[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 27th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
281/17:02:31
515 -0
8 3
1 3
2
N/A -3
0 -0
5 226
4
000/00:07:03
030 0
8 0
2 221
1
Coasting Arc #1 (Orbit 2703)
---------------------------------------
Vector Time (GMT): 2014/269/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5717444
10 A = 6797537
81 meter
Y = -2998091
57 meter E =
0014931
Z = 2108185
83 I = 51
41760
XDOT = 737
252672 Wp = 75
75928
YDOT = 5291
148669 meter/sec RA = 317
22754 deg
ZDOT = 5496
032516 TA = 307
63815
MA = 307
77354
Ha = 227
003 n
mi
Hp = 219
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18758018
71 X = 5740303
49
Y = -9836258
42 feet Y = -2934027
30 meter
Z = 6916620
18 Z = 2136016
67
XDOT = 2418
807978 XDOT = 651
332707
YDOT = 17359
411643 feet/sec YDOT = 5298
913451 meter/sec
ZDOT = 18031
602742 ZDOT = 5499
404613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21101011
33 X = -6431588
25
Y = 1305429
00 feet Y = 397894
76 meter
Z = 7035485
51 Z = 2144415
98
XDOT = 5104
913934 XDOT = 1555
977767
YDOT = -15242
797639 feet/sec YDOT = -4646
004720 meter/sec
ZDOT = 18045
004905 ZDOT = 5500
117495
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 14269
48105347
00016717 00000-0 10270-3 0 9001
2 25544 51
6462 317
5268 0001807 127
7381 232
3934 15
50644640 27047
Satellite: ISS
Catalog Number: 25544
Epoch time: 14269
48105347 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 317
5268 deg
Eccentricity:
0001807
Arg of perigee: 127
7381 deg
Mean anomaly: 232
3934 deg
Mean motion: 15
50644640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2704
Checksum: 302
Coasting Arc #2 (Orbit 2718)
---------------------------------------
Vector Time (GMT): 2014/270/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5524431
51 A = 6796448
31 meter
Y = 2958187
43 meter E =
0006761
Z = -2629539
44 I = 51
39066
XDOT = -527
379080 Wp = 126
09092
YDOT = -5596
715395 meter/sec RA = 312
25448 deg
ZDOT = -5201
531522 TA = 83
58948
MA = 83
51249
Ha = 226
972 n
mi
Hp = 219
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18124775
30 X = -5544326
40
Y = 9705339
34 feet Y = 2896298
10 meter
Z = -8627097
91 Z = -2656425
44
XDOT = -1730
246325 XDOT = -439
488359
YDOT = -18361
927150 feet/sec YDOT = -5602
122098 meter/sec
ZDOT = -17065
392134 ZDOT = -5203
879328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20431871
54 X = 6227634
44
Y = -1801430
62 feet Y = -549076
05 meter
Z = -8741932
45 Z = -2664541
01
XDOT = -5873
849955 XDOT = -1790
349466
YDOT = 16027
814067 feet/sec YDOT = 4885
277728 meter/sec
ZDOT = -17074
387651 ZDOT = -5204
273356
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 14270
44774865
00016717 00000-0 10270-3 0 9017
2 25544 51
6450 312
7329 0001807 129
3348 230
7963 15
50653814 27193
Satellite: ISS
Catalog Number: 25544
Epoch time: 14270
44774865 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 312
7329 deg
Eccentricity:
0001807
Arg of perigee: 129
3348 deg
Mean anomaly: 230
7963 deg
Mean motion: 15
50653814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2719
Checksum: 314
Coasting Arc #3 (Orbit 2734)
---------------------------------------
Vector Time (GMT): 2014/271/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5307366
38 A = 6795219
69 meter
Y = -2895912
68 meter E =
0014222
Z = 3089291
71 I = 51
36697
XDOT = 384
100629 Wp = 89
86859
YDOT = 5912
589646 meter/sec RA = 307
27834 deg
ZDOT = 4863
174231 TA = 305
75616
MA = 305
88833
Ha = 226
866 n
mi
Hp = 219
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17412619
37 X = 5324347
66
Y = -9501025
87 feet Y = -2836467
00 meter
Z = 10135471
50 Z = 3115116
11
XDOT = 1260
172668 XDOT = 294
332022
YDOT = 19398
259994 feet/sec YDOT = 5916
383496 meter/sec
ZDOT = 15955
296034 ZDOT = 4864
821498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19652484
36 X = -5990077
23
Y = 2236179
95 feet Y = 681587
65 meter
Z = 10245776
98 Z = 3122912
82
XDOT = 6423
846068 XDOT = 1957
988282
YDOT = -16965
091349 feet/sec YDOT = -5170
959843 meter/sec
ZDOT = 15961
260626 ZDOT = 4864
992239
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 14271
47887441
00016717 00000-0 10270-3 0 9027
2 25544 51
6454 307
6191 0001767 131
1566 228
9738 15
50692457 27358
Satellite: ISS
Catalog Number: 25544
Epoch time: 14271
47887441 = yrday
fracday
Element set: 902
Inclination: 51
6454 deg
RA of node: 307
6191 deg
Eccentricity:
0001767
Arg of perigee: 131
1566 deg
Mean anomaly: 228
9738 deg
Mean motion: 15
50692457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2735
Checksum: 329
Coasting Arc #4 (Orbit 2749)
---------------------------------------
Vector Time (GMT): 2014/272/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5100326
75 A = 6793892
78 meter
Y = 2747070
46 meter E =
0006639
Z = -3554533
91 I = 51
34395
XDOT = -265
181348 Wp = 94
34531
YDOT = -6230
447424 meter/sec RA = 302
29958 deg
ZDOT = -4442
302303 TA = 127
69940
MA = 127
63919
Ha = 226
898 n
mi
Hp = 219
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16733355
47 X = -5113399
01
Y = 9012698
35 feet Y = 2689961
89 meter
Z = -11661856
67 Z = -3579342
95
XDOT = -870
017547 XDOT = -173
911737
YDOT = -20441
100472 feet/sec YDOT = -6232
902936 meter/sec
ZDOT = -14574
482620 ZDOT = -4443
368282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18792121
58 X = 5727838
66
Y = -2368012
68 feet Y = -721770
26 meter
Z = -11767816
29 Z = -3586830
41
XDOT = -6849
184368 XDOT = -2087
631395
YDOT = 17966
653691 feet/sec YDOT = 5476
236045 meter/sec
ZDOT = -14577
924462 ZDOT = -4443
351376
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 14272
44554321
00016717 00000-0 10270-3 0 9034
2 25544 51
6449 302
8247 0001792 130
7013 229
4294 15
50697342 27509
Satellite: ISS
Catalog Number: 25544
Epoch time: 14272
44554321 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 302
8247 deg
Eccentricity:
0001792
Arg of perigee: 130
7013 deg
Mean anomaly: 229
4294 deg
Mean motion: 15
50697342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2750
Checksum: 297
Coasting Arc #5 (Orbit 2765)
---------------------------------------
Vector Time (GMT): 2014/273/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4885796
36 A = 6792514
58 meter
Y = -2570755
95 meter E =
0012472
Z = 3949028
44 I = 51
32396
XDOT = 210
662269 Wp = 104
65366
YDOT = 6544
498006 meter/sec RA = 297
31860 deg
ZDOT = 3986
041593 TA = 303
52364
MA = 303
64272
Ha = 226
759 n
mi
Hp = 219
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16029515
61 X = 4894996
67
Y = -8434238
67 feet Y = -2516068
06 meter
Z = 12956130
06 Z = 3972785
79
XDOT = 691
149175 XDOT = 118
101373
YDOT = 21471
450150 feet/sec YDOT = 6546
336545 meter/sec
ZDOT = 13077
564281 ZDOT = 3986
839628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17880415
56 X = -5449950
66
Y = 2394420
49 feet Y = 729819
37 meter
Z = 13057585
87 Z = 3979952
17
XDOT = 7032
928076 XDOT = 2143
636478
YDOT = -19053
086381 feet/sec YDOT = -5807
380729 meter/sec
ZDOT = 13079
818415 ZDOT = 3986
728653
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 14273
47664019
00016717 00000-0 10270-3 0 9045
2 25544 51
6451 297
7109 0001763 132
4816 227
6485 15
50736615 27665
Satellite: ISS
Catalog Number: 25544
Epoch time: 14273
47664019 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 297
7109 deg
Eccentricity:
0001763
Arg of perigee: 132
4816 deg
Mean anomaly: 227
6485 deg
Mean motion: 15
50736615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2766
Checksum: 324
Coasting Arc #6 (Orbit 2780)
---------------------------------------
Vector Time (GMT): 2014/274/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4700538
09 A = 6791176
96 meter
Y = 2312250
18 meter E =
0009662
Z = -4331266
12 I = 51
30636
XDOT = -183
232530 Wp = 78
88281
YDOT = -6829
483672 meter/sec RA = 292
33471 deg
ZDOT = -3451
824881 TA = 155
84533
MA = 155
80000
Ha = 226
828 n
mi
Hp = 219
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15421712
91 X = -4705004
77
Y = 7586122
65 feet Y = 2259660
42 meter
Z = -14210190
68 Z = -4354111
90
XDOT = -601
156595 XDOT = -90
082040
YDOT = -22406
442495 feet/sec YDOT = -6831
012123 meter/sec
ZDOT = -11324
884780 ZDOT = -3452
488234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16975585
16 X = 5174158
36
Y = -2103930
57 feet Y = -641278
04 meter
Z = -14307724
83 Z = -4360994
53
XDOT = -7043
417045 XDOT = -2146
833515
YDOT = 20090
525362 feet/sec YDOT = 6123
592130 meter/sec
ZDOT = -11326
525636 ZDOT = -3452
325014
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 14274
44328174
00016717 00000-0 10270-3 0 9053
2 25544 51
6454 292
9163 0001794 132
8373 227
2929 15
50741236 27812
Satellite: ISS
Catalog Number: 25544
Epoch time: 14274
44328174 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 292
9163 deg
Eccentricity:
0001794
Arg of perigee: 132
8373 deg
Mean anomaly: 227
2929 deg
Mean motion: 15
50741236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2781
Checksum: 319
Coasting Arc #7 (Orbit 2796)
---------------------------------------
Vector Time (GMT): 2014/275/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4524227
05 A = 6789888
53 meter
Y = -2026990
72 meter E =
0009884
Z = 4634249
93 I = 51
29082
XDOT = 209
538005 Wp = 118
57868
YDOT = 7097
151372 meter/sec RA = 287
34932 deg
ZDOT = 2890
329533 TA = 302
48089
MA = 302
57640
Ha = 226
674 n
mi
Hp = 219
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14843264
59 X = 4524045
25
Y = -6650232
02 feet Y = -1976398
53 meter
Z = 15204232
05 Z = 4656227
83
XDOT = 687
460646 XDOT = 116
120072
YDOT = 23284
617361 feet/sec YDOT = 7098
972466 meter/sec
ZDOT = 9482
708440 ZDOT = 2891
119962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16088211
16 X = -4903686
76
Y = 1690154
05 feet Y = 515158
96 meter
Z = 15298026
11 Z = 4662838
36
XDOT = 6827
653880 XDOT = 2081
068903
YDOT = -21135
039089 feet/sec YDOT = -6441
959914 meter/sec
ZDOT = 9484
855113 ZDOT = 2890
983839
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 14275
47434949
00016717 00000-0 10270-3 0 9066
2 25544 51
6448 287
8025 0001796 133
1464 226
9838 15
50779714 27976
Satellite: ISS
Catalog Number: 25544
Epoch time: 14275
47434949 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 287
8025 deg
Eccentricity:
0001796
Arg of perigee: 133
1464 deg
Mean anomaly: 226
9838 deg
Mean motion: 15
50779714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2797
Checksum: 356
Coasting Arc #8 (Orbit 2811)
---------------------------------------
Vector Time (GMT): 2014/276/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4395082
24 A = 6788804
73 meter
Y = 1673125
23 meter E =
0013100
Z = -4908122
80 I = 51
27960
XDOT = -256
758630 Wp = 80
35927
YDOT = -7305
802724 meter/sec RA = 282
36128 deg
ZDOT = -2263
585726 TA = 167
37835
MA = 167
34552
Ha = 226
745 n
mi
Hp = 219
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14419561
15 X = -4389622
70
Y = 5489256
02 feet Y = 1624006
64 meter
Z = -16102765
09 Z = -4929460
46
XDOT = -842
383957 XDOT = -164
048562
YDOT = -23969
169041 feet/sec YDOT = -7308
155809 meter/sec
ZDOT = -7426
462357 ZDOT = -2264
607142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15301794
77 X = 4663987
05
Y = -985611
68 feet Y = -300414
44 meter
Z = -16193775
51 Z = -4935862
78
XDOT = -6434
617894 XDOT = -1961
271534
YDOT = 22007
756028 feet/sec YDOT = 6707
964037 meter/sec
ZDOT = -7429
569715 ZDOT = -2264
532849
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 14276
44096263
00016717 00000-0 10270-3 0 9078
2 25544 51
6456 283
0079 0001783 136
3862 223
7430 15
50784829 28129
Satellite: ISS
Catalog Number: 25544
Epoch time: 14276
44096263 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 283
0079 deg
Eccentricity:
0001783
Arg of perigee: 136
3862 deg
Mean anomaly: 223
7430 deg
Mean motion: 15
50784829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2812
Checksum: 321
Coasting Arc #9 (Orbit 2827)
---------------------------------------
Vector Time (GMT): 2014/277/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4288457
21 A = 6787853
38 meter
Y = -1298906
54 meter E =
0006779
Z = 5095058
15 I = 51
26963
XDOT = 339
353388 Wp = 127
62734
YDOT = 7485
957817 meter/sec RA = 277
37192 deg
ZDOT = 1617
248942 TA = 306
65188
MA = 306
71419
Ha = 226
582 n
mi
Hp = 219
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14069741
51 X = 4277912
93
Y = -4261504
40 feet Y = -1251008
61 meter
Z = 16716070
03 Z = 5115865
46
XDOT = 1113
364133 XDOT = 247
762355
YDOT = 24560
229060 feet/sec YDOT = 7489
240757 meter/sec
ZDOT = 5305
934848 ZDOT = 1618
674148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14598503
88 X = -4449623
98
Y = 169496
21 feet Y = 51662
44 meter
Z = 16804761
19 Z = 5122091
21
XDOT = 5869
344329 XDOT = 1788
976151
YDOT = -22811
999013 feet/sec YDOT = -6953
097299 meter/sec
ZDOT = 5310
744502 ZDOT = 1618
714924
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 14277
47200023
00016717 00000-0 10270-3 0 9084
2 25544 51
6441 277
8936 0001820 135
2571 224
8727 15
50824175 28280
Satellite: ISS
Catalog Number: 25544
Epoch time: 14277
47200023 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 277
8936 deg
Eccentricity:
0001820
Arg of perigee: 135
2571 deg
Mean anomaly: 224
8727 deg
Mean motion: 15
50824175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2828
Checksum: 308
Coasting Arc #10 (Orbit 2842)
---------------------------------------
Vector Time (GMT): 2014/278/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4242104
03 A = 6787268
67 meter
Y = 878247
59 meter E =
0015392
Z = -5238418
36 I = 51
26544
XDOT = -428
417562 Wp = 88
34617
YDOT = -7583
331006 meter/sec RA = 272
38100 deg
ZDOT = -926
384222 TA = 172
73625
MA = 172
71392
Ha = 226
642 n
mi
Hp = 219
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13917664
14 X = -4226162
85
Y = 2881389
74 feet Y = 830898
07 meter
Z = -17186411
93 Z = -5258987
39
XDOT = -1405
569429 XDOT = -339
087060
YDOT = -24879
694903 feet/sec YDOT = -7587
622497 meter/sec
ZDOT = -3039
318315 ZDOT = -928
247436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14079367
59 X = 4291391
24
Y = 869609
19 feet Y = 265056
88 meter
Z = -17274018
79 Z = -5265120
93
XDOT = -5170
724169 XDOT = -1576
036727
YDOT = 23335
952725 feet/sec YDOT = 7112
798391 meter/sec
ZDOT = -3045
990054 ZDOT = -928
417768
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 14278
43858387
00016717 00000-0 10270-3 0 9094
2 25544 51
6450 273
0988 0001744 141
1457 218
9819 15
50828118 28433
Satellite: ISS
Catalog Number: 25544
Epoch time: 14278
43858387 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 273
0988 deg
Eccentricity:
0001744
Arg of perigee: 141
1457 deg
Mean anomaly: 218
9819 deg
Mean motion: 15
50828118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2843
Checksum: 341
Coasting Arc #11 (Orbit 2858)
---------------------------------------
Vector Time (GMT): 2014/279/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4226354
68 A = 6786863
23 meter
Y = -448272
59 meter E =
0004032
Z = 5288290
64 I = 51
26261
XDOT = 528
382324 Wp = 116
89474
YDOT = 7644
824603 meter/sec RA = 267
38887 deg
ZDOT = 223
825302 TA = 330
94899
MA = 330
97143
Ha = 226
457 n
mi
Hp = 219
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13865993
06 X = 4205364
23
Y = -1470710
60 feet Y = -401127
35 meter
Z = 17350034
90 Z = 5308770
91
XDOT = 1733
537810 XDOT = 441
769574
YDOT = 25081
445547 feet/sec YDOT = 7650
249069 meter/sec
ZDOT = 734
334980 ZDOT = 226
180645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13692047
60 X = -4173336
11
Y = -1981059
23 feet Y = -603826
85 meter
Z = 17437193
03 Z = 5314856
44
XDOT = 4387
882421 XDOT = 1337
426562
YDOT = -23730
671934 feet/sec YDOT = -7233
108806 meter/sec
ZDOT = 743
103618 ZDOT = 226
497983
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 14279
46959019
00016717 00000-0 10270-3 0 9104
2 25544 51
6434 267
9837 0001788 140
0150 220
1133 15
50870758 28594
Satellite: ISS
Catalog Number: 25544
Epoch time: 14279
46959019 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 267
9837 deg
Eccentricity:
0001788
Arg of perigee: 140
0150 deg
Mean anomaly: 220
1133 deg
Mean motion: 15
50870758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2859
Checksum: 322
Coasting Arc #12 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2014/280/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4276130
35 A = 6786938
21 meter
Y = 432
99 meter E =
0015798
Z = -5284178
54 I = 51
26588
XDOT = -614
716476 Wp = 98
73537
YDOT = -7610
655930 meter/sec RA = 262
39690 deg
ZDOT = 495
748244 TA = 176
03532
MA = 176
02279
Ha = 226
523 n
mi
Hp = 219
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14029299
06 X = -4250148
21
Y = 1420
57 feet Y = -47240
97 meter
Z = -17336543
77 Z = -5304888
53
XDOT = -2016
786338 XDOT = -531
974888
YDOT = -24969
343601 feet/sec YDOT = -7617
067380 meter/sec
ZDOT = 1626
470616 ZDOT = 492
964092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13543981
57 X = 4128205
58
Y = 3212577
20 feet Y = 979193
53 meter
Z = -17424606
03 Z = -5311019
92
XDOT = -3556
044624 XDOT = -1083
882401
YDOT = 23775
303385 feet/sec YDOT = 7246
712472 meter/sec
ZDOT = 1615
861247 ZDOT = 492
514508
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 14280
43614366
00016717 00000-0 10270-3 0 9117
2 25544 51
6441 263
1887 0001682 146
5982 213
5275 15
50871584 28740
Satellite: ISS
Catalog Number: 25544
Epoch time: 14280
43614366 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 263
1887 deg
Eccentricity:
0001682
Arg of perigee: 146
5982 deg
Mean anomaly: 213
5275 deg
Mean motion: 15
50871584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2874
Checksum: 321
Coasting Arc #13 (Orbit 2889)
---------------------------------------
Vector Time (GMT): 2014/281/10:06:01
818
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4356999
76 A = 6787191
84 meter
Y = 443007
76 meter E =
0004360
Z = 5181627
64 I = 51
27126
XDOT = 683
736787 Wp = 78
87347
YDOT = 7538
252210 meter/sec RA = 257
40438 deg
ZDOT = -1217
711904 TA = 22
88404
MA = 22
86462
Ha = 226
298 n
mi
Hp = 219
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14294618
65 X = 4326551
00
Y = 1453437
54 feet Y = 491561
03 meter
Z = 17000090
68 Z = 5202719
67
XDOT = 2243
230930 XDOT = 605
306844
YDOT = 24731
798589 feet/sec YDOT = 7545
459502 meter/sec
ZDOT = -3995
117794 ZDOT = -1214
581899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13547117
96 X = -4129161
56
Y = -4457485
94 feet Y = -1358641
71 meter
Z = 17089707
43 Z = 5208942
82
XDOT = 2752
092208 XDOT = 838
837705
YDOT = -23656
026657 feet/sec YDOT = -7210
356925 meter/sec
ZDOT = -3983
017164 ZDOT = -1214
023631
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 14281
46711766
00016717 00000-0 10270-3 0 9124
2 25544 51
6431 258
0730 0001694 147
3750 212
7506 15
50919603 28905
Satellite: ISS
Catalog Number: 25544
Epoch time: 14281
46711766 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 258
0730 deg
Eccentricity:
0001694
Arg of perigee: 147
3750 deg
Mean anomaly: 212
7506 deg
Mean motion: 15
50919603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2890
Checksum: 303
Coasting Arc #14 (Orbit 2893)
---------------------------------------
Vector Time (GMT): 2014/281/17:06:03
030
Vector Time (MET): N/A
Weight (LBS) : 946249
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4442653
54 A = 6789980
62 meter
Y = -1439481
40 meter E =
0011001
Z = -4939233
17 I = 51
27963
XDOT = -40
235147 Wp = 112
74841
YDOT = -7337
938558 meter/sec RA = 255
94233 deg
ZDOT = 2174
464190 TA = 178
60863
MA = 178
60557
Ha = 226
353 n
mi
Hp = 221
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14575634
99 X = -4402233
09
Y = -4722708
00 feet Y = -1488936
69 meter
Z = -16204833
23 Z = -4960716
97
XDOT = -132
005075 XDOT = 31
259328
YDOT = -24074
601569 feet/sec YDOT = -7337
988452 meter/sec
ZDOT = 7134
068865 ZDOT = 2174
443377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3976910
12 X = 1212162
20
Y = -14696111
60 feet Y = -4479374
82 meter
Z = -16295957
04 Z = -4967007
71
XDOT = 22961
701795 XDOT = 6998
726707
YDOT = -1699
261073 feet/sec YDOT = -517
934775 meter/sec
ZDOT = 7135
155012 ZDOT = 2174
795248
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 14281
72485968
00016717 00000-0 10270-3 0 9136
2 25544 51
6458 256
7937 0001946 244
7073 115
3876 15
50337900 28944
Satellite: ISS
Catalog Number: 25544
Epoch time: 14281
72485968 = yrday
fracday
Element set: 913
Inclination: 51
6458 deg
RA of node: 256
7937 deg
Eccentricity:
0001946
Arg of perigee: 244
7073 deg
Mean anomaly: 115
3876 deg
Mean motion: 15
50337900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2894
Checksum: 344
Coasting Arc #15 (Orbit 2909)
---------------------------------------
Vector Time (GMT): 2014/282/17:06:03
030
Vector Time (MET): N/A
Weight (LBS) : 946249
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4579241
49 A = 6790586
71 meter
Y = 1610669
38 meter E =
0005600
Z = 4745597
76 I = 51
29079
XDOT = 229
240332 Wp = 58
74520
YDOT = 7185
642537 meter/sec RA = 250
95854 deg
ZDOT = -2654
847736 TA = 57
63687
MA = 57
58268
Ha = 226
079 n
mi
Hp = 221
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15023758
19 X = 4537837
20
Y = 5284348
36 feet Y = 1661646
48 meter
Z = 15569546
45 Z = 4767742
77
XDOT = 752
100827 XDOT = 161
768445
YDOT = 23574
942706 feet/sec YDOT = 7187
828481 meter/sec
ZDOT = -8710
130369 ZDOT = -2653
898829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4252893
92 X = -1296282
07
Y = 15251799
04 feet Y = 4648748
35 meter
Z = 15663458
86 Z = 4774222
26
XDOT = -22351
684146 XDOT = -6812
793328
YDOT = 2726
954644 feet/sec YDOT = 831
175775 meter/sec
ZDOT = -8707
239936 ZDOT = -2653
966732
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 14282
75620355
00016717 00000-0 10270-3 0 9142
2 25544 51
6459 251
6815 0001978 250
9819 109
1118 15
50390675 29103
Satellite: ISS
Catalog Number: 25544
Epoch time: 14282
75620355 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 251
6815 deg
Eccentricity:
0001978
Arg of perigee: 250
9819 deg
Mean anomaly: 109
1118 deg
Mean motion: 15
50390675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2910
Checksum: 319
Coasting Arc #16 (Orbit 2924)
---------------------------------------
Vector Time (GMT): 2014/283/17:06:03
030
Vector Time (MET): N/A
Weight (LBS) : 946249
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4754538
02 A = 6791467
96 meter
Y = -1756676
04 meter E =
0008308
Z = -4528695
25 I = 51
30537
XDOT = -383
595007 Wp = 118
68558
YDOT = -6983
052495 meter/sec RA = 245
97557 deg
ZDOT = 3111
893704 TA = 182
70295
MA = 182
70744
Ha = 226
184 n
mi
Hp = 221
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15598878
03 X = -4712541
67
Y = -5763372
85 feet Y = -1809609
99 meter
Z = -14857924
04 Z = -4551690
44
XDOT = -1258
513801 XDOT = -320
597294
YDOT = -22910
277215 feet/sec YDOT = -6986
989558 meter/sec
ZDOT = 10209
625013 ZDOT = 3110
183916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4417559
61 X = 1346472
17
Y = -15941126
24 feet Y = -4858855
28 meter
Z = -14955434
82 Z = -4558416
53
XDOT = 21549
896805 XDOT = 6568
408546
YDOT = -3599
325081 feet/sec YDOT = -1097
074285 meter/sec
ZDOT = 10203
461888 ZDOT = 3110
015183
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 14283
72307421
00016717 00000-0 10270-3 0 9157
2 25544 51
6465 246
8885 0002015 253
9755 106
1173 15
50388277 29257
Satellite: ISS
Catalog Number: 25544
Epoch time: 14283
72307421 = yrday
fracday
Element set: 915
Inclination: 51
6465 deg
RA of node: 246
8885 deg
Eccentricity:
0002015
Arg of perigee: 253
9755 deg
Mean anomaly: 106
1173 deg
Mean motion: 15
50388277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2925
Checksum: 318
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