Date:
February 3rd 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9902 8 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 650)
---------------------------------------
Vector Time (GMT): 2008/029/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6135645
04 A = 6721357
68 meter
Y = -2542349
39 meter E =
0004733
Z = -1028283
61 I = 51
74494
XDOT = 2692
383959 Wp = 114
18339
YDOT = -4107
660920 meter/sec RA = 15
49500 deg
ZDOT = -5932
485663 TA = 77
05223
MA = 76
99937
Ha = 185
068 n
mi
Hp = 178
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20130069
03 X = -6101764
93
Y = -8341041
30 feet Y = -2610772
19 meter
Z = -3373633
89 Z = -1058007
99
XDOT = 8833
280706 XDOT = 2766
934932
YDOT = -13476
577821 feet/sec YDOT = -4077
136107 meter/sec
ZDOT = -19463
535641 ZDOT = -5919
225288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19344728
36 X = -5896273
20
Y = -9989616
26 feet Y = -3044835
04 meter
Z = -3487564
56 Z = -1063009
68
XDOT = 9307
945696 XDOT = 2837
061848
YDOT = -11272
886926 feet/sec YDOT = -3435
975935 meter/sec
ZDOT = -19413
218184 ZDOT = -5917
148902
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08029
66217475
00020000 00000-0 20000-3 0 9006
2 25544 51
6402 15
8285 0005895 343
9524 16
1453 15
77634465 6516
Satellite: ISS
Catalog Number: 25544
Epoch time: 08029
66217475 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 15
8285 deg
Eccentricity:
0005895
Arg of perigee: 343
9524 deg
Mean anomaly: 16
1453 deg
Mean motion: 15
77634465 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 651
Checksum: 294
Coasting Arc #2 (Orbit 666)
---------------------------------------
Vector Time (GMT): 2008/030/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3432823
05 A = 6711823
54 meter
Y = 3218851
28 meter E =
0010703
Z = 4785080
78 I = 51
68443
XDOT = -6537
646996 Wp = 28
35643
YDOT = -3211
507584 meter/sec RA = 10
30746 deg
ZDOT = -2518
238878 TA = 86
31557
MA = 86
19318
Ha = 185
198 n
mi
Hp = 178
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11262542
81 X = -3491806
38
Y = 10560535
71 feet Y = 3180133
46 meter
Z = 15699083
92 Z = 4768261
22
XDOT = -21448
973083 XDOT = -6489
016531
YDOT = -10536
442205 feet/sec YDOT = -3284
343235 meter/sec
ZDOT = -8261
938577 ZDOT = -2549
880432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12026123
10 X = -3665562
32
Y = 9785096
03 feet Y = 2982497
27 meter
Z = 15635065
72 Z = 4765568
03
XDOT = -19943
041684 XDOT = -6078
639105
YDOT = -11054
561776 feet/sec YDOT = -3369
430429 meter/sec
ZDOT = -8383
264369 ZDOT = -2555
218980
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08030
67565231
00020000 00000-0 20000-3 0 9016
2 25544 51
6402 10
5960 0005877 348
0684 12
0341 15
77672232 6673
Satellite: ISS
Catalog Number: 25544
Epoch time: 08030
67565231 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 10
5960 deg
Eccentricity:
0005877
Arg of perigee: 348
0684 deg
Mean anomaly: 12
0341 deg
Mean motion: 15
77672232 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 667
Checksum: 271
Coasting Arc #3 (Orbit 682)
---------------------------------------
Vector Time (GMT): 2008/031/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5027999
32 A = 6716962
47 meter
Y = 3032546
95 meter E =
0013473
Z = 3244920
19 I = 51
67348
XDOT = -5079
916352 Wp = 62
13369
YDOT = 3318
056724 meter/sec RA = 5
19179 deg
ZDOT = 4761
675913 TA = 335
93201
MA = 335
99491
Ha = 185
111 n
mi
Hp = 178
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16496060
75 X = 4977952
19
Y = 9949301
02 feet Y = 3088492
85 meter
Z = 10646063
60 Z = 3269224
53
XDOT = -16666
392232 XDOT = -5139
772886
YDOT = 10886
012874 feet/sec YDOT = 3260
915216 meter/sec
ZDOT = 15622
296304 ZDOT = 4736
852828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15927241
46 X = 4854623
20
Y = 10744183
87 feet Y = 3274827
24 meter
Z = 10739309
74 Z = 3273341
61
XDOT = -16485
345410 XDOT = -5024
733281
YDOT = 8888
896173 feet/sec YDOT = 2709
335554 meter/sec
ZDOT = 15527
674166 ZDOT = 4732
835086
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08031
68910409
00020000 00000-0 20000-3 0 9020
2 25544 51
6403 5
3625 0005872 352
1037 8
0034 15
77708985 6834
Satellite: ISS
Catalog Number: 25544
Epoch time: 08031
68910409 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 5
3625 deg
Eccentricity:
0005872
Arg of perigee: 352
1037 deg
Mean anomaly: 8
0034 deg
Mean motion: 15
77708985 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 683
Checksum: 276
Coasting Arc #4 (Orbit 697)
---------------------------------------
Vector Time (GMT): 2008/032/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5268085
24 A = 6716924
82 meter
Y = -2585352
43 meter E =
0007611
Z = -3264603
58 I = 51
64472
XDOT = 4773
996733 Wp = 32
45035
YDOT = 3752
049072 meter/sec RA = 359
97819 deg
ZDOT = 4743
800582 TA = 289
23740
MA = 289
31974
Ha = 185
255 n
mi
Hp = 177
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17283744
22 X = 5312462
13
Y = -8482127
39 feet Y = -2526193
32 meter
Z = -10710641
68 Z = -3238904
02
XDOT = 15662
718941 XDOT = 4708
641755
YDOT = 12309
872285 feet/sec YDOT = 3805
068829 meter/sec
ZDOT = 15563
650202 ZDOT = 4766
833859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17605923
86 X = 5366285
59
Y = -7924420
56 feet Y = -2415363
39 meter
Z = -10612593
87 Z = -3234718
61
XDOT = 14595
781768 XDOT = 4448
794283
YDOT = 11516
671667 feet/sec YDOT = 3510
281524 meter/sec
ZDOT = 15652
104667 ZDOT = 4770
761503
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08032
63919120
00020000 00000-0 20000-3 0 9036
2 25544 51
6406
4562 0005848 355
3649 4
7461 15
77758373 6989
Satellite: ISS
Catalog Number: 25544
Epoch time: 08032
63919120 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node:
4562 deg
Eccentricity:
0005848
Arg of perigee: 355
3649 deg
Mean anomaly: 4
7461 deg
Mean motion: 15
77758373 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 698
Checksum: 297
Coasting Arc #5 (Orbit 713)
---------------------------------------
Vector Time (GMT): 2008/033/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3106298
95 A = 6711252
37 meter
Y = -3537662
98 meter E =
0014793
Z = -4796350
65 I = 51
59776
XDOT = 6804
415055 Wp = 49
68199
YDOT = -2593
598867 meter/sec RA = 354
85759 deg
ZDOT = -2489
446618 TA = 195
91503
MA = 195
96156
Ha = 185
226 n
mi
Hp = 177
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10191269
53 X = -3043210
03
Y = -11606505
85 feet Y = -3572046
23 meter
Z = -15736058
55 Z = -4811287
83
XDOT = 22324
196375 XDOT = 6845
004417
YDOT = -8509
182634 feet/sec YDOT = -2517
280870 meter/sec
ZDOT = -8167
475781 ZDOT = -2456
293009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9930173
34 X = -3026716
84
Y = -11753833
13 feet Y = -3582568
34 meter
Z = -15793528
91 Z = -4813867
61
XDOT = 21635
732286 XDOT = 6594
571201
YDOT = -7455
100873 feet/sec YDOT = -2272
314746 meter/sec
ZDOT = -8040
914344 ZDOT = -2450
870692
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 08033
65259218
00020000 00000-0 20000-3 0 9045
2 25544 51
6413 355
2226 0005872 359
8852
2310 15
77812715 7141
Satellite: ISS
Catalog Number: 25544
Epoch time: 08033
65259218 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 355
2226 deg
Eccentricity:
0005872
Arg of perigee: 359
8852 deg
Mean anomaly:
2310 deg
Mean motion: 15
77812715 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 714
Checksum: 278
Coasting Arc #6 (Orbit 729)
---------------------------------------
Vector Time (GMT): 2008/034/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6369691
31 A = 6720975
52 meter
Y = 1918347
80 meter E =
0011664
Z = 938807
36 I = 51
60150
XDOT = -2204
438649 Wp = 100
30027
YDOT = -4383
252952 meter/sec RA = 349
66126 deg
ZDOT = -5939
973150 TA = 69
42859
MA = 69
30349
Ha = 185
277 n
mi
Hp = 177
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20897937
37 X = -6395229
62
Y = 6293792
00 feet Y = 1846975
42 meter
Z = 3080076
65 Z = 907802
23
XDOT = -7232
410267 XDOT = -2126
405945
YDOT = -14380
751156 feet/sec YDOT = -4407
467443 meter/sec
ZDOT = -19488
100885 ZDOT = -5950
492897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20899293
60 X = -6370104
69
Y = 6345907
90 feet Y = 1934232
73 meter
Z = 2961664
40 Z = 902715
31
XDOT = -6694
989057 XDOT = -2040
632665
YDOT = -12838
944064 feet/sec YDOT = -3913
310151 meter/sec
ZDOT = -19528
758758 ZDOT = -5952
365669
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 08034
66596732
00020000 00000-0 20000-3 0 9053
2 25544 51
6413 349
9886 0005756 3
3479 356
7724 15
77819508 7303
Satellite: ISS
Catalog Number: 25544
Epoch time: 08034
66596732 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 349
9886 deg
Eccentricity:
0005756
Arg of perigee: 3
3479 deg
Mean anomaly: 356
7724 deg
Mean motion: 15
77819508 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 730
Checksum: 328
Coasting Arc #7 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2008/035/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 681946
00 A = 6709018
29 meter
Y = 4131054
06 meter E =
0007333
Z = 5239980
37 I = 51
53379
XDOT = -7497
775454 Wp = 24
05795
YDOT = 1751
467268 meter/sec RA = 344
49655 deg
ZDOT = -398
237077 TA = 69
76399
MA = 69
68515
Ha = 185
189 n
mi
Hp = 177
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2237355
65 X = 610247
05
Y = 13553326
97 feet Y = 4138278
70 meter
Z = 17191536
65 Z = 5243119
32
XDOT = -24599
000833 XDOT = -7514
868872
YDOT = 5746
283688 feet/sec YDOT = 1667
527332 meter/sec
ZDOT = -1306
552091 ZDOT = -434
701683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2406439
21 X = 733482
67
Y = 13508545
04 feet Y = 4117404
53 meter
Z = 17203942
16 Z = 5243761
57
XDOT = -23488
211861 XDOT = -7159
206975
YDOT = 6053
981485 feet/sec YDOT = 1845
253557 meter/sec
ZDOT = -1445
867310 ZDOT = -440
700356
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 08035
67931346
00020000 00000-0 20000-3 0 9060
2 25544 51
6415 344
7547 0005804 5
5373 354
5855 15
77916925 7462
Satellite: ISS
Catalog Number: 25544
Epoch time: 08035
67931346 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 344
7547 deg
Eccentricity:
0005804
Arg of perigee: 5
5373 deg
Mean anomaly: 354
5855 deg
Mean motion: 15
77916925 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 746
Checksum: 314
Coasting Arc #8 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2008/036/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6426132
51 A = 6719901
07 meter
Y = -1049042
33 meter E =
0018258
Z = 1618405
50 I = 51
54315
XDOT = -620
119509 Wp = 48
35927
YDOT = 5110
083200 meter/sec RA = 339
34315 deg
ZDOT = 5745
096214 TA = 329
58178
MA = 329
68759
Ha = 185
293 n
mi
Hp = 177
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21083111
90 X = 6429523
78
Y = -3441739
93 feet Y = -977162
79 meter
Z = 5309729
34 Z = 1649630
89
XDOT = -2034
512824 XDOT = -705
122948
YDOT = 16765
364831 feet/sec YDOT = 5102
673085 meter/sec
ZDOT = 18848
740859 ZDOT = 5741
877571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20911404
07 X = 6373795
96
Y = -4216010
01 feet Y = -1285039
85 meter
Z = 5429074
14 Z = 1654781
80
XDOT = -1828
781299 XDOT = -557
412540
YDOT = 15308
043133 feet/sec YDOT = 4665
891547 meter/sec
ZDOT = 18836
926957 ZDOT = 5741
495336
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 08036
69263653
00020000 00000-0 20000-3 0 9073
2 25544 51
6419 339
5206 0005893 10
3428 349
7858 15
77906146 7624
Satellite: ISS
Catalog Number: 25544
Epoch time: 08036
69263653 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 339
5206 deg
Eccentricity:
0005893
Arg of perigee: 10
3428 deg
Mean anomaly: 349
7858 deg
Mean motion: 15
77906146 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 762
Checksum: 319
Coasting Arc #9 (Orbit 776)
---------------------------------------
Vector Time (GMT): 2008/037/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1694135
07 A = 6712355
10 meter
Y = -4747627
93 meter E =
0010452
Z = -4439778
32 I = 51
49155
XDOT = 6970
759754 Wp = 76
86198
YDOT = -524
523341 meter/sec RA = 334
12968 deg
ZDOT = 3229
495141 TA = 225
50391
MA = 225
58939
Ha = 185
296 n
mi
Hp = 176
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5558185
91 X = 1768664
81
Y = -15576207
12 feet Y = -4728266
30 meter
Z = -14566201
85 Z = -4431367
59
XDOT = 22869
946698 XDOT = 6960
419176
YDOT = -1720
877103 feet/sec YDOT = -446
630246 meter/sec
ZDOT = 10595
456500 ZDOT = 3263
332877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4790114
49 X = 1460026
90
Y = -15858407
62 feet Y = -4833642
64 meter
Z = -14534497
11 Z = -4430114
72
XDOT = 21526
716728 XDOT = 6561
343259
YDOT = -3301
051688 feet/sec YDOT = -1006
160555 meter/sec
ZDOT = 10724
847525 ZDOT = 3268
933526
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 08037
64259988
00020000 00000-0 20000-3 0 9086
2 25544 51
6423 334
6138 0005818 12
7164 347
4147 15
77961925 7777
Satellite: ISS
Catalog Number: 25544
Epoch time: 08037
64259988 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 334
6138 deg
Eccentricity:
0005818
Arg of perigee: 12
7164 deg
Mean anomaly: 347
4147 deg
Mean motion: 15
77961925 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 777
Checksum: 325
Coasting Arc #10 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2008/038/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5502343
60 A = 6714263
91 meter
Y = -271153
54 meter E =
0010796
Z = -3850897
23 I = 51
47279
XDOT = 3150
508415 Wp = 46
32059
YDOT = -5701
120403 meter/sec RA = 329
00265 deg
ZDOT = -4099
968330 TA = 180
76262
MA = 180
76427
Ha = 185
276 n
mi
Hp = 176
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18052308
41 X = -5480196
20
Y = -889611
36 feet Y = -332560
04 meter
Z = -12634177
27 Z = -3877572
99
XDOT = 10336
313697 XDOT = 3233
941350
YDOT = -18704
463265 feet/sec YDOT = -5665
423122 meter/sec
ZDOT = -13451
339664 ZDOT = -4084
460995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17998129
74 X = -5485829
95
Y = 393613
41 feet Y = 119973
37 meter
Z = -12736250
51 Z = -3882009
15
XDOT = 9082
076832 XDOT = 2768
217018
YDOT = -18086
262133 feet/sec YDOT = -5512
692698 meter/sec
ZDOT = -13392
590124 ZDOT = -4082
061470
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 08038
65586882
00020000 00000-0 20000-3 0 9095
2 25544 51
6422 329
3795 0005743 15
4278 344
7061 15
77994063 7931
Satellite: ISS
Catalog Number: 25544
Epoch time: 08038
65586882 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 329
3795 deg
Eccentricity:
0005743
Arg of perigee: 15
4278 deg
Mean anomaly: 344
7061 deg
Mean motion: 15
77994063 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 793
Checksum: 328
Coasting Arc #11 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2008/039/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3617819
32 A = 6718094
77 meter
Y = 5088618
74 meter E =
0015601
Z = 2469635
77 I = 51
46136
XDOT = -5434
030589 Wp = 83
12304
YDOT = -1268
536040 meter/sec RA = 323
77630 deg
ZDOT = -5316
171081 TA = 68
82696
MA = 68
66033
Ha = 185
354 n
mi
Hp = 176
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11869485
97 X = -3686448
86
Y = 16694943
38 feet Y = 5047778
56 meter
Z = 8102479
56 Z = 2451894
09
XDOT = -17828
184348 XDOT = -5393
617492
YDOT = -4161
863648 feet/sec YDOT = -1329
076626 meter/sec
ZDOT = -17441
506171 ZDOT = -5342
470661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10392931
65 X = -3167765
57
Y = 17682750
81 feet Y = 5389702
45 meter
Z = 8035129
26 Z = 2449107
40
XDOT = -16738
101674 XDOT = -5101
773390
YDOT = -1820
639369 feet/sec YDOT = -554
930880 meter/sec
ZDOT = -17542
241199 ZDOT = -5346
875117
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 08039
66911191
00020000 00000-0 20000-3 0 9104
2 25544 51
6421 324
1452 0005790 21
0310 339
1093 15
78038459 8095
Satellite: ISS
Catalog Number: 25544
Epoch time: 08039
66911191 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 324
1452 deg
Eccentricity:
0005790
Arg of perigee: 21
0310 deg
Mean anomaly: 339
1093 deg
Mean motion: 15
78038459 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 809
Checksum: 271
Coasting Arc #12 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2008/040/15:10:49
916
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3845949
03 A = 6709098
11 meter
Y = 2036812
58 meter E =
0006473
Z = 5100498
83 I = 51
40841
XDOT = -4902
337419 Wp = 64
72463
YDOT = 5790
950615 meter/sec RA = 318
62825 deg
ZDOT = 1385
357074 TA = 11
99751
MA = 11
98210
Ha = 185
213 n
mi
Hp = 176
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12617943
02 X = 3798110
53
Y = 6682455
97 feet Y = 2079552
89 meter
Z = 16733920
06 Z = 5119065
74
XDOT = -16083
784184 XDOT = -4973
458027
YDOT = 18999
181807 feet/sec YDOT = 5735
732283 meter/sec
ZDOT = 4545
134758 ZDOT = 1361
369110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13158088
50 X = 4010585
37
Y = 5323842
45 feet Y = 1622707
18 meter
Z = 16805153
77 Z = 5122210
87
XDOT = -13626
554151 XDOT = -4153
373705
YDOT = 19633
299309 feet/sec YDOT = 5984
229629 meter/sec
ZDOT = 4453
970453 ZDOT = 1357
570194
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 08040
68232682
00020000 00000-0 20000-3 0 9110
2 25544 51
6417 318
9102 0005758 23
8678 336
2753 15
78079226 8250
Satellite: ISS
Catalog Number: 25544
Epoch time: 08040
68232682 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 318
9102 deg
Eccentricity:
0005758
Arg of perigee: 23
8678 deg
Mean anomaly: 336
2753 deg
Mean motion: 15
78079226 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 825
Checksum: 302
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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