Date: March 27th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8234 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 1526)
---------------------------------------

Vector Time (GMT): 2008/085/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2039949
97                 A    =         6722554
51  meter
 Y    =        5919205
31  meter          E    =           
0004937
 Z    =       -2444509
86                 I    =           51
97551
 XDOT =      -4131
567134                 Wp   =           37
71823
 YDOT =       3643
004934  meter/sec      RA   =           88
76159  deg
 ZDOT =       5382
961347                 TA   =          294
78487
                                          MA   =          294
83623
                                          Ha   =            185
948  n
mi
                                          Hp   =            180
365

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6692749
25                 X    =         1985483
94
 Y    =       19419964
92  feet           Y    =         5941712
52  meter
 Z    =       -8020045
46                 Z    =        -2434732
36
 XDOT =     -13555
010281                 XDOT =       -4198
146326
 YDOT =      11952
115926  feet/sec       YDOT =        3596
431433  meter/sec
 ZDOT =      17660
634341                 ZDOT =        5362
728146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20338523
98                 X    =        -6199182
11
 Y    =       -2980439
29  feet           Y    =         -908437
89  meter
 Z    =       -7981884
69                 Z    =        -2432878
45
 XDOT =      -4522
340498                 XDOT =       -1378
409384
 YDOT =     -16145
809539  feet/sec       YDOT =       -4921
242748  meter/sec
 ZDOT =      17583
446058                 ZDOT =        5359
434358


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   08085
17230508  
00020000  00000-0  20000-3 0  9006
2 25544  51
6386  89
4983 0001037 281
6790  78
4258 15
76475578 15270


Satellite: ISS
Catalog Number: 25544
Epoch time:      08085
17230508   =   yrday
fracday
Element set:     900
Inclination:       51
6386  deg
RA of node:        89
4983  deg
Eccentricity:     
0001037     
Arg of perigee:   281
6790  deg
Mean anomaly:      78
4258  deg
Mean motion:   15
76475578  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1527
Checksum:              318


Coasting Arc #2 (Orbit 1542)
---------------------------------------

Vector Time (GMT): 2008/086/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3680944
06                 A    =         6714119
18  meter
 Y    =       -2520440
26  meter          E    =           
0012272
 Z    =       -5028726
05                 I    =           51
94596
 XDOT =       2278
743029                 Wp   =           73
53532
 YDOT =       7102
712173  meter/sec      RA   =           83
66667  deg
 ZDOT =      -1892
319177                 TA   =          178
27027
                                          MA   =          178
26602
                                          Ha   =            185
862  n
mi
                                          Hp   =            180
396

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12076588
13                 X    =         3733283
23
 Y    =       -8269160
97  feet           Y    =        -2478985
38  meter
 Z    =      -16498445
06                 Z    =        -5010716
69
 XDOT =       7476
191040                 XDOT =        2208
342637
 YDOT =      23302
861459  feet/sec       YDOT =        7127
800681  meter/sec
 ZDOT =      -6208
396249                 ZDOT =       -1881
420241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1973510
98                 X    =          601526
15
 Y    =       14580584
63  feet           Y    =         4444162
20  meter
 Z    =      -16429653
05                 Z    =        -5007758
25
 XDOT =     -23143
703437                 XDOT =       -7054
200808
 YDOT =      -3813
781175  feet/sec       YDOT =       -1162
440502  meter/sec
 ZDOT =      -6165
812730                 ZDOT =       -1879
339720


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   08086
18652290  
00020000  00000-0  20000-3 0  9015
2 25544  51
6391  84
2706 0001085 283
5422  76
5621 15
76512736 15437


Satellite: ISS
Catalog Number: 25544
Epoch time:      08086
18652290   =   yrday
fracday
Element set:     901
Inclination:       51
6391  deg
RA of node:        84
2706  deg
Eccentricity:     
0001085     
Arg of perigee:   283
5422  deg
Mean anomaly:      76
5621  deg
Mean motion:   15
76512736  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1543
Checksum:              284


Coasting Arc #3 (Orbit 1558)
---------------------------------------

Vector Time (GMT): 2008/087/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1942619
84                 A    =         6724676
77  meter
 Y    =       -6380348
03  meter          E    =           
0012627
 Z    =         809426
38                 I    =           51
97762
 XDOT =       4360
240765                 Wp   =          128
15931
 YDOT =      -2095
520295  meter/sec      RA   =           78
51138  deg
 ZDOT =      -5998
417047                 TA   =           43
04362
                                          MA   =           42
94492
                                          Ha   =            185
861  n
mi
                                          Hp   =            180
228

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6373424
66                 X    =        -1875061
48
 Y    =      -20932900
35  feet           Y    =        -6401693
76  meter
 Z    =        2655598
36                 Z    =          800153
32
 XDOT =      14305
251853                 XDOT =        4412
488500
 YDOT =      -6875
066585  feet/sec       YDOT =       -2046
469582  meter/sec
 ZDOT =     -19679
845955                 ZDOT =       -5977
107946

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21643955
89                 X    =         6597077
75
 Y    =        3246120
75  feet           Y    =          989417
61  meter
 Z    =        2619338
67                 Z    =          798374
43
 XDOT =        235
195844                 XDOT =          71
687693
 YDOT =      14393
797983  feet/sec       YDOT =        4387
229625  meter/sec
 ZDOT =     -19598
344875                 ZDOT =       -5973
575518


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   08087
20072149  
00020000  00000-0  20000-3 0  9029
2 25544  51
6394  79
0425 0000986 284
6709  75
4346 15
76543013 15590


Satellite: ISS
Catalog Number: 25544
Epoch time:      08087
20072149   =   yrday
fracday
Element set:     902
Inclination:       51
6394  deg
RA of node:        79
0425  deg
Eccentricity:     
0000986     
Arg of perigee:   284
6709  deg
Mean anomaly:      75
4346  deg
Mean motion:   15
76543013  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1559
Checksum:              301


Coasting Arc #4 (Orbit 1574)
---------------------------------------

Vector Time (GMT): 2008/088/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3983968
53                 A    =         6712648
48  meter
 Y    =        1121372
50  meter          E    =           
0001509
 Z    =        5283721
50                 I    =           51
93153
 XDOT =      -2159
985428                 Wp   =           66
87497
 YDOT =      -7397
840810  meter/sec      RA   =           73
38580  deg
 ZDOT =        -57
997825                 TA   =           23
67618
                                          MA   =           23
66924
                                          Ha   =            185
867  n
mi
                                          Hp   =            180
108

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13070762
88                 X    =        -4021879
22
 Y    =        3679043
63  feet           Y    =         1076609
57  meter
 Z    =       17335044
30                 Z    =         5264275
24
 XDOT =      -7086
566366                 XDOT =       -2076
819344
 YDOT =     -24271
131265  feet/sec       YDOT =       -7421
529995  meter/sec
 ZDOT =       -190
281578                 ZDOT =         -68
288977

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2116924
06                 X    =          645238
45
 Y    =      -13508333
83  feet           Y    =        -4117340
15  meter
 Z    =       17260576
90                 Z    =         5261023
84
 XDOT =      24038
034861                 XDOT =        7326
793026
 YDOT =       3469
973003  feet/sec       YDOT =        1057
647771  meter/sec
 ZDOT =       -230
548646                 ZDOT =         -70
271227


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   08088
21489861  
00020000  00000-0  20000-3 0  9035
2 25544  51
6403  73
8142 0001078 294
7385  65
3668 15
76616923 15758


Satellite: ISS
Catalog Number: 25544
Epoch time:      08088
21489861   =   yrday
fracday
Element set:     903
Inclination:       51
6403  deg
RA of node:        73
8142  deg
Eccentricity:     
0001078     
Arg of perigee:   294
7385  deg
Mean anomaly:      65
3668  deg
Mean motion:   15
76616923  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1575
Checksum:              315


Coasting Arc #5 (Orbit 1590)
---------------------------------------

Vector Time (GMT): 2008/089/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1782442
49                 A    =         6724399
20  meter
 Y    =        6411308
02  meter          E    =           
0013361
 Z    =         918760
13                 I    =           51
96170
 XDOT =      -4841
645530                 Wp   =           50
82596
 YDOT =        482
507898  meter/sec      RA   =           68
26216  deg
 ZDOT =       5976
829477                 TA   =          319
17434
                                          MA   =          319
27436
                                          Ha   =            185
826  n
mi
                                          Hp   =            180
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5847908
42                 X    =         1706154
60
 Y    =       21034475
14  feet           Y    =         6430813
77  meter
 Z    =        3014304
90                 Z    =          927233
89
 XDOT =     -15884
663812                 XDOT =       -4875
715505
 YDOT =       1583
031163  feet/sec       YDOT =         428
175394  meter/sec
 ZDOT =      19609
020595                 ZDOT =        5953
226021

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21613281
53                 X    =        -6587728
21
 Y    =       -3051569
52  feet           Y    =         -930118
39  meter
 Z    =        3047490
15                 Z    =          928875
00
 XDOT =       4711
979300                 XDOT =        1436
211291
 YDOT =     -13721
637884  feet/sec       YDOT =       -4182
355227  meter/sec
 ZDOT =      19518
534096                 ZDOT =        5949
249193


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   08089
22905813  
00020000  00000-0  20000-3 0  9048
2 25544  51
6405  68
5864 0000985 304
0602  56
0469 15
76608276 15911


Satellite: ISS
Catalog Number: 25544
Epoch time:      08089
22905813   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:        68
5864  deg
Eccentricity:     
0000985     
Arg of perigee:   304
0602  deg
Mean anomaly:      56
0469  deg
Mean motion:   15
76608276  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1591
Checksum:              301


Coasting Arc #6 (Orbit 1605)
---------------------------------------

Vector Time (GMT): 2008/090/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4507052
24                 A    =         6713903
33  meter
 Y    =         257360
60  meter          E    =           
0011972
 Z    =       -4980366
93                 I    =           51
91461
 XDOT =       1847
905742                 Wp   =          103
27392
 YDOT =       7185
511543  meter/sec      RA   =           63
10297  deg
 ZDOT =       2044
997903                 TA   =          186
44909
                                          MA   =          186
46451
                                          Ha   =            185
745  n
mi
                                          Hp   =            180
069

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14786916
79                 X    =         4528033
05
 Y    =         844358
91  feet           Y    =          307878
29  meter
 Z    =      -16339786
51                 Z    =        -4958420
79
 XDOT =       6062
682879                 XDOT =        1757
484701
 YDOT =      23574
512937  feet/sec       YDOT =        7205
670330  meter/sec
 ZDOT =       6709
310706                 ZDOT =        2053
755294

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6484552
17                 X    =        -1976491
50
 Y    =       13418693
95  feet           Y    =         4090017
92  meter
 Z    =      -16255574
71                 Z    =        -4954699
17
 XDOT =     -23104
301727                 XDOT =       -7042
191166
 YDOT =      -3001
328358  feet/sec       YDOT =        -914
804884  meter/sec
 ZDOT =       6743
662558                 ZDOT =        2055
468348


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   08090
17981247  
00020000  00000-0  20000-3 0  9050
2 25544  51
6404  63
6857 0000969 307
5530  52
5546 15
76668380 16064


Satellite: ISS
Catalog Number: 25544
Epoch time:      08090
17981247   =   yrday
fracday
Element set:     905
Inclination:       51
6404  deg
RA of node:        63
6857  deg
Eccentricity:     
0000969     
Arg of perigee:   307
5530  deg
Mean anomaly:      52
5546  deg
Mean motion:   15
76668380  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1606
Checksum:              306


Coasting Arc #7 (Orbit 1621)
---------------------------------------

Vector Time (GMT): 2008/091/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1360484
33                 A    =         6721598
88  meter
 Y    =       -6041248
28  meter          E    =           
0004028
 Z    =       -2613050
63                 I    =           51
92571
 XDOT =       5516
769657                 Wp   =          126
29303
 YDOT =       1034
830011  meter/sec      RA   =           58
00605  deg
 ZDOT =      -5272
706389                 TA   =           83
30159
                                          MA   =           83
25576
                                          Ha   =            185
727  n
mi
                                          Hp   =            179
962

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4463531
26                 X    =        -1280135
39
 Y    =      -19820368
37  feet           Y    =        -6056012
79  meter
 Z    =       -8573000
75                 Z    =        -2619464
53
 XDOT =      18099
637981                 XDOT =        5530
401699
 YDOT =       3395
111586  feet/sec       YDOT =        1096
597796  meter/sec
 ZDOT =     -17298
905475                 ZDOT =       -5245
873005

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20055997
56                 X    =         6113068
06
 Y    =        3177054
49  feet           Y    =          968366
21  meter
 Z    =       -8598240
64                 Z    =        -2620743
75
 XDOT =      -9612
655809                 XDOT =       -2929
937491
 YDOT =      14214
462227  feet/sec       YDOT =        4332
568087  meter/sec
 ZDOT =     -17195
860643                 ZDOT =       -5241
298324


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   08091
19393105  
00020000  00000-0  20000-3 0  9064
2 25544  51
6398  58
4570 0000987 306
8854  53
2220 15
76667737 16221


Satellite: ISS
Catalog Number: 25544
Epoch time:      08091
19393105   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:        58
4570  deg
Eccentricity:     
0000987     
Arg of perigee:   306
8854  deg
Mean anomaly:      53
2220  deg
Mean motion:   15
76667737  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1622
Checksum:              307


Coasting Arc #8 (Orbit 1637)
---------------------------------------

Vector Time (GMT): 2008/092/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5127726
42                 A    =         6717272
51  meter
 Y    =       -1470666
60  meter          E    =           
0010224
 Z    =        4076333
73                 I    =           51
89539
 XDOT =      -1188
527128                 Wp   =           71
40257
 YDOT =      -6568
114721  meter/sec      RA   =           52
82093  deg
 ZDOT =      -3853
722464                 TA   =           58
09835
                                          MA   =           57
99892
                                          Ha   =            185
774  n
mi
                                          Hp   =            179
864

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16823249
41                 X    =        -5130702
03
 Y    =       -4825021
64  feet           Y    =        -1528024
25  meter
 Z    =       13373798
31                 Z    =         4051416
26
 XDOT =      -3899
367218                 XDOT =       -1096
272573
 YDOT =     -21548
932811  feet/sec       YDOT =       -6580
889829  meter/sec
 ZDOT =     -12643
446404                 ZDOT =       -3859
271959

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10455580
59                 X    =         3186860
96
 Y    =      -14125690
01  feet           Y    =        -4305510
32  meter
 Z    =       13278055
29                 Z    =         4047151
25
 XDOT =      20489
571754                 XDOT =        6245
221471
 YDOT =       3226
388385  feet/sec       YDOT =         983
403180  meter/sec
 ZDOT =     -12665
425071                 ZDOT =       -3860
421562


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   08092
20802769  
00020000  00000-0  20000-3 0  9079
2 25544  51
6403  53
2280 0001089 318
0858  42
0223 15
76729010 16381


Satellite: ISS
Catalog Number: 25544
Epoch time:      08092
20802769   =   yrday
fracday
Element set:     907
Inclination:       51
6403  deg
RA of node:        53
2280  deg
Eccentricity:     
0001089     
Arg of perigee:   318
0858  deg
Mean anomaly:      42
0223  deg
Mean motion:   15
76729010  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1638
Checksum:              272


Coasting Arc #9 (Orbit 1653)
---------------------------------------

Vector Time (GMT): 2008/093/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         611994
22                 A    =         6717311
64  meter
 Y    =        5350041
52  meter          E    =           
0009972
 Z    =        4008247
20                 I    =           51
87706
 XDOT =      -6228
329591                 Wp   =           98
64800
 YDOT =      -2250
239054  meter/sec      RA   =           47
73324  deg
 ZDOT =       3944
740790                 TA   =          310
72776
                                          MA   =          310
81432
                                          Ha   =            185
629  n
mi
                                          Hp   =            179
799

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2007855
06                 X    =          532652
55
 Y    =       17552629
65  feet           Y    =         5356441
79  meter
 Z    =       13150417
33                 Z    =         4011027
23
 XDOT =     -20434
152201                 XDOT =       -6221
866858
 YDOT =      -7382
674061  feet/sec       YDOT =       -2319
851437  meter/sec
 ZDOT =      12942
062959                 ZDOT =        3914
499623

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17184944
31                 X    =        -5237971
03
 Y    =       -4063076
35  feet           Y    =        -1238425
67  meter
 Z    =       13161643
71                 Z    =         4011669
00
 XDOT =      13534
101389                 XDOT =        4125
194103
 YDOT =     -15592
457646  feet/sec       YDOT =       -4752
581090  meter/sec
 ZDOT =      12825
814620                 ZDOT =        3909
308296


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   08093
22210311  
00020000  00000-0  20000-3 0  9089
2 25544  51
6400  47
9989 0001055 316
0742  44
0339 15
76759426 16549


Satellite: ISS
Catalog Number: 25544
Epoch time:      08093
22210311   =   yrday
fracday
Element set:     908
Inclination:       51
6400  deg
RA of node:        47
9989  deg
Eccentricity:     
0001055     
Arg of perigee:   316
0742  deg
Mean anomaly:      44
0339  deg
Mean motion:   15
76759426  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1654
Checksum:              280


Coasting Arc #10 (Orbit 1668)
---------------------------------------

Vector Time (GMT): 2008/094/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5690002
10                 A    =         6721250
00  meter
 Y    =        2363563
75  meter          E    =           
0005072
 Z    =       -2682981
79                 I    =           51
86909
 XDOT =        106
252954                 Wp   =           41
40614
 YDOT =       5660
957318  meter/sec      RA   =           42
54509  deg
 ZDOT =       5221
640317                 TA   =          288
09291
                                          MA   =          288
14816
                                          Ha   =            185
690  n
mi
                                          Hp   =            179
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18667985
89                 X    =         5676182
85
 Y    =        7754474
24  feet           Y    =         2427115
13  meter
 Z    =       -8802433
71                 Z    =        -2655373
65
 XDOT =        348
598930                 XDOT =          17
577692
 YDOT =      18572
694614  feet/sec       YDOT =        5661
650088  meter/sec
 ZDOT =      17131
365871                 ZDOT =        5221
940670

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13320071
48                 X    =        -4059957
79
 Y    =       15266266
25  feet           Y    =         4653157
95  meter
 Z    =       -8696276
09                 Z    =        -2650624
95
 XDOT =     -16569
341856                 XDOT =       -5050
335398
 YDOT =      -4714
914351  feet/sec       YDOT =       -1437
105894  meter/sec
 ZDOT =      17133
111819                 ZDOT =        5222
172482


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   08094
17278067  
00020000  00000-0  20000-3 0  9097
2 25544  51
6395  43
0970 0001126 323
9635  36
1454 15
76764773 16693


Satellite: ISS
Catalog Number: 25544
Epoch time:      08094
17278067   =   yrday
fracday
Element set:     909
Inclination:       51
6395  deg
RA of node:        43
0970  deg
Eccentricity:     
0001126     
Arg of perigee:   323
9635  deg
Mean anomaly:      36
1454  deg
Mean motion:   15
76764773  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1669
Checksum:              312


Coasting Arc #11 (Orbit 1684)
---------------------------------------

Vector Time (GMT): 2008/095/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         532308
55                 A    =         6713559
76  meter
 Y    =       -4505137
66  meter          E    =           
0012635
 Z    =       -4960466
86                 I    =           51
82100
 XDOT =       6732
393589                 Wp   =           69
73423
 YDOT =       3090
685782  meter/sec      RA   =           37
44204  deg
 ZDOT =      -2084
507278                 TA   =          180
10944
                                          MA   =          180
10971
                                          Ha   =            185
652  n
mi
                                          Hp   =            179
704

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1746419
13                 X    =          606743
19
 Y    =      -14780635
38  feet           Y    =        -4498769
35  meter
 Z    =      -16274497
56                 Z    =        -4957699
70
 XDOT =      22087
905476                 XDOT =        6707
458851
 YDOT =      10140
045216  feet/sec       YDOT =        3165
831652  meter/sec
 ZDOT =      -6838
934640                 ZDOT =       -2051
862167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13530990
03                 X    =         4124245
76
 Y    =        6225715
68  feet           Y    =         1897598
14  meter
 Z    =      -16264353
84                 Z    =        -4957375
05
 XDOT =     -15906
813745                 XDOT =       -4848
396829
 YDOT =      17033
344082  feet/sec       YDOT =        5191
763276  meter/sec
 ZDOT =      -6713
382933                 ZDOT =       -2046
239118


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   08095
18681546  
00020000  00000-0  20000-3 0  9101
2 25544  51
6395  37
8674 0001086 329
3802  30
7299 15
76786121 16852


Satellite: ISS
Catalog Number: 25544
Epoch time:      08095
18681546   =   yrday
fracday
Element set:     910
Inclination:       51
6395  deg
RA of node:        37
8674  deg
Eccentricity:     
0001086     
Arg of perigee:   329
3802  deg
Mean anomaly:      30
7299  deg
Mean motion:   15
76786121  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1685
Checksum:              315


Coasting Arc #12 (Orbit 1700)
---------------------------------------

Vector Time (GMT): 2008/096/04:01:08
440
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5972284
00                 A    =         6723732
19  meter
 Y    =       -2945007
23  meter          E    =           
0012640
 Z    =         889173
64                 I    =           51
83277
 XDOT =       1403
120577                 Wp   =          122
43161
 YDOT =      -4664
749947  meter/sec      RA   =           32
27305  deg
 ZDOT =      -5971
156898                 TA   =           47
87665
                                          MA   =           47
76929
                                          Ha   =            185
619  n
mi
                                          Hp   =            179
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19594107
60                 X    =        -5943228
06
 Y    =       -9662097
20  feet           Y    =        -3011630
18  meter
 Z    =        2917236
34                 Z    =          860230
96
 XDOT =       4603
413965                 XDOT =        1484
185234
 YDOT =     -15304
297728  feet/sec       YDOT =       -4648
606741  meter/sec
 ZDOT =     -19590
409771                 ZDOT =       -5964
143165

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14870367
47                 X    =         4532488
00
 Y    =      -16024808
49  feet           Y    =        -4884361
63  meter
 Z    =        2805909
30                 Z    =          855241
16
 XDOT =      12146
244481                 XDOT =        3702
175318
 YDOT =       7813
033600  feet/sec       YDOT =        2381
412641  meter/sec
 ZDOT =     -19563
990626                 ZDOT =       -5963
104343


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   08096
20082769  
00020000  00000-0  20000-3 0  9118
2 25544  51
6404  32
6381 0001203 341
2796  18
8324 15
76861275 17016


Satellite: ISS
Catalog Number: 25544
Epoch time:      08096
20082769   =   yrday
fracday
Element set:     911
Inclination:       51
6404  deg
RA of node:        32
6381  deg
Eccentricity:     
0001203     
Arg of perigee:   341
2796  deg
Mean anomaly:      18
8324  deg
Mean motion:   15
76861275  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1701
Checksum:              276

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 may contain past, current and future orbital data 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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