Date:
September 16th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12260 09 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 ET - UTC (sec) : 66 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 3767)
---------------------------------------
Vector Time (GMT): 2010/258/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4901524
13 A = 6739747
39 meter
Y = -4352642
09 meter E =
0004152
Z = -1569955
38 I = 51
92970
XDOT = 2204
083297 Wp = 90
23715
YDOT = 4563
261736 meter/sec RA = 127
58216 deg
ZDOT = -5783
262166 TA = 106
97154
MA = 106
92602
Ha = 195
748 n
mi
Hp = 188
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16081115
91 X = 4957458
43
Y = -14280321
81 feet Y = -4297517
58 meter
Z = -5150772
24 Z = -1546007
87
XDOT = 7231
244413 XDOT = 2180
986268
YDOT = 14971
331156 feet/sec YDOT = 4587
779885 meter/sec
ZDOT = -18973
957238 ZDOT = -5772
610914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17438227
25 X = -5315171
67
Y = 12626048
41 feet Y = 3848419
56 meter
Z = -5054845
83 Z = -1540717
01
XDOT = -4914
398954 XDOT = -1497
908801
YDOT = -14348
999307 feet/sec YDOT = -4373
574989 meter/sec
ZDOT = -18931
208243 ZDOT = -5770
232272
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 10258
53102900
00016717 00000-0 10270-3 0 9003
2 25544 51
6449 128
3626 0006580 352
9001 7
2067 15
70981266 37689
Satellite: ISS
Catalog Number: 25544
Epoch time: 10258
53102900 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 128
3626 deg
Eccentricity:
0006580
Arg of perigee: 352
9001 deg
Mean anomaly: 7
2067 deg
Mean motion: 15
70981266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3768
Checksum: 296
Coasting Arc #2 (Orbit 3783)
---------------------------------------
Vector Time (GMT): 2010/259/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3056344
40 A = 6728676
36 meter
Y = -2874886
06 meter E =
0008392
Z = 5258926
65 I = 51
91072
XDOT = 4568
638169 Wp = 16
16974
YDOT = -6155
539623 meter/sec RA = 122
46835 deg
ZDOT = -701
717634 TA = 80
52878
MA = 80
43394
Ha = 195
876 n
mi
Hp = 188
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10027376
63 X = -3049516
54
Y = -9432040
86 feet Y = -2909025
64 meter
Z = 17253696
35 Z = 5244095
64
XDOT = 14988
970370 XDOT = 4640
539797
YDOT = -20195
339970 feet/sec YDOT = -6104
048362 meter/sec
ZDOT = -2302
223208 ZDOT = -679
348500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9329698
14 X = 2843691
99
Y = 10223379
24 feet Y = 3116085
99 meter
Z = 17194213
10 Z = 5240796
15
XDOT = -15848
221775 XDOT = -4830
537997
YDOT = 18229
291085 feet/sec YDOT = 5556
287923 meter/sec
ZDOT = -2212
632242 ZDOT = -674
410307
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 10259
54878812
00016717 00000-0 10270-3 0 9018
2 25544 51
6449 123
1588 0006730 356
9862 3
1258 15
71046921 37841
Satellite: ISS
Catalog Number: 25544
Epoch time: 10259
54878812 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 123
1588 deg
Eccentricity:
0006730
Arg of perigee: 356
9862 deg
Mean anomaly: 3
1258 deg
Mean motion: 15
71046921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3784
Checksum: 323
Coasting Arc #3 (Orbit 3798)
---------------------------------------
Vector Time (GMT): 2010/260/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2833479
54 A = 6740499
82 meter
Y = 6094124
80 meter E =
0017099
Z = -366025
50 I = 51
96511
XDOT = -4445
199195 Wp = 26
86323
YDOT = -1710
772696 meter/sec RA = 117
37800 deg
ZDOT = 6051
664769 TA = 329
17763
MA = 329
27792
Ha = 195
907 n
mi
Hp = 187
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9296192
72 X = -2899636
50
Y = 19993847
78 feet Y = 6062069
22 meter
Z = -1200871
07 Z = -379951
36
XDOT = -14583
986859 XDOT = -4455
136338
YDOT = -5612
771312 feet/sec YDOT = -1760
536927 meter/sec
ZDOT = 19854
543204 ZDOT = 6030
046061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10551366
29 X = 3216056
45
Y = -19357293
11 feet Y = -5900102
94 meter
Z = -1256627
27 Z = -383019
99
XDOT = 12899
991641 XDOT = 3931
917452
YDOT = 5773
523923 feet/sec YDOT = 1759
770092 meter/sec
ZDOT = 19767
859656 ZDOT = 6025
243623
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 10260
50292511
00016717 00000-0 10270-3 0 9023
2 25544 51
6442 118
2802 0006811
0855
0307 15
71058383 37999
Satellite: ISS
Catalog Number: 25544
Epoch time: 10260
50292511 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 118
2802 deg
Eccentricity:
0006811
Arg of perigee:
0855 deg
Mean anomaly:
0307 deg
Mean motion: 15
71058383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 266
Coasting Arc #4 (Orbit 3814)
---------------------------------------
Vector Time (GMT): 2010/261/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4356860
69 A = 6729180
30 meter
Y = -11768
65 meter E =
0016929
Z = -5142349
21 I = 51
93891
XDOT = -1746
361952 Wp = 55
82242
YDOT = 7333
128411 meter/sec RA = 112
30217 deg
ZDOT = -1490
581879 TA = 199
88169
MA = 199
94774
Ha = 195
966 n
mi
Hp = 187
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14294162
38 X = 4381648
89
Y = -38611
06 feet Y = 37090
71 meter
Z = -16871224
44 Z = -5121123
53
XDOT = -5729
533962 XDOT = -1820
991629
YDOT = 24058
820245 feet/sec YDOT = 7313
182188 meter/sec
ZDOT = -4890
360494 ZDOT = -1499
247300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14379976
66 X = -4383016
89
Y = -636305
77 feet Y = -193946
00 meter
Z = -16786130
27 Z = -5116412
51
XDOT = 6776
636578 XDOT = 2065
518829
YDOT = -22716
082663 feet/sec YDOT = -6923
861996 meter/sec
ZDOT = -4925
021087 ZDOT = -1501
146427
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 10261
52065660
00016717 00000-0 10270-3 0 9030
2 25544 51
6430 113
0760 0006818 3
5058 356
6150 15
71084083 38153
Satellite: ISS
Catalog Number: 25544
Epoch time: 10261
52065660 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 113
0760 deg
Eccentricity:
0006818
Arg of perigee: 3
5058 deg
Mean anomaly: 356
6150 deg
Mean motion: 15
71084083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3815
Checksum: 277
Coasting Arc #5 (Orbit 3830)
---------------------------------------
Vector Time (GMT): 2010/262/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 173971
93 A = 6738240
92 meter
Y = -6366495
06 meter E =
0014257
Z = 2192666
44 I = 51
98102
XDOT = 5062
247826 Wp = 80
55034
YDOT = -1772
737504 meter/sec RA = 107
17979 deg
ZDOT = -5516
323195 TA = 75
04325
MA = 74
88546
Ha = 195
987 n
mi
Hp = 187
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 570774
06 X = 234498
82
Y = -20887450
98 feet Y = -6364211
02 meter
Z = 7193787
52 Z = 2193659
06
XDOT = 16608
424625 XDOT = 5108
491784
YDOT = -5816
067925 feet/sec YDOT = -1715
870238 meter/sec
ZDOT = -18098
173213 ZDOT = -5491
618515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1148897
96 X = -350184
10
Y = 20862288
82 feet Y = 6358825
63 meter
Z = 7197701
65 Z = 2193859
46
XDOT = -15359
752382 XDOT = -4681
652526
YDOT = 5400
834264 feet/sec YDOT = 1646
174284 meter/sec
ZDOT = -17999
144702 ZDOT = -5486
139305
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 10262
53837256
00016717 00000-0 10270-3 0 9041
2 25544 51
6436 107
8725 0006961 6
6750 353
4504 15
71141732 38314
Satellite: ISS
Catalog Number: 25544
Epoch time: 10262
53837256 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 107
8725 deg
Eccentricity:
0006961
Arg of perigee: 6
6750 deg
Mean anomaly: 353
4504 deg
Mean motion: 15
71141732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3831
Checksum: 299
Coasting Arc #6 (Orbit 3846)
---------------------------------------
Vector Time (GMT): 2010/263/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4133409
16 A = 6732310
42 meter
Y = 3035660
81 meter E =
0010994
Z = 4350598
10 I = 51
96698
XDOT = -1315
924343 Wp = 70
70808
YDOT = -6755
109817 meter/sec RA = 102
13208 deg
ZDOT = 3459
702087 TA = 344
50838
MA = 344
54200
Ha = 196
254 n
mi
Hp = 187
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13561053
67 X = -4188181
60
Y = 9959517
10 feet Y = 2989132
68 meter
Z = 14273615
80 Z = 4330384
78
XDOT = -4317
337083 XDOT = -1257
096190
YDOT = -22162
433784 feet/sec YDOT = -6769
496044 meter/sec
ZDOT = 11350
728633 ZDOT = 3453
452842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13769269
97 X = 4196873
49
Y = -9788130
29 feet Y = -2983422
11 meter
Z = 14192602
84 Z = 4325905
35
XDOT = 3392
690043 XDOT = 1034
091925
YDOT = 21211
229415 feet/sec YDOT = 6465
182726 meter/sec
ZDOT = 11325
607780 ZDOT = 3452
045251
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 10263
55607602
00016717 00000-0 10270-3 0 9055
2 25544 51
6421 102
6676 0006891 10
6950 349
4357 15
71101202 38471
Satellite: ISS
Catalog Number: 25544
Epoch time: 10263
55607602 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 102
6676 deg
Eccentricity:
0006891
Arg of perigee: 10
6950 deg
Mean anomaly: 349
4357 deg
Mean motion: 15
71101202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3847
Checksum: 290
Coasting Arc #7 (Orbit 3861)
---------------------------------------
Vector Time (GMT): 2010/264/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2334408
64 A = 6734235
94 meter
Y = 5081374
25 meter E =
0009140
Z = -3754345
23 I = 51
97816
XDOT = -3988
114847 Wp = 55
43944
YDOT = 4989
627472 meter/sec RA = 96
99096 deg
ZDOT = 4285
926030 TA = 259
52277
MA = 259
62577
Ha = 196
145 n
mi
Hp = 187
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7658821
00 X = 2295652
19
Y = 16671175
37 feet Y = 5107261
93 meter
Z = -12317405
61 Z = -3743099
34
XDOT = -13084
366297 XDOT = -4064
433612
YDOT = 16370
168873 feet/sec YDOT = 4944
603688 meter/sec
ZDOT = 14061
437105 ZDOT = 4266
365909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7809474
48 X = -2380327
82
Y = -16634529
77 feet Y = -5070204
67 meter
Z = -12272271
02 Z = -3740588
21
XDOT = 11878
005993 XDOT = 3620
416227
YDOT = -15862
399643 feet/sec YDOT = -4834
859411 meter/sec
ZDOT = 13983
056733 ZDOT = 4262
035692
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 10264
51015658
00016717 00000-0 10270-3 0 9067
2 25544 51
6411 97
7879 0006744 14
6797 345
4560 15
71149114 38622
Satellite: ISS
Catalog Number: 25544
Epoch time: 10264
51015658 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 97
7879 deg
Eccentricity:
0006744
Arg of perigee: 14
6797 deg
Mean anomaly: 345
4560 deg
Mean motion: 15
71149114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3862
Checksum: 323
Coasting Arc #8 (Orbit 3877)
---------------------------------------
Vector Time (GMT): 2010/265/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2572460
67 A = 6736217
16 meter
Y = -5432575
69 meter E =
0008264
Z = -3052552
79 I = 51
98720
XDOT = 3721
764414 Wp = 51
70586
YDOT = 4545
229206 meter/sec RA = 91
95105 deg
ZDOT = -4956
661946 TA = 163
37330
MA = 163
34619
Ha = 196
177 n
mi
Hp = 187
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8439831
59 X = 2647846
34
Y = -17823411
05 feet Y = -5403387
72 meter
Z = -10014936
98 Z = -3039872
03
XDOT = 12210
513168 XDOT = 3694
740864
YDOT = 14912
169312 feet/sec YDOT = 4586
696575 meter/sec
ZDOT = -16262
014258 ZDOT = -4938
647690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8107309
79 X = -2471108
02
Y = 18005310
37 feet Y = 5488018
60 meter
Z = -9964137
08 Z = -3037068
98
XDOT = -11316
939802 XDOT = -3449
403252
YDOT = -14047
791327 feet/sec YDOT = -4281
766796 meter/sec
ZDOT = -16189
751724 ZDOT = -4934
636325
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 10265
52782838
00016717 00000-0 10270-3 0 9071
2 25544 51
6406 92
5838 0006870 18
6600 341
4813 15
71181076 38788
Satellite: ISS
Catalog Number: 25544
Epoch time: 10265
52782838 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 92
5838 deg
Eccentricity:
0006870
Arg of perigee: 18
6600 deg
Mean anomaly: 341
4813 deg
Mean motion: 15
71181076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3878
Checksum: 323
Coasting Arc #9 (Orbit 3893)
---------------------------------------
Vector Time (GMT): 2010/266/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3904142
28 A = 6730336
26 meter
Y = -2650601
84 meter E =
0013305
Z = 4795215
99 I = 51
96702
XDOT = 1623
014057 Wp = 42
15484
YDOT = -7071
885237 meter/sec RA = 86
81572 deg
ZDOT = -2573
895435 TA = 73
03438
MA = 72
88859
Ha = 196
297 n
mi
Hp = 186
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12808865
76 X = -3897507
08
Y = -8696200
26 feet Y = -2694222
67 meter
Z = 15732335
92 Z = 4776265
93
XDOT = 5324
849269 XDOT = 1714
476177
YDOT = -23201
723220 feet/sec YDOT = -7053
224613 meter/sec
ZDOT = -8444
538828 ZDOT = -2565
787822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13231791
95 X = 4033050
19
Y = 8185110
12 feet Y = 2494821
57 meter
Z = 15656340
20 Z = 4772052
49
XDOT = -3867
586169 XDOT = -1178
840264
YDOT = 22429
348402 feet/sec YDOT = 6836
465393 meter/sec
ZDOT = -8412
078363 ZDOT = -2564
001485
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 10266
54548469
00016717 00000-0 10270-3 0 9085
2 25544 51
6405 87
3785 0006733 22
1938 337
9514 15
71179095 38946
Satellite: ISS
Catalog Number: 25544
Epoch time: 10266
54548469 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 87
3785 deg
Eccentricity:
0006733
Arg of perigee: 22
1938 deg
Mean anomaly: 337
9514 deg
Mean motion: 15
71179095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3894
Checksum: 345
Coasting Arc #10 (Orbit 3909)
---------------------------------------
Vector Time (GMT): 2010/267/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -133615
98 A = 6739310
33 meter
Y = 6584369
31 meter E =
0019959
Z = 1377236
53 I = 51
99443
XDOT = -4819
792694 Wp = 49
36266
YDOT = -1332
299649 meter/sec RA = 81
75715 deg
ZDOT = 5859
665882 TA = 325
69454
MA = 325
82328
Ha = 196
279 n
mi
Hp = 186
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -438372
63 X = -213924
13
Y = 21602261
53 feet Y = 6582426
26 meter
Z = 4518492
54 Z = 1376391
64
XDOT = -15812
968156 XDOT = -4833
002005
YDOT = -4371
061842 feet/sec YDOT = -1386
270701 meter/sec
ZDOT = 19224
625596 ZDOT = 5836
219099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -750562
67 X = -228771
50
Y = -21594370
46 feet Y = -6581964
11 meter
Z = 4515137
75 Z = 1376213
99
XDOT = 14572
654962 XDOT = 4441
745232
YDOT = 3522
500449 feet/sec YDOT = 1073
658137 meter/sec
ZDOT = 19130
612180 ZDOT = 5831
010592
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 10267
56312524
00016717 00000-0 10270-3 0 9090
2 25544 51
6402 82
1731 0006760 26
7309 333
4200 15
71212165 39107
Satellite: ISS
Catalog Number: 25544
Epoch time: 10267
56312524 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 82
1731 deg
Eccentricity:
0006760
Arg of perigee: 26
7309 deg
Mean anomaly: 333
4200 deg
Mean motion: 15
71212165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3910
Checksum: 271
Coasting Arc #11 (Orbit 3924)
---------------------------------------
Vector Time (GMT): 2010/268/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4168273
71 A = 6728081
02 meter
Y = -349391
87 meter E =
0018927
Z = -5285077
21 I = 51
95197
XDOT = 1338
064496 Wp = 75
71439
YDOT = 7544
955736 meter/sec RA = 76
64839 deg
ZDOT = 562
752120 TA = 199
58588
MA = 199
65868
Ha = 196
317 n
mi
Hp = 186
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13675438
69 X = 4197545
24
Y = -1146298
80 feet Y = -302616
57 meter
Z = -17339492
15 Z = -5264756
29
XDOT = 4389
975380 XDOT = 1250
862168
YDOT = 24753
791784 feet/sec YDOT = 7559
431255 meter/sec
ZDOT = 1846
299605 ZDOT = 569
040010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13656703
04 X = -4162563
09
Y = 2155186
31 feet Y = 656900
79 meter
Z = -17258019
78 Z = -5260244
43
XDOT = -6027
136792 XDOT = -1837
071294
YDOT = -23369
743679 feet/sec YDOT = -7123
097873 meter/sec
ZDOT = 1871
533707 ZDOT = 570
443474
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 10268
51714840
00016717 00000-0 10270-3 0 9105
2 25544 51
6408 77
2939 0006774 31
4817 328
6749 15
71243495 39250
Satellite: ISS
Catalog Number: 25544
Epoch time: 10268
51714840 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 77
2939 deg
Eccentricity:
0006774
Arg of perigee: 31
4817 deg
Mean anomaly: 328
6749 deg
Mean motion: 15
71243495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3925
Checksum: 329
Coasting Arc #12 (Orbit 3940)
---------------------------------------
Vector Time (GMT): 2010/269/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2412464
17 A = 6739777
27 meter
Y = -6278713
92 meter E =
0013752
Z = 386619
74 I = 51
98396
XDOT = 4301
847114 Wp = 101
01355
YDOT = -2036
029181 meter/sec RA = 71
55716 deg
ZDOT = -6044
258284 TA = 74
80944
MA = 74
65740
Ha = 196
275 n
mi
Hp = 186
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7914908
70 X = -2343953
29
Y = -20599455
12 feet Y = -6305308
45 meter
Z = 1268437
47 Z = 375066
68
XDOT = 14113
671633 XDOT = 4353
657078
YDOT = -6679
885763 feet/sec YDOT = -1987
634119 meter/sec
ZDOT = -19830
243714 ZDOT = -6023
233540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9755095
37 X = 2973353
07
Y = 19797394
44 feet Y = 6034245
83 meter
Z = 1222109
69 Z = 372499
03
XDOT = -12124
011619 XDOT = -3695
398742
YDOT = 7230
384185 feet/sec YDOT = 2203
821100 meter/sec
ZDOT = -19745
950754 ZDOT = -6018
565790
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 10269
53475547
00016717 00000-0 10270-3 0 9117
2 25544 51
6409 72
0885 0006927 32
9945 327
1648 15
71310956 39419
Satellite: ISS
Catalog Number: 25544
Epoch time: 10269
53475547 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 72
0885 deg
Eccentricity:
0006927
Arg of perigee: 32
9945 deg
Mean anomaly: 327
1648 deg
Mean motion: 15
71310956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3941
Checksum: 330
Coasting Arc #13 (Orbit 3956)
---------------------------------------
Vector Time (GMT): 2010/270/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3043380
64 A = 6728519
93 meter
Y = 3088850
62 meter E =
0008386
Z = 5137533
98 I = 51
93554
XDOT = -4031
932286 Wp = 70
68795
YDOT = -6399
360528 meter/sec RA = 66
48025 deg
ZDOT = 1459
851892 TA = 5
38834
MA = 5
37933
Ha = 196
491 n
mi
Hp = 186
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9984844
62 X = -3102652
21
Y = 10134024
33 feet Y = 3054486
59 meter
Z = 16855426
43 Z = 5122604
82
XDOT = -13228
124298 XDOT = -3967
165615
YDOT = -20995
277324 feet/sec YDOT = -6444
085804 meter/sec
ZDOT = 4789
540329 ZDOT = 1440
422095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8934849
22 X = 2723342
04
Y = -11161467
33 feet Y = -3402015
24 meter
Z = 16795567
51 Z = 5119288
98
XDOT = 14625
897062 XDOT = 4457
973425
YDOT = 18794
218447 feet/sec YDOT = 5728
477783 meter/sec
ZDOT = 4711
643667 ZDOT = 1436
108990
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 10270
55234945
00016717 00000-0 10270-3 0 9127
2 25544 51
6413 66
8836 0006848 38
2262 321
9384 15
71284944 39577
Satellite: ISS
Catalog Number: 25544
Epoch time: 10270
55234945 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 66
8836 deg
Eccentricity:
0006848
Arg of perigee: 38
2262 deg
Mean anomaly: 321
9384 deg
Mean motion: 15
71284944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3957
Checksum: 328
Coasting Arc #14 (Orbit 3971)
---------------------------------------
Vector Time (GMT): 2010/271/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4416894
62 A = 6737907
26 meter
Y = 4617925
14 meter E =
0013269
Z = -2124790
13 I = 51
95574
XDOT = -2341
653474 Wp = 41
67645
YDOT = 4782
548275 meter/sec RA = 61
35652 deg
ZDOT = 5555
865445 TA = 294
70487
MA = 294
84294
Ha = 196
434 n
mi
Hp = 186
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14491124
07 X = 4375249
87
Y = 15150673
04 feet Y = 4667084
58 meter
Z = -6971096
22 Z = -2103433
83
XDOT = -7682
590139 XDOT = -2421
948617
YDOT = 15690
775180 feet/sec YDOT = 4755
913758 meter/sec
ZDOT = 18227
905003 ZDOT = 5544
294279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16308807
73 X = -4970924
60
Y = -13219103
39 feet Y = -4029182
71 meter
Z = -6885481
01 Z = -2098694
61
XDOT = 4808
194411 XDOT = 1465
537657
YDOT = -15351
437441 feet/sec YDOT = -4679
118132 meter/sec
ZDOT = 18181
498480 ZDOT = 5541
720737
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 10271
50632651
00016717 00000-0 10270-3 0 9130
2 25544 51
6429 62
0048 0006822 42
6925 317
4765 15
71317009 39723
Satellite: ISS
Catalog Number: 25544
Epoch time: 10271
50632651 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 62
0048 deg
Eccentricity:
0006822
Arg of perigee: 42
6925 deg
Mean anomaly: 317
4765 deg
Mean motion: 15
71317009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3972
Checksum: 297
Coasting Arc #15 (Orbit 3987)
---------------------------------------
Vector Time (GMT): 2010/272/12:03:09
023
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 876550
77 A = 6731162
61 meter
Y = -4981543
34 meter E =
0016091
Z = -4457607
51 I = 51
91828
XDOT = 5719
613018 Wp = 59
24669
YDOT = 3942
443266 meter/sec RA = 56
30497 deg
ZDOT = -3281
803807 TA = 177
89081
MA = 177
88401
Ha = 196
395 n
mi
Hp = 185
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2875822
72 X = 953844
71
Y = -16343646
11 feet Y = -4971309
16 meter
Z = -14624696
56 Z = -4453161
29
XDOT = 18765
134574 XDOT = 5691
045423
YDOT = 12934
525152 feet/sec YDOT = 4006
243598 meter/sec
ZDOT = -10767
072856 ZDOT = -3254
087037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -614939
17 X = -187433
46
Y = 16599057
36 feet Y = 5059392
68 meter
Z = -14606848
35 Z = -4452167
38
XDOT = -19262
125073 XDOT = -5871
095722
YDOT = -10088
639832 feet/sec YDOT = -3075
017421 meter/sec
ZDOT = -10655
957012 ZDOT = -3247
935697
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 10272
52388553
00016717 00000-0 10270-3 0 9143
2 25544 51
6432 56
8006 0006896 45
8544 314
3184 15
71351077 39886
Satellite: ISS
Catalog Number: 25544
Epoch time: 10272
52388553 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 56
8006 deg
Eccentricity:
0006896
Arg of perigee: 45
8544 deg
Mean anomaly: 314
3184 deg
Mean motion: 15
71351077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3988
Checksum: 323
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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