Date:
February 3rd 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 701)
---------------------------------------
Vector Time (GMT): 2008/032/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6353933
45 A = 6720034
24 meter
Y = 1268010
86 meter E =
0016831
Z = 1744265
98 I = 51
64906
XDOT = -2482
081851 Wp = 45
78751
YDOT = 4558
686542 meter/sec RA = 358
98779 deg
ZDOT = 5705
440568 TA = 333
57105
MA = 333
65680
Ha = 185
018 n
mi
Hp = 177
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20846238
35 X = 6330808
93
Y = 4160140
62 feet Y = 1338934
72 meter
Z = 5722657
42 Z = 1775076
84
XDOT = -8143
313160 XDOT = -2560
588874
YDOT = 14956
320677 feet/sec YDOT = 4530
491078 meter/sec
ZDOT = 18718
637034 ZDOT = 5693
192478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10893649
29 X = 3320384
30
Y = -18216387
11 feet Y = -5552354
79 meter
Z = 5840622
98 Z = 1780221
89
XDOT = 9999
309855 XDOT = 3047
789644
YDOT = 11989
375595 feet/sec YDOT = 3654
361681 meter/sec
ZDOT = 18672
225504 ZDOT = 5691
294334
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
89253769
00020000 00000-0 20000-3 0 9001
2 25544 51
6399 359
1493 0005819 353
0172 7
0911 15
77792346 7021
Satellite: ISS
Catalog Number: 25544
Epoch time: 08032
89253769 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 359
1493 deg
Eccentricity:
0005819
Arg of perigee: 353
0172 deg
Mean anomaly: 7
0911 deg
Mean motion: 15
77792346 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 702
Checksum: 304
Coasting Arc #2 (Orbit 716)
---------------------------------------
Vector Time (GMT): 2008/033/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3279602
07 A = 6712951
38 meter
Y = -3868845
78 meter E =
0008767
Z = -4403470
03 I = 51
59507
XDOT = 6686
503595 Wp = 73
04977
YDOT = 1910
341177 meter/sec RA = 353
78041 deg
ZDOT = 3309
458636 TA = 230
16673
MA = 230
24391
Ha = 185
176 n
mi
Hp = 177
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10759849
32 X = 3344011
20
Y = -12693063
60 feet Y = -3831810
90 meter
Z = -14447080
13 Z = -4387381
91
XDOT = 21937
347751 XDOT = 6648
568473
YDOT = 6267
523546 feet/sec YDOT = 1984
901076 meter/sec
ZDOT = 10857
803924 ZDOT = 3341
849065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8574273
36 X = -2613438
52
Y = -14322488
38 feet Y = -4365494
46 meter
Z = -14385913
54 Z = -4384826
45
XDOT = 11870
273714 XDOT = 3618
059428
YDOT = -18110
555416 feet/sec YDOT = -5520
097291 meter/sec
ZDOT = 10981
876768 ZDOT = 3347
276039
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
84259339
00020000 00000-0 20000-3 0 9017
2 25544 51
6389 354
2418 0005782 357
4628 2
6507 15
77812522 7173
Satellite: ISS
Catalog Number: 25544
Epoch time: 08033
84259339 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 354
2418 deg
Eccentricity:
0005782
Arg of perigee: 357
4628 deg
Mean anomaly: 2
6507 deg
Mean motion: 15
77812522 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 717
Checksum: 302
Coasting Arc #3 (Orbit 732)
---------------------------------------
Vector Time (GMT): 2008/034/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5068202
62 A = 6714578
10 meter
Y = -2118108
04 meter E =
0010161
Z = -3873427
58 I = 51
57187
XDOT = 4915
369125 Wp = 40
13375
YDOT = -4290
126267 meter/sec RA = 348
66231 deg
ZDOT = -4083
854800 TA = 187
22710
MA = 187
24176
Ha = 185
191 n
mi
Hp = 177
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16627961
35 X = -5025324
97
Y = -6949173
37 feet Y = -2174543
51 meter
Z = -12708095
72 Z = -3897944
35
XDOT = 16126
539125 XDOT = 4982
814817
YDOT = -14075
217413 feet/sec YDOT = -4234
782372 meter/sec
ZDOT = -13398
473753 ZDOT = -4059
813026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11631173
96 X = -3545181
82
Y = 13678392
48 feet Y = 4169174
03 meter
Z = -12802077
08 Z = -3902073
09
XDOT = -7517
933908 XDOT = -2291
466255
YDOT = -18852
355029 feet/sec YDOT = -5746
197813 meter/sec
ZDOT = -13306
923309 ZDOT = -4055
950225
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
85595879
00020000 00000-0 20000-3 0 9022
2 25544 51
6384 349
0081 0005789 2
0237 358
0951 15
77859347 7337
Satellite: ISS
Catalog Number: 25544
Epoch time: 08034
85595879 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 349
0081 deg
Eccentricity:
0005789
Arg of perigee: 2
0237 deg
Mean anomaly: 358
0951 deg
Mean motion: 15
77859347 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 733
Checksum: 321
Coasting Arc #4 (Orbit 748)
---------------------------------------
Vector Time (GMT): 2008/035/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5102227
12 A = 6718350
34 meter
Y = 3583031
77 meter E =
0013966
Z = 2494963
09 I = 51
55733
XDOT = -4713
533910 Wp = 80
37336
YDOT = -2995
765878 meter/sec RA = 343
44320 deg
ZDOT = -5309
563218 TA = 71
30903
MA = 71
15748
Ha = 185
145 n
mi
Hp = 177
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16739590
28 X = -5154033
67
Y = 11755353
56 feet Y = 3525685
92 meter
Z = 8185574
44 Z = 2470051
57
XDOT = -15464
350100 XDOT = -4653
892296
YDOT = -9828
628209 feet/sec YDOT = -3048
141454 meter/sec
ZDOT = -17419
826832 ZDOT = -5332
316275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6463148
08 X = 1969967
53
Y = 19446729
66 feet Y = 5927363
20 meter
Z = 8090628
63 Z = 2466023
61
XDOT = -12394
792929 XDOT = -3777
932885
YDOT = 11440
990075 feet/sec YDOT = 3487
213775 meter/sec
ZDOT = -17507
151759 ZDOT = -5336
179856
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
86929496
00020000 00000-0 20000-3 0 9031
2 25544 51
6391 343
7733 0005821 3
5818 356
5388 15
77935442 7493
Satellite: ISS
Catalog Number: 25544
Epoch time: 08035
86929496 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 343
7733 deg
Eccentricity:
0005821
Arg of perigee: 3
5818 deg
Mean anomaly: 356
5388 deg
Mean motion: 15
77935442 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 749
Checksum: 326
Coasting Arc #5 (Orbit 764)
---------------------------------------
Vector Time (GMT): 2008/036/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3012069
98 A = 6709690
64 meter
Y = 3159775
33 meter E =
0005543
Z = 5090756
29 I = 51
49939
XDOT = -6518
159255 Wp = 57
72559
YDOT = 3850
549609 meter/sec RA = 338
30333 deg
ZDOT = 1468
392872 TA = 18
20250
MA = 18
18267
Ha = 185
231 n
mi
Hp = 177
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9882119
37 X = 2951783
82
Y = 10366716
95 feet Y = 3193120
68 meter
Z = 16701956
35 Z = 5105242
20
XDOT = -21385
036926 XDOT = -6567
865220
YDOT = 12633
036775 feet/sec YDOT = 3777
381851 meter/sec
ZDOT = 4817
561916 ZDOT = 1436
608086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12620814
35 X = 3846824
21
Y = -6631416
89 feet Y = -2021255
87 meter
Z = 16757678
97 Z = 5107740
55
XDOT = 5911
563983 XDOT = 1801
844702
YDOT = 23104
014763 feet/sec YDOT = 7042
103700 meter/sec
ZDOT = 4696
350857 ZDOT = 1431
447741
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
88260832
00020000 00000-0 20000-3 0 9047
2 25544 51
6382 338
5383 0005671 10
5369 349
5914 15
77895128 7659
Satellite: ISS
Catalog Number: 25544
Epoch time: 08036
88260832 = yrday
fracday
Element set: 904
Inclination: 51
6382 deg
RA of node: 338
5383 deg
Eccentricity:
0005671
Arg of perigee: 10
5369 deg
Mean anomaly: 349
5914 deg
Mean motion: 15
77895128 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 765
Checksum: 318
Coasting Arc #6 (Orbit 780)
---------------------------------------
Vector Time (GMT): 2008/037/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5995521
38 A = 6720897
36 meter
Y = -3015998
05 meter E =
0017320
Z = 26482
50 I = 51
51132
XDOT = 2128
696174 Wp = 35
88352
YDOT = 4301
927838 meter/sec RA = 333
11593 deg
ZDOT = 6036
318139 TA = 324
40532
MA = 324
52072
Ha = 185
200 n
mi
Hp = 176
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19670345
74 X = 6028672
50
Y = -9895006
73 feet Y = -2948767
36 meter
Z = 86884
86 Z = 55688
27
XDOT = 6983
911333 XDOT = 2051
110746
YDOT = 14113
936477 feet/sec YDOT = 4325
298190 meter/sec
ZDOT = 19804
193368 ZDOT = 6046
470662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4599068
15 X = -1401795
97
Y = -21532544
08 feet Y = -6563119
43 meter
Z = 198309
62 Z = 60444
77
XDOT = 13822
733257 XDOT = 4213
169097
YDOT = -2743
553295 feet/sec YDOT = -836
235044 meter/sec
ZDOT = 19843
457778 ZDOT = 6048
285931
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
89588974
00020000 00000-0 20000-3 0 9050
2 25544 51
6383 333
3035 0005482 14
3438 345
7882 15
77976419 7819
Satellite: ISS
Catalog Number: 25544
Epoch time: 08037
89588974 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 333
3035 deg
Eccentricity:
0005482
Arg of perigee: 14
3438 deg
Mean anomaly: 345
7882 deg
Mean motion: 15
77976419 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 781
Checksum: 331
Coasting Arc #7 (Orbit 795)
---------------------------------------
Vector Time (GMT): 2008/038/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -676070
37 A = 6709511
89 meter
Y = -4350075
04 meter E =
0015418
Z = -5075881
10 I = 51
44802
XDOT = 6959
215006 Wp = 81
36092
YDOT = -2894
302324 meter/sec RA = 327
92492 deg
ZDOT = 1559
829635 TA = 203
62274
MA = 203
69361
Ha = 185
205 n
mi
Hp = 176
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2218078
64 X = -602719
96
Y = -14271899
75 feet Y = -4357225
14 meter
Z = -16653153
22 Z = -5078987
17
XDOT = 22832
070229 XDOT = 6983
485184
YDOT = -9495
742533 feet/sec YDOT = -2816
344711 meter/sec
ZDOT = 5117
551295 ZDOT = 1593
695415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14369643
15 X = -4379867
23
Y = -1307615
48 feet Y = -398561
20 meter
Z = -16665473
44 Z = -5079636
30
XDOT = -3936
072614 XDOT = -1199
714933
YDOT = -23352
594558 feet/sec YDOT = -7117
870821 meter/sec
ZDOT = 5246
810482 ZDOT = 1599
227835
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
84581704
00020000 00000-0 20000-3 0 9061
2 25544 51
6386 328
3962 0005415 19
5741 340
5632 15
78019339 7967
Satellite: ISS
Catalog Number: 25544
Epoch time: 08038
84581704 = yrday
fracday
Element set: 906
Inclination: 51
6386 deg
RA of node: 328
3962 deg
Eccentricity:
0005415
Arg of perigee: 19
5741 deg
Mean anomaly: 340
5632 deg
Mean motion: 15
78019339 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 796
Checksum: 310
Coasting Arc #8 (Orbit 811)
---------------------------------------
Vector Time (GMT): 2008/039/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5902050
21 A = 6717485
08 meter
Y = 1856801
20 meter E =
0006594
Z = -2624575
46 I = 51
45179
XDOT = 544
118223 Wp = 69
77885
YDOT = -5634
768930 meter/sec RA = 322
78118 deg
ZDOT = -5218
337542 TA = 140
17618
MA = 140
12778
Ha = 185
213 n
mi
Hp = 176
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19363681
78 X = -5909625
23
Y = 6091867
46 feet Y = 1790758
69 meter
Z = -8610811
89 Z = -2653265
28
XDOT = 1785
164774 XDOT = 632
435680
YDOT = -18486
774705 feet/sec YDOT = -5628
190622 meter/sec
ZDOT = -17120
529992 ZDOT = -5215
479620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1704506
70 X = 519533
64
Y = 20180656
19 feet Y = 6151064
01 meter
Z = -8720371
28 Z = -2657969
16
XDOT = -16151
391014 XDOT = -4922
943981
YDOT = -6017
722352 feet/sec YDOT = -1834
201773 meter/sec
ZDOT = -17110
172799 ZDOT = -5215
180669
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
85904517
00020000 00000-0 20000-3 0 9075
2 25544 51
6386 323
1614 0005534 23
1502 336
9912 15
78086793 8129
Satellite: ISS
Catalog Number: 25544
Epoch time: 08039
85904517 = yrday
fracday
Element set: 907
Inclination: 51
6386 deg
RA of node: 323
1614 deg
Eccentricity:
0005534
Arg of perigee: 23
1502 deg
Mean anomaly: 336
9912 deg
Mean motion: 15
78086793 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 812
Checksum: 296
Coasting Arc #9 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2008/040/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1504442
94 A = 6714587
45 meter
Y = 5386357
26 meter E =
0015351
Z = 3709150
88 I = 51
41849
XDOT = -6319
097986 Wp = 66
85635
YDOT = 1179
193352 meter/sec RA = 317
55026 deg
ZDOT = -4255
585515 TA = 68
14800
MA = 67
98479
Ha = 185
239 n
mi
Hp = 176
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4935836
42 X = -1582580
19
Y = 17671775
79 feet Y = 5369096
99 meter
Z = 12169130
18 Z = 3701652
45
XDOT = -20731
948774 XDOT = -6311
141860
YDOT = 3868
744593 feet/sec YDOT = 1108
573910 meter/sec
ZDOT = -13961
894735 ZDOT = -4286
263723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16290885
14 X = 4965461
79
Y = 8482038
97 feet Y = 2585325
48 meter
Z = 12141002
69 Z = 3700577
62
XDOT = 221
793519 XDOT = 67
602665
YDOT = 19820
053688 feet/sec YDOT = 6041
152364 meter/sec
ZDOT = -14079
125473 ZDOT = -4291
317444
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
87224675
00020000 00000-0 20000-3 0 9080
2 25544 51
6378 317
9259 0005305 27
3436 332
8007 15
78087501 8289
Satellite: ISS
Catalog Number: 25544
Epoch time: 08040
87224675 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 317
9259 deg
Eccentricity:
0005305
Arg of perigee: 27
3436 deg
Mean anomaly: 332
8007 deg
Mean motion: 15
78087501 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 828
Checksum: 301
Coasting Arc #10 (Orbit 843)
---------------------------------------
Vector Time (GMT): 2008/041/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4937934
58 A = 6711199
52 meter
Y = -34587
99 meter E =
0010371
Z = 4535516
55 I = 51
38789
XDOT = -2727
815888 Wp = 84
60098
YDOT = 6555
516172 meter/sec RA = 312
41531 deg
ZDOT = 3014
910829 TA = 335
36216
MA = 335
41166
Ha = 184
981 n
mi
Hp = 176
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16200572
78 X = 4915922
00
Y = -113477
65 feet Y = 20507
92 meter
Z = 14880303
66 Z = 4559451
17
XDOT = -8949
527191 XDOT = -2815
563588
YDOT = 21507
598990 feet/sec YDOT = 6524
521685 meter/sec
ZDOT = 9891
439727 ZDOT = 3001
445912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2882425
16 X = 878563
19
Y = -15856546
89 feet Y = -4833075
49 meter
Z = 14971854
20 Z = 4563421
16
XDOT = 18303
918223 XDOT = 5579
034274
YDOT = 12634
049981 feet/sec YDOT = 3850
858434 meter/sec
ZDOT = 9840
615469 ZDOT = 2999
419595
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 08041
88541879
00020000 00000-0 20000-3 0 9091
2 25544 51
6383 312
6906 0005211 30
5451 329
6017 15
78175231 8446
Satellite: ISS
Catalog Number: 25544
Epoch time: 08041
88541879 = yrday
fracday
Element set: 909
Inclination: 51
6383 deg
RA of node: 312
6906 deg
Eccentricity:
0005211
Arg of perigee: 30
5451 deg
Mean anomaly: 329
6017 deg
Mean motion: 15
78175231 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 844
Checksum: 289
Coasting Arc #11 (Orbit 858)
---------------------------------------
Vector Time (GMT): 2008/042/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3067340
39 A = 6719514
07 meter
Y = -5818361
18 meter E =
0014161
Z = -1345243
89 I = 51
39818
XDOT = 4894
127818 Wp = 36
29588
YDOT = 1243
184957 meter/sec RA = 307
19485 deg
ZDOT = 5824
730227 TA = 308
84748
MA = 308
97378
Ha = 185
189 n
mi
Hp = 176
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10063452
72 X = 3138709
10
Y = -19089111
49 feet Y = -5783661
43 meter
Z = -4413529
84 Z = -1330169
41
XDOT = 16056
849795 XDOT = 4851
567447
YDOT = 4078
690805 feet/sec YDOT = 1297
676092 meter/sec
ZDOT = 19110
007307 ZDOT = 5848
402194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17111662
98 X = -5215634
88
Y = -13166572
06 feet Y = -4013171
16 meter
Z = -4356474
93 Z = -1327853
56
XDOT = 5752
782892 XDOT = 1753
448226
YDOT = -13782
870889 feet/sec YDOT = -4201
019047 meter/sec
ZDOT = 19200
684990 ZDOT = 5852
368785
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 08042
83524461
00020000 00000-0 20000-3 0 9107
2 25544 51
6392 307
7828 0005271 35
4136 324
7379 15
78186562 8596
Satellite: ISS
Catalog Number: 25544
Epoch time: 08042
83524461 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 307
7828 deg
Eccentricity:
0005271
Arg of perigee: 35
4136 deg
Mean anomaly: 324
7379 deg
Mean motion: 15
78186562 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 859
Checksum: 305
Coasting Arc #12 (Orbit 874)
---------------------------------------
Vector Time (GMT): 2008/043/19:59:02
943
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3517144
92 A = 6708018
74 meter
Y = -2292525
24 meter E =
0018850
Z = -5247575
54 I = 51
34332
XDOT = 4129
003972 Wp = 77
80529
YDOT = -6492
267917 meter/sec RA = 302
02096 deg
ZDOT = 73
010433 TA = 192
86684
MA = 192
91500
Ha = 185
141 n
mi
Hp = 175
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11539189
37 X = -3465756
62
Y = -7521408
27 feet Y = -2331568
67 meter
Z = -17216455
18 Z = -5264536
83
XDOT = 13546
600957 XDOT = 4200
939968
YDOT = -21300
091590 feet/sec YDOT = -6445
692827 meter/sec
ZDOT = 239
535541 ZDOT = 93
243723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9171713
63 X = -2795538
31
Y = 10166498
11 feet Y = 3098748
63 meter
Z = -17281573
65 Z = -5267423
65
XDOT = -18254
642875 XDOT = -5564
015148
YDOT = -15953
877718 feet/sec YDOT = -4862
741928 meter/sec
ZDOT = 316
253076 ZDOT = 96
393938
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 08043
84836440
00020000 00000-0 20000-3 0 9113
2 25544 51
6392 302
5481 0005299 39
3337 320
8213 15
78250891 8759
Satellite: ISS
Catalog Number: 25544
Epoch time: 08043
84836440 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 302
5481 deg
Eccentricity:
0005299
Arg of perigee: 39
3337 deg
Mean anomaly: 320
8213 deg
Mean motion: 15
78250891 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 875
Checksum: 294
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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