[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 17th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 ET - UTC (sec) : 68 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
017/20:15:07
803 0
7 0
8 0
8
N/A 0
4 -0
1 221
6
000/00:00:15
606 -0
2 -0
0 214
1
018/18:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
1
023/19:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 213
7
029/16:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
4
Coasting Arc #1 (Orbit 1476)
---------------------------------------
Vector Time (GMT): 2018/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3221176
16 A = 6776902
37 meter
Y = 2709845
36 meter E =
0004408
Z = 5307650
59 I = 51
94725
XDOT = -4317
727617 Wp = 57
07822
YDOT = -6313
095794 meter/sec RA = 59
17900 deg
ZDOT = 604
752764 TA = 27
18838
MA = 27
16531
Ha = 221
580 n
mi
Hp = 213
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10568163
27 X = -3277020
40
Y = 8890568
75 feet Y = 2673511
30 meter
Z = 17413551
82 Z = 5291868
02
XDOT = -14165
773023 XDOT = -4249
749509
YDOT = -20712
256543 feet/sec YDOT = -6360
999538 meter/sec
ZDOT = 1984
096994 ZDOT = 583
943638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12470368
95 X = -3800968
45
Y = -6138186
27 feet Y = -1870919
18 meter
Z = 17342797
99 Z = 5286084
83
XDOT = 12699
714597 XDOT = 3870
873009
YDOT = -20472
178555 feet/sec YDOT = -6239
920024 meter/sec
ZDOT = 1892
469620 ZDOT = 576
824740
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 18015
54922922
00016717 00000-0 10270-3 0 9007
2 25544 51
6405 59
6508 0003688 17
3608 342
7670 15
54317764 14777
Satellite: ISS
Catalog Number: 25544
Epoch time: 18015
54922922 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 59
6508 deg
Eccentricity:
0003688
Arg of perigee: 17
3608 deg
Mean anomaly: 342
7670 deg
Mean motion: 15
54317764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1477
Checksum: 318
Coasting Arc #2 (Orbit 1491)
---------------------------------------
Vector Time (GMT): 2018/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4220909
98 A = 6777541
18 meter
Y = -1107721
15 meter E =
0014873
Z = -5198324
03 I = 51
93189
XDOT = 3469
821414 Wp = 86
23077
YDOT = 6682
165967 meter/sec RA = 54
19779 deg
ZDOT = 1397
884255 TA = 197
15071
MA = 197
20102
Ha = 221
557 n
mi
Hp = 213
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13848129
84 X = 4258233
40
Y = -3634255
73 feet Y = -1060310
99 meter
Z = -17054868
87 Z = -5177730
08
XDOT = 11383
928524 XDOT = 3388
051680
YDOT = 21923
116691 feet/sec YDOT = 6720
510586 meter/sec
ZDOT = 4586
234433 ZDOT = 1414
541033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9195831
35 X = 2802889
40
Y = 11114947
20 feet Y = 3387835
91 meter
Z = -16962950
84 Z = -5170307
42
XDOT = -14259
081653 XDOT = -4346
168088
YDOT = 18885
723399 feet/sec YDOT = 5756
368492 meter/sec
ZDOT = 4659
297075 ZDOT = 1420
153749
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 18016
51364683
00016717 00000-0 10270-3 0 9010
2 25544 51
6410 54
8419 0003718 19
8304 340
2992 15
54293629 14925
Satellite: ISS
Catalog Number: 25544
Epoch time: 18016
51364683 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 54
8419 deg
Eccentricity:
0003718
Arg of perigee: 19
8304 deg
Mean anomaly: 340
2992 deg
Mean motion: 15
54293629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1492
Checksum: 309
Coasting Arc #3 (Orbit 1507)
---------------------------------------
Vector Time (GMT): 2018/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5057450
97 A = 6780292
14 meter
Y = -482993
92 meter E =
0012203
Z = 4485181
38 I = 51
92102
XDOT = -2279
428289 Wp = 56
03962
YDOT = -6557
383378 meter/sec RA = 49
22042 deg
ZDOT = -3263
417061 TA = 66
73875
MA = 66
61032
Ha = 221
688 n
mi
Hp = 213
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16592686
91 X = -5073460
35
Y = -1584625
71 feet Y = -539639
57 meter
Z = 14715162
00 Z = 4460575
59
XDOT = -7478
439267 XDOT = -2190
080793
YDOT = -21513
724992 feet/sec YDOT = -6582
373744 meter/sec
ZDOT = -10706
748888 ZDOT = -3274
272898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5890349
67 X = -1795378
58
Y = -15695325
42 feet Y = -4783935
19 meter
Z = 14605643
80 Z = 4451800
23
XDOT = 14948
030204 XDOT = 4556
159606
YDOT = -15657
215823 feet/sec YDOT = -4772
319383 meter/sec
ZDOT = -10753
987723 ZDOT = -3277
815458
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 18017
54235380
00016717 00000-0 10270-3 0 9026
2 25544 51
6405 49
7124 0003846 24
7294 335
4043 15
54343027 15089
Satellite: ISS
Catalog Number: 25544
Epoch time: 18017
54235380 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 49
7124 deg
Eccentricity:
0003846
Arg of perigee: 24
7294 deg
Mean anomaly: 335
4043 deg
Mean motion: 15
54343027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1508
Checksum: 289
Coasting Arc #4 (Orbit 1512)
---------------------------------------
Vector Time (GMT): 2018/017/20:15:15
606
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1187710
84 A = 6778725
66 meter
Y = -4471396
53 meter E =
0014639
Z = -4967977
90 I = 51
90870
XDOT = 6087
586055 Wp = 61
77886
YDOT = 4081
605427 meter/sec RA = 47
55347 deg
ZDOT = -2216
472011 TA = 186
63162
MA = 186
65101
Ha = 221
591 n
mi
Hp = 214
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3896689
12 X = 1261754
27
Y = -14669936
12 feet Y = -4457700
47 meter
Z = -16299140
10 Z = -4962028
93
XDOT = 19972
395193 XDOT = 6052
258245
YDOT = 13391
093920 feet/sec YDOT = 4149
483571 meter/sec
ZDOT = -7271
889799 ZDOT = -2186
986795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10730930
28 X = -3270787
55
Y = -10776188
37 feet Y = -3284582
21 meter
Z = -16271880
02 Z = -4959669
03
XDOT = 20793
725223 XDOT = 6337
927448
YDOT = -9914
424748 feet/sec YDOT = -3021
916663 meter/sec
ZDOT = -7141
251045 ZDOT = -2176
653319
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 18017
86382611
00016717 00000-0 10270-3 0 9032
2 25544 51
6421 48
1103 0003580 16
4212 343
7056 15
54198369 15139
Satellite: ISS
Catalog Number: 25544
Epoch time: 18017
86382611 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 48
1103 deg
Eccentricity:
0003580
Arg of perigee: 16
4212 deg
Mean anomaly: 343
7056 deg
Mean motion: 15
54198369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1513
Checksum: 285
Coasting Arc #5 (Orbit 1527)
---------------------------------------
Vector Time (GMT): 2018/018/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5116157
39 A = 6780942
88 meter
Y = 11506
13 meter E =
0011974
Z = 4445561
48 I = 51
89226
XDOT = -2917
524052 Wp = 56
44305
YDOT = -6264
702556 meter/sec RA = 42
83312 deg
ZDOT = -3328
514345 TA = 67
08880
MA = 66
96246
Ha = 221
816 n
mi
Hp = 214
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16785293
27 X = -5137499
56
Y = 37749
76 feet Y = -45825
75 meter
Z = 14585175
45 Z = 4420657
64
XDOT = -9571
929306 XDOT = -2831
085793
YDOT = -20553
486076 feet/sec YDOT = -6296
844877 meter/sec
ZDOT = -10920
322653 ZDOT = -3342
476669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12857435
96 X = -3918946
48
Y = 10938799
34 feet Y = 3334146
04 meter
Z = 14474247
74 Z = 4411750
71
XDOT = -19734
901318 XDOT = -6015
197922
YDOT = -8609
280110 feet/sec YDOT = -2624
108577 meter/sec
ZDOT = -10981
442042 ZDOT = -3347
143535
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 18018
82832687
00016717 00000-0 10270-3 0 9043
2 25544 51
6402 43
3019 0003592 20
3748 339
7547 15
54171843 15286
Satellite: ISS
Catalog Number: 25544
Epoch time: 18018
82832687 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 43
3019 deg
Eccentricity:
0003592
Arg of perigee: 20
3748 deg
Mean anomaly: 339
7547 deg
Mean motion: 15
54171843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1528
Checksum: 313
Coasting Arc #6 (Orbit 1542)
---------------------------------------
Vector Time (GMT): 2018/019/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5805203
18 A = 6784688
10 meter
Y = 1251634
59 meter E =
0007098
Z = -3281701
74 I = 51
88082
XDOT = 1425
058409 Wp = 56
09417
YDOT = 5837
086174 meter/sec RA = 37
86308 deg
ZDOT = 4758
346610 TA = 265
96956
MA = 266
05070
Ha = 221
761 n
mi
Hp = 214
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19045942
20 X = 5806716
06
Y = 4106412
69 feet Y = 1316560
87 meter
Z = -10766737
99 Z = -3253498
96
XDOT = 4675
388480 XDOT = 1336
567565
YDOT = 19150
545190 feet/sec YDOT = 5852
527272 meter/sec
ZDOT = 15611
373392 ZDOT = 4765
054103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17080534
39 X = 5206146
88
Y = -9515801
56 feet Y = -2900416
32 meter
Z = -10641336
94 Z = -3243479
50
XDOT = 15370
261008 XDOT = 4684
855555
YDOT = 10140
550589 feet/sec YDOT = 3090
839819 meter/sec
ZDOT = 15640
248199 ZDOT = 4767
147651
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 18019
79282473
00016717 00000-0 10270-3 0 9053
2 25544 51
6408 38
4930 0003543 22
5574 337
5734 15
54189589 15433
Satellite: ISS
Catalog Number: 25544
Epoch time: 18019
79282473 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 38
4930 deg
Eccentricity:
0003543
Arg of perigee: 22
5574 deg
Mean anomaly: 337
5734 deg
Mean motion: 15
54189589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1543
Checksum: 330
Coasting Arc #7 (Orbit 1558)
---------------------------------------
Vector Time (GMT): 2018/020/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6125218
79 A = 6787983
88 meter
Y = -2343567
83 meter E =
0014434
Z = 1731825
24 I = 51
86585
XDOT = 334
442053 Wp = 101
19164
YDOT = -5115
978739 meter/sec RA = 32
90211 deg
ZDOT = -5702
785058 TA = 59
86727
MA = 59
72430
Ha = 221
797 n
mi
Hp = 213
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20095862
19 X = -6106969
28
Y = -7688870
85 feet Y = -2411962
20 meter
Z = 5681841
35 Z = 1702115
95
XDOT = 1097
250831 XDOT = 419
326034
YDOT = -16784
707148 feet/sec YDOT = -5111
764133 meter/sec
ZDOT = -18709
924732 ZDOT = -5700
954349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20074974
78 X = -6118852
31
Y = 7838332
57 feet Y = 2389123
77 meter
Z = 5549924
61 Z = 1691617
02
XDOT = -9806
710875 XDOT = -2989
085475
YDOT = -11785
990054 feet/sec YDOT = -3592
369768 meter/sec
ZDOT = -18700
892539 ZDOT = -5700
032046
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 18020
82161970
00016717 00000-0 10270-3 0 9068
2 25544 51
6415 33
3640 0003537 26
7645 333
3689 15
54174788 15596
Satellite: ISS
Catalog Number: 25544
Epoch time: 18020
82161970 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 33
3640 deg
Eccentricity:
0003537
Arg of perigee: 26
7645 deg
Mean anomaly: 333
3689 deg
Mean motion: 15
54174788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1559
Checksum: 318
Coasting Arc #8 (Orbit 1574)
---------------------------------------
Vector Time (GMT): 2018/021/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6004346
74 A = 6789162
94 meter
Y = 3151365
23 meter E =
0015684
Z = -38055
85 I = 51
84222
XDOT = -2179
744423 Wp = 41
28151
YDOT = 4208
744431 meter/sec RA = 27
94526 deg
ZDOT = 6031
940422 TA = 318
30956
MA = 318
42899
Ha = 221
858 n
mi
Hp = 213
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19699300
32 X = 5968845
92
Y = 10339124
78 feet Y = 3218311
46 meter
Z = -124855
15 Z = -8975
56
XDOT = -7151
392463 XDOT = -2255
945220
YDOT = 13808
216637 feet/sec YDOT = 4183
943009 meter/sec
ZDOT = 19789
830782 ZDOT = 6021
167059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21436525
63 X = 6533853
01
Y = -5954063
75 feet Y = -1814798
63 meter
Z = 4112
42 Z = 1253
47
XDOT = 3715
145559 XDOT = 1132
376366
YDOT = 13487
328233 feet/sec YDOT = 4110
937646 meter/sec
ZDOT = 19741
127180 ZDOT = 6017
095564
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 18021
85041131
00016717 00000-0 10270-3 0 9079
2 25544 51
6418 28
2348 0003689 29
1006 331
0352 15
54187078 15759
Satellite: ISS
Catalog Number: 25544
Epoch time: 18021
85041131 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 28
2348 deg
Eccentricity:
0003689
Arg of perigee: 29
1006 deg
Mean anomaly: 331
0352 deg
Mean motion: 15
54187078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1575
Checksum: 292
Coasting Arc #9 (Orbit 1589)
---------------------------------------
Vector Time (GMT): 2018/022/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5399372
21 A = 6787927
93 meter
Y = -3744483
61 meter E =
0007201
Z = -1701433
72 I = 51
80888
XDOT = 3999
608773 Wp = 114
36234
YDOT = -3182
660449 meter/sec RA = 22
98791 deg
ZDOT = -5710
021603 TA = 84
23667
MA = 84
15457
Ha = 221
821 n
mi
Hp = 213
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17714475
75 X = -5348834
54
Y = -12285051
21 feet Y = -3804580
54 meter
Z = -5582131
62 Z = -1727538
84
XDOT = 13122
076027 XDOT = 4062
636769
YDOT = -10441
799372 feet/sec YDOT = -3137
581741 meter/sec
ZDOT = -18733
666677 ZDOT = -5690
440043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21238049
58 X = -6473357
51
Y = 3516584
23 feet Y = 1071854
87 meter
Z = -5697737
56 Z = -1736670
41
XDOT = 2471
197828 XDOT = 753
221098
YDOT = -15172
389019 feet/sec YDOT = -4624
544173 meter/sec
ZDOT = -18645
916970 ZDOT = -5683
275492
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 18022
81490208
00016717 00000-0 10270-3 0 9080
2 25544 51
6421 23
4273 0003461 32
6404 327
4962 15
54168932 15907
Satellite: ISS
Catalog Number: 25544
Epoch time: 18022
81490208 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 23
4273 deg
Eccentricity:
0003461
Arg of perigee: 32
6404 deg
Mean anomaly: 327
4962 deg
Mean motion: 15
54168932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1590
Checksum: 291
Coasting Arc #10 (Orbit 1605)
---------------------------------------
Vector Time (GMT): 2018/023/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4346104
44 A = 6784674
71 meter
Y = 4081889
04 meter E =
0015273
Z = 3220455
01 I = 51
76817
XDOT = -5589
486747 Wp = 75
73995
YDOT = 2155
141294 meter/sec RA = 18
02061 deg
ZDOT = 4796
232398 TA = 321
48879
MA = 321
59767
Ha = 221
851 n
mi
Hp = 213
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14258872
83 X = 4284493
54
Y = 13392024
41 feet Y = 4130145
71 meter
Z = 10565797
28 Z = 3241416
96
XDOT = -18338
211111 XDOT = -5636
468013
YDOT = 7070
673537 feet/sec YDOT = 2092
373186 meter/sec
ZDOT = 15735
670597 ZDOT = 4768
966774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19501371
19 X = 5944017
94
Y = -626242
87 feet Y = -190878
83 meter
Z = 10658432
62 Z = 3248690
26
XDOT = -8026
492413 XDOT = -2446
474888
YDOT = 16644
721549 feet/sec YDOT = 5073
311128 meter/sec
ZDOT = 15613
887144 ZDOT = 4759
112802
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 18023
84368914
00016717 00000-0 10270-3 0 9093
2 25544 51
6427 18
2979 0003695 35
1135 325
0260 15
54189193 16061
Satellite: ISS
Catalog Number: 25544
Epoch time: 18023
84368914 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 18
2979 deg
Eccentricity:
0003695
Arg of perigee: 35
1135 deg
Mean anomaly: 325
0260 deg
Mean motion: 15
54189193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1606
Checksum: 318
Coasting Arc #11 (Orbit 1605)
---------------------------------------
Vector Time (GMT): 2018/023/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1742865
00 A = 6779424
77 meter
Y = -4508641
92 meter E =
0014263
Z = -4767212
96 I = 51
74937
XDOT = 7167
595106 Wp = 61
86395
YDOT = 76
334519 meter/sec RA = 17
83341 deg
ZDOT = -2692
207318 TA = 181
53587
MA = 181
54025
Ha = 221
821 n
mi
Hp = 213
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5718061
02 X = -1669162
26
Y = -14792132
29 feet Y = -4527719
79 meter
Z = -15640462
45 Z = -4775500
04
XDOT = 23515
731975 XDOT = 7179
285988
YDOT = 250
441336 feet/sec YDOT = 156
552819 meter/sec
ZDOT = -8832
701175 ZDOT = -2657
361609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15545810
70 X = -4738363
10
Y = -2949567
06 feet Y = -899028
04 meter
Z = -15676584
10 Z = -4778222
83
XDOT = 12324
525073 XDOT = 3756
515242
YDOT = -18829
528927 feet/sec YDOT = -5739
240417 meter/sec
ZDOT = -8677
550797 ZDOT = -2644
917483
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 18023
84368770
00016717 00000-0 10270-3 0 9105
2 25544 51
6424 18
2983 0003630 33
0826 327
0553 15
54214783 16067
Satellite: ISS
Catalog Number: 25544
Epoch time: 18023
84368770 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 18
2983 deg
Eccentricity:
0003630
Arg of perigee: 33
0826 deg
Mean anomaly: 327
0553 deg
Mean motion: 15
54214783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1606
Checksum: 296
Coasting Arc #12 (Orbit 1621)
---------------------------------------
Vector Time (GMT): 2018/024/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -32302
53 A = 6777310
33 meter
Y = 4258145
10 meter E =
0005240
Z = 5267963
34 I = 51
71044
XDOT = -7555
277024 Wp = 74
20832
YDOT = -1063
257278 meter/sec RA = 12
84116 deg
ZDOT = 813
834754 TA = 8
02954
MA = 8
02116
Ha = 221
937 n
mi
Hp = 213
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -105979
44 X = -105504
63
Y = 13970292
31 feet Y = 4257374
58 meter
Z = 17283344
28 Z = 5267628
62
XDOT = -24787
654279 XDOT = -7546
779020
YDOT = -3488
376895 feet/sec YDOT = -1147
698047 meter/sec
ZDOT = 2670
061528 ZDOT = 777
154790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11921509
85 X = 3633676
20
Y = 7289372
54 feet Y = 2221800
75 meter
Z = 17281115
10 Z = 5267283
88
XDOT = -15077
647470 XDOT = -4595
666949
YDOT = 18721
333363 feet/sec YDOT = 5706
262409 meter/sec
ZDOT = 2506
926125 ZDOT = 764
111083
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 18024
87247133
00016717 00000-0 10270-3 0 9119
2 25544 51
6422 13
1689 0003669 38
4133 321
7280 15
54205752 16226
Satellite: ISS
Catalog Number: 25544
Epoch time: 18024
87247133 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 13
1689 deg
Eccentricity:
0003669
Arg of perigee: 38
4133 deg
Mean anomaly: 321
7280 deg
Mean motion: 15
54205752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1622
Checksum: 289
Coasting Arc #13 (Orbit 1636)
---------------------------------------
Vector Time (GMT): 2018/025/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1849950
72 A = 6777556
63 meter
Y = -3915816
48 meter E =
0016350
Z = -5227390
99 I = 51
67767
XDOT = 7320
349077 Wp = 87
71615
YDOT = 1926
833972 meter/sec RA = 7
84410 deg
ZDOT = 1151
004654 TA = 193
30915
MA = 193
35233
Ha = 221
915 n
mi
Hp = 213
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6069392
13 X = 1918992
66
Y = -12847166
92 feet Y = -3894742
96 meter
Z = -17150232
92 Z = -5218237
00
XDOT = 24016
893297 XDOT = 7292
667707
YDOT = 6321
633768 feet/sec YDOT = 2008
540342 meter/sec
ZDOT = 3776
261987 ZDOT = 1186
496896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8127015
42 X = -2477114
30
Y = -11715735
86 feet Y = -3570956
29 meter
Z = -17108794
86 Z = -5214760
67
XDOT = 16479
459526 XDOT = 5022
939263
YDOT = -17158
378133 feet/sec YDOT = -5229
873655 meter/sec
ZDOT = 3933
948503 ZDOT = 1199
067504
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 18025
83695317
00016717 00000-0 10270-3 0 9128
2 25544 51
6408 8
3603 0003660 40
8612 319
2814 15
54223198 16377
Satellite: ISS
Catalog Number: 25544
Epoch time: 18025
83695317 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 8
3603 deg
Eccentricity:
0003660
Arg of perigee: 40
8612 deg
Mean anomaly: 319
2814 deg
Mean motion: 15
54223198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1637
Checksum: 299
Coasting Arc #14 (Orbit 1652)
---------------------------------------
Vector Time (GMT): 2018/026/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3569998
14 A = 6780067
96 meter
Y = 3465727
67 meter E =
0011935
Z = 4600105
27 I = 51
65436
XDOT = -6518
143490 Wp = 58
40371
YDOT = -2706
488410 meter/sec RA = 2
84918 deg
ZDOT = -3007
591124 TA = 61
64712
MA = 61
52681
Ha = 221
940 n
mi
Hp = 213
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11712592
33 X = -3630832
21
Y = 11370497
60 feet Y = 3425465
22 meter
Z = 15092208
90 Z = 4582615
96
XDOT = -21384
985203 XDOT = -6472
785199
YDOT = -8879
555150 feet/sec YDOT = -2779
125051 meter/sec
ZDOT = -9867
424948 ZDOT = -3039
143655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4338058
17 X = 1322240
13
Y = 15811915
58 feet Y = 4819471
87 meter
Z = 15013739
75 Z = 4576187
87
XDOT = -16841
869215 XDOT = -5133
401737
YDOT = 14160
038306 feet/sec YDOT = 4315
979676 meter/sec
ZDOT = -10007
427194 ZDOT = -3050
263809
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 18026
86572979
00016717 00000-0 10270-3 0 9131
2 25544 51
6415 3
2314 0003603 41
3240 318
8185 15
54255194 16533
Satellite: ISS
Catalog Number: 25544
Epoch time: 18026
86572979 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 3
2314 deg
Eccentricity:
0003603
Arg of perigee: 41
3240 deg
Mean anomaly: 318
8185 deg
Mean motion: 15
54255194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1653
Checksum: 298
Coasting Arc #15 (Orbit 1667)
---------------------------------------
Vector Time (GMT): 2018/027/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4994528
87 A = 6783923
58 meter
Y = -2966043
49 meter E =
0007943
Z = -3508419
73 I = 51
63314
XDOT = 5178
712125 Wp = 73
11579
YDOT = 3386
960325 meter/sec RA = 357
85960 deg
ZDOT = 4519
696211 TA = 245
63073
MA = 245
71366
Ha = 221
990 n
mi
Hp = 213
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16386249
58 X = 5044366
63
Y = -9731113
82 feet Y = -2909912
43 meter
Z = -11510563
42 Z = -3484037
41
XDOT = 16990
525346 XDOT = 5118
499282
YDOT = 11112
074558 feet/sec YDOT = 3444
535353 meter/sec
ZDOT = 14828
399643 ZDOT = 4544
706225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1002878
90 X = -305677
49
Y = -19097040
26 feet Y = -5820777
87 meter
Z = -11401495
92 Z = -3475175
96
XDOT = 16279
713287 XDOT = 4962
056610
YDOT = -9752
827728 feet/sec YDOT = -2972
661891 meter/sec
ZDOT = 14939
151138 ZDOT = 4553
453267
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 18027
83020600
00016717 00000-0 10270-3 0 9149
2 25544 51
6405 358
4215 0003603 46
5320 313
6132 15
54226306 16687
Satellite: ISS
Catalog Number: 25544
Epoch time: 18027
83020600 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 358
4215 deg
Eccentricity:
0003603
Arg of perigee: 46
5320 deg
Mean anomaly: 313
6132 deg
Mean motion: 15
54226306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1668
Checksum: 270
Coasting Arc #16 (Orbit 1683)
---------------------------------------
Vector Time (GMT): 2018/028/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6039099
61 A = 6787326
19 meter
Y = 2350265
81 meter E =
0015980
Z = 1998871
36 I = 51
61158
XDOT = -3418
219021 Wp = 99
76414
YDOT = -4018
187384 meter/sec RA = 352
88018 deg
ZDOT = -5567
449827 TA = 58
14707
MA = 57
99163
Ha = 221
993 n
mi
Hp = 213
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19813318
92 X = -6074641
38
Y = 7710845
85 feet Y = 2282533
63 meter
Z = 6557976
91 Z = 1969449
79
XDOT = -11214
629333 XDOT = -3345
989222
YDOT = -13183
029475 feet/sec YDOT = -4056
008088 meter/sec
ZDOT = -18265
911506 ZDOT = -5583
878869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1995408
25 X = -608200
44
Y = 21207290
17 feet Y = 6463982
04 meter
Z = 6426585
49 Z = 1958823
26
XDOT = -15209
952388 XDOT = -4635
993488
YDOT = 4161
880397 feet/sec YDOT = 1268
541145 meter/sec
ZDOT = -18338
350311 ZDOT = -5589
529175
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 18028
85897607
00016717 00000-0 10270-3 0 9152
2 25544 51
6401 353
2925 0003727 49
1963 310
9512 15
54259019 16840
Satellite: ISS
Catalog Number: 25544
Epoch time: 18028
85897607 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 353
2925 deg
Eccentricity:
0003727
Arg of perigee: 49
1963 deg
Mean anomaly: 310
9512 deg
Mean motion: 15
54259019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1684
Checksum: 326
Coasting Arc #17 (Orbit 1697)
---------------------------------------
Vector Time (GMT): 2018/029/16:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 905759
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3132087
35 A = 6778496
98 meter
Y = 3383117
26 meter E =
0008256
Z = 4962476
72 I = 51
55541
XDOT = -6699
377950 Wp = 98
21959
YDOT = 3082
327285 meter/sec RA = 348
50324 deg
ZDOT = 2122
815301 TA = 331
07452
MA = 331
12025
Ha = 221
984 n
mi
Hp = 213
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10275877
12 X = 3069919
05
Y = 11099466
09 feet Y = 3417794
55 meter
Z = 16281091
61 Z = 4977540
18
XDOT = -21979
586449 XDOT = -6743
658757
YDOT = 10112
622325 feet/sec YDOT = 3007
162552 meter/sec
ZDOT = 6964
617128 ZDOT = 2090
165342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13658704
46 X = 4163173
12
Y = 6329510
14 feet Y = 1929234
69 meter
Z = 16347563
61 Z = 4982737
39
XDOT = -15971
063899 XDOT = -4867
980276
YDOT = 16818
233088 feet/sec YDOT = 5126
197445 meter/sec
ZDOT = 6818
729449 ZDOT = 2078
348736
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 18029
75915023
00016717 00000-0 10270-3 0 9166
2 25544 51
6422 348
8058 0003708 55
8539 304
2965 15
54223831 16988
Satellite: ISS
Catalog Number: 25544
Epoch time: 18029
75915023 = yrday
fracday
Element set: 916
Inclination: 51
6422 deg
RA of node: 348
8058 deg
Eccentricity:
0003708
Arg of perigee: 55
8539 deg
Mean anomaly: 304
2965 deg
Mean motion: 15
54223831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1698
Checksum: 328
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