[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 10th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 ET - UTC (sec) : 67 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
258/03:19:38
134 -3
4 4
2 4
2
N/A -1
6 -0
5 234
6
000/00:09:16
267 2
0 -0
0 214
8
Coasting Arc #1 (Orbit 3128)
---------------------------------------
Vector Time (GMT): 2012/254/12:55:11
385
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4567859
96 A = 6789457
47 meter
Y = 224184
39 meter E =
0021542
Z = 5006548
53 I = 51
92244
XDOT = -2642
826285 Wp = 55
81327
YDOT = -6893
996618 meter/sec RA = 56
24715 deg
ZDOT = -2084
358100 TA = 54
47781
MA = 54
27709
Ha = 232
312 n
mi
Hp = 215
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14986417
20 X = -4594347
88
Y = 735513
09 feet Y = 172955
87 meter
Z = 16425684
14 Z = 4984293
85
XDOT = -8670
689912 XDOT = -2555
414483
YDOT = -22618
099139 feet/sec YDOT = -6923
061702 meter/sec
ZDOT = -6838
445210 ZDOT = -2096
984101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15028673
77 X = 4580739
76
Y = -1512968
24 feet Y = -461152
72 meter
Z = 16333605
59 Z = 4978482
98
XDOT = 9672
389588 XDOT = 2948
144346
YDOT = 21047
953277 feet/sec YDOT = 6415
416159 meter/sec
ZDOT = -6889
953030 ZDOT = -2100
057683
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 12254
58306973
00016717 00000-0 10270-3 0 9002
2 25544 51
6441 56
6937 0015387 55
8183 304
4424 15
50480159 31297
Satellite: ISS
Catalog Number: 25544
Epoch time: 12254
58306973 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 56
6937 deg
Eccentricity:
0015387
Arg of perigee: 55
8183 deg
Mean anomaly: 304
4424 deg
Mean motion: 15
50480159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3129
Checksum: 313
Coasting Arc #2 (Orbit 3143)
---------------------------------------
Vector Time (GMT): 2012/255/12:55:11
385
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4787523
30 A = 6790082
94 meter
Y = -82869
04 meter E =
0024266
Z = -4833091
27 I = 51
90858
XDOT = 2722
514974 Wp = 79
39883
YDOT = 6656
686912 meter/sec RA = 51
30620 deg
ZDOT = 2598
127727 TA = 216
09509
MA = 216
25915
Ha = 232
135 n
mi
Hp = 215
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15707097
44 X = 4811572
02
Y = -271880
06 feet Y = -29197
80 meter
Z = -15856598
65 Z = -4809775
46
XDOT = 8932
135741 XDOT = 2635
255158
YDOT = 21839
523990 feet/sec YDOT = 6686
644032 meter/sec
ZDOT = 8524
041098 ZDOT = 2611
141121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15747772
76 X = -4799921
14
Y = 1357952
54 feet Y = 413903
93 meter
Z = -15760144
91 Z = -4803692
17
XDOT = -10260
198001 XDOT = -3127
308351
YDOT = -20030
081727 feet/sec YDOT = -6105
168910 meter/sec
ZDOT = 8577
171741 ZDOT = 2614
321947
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 12255
54984044
00016717 00000-0 10270-3 0 9011
2 25544 51
6453 51
9014 0015341 58
9548 301
3107 15
50538172 31443
Satellite: ISS
Catalog Number: 25544
Epoch time: 12255
54984044 = yrday
fracday
Element set: 901
Inclination: 51
6453 deg
RA of node: 51
9014 deg
Eccentricity:
0015341
Arg of perigee: 58
9548 deg
Mean anomaly: 301
3107 deg
Mean motion: 15
50538172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3144
Checksum: 288
Coasting Arc #3 (Orbit 3159)
---------------------------------------
Vector Time (GMT): 2012/256/12:55:11
385
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5031177
00 A = 6791132
24 meter
Y = -108549
73 meter E =
0024229
Z = 4546875
11 I = 51
89212
XDOT = -2728
445033 Wp = 64
21926
YDOT = -6440
852215 meter/sec RA = 46
36184 deg
ZDOT = -3149
513306 TA = 57
34891
MA = 57
11538
Ha = 232
272 n
mi
Hp = 215
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16506486
23 X = -5051676
75
Y = -356134
30 feet Y = -164925
75 meter
Z = 14917569
27 Z = 4522384
32
XDOT = -8951
591317 XDOT = -2640
919813
YDOT = -21131
404906 feet/sec YDOT = -6470
874259 meter/sec
ZDOT = -10333
048905 ZDOT = -3162
554740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16566704
27 X = 5049531
46
Y = -1071010
07 feet Y = -326443
87 meter
Z = 14816276
16 Z = 4516000
97
XDOT = 10591
453535 XDOT = 3228
275037
YDOT = 19082
926676 feet/sec YDOT = 5816
476051 meter/sec
ZDOT = -10386
314769 ZDOT = -3165
748741
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 12256
58104494
00016717 00000-0 10270-3 0 9020
2 25544 51
6450 46
7870 0015386 62
8135 297
4582 15
50546022 31600
Satellite: ISS
Catalog Number: 25544
Epoch time: 12256
58104494 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 46
7870 deg
Eccentricity:
0015386
Arg of perigee: 62
8135 deg
Mean anomaly: 297
4582 deg
Mean motion: 15
50546022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3160
Checksum: 304
Coasting Arc #4 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2012/257/12:55:11
385
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5286011
44 A = 6792045
95 meter
Y = 187216
66 meter E =
0021847
Z = -4277038
50 I = 51
87501
XDOT = 2697
818779 Wp = 80
24785
YDOT = 6172
589607 meter/sec RA = 41
41922 deg
ZDOT = 3623
804932 TA = 226
69003
MA = 226
87240
Ha = 232
124 n
mi
Hp = 214
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17342557
21 X = 5304301
79
Y = 614227
89 feet Y = 246429
97 meter
Z = -14032278
53 Z = -4251315
10
XDOT = 8851
111480 XDOT = 2610
991610
YDOT = 20251
278237 feet/sec YDOT = 6202
273191 meter/sec
ZDOT = 11889
123793 ZDOT = 3636
699173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17398636
62 X = -5303104
44
Y = 1184576
56 feet Y = 361058
94 meter
Z = -13925897
80 Z = -4244613
65
XDOT = -10730
584303 XDOT = -3270
682095
YDOT = -17971
704127 feet/sec YDOT = -5477
775418 meter/sec
ZDOT = 11941
805789 ZDOT = 3639
862405
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 12257
54777892
00016717 00000-0 10270-3 0 9036
2 25544 51
6461 41
9943 0015335 65
6119 294
6631 15
50590545 31756
Satellite: ISS
Catalog Number: 25544
Epoch time: 12257
54777892 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 41
9943 deg
Eccentricity:
0015335
Arg of perigee: 65
6119 deg
Mean anomaly: 294
6631 deg
Mean motion: 15
50590545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 326
Coasting Arc #5 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2012/258/03:24:16
267
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1483847
49 A = 6790265
16 meter
Y = 4057977
20 meter E =
0021168
Z = 5219608
50 I = 51
84963
XDOT = -6481
863367 Wp = 73
94505
YDOT = -3931
645269 meter/sec RA = 38
47533 deg
ZDOT = 1215
599938 TA = 4
44957
MA = 4
43078
Ha = 234
618 n
mi
Hp = 214
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4868266
04 X = -1554469
85
Y = 13313573
49 feet Y = 4040989
62 meter
Z = 17124699
79 Z = 5212228
08
XDOT = -21265
955930 XDOT = -6443
322215
YDOT = -12899
098650 feet/sec YDOT = -4003
913872 meter/sec
ZDOT = 3988
188774 ZDOT = 1184
205631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5620797
64 X = 1713219
12
Y = 13054393
50 feet Y = 3978979
14 meter
Z = 17093742
73 Z = 5210172
78
XDOT = -23344
464846 XDOT = -7115
392885
YDOT = 5005
654627 feet/sec YDOT = 1525
723530 meter/sec
ZDOT = 3858
750967 ZDOT = 1176
147295
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 12258
19229172
00016717 00000-0 10270-3 0 9042
2 25544 51
6475 38
8038 0018842 65
2714 295
0395 15
49852110 31854
Satellite: ISS
Catalog Number: 25544
Epoch time: 12258
19229172 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 38
8038 deg
Eccentricity:
0018842
Arg of perigee: 65
2714 deg
Mean anomaly: 295
0395 deg
Mean motion: 15
49852110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 320
Coasting Arc #6 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2012/259/03:24:16
267
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1450771
33 A = 6790066
79 meter
Y = -4032918
62 meter E =
0033152
Z = -5295264
15 I = 51
82565
XDOT = 6683
247956 Wp = 74
52518
YDOT = 3584
830990 meter/sec RA = 33
53396 deg
ZDOT = -895
281433 TA = 186
87558
MA = 186
92117
Ha = 234
597 n
mi
Hp = 214
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4759748
44 X = 1521483
54
Y = -13231360
32 feet Y = -4016300
51 meter
Z = -17372913
89 Z = -5288044
11
XDOT = 21926
666522 XDOT = 6647
013976
YDOT = 11761
256530 feet/sec YDOT = 3659
364526 meter/sec
ZDOT = -2937
275044 ZDOT = -862
903116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5862609
36 X = -1786923
33
Y = -12822070
11 feet Y = -3908166
97 meter
Z = -17342622
86 Z = -5286031
45
XDOT = 22928
045265 XDOT = 6988
468197
YDOT = -6673
728248 feet/sec YDOT = -2034
152370 meter/sec
ZDOT = -2803
738622 ZDOT = -854
579532
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 12259
15949841
00016717 00000-0 10270-3 0 9052
2 25544 51
6486 34
0132 0018977 68
5131 291
8041 15
49861554 32009
Satellite: ISS
Catalog Number: 25544
Epoch time: 12259
15949841 = yrday
fracday
Element set: 905
Inclination: 51
6486 deg
RA of node: 34
0132 deg
Eccentricity:
0018977
Arg of perigee: 68
5131 deg
Mean anomaly: 291
8041 deg
Mean motion: 15
49861554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 315
Coasting Arc #7 (Orbit 3215)
---------------------------------------
Vector Time (GMT): 2012/260/03:24:16
267
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1442782
10 A = 6789723
16 meter
Y = 3964996
88 meter E =
0021044
Z = 5301481
61 I = 51
79936
XDOT = -6924
447799 Wp = 76
37107
YDOT = -3268
964116 meter/sec RA = 28
59070 deg
ZDOT = 563
373282 TA = 8
28875
MA = 8
25404
Ha = 234
571 n
mi
Hp = 214
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4733537
09 X = -1512765
73
Y = 13008519
96 feet Y = 3948472
21 meter
Z = 17393312
36 Z = 5294302
10
XDOT = -22718
004590 XDOT = -6890
115664
YDOT = -10724
947888 feet/sec YDOT = -3346
205573 meter/sec
ZDOT = 1848
337538 ZDOT = 529
818429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5940889
94 X = 1810783
25
Y = 12545140
07 feet Y = 3823758
69 meter
Z = 17363195
77 Z = 5292302
07
XDOT = -22627
892407 XDOT = -6896
981606
YDOT = 8362
585942 feet/sec YDOT = 2548
916195 meter/sec
ZDOT = 1709
912019 ZDOT = 521
181183
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 12260
19116362
00016717 00000-0 10270-3 0 9063
2 25544 51
6487 28
9032 0018839 72
0909 288
2294 15
49911742 32163
Satellite: ISS
Catalog Number: 25544
Epoch time: 12260
19116362 = yrday
fracday
Element set: 906
Inclination: 51
6487 deg
RA of node: 28
9032 deg
Eccentricity:
0018839
Arg of perigee: 72
0909 deg
Mean anomaly: 288
2294 deg
Mean motion: 15
49911742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3216
Checksum: 320
Coasting Arc #8 (Orbit 3230)
---------------------------------------
Vector Time (GMT): 2012/261/03:24:16
267
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1457027
01 A = 6789655
59 meter
Y = -3960464
82 meter E =
0033504
Z = -5347726
43 I = 51
77291
XDOT = 7060
542975 Wp = 80
67696
YDOT = 2901
377913 meter/sec RA = 23
64553 deg
ZDOT = -220
938947 TA = 187
18832
MA = 187
23648
Ha = 234
520 n
mi
Hp = 214
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4780272
35 X = 1527183
67
Y = -12993650
98 feet Y = -3943779
86 meter
Z = -17545034
20 Z = -5340477
29
XDOT = 23164
511074 XDOT = 7028
647684
YDOT = 9518
956406 feet/sec YDOT = 2980
154943 meter/sec
ZDOT = -724
865313 ZDOT = -186
716796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6112316
27 X = -1863034
00
Y = -12465615
31 feet Y = -3799519
55 meter
Z = -17514628
73 Z = -5338458
84
XDOT = 21902
120866 XDOT = 6675
766440
YDOT = -9900
409097 feet/sec YDOT = -3017
644693 meter/sec
ZDOT = -583
652669 ZDOT = -177
897333
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 12261
15833314
00016717 00000-0 10270-3 0 9074
2 25544 51
6496 24
1127 0018910 75
2625 285
0620 15
49922368 32317
Satellite: ISS
Catalog Number: 25544
Epoch time: 12261
15833314 = yrday
fracday
Element set: 907
Inclination: 51
6496 deg
RA of node: 24
1127 deg
Eccentricity:
0018910
Arg of perigee: 75
2625 deg
Mean anomaly: 285
0620 deg
Mean motion: 15
49922368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3231
Checksum: 295
Coasting Arc #9 (Orbit 3246)
---------------------------------------
Vector Time (GMT): 2012/262/03:24:16
267
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1497393
13 A = 6789466
91 meter
Y = 3920793
32 meter E =
0021254
Z = 5318944
03 I = 51
74484
XDOT = -7235
236564 Wp = 78
54697
YDOT = -2565
945534 meter/sec RA = 18
69814 deg
ZDOT = -140
812099 TA = 12
81824
MA = 12
76429
Ha = 234
493 n
mi
Hp = 214
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4912707
12 X = -1566963
46
Y = 12863495
13 feet Y = 3903660
15 meter
Z = 17450603
76 Z = 5311500
25
XDOT = -23737
652769 XDOT = -7205
321844
YDOT = -8418
456475 feet/sec YDOT = -2646
687215 meter/sec
ZDOT = -461
981952 ZDOT = -175
887939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6140830
58 X = 1871725
16
Y = 12368615
10 feet Y = 3769953
88 meter
Z = 17419395
23 Z = 5309431
67
XDOT = -21294
410777 XDOT = -6490
536405
YDOT = 11448
175350 feet/sec YDOT = 3489
403847 meter/sec
ZDOT = -606
749403 ZDOT = -184
937218
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 12262
18995870
00016717 00000-0 10270-3 0 9085
2 25544 51
6497 19
0028 0018804 78
8509 281
4755 15
49972854 32474
Satellite: ISS
Catalog Number: 25544
Epoch time: 12262
18995870 = yrday
fracday
Element set: 908
Inclination: 51
6497 deg
RA of node: 19
0028 deg
Eccentricity:
0018804
Arg of perigee: 78
8509 deg
Mean anomaly: 281
4755 deg
Mean motion: 15
49972854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3247
Checksum: 353
Coasting Arc #10 (Orbit 3261)
---------------------------------------
Vector Time (GMT): 2012/263/03:24:16
267
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1549688
00 A = 6789566
20 meter
Y = -3950680
34 meter E =
0033307
Z = -5328552
86 I = 51
71623
XDOT = 7298
083668 Wp = 86
90258
YDOT = 2192
842367 meter/sec RA = 13
74854 deg
ZDOT = 501
135547 TA = 187
86663
MA = 187
91900
Ha = 234
416 n
mi
Hp = 214
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5084278
21 X = 1619635
37
Y = -12961549
66 feet Y = -3932960
16 meter
Z = -17482128
82 Z = -5320854
19
XDOT = 23943
844054 XDOT = 7270
586002
YDOT = 7194
364721 feet/sec YDOT = 2274
300389 meter/sec
ZDOT = 1644
145497 ZDOT = 536
522728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6312996
86 X = -1924201
44
Y = -12454916
67 feet Y = -3796258
60 meter
Z = -17449859
71 Z = -5318717
24
XDOT = 20291
891709 XDOT = 6184
968593
YDOT = -12772
933199 feet/sec YDOT = -3893
190039 meter/sec
ZDOT = 1790
231263 ZDOT = 545
662489
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 12263
15709047
00016717 00000-0 10270-3 0 9093
2 25544 51
6498 14
2121 0018811 82
0197 278
3087 15
49982422 32626
Satellite: ISS
Catalog Number: 25544
Epoch time: 12263
15709047 = yrday
fracday
Element set: 909
Inclination: 51
6498 deg
RA of node: 14
2121 deg
Eccentricity:
0018811
Arg of perigee: 82
0197 deg
Mean anomaly: 278
3087 deg
Mean motion: 15
49982422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3262
Checksum: 313
Coasting Arc #11 (Orbit 3277)
---------------------------------------
Vector Time (GMT): 2012/264/03:24:16
267
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1627089
10 A = 6789569
99 meter
Y = 3951759
36 meter E =
0021892
Z = 5257584
84 I = 51
68716
XDOT = -7397
477130 Wp = 80
92666
YDOT = -1855
090640 meter/sec RA = 8
79668 deg
ZDOT = -888
456080 TA = 17
59169
MA = 17
51599
Ha = 234
388 n
mi
Hp = 214
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5338218
82 X = -1696698
02
Y = 12965089
75 feet Y = 3933175
40 meter
Z = 17249294
09 Z = 5249511
06
XDOT = -24269
938090 XDOT = -7371
867350
YDOT = -6086
255380 feet/sec YDOT = -1937
670713 meter/sec
ZDOT = -2914
882151 ZDOT = -924
330760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6365635
95 X = 1940245
84
Y = 12539319
69 feet Y = 3821984
64 meter
Z = 17215470
36 Z = 5247275
37
XDOT = -19415
968491 XDOT = -5917
987196
YDOT = 14091
350539 feet/sec YDOT = 4295
043644 meter/sec
ZDOT = -3063
014106 ZDOT = -933
606700
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 12264
18867577
00016717 00000-0 10270-3 0 9102
2 25544 51
6498 9
1019 0018735 85
6269 274
7022 15
50033151 32783
Satellite: ISS
Catalog Number: 25544
Epoch time: 12264
18867577 = yrday
fracday
Element set: 910
Inclination: 51
6498 deg
RA of node: 9
1019 deg
Eccentricity:
0018735
Arg of perigee: 85
6269 deg
Mean anomaly: 274
7022 deg
Mean motion: 15
50033151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3278
Checksum: 319
Coasting Arc #12 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2012/265/03:24:16
267
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1703746
42 A = 6789859
15 meter
Y = -4026409
66 meter E =
0032513
Z = -5223410
84 I = 51
65732
XDOT = 7382
739740 Wp = 93
14373
YDOT = 1495
152005 meter/sec RA = 3
84209 deg
ZDOT = 1260
612263 TA = 188
97579
MA = 189
03406
Ha = 234
298 n
mi
Hp = 214
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5589719
23 X = 1774018
32
Y = -13210005
45 feet Y = -4006964
68 meter
Z = -17137174
67 Z = -5214963
13
XDOT = 24221
587074 XDOT = 7359
348108
YDOT = 4905
354348 feet/sec YDOT = 1577
579682 meter/sec
ZDOT = 4135
867005 ZDOT = 1296
420703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6610896
26 X = -2015001
18
Y = -12777193
27 feet Y = -3894488
51 meter
Z = -17101793
58 Z = -5212626
68
XDOT = 18196
420163 XDOT = 5546
268866
YDOT = -15126
145696 feet/sec YDOT = -4610
449208 meter/sec
ZDOT = 4283
761389 ZDOT = 1305
690471
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 12265
15576943
00016717 00000-0 10270-3 0 9115
2 25544 51
6491 4
3104 0018710 88
8772 271
4522 15
50040981 32930
Satellite: ISS
Catalog Number: 25544
Epoch time: 12265
15576943 = yrday
fracday
Element set: 911
Inclination: 51
6491 deg
RA of node: 4
3104 deg
Eccentricity:
0018710
Arg of perigee: 88
8772 deg
Mean anomaly: 271
4522 deg
Mean motion: 15
50040981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 299
Coasting Arc #13 (Orbit 3308)
---------------------------------------
Vector Time (GMT): 2012/266/03:24:16
267
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1802675
96 A = 6790085
60 meter
Y = 4076422
42 meter E =
0022990
Z = 5103145
94 I = 51
62836
XDOT = -7402
254470 Wp = 84
04420
YDOT = -1175
929733 meter/sec RA = 358
88563 deg
ZDOT = -1666
701026 TA = 22
07901
MA = 21
98015
Ha = 234
259 n
mi
Hp = 214
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5914291
20 X = -1872915
44
Y = 13374089
31 feet Y = 4055871
27 meter
Z = 16742604
80 Z = 5094217
78
XDOT = -24285
611779 XDOT = -7380
458323
YDOT = -3858
037182 feet/sec YDOT = -1258
584564 meter/sec
ZDOT = -5468
179219 ZDOT = -1702
608038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6758544
33 X = 2060004
31
Y = 13016039
79 feet Y = 3967288
93 meter
Z = 16705229
94 Z = 5091754
08
XDOT = -17120
948687 XDOT = -5218
465160
YDOT = 16135
534213 feet/sec YDOT = 4918
110828 meter/sec
ZDOT = -5616
515459 ZDOT = -1711
913912
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 12266
18731415
00016717 00000-0 10270-3 0 9127
2 25544 51
6491 359
1998 0018640 92
5026 267
8259 15
50091035 33098
Satellite: ISS
Catalog Number: 25544
Epoch time: 12266
18731415 = yrday
fracday
Element set: 912
Inclination: 51
6491 deg
RA of node: 359
1998 deg
Eccentricity:
0018640
Arg of perigee: 92
5026 deg
Mean anomaly: 267
8259 deg
Mean motion: 15
50091035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3309
Checksum: 319
Coasting Arc #14 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2012/267/03:24:16
267
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1886593
78 A = 6790568
35 meter
Y = -4201065
03 meter E =
0031105
Z = -5018559
72 I = 51
59858
XDOT = 7310
718211 Wp = 99
25055
YDOT = 850
212480 meter/sec RA = 353
92622 deg
ZDOT = 2042
539587 TA = 190
66805
MA = 190
73419
Ha = 234
175 n
mi
Hp = 214
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6189612
14 X = 1957809
81
Y = -13783021
76 feet Y = -4179570
02 meter
Z = -16465090
95 Z = -5009221
54
XDOT = 23985
295968 XDOT = 7290
745397
YDOT = 2789
411022 feet/sec YDOT = 931
853913 meter/sec
ZDOT = 6701
245364 ZDOT = 2078
006214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7140469
50 X = -2176415
10
Y = -13363464
95 feet Y = -4073184
12 meter
Z = -16426007
04 Z = -5006646
95
XDOT = 15770
726602 XDOT = 4806
917468
YDOT = -16819
657286 feet/sec YDOT = -5126
631541 meter/sec
ZDOT = 6847
796671 ZDOT = 2087
208425
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 12267
15436973
00016717 00000-0 10270-3 0 9137
2 25544 51
6481 354
4075 0018635 95
8878 264
4397 15
50098125 33246
Satellite: ISS
Catalog Number: 25544
Epoch time: 12267
15436973 = yrday
fracday
Element set: 913
Inclination: 51
6481 deg
RA of node: 354
4075 deg
Eccentricity:
0018635
Arg of perigee: 95
8878 deg
Mean anomaly: 264
4397 deg
Mean motion: 15
50098125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 337
Coasting Arc #15 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2012/268/03:24:16
267
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1988691
22 A = 6791030
99 meter
Y = 4302317
98 meter E =
0024505
Z = 4842516
65 I = 51
57086
XDOT = -7251
623977 Wp = 88
33633
YDOT = -572
689657 meter/sec RA = 348
96554 deg
ZDOT = -2457
791325 TA = 25
84261
MA = 25
72041
Ha = 234
115 n
mi
Hp = 214
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6524577
48 X = -2060176
63
Y = 14115216
48 feet Y = 4279679
80 meter
Z = 15887521
82 Z = 4832681
80
XDOT = -23791
417248 XDOT = -7232
741712
YDOT = -1878
903074 feet/sec YDOT = -653
676412 meter/sec
ZDOT = -8063
619833 ZDOT = -2492
973410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7440215
48 X = 2267777
68
Y = 13702495
31 feet Y = 4176520
57 meter
Z = 15846375
39 Z = 4829975
22
XDOT = -14592
246355 XDOT = -4447
716689
YDOT = 17460
296218 feet/sec YDOT = 5321
898287 meter/sec
ZDOT = -8209
024537 ZDOT = -2502
110679
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 12268
18587394
00016717 00000-0 10270-3 0 9146
2 25544 51
6483 349
2966 0018542 99
5454 260
7793 15
50146007 33407
Satellite: ISS
Catalog Number: 25544
Epoch time: 12268
18587394 = yrday
fracday
Element set: 914
Inclination: 51
6483 deg
RA of node: 349
2966 deg
Eccentricity:
0018542
Arg of perigee: 99
5454 deg
Mean anomaly: 260
7793 deg
Mean motion: 15
50146007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 337
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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