 15
77383169  5565


Satellite: ISS
Catalog Number: 25544
Epoch time:      08023
64399977   =   yrday
fracday
Element set:     902
Inclination:       51
6362  deg
RA of node:        46
8902  deg
Eccentricity:     
0005855     
Arg of perigee:   321
3010  deg
Mean anomaly:      38
7734  deg
Mean motion:   15
77383169  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             556
Checksum:              305


Coasting Arc #4 (Orbit 570)
---------------------------------------

Vector Time (GMT): 2008/024/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5337981
56                 A    =         6722171
92  meter
 Y    =        4017790
94  meter          E    =           
0013473
 Z    =        -662696
91                 I    =           51
87015
 XDOT =      -2403
289385                 Wp   =           16
14904
 YDOT =       4178
587489  meter/sec      RA   =           41
43352  deg
 ZDOT =       6017
217809                 TA   =          336
64236
                                          MA   =          336
70351
                                          Ha   =            184
732  n
mi
                                          Hp   =            179
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17513062
87                 X    =         5295876
45
 Y    =       13181728
81  feet           Y    =         4077247
90  meter
 Z    =       -2174202
46                 Z    =         -636867
86
 XDOT =      -7884
807693                 XDOT =       -2479
066056
 YDOT =      13709
276539  feet/sec       YDOT =        4151
288581  meter/sec
 ZDOT =      19741
528245                 ZDOT =        6005
359110

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10662979
37                 X    =         3250076
11
 Y    =       19162142
13  feet           Y    =         5840620
92  meter
 Z    =       -2075013
68                 Z    =         -632464
17
 XDOT =     -11476
831756                 XDOT =       -3498
138319
 YDOT =       8503
780265  feet/sec       YDOT =        2591
952225  meter/sec
 ZDOT =      19696
579711                 ZDOT =        6003
517496


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   08024
59428164  
00020000  00000-0  20000-3 0  9035
2 25544  51
6361  41
9853 0005628 325
4439  34
6360 15
77460622  5710


Satellite: ISS
Catalog Number: 25544
Epoch time:      08024
59428164   =   yrday
fracday
Element set:     903
Inclination:       51
6361  deg
RA of node:        41
9853  deg
Eccentricity:     
0005628     
Arg of perigee:   325
4439  deg
Mean anomaly:      34
6360  deg
Mean motion:   15
77460622  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             571
Checksum:              287


Coasting Arc #5 (Orbit 586)
---------------------------------------

Vector Time (GMT): 2008/025/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2961148
51                 A    =         6710389
08  meter
 Y    =       -2955786
95  meter          E    =           
0012491
 Z    =       -5256176
95                 I    =           51
80784
 XDOT =       5908
348540                 Wp   =           71
89088
 YDOT =       4901
315451  meter/sec      RA   =           36
28632  deg
 ZDOT =        577
244344                 TA   =          203
55512
                                          MA   =          203
61237
                                          Ha   =            184
902  n
mi
                                          Hp   =            179
410

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9715054
17                 X    =         3019513
38
 Y    =       -9697463
75  feet           Y    =        -2922347
25  meter
 Z    =      -17244675
02                 Z    =        -5241650
37
 XDOT =      19384
345605                 XDOT =        5850
298086
 YDOT =      16080
431271  feet/sec       YDOT =        4967
061376  meter/sec
 ZDOT =       1893
846274                 ZDOT =         605
805457

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12819000
85                 X    =         3907231
46
 Y    =       -5098973
32  feet           Y    =        -1554167
07  meter
 Z    =      -17189403
29                 Z    =        -5239330
12
 XDOT =      11189
592143                 XDOT =        3410
587685
 YDOT =      21431
250524  feet/sec       YDOT =        6532
245160  meter/sec
 ZDOT =       2003
572282                 ZDOT =         610
688831


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   08025
60788957  
00020000  00000-0  20000-3 0  9048
2 25544  51
6364  36
7520 0005834 329
7267  30
3561 15
77456296  5876


Satellite: ISS
Catalog Number: 25544
Epoch time:      08025
60788957   =   yrday
fracday
Element set:     904
Inclination:       51
6364  deg
RA of node:        36
7520  deg
Eccentricity:     
0005834     
Arg of perigee:   329
7267  deg
Mean anomaly:      30
3561  deg
Mean motion:   15
77456296  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             587
Checksum:              316


Coasting Arc #6 (Orbit 602)
---------------------------------------

Vector Time (GMT): 2008/026/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4781939
19                 A    =         6720920
52  meter
 Y    =       -4419873
38  meter          E    =           
0002275
 Z    =       -1663657
77                 I    =           51
82053
 XDOT =       4411
669659                 Wp   =          110
55150
 YDOT =      -2612
835146  meter/sec      RA   =           31
15710  deg
 ZDOT =      -5746
194485                 TA   =           87
80330
                                          MA   =           87
77725
                                          Ha   =            184
941  n
mi
                                          Hp   =            179
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15688776
86                 X    =        -4724078
51
 Y    =      -14500896
92  feet           Y    =        -4473024
21  meter
 Z    =       -5458194
80                 Z    =        -1686747
43
 XDOT =      14473
981820                 XDOT =        4468
472256
 YDOT =      -8572
293787  feet/sec       YDOT =       -2563
183680  meter/sec
 ZDOT =     -18852
344112                 ZDOT =       -5724
625129

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9090280
49                 X    =        -2770717
49
 Y    =      -19308128
74  feet           Y    =        -5885117
64  meter
 Z    =       -5546943
88                 Z    =        -1690708
49
 XDOT =      15321
418304                 XDOT =        4669
968299
 YDOT =      -1827
516837  feet/sec       YDOT =        -557
027132  meter/sec
 ZDOT =     -18770
102239                 ZDOT =       -5721
127162


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   08026
62146937  
00020000  00000-0  20000-3 0  9058
2 25544  51
6371  31
5191 0005926 334
1433  25
9435 15
77522754  6030


Satellite: ISS
Catalog Number: 25544
Epoch time:      08026
62146937   =   yrday
fracday
Element set:     905
Inclination:       51
6371  deg
RA of node:        31
5191  deg
Eccentricity:     
0005926     
Arg of perigee:   334
1433  deg
Mean anomaly:      25
9435  deg
Mean motion:   15
77522754  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             603
Checksum:              280


Coasting Arc #7 (Orbit 618)
---------------------------------------

Vector Time (GMT): 2008/027/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4695798
59                 A    =         6713304
47  meter
 Y    =        1657775
82  meter          E    =           
0010724
 Z    =        4501823
41                 I    =           51
76942
 XDOT =      -4832
816150                 Wp   =           33
27700
 YDOT =      -5110
914799  meter/sec      RA   =           25
96683  deg
 ZDOT =      -3146
666940                 TA   =           88
10620
                                          MA   =           87
98339
                                          Ha   =            185
053  n
mi
                                          Hp   =            178
898

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15406163
36                 X    =        -4735855
75
 Y    =        5438897
03  feet           Y    =         1605040
70  meter
 Z    =       14769761
85                 Z    =         4478914
36
 XDOT =     -15855
696031                 XDOT =       -4760
020268
 YDOT =     -16768
093171  feet/sec       YDOT =       -5164
551041  meter/sec
 ZDOT =     -10323
710432                 ZDOT =       -3169
967576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16409854
42                 X    =        -5001723
63
 Y    =        -473262
15  feet           Y    =         -144250
30  meter
 Z    =       14682303
51                 Z    =         4475166
11
 XDOT =      -8773
202023                 XDOT =       -2674
071977
 YDOT =     -20118
835064  feet/sec       YDOT =       -6132
220928  meter/sec
 ZDOT =     -10413
330887                 ZDOT =       -3173
983254


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   08027
63502107  
00020000  00000-0  20000-3 0  9066
2 25544  51
6371  26
2866 0005958 337
2186  22
8714 15
77565469  6197


Satellite: ISS
Catalog Number: 25544
Epoch time:      08027
63502107   =   yrday
fracday
Element set:     906
Inclination:       51
6371  deg
RA of node:        26
2866  deg
Eccentricity:     
0005958     
Arg of perigee:   337
2186  deg
Mean anomaly:      22
8714  deg
Mean motion:   15
77565469  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             619
Checksum:              305


Coasting Arc #8 (Orbit 634)
---------------------------------------

Vector Time (GMT): 2008/028/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3445752
50                 A    =         6715843
51  meter
 Y    =        4422291
18  meter          E    =           
0010590
 Z    =        3685651
96                 I    =           51
75301
 XDOT =      -6257
048278                 Wp   =           66
20515
 YDOT =       1264
963308  meter/sec      RA   =           20
86265  deg
 ZDOT =       4326
468857                 TA   =          338
18050
                                          MA   =          338
22557
                                          Ha   =            184
890  n
mi
                                          Hp   =            178
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11304962
27                 X    =         3378141
70
 Y    =       14508829
33  feet           Y    =         4460445
44  meter
 Z    =       12092034
00                 Z    =         3702227
05
 XDOT =     -20528
373615                 XDOT =       -6291
745151
 YDOT =       4150
142086  feet/sec       YDOT =        1194
799348  meter/sec
 ZDOT =      14194
451630                 ZDOT =        4295
988310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5592046
85                 X    =         1704455
88
 Y    =       17478262
79  feet           Y    =         5327374
50  meter
 Z    =       12155859
84                 Z    =         3705106
08
 XDOT =     -19509
685791                 XDOT =       -5946
552229
 YDOT =      -3561
571450  feet/sec       YDOT =       -1085
566978  meter/sec
 ZDOT =      14077
997506                 ZDOT =        4290
973640


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   08028
64854319  
00020000  00000-0  20000-3 0  9074
2 25544  51
6380  21
0542 0005820 340
2515  19
8424 15
77638185  6357


Satellite: ISS
Catalog Number: 25544
Epoch time:      08028
64854319   =   yrday
fracday
Element set:     907
Inclination:       51
6380  deg
RA of node:        21
0542  deg
Eccentricity:     
0005820     
Arg of perigee:   340
2515  deg
Mean anomaly:      19
8424  deg
Mean motion:   15
77638185  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             635
Checksum:              283


Coasting Arc #9 (Orbit 649)
---------------------------------------

Vector Time (GMT): 2008/029/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6060656
38                 A    =         6718455
80  meter
 Y    =        -615160
11  meter          E    =           
0008498
 Z    =       -2824508
18                 I    =           51
73363
 XDOT =       2883
601722                 Wp   =           17
12620
 YDOT =       4995
390108  meter/sec      RA   =           15
65700  deg
 ZDOT =       5111
327315                 TA   =          310
47869
                                          MA   =          310
55273
                                          Ha   =            185
212  n
mi
                                          Hp   =            178
495

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19884043
26                 X    =         6080805
54
 Y    =       -2018241
81  feet           Y    =         -547273
64  meter
 Z    =       -9266759
13                 Z    =        -2795016
96
 XDOT =       9460
635570                 XDOT =        2802
698597
 YDOT =      16389
075156  feet/sec       YDOT =        5027
183654  meter/sec
 ZDOT =      16769
446573                 ZDOT =        5125
139337

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19504826
76                 X    =         5945071
20
 Y    =        4592040
31  feet           Y    =         1399653
89  meter
 Z    =       -9154026
43                 Z    =        -2790147
26
 XDOT =       3845
135113                 XDOT =        1171
997182
 YDOT =      17124
721806  feet/sec       YDOT =        5219
615207  meter/sec
 ZDOT =      16822
756666                 ZDOT =        5127
576232


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   08029
59869610  
00020000  00000-0  20000-3 0  9080
2 25544  51
6379  16
1482 0005975 345
1060  14
9928 15
77631235  6504


Satellite: ISS
Catalog Number: 25544
Epoch time:      08029
59869610   =   yrday
fracday
Element set:     908
Inclination:       51
6379  deg
RA of node:        16
1482  deg
Eccentricity:     
0005975     
Arg of perigee:   345
1060  deg
Mean anomaly:      14
9928  deg
Mean motion:   15
77631235  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             650
Checksum:              306


Coasting Arc #10 (Orbit 665)
---------------------------------------

Vector Time (GMT): 2008/030/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1417727
22                 A    =         6710801
97  meter
 Y    =       -4273738
74  meter          E    =           
0014727
 Z    =       -4988502
08                 I    =           51
68090
 XDOT =       7442
338420                 Wp   =           51
59298
 YDOT =       -184
580512  meter/sec      RA   =           10
53774  deg
 ZDOT =      -1951
863076                 TA   =          199
51919
                                          MA   =          199
57564
                                          Ha   =            185
121  n
mi
                                          Hp   =            178
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4651336
02                 X    =        -1345599
30
 Y    =      -14021452
58  feet           Y    =        -4289189
04  meter
 Z    =      -16366476
66                 Z    =        -4995214
34
 XDOT =      24417
120801                 XDOT =        7453
330983
 YDOT =       -605
579106  feet/sec       YDOT =        -101
294487  meter/sec
 ZDOT =      -6403
750249                 ZDOT =       -1915
681936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =           8445
25                 X    =            2574
11
 Y    =      -14743863
78  feet           Y    =        -4493929
68  meter
 Z    =      -16392560
11                 Z    =        -4996452
32
 XDOT =      22362
927525                 XDOT =        6816
220310
 YDOT =       6997
415335  feet/sec       YDOT =        2132
812194  meter/sec
 ZDOT =      -6265
389395                 ZDOT =       -1909
690687


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   08030
61216284  
00020000  00000-0  20000-3 0  9099
2 25544  51
6386  10
9148 0005928 348
8630  11
2403 15
77695933  6664


Satellite: ISS
Catalog Number: 25544
Epoch time:      08030
61216284   =   yrday
fracday
Element set:     909
Inclination:       51
6386  deg
RA of node:        10
9148  deg
Eccentricity:     
0005928     
Arg of perigee:   348
8630  deg
Mean anomaly:      11
2403  deg
Mean motion:   15
77695933  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             666
Checksum:              295


Coasting Arc #11 (Orbit 681)
---------------------------------------

Vector Time (GMT): 2008/031/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6697872
76                 A    =         6721491
58  meter
 Y    =        -254562
72  meter          E    =           
0009549
 Z    =         470670
34                 I    =           51
68885
 XDOT =       -247
488720                 Wp   =          105
61436
 YDOT =      -4800
212835  meter/sec      RA   =            5
35693  deg
 ZDOT =      -6019
910588                 TA   =           69
26386
                                          MA   =           69
16155
                                          Ha   =            185
171  n
mi
                                          Hp   =            178
038

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21974648
16                 X    =        -6696814
80
 Y    =        -835179
54  feet           Y    =         -329456
26  meter
 Z    =        1544194
01                 Z    =          438135
04
 XDOT =       -811
970867                 XDOT =        -164
550347
 YDOT =     -15748
729774  feet/sec       YDOT =       -4802
516263  meter/sec
 ZDOT =     -19750
362821                 ZDOT =       -6020
911737

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20771059
10                 X    =        -6331018
82
 Y    =       -7246701
49  feet           Y    =        -2208794
62  meter
 Z    =        1419733
40                 Z    =          432734
74
 XDOT =       3421
795247                 XDOT =        1042
963191
 YDOT =     -13746
674805  feet/sec       YDOT =       -4189
986481  meter/sec
 ZDOT =     -19754
651490                 ZDOT =       -6021
217774


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   08031
62560003  
00020000  00000-0  20000-3 0  9104
2 25544  51
6392   5
6815 0005889 352
8588   7
2493 15
77733477  6824


Satellite: ISS
Catalog Number: 25544
Epoch time:      08031
62560003   =   yrday
fracday
Element set:     910
Inclination:       51
6392  deg
RA of node:         5
6815  deg
Eccentricity:     
0005889     
Arg of perigee:   352
8588  deg
Mean anomaly:       7
2493  deg
Mean motion:   15
77733477  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             682
Checksum:              300


Coasting Arc #12 (Orbit 697)
---------------------------------------

Vector Time (GMT): 2008/032/14:14:00
847
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1023794
83                 A    =         6709580
49  meter
 Y    =        4114386
10  meter          E    =           
0008174
 Z    =        5199087
97                 I    =           51
62013
 XDOT =      -7619
262593                 Wp   =           17
70283
 YDOT =       -742
171530  meter/sec      RA   =             
19086  deg
 ZDOT =       -905
012698                 TA   =           80
95672
                                          MA   =           80
86423
                                          Ha   =            185
204  n
mi
                                          Hp   =            177
773

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3358906
93                 X    =        -1094982
29
 Y    =       13498642
07  feet           Y    =         4102539
01  meter
 Z    =       17057375
23                 Z    =         5193941
86
 XDOT =     -24997
580685                 XDOT =       -7606
000917
 YDOT =      -2434
945964  feet/sec       YDOT =        -827
300237  meter/sec
 ZDOT =      -2969
201764                 ZDOT =        -941
994369

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7057369
23                 X    =        -2151086
14
 Y    =       12014442
80  feet           Y    =         3662002
16  meter
 Z    =       17038085
20                 Z    =         5193208
37
 XDOT =     -22453
828726                 XDOT =       -6843
926996
 YDOT =      -8740
728728  feet/sec       YDOT =       -2664
174116  meter/sec
 ZDOT =      -3110
718110                 ZDOT =        -948
146880


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   08032
63900612  
00020000  00000-0  20000-3 0  9111
2 25544  51
6392    
4485 0005922 356
1241   3
9877 15
77802488  6986


Satellite: ISS
Catalog Number: 25544
Epoch time:      08032
63900612   =   yrday
fracday
Element set:     911
Inclination:       51
6392  deg
RA of node:          
4485  deg
Eccentricity:     
0005922     
Arg of perigee:   356
1241  deg
Mean anomaly:       3
9877  deg
Mean motion:   15
77802488  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             698
Checksum:              289

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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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