Date:
November 2nd 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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 3234)
---------------------------------------
Vector Time (GMT): 2007/304/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4743323
81 A = 6717948
36 meter
Y = -1238762
14 meter E =
0011059
Z = -4602890
21 I = 51
91372
XDOT = -1068
341495 Wp = 86
82906
YDOT = 7008
495311 meter/sec RA = 117
98611 deg
ZDOT = -2992
647499 TA = 153
58875
MA = 153
53234
Ha = 188
073 n
mi
Hp = 180
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15562085
98 X = 4779183
59
Y = -4064180
25 feet Y = -1185518
89 meter
Z = -15101345
83 Z = -4579759
80
XDOT = -3505
057398 XDOT = -1132
094218
YDOT = 22993
751020 feet/sec YDOT = 6996
192193 meter/sec
ZDOT = -9818
397306 ZDOT = -2997
992095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14591575
88 X = 4447512
33
Y = -6959025
62 feet Y = -2121111
01 meter
Z = -15013480
70 Z = -4576108
92
XDOT = 468
157630 XDOT = 142
694445
YDOT = 22166
610079 feet/sec YDOT = 6756
382752 meter/sec
ZDOT = -9837
899200 ZDOT = -2998
591676
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 07304
94294243
00020000 00000-0 20000-3 0 9000
2 25544 51
6391 118
7151 0003192 156
1456 203
9856 15
75799833 32357
Satellite: ISS
Catalog Number: 25544
Epoch time: 07304
94294243 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 118
7151 deg
Eccentricity:
0003192
Arg of perigee: 156
1456 deg
Mean anomaly: 203
9856 deg
Mean motion: 15
75799833 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3235
Checksum: 299
Coasting Arc #2 (Orbit 3250)
---------------------------------------
Vector Time (GMT): 2007/305/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 922070
13 A = 6725073
70 meter
Y = -6329193
75 meter E =
0016355
Z = 2049805
88 I = 51
94957
XDOT = 5196
784095 Wp = 118
82918
YDOT = -1062
736989 meter/sec RA = 112
81622 deg
ZDOT = -5593
493328 TA = 38
36799
MA = 38
25177
Ha = 187
916 n
mi
Hp = 180
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3025164
46 X = 982817
90
Y = -20765071
37 feet Y = -6318543
04 meter
Z = 6725084
92 Z = 2054432
74
XDOT = 17049
816584 XDOT = 5235
454026
YDOT = -3486
669911 feet/sec YDOT = -1004
407243 meter/sec
ZDOT = -18351
356063 ZDOT = -5568
153166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1367129
85 X = -416701
18
Y = -20934272
81 feet Y = -6380766
35 meter
Z = 6741939
93 Z = 2054943
29
XDOT = 14536
000739 XDOT = 4430
573025
YDOT = -6855
365601 feet/sec YDOT = -2089
515435 meter/sec
ZDOT = -18255
053243 ZDOT = -5564
140228
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 07305
95759932
00020000 00000-0 20000-3 0 9014
2 25544 51
6379 113
4899 0003065 157
8059 202
3238 15
75853448 32518
Satellite: ISS
Catalog Number: 25544
Epoch time: 07305
95759932 = yrday
fracday
Element set: 901
Inclination: 51
6379 deg
RA of node: 113
4899 deg
Eccentricity:
0003065
Arg of perigee: 157
8059 deg
Mean anomaly: 202
3238 deg
Mean motion: 15
75853448 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3251
Checksum: 314
Coasting Arc #3 (Orbit 3266)
---------------------------------------
Vector Time (GMT): 2007/306/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4354679
89 A = 6715660
65 meter
Y = 557043
69 meter E =
0007724
Z = 5079060
54 I = 51
92763
XDOT = 1006
166733 Wp = 138
74734
YDOT = -7455
268958 meter/sec RA = 107
71968 deg
ZDOT = 1673
202739 TA = 295
20355
MA = 295
28362
Ha = 187
892 n
mi
Hp = 180
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14287007
52 X = -4385258
64
Y = 1827571
15 feet Y = 508176
18 meter
Z = 16663584
44 Z = 5057830
98
XDOT = 3301
071960 XDOT = 1081
329682
YDOT = -24459
543825 feet/sec YDOT = -7443
597187 meter/sec
ZDOT = 5489
510298 ZDOT = 1678
273272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13608961
91 X = -4148011
59
Y = 4993855
30 feet Y = 1522127
10 meter
Z = 16582858
97 Z = 5054455
41
XDOT = -1912
472917 XDOT = -582
921745
YDOT = -23579
570679 feet/sec YDOT = -7187
053143 meter/sec
ZDOT = 5507
923279 ZDOT = 1678
815015
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 07306
97222613
00020000 00000-0 20000-3 0 9029
2 25544 51
6374 108
2643 0002958 162
0325 198
0945 15
75887313 32677
Satellite: ISS
Catalog Number: 25544
Epoch time: 07306
97222613 = yrday
fracday
Element set: 902
Inclination: 51
6374 deg
RA of node: 108
2643 deg
Eccentricity:
0002958
Arg of perigee: 162
0325 deg
Mean anomaly: 198
0945 deg
Mean motion: 15
75887313 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3267
Checksum: 298
Coasting Arc #4 (Orbit 3281)
---------------------------------------
Vector Time (GMT): 2007/307/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -813548
86 A = 6726227
78 meter
Y = 6622687
41 meter E =
0008819
Z = -827672
94 I = 51
97230
XDOT = -4834
773024 Wp = 54
83524
YDOT = 148
808995 meter/sec RA = 102
57028 deg
ZDOT = 5992
468029 TA = 296
17404
MA = 296
26470
Ha = 187
560 n
mi
Hp = 180
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2669123
57 X = -883523
54
Y = 21727977
06 feet Y = 6613198
59 meter
Z = -2715462
41 Z = -831795
24
XDOT = -15862
116221 XDOT = -4865
188444
YDOT = 488
218489 feet/sec YDOT = 94
573809 meter/sec
ZDOT = 19660
328178 ZDOT = 5968
906482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2641322
57 X = 805075
12
Y = 21729506
28 feet Y = 6623153
51 meter
Z = -2730369
21 Z = -832216
53
XDOT = -13803
511019 XDOT = -4207
310159
YDOT = 4116
695584 feet/sec YDOT = 1254
768814 meter/sec
ZDOT = 19570
676006 ZDOT = 5965
142047
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 07307
92341062
00020000 00000-0 20000-3 0 9036
2 25544 51
6379 103
3662 0003005 166
5432 193
5813 15
75984183 32825
Satellite: ISS
Catalog Number: 25544
Epoch time: 07307
92341062 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 103
3662 deg
Eccentricity:
0003005
Arg of perigee: 166
5432 deg
Mean anomaly: 193
5813 deg
Mean motion: 15
75984183 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3282
Checksum: 283
Coasting Arc #5 (Orbit 3297)
---------------------------------------
Vector Time (GMT): 2007/308/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4133851
64 A = 6714518
12 meter
Y = 350956
37 meter E =
0015613
Z = -5292590
06 I = 51
93664
XDOT = -864
359640 Wp = 98
59062
YDOT = 7642
347157 meter/sec RA = 97
45072 deg
ZDOT = -171
054190 TA = 169
80692
MA = 169
77522
Ha = 187
454 n
mi
Hp = 180
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13562505
39 X = 4155330
88
Y = 1151431
64 feet Y = 397303
45 meter
Z = -17364140
63 Z = -5272455
28
XDOT = -2835
825589 XDOT = -948
922311
YDOT = 25073
317443 feet/sec YDOT = 7632
208581 meter/sec
ZDOT = -561
201411 ZDOT = -175
458856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13497729
47 X = 4114107
94
Y = -2394875
23 feet Y = -729957
97 meter
Z = -17287469
42 Z = -5269220
68
XDOT = 3526
279092 XDOT = 1074
809867
YDOT = 23975
664178 feet/sec YDOT = 7307
782441 meter/sec
ZDOT = -577
068529 ZDOT = -175
890488
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 07308
93797787
00020000 00000-0 20000-3 0 9048
2 25544 51
6370 98
1397 0002706 171
7746 188
3463 15
75965530 32980
Satellite: ISS
Catalog Number: 25544
Epoch time: 07308
93797787 = yrday
fracday
Element set: 904
Inclination: 51
6370 deg
RA of node: 98
1397 deg
Eccentricity:
0002706
Arg of perigee: 171
7746 deg
Mean anomaly: 188
3463 deg
Mean motion: 15
75965530 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3298
Checksum: 340
Coasting Arc #6 (Orbit 3313)
---------------------------------------
Vector Time (GMT): 2007/309/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 696019
02 A = 6726280
65 meter
Y = -6661197
45 meter E =
0013254
Z = -543762
21 I = 51
97891
XDOT = 4685
986298 Wp = 145
37079
YDOT = 975
911799 meter/sec RA = 92
32552 deg
ZDOT = -6038
950649 TA = 40
52517
MA = 40
42656
Ha = 187
309 n
mi
Hp = 180
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2283526
97 X = 773095
37
Y = -21854322
35 feet Y = -6652983
22 meter
Z = -1783996
74 Z = -540193
54
XDOT = 15373
970794 XDOT = 4704
062036
YDOT = 3201
810365 feet/sec YDOT = 1028
414122 meter/sec
ZDOT = -19812
830214 ZDOT = -6016
141714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3768261
27 X = -1148566
04
Y = -21648825
41 feet Y = -6598561
98 meter
Z = -1771188
99 Z = -539858
40
XDOT = 14192
108372 XDOT = 4325
754632
YDOT = -878
605038 feet/sec YDOT = -267
798816 meter/sec
ZDOT = -19725
908059 ZDOT = -6012
456777
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 07309
95251411
00020000 00000-0 20000-3 0 9051
2 25544 51
6365 92
9130 0002546 173
6503 186
4694 15
76030671 33149
Satellite: ISS
Catalog Number: 25544
Epoch time: 07309
95251411 = yrday
fracday
Element set: 905
Inclination: 51
6365 deg
RA of node: 92
9130 deg
Eccentricity:
0002546
Arg of perigee: 173
6503 deg
Mean anomaly: 186
4694 deg
Mean motion: 15
76030671 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3314
Checksum: 282
Coasting Arc #7 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2007/310/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4097192
37 A = 6714826
09 meter
Y = -1355328
95 meter E =
0003599
Z = 5141388
02 I = 51
94021
XDOT = 730
169963 Wp = 86
92828
YDOT = -7542
796520 meter/sec RA = 87
17958 deg
ZDOT = -1405
466249 TA = 16
46893
MA = 16
45724
Ha = 187
222 n
mi
Hp = 180
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13442232
18 X = -4106708
98
Y = -4446617
28 feet Y = -1401199
25 meter
Z = 16868070
94 Z = 5121460
21
XDOT = 2395
570745 XDOT = 821
288072
YDOT = -24746
707744 feet/sec YDOT = -7534
121890 meter/sec
ZDOT = -4611
109742 ZDOT = -1401
697597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14244795
73 X = -4341813
74
Y = -331619
90 feet Y = -101077
75 meter
Z = 16792071
09 Z = 5118223
27
XDOT = -4880
247557 XDOT = -1487
499455
YDOT = -23347
335955 feet/sec YDOT = -7116
267999 meter/sec
ZDOT = -4597
632804 ZDOT = -1401
358479
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 07310
96701835
00020000 00000-0 20000-3 0 9065
2 25544 51
6361 87
6865 0002408 181
2806 178
8352 15
76079158 33306
Satellite: ISS
Catalog Number: 25544
Epoch time: 07310
96701835 = yrday
fracday
Element set: 906
Inclination: 51
6361 deg
RA of node: 87
6865 deg
Eccentricity:
0002408
Arg of perigee: 181
2806 deg
Mean anomaly: 178
8352 deg
Mean motion: 15
76079158 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3330
Checksum: 303
Coasting Arc #8 (Orbit 3345)
---------------------------------------
Vector Time (GMT): 2007/311/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -609602
75 A = 6724427
82 meter
Y = 6415624
33 meter E =
0013131
Z = 1902324
67 I = 51
97110
XDOT = -4768
030820 Wp = 76
62525
YDOT = -2140
413044 meter/sec RA = 82
07995 deg
ZDOT = 5661
207566 TA = 304
43879
MA = 304
56282
Ha = 186
896 n
mi
Hp = 180
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2000009
01 X = -690539
35
Y = 21048636
26 feet Y = 6408354
85 meter
Z = 6241222
66 Z = 1899166
57
XDOT = -15643
145736 XDOT = -4771
243997
YDOT = -7022
352506 feet/sec YDOT = -2193
749873 meter/sec
ZDOT = 18573
515635 ZDOT = 5638
035936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4509897
47 X = 1374616
75
Y = 20660270
80 feet Y = 6297250
54 meter
Z = 6229929
34 Z = 1898882
46
XDOT = -15635
011917 XDOT = -4765
551632
YDOT = -2190
267464 feet/sec YDOT = -667
593523 meter/sec
ZDOT = 18485
082051 ZDOT = 5634
253009
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 07311
98148951
00020000 00000-0 20000-3 0 9073
2 25544 51
6364 82
4605 0002500 185
8211 174
2925 15
76176614 33465
Satellite: ISS
Catalog Number: 25544
Epoch time: 07311
98148951 = yrday
fracday
Element set: 907
Inclination: 51
6364 deg
RA of node: 82
4605 deg
Eccentricity:
0002500
Arg of perigee: 185
8211 deg
Mean anomaly: 174
2925 deg
Mean motion: 15
76176614 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3346
Checksum: 290
Coasting Arc #9 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2007/312/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4268576
89 A = 6716846
81 meter
Y = 2366107
97 meter E =
0011134
Z = -4625721
57 I = 51
94022
XDOT = -725
135881 Wp = 120
60903
YDOT = 7070
960273 meter/sec RA = 76
91014 deg
ZDOT = 2947
399428 TA = 178
50164
MA = 178
49830
Ha = 186
829 n
mi
Hp = 180
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14004517
36 X = 4264273
12
Y = 7762821
43 feet Y = 2413817
67 meter
Z = -15176251
89 Z = -4604994
53
XDOT = -2379
054727 XDOT = -818
468939
YDOT = 23198
688559 feet/sec YDOT = 7062
329464 meter/sec
ZDOT = 9669
945630 ZDOT = 2943
650072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15840868
94 X = 4828296
85
Y = 2801960
21 feet Y = 854037
47 meter
Z = -15097099
54 Z = -4601595
94
XDOT = 5385
552662 XDOT = 1641
516451
YDOT = 21588
094764 feet/sec YDOT = 6580
051284 meter/sec
ZDOT = 9656
463032 ZDOT = 2943
289932
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 07312
93253091
00020000 00000-0 20000-3 0 9082
2 25544 51
6366 77
5601 0002125 189
1247 170
9879 15
76151335 33618
Satellite: ISS
Catalog Number: 25544
Epoch time: 07312
93253091 = yrday
fracday
Element set: 908
Inclination: 51
6366 deg
RA of node: 77
5601 deg
Eccentricity:
0002125
Arg of perigee: 189
1247 deg
Mean anomaly: 170
9879 deg
Mean motion: 15
76151335 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3361
Checksum: 292
Coasting Arc #10 (Orbit 3376)
---------------------------------------
Vector Time (GMT): 2007/313/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 720251
09 A = 6721351
76 meter
Y = -5861513
59 meter E =
0004857
Z = -3210008
99 I = 51
94928
XDOT = 5042
594918 Wp = 122
48061
YDOT = 3256
795701 meter/sec RA = 71
82638 deg
ZDOT = -4823
309549 TA = 94
85319
MA = 94
79773
Ha = 186
658 n
mi
Hp = 180
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2363028
52 X = 801336
06
Y = -19230687
63 feet Y = -5853005
82 meter
Z = -10531525
55 Z = -3206313
20
XDOT = 16543
946582 XDOT = 5029
233711
YDOT = 10685
025267 feet/sec YDOT = 3313
110371 meter/sec
ZDOT = -15824
506395 ZDOT = -4798
844101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4237574
64 X = -1291612
75
Y = -18913719
89 feet Y = -5764901
82 meter
Z = -10518100
68 Z = -3205917
09
XDOT = 17890
327196 XDOT = 5452
971729
YDOT = 4725
634389 feet/sec YDOT = 1440
373362 meter/sec
ZDOT = -15731
029273 ZDOT = -4794
817722
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 07313
94694205
00020000 00000-0 20000-3 0 9091
2 25544 51
6375 72
3331 0001982 193
3614 166
7498 15
76231702 33770
Satellite: ISS
Catalog Number: 25544
Epoch time: 07313
94694205 = yrday
fracday
Element set: 909
Inclination: 51
6375 deg
RA of node: 72
3331 deg
Eccentricity:
0001982
Arg of perigee: 193
3614 deg
Mean anomaly: 166
7498 deg
Mean motion: 15
76231702 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3377
Checksum: 303
Coasting Arc #11 (Orbit 3392)
---------------------------------------
Vector Time (GMT): 2007/314/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4560485
66 A = 6719810
86 meter
Y = -3258544
40 meter E =
0011136
Z = 3696706
62 I = 51
93432
XDOT = 977
959292 Wp = 93
04860
YDOT = -6298
274829 meter/sec RA = 66
64453 deg
ZDOT = -4334
743270 TA = 42
57948
MA = 42
49319
Ha = 186
564 n
mi
Hp = 180
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14962223
30 X = -4541667
70
Y = -10690762
45 feet Y = -3309437
36 meter
Z = 12128302
55 Z = 3674596
55
XDOT = 3208
527861 XDOT = 1069
372954
YDOT = -20663
631328 feet/sec YDOT = -6286
827326 meter/sec
ZDOT = -14221
598656 ZDOT = -4329
770557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17846550
30 X = -5439628
53
Y = -4658749
97 feet Y = -1419986
99 meter
Z = 12043792
66 Z = 3670948
00
XDOT = -4600
844866 XDOT = -1402
337515
YDOT = -19183
771445 feet/sec YDOT = -5847
213537 meter/sec
ZDOT = -14203
349099 ZDOT = -4329
180805
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 07314
96132103
00020000 00000-0 20000-3 0 9100
2 25544 51
6377 67
1067 0001877 201
7092 158
3993 15
76282188 33936
Satellite: ISS
Catalog Number: 25544
Epoch time: 07314
96132103 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 67
1067 deg
Eccentricity:
0001877
Arg of perigee: 201
7092 deg
Mean anomaly: 158
3993 deg
Mean motion: 15
76282188 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3393
Checksum: 298
Coasting Arc #12 (Orbit 3408)
---------------------------------------
Vector Time (GMT): 2007/315/22:07:24
088
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1064744
66 A = 6717516
78 meter
Y = 5067987
50 meter E =
0009745
Z = 4274326
68 I = 51
91580
XDOT = -5425
147011 Wp = 119
14950
YDOT = -4154
109786 meter/sec RA = 61
56318 deg
ZDOT = 3563
328936 TA = 294
82266
MA = 294
92398
Ha = 186
296 n
mi
Hp = 180
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3493256
75 X = -1142101
06
Y = 16627255
58 feet Y = 5055648
04 meter
Z = 14023381
49 Z = 4268966
52
XDOT = -17799
038751 XDOT = -5395
602445
YDOT = -13628
969115 feet/sec YDOT = -4214
611961 meter/sec
ZDOT = 11690
711732 ZDOT = 3537
044187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2851897
17 X = 869258
26
Y = 16765796
78 feet Y = 5110214
86 meter
Z = 14003515
29 Z = 4268271
46
XDOT = -20423
618392 XDOT = -6225
118886
YDOT = -6235
918705 feet/sec YDOT = -1900
708021 meter/sec
ZDOT = 11590
216603 ZDOT = 3532
698021
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 07315
97566674
00020000 00000-0 20000-3 0 9117
2 25544 51
6387 61
8803 0001975 207
5756 152
5304 15
76362186 34093
Satellite: ISS
Catalog Number: 25544
Epoch time: 07315
97566674 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 61
8803 deg
Eccentricity:
0001975
Arg of perigee: 207
5756 deg
Mean anomaly: 152
5304 deg
Mean motion: 15
76362186 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3409
Checksum: 312
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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