Date:
June 10th 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 937)
---------------------------------------
Vector Time (GMT): 2007/159/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6130183
23 A = 6718727
87 meter
Y = -1997272
27 meter E =
0003782
Z = -1882542
48 I = 51
81392
XDOT = -34
978413 Wp = 232
44316
YDOT = 5230
312435 meter/sec RA = 148
67705 deg
ZDOT = -5657
531902 TA = 328
44787
MA = 328
47054
Ha = 182
719 n
mi
Hp = 180
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20112149
70 X = 6161206
46
Y = -6552730
54 feet Y = -1928547
44 meter
Z = -6176320
49 Z = -1852686
92
XDOT = -114
758572 XDOT = -65
978653
YDOT = 17159
817701 feet/sec YDOT = 5229
748627 meter/sec
ZDOT = -18561
456373 ZDOT = -5657
776507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16810918
52 X = 5123967
97
Y = -12892123
62 feet Y = -3929519
28 meter
Z = -6063822
61 Z = -1848253
13
XDOT = 4768
256410 XDOT = 1453
364554
YDOT = 14956
732761 feet/sec YDOT = 4558
812145 meter/sec
ZDOT = -18561
736557 ZDOT = -5657
617302
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 07159
37211558
00020000 00000-0 20000-3 0 9003
2 25544 51
6323 149
4668 0008192 294
2706 65
7603 15
78210966 9382
Satellite: ISS
Catalog Number: 25544
Epoch time: 07159
37211558 = yrday
fracday
Element set: 900
Inclination: 51
6323 deg
RA of node: 149
4668 deg
Eccentricity:
0008192
Arg of perigee: 294
2706 deg
Mean anomaly: 65
7603 deg
Mean motion: 15
78210966 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 938
Checksum: 307
Coasting Arc #2 (Orbit 953)
---------------------------------------
Vector Time (GMT): 2007/160/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1208566
62 A = 6712183
02 meter
Y = -5054536
55 meter E =
0007228
Z = 4250329
23 I = 51
81554
XDOT = 6667
709186 Wp = 17
62162
YDOT = -1428
145162 meter/sec RA = 143
47944 deg
ZDOT = -3585
973464 TA = 108
72760
MA = 108
64915
Ha = 182
860 n
mi
Hp = 179
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3965113
59 X = 1244349
92
Y = -16583125
17 feet Y = -5040822
09 meter
Z = 13944649
71 Z = 4256286
82
XDOT = 21875
686306 XDOT = 6700
603459
YDOT = -4685
515624 feet/sec YDOT = -1353
398766 meter/sec
ZDOT = -11765
004803 ZDOT = -3553
501815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2152601
42 X = -656112
91
Y = -16896088
34 feet Y = -5149927
73 meter
Z = 13966528
83 Z = 4256997
99
XDOT = 17688
672091 XDOT = 5391
507253
YDOT = -11900
024973 feet/sec YDOT = -3627
127612 meter/sec
ZDOT = -11642
549998 ZDOT = -3548
649239
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 07160
38523366
00020000 00000-0 20000-3 0 9010
2 25544 51
6315 144
2305 0008290 298
2625 61
7703 15
78254412 9546
Satellite: ISS
Catalog Number: 25544
Epoch time: 07160
38523366 = yrday
fracday
Element set: 901
Inclination: 51
6315 deg
RA of node: 144
2305 deg
Eccentricity:
0008290
Arg of perigee: 298
2625 deg
Mean anomaly: 61
7703 deg
Mean motion: 15
78254412 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 954
Checksum: 278
Coasting Arc #3 (Orbit 969)
---------------------------------------
Vector Time (GMT): 2007/161/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5266533
21 A = 6712708
98 meter
Y = 321775
12 meter E =
0003758
Z = 4145756
43 I = 51
83901
XDOT = 2571
236230 Wp = 62
69408
YDOT = -6225
751419 meter/sec RA = 138
37442 deg
ZDOT = 3748
680680 TA = 349
09700
MA = 349
10515
Ha = 183
171 n
mi
Hp = 179
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17278652
27 X = -5289879
47
Y = 1055692
65 feet Y = 262750
74 meter
Z = 13601563
08 Z = 4120114
67
XDOT = 8435
814404 XDOT = 2622
451790
YDOT = -20425
693631 feet/sec YDOT = -6196
712520 meter/sec
ZDOT = 12298
821130 ZDOT = 3761
295505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15767890
79 X = -4806053
11
Y = 7325565
14 feet Y = 2232832
26 meter
Z = 13504760
07 Z = 4116250
87
XDOT = 856
715858 XDOT = 261
126994
YDOT = -20920
811177 feet/sec YDOT = -6376
663247 meter/sec
ZDOT = 12345
706204 ZDOT = 3762
971251
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 07161
39833691
00020000 00000-0 20000-3 0 9028
2 25544 51
6311 138
9933 0008081 302
9453 57
0935 15
78247439 9703
Satellite: ISS
Catalog Number: 25544
Epoch time: 07161
39833691 = yrday
fracday
Element set: 902
Inclination: 51
6311 deg
RA of node: 138
9933 deg
Eccentricity:
0008081
Arg of perigee: 302
9453 deg
Mean anomaly: 57
0935 deg
Mean motion: 15
78247439 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 970
Checksum: 303
Coasting Arc #4 (Orbit 984)
---------------------------------------
Vector Time (GMT): 2007/162/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3072117
82 A = 6718095
33 meter
Y = 5608911
71 meter E =
0010050
Z = -2036091
36 I = 51
87963
XDOT = -5236
430412 Wp = 347
16098
YDOT = -837
874096 meter/sec RA = 133
17763 deg
ZDOT = 5597
121781 TA = 350
15656
MA = 350
17623
Ha = 183
107 n
mi
Hp = 179
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10079126
71 X = -3124718
06
Y = 18401941
30 feet Y = 5574263
76 meter
Z = -6680089
76 Z = -2051142
85
XDOT = -17179
889804 XDOT = -5253
862184
YDOT = -2748
930760 feet/sec YDOT = -896
529097 meter/sec
ZDOT = 18363
260437 ZDOT = 5571
640371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2262880
02 X = -689725
83
Y = 20840968
22 feet Y = 6352327
11 meter
Z = -6736264
24 Z = -2053213
34
XDOT = -15504
407849 XDOT = -4725
743513
YDOT = 4216
241650 feet/sec YDOT = 1285
110455 meter/sec
ZDOT = 18266
916619 ZDOT = 5567
756185
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 07162
34810412
00020000 00000-0 20000-3 0 9031
2 25544 51
6320 134
0842 0008095 306
0745 53
9670 15
78309250 9850
Satellite: ISS
Catalog Number: 25544
Epoch time: 07162
34810412 = yrday
fracday
Element set: 903
Inclination: 51
6320 deg
RA of node: 134
0842 deg
Eccentricity:
0008095
Arg of perigee: 306
0745 deg
Mean anomaly: 53
9670 deg
Mean motion: 15
78309250 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 985
Checksum: 273
Coasting Arc #5 (Orbit 1000)
---------------------------------------
Vector Time (GMT): 2007/163/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3747123
53 A = 6708088
49 meter
Y = 1888996
39 meter E =
0010798
Z = -5241365
36 I = 51
86430
XDOT = -4255
032711 Wp = 51
28510
YDOT = 6376
641240 meter/sec RA = 128
05058 deg
ZDOT = -738
229350 TA = 211
68238
MA = 211
74741
Ha = 183
403 n
mi
Hp = 179
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12293712
37 X = 3751183
99
Y = 6197494
73 feet Y = 1930922
48 meter
Z = -17196080
59 Z = -5223151
35
XDOT = -13960
081072 XDOT = -4322
434761
YDOT = 20920
738976 feet/sec YDOT = 6328
682347 meter/sec
ZDOT = -2422
012303 ZDOT = -759
063189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13832140
44 X = 4216036
41
Y = 765058
93 feet Y = 233189
96 meter
Z = -17127056
62 Z = -5220326
86
XDOT = -4430
862793 XDOT = -1350
526979
YDOT = 23730
938629 feet/sec YDOT = 7233
190094 meter/sec
ZDOT = -2499
951856 ZDOT = -761
985326
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 07163
36117234
00020000 00000-0 20000-3 0 9047
2 25544 51
6319 128
8473 0008216 309
9174 50
1269 15
78292254 10010
Satellite: ISS
Catalog Number: 25544
Epoch time: 07163
36117234 = yrday
fracday
Element set: 904
Inclination: 51
6319 deg
RA of node: 128
8473 deg
Eccentricity:
0008216
Arg of perigee: 309
9174 deg
Mean anomaly: 50
1269 deg
Mean motion: 15
78292254 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1001
Checksum: 279
Coasting Arc #6 (Orbit 1016)
---------------------------------------
Vector Time (GMT): 2007/164/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4139201
35 A = 6719620
34 meter
Y = -5229063
03 meter E =
0002530
Z = -810394
84 I = 51
91945
XDOT = 3301
446039 Wp = 162
45610
YDOT = 3540
921256 meter/sec RA = 122
90065 deg
ZDOT = -5992
341295 TA = 26
35913
MA = 26
34626
Ha = 183
466 n
mi
Hp = 178
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13580056
91 X = 4201302
66
Y = -17155718
61 feet Y = -5182428
76 meter
Z = -2658775
71 Z = -790136
59
XDOT = 10831
515876 XDOT = 3290
715653
YDOT = 11617
195723 feet/sec YDOT = 3577
781147 meter/sec
ZDOT = -19659
912386 ZDOT = -5976
327974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5295264
62 X = 1613996
66
Y = -21238991
00 feet Y = -6473644
46 meter
Z = -2582856
77 Z = -787254
74
XDOT = 13213
870286 XDOT = 4027
587663
YDOT = 5674
930760 feet/sec YDOT = 1729
718896 meter/sec
ZDOT = -19599
004821 ZDOT = -5973
776669
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 07164
37422313
00020000 00000-0 20000-3 0 9057
2 25544 51
6310 123
6099 0008145 314
3601 45
6897 15
78326543 10176
Satellite: ISS
Catalog Number: 25544
Epoch time: 07164
37422313 = yrday
fracday
Element set: 905
Inclination: 51
6310 deg
RA of node: 123
6099 deg
Eccentricity:
0008145
Arg of perigee: 314
3601 deg
Mean anomaly: 45
6897 deg
Mean motion: 15
78326543 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1017
Checksum: 275
Coasting Arc #7 (Orbit 1032)
---------------------------------------
Vector Time (GMT): 2007/165/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2022116
05 A = 6709755
55 meter
Y = -4237062
37 meter E =
0009811
Z = 4796824
70 I = 51
90097
XDOT = 5014
787674 Wp = 4
60133
YDOT = -5272
576898 meter/sec RA = 117
72295 deg
ZDOT = -2533
364007 TA = 110
14815
MA = 110
04258
Ha = 183
613 n
mi
Hp = 178
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6634239
02 X = -1997888
60
Y = -13901123
28 feet Y = -4259540
47 meter
Z = 15737613
84 Z = 4787059
04
XDOT = 16452
715467 XDOT = 5085
680408
YDOT = -17298
480635 feet/sec YDOT = -5216
101758 meter/sec
ZDOT = -8311
561702 ZDOT = -2508
831000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12031757
91 X = -3667279
81
Y = -9678143
67 feet Y = -2949898
19 meter
Z = 15700228
71 Z = 4785429
71
XDOT = 6786
128179 XDOT = 2068
411869
YDOT = -21823
365815 feet/sec YDOT = -6651
761901 meter/sec
ZDOT = -8219
479100 ZDOT = -2505
297230
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 07165
38725551
00020000 00000-0 20000-3 0 9060
2 25544 51
6308 118
3726 0008249 318
4384 41
6154 15
78373077 10333
Satellite: ISS
Catalog Number: 25544
Epoch time: 07165
38725551 = yrday
fracday
Element set: 906
Inclination: 51
6308 deg
RA of node: 118
3726 deg
Eccentricity:
0008249
Arg of perigee: 318
4384 deg
Mean anomaly: 41
6154 deg
Mean motion: 15
78373077 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1033
Checksum: 295
Coasting Arc #8 (Orbit 1048)
---------------------------------------
Vector Time (GMT): 2007/166/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4444347
72 A = 6714609
75 meter
Y = 3663579
29 meter E =
0009747
Z = 3438759
60 I = 51
92974
XDOT = -1399
405179 Wp = 49
18283
YDOT = -6024
279653 meter/sec RA = 112
61936 deg
ZDOT = 4607
326844 TA = 351
44590
MA = 351
46250
Ha = 183
846 n
mi
Hp = 178
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14581193
32 X = -4501688
98
Y = 12019617
11 feet Y = 3613558
66 meter
Z = 11282019
70 Z = 3417030
53
XDOT = -4591
224342 XDOT = -1354
318381
YDOT = -19764
697024 feet/sec YDOT = -6039
677608 meter/sec
ZDOT = 15115
901720 ZDOT = 4600
636582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7782734
91 X = -2372177
60
Y = 17272753
26 feet Y = 5264735
19 meter
Z = 11200330
12 Z = 3413860
62
XDOT = -11707
384619 XDOT = -3568
410832
YDOT = -15064
672157 feet/sec YDOT = -4591
712074 meter/sec
ZDOT = 15089
933278 ZDOT = 4599
411663
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
40027086
00020000 00000-0 20000-3 0 9073
2 25544 51
6308 113
1358 0008323 322
1006 37
9573 15
78392590 10494
Satellite: ISS
Catalog Number: 25544
Epoch time: 07166
40027086 = yrday
fracday
Element set: 907
Inclination: 51
6308 deg
RA of node: 113
1358 deg
Eccentricity:
0008323
Arg of perigee: 322
1006 deg
Mean anomaly: 37
9573 deg
Mean motion: 15
78392590 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1049
Checksum: 279
Coasting Arc #9 (Orbit 1063)
---------------------------------------
Vector Time (GMT): 2007/167/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 494342
21 A = 6715964
84 meter
Y = 6027884
27 meter E =
0008815
Z = -2907929
91 I = 51
94489
XDOT = -5056
666306 Wp = 357
31421
YDOT = 2856
889830 meter/sec RA = 107
42175 deg
ZDOT = 5070
461259 TA = 329
29819
MA = 329
34974
Ha = 183
932 n
mi
Hp = 178
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1621857
65 X = 441026
91
Y = 19776523
19 feet Y = 6033114
87 meter
Z = -9540452
48 Z = -2905656
49
XDOT = -16590
112554 XDOT = -5112
867895
YDOT = 9372
998129 feet/sec YDOT = 2800
027916 meter/sec
ZDOT = 16635
371585 ZDOT = 5045
760257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10574288
37 X = 3223043
10
Y = 16795911
00 feet Y = 5119393
67 meter
Z = -9531176
43 Z = -2905102
58
XDOT = -9286
593823 XDOT = -2830
553797
YDOT = 15218
982604 feet/sec YDOT = 4638
745898 meter/sec
ZDOT = 16542
345574 ZDOT = 5042
106931
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
34995638
00020000 00000-0 20000-3 0 9085
2 25544 51
6312 108
2266 0008325 326
3877 33
6759 15
78407912 10647
Satellite: ISS
Catalog Number: 25544
Epoch time: 07167
34995638 = yrday
fracday
Element set: 908
Inclination: 51
6312 deg
RA of node: 108
2266 deg
Eccentricity:
0008325
Arg of perigee: 326
3877 deg
Mean anomaly: 33
6759 deg
Mean motion: 15
78407912 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1064
Checksum: 314
Coasting Arc #10 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2007/168/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4289058
40 A = 6708568
26 meter
Y = -1099825
63 meter E =
0013599
Z = -5050028
48 I = 51
92686
XDOT = -197
841256 Wp = 40
52776
YDOT = 7485
580772 meter/sec RA = 102
31161 deg
ZDOT = -1790
846013 TA = 212
24524
MA = 212
32845
Ha = 184
036 n
mi
Hp = 177
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14071713
91 X = 4325569
91
Y = -3608351
81 feet Y = -1051657
72 meter
Z = -16568334
90 Z = -5029103
99
XDOT = -649
085484 XDOT = -272
831893
YDOT = 24558
992034 feet/sec YDOT = 7482
949499 meter/sec
ZDOT = -5875
479045 ZDOT = -1791
987626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10754125
75 X = 3277857
53
Y = -9899113
06 feet Y = -3017249
66 meter
Z = -16489372
22 Z = -5025960
65
XDOT = 10393
014806 XDOT = 3167
790913
YDOT = 21124
341302 feet/sec YDOT = 6438
699229 meter/sec
ZDOT = -5878
946115 ZDOT = -1791
902776
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
36293697
00020000 00000-0 20000-3 0 9095
2 25544 51
6307 102
9888 0008357 329
8821 30
1863 15
78432791 10803
Satellite: ISS
Catalog Number: 25544
Epoch time: 07168
36293697 = yrday
fracday
Element set: 909
Inclination: 51
6307 deg
RA of node: 102
9888 deg
Eccentricity:
0008357
Arg of perigee: 329
8821 deg
Mean anomaly: 30
1863 deg
Mean motion: 15
78432791 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1080
Checksum: 320
Coasting Arc #11 (Orbit 1095)
---------------------------------------
Vector Time (GMT): 2007/169/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 775817
70 A = 6719446
65 meter
Y = -6673322
98 meter E =
0005313
Z = 77465
78 I = 51
96905
XDOT = 4722
710395 Wp = 100
95458
YDOT = 474
589905 meter/sec RA = 97
14799 deg
ZDOT = -6066
641876 TA = 78
20671
MA = 78
14712
Ha = 184
127 n
mi
Hp = 177
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2545333
66 X = 850005
80
Y = -21894104
26 feet Y = -6664232
56 meter
Z = 254152
82 Z = 81413
55
XDOT = 15494
456678 XDOT = 4746
522738
YDOT = 1557
053495 feet/sec YDOT = 527
536230 meter/sec
ZDOT = -19903
680696 ZDOT = -6043
641297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8504314
83 X = -2592115
16
Y = -20334693
31 feet Y = -6198014
52 meter
Z = 268319
82 Z = 81783
88
XDOT = 12885
805555 XDOT = 3927
593533
YDOT = -5664
794098 feet/sec YDOT = -1726
629241 meter/sec
ZDOT = -19816
684639 ZDOT = -6040
125478
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
37589895
00020000 00000-0 20000-3 0 9107
2 25544 51
6307 97
7512 0008510 334
0450 26
0287 15
78482159 10969
Satellite: ISS
Catalog Number: 25544
Epoch time: 07169
37589895 = yrday
fracday
Element set: 910
Inclination: 51
6307 deg
RA of node: 97
7512 deg
Eccentricity:
0008510
Arg of perigee: 334
0450 deg
Mean anomaly: 26
0287 deg
Mean motion: 15
78482159 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1096
Checksum: 308
Coasting Arc #12 (Orbit 1111)
---------------------------------------
Vector Time (GMT): 2007/170/08:15:27
185
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3920338
24 A = 6708187
61 meter
Y = -1938420
42 meter E =
0010779
Z = 5088539
25 I = 51
93295
XDOT = 1527
620446 Wp = 3
63079
YDOT = -7377
452707 meter/sec RA = 91
98729 deg
ZDOT = -1622
719320 TA = 101
94209
MA = 101
82123
Ha = 184
290 n
mi
Hp = 177
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12862002
11 X = -3923090
06
Y = -6359647
05 feet Y = -1982276
10 meter
Z = 16694682
58 Z = 5069487
47
XDOT = 5011
878105 XDOT = 1617
885443
YDOT = -24204
241166 feet/sec YDOT = -7359
865024 meter/sec
ZDOT = -5323
882284 ZDOT = -1615
080243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14393951
42 X = -4387276
39
Y = 1047476
85 feet Y = 319270
94 meter
Z = 16622442
36 Z = 5066520
43
XDOT = -7785
949888 XDOT = -2373
157526
YDOT = -22390
635303 feet/sec YDOT = -6824
665640 meter/sec
ZDOT = -5295
839873 ZDOT = -1614
171993
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
38884287
00020000 00000-0 20000-3 0 9114
2 25544 51
6303 92
5136 0008548 336
8976 23
1803 15
78496069 11120
Satellite: ISS
Catalog Number: 25544
Epoch time: 07170
38884287 = yrday
fracday
Element set: 911
Inclination: 51
6303 deg
RA of node: 92
5136 deg
Eccentricity:
0008548
Arg of perigee: 336
8976 deg
Mean anomaly: 23
1803 deg
Mean motion: 15
78496069 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1112
Checksum: 306
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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