[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 20th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
There are no maneuvers
Coasting Arc #1 (Orbit 2528)
---------------------------------------
Vector Time (GMT): 2013/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2257007
79 A = 6782884
16 meter
Y = 3662152
34 meter E =
0013474
Z = 5239419
23 I = 51
89589
XDOT = -5621
926568 Wp = 145
16453
YDOT = -5094
539768 meter/sec RA = 48
87169 deg
ZDOT = 1126
896696 TA = 294
00410
MA = 294
14509
Ha = 226
836 n
mi
Hp = 215
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7404881
19 X = -2323242
86
Y = 12014935
49 feet Y = 3636542
91 meter
Z = 17189695
65 Z = 5228293
80
XDOT = -18444
640971 XDOT = -5570
014691
YDOT = -16714
369318 feet/sec YDOT = -5157
117395 meter/sec
ZDOT = 3697
167637 ZDOT = 1099
711988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1736836
09 X = -529387
64
Y = 14063590
80 feet Y = 4286582
48 meter
Z = 17142794
14 Z = 5225123
65
XDOT = -22770
879876 XDOT = -6940
564186
YDOT = -7230
407418 feet/sec YDOT = -2203
828181 meter/sec
ZDOT = 3584
462202 ZDOT = 1092
544079
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 13107
55017185
00016717 00000-0 10270-3 0 9001
2 25544 51
6457 49
2427 0010055 153
8949 206
2712 15
52364595 25291
Satellite: ISS
Catalog Number: 25544
Epoch time: 13107
55017185 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 49
2427 deg
Eccentricity:
0010055
Arg of perigee: 153
8949 deg
Mean anomaly: 206
2712 deg
Mean motion: 15
52364595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2529
Checksum: 306
Coasting Arc #2 (Orbit 2543)
---------------------------------------
Vector Time (GMT): 2013/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3037413
34 A = 6782568
96 meter
Y = -2897637
57 meter E =
0021088
Z = -5343841
86 I = 51
87375
XDOT = 5427
608797 Wp = 116
75449
YDOT = 5390
950552 meter/sec RA = 43
90600 deg
ZDOT = 153
076321 TA = 154
75445
MA = 154
65124
Ha = 226
744 n
mi
Hp = 215
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9965266
86 X = 3095548
67
Y = -9506684
95 feet Y = -2863346
49 meter
Z = -17532289
56 Z = -5328944
96
XDOT = 17807
115477 XDOT = 5366
179032
YDOT = 17686
845642 feet/sec YDOT = 5451
302027 meter/sec
ZDOT = 502
218900 ZDOT = 179
293838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4896395
94 X = 1492421
48
Y = -12957533
20 feet Y = -3949456
12 meter
Z = -17469757
29 Z = -5324782
02
XDOT = 22803
762291 XDOT = 6950
586746
YDOT = 7754
609715 feet/sec YDOT = 2363
605041 meter/sec
ZDOT = 610
843921 ZDOT = 186
185227
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 13108
51581358
00016717 00000-0 10270-3 0 9017
2 25544 51
6458 44
4409 0010024 156
9192 203
2412 15
52345313 25447
Satellite: ISS
Catalog Number: 25544
Epoch time: 13108
51581358 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node: 44
4409 deg
Eccentricity:
0010024
Arg of perigee: 156
9192 deg
Mean anomaly: 203
2412 deg
Mean motion: 15
52345313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2544
Checksum: 278
Coasting Arc #3 (Orbit 2559)
---------------------------------------
Vector Time (GMT): 2013/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3790183
73 A = 6783118
40 meter
Y = 2170350
28 meter E =
0009792
Z = 5182360
34 I = 51
85343
XDOT = -5103
974248 Wp = 133
63802
YDOT = -5551
244113 meter/sec RA = 38
94121 deg
ZDOT = -1412
944167 TA = 329
87686
MA = 329
93313
Ha = 226
678 n
mi
Hp = 215
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12434985
98 X = -3839345
98
Y = 7120571
78 feet Y = 2127691
46 meter
Z = 17002494
54 Z = 5163828
34
XDOT = -16745
322336 XDOT = -5034
655972
YDOT = -18212
743154 feet/sec YDOT = -5607
932468 meter/sec
ZDOT = -4635
643591 ZDOT = -1437
570251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7952582
16 X = -2423947
04
Y = 12029983
07 feet Y = 3666738
84 meter
Z = 16924898
34 Z = 5158709
01
XDOT = -22276
498033 XDOT = -6789
876600
YDOT = -8083
722611 feet/sec YDOT = -2463
918652 meter/sec
ZDOT = -4737
602215 ZDOT = -1444
021155
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 13109
54581753
00016717 00000-0 10270-3 0 9021
2 25544 51
6461 39
3209 0009985 160
7833 199
3697 15
52380831 25603
Satellite: ISS
Catalog Number: 25544
Epoch time: 13109
54581753 = yrday
fracday
Element set: 902
Inclination: 51
6461 deg
RA of node: 39
3209 deg
Eccentricity:
0009985
Arg of perigee: 160
7833 deg
Mean anomaly: 199
3697 deg
Mean motion: 15
52380831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2560
Checksum: 328
Coasting Arc #4 (Orbit 2574)
---------------------------------------
Vector Time (GMT): 2013/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4571775
87 A = 6784764
54 meter
Y = -1475955
71 meter E =
0018733
Z = -4808036
82 I = 51
83488
XDOT = 4558
690122 Wp = 134
27421
YDOT = 5557
210450 meter/sec RA = 33
97465 deg
ZDOT = 2622
341347 TA = 161
60365
MA = 161
53582
Ha = 226
468 n
mi
Hp = 215
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14999264
66 X = 4611296
81
Y = -4842374
38 feet Y = -1424610
58 meter
Z = -15774399
01 Z = -4785731
32
XDOT = 14956
332420 XDOT = 4483
470690
YDOT = 18232
317749 feet/sec YDOT = 5607
768200 meter/sec
ZDOT = 8603
482109 ZDOT = 2644
304093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11070381
35 X = 3374252
24
Y = -11349275
92 feet Y = -3459259
30 meter
Z = -15681160
26 Z = -4779617
65
XDOT = 20878
734398 XDOT = 6363
838244
YDOT = 8323
609828 feet/sec YDOT = 2537
036275 meter/sec
ZDOT = 8694
323931 ZDOT = 2650
029934
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 13110
51143494
00016717 00000-0 10270-3 0 9037
2 25544 51
6465 34
5191 0009967 164
2494 195
8970 15
52388670 25756
Satellite: ISS
Catalog Number: 25544
Epoch time: 13110
51143494 = yrday
fracday
Element set: 903
Inclination: 51
6465 deg
RA of node: 34
5191 deg
Eccentricity:
0009967
Arg of perigee: 164
2494 deg
Mean anomaly: 195
8970 deg
Mean motion: 15
52388670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2575
Checksum: 327
Coasting Arc #5 (Orbit 2590)
---------------------------------------
Vector Time (GMT): 2013/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5258797
42 A = 6787024
59 meter
Y = 851546
88 meter E =
0014085
Z = 4189887
06 I = 51
81671
XDOT = -3858
401658 Wp = 120
31834
YDOT = -5489
368770 meter/sec RA = 29
01154 deg
ZDOT = -3724
715845 TA = 7
82414
MA = 7
80219
Ha = 226
484 n
mi
Hp = 215
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17253272
38 X = -5288282
26
Y = 2793788
97 feet Y = 792575
16 meter
Z = 13746348
63 Z = 4164268
41
XDOT = -12658
798091 XDOT = -3778
637784
YDOT = -18009
740059 feet/sec YDOT = -5532
070162 meter/sec
ZDOT = -12220
196341 ZDOT = -3743
265579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13826069
25 X = -4214185
91
Y = 10828197
26 feet Y = 3300434
52 meter
Z = 13639381
17 Z = 4157283
38
XDOT = -18932
385928 XDOT = -5770
591231
YDOT = -8674
802747 feet/sec YDOT = -2644
079877 meter/sec
ZDOT = -12296
804545 ZDOT = -3748
066025
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 13111
54141475
00016717 00000-0 10270-3 0 9049
2 25544 51
6467 29
3986 0009988 167
9776 192
1616 15
52399669 25913
Satellite: ISS
Catalog Number: 25544
Epoch time: 13111
54141475 = yrday
fracday
Element set: 904
Inclination: 51
6467 deg
RA of node: 29
3986 deg
Eccentricity:
0009988
Arg of perigee: 167
9776 deg
Mean anomaly: 192
1616 deg
Mean motion: 15
52399669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2591
Checksum: 356
Coasting Arc #6 (Orbit 2605)
---------------------------------------
Vector Time (GMT): 2013/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5880180
02 A = 6789483
09 meter
Y = -302541
68 meter E =
0011442
Z = -3396163
94 I = 51
79879
XDOT = 2955
695097 Wp = 146
90207
YDOT = 5319
137205 meter/sec RA = 24
04982 deg
ZDOT = 4641
747276 TA = 173
61841
MA = 173
60383
Ha = 226
177 n
mi
Hp = 215
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19291929
20 X = 5899623
91
Y = -992590
81 feet Y = -236677
37 meter
Z = -11142270
14 Z = -3367550
97
XDOT = 9697
162391 XDOT = 2873
447072
YDOT = 17451
237549 feet/sec YDOT = 5351
730174 meter/sec
ZDOT = 15228
829646 ZDOT = 4655
905707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16289027
87 X = 4964895
70
Y = -10510816
93 feet Y = -3203697
00 meter
Z = -11022896
67 Z = -3359778
90
XDOT = 16257
313126 XDOT = 4955
229041
YDOT = 9155
899004 feet/sec YDOT = 2790
718016 meter/sec
ZDOT = 15287
138682 ZDOT = 4659
519870
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 13112
50700841
00016717 00000-0 10270-3 0 9055
2 25544 51
6475 24
5971 0009955 171
7739 188
3578 15
52437329 26066
Satellite: ISS
Catalog Number: 25544
Epoch time: 13112
50700841 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node: 24
5971 deg
Eccentricity:
0009955
Arg of perigee: 171
7739 deg
Mean anomaly: 188
3578 deg
Mean motion: 15
52437329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2606
Checksum: 325
Coasting Arc #7 (Orbit 2621)
---------------------------------------
Vector Time (GMT): 2013/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6331981
74 A = 6791898
30 meter
Y = -179090
16 meter E =
0019697
Z = 2414930
29 I = 51
77848
XDOT = -1908
888399 Wp = 134
25901
YDOT = -5138
003174 meter/sec RA = 19
09170 deg
ZDOT = -5372
529806 TA = 18
77710
MA = 18
70455
Ha = 226
179 n
mi
Hp = 216
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20774218
31 X = -6341239
77
Y = -587566
14 feet Y = -249949
94 meter
Z = 7922999
64 Z = 2384147
13
XDOT = -6262
757213 XDOT = -1825
193556
YDOT = -16856
965794 feet/sec YDOT = -5158
882044 meter/sec
ZDOT = -17626
410125 ZDOT = -5381
599445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18172039
14 X = -5538837
53
Y = 10183698
67 feet Y = 3103991
35 meter
Z = 7794650
66 Z = 2375809
52
XDOT = -13191
480682 XDOT = -4020
763312
YDOT = -9984
658664 feet/sec YDOT = -3043
323961 meter/sec
ZDOT = -17663
514021 ZDOT = -5383
839074
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 13113
53696400
00016717 00000-0 10270-3 0 9065
2 25544 51
6476 19
4762 0009985 175
5797 184
5445 15
52425068 26223
Satellite: ISS
Catalog Number: 25544
Epoch time: 13113
53696400 = yrday
fracday
Element set: 906
Inclination: 51
6476 deg
RA of node: 19
4762 deg
Eccentricity:
0009985
Arg of perigee: 175
5797 deg
Mean anomaly: 184
5445 deg
Mean motion: 15
52425068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2622
Checksum: 332
Coasting Arc #8 (Orbit 2636)
---------------------------------------
Vector Time (GMT): 2013/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6637091
76 A = 6793418
29 meter
Y = 580901
41 meter E =
0006189
Z = -1341685
49 I = 51
75547
XDOT = 742
636318 Wp = 117
18858
YDOT = 4918
321576 meter/sec RA = 14
13481 deg
ZDOT = 5821
067500 TA = 228
25308
MA = 228
30600
Ha = 225
863 n
mi
Hp = 216
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21775235
44 X = 6636620
39
Y = 1905844
53 feet Y = 655118
83 meter
Z = -4401855
29 Z = -1309443
64
XDOT = 2436
470858 XDOT = 659
305654
YDOT = 16136
225644 feet/sec YDOT = 4926
160669 meter/sec
ZDOT = 19097
990484 ZDOT = 5824
472489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19521958
04 X = 5950292
81
Y = -9891973
94 feet Y = -3015073
66 meter
Z = -4267488
45 Z = -1300730
48
XDOT = 9767
548141 XDOT = 2977
148674
YDOT = 11057
682355 feet/sec YDOT = 3370
381582 meter/sec
ZDOT = 19111
495374 ZDOT = 5825
183790
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 13114
50253455
00016717 00000-0 10270-3 0 9073
2 25544 51
6483 14
6751 0009888 179
7605 180
3553 15
52473883 26370
Satellite: ISS
Catalog Number: 25544
Epoch time: 13114
50253455 = yrday
fracday
Element set: 907
Inclination: 51
6483 deg
RA of node: 14
6751 deg
Eccentricity:
0009888
Arg of perigee: 179
7605 deg
Mean anomaly: 180
3553 deg
Mean motion: 15
52473883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2637
Checksum: 327
Coasting Arc #9 (Orbit 2652)
---------------------------------------
Vector Time (GMT): 2013/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6712582
50 A = 6794225
52 meter
Y = -949995
12 meter E =
0020238
Z = 168478
32 I = 51
72809
XDOT = 512
079983 Wp = 155
16362
YDOT = -4729
455560 meter/sec RA = 9
17871 deg
ZDOT = -6021
346887 TA = 23
02297
MA = 22
93240
Ha = 225
806 n
mi
Hp = 216
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22022908
47 X = -6702278
99
Y = -3116781
90 feet Y = -1025001
83 meter
Z = 552750
38 Z = 135893
52
XDOT = 1680
052439 XDOT = 594
178456
YDOT = -15516
586483 feet/sec YDOT = -4723
270385 meter/sec
ZDOT = -19755
075090 ZDOT = -6018
659566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20194070
67 X = -6155152
74
Y = 9330271
65 feet Y = 2843866
80 meter
Z = 417013
94 Z = 127105
85
XDOT = -6224
025581 XDOT = -1897
082997
YDOT = -12541
186294 feet/sec YDOT = -3822
553583 meter/sec
ZDOT = -19743
195942 ZDOT = -6017
726123
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 13115
53246605
00016717 00000-0 10270-3 0 9087
2 25544 51
6484 9
5540 0009999 183
7131 176
3948 15
52446100 26535
Satellite: ISS
Catalog Number: 25544
Epoch time: 13115
53246605 = yrday
fracday
Element set: 908
Inclination: 51
6484 deg
RA of node: 9
5540 deg
Eccentricity:
0009999
Arg of perigee: 183
7131 deg
Mean anomaly: 176
3948 deg
Mean motion: 15
52446100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2653
Checksum: 316
Coasting Arc #10 (Orbit 2668)
---------------------------------------
Vector Time (GMT): 2013/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6601309
26 A = 6793618
68 meter
Y = 1267469
62 meter E =
0010148
Z = 985313
97 I = 51
69613
XDOT = -1762
717427 Wp = 101
53570
YDOT = 4547
663577 meter/sec RA = 4
22004 deg
ZDOT = 5906
154922 TA = 269
11482
MA = 269
23109
Ha = 225
514 n
mi
Hp = 216
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21657838
78 X = 6581859
01
Y = 4158364
90 feet Y = 1341180
88 meter
Z = 3232657
39 Z = 1017336
02
XDOT = -5783
193657 XDOT = -1842
130538
YDOT = 14920
156091 feet/sec YDOT = 4527
507832 meter/sec
ZDOT = 19377
148695 ZDOT = 5897
398631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20288110
12 X = 6183815
97
Y = -8594574
73 feet Y = -2619626
38 meter
Z = 3365995
55 Z = 1025955
44
XDOT = 2779
443922 XDOT = 847
174507
YDOT = 14201
552610 feet/sec YDOT = 4328
633235 meter/sec
ZDOT = 19339
984317 ZDOT = 5894
827220
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 13116
56238345
00016717 00000-0 10270-3 0 9094
2 25544 51
6483 4
4325 0009754 188
0847 172
0149 15
52500059 26697
Satellite: ISS
Catalog Number: 25544
Epoch time: 13116
56238345 = yrday
fracday
Element set: 909
Inclination: 51
6483 deg
RA of node: 4
4325 deg
Eccentricity:
0009754
Arg of perigee: 188
0847 deg
Mean anomaly: 172
0149 deg
Mean motion: 15
52500059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2669
Checksum: 315
Coasting Arc #11 (Orbit 2683)
---------------------------------------
Vector Time (GMT): 2013/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6238064
98 A = 6792119
82 meter
Y = -1603598
89 meter E =
0014447
Z = -2129604
16 I = 51
66033
XDOT = 3007
662401 Wp = 171
32552
YDOT = -4400
975703 meter/sec RA = 359
25793 deg
ZDOT = -5514
956937 TA = 32
26742
MA = 32
17912
Ha = 225
353 n
mi
Hp = 216
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20466092
44 X = -6209324
30
Y = -5261151
22 feet Y = -1673196
15 meter
Z = -6986890
28 Z = -2159838
96
XDOT = 9867
658797 XDOT = 3083
442251
YDOT = -14438
896663 feet/sec YDOT = -4366
918366 meter/sec
ZDOT = -18093
690738 ZDOT = -5500
161647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19769848
30 X = -6025849
76
Y = 7342992
89 feet Y = 2238144
23 meter
Z = -7112723
90 Z = -2167958
24
XDOT = 481
363133 XDOT = 146
719483
YDOT = -16111
168621 feet/sec YDOT = -4910
684196 meter/sec
ZDOT = -18031
362982 ZDOT = -5495
959437
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 13117
52792088
00016717 00000-0 10270-3 0 9102
2 25544 51
6483 359
6313 0009919 192
4682 167
6226 15
52484880 26844
Satellite: ISS
Catalog Number: 25544
Epoch time: 13117
52792088 = yrday
fracday
Element set: 910
Inclination: 51
6483 deg
RA of node: 359
6313 deg
Eccentricity:
0009919
Arg of perigee: 192
4682 deg
Mean anomaly: 167
6226 deg
Mean motion: 15
52484880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2684
Checksum: 340
Coasting Arc #12 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2013/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5702771
99 A = 6789749
35 meter
Y = 1929255
16 meter E =
0013179
Z = 3140470
75 I = 51
62168
XDOT = -4124
016552 Wp = 128
82258
YDOT = 4268
497659 meter/sec RA = 354
28894 deg
ZDOT = 4844
755638 TA = 267
33315
MA = 267
48401
Ha = 225
137 n
mi
Hp = 217
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18709881
87 X = 5665518
99
Y = 6329577
28 feet Y = 1992818
76 meter
Z = 10303381
72 Z = 3168084
34
XDOT = -13530
238033 XDOT = -4194
976210
YDOT = 14004
257411 feet/sec YDOT = 4221
983417 meter/sec
ZDOT = 15894
867578 ZDOT = 4824
548953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18825069
41 X = 5737881
16
Y = -5775811
74 feet Y = -1760467
42 meter
Z = 10418237
05 Z = 3175478
65
XDOT = -3278
731981 XDOT = -999
357508
YDOT = 17958
883861 feet/sec YDOT = 5473
867801 meter/sec
ZDOT = 15809
992705 ZDOT = 4818
885776
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 13118
55781571
00016717 00000-0 10270-3 0 9112
2 25544 51
6478 354
5090 0009627 196
0603 164
0245 15
52519951 27002
Satellite: ISS
Catalog Number: 25544
Epoch time: 13118
55781571 = yrday
fracday
Element set: 911
Inclination: 51
6478 deg
RA of node: 354
5090 deg
Eccentricity:
0009627
Arg of perigee: 196
0603 deg
Mean anomaly: 164
0245 deg
Mean motion: 15
52519951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2700
Checksum: 308
Coasting Arc #13 (Orbit 2714)
---------------------------------------
Vector Time (GMT): 2013/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4944358
95 A = 6786971
24 meter
Y = -2318059
90 meter E =
0007631
Z = -4028104
36 I = 51
58172
XDOT = 5126
090296 Wp = 153
43544
YDOT = -4133
560161 meter/sec RA = 349
31331 deg
ZDOT = -3922
903020 TA = 75
82220
MA = 75
73743
Ha = 224
894 n
mi
Hp = 217
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16221650
08 X = -4898502
75
Y = -7605183
38 feet Y = -2373094
30 meter
Z = -13215565
48 Z = -4052012
60
XDOT = 16817
881550 XDOT = 5190
988299
YDOT = -13561
549084 feet/sec YDOT = -4075
873990 meter/sec
ZDOT = -12870
416732 ZDOT = -3897
843139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17480186
72 X = -5327960
91
Y = 3576037
71 feet Y = 1089976
29 meter
Z = -13314914
31 Z = -4058385
88
XDOT = 5668
358818 XDOT = 1727
715768
YDOT = -19706
479307 feet/sec YDOT = -6006
534893 meter/sec
ZDOT = -12765
324118 ZDOT = -3890
870791
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 13119
52332979
00016717 00000-0 10270-3 0 9125
2 25544 51
6473 349
7072 0009760 200
9316 159
1437 15
52541181 27151
Satellite: ISS
Catalog Number: 25544
Epoch time: 13119
52332979 = yrday
fracday
Element set: 912
Inclination: 51
6473 deg
RA of node: 349
7072 deg
Eccentricity:
0009760
Arg of perigee: 200
9316 deg
Mean anomaly: 159
1437 deg
Mean motion: 15
52541181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2715
Checksum: 310
Coasting Arc #14 (Orbit 2730)
---------------------------------------
Vector Time (GMT): 2013/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4078027
31 A = 6784529
57 meter
Y = 2724995
54 meter E =
0012745
Z = 4690488
73 I = 51
54363
XDOT = -5912
381965 Wp = 165
20617
YDOT = 3979
968476 meter/sec RA = 344
33040 deg
ZDOT = 2814
403304 TA = 256
75170
MA = 256
89389
Ha = 224
754 n
mi
Hp = 217
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13379354
68 X = 4024467
43
Y = 8940274
09 feet Y = 2770299
01 meter
Z = 15388742
57 Z = 4710169
56
XDOT = -19397
578626 XDOT = -5970
119119
YDOT = 13057
639356 feet/sec YDOT = 3913
529586 meter/sec
ZDOT = 9233
606639 ZDOT = 2785
541134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15977100
27 X = 4869820
16
Y = -1071366
66 feet Y = -326552
56 meter
Z = 15470406
29 Z = 4715379
84
XDOT = -7454
004599 XDOT = -2271
980602
YDOT = 21074
151467 feet/sec YDOT = 6423
401367 meter/sec
ZDOT = 9112
682985 ZDOT = 2777
545774
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 13120
55320221
00016717 00000-0 10270-3 0 9138
2 25544 51
6474 344
5850 0009599 203
9709 156
0997 15
52546439 27314
Satellite: ISS
Catalog Number: 25544
Epoch time: 13120
55320221 = yrday
fracday
Element set: 913
Inclination: 51
6474 deg
RA of node: 344
5850 deg
Eccentricity:
0009599
Arg of perigee: 203
9709 deg
Mean anomaly: 156
0997 deg
Mean motion: 15
52546439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2731
Checksum: 316
Coasting Arc #15 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2013/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3065317
79 A = 6782547
99 meter
Y = -3208908
01 meter E =
0010555
Z = -5135667
95 I = 51
50715
XDOT = 6496
565615 Wp = 122
82873
YDOT = -3756
857174 meter/sec RA = 339
34021 deg
ZDOT = -1538
109097 TA = 132
35181
MA = 132
26238
Ha = 224
509 n
mi
Hp = 217
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10056816
91 X = -3004259
46
Y = -10527913
42 feet Y = -3242844
85 meter
Z = -16849304
31 Z = -5150410
81
XDOT = 21314
191651 XDOT = 6545
564512
YDOT = -12325
646896 feet/sec YDOT = -3683
934492 meter/sec
ZDOT = -5046
289687 ZDOT = -1506
430247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14352866
26 X = -4374753
64
Y = -1977938
26 feet Y = -602875
58 meter
Z = -16910309
68 Z = -5154262
39
XDOT = 8780
747631 XDOT = 2676
371878
YDOT = -21929
056558 feet/sec YDOT = -6683
976439 meter/sec
ZDOT = -4913
657338 ZDOT = -1497
682757
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 13121
51869422
00016717 00000-0 10270-3 0 9147
2 25544 51
6463 339
7823 0009660 208
6156 151
4466 15
52597635 27465
Satellite: ISS
Catalog Number: 25544
Epoch time: 13121
51869422 = yrday
fracday
Element set: 914
Inclination: 51
6463 deg
RA of node: 339
7823 deg
Eccentricity:
0009660
Arg of perigee: 208
6156 deg
Mean anomaly: 151
4466 deg
Mean motion: 15
52597635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 326
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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