Date: June 17th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4843 76 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 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 1049)
---------------------------------------

Vector Time (GMT): 2007/166/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -164236
05                 A    =         6717063
66  meter
 Y    =        6126480
10  meter          E    =           
0009367
 Z    =       -2735337
22                 I    =           51
93750
 XDOT =      -5265
393281                 Wp   =          354
52954
 YDOT =       2174
846511  meter/sec      RA   =          111
99148  deg
 ZDOT =       5194
944536                 TA   =          334
29568
                                          MA   =          334
34220
                                          Ha   =            184
206  n
mi
                                          Hp   =            178
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -538832
19                 X    =         -219443
26
 Y    =       20100000
33  feet           Y    =         6124335
50  meter
 Z    =       -8974203
49                 Z    =        -2736267
70
 XDOT =     -17274
912340                 XDOT =       -5314
557505
 YDOT =       7135
323199  feet/sec       YDOT =        2115
689784  meter/sec
 ZDOT =      17043
781286                 ZDOT =        5169
246343

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18399388
04                 X    =         5608133
47
 Y    =        8106312
47  feet           Y    =         2470804
04  meter
 Z    =       -8977020
63                 Z    =        -2736195
89
 XDOT =        573
913854                 XDOT =         174
928943
 YDOT =      17436
672890  feet/sec       YDOT =        5314
697897  meter/sec
 ZDOT =      16946
921791                 ZDOT =        5165
421762


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   07166
46384241  
00020000  00000-0  20000-3 0  9001
2 25544  51
6309 112
8167 0008419 323
7097  36
3497 15
78167698 10501


Satellite: ISS
Catalog Number: 25544
Epoch time:      07166
46384241   =   yrday
fracday
Element set:     900
Inclination:       51
6309  deg
RA of node:       112
8167  deg
Eccentricity:     
0008419     
Arg of perigee:   323
7097  deg
Mean anomaly:      36
3497  deg
Mean motion:   15
78167698  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1050
Checksum:              304


Coasting Arc #2 (Orbit 1065)
---------------------------------------

Vector Time (GMT): 2007/167/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4345835
88                 A    =         6709052
53  meter
 Y    =        -598073
88  meter          E    =           
0013304
 Z    =       -5086029
31                 I    =           51
92138
 XDOT =       -913
505536                 Wp   =           41
00650
 YDOT =       7464
593097  meter/sec      RA   =          106
88127  deg
 ZDOT =      -1650
927224                 TA   =          213
14464
                                          MA   =          213
22807
                                          Ha   =            184
303  n
mi
                                          Hp   =            178
444

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14257991
73                 X    =         4376907
50
 Y    =       -1962184
63  feet           Y    =         -549301
38  meter
 Z    =      -16686447
86                 Z    =        -5064842
02
 XDOT =      -2997
065407                 XDOT =        -988
887957
 YDOT =      24490
134832  feet/sec       YDOT =        7453
956669  meter/sec
 ZDOT =      -5416
427901                 ZDOT =       -1655
546360

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3409250
86                 X    =         1039139
66
 Y    =      -14077680
41  feet           Y    =        -4290876
99  meter
 Z    =      -16606443
38                 Z    =        -5061643
94
 XDOT =      20692
874280                 XDOT =        6307
188081
 YDOT =      11449
044660  feet/sec       YDOT =        3489
668812  meter/sec
 ZDOT =      -5433
037768                 ZDOT =       -1655
989912


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   07167
47697052  
00020000  00000-0  20000-3 0  9011
2 25544  51
6320 107
5805 0008457 327
0826  32
9812 15
78206983 10664


Satellite: ISS
Catalog Number: 25544
Epoch time:      07167
47697052   =   yrday
fracday
Element set:     901
Inclination:       51
6320  deg
RA of node:       107
5805  deg
Eccentricity:     
0008457     
Arg of perigee:   327
0826  deg
Mean anomaly:      32
9812  deg
Mean motion:   15
78206983  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1066
Checksum:              297


Coasting Arc #3 (Orbit 1081)
---------------------------------------

Vector Time (GMT): 2007/168/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1344146
07                 A    =         6720139
01  meter
 Y    =       -6583421
65  meter          E    =           
0004829
 Z    =          27224
42                 I    =           51
96700
 XDOT =       4655
406623                 Wp   =          104
77451
 YDOT =        921
747207  meter/sec      RA   =          101
72114  deg
 ZDOT =      -6066
863781                 TA   =           74
93076
                                          MA   =           74
87734
                                          Ha   =            184
379  n
mi
                                          Hp   =            178
092

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4409928
04                 X    =         1417530
70
 Y    =      -21599152
40  feet           Y    =        -6567980
35  meter
 Z    =          89318
96                 Z    =           33931
04
 XDOT =      15273
643776                 XDOT =        4674
224927
 YDOT =       3024
105010  feet/sec       YDOT =         973
913108  meter/sec
 ZDOT =     -19904
408730                 ZDOT =       -6044
202136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18704814
39                 X    =        -5701227
43
 Y    =      -11666009
09  feet           Y    =        -3555799
57  meter
 Z    =         113922
36                 Z    =           34723
54
 XDOT =       7349
584930                 XDOT =        2240
153487
 YDOT =     -11999
830639  feet/sec       YDOT =       -3657
548379  meter/sec
 ZDOT =     -19818
650173                 ZDOT =       -6040
724573


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   07168
49008068  
00020000  00000-0  20000-3 0  9028
2 25544  51
6327 102
3446 0008511 330
8958  29
1732 15
78238597 10827


Satellite: ISS
Catalog Number: 25544
Epoch time:      07168
49008068   =   yrday
fracday
Element set:     902
Inclination:       51
6327  deg
RA of node:       102
3446  deg
Eccentricity:     
0008511     
Arg of perigee:   330
8958  deg
Mean anomaly:      29
1732  deg
Mean motion:   15
78238597  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1082
Checksum:              297


Coasting Arc #4 (Orbit 1097)
---------------------------------------

Vector Time (GMT): 2007/169/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3762694
08                 A    =         6708804
96  meter
 Y    =       -2213854
53  meter          E    =           
0010571
 Z    =        5096192
99                 I    =           51
93389
 XDOT =       2089
699347                 Wp   =            1
77764
 YDOT =      -7244
221843  meter/sec      RA   =           96
56266  deg
 ZDOT =      -1593
657924                 TA   =          103
50999
                                          MA   =          103
39218
                                          Ha   =            184
551  n
mi
                                          Hp   =            177
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12344796
84                 X    =        -3762414
85
 Y    =       -7263302
25  feet           Y    =        -2255930
50  meter
 Z    =       16719793
28                 Z    =         5077914
30
 XDOT =       6855
968986                 XDOT =        2178
291588
 YDOT =     -23767
132031  feet/sec       YDOT =       -7220
358001  meter/sec
 ZDOT =      -5228
536497                 ZDOT =       -1583
292499

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10986925
53                 X    =        -3348814
90
 Y    =        9314026
46  feet           Y    =         2838915
27  meter
 Z    =       16650448
47                 Z    =         5075056
69
 XDOT =     -19444
576029                 XDOT =       -5926
706774
 YDOT =     -13597
244690  feet/sec       YDOT =       -4144
440182  meter/sec
 ZDOT =      -5190
175036                 ZDOT =       -1581
965351


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   07169
50317290  
00020000  00000-0  20000-3 0  9032
2 25544  51
6330  97
1088 0008534 334
6818  25
3928 15
78266097 10984


Satellite: ISS
Catalog Number: 25544
Epoch time:      07169
50317290   =   yrday
fracday
Element set:     903
Inclination:       51
6330  deg
RA of node:        97
1088  deg
Eccentricity:     
0008534     
Arg of perigee:   334
6818  deg
Mean anomaly:      25
3928  deg
Mean motion:   15
78266097  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1098
Checksum:              308


Coasting Arc #5 (Orbit 1113)
---------------------------------------

Vector Time (GMT): 2007/170/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2261063
24                 A    =         6716818
76  meter
 Y    =        5706109
69  meter          E    =           
0014755
 Z    =        2704435
34                 I    =           51
96322
 XDOT =      -3981
042446                 Wp   =           43
89891
 YDOT =      -4053
835882  meter/sec      RA   =           91
45214  deg
 ZDOT =       5218
448575                 TA   =          346
89457
                                          MA   =          346
93287
                                          Ha   =            184
649  n
mi
                                          Hp   =            177
573

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7418186
50                 X    =        -2337839
24
 Y    =       18720832
31  feet           Y    =         5680395
48  meter
 Z    =        8872819
36                 Z    =         2693265
70
 XDOT =     -13061
162882                 XDOT =       -3960
765942
 YDOT =     -13299
986488  feet/sec       YDOT =       -4098
241639  meter/sec
 ZDOT =      17120
894276                 ZDOT =        5199
157477

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15397002
82                 X    =         4693006
46
 Y    =       13006439
29  feet           Y    =         3964362
70  meter
 Z    =        8831241
00                 Z    =         2691762
26
 XDOT =     -15830
638306                 XDOT =       -4825
178556
 YDOT =       7150
892305  feet/sec       YDOT =        2179
591975  meter/sec
 ZDOT =      17047
509355                 ZDOT =        5196
080852


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   07170
51624671  
00020000  00000-0  20000-3 0  9040
2 25544  51
6330  91
8721 0008548 338
3300  21
7503 15
78295356 11149


Satellite: ISS
Catalog Number: 25544
Epoch time:      07170
51624671   =   yrday
fracday
Element set:     904
Inclination:       51
6330  deg
RA of node:        91
8721  deg
Eccentricity:     
0008548     
Arg of perigee:   338
3300  deg
Mean anomaly:      21
7503  deg
Mean motion:   15
78295356  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1114
Checksum:              271


Coasting Arc #6 (Orbit 1128)
---------------------------------------

Vector Time (GMT): 2007/171/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3162059
45                 A    =         6714159
58  meter
 Y    =        4667220
34  meter          E    =           
0007721
 Z    =       -3642603
54                 I    =           51
95398
 XDOT =      -3090
535810                 Wp   =           21
11595
 YDOT =       5521
186679  meter/sec      RA   =           86
25695  deg
 ZDOT =       4401
310576                 TA   =          295
32234
                                          MA   =          295
40230
                                          Ha   =            184
758  n
mi
                                          Hp   =            177
376

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10374210
78                 X    =         3127329
82
 Y    =       15312402
70  feet           Y    =         4702386
62  meter
 Z    =      -11950799
02                 Z    =        -3627326
08
 XDOT =     -10139
553184                 XDOT =       -3173
425379
 YDOT =      18114
129524  feet/sec       YDOT =        5486
162463  meter/sec
 ZDOT =      14439
995327                 ZDOT =        4386
096387

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17739305
77                 X    =         5406940
40
 Y    =       -5366621
65  feet           Y    =        -1635746
28  meter
 Z    =      -11892515
54                 Z    =        -3624838
74
 XDOT =      13822
642355                 XDOT =        4213
141390
 YDOT =      13889
799786  feet/sec       YDOT =        4233
610975  meter/sec
 ZDOT =      14383
103105                 ZDOT =        4383
969826


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   07171
46598707  
00020000  00000-0  20000-3 0  9056
2 25544  51
6331  86
9628 0008602 341
5671  18
5181 15
78319444 11296


Satellite: ISS
Catalog Number: 25544
Epoch time:      07171
46598707   =   yrday
fracday
Element set:     905
Inclination:       51
6331  deg
RA of node:        86
9628  deg
Eccentricity:     
0008602     
Arg of perigee:   341
5671  deg
Mean anomaly:      18
5181  deg
Mean motion:   15
78319444  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1129
Checksum:              304


Coasting Arc #7 (Orbit 1144)
---------------------------------------

Vector Time (GMT): 2007/172/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3144390
35                 A    =         6710282
60  meter
 Y    =       -3648723
44  meter          E    =           
0014561
 Z    =       -4684391
83                 I    =           51
93880
 XDOT =       3224
094907                 Wp   =           34
49104
 YDOT =       6398
778206  meter/sec      RA   =           81
15720  deg
 ZDOT =      -2812
396475                 TA   =          207
82101
                                          MA   =          207
89896
                                          Ha   =            184
774  n
mi
                                          Hp   =            177
140

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10316241
30                 X    =         3207712
98
 Y    =      -11970877
44  feet           Y    =        -3613206
42  meter
 Z    =      -15368739
60                 Z    =        -4668963
17
 XDOT =      10577
739197                 XDOT =        3165
965226
 YDOT =      20993
366818  feet/sec       YDOT =        6434
507206  meter/sec
 ZDOT =      -9227
022556                 ZDOT =       -2796
874263

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8530321
03                 X    =        -2600041
85
 Y    =      -13369265
29  feet           Y    =        -4074952
06  meter
 Z    =      -15310821
89                 Z    =        -4666738
51
 XDOT =      22170
683605                 XDOT =        6757
624363
 YDOT =      -3618
782651  feet/sec       YDOT =       -1103
004952  meter/sec
 ZDOT =      -9167
618838                 ZDOT =       -2794
290222


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   07172
47902602  
00020000  00000-0  20000-3 0  9062
2 25544  51
6337  81
7258 0008612 345
9486  14
1439 15
78366710 11451


Satellite: ISS
Catalog Number: 25544
Epoch time:      07172
47902602   =   yrday
fracday
Element set:     906
Inclination:       51
6337  deg
RA of node:        81
7258  deg
Eccentricity:     
0008612     
Arg of perigee:   345
9486  deg
Mean anomaly:      14
1439  deg
Mean motion:   15
78366710  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1145
Checksum:              295


Coasting Arc #8 (Orbit 1160)
---------------------------------------

Vector Time (GMT): 2007/173/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2401785
30                 A    =         6719281
74  meter
 Y    =       -6183697
47  meter          E    =           
0009916
 Z    =        1063484
21                 I    =           51
96372
 XDOT =       4133
107187                 Wp   =           85
44662
 YDOT =      -2635
485711  meter/sec      RA   =           75
97823  deg
 ZDOT =      -5942
060965                 TA   =           82
95934
                                          MA   =           82
84658
                                          Ha   =            184
863  n
mi
                                          Hp   =            176
907

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7879873
03                 X    =        -2337625
98
 Y    =      -20287721
36  feet           Y    =        -6210196
99  meter
 Z    =        3489121
44                 Z    =         1051971
41
 XDOT =      13560
062949                 XDOT =        4191
135758
 YDOT =      -8646
606665  feet/sec       YDOT =       -2588
941754  meter/sec
 ZDOT =     -19494
950671                 ZDOT =       -5921
841784

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21660301
00                 X    =        -6602059
75
 Y    =        2195907
10  feet           Y    =          669312
48  meter
 Z    =        3444903
19                 Z    =         1050006
49
 XDOT =      -4523
069447                 XDOT =       -1378
631567
 YDOT =     -13901
781607  feet/sec       YDOT =       -4237
263034  meter/sec
 ZDOT =     -19418
804789                 ZDOT =       -5918
851700


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   07173
49204728  
00020000  00000-0  20000-3 0  9070
2 25544  51
6340  76
4887 0008583 349
3640  10
7343 15
78372298 11613


Satellite: ISS
Catalog Number: 25544
Epoch time:      07173
49204728   =   yrday
fracday
Element set:     907
Inclination:       51
6340  deg
RA of node:        76
4887  deg
Eccentricity:     
0008583     
Arg of perigee:   349
3640  deg
Mean anomaly:      10
7343  deg
Mean motion:   15
78372298  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1161
Checksum:              305


Coasting Arc #9 (Orbit 1176)
---------------------------------------

Vector Time (GMT): 2007/174/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4066493
23                 A    =         6707534
82  meter
 Y    =         863589
46  meter          E    =           
0009636
 Z    =        5263458
83                 I    =           51
91647
 XDOT =      -2179
916061                 Wp   =            7
60452
 YDOT =      -7380
042707  meter/sec      RA   =           70
83642  deg
 ZDOT =       -463
866300                 TA   =           86
83481
                                          MA   =           86
72457
                                          Ha   =            184
967  n
mi
                                          Hp   =            176
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13341513
24                 X    =        -4101416
74
 Y    =        2833298
77  feet           Y    =          817919
67  meter
 Z    =       17268565
70                 Z    =         5243619
07
 XDOT =      -7151
955582                 XDOT =       -2094
975946
 YDOT =     -24212
738539  feet/sec       YDOT =       -7403
944765  meter/sec
 ZDOT =      -1521
871062                 ZDOT =        -474
251027

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -621501
96                 X    =         -189433
80
 Y    =       13719289
93  feet           Y    =         4181639
57  meter
 Z    =       17193654
00                 Z    =         5240625
74
 XDOT =     -24229
614490                 XDOT =       -7385
186496
 YDOT =        898
906983  feet/sec       YDOT =         273
986848  meter/sec
 ZDOT =      -1561
951926                 ZDOT =        -476
082947


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   07174
50504879  
00020000  00000-0  20000-3 0  9084
2 25544  51
6340  71
2518 0008666 352
0704   8
0323 15
78445174 11770


Satellite: ISS
Catalog Number: 25544
Epoch time:      07174
50504879   =   yrday
fracday
Element set:     908
Inclination:       51
6340  deg
RA of node:        71
2518  deg
Eccentricity:     
0008666     
Arg of perigee:   352
0704  deg
Mean anomaly:       8
0323  deg
Mean motion:   15
78445174  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1177
Checksum:              286


Coasting Arc #10 (Orbit 1192)
---------------------------------------

Vector Time (GMT): 2007/175/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1272097
06                 A    =         6718141
67  meter
 Y    =        6321839
55  meter          E    =           
0019022
 Z    =        1840821
24                 I    =           51
94194
 XDOT =      -5171
358964                 Wp   =           40
72266
 YDOT =       -622
599370  meter/sec      RA   =           65
70840  deg
 ZDOT =       5693
285914                 TA   =          339
68016
                                          MA   =          339
75575
                                          Ha   =            185
081  n
mi
                                          Hp   =            176
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4173546
78                 X    =         1192368
37
 Y    =       20740943
42  feet           Y    =         6335618
80  meter
 Z    =        6039439
78                 Z    =         1846808
39
 XDOT =     -16966
400801                 XDOT =       -5191
669681
 YDOT =      -2042
648851  feet/sec       YDOT =        -680
542817  meter/sec
 ZDOT =      18678
759560                 ZDOT =        5668
113919

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21134039
94                 X    =         6441655
37
 Y    =         821726
17  feet           Y    =          250462
14  meter
 Z    =        6062770
11                 Z    =         1847932
33
 XDOT =      -5915
353268                 XDOT =       -1802
999676
 YDOT =      14579
551928  feet/sec       YDOT =        4443
847428  meter/sec
 ZDOT =      18583
522487                 ZDOT =        5664
257654


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   07175
51803597  
00020000  00000-0  20000-3 0  9096
2 25544  51
6346  66
0144 0008723 356
7889   3
3218 15
78422218 11935


Satellite: ISS
Catalog Number: 25544
Epoch time:      07175
51803597   =   yrday
fracday
Element set:     909
Inclination:       51
6346  deg
RA of node:        66
0144  deg
Eccentricity:     
0008723     
Arg of perigee:   356
7889  deg
Mean anomaly:       3
3218  deg
Mean motion:   15
78422218  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1193
Checksum:              303


Coasting Arc #11 (Orbit 1207)
---------------------------------------

Vector Time (GMT): 2007/176/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4864198
05                 A    =         6711726
86  meter
 Y    =        1844343
74  meter          E    =           
0009698
 Z    =       -4243783
71                 I    =           51
90830
 XDOT =        575
483729                 Wp   =           52
86623
 YDOT =       6778
219414  meter/sec      RA   =           60
51682  deg
 ZDOT =       3616
770152                 TA   =          253
69891
                                          MA   =          253
80559
                                          Ha   =            185
174  n
mi
                                          Hp   =            176
253

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15958655
01                 X    =         4863828
46
 Y    =        6050996
54  feet           Y    =         1898736
57  meter
 Z    =      -13923174
91                 Z    =        -4220153
89
 XDOT =       1888
069976                 XDOT =         482
076196
 YDOT =      22238
252669  feet/sec       YDOT =        6784
131928  meter/sec
 ZDOT =      11866
043806                 ZDOT =        3619
340105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9385606
99                 X    =         2860733
01
 Y    =      -14341860
57  feet           Y    =        -4371399
10  meter
 Z    =      -13833634
56                 Z    =        -4216491
82
 XDOT =      21058
023649                 XDOT =        6418
485608
 YDOT =       2361
310650  feet/sec       YDOT =         719
727486  meter/sec
 ZDOT =      11876
495748                 ZDOT =        3619
955904


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   07176
46769283  
00020000  00000-0  20000-3 0  9106
2 25544  51
6353  61
1048 0008725 359
7171    
3988 15
78463540 12082


Satellite: ISS
Catalog Number: 25544
Epoch time:      07176
46769283   =   yrday
fracday
Element set:     910
Inclination:       51
6353  deg
RA of node:        61
1048  deg
Eccentricity:     
0008725     
Arg of perigee:   359
7171  deg
Mean anomaly:        
3988  deg
Mean motion:   15
78463540  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1208
Checksum:              300


Coasting Arc #12 (Orbit 1223)
---------------------------------------

Vector Time (GMT): 2007/177/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         430745
87                 A    =         6711634
46  meter
 Y    =       -5210367
02  meter          E    =           
0014266
 Z    =       -4223136
39                 I    =           51
89360
 XDOT =       5841
759258                 Wp   =           35
00746
 YDOT =       3439
873065  meter/sec      RA   =           55
41576  deg
 ZDOT =      -3642
759579                 TA   =          197
98704
                                          MA   =          198
03757
                                          Ha   =            185
142  n
mi
                                          Hp   =            175
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1413208
24                 X    =          509492
31
 Y    =      -17094380
00  feet           Y    =        -5205109
11  meter
 Z    =      -13855434
34                 Z    =        -4220853
50
 XDOT =      19165
876831                 XDOT =        5820
555898
 YDOT =      11285
672787  feet/sec       YDOT =        3505
081018  meter/sec
 ZDOT =     -11951
310954                 ZDOT =       -3614
430990

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16450322
55                 X    =        -5014058
31
 Y    =       -4881140
39  feet           Y    =        -1487771
59  meter
 Z    =      -13847360
84                 Z    =        -4220675
58
 XDOT =      14549
925982                 XDOT =        4434
817439
 YDOT =     -15385
654843  feet/sec       YDOT =       -4689
547596  meter/sec
 ZDOT =     -11843
833362                 ZDOT =       -3610
000409


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   07177
48064357  
00020000  00000-0  20000-3 0  9110
2 25544  51
6358  55
8677 0008763   2
9635 357
1581 15
78500226 12242


Satellite: ISS
Catalog Number: 25544
Epoch time:      07177
48064357   =   yrday
fracday
Element set:     911
Inclination:       51
6358  deg
RA of node:        55
8677  deg
Eccentricity:     
0008763     
Arg of perigee:     2
9635  deg
Mean anomaly:     357
1581  deg
Mean motion:   15
78500226  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1224
Checksum:              304

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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