Date:
July 12th 2008
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) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 3235)
---------------------------------------
Vector Time (GMT): 2008/193/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4271952
72 A = 6724062
80 meter
Y = 3914925
15 meter E =
0015262
Z = 3410602
20 I = 51
33395
XDOT = -1780
653364 Wp = 51
30491
YDOT = 5939
720693 meter/sec RA = 250
60084 deg
ZDOT = -4564
509561 TA = 88
17968
MA = 88
00489
Ha = 190
424 n
mi
Hp = 181
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14015592
90 X = 4211289
84
Y = 12844242
62 feet Y = 3962356
92 meter
Z = 11189639
78 Z = 3431208
52
XDOT = -5842
038597 XDOT = -1824
766395
YDOT = 19487
272615 feet/sec YDOT = 5919
562391 meter/sec
ZDOT = -14975
425070 ZDOT = -4573
266289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9806088
59 X = 2988895
80
Y = -16231471
80 feet Y = -4947352
60 meter
Z = 11269401
09 Z = 3434913
45
XDOT = 19059
897133 XDOT = 5809
456646
YDOT = 1042
094784 feet/sec YDOT = 317
630490 meter/sec
ZDOT = -15008
632287 ZDOT = -4574
631121
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 08193
51810149
00020000 00000-0 20000-3 0 9009
2 25544 51
6397 251
2621 0009381 356
7443 3
3658 15
75050001 32368
Satellite: ISS
Catalog Number: 25544
Epoch time: 08193
51810149 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 251
2621 deg
Eccentricity:
0009381
Arg of perigee: 356
7443 deg
Mean anomaly: 3
3658 deg
Mean motion: 15
75050001 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3236
Checksum: 269
Coasting Arc #2 (Orbit 3251)
---------------------------------------
Vector Time (GMT): 2008/194/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1395342
97 A = 6721456
14 meter
Y = -5045699
78 meter E =
0011722
Z = 4203125
90 I = 51
33551
XDOT = 5183
741485 Wp = 56
95155
YDOT = 4430
716253 meter/sec RA = 245
48660 deg
ZDOT = 3597
110883 TA = 356
35108
MA = 356
35962
Ha = 190
491 n
mi
Hp = 181
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4577896
89 X = 1431243
09
Y = -16554133
14 feet Y = -5029896
19 meter
Z = 13789783
13 Z = 4209990
88
XDOT = 17007
025868 XDOT = 5116
337154
YDOT = 14536
470645 feet/sec YDOT = 4488
306384 meter/sec
ZDOT = 11801
544892 ZDOT = 3622
130441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17135184
68 X = -5222804
29
Y = -814981
23 feet Y = -248406
28 meter
Z = 13815782
08 Z = 4211050
38
XDOT = 10472
479804 XDOT = 3192
011844
YDOT = -18431
237606 feet/sec YDOT = -5617
841222 meter/sec
ZDOT = 11898
367164 ZDOT = 3626
622311
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 08194
53327337
00020000 00000-0 20000-3 0 9015
2 25544 51
6392 246
0407 0009300 1
0106 359
1074 15
75048735 32527
Satellite: ISS
Catalog Number: 25544
Epoch time: 08194
53327337 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 246
0407 deg
Eccentricity:
0009300
Arg of perigee: 1
0106 deg
Mean anomaly: 359
1074 deg
Mean motion: 15
75048735 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3252
Checksum: 264
Coasting Arc #3 (Orbit 3266)
---------------------------------------
Vector Time (GMT): 2008/195/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4776290
62 A = 6725550
94 meter
Y = -3775487
15 meter E =
0012413
Z = -2846815
58 I = 51
36238
XDOT = 1443
913553 Wp = 24
04874
YDOT = -5627
248916 meter/sec RA = 240
27368 deg
ZDOT = 5059
284323 TA = 303
11310
MA = 303
23218
Ha = 190
604 n
mi
Hp = 180
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15670244
80 X = -4719888
25
Y = -12386768
88 feet Y = -3828582
52 meter
Z = -9339946
11 Z = -2869882
39
XDOT = 4737
249188 XDOT = 1482
154004
YDOT = -18462
102742 feet/sec YDOT = -5610
889304 meter/sec
ZDOT = 16598
701846 ZDOT = 5066
390755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8409258
36 X = -2563141
95
Y = 18072020
26 feet Y = 5508351
77 meter
Z = -9429192
25 Z = -2874017
80
XDOT = -17717
699827 XDOT = -5400
354907
YDOT = 398
075846 feet/sec YDOT = 121
333518 meter/sec
ZDOT = 16625
579527 ZDOT = 5067
476640
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 08195
48498813
00020000 00000-0 20000-3 0 9029
2 25544 51
6386 241
1459 0009388 5
3006 354
8255 15
75062118 32675
Satellite: ISS
Catalog Number: 25544
Epoch time: 08195
48498813 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 241
1459 deg
Eccentricity:
0009388
Arg of perigee: 5
3006 deg
Mean anomaly: 354
8255 deg
Mean motion: 15
75062118 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3267
Checksum: 306
Coasting Arc #4 (Orbit 3282)
---------------------------------------
Vector Time (GMT): 2008/196/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1181006
70 A = 6719923
00 meter
Y = 4757621
94 meter E =
0017308
Z = -4612506
34 I = 51
35905
XDOT = -5744
449261 Wp = 41
99581
YDOT = -4223
288905 meter/sec RA = 235
15579 deg
ZDOT = -2878
886678 TA = 199
32823
MA = 199
39396
Ha = 190
838 n
mi
Hp = 180
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3874693
88 X = -1211712
80
Y = 15608995
87 feet Y = 4744244
41 meter
Z = -15132894
81 Z = -4618317
35
XDOT = -18846
618312 XDOT = -5682
811796
YDOT = -13855
934729 feet/sec YDOT = -4287
181469 meter/sec
ZDOT = -9445
166266 ZDOT = -2906
644137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16060418
46 X = 4895215
55
Y = -227390
71 feet Y = -69308
69 meter
Z = -15154859
36 Z = -4619201
13
XDOT = -8743
798629 XDOT = -2665
109822
YDOT = 20484
748715 feet/sec YDOT = 6243
751408 meter/sec
ZDOT = -9552
544130 ZDOT = -2911
615451
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 08196
50013972
00020000 00000-0 20000-3 0 9033
2 25544 51
6389 235
9239 0009440 9
4912 350
6428 15
75053664 32835
Satellite: ISS
Catalog Number: 25544
Epoch time: 08196
50013972 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 235
9239 deg
Eccentricity:
0009440
Arg of perigee: 9
4912 deg
Mean anomaly: 350
6428 deg
Mean motion: 15
75053664 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3283
Checksum: 300
Coasting Arc #5 (Orbit 3298)
---------------------------------------
Vector Time (GMT): 2008/197/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5266447
19 A = 6726925
86 meter
Y = 3578714
37 meter E =
0016220
Z = 2165706
64 I = 51
40074
XDOT = -1299
470225 Wp = 72
84901
YDOT = 5251
096500 meter/sec RA = 229
95171 deg
ZDOT = -5478
704807 TA = 82
81866
MA = 82
63428
Ha = 190
902 n
mi
Hp = 180
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17278370
03 X = 5215517
50
Y = 11741188
89 feet Y = 3637321
63 meter
Z = 7105336
74 Z = 2191167
79
XDOT = -4263
353756 XDOT = -1331
477917
YDOT = 17228
006889 feet/sec YDOT = 5236
387152 meter/sec
ZDOT = -17974
753305 ZDOT = -5485
094332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6728875
56 X = 2050961
27
Y = -19741090
10 feet Y = -6017084
26 meter
Z = 7203817
95 Z = 2195723
71
XDOT = 16274
302893 XDOT = 4960
407522
YDOT = -1066
296821 feet/sec YDOT = -325
007271 meter/sec
ZDOT = -17998
902415 ZDOT = -5486
065456
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 08197
51527898
00020000 00000-0 20000-3 0 9043
2 25544 51
6384 230
7022 0009646 13
1933 346
9482 15
75110507 32991
Satellite: ISS
Catalog Number: 25544
Epoch time: 08197
51527898 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 230
7022 deg
Eccentricity:
0009646
Arg of perigee: 13
1933 deg
Mean anomaly: 346
9482 deg
Mean motion: 15
75110507 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3299
Checksum: 306
Coasting Arc #6 (Orbit 3314)
---------------------------------------
Vector Time (GMT): 2008/198/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1120514
13 A = 6718426
67 meter
Y = -4425825
91 meter E =
0009958
Z = 4920044
11 I = 51
39100
XDOT = 6304
909212 Wp = 55
07769
YDOT = 3915
264388 meter/sec RA = 224
82723 deg
ZDOT = 2088
713152 TA = 14
65183
MA = 14
62299
Ha = 190
979 n
mi
Hp = 180
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3676227
47 X = 1146020
76
Y = -14520426
21 feet Y = -4413153
99 meter
Z = 16141877
01 Z = 4925548
62
XDOT = 20685
397676 XDOT = 6250
513049
YDOT = 12845
355604 feet/sec YDOT = 3985
464961 meter/sec
ZDOT = 6852
733439 ZDOT = 2119
210629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14941188
86 X = -4554074
37
Y = 667811
96 feet Y = 203549
09 meter
Z = 16162689
19 Z = 4926387
66
XDOT = 6532
402812 XDOT = 1991
076377
YDOT = -22345
914713 feet/sec YDOT = -6811
034804 meter/sec
ZDOT = 6970
678042 ZDOT = 2124
662667
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 08198
53040905
00020000 00000-0 20000-3 0 9056
2 25544 51
6376 225
4803 0009630 17
9759 342
1744 15
75107682 33159
Satellite: ISS
Catalog Number: 25544
Epoch time: 08198
53040905 = yrday
fracday
Element set: 905
Inclination: 51
6376 deg
RA of node: 225
4803 deg
Eccentricity:
0009630
Arg of perigee: 17
9759 deg
Mean anomaly: 342
1744 deg
Mean motion: 15
75107682 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3315
Checksum: 297
Coasting Arc #7 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2008/199/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5715222
19 A = 6727968
13 meter
Y = -3214190
97 meter E =
0017825
Z = -1468740
04 I = 51
44592
XDOT = 1291
380211 Wp = 29
07590
YDOT = -4921
047657 meter/sec RA = 219
63650 deg
ZDOT = 5788
771362 TA = 314
69348
MA = 314
83855
Ha = 191
014 n
mi
Hp = 180
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18750728
97 X = -5671721
08
Y = -10545245
97 feet Y = -3277858
37 meter
Z = -4818700
92 Z = -1496399
05
XDOT = 4236
811715 XDOT = 1318
191834
YDOT = -16145
169478 feet/sec YDOT = -4906
457830 meter/sec
ZDOT = 18992
032027 ZDOT = 5795
109026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4460246
77 X = -1359483
21
Y = 21020372
61 feet Y = 6407009
57 meter
Z = -4925653
48 Z = -1501339
18
XDOT = -15107
814235 XDOT = -4604
861779
YDOT = 1216
735804 feet/sec YDOT = 370
861073 meter/sec
ZDOT = 19016
008123 ZDOT = 5796
079276
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 08199
48208350
00020000 00000-0 20000-3 0 9062
2 25544 51
6383 220
5851 0009653 21
4508 338
7059 15
75133636 33308
Satellite: ISS
Catalog Number: 25544
Epoch time: 08199
48208350 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 220
5851 deg
Eccentricity:
0009653
Arg of perigee: 21
4508 deg
Mean anomaly: 338
7059 deg
Mean motion: 15
75133636 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3330
Checksum: 292
Coasting Arc #8 (Orbit 3345)
---------------------------------------
Vector Time (GMT): 2008/200/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1187758
80 A = 6717459
23 meter
Y = 4167028
90 meter E =
0021245
Z = -5150748
42 I = 51
43357
XDOT = -6756
813167 Wp = 58
64195
YDOT = -3454
633145 meter/sec RA = 214
50259 deg
ZDOT = -1229
587924 TA = 199
51361
MA = 199
59505
Ha = 191
187 n
mi
Hp = 179
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3896846
45 X = -1209245
99
Y = 13671354
66 feet Y = 4153627
40 meter
Z = -16898780
89 Z = -5156569
95
XDOT = -22168
022203 XDOT = -6711
707733
YDOT = -11334
098246 feet/sec YDOT = -3529
939308 meter/sec
ZDOT = -4034
081116 ZDOT = -1262
302894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14171942
73 X = 4319608
14
Y = -708188
67 feet Y = -215855
91 meter
Z = -16920834
92 Z = -5157470
48
XDOT = -3818
391753 XDOT = -1163
845806
YDOT = 23556
361228 feet/sec YDOT = 7179
978902 meter/sec
ZDOT = -4160
570818 ZDOT = -1268
141985
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 08200
49719177
00020000 00000-0 20000-3 0 9071
2 25544 51
6383 215
3628 0009657 24
9944 335
1686 15
75118930 33462
Satellite: ISS
Catalog Number: 25544
Epoch time: 08200
49719177 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 215
3628 deg
Eccentricity:
0009657
Arg of perigee: 24
9944 deg
Mean anomaly: 335
1686 deg
Mean motion: 15
75118930 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3346
Checksum: 315
Coasting Arc #9 (Orbit 3361)
---------------------------------------
Vector Time (GMT): 2008/201/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6077142
51 A = 6728686
51 meter
Y = 2808436
84 meter E =
0015405
Z = 663862
39 I = 51
49556
XDOT = -1471
775802 Wp = 89
06084
YDOT = 4625
344050 meter/sec RA = 209
32789 deg
ZDOT = -5974
896729 TA = 83
69505
MA = 83
51961
Ha = 191
277 n
mi
Hp = 179
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19938131
58 X = 6042061
60
Y = 9214031
62 feet Y = 2876198
69 meter
Z = 2178026
22 Z = 693299
73
XDOT = -4828
660769 XDOT = -1494
363391
YDOT = 15175
013286 feet/sec YDOT = 4608
760356 meter/sec
ZDOT = -19602
679557 ZDOT = -5982
100680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2079730
24 X = 633901
78
Y = -21853912
74 feet Y = -6661072
60 meter
Z = 2291830
74 Z = 698550
01
XDOT = 14286
581329 XDOT = 4354
549989
YDOT = -738
077034 feet/sec YDOT = -224
965880 meter/sec
ZDOT = -19630
017682 ZDOT = -5983
229389
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 08201
51228900
00020000 00000-0 20000-3 0 9085
2 25544 51
6370 210
1400 0009791 29
4088 330
7625 15
75152511 33622
Satellite: ISS
Catalog Number: 25544
Epoch time: 08201
51228900 = yrday
fracday
Element set: 908
Inclination: 51
6370 deg
RA of node: 210
1400 deg
Eccentricity:
0009791
Arg of perigee: 29
4088 deg
Mean anomaly: 330
7625 deg
Mean motion: 15
75152511 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3362
Checksum: 259
Coasting Arc #10 (Orbit 3377)
---------------------------------------
Vector Time (GMT): 2008/202/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1398809
73 A = 6716796
27 meter
Y = -3947591
55 meter E =
0010815
Z = 5244186
01 I = 51
48143
XDOT = 7125
247934 Wp = 46
13318
YDOT = 2928
347087 meter/sec RA = 204
18183 deg
ZDOT = 310
763783 TA = 40
95436
MA = 40
87317
Ha = 191
268 n
mi
Hp = 179
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4589270
78 X = 1417373
58
Y = -12951415
83 feet Y = -3931846
06 meter
Z = 17205334
69 Z = 5251025
93
XDOT = 23376
797685 XDOT = 7090
463527
YDOT = 9607
437950 feet/sec YDOT = 3007
831174 meter/sec
ZDOT = 1019
566218 ZDOT = 345
293385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13704634
26 X = -4177172
52
Y = 297220
91 feet Y = 90592
93 meter
Z = 17231331
34 Z = 5252109
79
XDOT = 894
962032 XDOT = 272
784427
YDOT = -24253
858298 feet/sec YDOT = -7392
576009 meter/sec
ZDOT = 1153
038573 ZDOT = 351
446157
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 08202
52737480
00020000 00000-0 20000-3 0 9096
2 25544 51
6366 204
9173 0009811 32
8778 327
2994 15
75170848 33782
Satellite: ISS
Catalog Number: 25544
Epoch time: 08202
52737480 = yrday
fracday
Element set: 909
Inclination: 51
6366 deg
RA of node: 204
9173 deg
Eccentricity:
0009811
Arg of perigee: 32
8778 deg
Mean anomaly: 327
2994 deg
Mean motion: 15
75170848 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3378
Checksum: 320
Coasting Arc #11 (Orbit 3393)
---------------------------------------
Vector Time (GMT): 2008/203/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6317560
11 A = 6728701
88 meter
Y = -2280012
07 meter E =
0022069
Z = 120593
39 I = 51
55001
XDOT = 1740
110283 Wp = 42
32176
YDOT = -4469
488181 meter/sec RA = 199
02768 deg
ZDOT = 6035
929255 TA = 318
99174
MA = 319
15748
Ha = 191
243 n
mi
Hp = 179
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20726903
24 X = -6292180
93
Y = -7480354
57 feet Y = -2350516
77 meter
Z = 395647
62 Z = 89964
67
XDOT = 5709
023238 XDOT = 1760
638559
YDOT = -14663
675133 feet/sec YDOT = -4449
915046 meter/sec
ZDOT = 19802
917503 ZDOT = 6044
432009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 580450
82 X = 176921
41
Y = 22029592
73 feet Y = 6714619
87 meter
Z = 277272
83 Z = 84512
76
XDOT = -14088
083681 XDOT = -4294
047906
YDOT = 84
965321 feet/sec YDOT = 25
897430 meter/sec
ZDOT = 19835
274251 ZDOT = 6045
791592
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 08203
54244799
00020000 00000-0 20000-3 0 9107
2 25544 51
6373 199
6958 0009702 36
8194 323
3634 15
75226217 33944
Satellite: ISS
Catalog Number: 25544
Epoch time: 08203
54244799 = yrday
fracday
Element set: 910
Inclination: 51
6373 deg
RA of node: 199
6958 deg
Eccentricity:
0009702
Arg of perigee: 36
8194 deg
Mean anomaly: 323
3634 deg
Mean motion: 15
75226217 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3394
Checksum: 313
Coasting Arc #12 (Orbit 3408)
---------------------------------------
Vector Time (GMT): 2008/204/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1671365
78 A = 6716866
33 meter
Y = 3876526
54 meter E =
0022024
Z = -5242058
60 I = 51
53733
XDOT = -7304
239585 Wp = 73
47365
YDOT = -2315
043371 meter/sec RA = 193
86949 deg
ZDOT = 625
196616 TA = 202
43953
MA = 202
53602
Ha = 191
426 n
mi
Hp = 179
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5483483
51 X = -1689124
88
Y = 12718262
93 feet Y = 3857737
47 meter
Z = -17198354
97 Z = -5250220
82
XDOT = -23964
040632 XDOT = -7280
846585
YDOT = -7595
286649 feet/sec YDOT = -2396
592823 meter/sec
ZDOT = 2051
170001 ZDOT = 589
769760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13810516
90 X = 4209445
55
Y = 147287
81 feet Y = 44893
33 meter
Z = -17229455
77 Z = -5251538
12
XDOT = 2097
643676 XDOT = 639
361792
YDOT = 24055
868347 feet/sec YDOT = 7332
228672 meter/sec
ZDOT = 1914
271745 ZDOT = 583
470028
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 08204
49407185
00020000 00000-0 20000-3 0 9113
2 25544 51
6368 194
7993 0009812 39
4724 320
7153 15
75177066 34094
Satellite: ISS
Catalog Number: 25544
Epoch time: 08204
49407185 = yrday
fracday
Element set: 911
Inclination: 51
6368 deg
RA of node: 194
7993 deg
Eccentricity:
0009812
Arg of perigee: 39
4724 deg
Mean anomaly: 320
7153 deg
Mean motion: 15
75177066 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3409
Checksum: 309
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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