[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 27th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 3 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
There are no maneuvers
Coasting Arc #1 (Orbit 3650)
---------------------------------------
Vector Time (GMT): 2014/330/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 727459
99 A = 6785118
84 meter
Y = -4157090
39 meter E =
0021544
Z = -5331473
20 I = 51
71993
XDOT = 7456
579017 Wp = 80
92338
YDOT = 1676
867347 meter/sec RA = 14
37679 deg
ZDOT = -287
758097 TA = 186
31581
MA = 186
34301
Ha = 227
674 n
mi
Hp = 216
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2386679
76 X = 799790
29
Y = -13638747
99 feet Y = -4148550
72 meter
Z = -17491709
98 Z = -5327763
83
XDOT = 24463
841920 XDOT = 7438
671552
YDOT = 5501
533290 feet/sec YDOT = 1760
151537 meter/sec
ZDOT = -944
088246 ZDOT = -251
578161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10538604
30 X = 3212166
59
Y = 9012872
42 feet Y = 2747123
51 meter
Z = -17475055
22 Z = -5326396
83
XDOT = -16394
528714 XDOT = -4997
052352
YDOT = 17623
113629 feet/sec YDOT = 5371
525034 meter/sec
ZDOT = -790
133362 ZDOT = -240
832649
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 14330
50360560
00016717 00000-0 10270-3 0 9003
2 25544 51
6458 14
8479 0007043 67
1079 293
0815 15
51474822 36510
Satellite: ISS
Catalog Number: 25544
Epoch time: 14330
50360560 = yrday
fracday
Element set: 900
Inclination: 51
6458 deg
RA of node: 14
8479 deg
Eccentricity:
0007043
Arg of perigee: 67
1079 deg
Mean anomaly: 293
0815 deg
Mean motion: 15
51474822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3651
Checksum: 297
Coasting Arc #2 (Orbit 3666)
---------------------------------------
Vector Time (GMT): 2014/331/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1436798
65 A = 6785005
78 meter
Y = 3994438
99 meter E =
0010214
Z = 5285256
23 I = 51
68971
XDOT = -7433
185327 Wp = 67
72461
YDOT = -1773
000788 meter/sec RA = 9
40878 deg
ZDOT = -675
902886 TA = 28
75050
MA = 28
69424
Ha = 227
663 n
mi
Hp = 216
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4713906
33 X = -1507032
85
Y = 13105114
81 feet Y = 3977978
84 meter
Z = 17340079
49 Z = 5278106
00
XDOT = -24387
090969 XDOT = -7409
523426
YDOT = -5816
931720 feet/sec YDOT = -1855
991154 meter/sec
ZDOT = -2217
529153 ZDOT = -711
955088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9092040
07 X = -2771253
81
Y = -10601137
05 feet Y = -3231226
57 meter
Z = 17308784
02 Z = 5275717
37
XDOT = 16188
306306 XDOT = 4934
195762
YDOT = -17780
847268 feet/sec YDOT = -5419
602247 meter/sec
ZDOT = -2370
917356 ZDOT = -722
655610
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 14331
53416925
00016717 00000-0 10270-3 0 9015
2 25544 51
6457 9
7306 0007142 70
7412 289
4512 15
51558780 36678
Satellite: ISS
Catalog Number: 25544
Epoch time: 14331
53416925 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node: 9
7306 deg
Eccentricity:
0007142
Arg of perigee: 70
7412 deg
Mean anomaly: 289
4512 deg
Mean motion: 15
51558780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3667
Checksum: 307
Coasting Arc #3 (Orbit 3681)
---------------------------------------
Vector Time (GMT): 2014/332/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2144956
58 A = 6785765
75 meter
Y = -3906422
01 meter E =
0020054
Z = -5134713
23 I = 51
66189
XDOT = 7242
680107 Wp = 92
03932
YDOT = 1849
665099 meter/sec RA = 4
43844 deg
ZDOT = 1623
125816 TA = 193
62920
MA = 193
68343
Ha = 227
654 n
mi
Hp = 216
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7037259
12 X = 2213422
61
Y = -12816345
17 feet Y = -3882052
76 meter
Z = -16846172
00 Z = -5124127
08
XDOT = 23762
073843 XDOT = 7213
573758
YDOT = 6068
455049 feet/sec YDOT = 1930
494657 meter/sec
ZDOT = 5325
215932 ZDOT = 1658
239291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7922346
25 X = 2414731
14
Y = 12351658
54 feet Y = 3764785
52 meter
Z = -16800243
80 Z = -5120714
31
XDOT = -15658
273262 XDOT = -4772
641690
YDOT = 17468
059826 feet/sec YDOT = 5324
264635 meter/sec
ZDOT = 5474
580979 ZDOT = 1668
652282
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 14332
50029858
00016717 00000-0 10270-3 0 9029
2 25544 51
6465 4
9326 0007242 73
6289 286
5659 15
51560707 36820
Satellite: ISS
Catalog Number: 25544
Epoch time: 14332
50029858 = yrday
fracday
Element set: 902
Inclination: 51
6465 deg
RA of node: 4
9326 deg
Eccentricity:
0007242
Arg of perigee: 73
6289 deg
Mean anomaly: 286
5659 deg
Mean motion: 15
51560707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3682
Checksum: 323
Coasting Arc #4 (Orbit 3697)
---------------------------------------
Vector Time (GMT): 2014/333/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2862563
52 A = 6786832
29 meter
Y = 3831170
51 meter E =
0014636
Z = 4805846
54 I = 51
63424
XDOT = -6957
302759 Wp = 68
76337
YDOT = -1966
088406 meter/sec RA = 359
46735 deg
ZDOT = -2565
229810 TA = 46
54199
MA = 46
42034
Ha = 227
649 n
mi
Hp = 215
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9391612
61 X = -2928537
24
Y = 12569457
06 feet Y = 3798790
52 meter
Z = 15767213
07 Z = 4791780
32
XDOT = -22825
796453 XDOT = -6922
339264
YDOT = -6450
421281 feet/sec YDOT = -2043
693952 meter/sec
ZDOT = -8416
108302 ZDOT = -2598
942753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6840682
23 X = -2085039
94
Y = -14188401
14 feet Y = -4324624
67 meter
Z = 15706463
18 Z = 4787329
98
XDOT = 15114
440339 XDOT = 4606
881415
YDOT = -16804
308875 feet/sec YDOT = -5121
953345 meter/sec
ZDOT = -8559
471247 ZDOT = -2608
926836
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 14333
53080685
00016717 00000-0 10270-3 0 9039
2 25544 51
6457 359
8150 0007345 77
3892 282
8080 15
51649054 36980
Satellite: ISS
Catalog Number: 25544
Epoch time: 14333
53080685 = yrday
fracday
Element set: 903
Inclination: 51
6457 deg
RA of node: 359
8150 deg
Eccentricity:
0007345
Arg of perigee: 77
3892 deg
Mean anomaly: 282
8080 deg
Mean motion: 15
51649054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3698
Checksum: 333
Coasting Arc #5 (Orbit 3712)
---------------------------------------
Vector Time (GMT): 2014/334/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3520465
71 A = 6788517
84 meter
Y = -3825456
82 meter E =
0015589
Z = -4379780
80 I = 51
60974
XDOT = 6517
817472 Wp = 96
21541
YDOT = 2093
607910 meter/sec RA = 354
49609 deg
ZDOT = 3419
232583 TA = 208
49784
MA = 208
58316
Ha = 227
610 n
mi
Hp = 215
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11550084
36 X = 3584257
00
Y = -12550711
36 feet Y = -3785731
98 meter
Z = -14369359
59 Z = -4362523
78
XDOT = 21383
915590 XDOT = 6477
312137
YDOT = 6868
792357 feet/sec YDOT = 2166
267871 meter/sec
ZDOT = 11217
954669 ZDOT = 3450
797173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6117011
24 X = 1864465
02
Y = 15988689
25 feet Y = 4873352
48 meter
Z = -14295009
23 Z = -4357118
81
XDOT = -14413
791218 XDOT = -4393
323563
YDOT = 15637
993003 feet/sec YDOT = 4766
460267 meter/sec
ZDOT = 11352
123730 ZDOT = 3460
127313
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 14334
49688418
00016717 00000-0 10270-3 0 9044
2 25544 51
6469 355
0173 0007436 80
4977 279
7014 15
51657324 37135
Satellite: ISS
Catalog Number: 25544
Epoch time: 14334
49688418 = yrday
fracday
Element set: 904
Inclination: 51
6469 deg
RA of node: 355
0173 deg
Eccentricity:
0007436
Arg of perigee: 80
4977 deg
Mean anomaly: 279
7014 deg
Mean motion: 15
51657324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3713
Checksum: 333
Coasting Arc #6 (Orbit 3728)
---------------------------------------
Vector Time (GMT): 2014/335/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4150119
65 A = 6790359
97 meter
Y = 3811504
27 meter E =
0019107
Z = 3774605
08 I = 51
58406
XDOT = -5974
831423 Wp = 83
43181
YDOT = -2302
017152 meter/sec RA = 349
52453 deg
ZDOT = -4224
183134 TA = 51
30800
MA = 51
13726
Ha = 227
585 n
mi
Hp = 215
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13615878
13 X = -4210768
40
Y = 12504935
26 feet Y = 3764755
79 meter
Z = 12383874
93 Z = 3754296
83
XDOT = -19602
465298 XDOT = -5928
125662
YDOT = -7552
549710 feet/sec YDOT = -2368
570399 meter/sec
ZDOT = -13858
868549 ZDOT = -4253
094996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5474181
56 X = -1668530
54
Y = -17718769
32 feet Y = -5400680
89 meter
Z = 12296521
92 Z = 3747979
88
XDOT = 13860
767238 XDOT = 4224
761854
YDOT = -14032
379639 feet/sec YDOT = -4277
069314 meter/sec
ZDOT = -13981
677405 ZDOT = -4261
615273
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 14335
52733754
00016717 00000-0 10270-3 0 9054
2 25544 51
6455 349
8989 0007502 84
0837 276
1169 15
51731692 37295
Satellite: ISS
Catalog Number: 25544
Epoch time: 14335
52733754 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 349
8989 deg
Eccentricity:
0007502
Arg of perigee: 84
0837 deg
Mean anomaly: 276
1169 deg
Mean motion: 15
51731692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3729
Checksum: 343
Coasting Arc #7 (Orbit 3743)
---------------------------------------
Vector Time (GMT): 2014/336/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4669133
73 A = 6792220
23 meter
Y = -3843280
32 meter E =
0012003
Z = -3100602
78 I = 51
56075
XDOT = 5323
444539 Wp = 81
90204
YDOT = 2546
145999 meter/sec RA = 344
55431 deg
ZDOT = 4878
321301 TA = 242
47254
MA = 242
59456
Ha = 227
521 n
mi
Hp = 215
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15318680
20 X = 4726825
14
Y = -12609187
40 feet Y = -3790744
39 meter
Z = -10172581
30 Z = -3077780
37
XDOT = 17465
369224 XDOT = 5270
879585
YDOT = 8353
497371 feet/sec YDOT = 2605
382188 meter/sec
ZDOT = 16004
991144 ZDOT = 4904
054648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5179396
19 X = 1578679
96
Y = 19204508
66 feet Y = 5853534
24 meter
Z = -10074506
57 Z = -3070709
60
XDOT = -13349
088302 XDOT = -4068
802115
YDOT = 12022
503536 feet/sec YDOT = 3664
459078 meter/sec
ZDOT = 16114
192476 ZDOT = 4911
605867
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 14336
49336265
00016717 00000-0 10270-3 0 9068
2 25544 51
6462 345
1013 0007587 88
0076 272
1944 15
51765174 37448
Satellite: ISS
Catalog Number: 25544
Epoch time: 14336
49336265 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 345
1013 deg
Eccentricity:
0007587
Arg of perigee: 88
0076 deg
Mean anomaly: 272
1944 deg
Mean motion: 15
51765174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3744
Checksum: 320
Coasting Arc #8 (Orbit 3759)
---------------------------------------
Vector Time (GMT): 2014/337/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5124970
90 A = 6793992
81 meter
Y = 3827158
28 meter E =
0021204
Z = 2264428
42 I = 51
53547
XDOT = -4578
756682 Wp = 101
86085
YDOT = -2896
857951 meter/sec RA = 339
58334 deg
ZDOT = -5428
014722 TA = 52
91134
MA = 52
71769
Ha = 227
466 n
mi
Hp = 215
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16814208
98 X = -5178386
23
Y = 12556293
55 feet Y = 3769548
77 meter
Z = 7429227
08 Z = 2239402
00
XDOT = -15022
167593 XDOT = -4519
655021
YDOT = -9504
127135 feet/sec YDOT = -2947
729902 meter/sec
ZDOT = -17808
447250 ZDOT = -5450
114630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4876302
12 X = -1486296
89
Y = -20449572
70 feet Y = -6233029
76 meter
Z = 7321762
11 Z = 2231673
09
XDOT = 13130
546732 XDOT = 4002
190644
YDOT = -9586
975768 feet/sec YDOT = -2922
110214 meter/sec
ZDOT = -17902
082422 ZDOT = -5456
554722
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 14337
52376108
00016717 00000-0 10270-3 0 9074
2 25544 51
6447 339
9819 0007584 91
0317 269
1703 15
51804404 37602
Satellite: ISS
Catalog Number: 25544
Epoch time: 14337
52376108 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 339
9819 deg
Eccentricity:
0007584
Arg of perigee: 91
0317 deg
Mean anomaly: 269
1703 deg
Mean motion: 15
51804404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3760
Checksum: 320
Coasting Arc #9 (Orbit 3774)
---------------------------------------
Vector Time (GMT): 2014/338/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5439076
39 A = 6795092
15 meter
Y = -3819262
60 meter E =
0014256
Z = -1406858
45 I = 51
51101
XDOT = 3793
851022 Wp = 64
36222
YDOT = 3291
051321 meter/sec RA = 334
61365 deg
ZDOT = 5784
970627 TA = 280
29583
MA = 280
45652
Ha = 227
365 n
mi
Hp = 215
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17844738
80 X = 5488214
21
Y = -12530389
12 feet Y = -3758164
50 meter
Z = -4615677
32 Z = -1380316
59
XDOT = 12447
017789 XDOT = 3728
665742
YDOT = 10797
412471 feet/sec YDOT = 3333
111813 meter/sec
ZDOT = 18979
562424 ZDOT = 5803
242796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4819183
55 X = 1468887
15
Y = 21289892
01 feet Y = 6489159
08 meter
Z = -4501755
17 Z = -1372134
98
XDOT = -13113
850922 XDOT = -3997
101761
YDOT = 6961
122865 feet/sec YDOT = 2121
750249 meter/sec
ZDOT = 19056
796816 ZDOT = 5808
511670
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 14338
48973364
00016717 00000-0 10270-3 0 9088
2 25544 51
6448 335
1839 0007635 95
8896 264
3126 15
51872419 37757
Satellite: ISS
Catalog Number: 25544
Epoch time: 14338
48973364 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 335
1839 deg
Eccentricity:
0007635
Arg of perigee: 95
8896 deg
Mean anomaly: 264
3126 deg
Mean motion: 15
51872419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3775
Checksum: 359
Coasting Arc #10 (Orbit 3790)
---------------------------------------
Vector Time (GMT): 2014/339/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5667598
72 A = 6795823
71 meter
Y = 3712402
38 meter E =
0019592
Z = 425884
84 I = 51
48455
XDOT = -2946
109200 Wp = 118
20446
YDOT = -3788
795679 meter/sec RA = 329
64191 deg
ZDOT = -5978
644695 TA = 57
19667
MA = 57
00812
Ha = 227
298 n
mi
Hp = 215
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18594483
99 X = -5710759
28
Y = 12179797
83 feet Y = 3648782
26 meter
Z = 1397259
99 Z = 398247
47
XDOT = -9665
712597 XDOT = -2874
480271
YDOT = -12430
432017 feet/sec YDOT = -3821
340033 meter/sec
ZDOT = -19614
976035 ZDOT = -5992
782995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4592873
20 X = -1399907
75
Y = -21756036
25 feet Y = -6631239
85 meter
Z = 1278689
98 Z = 389744
71
XDOT = 13462
043180 XDOT = 4103
230761
YDOT = -4040
653025 feet/sec YDOT = -1231
591042 meter/sec
ZDOT = -19674
486037 ZDOT = -5996
783344
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 14339
52007668
00016717 00000-0 10270-3 0 9090
2 25544 51
6438 330
0636 0007589 98
0852 262
1160 15
51875826 37917
Satellite: ISS
Catalog Number: 25544
Epoch time: 14339
52007668 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 330
0636 deg
Eccentricity:
0007589
Arg of perigee: 98
0852 deg
Mean anomaly: 262
1160 deg
Mean motion: 15
51875826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3791
Checksum: 331
Coasting Arc #11 (Orbit 3806)
---------------------------------------
Vector Time (GMT): 2014/340/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5750811
91 A = 6795498
17 meter
Y = -3572809
74 meter E =
0018613
Z = 515646
05 I = 51
45768
XDOT = 2130
849751 Wp = 69
38175
YDOT = 4315
167581 meter/sec RA = 324
66999 deg
ZDOT = 5965
916608 TA = 296
19020
MA = 296
38147
Ha = 227
145 n
mi
Hp = 215
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18867493
13 X = 5787831
61
Y = -11721816
74 feet Y = -3508293
49 meter
Z = 1691752
14 Z = 543672
63
XDOT = 6990
976873 XDOT = 2053
457326
YDOT = 14157
373955 feet/sec YDOT = 4338
562873 meter/sec
ZDOT = 19573
217218 ZDOT = 5976
080496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4448667
82 X = 1355953
95
Y = 21752505
42 feet Y = 6630163
65 meter
Z = 1811952
70 Z = 552283
18
XDOT = -14076
208086 XDOT = -4290
428225
YDOT = 1201
828856 feet/sec YDOT = 366
317435 meter/sec
ZDOT = 19615
679030 ZDOT = 5978
858968
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 14340
55038838
00016717 00000-0 10270-3 0 9100
2 25544 51
6437 324
9451 0007562 103
6700 256
5294 15
51965225 38075
Satellite: ISS
Catalog Number: 25544
Epoch time: 14340
55038838 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 324
9451 deg
Eccentricity:
0007562
Arg of perigee: 103
6700 deg
Mean anomaly: 256
5294 deg
Mean motion: 15
51965225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 309
Coasting Arc #12 (Orbit 3821)
---------------------------------------
Vector Time (GMT): 2014/341/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5746554
76 A = 6794620
11 meter
Y = 3285395
94 meter E =
0014839
Z = -1519639
11 I = 51
42956
XDOT = -1297
990958 Wp = 123
89445
YDOT = -4904
212191 meter/sec RA = 319
69398 deg
ZDOT = -5742
822271 TA = 72
73530
MA = 72
57297
Ha = 227
103 n
mi
Hp = 215
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18853526
11 X = -5775483
75
Y = 10778858
06 feet Y = 3220972
63 meter
Z = -4985692
63 Z = -1547625
25
XDOT = -4258
500520 XDOT = -1215
157440
YDOT = -16089
935011 feet/sec YDOT = -4918
263472 meter/sec
ZDOT = -18841
280417 ZDOT = -5748
927048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3943556
82 X = -1201996
12
Y = -21327844
02 feet Y = -6500726
86 meter
Z = -5105662
33 Z = -1556205
88
XDOT = 14999
668923 XDOT = 4571
899088
YDOT = 1705
731141 feet/sec YDOT = 519
906852 meter/sec
ZDOT = -18866
322550 ZDOT = -5750
455113
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 14341
51628360
00016717 00000-0 10270-3 0 9113
2 25544 51
6436 320
1446 0007553 104
9894 255
2094 15
51956809 38223
Satellite: ISS
Catalog Number: 25544
Epoch time: 14341
51628360 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 320
1446 deg
Eccentricity:
0007553
Arg of perigee: 104
9894 deg
Mean anomaly: 255
2094 deg
Mean motion: 15
51956809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3822
Checksum: 310
Coasting Arc #13 (Orbit 3837)
---------------------------------------
Vector Time (GMT): 2014/342/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5620957
49 A = 6792864
48 meter
Y = -2933599
73 meter E =
0020254
Z = 2418057
20 I = 51
40118
XDOT = 554
514000 Wp = 86
71987
YDOT = 5485
887589 meter/sec RA = 314
71582 deg
ZDOT = 5328
945105 TA = 300
40591
MA = 300
60594
Ha = 226
904 n
mi
Hp = 215
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18441461
60 X = 5641597
74
Y = -9624671
02 feet Y = -2870627
36 meter
Z = 7933258
54 Z = 2445412
99
XDOT = 1819
271653 XDOT = 467
241906
YDOT = 17998
318861 feet/sec YDOT = 5491
600053 meter/sec
ZDOT = 17483
415700 ZDOT = 5331
427408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3349491
03 X = 1020924
87
Y = 20484853
98 feet Y = 6243783
49 meter
Z = 8050469
33 Z = 2453783
05
XDOT = -16129
783912 XDOT = -4916
358136
YDOT = -4284
967312 feet/sec YDOT = -1306
058037 meter/sec
ZDOT = 17492
903548 ZDOT = 5331
837001
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 14342
54653943
00016717 00000-0 10270-3 0 9123
2 25544 51
6436 315
0259 0007454 110
5132 249
6820 15
52040533 38386
Satellite: ISS
Catalog Number: 25544
Epoch time: 14342
54653943 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 315
0259 deg
Eccentricity:
0007454
Arg of perigee: 110
5132 deg
Mean anomaly: 249
6820 deg
Mean motion: 15
52040533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3838
Checksum: 293
Coasting Arc #14 (Orbit 3852)
---------------------------------------
Vector Time (GMT): 2014/343/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5429108
41 A = 6790690
86 meter
Y = 2404810
15 meter E =
0012088
Z = -3301529
91 I = 51
37291
XDOT = 159
389924 Wp = 104
63061
YDOT = -6052
720213 meter/sec RA = 309
73129 deg
ZDOT = -4688
293852 TA = 113
83413
MA = 113
70738
Ha = 226
909 n
mi
Hp = 215
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17812035
48 X = -5439558
27
Y = 7889797
08 feet Y = 2344040
19 meter
Z = -10831791
04 Z = -3327928
95
XDOT = 522
932821 XDOT = 249
835250
YDOT = -19858
005948 feet/sec YDOT = -6050
431698 meter/sec
ZDOT = -15381
541510 ZDOT = -4687
300395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2238346
44 X = -682248
00
Y = -19288494
26 feet Y = -5879133
05 meter
Z = -10944815
98 Z = -3335979
91
XDOT = 17364
268417 XDOT = 5292
629013
YDOT = 6677
654276 feet/sec YDOT = 2035
349023 meter/sec
ZDOT = -15376
106194 ZDOT = -4686
637168
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 14343
51238126
00016717 00000-0 10270-3 0 9134
2 25544 51
6439 310
2254 0007513 112
0413 248
1537 15
52043433 38534
Satellite: ISS
Catalog Number: 25544
Epoch time: 14343
51238126 = yrday
fracday
Element set: 913
Inclination: 51
6439 deg
RA of node: 310
2254 deg
Eccentricity:
0007513
Arg of perigee: 112
0413 deg
Mean anomaly: 248
1537 deg
Mean motion: 15
52043433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3853
Checksum: 272
Coasting Arc #15 (Orbit 3868)
---------------------------------------
Vector Time (GMT): 2014/344/11:41:21
891
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5158978
23 A = 6788231
08 meter
Y = -1800968
67 meter E =
0017929
Z = 4016888
36 I = 51
34623
XDOT = -758
564796 Wp = 107
97551
YDOT = 6562
680952 meter/sec RA = 304
74347 deg
ZDOT = 3896
805572 TA = 301
35190
MA = 301
52723
Ha = 226
648 n
mi
Hp = 215
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16925781
60 X = 5159220
93
Y = -5908689
85 feet Y = -1743276
56 meter
Z = 13178767
58 Z = 4041950
38
XDOT = -2488
729647 XDOT = -850
823254
YDOT = 21531
105485 feet/sec YDOT = 6553
682057 meter/sec
ZDOT = 12784
795183 ZDOT = 3892
896965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 922641
91 X = 281221
26
Y = 17824318
11 feet Y = 5432852
16 meter
Z = 13285971
13 Z = 4049564
00
XDOT = -18636
144948 XDOT = -5680
296980
YDOT = -8599
592034 feet/sec YDOT = -2621
155652 meter/sec
ZDOT = 12766
840757 ZDOT = 3891
333063
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 14344
54258074
00016717 00000-0 10270-3 0 9143
2 25544 51
6441 305
1067 0007371 117
3964 242
7939 15
52119909 38698
Satellite: ISS
Catalog Number: 25544
Epoch time: 14344
54258074 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 305
1067 deg
Eccentricity:
0007371
Arg of perigee: 117
3964 deg
Mean anomaly: 242
7939 deg
Mean motion: 15
52119909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3869
Checksum: 325
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