Date:
November 15th 2006
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) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 1671)
---------------------------------------
Vector Time (GMT): 2006/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4395936
16 A = 6710265
44 meter
Y = 1200373
41 meter E =
0009036
Z = -4928670
29 I = 51
82888
XDOT = -4101
845319 Wp = 137
92884
YDOT = 6150
768567 meter/sec RA = 137
03486 deg
ZDOT = -2169
314129 TA = 111
13366
MA = 111
03706
Ha = 185
682 n
mi
Hp = 178
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14422362
73 X = 4406129
57
Y = 3938232
97 feet Y = 1249588
38 meter
Z = -16170178
11 Z = -4907289
78
XDOT = -13457
497767 XDOT = -4159
780956
YDOT = 20179
686900 feet/sec YDOT = 6104
575601 meter/sec
ZDOT = -7117
172339 ZDOT = -2189
381628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12079126
50 X = -3681717
76
Y = 8954880
30 feet Y = 2729447
51 meter
Z = -16090174
27 Z = -4904285
12
XDOT = -6881
710600 XDOT = -2097
545391
YDOT = -22151
581411 feet/sec YDOT = -6751
802014 meter/sec
ZDOT = -7191
286024 ZDOT = -2191
903980
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 06317
51959513
00020000 00000-0 20000-3 0 9004
2 25544 51
6281 137
8275 0011798 210
6304 149
4173 15
78013028 16720
Satellite: ISS
Catalog Number: 25544
Epoch time: 06317
51959513 = yrday
fracday
Element set: 900
Inclination: 51
6281 deg
RA of node: 137
8275 deg
Eccentricity:
0011798
Arg of perigee: 210
6304 deg
Mean anomaly: 149
4173 deg
Mean motion: 15
78013028 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1672
Checksum: 286
Coasting Arc #2 (Orbit 1687)
---------------------------------------
Vector Time (GMT): 2006/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4110188
54 A = 6720398
63 meter
Y = -5269741
00 meter E =
0018124
Z = 580443
28 I = 51
88421
XDOT = 4092
278006 Wp = 169
04583
YDOT = 2525
835384 meter/sec RA = 131
85996 deg
ZDOT = -6033
253167 TA = 4
64014
MA = 4
62336
Ha = 185
197 n
mi
Hp = 178
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13484870
52 X = 4165990
31
Y = -17289176
52 feet Y = -5223466
61 meter
Z = 1904341
48 Z = 600546
28
XDOT = 13426
108943 XDOT = 4093
038493
YDOT = 8286
861497 feet/sec YDOT = 2571
601910 meter/sec
ZDOT = -19794
137687 ZDOT = -6013
370682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5595746
40 X = 1705583
50
Y = 21193305
48 feet Y = 6459719
51 meter
Z = 1978711
51 Z = 603111
27
XDOT = -13246
798431 XDOT = -4037
624162
YDOT = 5342
562089 feet/sec YDOT = 1628
412925 meter/sec
ZDOT = -19719
546577 ZDOT = -6010
517797
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 06318
53282902
00020000 00000-0 20000-3 0 9019
2 25544 51
6284 132
5913 0011671 216
0547 143
9832 15
78095763 16887
Satellite: ISS
Catalog Number: 25544
Epoch time: 06318
53282902 = yrday
fracday
Element set: 901
Inclination: 51
6284 deg
RA of node: 132
5913 deg
Eccentricity:
0011671
Arg of perigee: 216
0547 deg
Mean anomaly: 143
9832 deg
Mean motion: 15
78095763 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1688
Checksum: 298
Coasting Arc #3 (Orbit 1703)
---------------------------------------
Vector Time (GMT): 2006/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2696825
27 A = 6708834
26 meter
Y = -3241229
91 meter E =
0008700
Z = 5221049
30 I = 51
86203
XDOT = 5119
089929 Wp = 210
49479
YDOT = -5689
300094 meter/sec RA = 126
70734 deg
ZDOT = -895
749825 TA = 247
95835
MA = 248
05078
Ha = 185
242 n
mi
Hp = 178
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8847851
93 X = -2685744
33
Y = -10633956
40 feet Y = -3271325
46 meter
Z = 17129426
83 Z = 5207974
73
XDOT = 16794
914466 XDOT = 5186
679485
YDOT = -18665
682722 feet/sec YDOT = -5631
677659 meter/sec
ZDOT = -2938
811762 ZDOT = -870
716763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13864238
38 X = 4225819
86
Y = -913049
87 feet Y = -278297
60 meter
Z = 17080164
23 Z = 5206034
06
XDOT = 5027
227252 XDOT = 1532
298866
YDOT = 23587
101932 feet/sec YDOT = 7189
348669 meter/sec
ZDOT = -2846
079061 ZDOT = -867
484898
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 06319
54603884
00020000 00000-0 20000-3 0 9028
2 25544 51
6276 127
3546 0011724 218
3351 141
6982 15
78048275 17045
Satellite: ISS
Catalog Number: 25544
Epoch time: 06319
54603884 = yrday
fracday
Element set: 902
Inclination: 51
6276 deg
RA of node: 127
3546 deg
Eccentricity:
0011724
Arg of perigee: 218
3351 deg
Mean anomaly: 141
6982 deg
Mean motion: 15
78048275 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1704
Checksum: 295
Coasting Arc #4 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2006/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4636326
85 A = 6718508
77 meter
Y = 4381476
34 meter E =
0006530
Z = 2111380
99 I = 51
91177
XDOT = -2096
892753 Wp = 125
73904
YDOT = -4903
749238 meter/sec RA = 121
58344 deg
ZDOT = 5555
959441 TA = 257
79112
MA = 257
86426
Ha = 184
830 n
mi
Hp = 178
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15211046
10 X = -4695233
49
Y = 14374922
38 feet Y = 4329300
95 meter
Z = 6927102
99 Z = 2088714
22
XDOT = -6879
569399 XDOT = -2068
892959
YDOT = -16088
416134 feet/sec YDOT = -4927
041432 meter/sec
ZDOT = 18228
213388 ZDOT = 5545
840402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2917292
06 X = -889190
62
Y = -20752384
74 feet Y = -6325326
87 meter
Z = 6843026
18 Z = 2085754
38
XDOT = 15650
298167 XDOT = 4770
210881
YDOT = 3815
087103 feet/sec YDOT = 1162
838549 meter/sec
ZDOT = 18189
769900 ZDOT = 5544
241866
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 06320
55921538
00020000 00000-0 20000-3 0 9031
2 25544 51
6278 122
1175 0011773 222
4966 137
5288 15
78146677 17206
Satellite: ISS
Catalog Number: 25544
Epoch time: 06320
55921538 = yrday
fracday
Element set: 903
Inclination: 51
6278 deg
RA of node: 122
1175 deg
Eccentricity:
0011773
Arg of perigee: 222
4966 deg
Mean anomaly: 137
5288 deg
Mean motion: 15
78146677 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1720
Checksum: 299
Coasting Arc #5 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2006/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1016946
70 A = 6712921
46 meter
Y = 5209560
17 meter E =
0010769
Z = -4116107
86 I = 51
90801
XDOT = -5334
752139 Wp = 185
91891
YDOT = 4051
876771 meter/sec RA = 116
39003 deg
ZDOT = 3798
870407 TA = 122
94518
MA = 122
84157
Ha = 184
549 n
mi
Hp = 178
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3336439
29 X = 978612
93
Y = 17091732
84 feet Y = 5220718
04 meter
Z = -13504290
88 Z = -4111260
34
XDOT = -17502
467649 XDOT = -5398
119016
YDOT = 13293
558959 feet/sec YDOT = 3991
866180 meter/sec
ZDOT = 12463
485586 ZDOT = 3772
799705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16039134
82 X = -4888728
29
Y = -6820003
53 feet Y = -2078737
07 meter
Z = -13485501
00 Z = -4110380
70
XDOT = -1568
796012 XDOT = -478
169024
YDOT = -20837
489357 feet/sec YDOT = -6351
266756 meter/sec
ZDOT = 12366
643173 ZDOT = 3769
352839
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 06321
50904388
00020000 00000-0 20000-3 0 9042
2 25544 51
6287 117
2081 0011658 225
8778 134
1429 15
78183643 17357
Satellite: ISS
Catalog Number: 25544
Epoch time: 06321
50904388 = yrday
fracday
Element set: 904
Inclination: 51
6287 deg
RA of node: 117
2081 deg
Eccentricity:
0011658
Arg of perigee: 225
8778 deg
Mean anomaly: 134
1429 deg
Mean motion: 15
78183643 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1735
Checksum: 301
Coasting Arc #6 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2006/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4552880
88 A = 6712204
00 meter
Y = -2438603
72 meter E =
0004436
Z = -4283563
70 I = 51
91788
XDOT = 322
968864 Wp = 191
22598
YDOT = 6834
344674 meter/sec RA = 111
29225 deg
ZDOT = -3551
121512 TA = 42
97054
MA = 42
93590
Ha = 184
294 n
mi
Hp = 178
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14937273
23 X = 4600620
70
Y = -8000668
38 feet Y = -2387423
74 meter
Z = -14053686
68 Z = -4261329
31
XDOT = 1059
609133 XDOT = 263
773480
YDOT = 22422
390663 feet/sec YDOT = 6837
625496 meter/sec
ZDOT = -11650
661128 ZDOT = -3549
695922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1567273
56 X = -477704
98
Y = 16940927
92 feet Y = 5163594
83 meter
Z = -13970953
80 Z = -4258346
72
XDOT = -18115
398896 XDOT = -5521
573583
YDOT = -11269
013243 feet/sec YDOT = -3434
795236 meter/sec
ZDOT = -11644
448756 ZDOT = -3549
227981
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 06322
52216522
00020000 00000-0 20000-3 0 9052
2 25544 51
6290 111
9719 0011527 230
3830 129
6319 15
78238999 17515
Satellite: ISS
Catalog Number: 25544
Epoch time: 06322
52216522 = yrday
fracday
Element set: 905
Inclination: 51
6290 deg
RA of node: 111
9719 deg
Eccentricity:
0011527
Arg of perigee: 230
3830 deg
Mean anomaly: 129
6319 deg
Mean motion: 15
78238999 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1751
Checksum: 289
Coasting Arc #7 (Orbit 1766)
---------------------------------------
Vector Time (GMT): 2006/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 361734
68 A = 6718589
05 meter
Y = -6442867
60 meter E =
0012955
Z = 1838899
93 I = 51
94843
XDOT = 5026
091110 Wp = 164
30050
YDOT = -1342
052769 meter/sec RA = 106
10199 deg
ZDOT = -5693
745252 TA = 355
33274
MA = 355
34480
Ha = 183
960 n
mi
Hp = 179
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1186793
59 X = 424819
52
Y = -21138017
06 feet Y = -6438469
89 meter
Z = 6033136
24 Z = 1840810
05
XDOT = 16489
800231 XDOT = 5068
384622
YDOT = -4403
060267 feet/sec YDOT = -1285
611337 meter/sec
ZDOT = -18680
266574 ZDOT = -5669
225105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17239981
30 X = 5254746
30
Y = 12285402
72 feet Y = 3744590
75 meter
Z = 6039445
54 Z = 1840823
00
XDOT = -4263
447055 XDOT = -1299
498662
YDOT = 15116
267270 feet/sec YDOT = 4607
438264 meter/sec
ZDOT = -18588
846258 ZDOT = -5665
880339
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 06323
53525744
00020000 00000-0 20000-3 0 9064
2 25544 51
6286 106
7343 0011602 234
4645 125
5439 15
78265444 17678
Satellite: ISS
Catalog Number: 25544
Epoch time: 06323
53525744 = yrday
fracday
Element set: 906
Inclination: 51
6286 deg
RA of node: 106
7343 deg
Eccentricity:
0011602
Arg of perigee: 234
4645 deg
Mean anomaly: 125
5439 deg
Mean motion: 15
78265444 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1767
Checksum: 294
Coasting Arc #8 (Orbit 1782)
---------------------------------------
Vector Time (GMT): 2006/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4156129
92 A = 6707910
95 meter
Y = -242370
11 meter E =
0010073
Z = 5266345
17 I = 51
92083
XDOT = 1080
118849 Wp = 226
31595
YDOT = -7610
314096 meter/sec RA = 100
97566 deg
ZDOT = 495
947193 TA = 218
95587
MA = 219
02848
Ha = 183
622 n
mi
Hp = 179
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13635596
85 X = -4178694
54
Y = -795177
52 feet Y = -288972
94 meter
Z = 17278035
33 Z = 5246099
24
XDOT = 3543
697012 XDOT = 1162
728872
YDOT = -24968
222100 feet/sec YDOT = -7597
773761 meter/sec
ZDOT = 1627
123338 ZDOT = 501
394497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7825900
27 X = 2385334
40
Y = -11310435
84 feet Y = -3447420
84 meter
Z = 17202373
09 Z = 5243283
32
XDOT = 18655
037234 XDOT = 5686
055349
YDOT = 15443
181176 feet/sec YDOT = 4707
081623 meter/sec
ZDOT = 1646
510540 ZDOT = 501
856413
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 06324
54832038
00020000 00000-0 20000-3 0 9074
2 25544 51
6299 101
4973 0011474 238
9927 121
0112 15
78318285 17831
Satellite: ISS
Catalog Number: 25544
Epoch time: 06324
54832038 = yrday
fracday
Element set: 907
Inclination: 51
6299 deg
RA of node: 101
4973 deg
Eccentricity:
0011474
Arg of perigee: 238
9927 deg
Mean anomaly: 121
0112 deg
Mean motion: 15
78318285 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1783
Checksum: 297
Coasting Arc #9 (Orbit 1798)
---------------------------------------
Vector Time (GMT): 2006/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1468797
08 A = 6719283
75 meter
Y = 6474090
93 meter E =
0002720
Z = 1026673
58 I = 51
96538
XDOT = -4480
346276 Wp = 28
12511
YDOT = -1961
077997 meter/sec RA = 95
83396 deg
ZDOT = 5952
600281 TA = 343
06365
MA = 343
07273
Ha = 183
223 n
mi
Hp = 179
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4818888
06 X = -1546069
64
Y = 21240455
82 feet Y = 6457233
85 meter
Z = 3368351
65 Z = 1019351
04
XDOT = -14699
298807 XDOT = -4487
001709
YDOT = -6433
982931 feet/sec YDOT = -2011
217641 meter/sec
ZDOT = 19529
528480 ZDOT = 5930
817738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15877575
76 X = -4839485
09
Y = -14915072
35 feet Y = -4546114
05 meter
Z = 3341802
36 Z = 1018581
36
XDOT = 11951
370308 XDOT = 3642
777670
YDOT = -8362
252195 feet/sec YDOT = -2548
814469 meter/sec
ZDOT = 19447
905288 ZDOT = 5927
721532
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 06325
56135244
00020000 00000-0 20000-3 0 9083
2 25544 51
6313 96
2604 0011446 242
5492 117
4510 15
78383384 17997
Satellite: ISS
Catalog Number: 25544
Epoch time: 06325
56135244 = yrday
fracday
Element set: 908
Inclination: 51
6313 deg
RA of node: 96
2604 deg
Eccentricity:
0011446
Arg of perigee: 242
5492 deg
Mean anomaly: 117
4510 deg
Mean motion: 15
78383384 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1799
Checksum: 292
Coasting Arc #10 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2006/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3643279
88 A = 6710077
29 meter
Y = 3116885
44 meter E =
0008112
Z = -4697853
85 I = 51
93654
XDOT = -2251
264117 Wp = 180
23203
YDOT = 6825
800063 meter/sec RA = 90
65648 deg
ZDOT = 2774
856500 TA = 117
03177
MA = 116
94895
Ha = 182
866 n
mi
Hp = 179
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11953017
97 X = 3630977
53
Y = 10226002
11 feet Y = 3157558
48 meter
Z = -15412906
34 Z = -4680183
82
XDOT = -7386
037129 XDOT = -2340
903925
YDOT = 22394
357161 feet/sec YDOT = 6800
123597 meter/sec
ZDOT = 9103
859909 ZDOT = 2763
702787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14818080
52 X = -4516550
94
Y = 5469261
28 feet Y = 1667030
84 meter
Z = -15346501
58 Z = -4677613
68
XDOT = -15462
746549 XDOT = -4713
045148
YDOT = -16389
798551 feet/sec YDOT = -4995
610598 meter/sec
ZDOT = 9063
027369 ZDOT = 2762
410742
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 06326
51104455
00020000 00000-0 20000-3 0 9090
2 25544 51
6316 91
3516 0011413 246
9816 113
0146 15
78414952 18141
Satellite: ISS
Catalog Number: 25544
Epoch time: 06326
51104455 = yrday
fracday
Element set: 909
Inclination: 51
6316 deg
RA of node: 91
3516 deg
Eccentricity:
0011413
Arg of perigee: 246
9816 deg
Mean anomaly: 113
0146 deg
Mean motion: 15
78414952 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1814
Checksum: 273
Coasting Arc #11 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2006/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2453914
91 A = 6713831
51 meter
Y = -5082705
43 meter E =
0005979
Z = -3628918
10 I = 51
94924
XDOT = 3853
298253 Wp = 242
56681
YDOT = 5012
377812 meter/sec RA = 85
55560 deg
ZDOT = -4411
952057 TA = 340
80934
MA = 340
83185
Ha = 182
548 n
mi
Hp = 179
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8050901
93 X = 2528197
02
Y = -16675542
75 feet Y = -5054848
53 meter
Z = -11905899
27 Z = -3616817
05
XDOT = 12642
054636 XDOT = 3818
395635
YDOT = 16444
809094 feet/sec YDOT = 5055
273024 meter/sec
ZDOT = -14474
908325 ZDOT = -4393
316417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10805890
72 X = 3293635
49
Y = 15072605
10 feet Y = 4594130
03 meter
Z = -11861302
07 Z = -3615324
87
XDOT = -19417
966207 XDOT = -5918
596100
YDOT = 2578
254552 feet/sec YDOT = 785
851987 meter/sec
ZDOT = -14404
660856 ZDOT = -4390
540629
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 06327
52402016
00020000 00000-0 20000-3 0 9108
2 25544 51
6323 86
1142 0011398 251
2520 108
7409 15
78447112 18304
Satellite: ISS
Catalog Number: 25544
Epoch time: 06327
52402016 = yrday
fracday
Element set: 910
Inclination: 51
6323 deg
RA of node: 86
1142 deg
Eccentricity:
0011398
Arg of perigee: 251
2520 deg
Mean anomaly: 108
7409 deg
Mean motion: 15
78447112 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1830
Checksum: 254
Coasting Arc #12 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2006/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3028587
29 A = 6716366
56 meter
Y = -5363200
09 meter E =
0006283
Z = 2667775
79 I = 51
95500
XDOT = 3392
060641 Wp = 156
21776
YDOT = -4521
825836 meter/sec RA = 80
35955 deg
ZDOT = -5241
069544 TA = 353
47178
MA = 353
47996
Ha = 182
138 n
mi
Hp = 179
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9936310
02 X = -2981349
90
Y = -17595800
84 feet Y = -5396803
70 meter
Z = 8752545
24 Z = 2653176
67
XDOT = 11128
807876 XDOT = 3467
832748
YDOT = -14835
386601 feet/sec YDOT = -4483
469515 meter/sec
ZDOT = -17195
110054 ZDOT = -5224
407276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20217072
77 X = 6162163
78
Y = -758823
47 feet Y = -231289
39 meter
Z = 8697336
81 Z = 2650948
26
XDOT = 7943
822709 XDOT = 2421
277162
YDOT = 15320
725369 feet/sec YDOT = 4669
757093 meter/sec
ZDOT = -17133
390941 ZDOT = -5222
257559
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 06328
53696645
00020000 00000-0 20000-3 0 9114
2 25544 51
6327 80
8774 0011273 255
3251 104
6665 15
78487173 18465
Satellite: ISS
Catalog Number: 25544
Epoch time: 06328
53696645 = yrday
fracday
Element set: 911
Inclination: 51
6327 deg
RA of node: 80
8774 deg
Eccentricity:
0011273
Arg of perigee: 255
3251 deg
Mean anomaly: 104
6665 deg
Mean motion: 15
78487173 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1846
Checksum: 311
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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