[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 18th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12647 59 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
271/15:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
0
Coasting Arc #1 (Orbit 225)
---------------------------------------
Vector Time (GMT): 2015/259/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6666946
94 A = 6789111
94 meter
Y = -580657
59 meter E =
0010247
Z = 1104566
35 I = 51
58864
XDOT = -550
618726 Wp = 35
45786
YDOT = 4895
835632 meter/sec RA = 347
50235 deg
ZDOT = 5877
913391 TA = 336
53738
MA = 336
58411
Ha = 219
272 n
mi
Hp = 216
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21873185
49 X = 6667578
88
Y = -1905044
58 feet Y = -506099
71 meter
Z = 3623905
33 Z = 1136954
88
XDOT = -1806
491882 XDOT = -633
877102
YDOT = 16062
452860 feet/sec YDOT = 4889
213515 meter/sec
ZDOT = 19284
492753 ZDOT = 5875
035691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21865615
48 X = -6664639
60
Y = 1711149
95 feet Y = 521558
50 meter
Z = 3763635
68 Z = 1147156
16
XDOT = 2196
519794 XDOT = 669
499233
YDOT = -14451
988646 feet/sec YDOT = -4404
966139 meter/sec
ZDOT = 19271
135243 ZDOT = 5873
842022
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 15259
57653182
00016717 00000-0 10270-3 0 9006
2 25544 51
6456 347
7403 0005609 280
0692 79
9827 15
54012208 2264
Satellite: ISS
Catalog Number: 25544
Epoch time: 15259
57653182 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 347
7403 deg
Eccentricity:
0005609
Arg of perigee: 280
0692 deg
Mean anomaly: 79
9827 deg
Mean motion: 15
54012208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 226
Checksum: 314
Coasting Arc #2 (Orbit 240)
---------------------------------------
Vector Time (GMT): 2015/260/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6228130
14 A = 6786475
94 meter
Y = -269382
68 meter E =
0001952
Z = -2678947
82 I = 51
54805
XDOT = 2450
306783 Wp = 225
82914
YDOT = -5087
094789 meter/sec RA = 342
52429 deg
ZDOT = -5184
024921 TA = 344
44642
MA = 344
45242
Ha = 219
406 n
mi
Hp = 216
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20433497
85 X = -6211641
52
Y = -883801
46 feet Y = -338937
88 meter
Z = -8789198
90 Z = -2709163
03
XDOT = 8039
064248 XDOT = 2532
192055
YDOT = -16689
943534 feet/sec YDOT = -5059
236639 meter/sec
ZDOT = -17007
955779 ZDOT = -5171
922190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20383645
78 X = 6212935
23
Y = 714486
68 feet Y = 217775
54 meter
Z = -8919386
20 Z = -2718628
91
XDOT = -7955
774100 XDOT = -2424
919946
YDOT = 15272
481241 feet/sec YDOT = 4655
052282 meter/sec
ZDOT = -16954
798670 ZDOT = -5167
822635
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 15260
54112355
00016717 00000-0 10270-3 0 9018
2 25544 51
6443 342
9331 0005620 283
5930 76
4596 15
54031906 2411
Satellite: ISS
Catalog Number: 25544
Epoch time: 15260
54112355 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 342
9331 deg
Eccentricity:
0005620
Arg of perigee: 283
5930 deg
Mean anomaly: 76
4596 deg
Mean motion: 15
54031906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 241
Checksum: 283
Coasting Arc #3 (Orbit 256)
---------------------------------------
Vector Time (GMT): 2015/261/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5355860
55 A = 6782645
00 meter
Y = 1208609
41 meter E =
0005246
Z = 3977971
21 I = 51
50602
XDOT = -4107
426903 Wp = 93
72581
YDOT = 5115
819270 meter/sec RA = 337
53409 deg
ZDOT = 3970
978891 TA = 314
83188
MA = 314
87451
Ha = 219
378 n
mi
Hp = 216
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17571720
96 X = 5322623
86
Y = 3965253
97 feet Y = 1268316
77 meter
Z = 13051086
63 Z = 4003908
30
XDOT = -13475
810049 XDOT = -4183
617663
YDOT = 16784
183957 feet/sec YDOT = 5069
461749 meter/sec
ZDOT = 13028
145969 ZDOT = 3950
840005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17583664
13 X = -5359500
83
Y = -3518383
35 feet Y = -1072403
24 meter
Z = 13162644
61 Z = 4011974
08
XDOT = 12868
916609 XDOT = 3922
445782
YDOT = -15844
014968 feet/sec YDOT = -4829
255762 meter/sec
ZDOT = 12940
350044 ZDOT = 3944
218693
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 15261
57000564
00016717 00000-0 10270-3 0 9021
2 25544 51
6447 337
8041 0005673 288
2488 71
8047 15
54079142 2575
Satellite: ISS
Catalog Number: 25544
Epoch time: 15261
57000564 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 337
8041 deg
Eccentricity:
0005673
Arg of perigee: 288
2488 deg
Mean anomaly: 71
8047 deg
Mean motion: 15
54079142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 257
Checksum: 310
Coasting Arc #4 (Orbit 271)
---------------------------------------
Vector Time (GMT): 2015/262/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4150349
10 A = 6779298
21 meter
Y = -2226289
63 meter E =
0008553
Z = -4883790
78 I = 51
46466
XDOT = 5395
227293 Wp = 47
81786
YDOT = -4908
965200 meter/sec RA = 332
53231 deg
ZDOT = -2344
226005 TA = 199
14002
MA = 199
17218
Ha = 219
723 n
mi
Hp = 216
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13616630
91 X = -4101421
90
Y = -7304099
85 feet Y = -2272428
48 meter
Z = -16022935
64 Z = -4903833
48
XDOT = 17700
876945 XDOT = 5461
107015
YDOT = -16105
528871 feet/sec YDOT = -4848
264088 meter/sec
ZDOT = -7691
030200 ZDOT = -2317
856325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13813936
82 X = 4210487
94
Y = 6721301
18 feet Y = 2048652
60 meter
Z = -16108886
94 Z = -4909988
74
XDOT = -16554
925773 XDOT = -5045
941375
YDOT = 15842
748095 feet/sec YDOT = 4828
869619 meter/sec
ZDOT = -7576
425500 ZDOT = -2309
294492
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 15262
53457111
00016717 00000-0 10270-3 0 9033
2 25544 51
6437 332
9963 0005657 293
0258 67
0297 15
54067740 2726
Satellite: ISS
Catalog Number: 25544
Epoch time: 15262
53457111 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 332
9963 deg
Eccentricity:
0005657
Arg of perigee: 293
0258 deg
Mean anomaly: 67
0297 deg
Mean motion: 15
54067740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 272
Checksum: 313
Coasting Arc #5 (Orbit 287)
---------------------------------------
Vector Time (GMT): 2015/263/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2713024
52 A = 6777422
05 meter
Y = 3267447
13 meter E =
0003078
Z = 5283817
31 I = 51
43156
XDOT = -6244
951975 Wp = 304
42584
YDOT = 4422
818843 meter/sec RA = 327
52053 deg
ZDOT = 473
414920 TA = 141
05572
MA = 141
03355
Ha = 219
789 n
mi
Hp = 216
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8900999
07 X = 2650618
51
Y = 10719970
91 feet Y = 3297437
49 meter
Z = 17335358
61 Z = 5296844
88
XDOT = -20488
687583 XDOT = -6296
244556
YDOT = 14510
560508 feet/sec YDOT = 4352
696924 meter/sec
ZDOT = 1553
198555 ZDOT = 442
952988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9416753
92 X = -2870226
60
Y = -10175583
50 feet Y = -3101517
85 meter
Z = 17390873
04 Z = 5300738
10
XDOT = 18849
899902 XDOT = 5745
449490
YDOT = -15026
134820 feet/sec YDOT = -4579
965893 meter/sec
ZDOT = 1421
057506 ZDOT = 433
138328
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 15263
56342422
00016717 00000-0 10270-3 0 9046
2 25544 51
6442 327
8674 0005694 297
6019 62
4556 15
54124149 2881
Satellite: ISS
Catalog Number: 25544
Epoch time: 15263
56342422 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 327
8674 deg
Eccentricity:
0005694
Arg of perigee: 297
6019 deg
Mean anomaly: 62
4556 deg
Mean motion: 15
54124149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 288
Checksum: 321
Coasting Arc #6 (Orbit 302)
---------------------------------------
Vector Time (GMT): 2015/264/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1199438
26 A = 6778132
40 meter
Y = -4255369
58 meter E =
0008717
Z = -5145176
70 I = 51
40689
XDOT = 6602
278676 Wp = 86
88457
YDOT = -3608
616195 meter/sec RA = 322
50504 deg
ZDOT = 1448
016148 TA = 197
09298
MA = 197
12236
Ha = 220
064 n
mi
Hp = 216
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3935164
88 X = -1126771
09
Y = -13961186
28 feet Y = -4268376
60 meter
Z = -16880500
99 Z = -5150826
52
XDOT = 21661
019278 XDOT = 6635
106452
YDOT = -11839
291978 feet/sec YDOT = -3534
601498 meter/sec
ZDOT = 4750
709147 ZDOT = 1480
168890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4892151
25 X = 1491127
70
Y = 13626157
16 feet Y = 4153252
70 meter
Z = -16904030
76 Z = -5152348
57
XDOT = -19659
733706 XDOT = -5992
286834
YDOT = 13114
128938 feet/sec YDOT = 3997
186500 meter/sec
ZDOT = 4889
973544 ZDOT = 1490
463936
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 15264
52796250
00016717 00000-0 10270-3 0 9056
2 25544 51
6437 323
0589 0005680 303
2274 56
8333 15
54112281 3032
Satellite: ISS
Catalog Number: 25544
Epoch time: 15264
52796250 = yrday
fracday
Element set: 905
Inclination: 51
6437 deg
RA of node: 323
0589 deg
Eccentricity:
0005680
Arg of perigee: 303
2274 deg
Mean anomaly: 56
8333 deg
Mean motion: 15
54112281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 303
Checksum: 292
Coasting Arc #7 (Orbit 318)
---------------------------------------
Vector Time (GMT): 2015/265/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -297989
90 A = 6780762
50 meter
Y = 5101390
81 meter E =
0007840
Z = 4457431
87 I = 51
39184
XDOT = -6502
551149 Wp = 30
34668
YDOT = 2455
265826 meter/sec RA = 317
49280 deg
ZDOT = -3235
548976 TA = 92
38585
MA = 92
29609
Ha = 220
182 n
mi
Hp = 216
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -977657
17 X = -376665
31
Y = 16736846
48 feet Y = 5097618
96 meter
Z = 14624120
32 Z = 4455792
78
XDOT = -21333
829228 XDOT = -6513
806137
YDOT = 8055
334075 feet/sec YDOT = 2382
486818 meter/sec
ZDOT = -10615
318162 ZDOT = -3267
164683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -510782
33 X = -155686
45
Y = -16764606
54 feet Y = -5109852
07 meter
Z = 14616080
45 Z = 4454981
32
XDOT = 19189
658478 XDOT = 5849
007904
YDOT = -9984
893055 feet/sec YDOT = -3043
395403 meter/sec
ZDOT = -10752
040860 ZDOT = -3277
222054
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 15265
55678664
00016717 00000-0 10270-3 0 9069
2 25544 51
6439 317
9300 0005729 307
4967 52
5664 15
54180774 3195
Satellite: ISS
Catalog Number: 25544
Epoch time: 15265
55678664 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 317
9300 deg
Eccentricity:
0005729
Arg of perigee: 307
4967 deg
Mean anomaly: 52
5664 deg
Mean motion: 15
54180774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 319
Checksum: 338
Coasting Arc #8 (Orbit 333)
---------------------------------------
Vector Time (GMT): 2015/266/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1626484
24 A = 6784499
49 meter
Y = -5691603
04 meter E =
0004195
Z = -3311058
55 I = 51
38180
XDOT = 5990
296877 Wp = 7
95058
YDOT = -1007
028630 meter/sec RA = 312
48793 deg
ZDOT = 4678
437446 TA = 313
38159
MA = 313
41652
Ha = 220
315 n
mi
Hp = 215
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5336234
37 X = 1706092
10
Y = -18673238
31 feet Y = -5672969
81 meter
Z = -10863053
00 Z = -3302963
53
XDOT = 19653
204976 XDOT = 5978
386430
YDOT = -3303
899705 feet/sec YDOT = -940
107345 meter/sec
ZDOT = 15349
204220 ZDOT = 4707
508273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3292913
96 X = -1003680
18
Y = 19159907
39 feet Y = 5839939
77 meter
Z = -10827087
00 Z = -3300096
12
XDOT = -17668
408309 XDOT = -5385
330853
YDOT = 5699
116432 feet/sec YDOT = 1737
090688 meter/sec
ZDOT = 15474
679002 ZDOT = 4716
682160
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 15266
52129807
00016717 00000-0 10270-3 0 9078
2 25544 51
6440 313
1214 0005506 312
6085 47
4602 15
54200102 3341
Satellite: ISS
Catalog Number: 25544
Epoch time: 15266
52129807 = yrday
fracday
Element set: 907
Inclination: 51
6440 deg
RA of node: 313
1214 deg
Eccentricity:
0005506
Arg of perigee: 312
6085 deg
Mean anomaly: 47
4602 deg
Mean motion: 15
54200102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 334
Checksum: 263
Coasting Arc #9 (Orbit 349)
---------------------------------------
Vector Time (GMT): 2015/267/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2752851
71 A = 6787747
02 meter
Y = 5937419
36 meter E =
0009004
Z = 1789009
75 I = 51
37181
XDOT = -5151
971485 Wp = 100
49746
YDOT = -683
621623 meter/sec RA = 307
49194 deg
ZDOT = -5636
198714 TA = 59
77598
MA = 59
68685
Ha = 220
495 n
mi
Hp = 215
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9031665
72 X = -2827731
10
Y = 19479722
30 feet Y = 5906216
68 meter
Z = 5869454
57 Z = 1775454
44
XDOT = -16902
793586 XDOT = -5116
565677
YDOT = -2242
853093 feet/sec YDOT = -741
037019 meter/sec
ZDOT = -18491
465598 ZDOT = -5661
139856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6492494
77 X = 1978912
40
Y = -20483490
30 feet Y = -6243367
84 meter
Z = 5809922
59 Z = 1770864
40
XDOT = 15439
953837 XDOT = 4706
097930
YDOT = -402
729449 feet/sec YDOT = -122
751936 meter/sec
ZDOT = -18598
821905 ZDOT = -5668
920917
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 15267
55009373
00016717 00000-0 10270-3 0 9088
2 25544 51
6438 307
9921 0005647 317
5195 42
5521 15
54215523 3503
Satellite: ISS
Catalog Number: 25544
Epoch time: 15267
55009373 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 307
9921 deg
Eccentricity:
0005647
Arg of perigee: 317
5195 deg
Mean anomaly: 42
5521 deg
Mean motion: 15
54215523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 350
Checksum: 305
Coasting Arc #10 (Orbit 364)
---------------------------------------
Vector Time (GMT): 2015/268/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3582221
36 A = 6789121
02 meter
Y = -5756114
35 meter E =
0013898
Z = -89667
92 I = 51
35751
XDOT = 4107
776802 Wp = 20
76159
YDOT = 2467
713445 meter/sec RA = 302
50124 deg
ZDOT = 5991
665631 TA = 338
26825
MA = 338
32716
Ha = 220
665 n
mi
Hp = 215
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11752694
74 X = 3646756
96
Y = -18884889
60 feet Y = -5715694
76 meter
Z = -294186
09 Z = -72108
72
XDOT = 13476
958013 XDOT = 4050
771717
YDOT = 8096
172719 feet/sec YDOT = 2513
331364 meter/sec
ZDOT = 19657
695641 ZDOT = 6011
481588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8882596
33 X = -2707415
36
Y = 20393715
54 feet Y = 6216004
50 meter
Z = -217447
03 Z = -66277
86
XDOT = -12899
862807 XDOT = -3931
878184
YDOT = -5422
213133 feet/sec YDOT = -1652
690563 meter/sec
ZDOT = 19742
632901 ZDOT = 6017
554508
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 15268
51457695
00016717 00000-0 10270-3 0 9090
2 25544 51
6436 303
1837 0005690 322
2421 37
8332 15
54200291 3657
Satellite: ISS
Catalog Number: 25544
Epoch time: 15268
51457695 = yrday
fracday
Element set: 909
Inclination: 51
6436 deg
RA of node: 303
1837 deg
Eccentricity:
0005690
Arg of perigee: 322
2421 deg
Mean anomaly: 37
8332 deg
Mean motion: 15
54200291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 365
Checksum: 301
Coasting Arc #11 (Orbit 380)
---------------------------------------
Vector Time (GMT): 2015/269/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4148274
50 A = 6787817
31 meter
Y = 5113361
87 meter E =
0002198
Z = -1646622
43 I = 51
33702
XDOT = -2937
463157 Wp = 132
74310
YDOT = -4212
801506 meter/sec RA = 297
50914 deg
ZDOT = -5688
350306 TA = 65
35847
MA = 65
33558
Ha = 220
735 n
mi
Hp = 215
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13609824
48 X = -4197146
36
Y = 16776121
62 feet Y = 5066699
63 meter
Z = -5402304
58 Z = -1666893
43
XDOT = -9637
346314 XDOT = -2862
504370
YDOT = -13821
527252 feet/sec YDOT = -4245
231885 meter/sec
ZDOT = -18662
566620 ZDOT = -5702
437242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10669653
28 X = 3252110
32
Y = -18757993
35 feet Y = -5717436
37 meter
Z = -5490597
25 Z = -1673534
04
XDOT = 10269
187190 XDOT = 3130
048256
YDOT = 11315
417315 feet/sec YDOT = 3448
939198 meter/sec
ZDOT = -18722
497738 ZDOT = -5706
617311
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 15269
54334341
00016717 00000-0 10270-3 0 9108
2 25544 51
6433 298
0539 0005593 325
6955 34
3835 15
54238769 3815
Satellite: ISS
Catalog Number: 25544
Epoch time: 15269
54334341 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 298
0539 deg
Eccentricity:
0005593
Arg of perigee: 325
6955 deg
Mean anomaly: 34
3835 deg
Mean motion: 15
54238769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 381
Checksum: 327
Coasting Arc #12 (Orbit 396)
---------------------------------------
Vector Time (GMT): 2015/270/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4430054
51 A = 6784579
24 meter
Y = -4015918
32 meter E =
0011530
Z = 3190612
05 I = 51
31115
XDOT = 1760
367471 Wp = 60
29675
YDOT = 5741
968351 meter/sec RA = 292
50921 deg
ZDOT = 4775
621116 TA = 336
79753
MA = 336
84954
Ha = 220
796 n
mi
Hp = 215
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14534299
57 X = 4459133
35
Y = -13175585
04 feet Y = -3966215
44 meter
Z = 10467887
30 Z = 3212203
76
XDOT = 5775
483828 XDOT = 1672
830251
YDOT = 18838
478842 feet/sec YDOT = 5761
165246 meter/sec
ZDOT = 15668
048281 ZDOT = 4783
959153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11869037
38 X = -3617682
59
Y = 15556216
73 feet Y = 4741534
86 meter
Z = 10561659
08 Z = 3219193
69
XDOT = -7828
595175 XDOT = -2386
155809
YDOT = -16650
637807 feet/sec YDOT = -5075
114403 meter/sec
ZDOT = 15702
934174 ZDOT = 4786
254336
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 15270
57209510
00016717 00000-0 10270-3 0 9113
2 25544 51
6420 292
9239 0005655 331
3272 28
7569 15
54249506 3975
Satellite: ISS
Catalog Number: 25544
Epoch time: 15270
57209510 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 292
9239 deg
Eccentricity:
0005655
Arg of perigee: 331
3272 deg
Mean anomaly: 28
7569 deg
Mean motion: 15
54249506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 397
Checksum: 312
Coasting Arc #13 (Orbit 411)
---------------------------------------
Vector Time (GMT): 2015/271/12:20:48
186
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4499839
79 A = 6780550
86 meter
Y = 2535155
05 meter E =
0010305
Z = -4403329
07 I = 51
28693
XDOT = -621
712926 Wp = 36
12531
YDOT = -6875
376285 meter/sec RA = 287
49782 deg
ZDOT = -3318
872103 TA = 200
12370
MA = 200
16436
Ha = 220
942 n
mi
Hp = 214
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14763253
92 X = -4506464
13
Y = 8317437
83 feet Y = 2484797
16 meter
Z = -14446617
68 Z = -4425205
12
XDOT = -2039
740571 XDOT = -528
662588
YDOT = -22557
008810 feet/sec YDOT = -6881
808927 meter/sec
ZDOT = -10888
688003 ZDOT = -3321
665219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12752941
49 X = 3887096
57
Y = -11034045
32 feet Y = -3363177
01 meter
Z = -14541338
59 Z = -4432200
00
XDOT = 5555
082492 XDOT = 1693
189144
YDOT = 20802
463744 feet/sec YDOT = 6340
590949 meter/sec
ZDOT = -10899
484048 ZDOT = -3322
162738
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 15271
53653405
00016717 00000-0 10270-3 0 9127
2 25544 51
6422 288
1147 0005665 334
0263 26
0605 15
54288345 4127
Satellite: ISS
Catalog Number: 25544
Epoch time: 15271
53653405 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 288
1147 deg
Eccentricity:
0005665
Arg of perigee: 334
0263 deg
Mean anomaly: 26
0605 deg
Mean motion: 15
54288345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 412
Checksum: 288
Coasting Arc #14 (Orbit 413)
---------------------------------------
Vector Time (GMT): 2015/271/15:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 892142
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3866515
47 A = 6785244
11 meter
Y = 4772347
29 meter E =
0003776
Z = -2889424
10 I = 51
29994
XDOT = -2629
033722 Wp = 25
47592
YDOT = -5164
757884 meter/sec RA = 286
87314 deg
ZDOT = -5011
457997 TA = 187
57903
MA = 187
58474
Ha = 221
011 n
mi
Hp = 214
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12685418
19 X = -3905557
75
Y = 15657307
37 feet Y = 4728890
62 meter
Z = -9479737
85 Z = -2908302
64
XDOT = -8625
438722 XDOT = -2546
740699
YDOT = -16944
743713 feet/sec YDOT = -5193
698112 meter/sec
ZDOT = -16441
791330 ZDOT = -5024
028792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6001271
34 X = -1829187
50
Y = -19196106
21 feet Y = -5850973
17 meter
Z = -9561944
75 Z = -2914480
76
XDOT = 17423
733849 XDOT = 5310
754077
YDOT = 2770
764389 feet/sec YDOT = 844
528986 meter/sec
ZDOT = -16495
028404 ZDOT = -5027
684658
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 15271
66512566
00016717 00000-0 10270-3 0 9134
2 25544 51
6407 287
4725 0005897 334
7044 25
3820 15
54295200 4146
Satellite: ISS
Catalog Number: 25544
Epoch time: 15271
66512566 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 287
4725 deg
Eccentricity:
0005897
Arg of perigee: 334
7044 deg
Mean anomaly: 25
3820 deg
Mean motion: 15
54295200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 414
Checksum: 304
Coasting Arc #15 (Orbit 429)
---------------------------------------
Vector Time (GMT): 2015/272/15:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 892142
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4133322
94 A = 6781171
79 meter
Y = -3368388
66 meter E =
0007884
Z = 4181502
98 I = 51
27877
XDOT = 1625
239401 Wp = 70
32458
YDOT = 6543
661290 meter/sec RA = 281
86350 deg
ZDOT = 3661
665076 TA = 341
94965
MA = 341
97763
Ha = 220
837 n
mi
Hp = 214
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13560770
81 X = 4150369
41
Y = -11051143
89 feet Y = -3322071
23 meter
Z = 13718841
81 Z = 4201624
02
XDOT = 5332
150265 XDOT = 1534
158542
YDOT = 21468
705020 feet/sec YDOT = 6561
327027 meter/sec
ZDOT = 12013
336862 ZDOT = 3669
338159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1998110
31 X = 609024
02
Y = 17309732
54 feet Y = 5276006
48 meter
Z = 13806144
34 Z = 4208112
79
XDOT = -19634
841220 XDOT = -5984
699604
YDOT = -7348
593995 feet/sec YDOT = -2239
851450 meter/sec
ZDOT = 12045
228454 ZDOT = 3671
385633
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 15272
69384254
00016717 00000-0 10270-3 0 9140
2 25544 51
6409 282
3428 0005851 336
4984 23
5901 15
54346903 4309
Satellite: ISS
Catalog Number: 25544
Epoch time: 15272
69384254 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 282
3428 deg
Eccentricity:
0005851
Arg of perigee: 336
4984 deg
Mean anomaly: 23
5901 deg
Mean motion: 15
54346903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 430
Checksum: 313
Coasting Arc #16 (Orbit 444)
---------------------------------------
Vector Time (GMT): 2015/273/15:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 892142
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4255875
35 A = 6777946
65 meter
Y = 1650622
35 meter E =
0013888
Z = -5022221
27 I = 51
26251
XDOT = -636
606432 Wp = 50
55965
YDOT = -7395
530758 meter/sec RA = 276
84118 deg
ZDOT = -1886
017727 TA = 201
00836
MA = 201
06547
Ha = 221
159 n
mi
Hp = 214
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13962845
62 X = -4249620
24
Y = 5415427
67 feet Y = 1603064
74 meter
Z = -16477103
92 Z = -5042880
81
XDOT = -2088
603778 XDOT = -544
698781
YDOT = -24263
552355 feet/sec YDOT = -7402
136043 meter/sec
ZDOT = -6187
722201 ZDOT = -1888
886192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2697592
33 X = 822226
14
Y = -14630777
61 feet Y = -4459461
01 meter
Z = -16566418
15 Z = -5049444
25
XDOT = 20637
269697 XDOT = 6290
239804
YDOT = 10842
978659 feet/sec YDOT = 3304
939895 meter/sec
ZDOT = -6198
766014 ZDOT = -1889
383881
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 15273
65825192
00016717 00000-0 10270-3 0 9159
2 25544 51
6412 277
5325 0005944 341
5678 18
5259 15
54333563 4459
Satellite: ISS
Catalog Number: 25544
Epoch time: 15273
65825192 = yrday
fracday
Element set: 915
Inclination: 51
6412 deg
RA of node: 277
5325 deg
Eccentricity:
0005944
Arg of perigee: 341
5678 deg
Mean anomaly: 18
5259 deg
Mean motion: 15
54333563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 445
Checksum: 322
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