[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 24th 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
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
3
030/15:25:11
379 1
1 1
1 1
1
N/A -0
5 -0
1 222
1
000/00:00:22
759 0
0 -0
0 213
8
037/00:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
7
Coasting Arc #1 (Orbit 1617)
---------------------------------------
Vector Time (GMT): 2018/024/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6565458
18 A = 6789085
58 meter
Y = -1711955
86 meter E =
0011964
Z = -88415
50 I = 51
75537
XDOT = 1265
410344 Wp = 116
59954
YDOT = -4574
761576 meter/sec RA = 14
02608 deg
ZDOT = -6020
236428 TA = 64
35108
MA = 64
22754
Ha = 221
947 n
mi
Hp = 213
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21540217
12 X = -6545397
20
Y = -5616653
09 feet Y = -1785263
15 meter
Z = -290077
09 Z = -120259
20
XDOT = 4151
608741 XDOT = 1345
715390
YDOT = -15009
060290 feet/sec YDOT = -4560
161906 meter/sec
ZDOT = -19751
431852 ZDOT = -6013
894492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16633184
43 X = -5069794
61
Y = -14790632
65 feet Y = -4508184
83 meter
Z = -431568
66 Z = -131542
13
XDOT = 9556
776773 XDOT = 2912
905560
YDOT = -10212
655085 feet/sec YDOT = -3112
817270 meter/sec
ZDOT = -19722
400256 ZDOT = -6011
387598
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
61527742
00016717 00000-0 10270-3 0 9006
2 25544 51
6402 14
4489 0003832 38
1215 322
0208 15
54208859 16186
Satellite: ISS
Catalog Number: 25544
Epoch time: 18024
61527742 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 14
4489 deg
Eccentricity:
0003832
Arg of perigee: 38
1215 deg
Mean anomaly: 322
0208 deg
Mean motion: 15
54208859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1618
Checksum: 286
Coasting Arc #2 (Orbit 1633)
---------------------------------------
Vector Time (GMT): 2018/025/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6085991
86 A = 6787656
70 meter
Y = 2394915
44 meter E =
0017496
Z = 1782018
58 I = 51
71800
XDOT = -3251
122389 Wp = 60
53115
YDOT = 4015
580624 meter/sec RA = 9
06214 deg
ZDOT = 5673
198264 TA = 319
03523
MA = 319
16654
Ha = 221
942 n
mi
Hp = 213
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19967164
91 X = 6050102
91
Y = 7857334
13 feet Y = 2462772
49 meter
Z = 5846517
66 Z = 1811494
85
XDOT = -10666
412038 XDOT = -3323
341263
YDOT = 13174
477113 feet/sec YDOT = 3978
820494 meter/sec
ZDOT = 18612
855198 ZDOT = 5657
230189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14454987
38 X = 4405880
15
Y = 15809234
35 feet Y = 4818654
63 meter
Z = 5977339
86 Z = 1821893
19
XDOT = -14325
380520 XDOT = -4366
375982
YDOT = 6047
454113 feet/sec YDOT = 1843
264014 meter/sec
ZDOT = 18541
060910 ZDOT = 5651
315365
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
64405705
00016717 00000-0 10270-3 0 9015
2 25544 51
6395 9
3206 0003787 42
7806 317
3641 15
54221535 16345
Satellite: ISS
Catalog Number: 25544
Epoch time: 18025
64405705 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 9
3206 deg
Eccentricity:
0003787
Arg of perigee: 42
7806 deg
Mean anomaly: 317
3641 deg
Mean motion: 15
54221535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1634
Checksum: 294
Coasting Arc #3 (Orbit 1648)
---------------------------------------
Vector Time (GMT): 2018/026/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5102947
69 A = 6784270
51 meter
Y = -2999281
70 meter E =
0007862
Z = -3324428
60 I = 51
67491
XDOT = 5031
428855 Wp = 70
79237
YDOT = -3362
168825 meter/sec RA = 4
08832 deg
ZDOT = -4696
388407 TA = 147
83171
MA = 147
78372
Ha = 221
996 n
mi
Hp = 213
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16741954
38 X = -5052881
47
Y = -9840163
05 feet Y = -3056066
33 meter
Z = -10906917
97 Z = -3349095
23
XDOT = 16507
312517 XDOT = 5091
463984
YDOT = -11030
737615 feet/sec YDOT = -3305
568139 meter/sec
ZDOT = -15408
098448 ZDOT = -4671
801941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10933017
09 X = -3332383
61
Y = -15974820
03 feet Y = -4869125
15 meter
Z = -11016213
83 Z = -3357741
98
XDOT = 18552
792711 XDOT = 5654
891218
YDOT = -2162
519911 feet/sec YDOT = -659
136069 meter/sec
ZDOT = -15298
049353 ZDOT = -4662
845443
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
60853668
00016717 00000-0 10270-3 0 9028
2 25544 51
6402 4
5119 0003839 44
5828 315
5633 15
54225474 16499
Satellite: ISS
Catalog Number: 25544
Epoch time: 18026
60853668 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 4
5119 deg
Eccentricity:
0003839
Arg of perigee: 44
5828 deg
Mean anomaly: 315
5633 deg
Mean motion: 15
54225474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1649
Checksum: 311
Coasting Arc #4 (Orbit 1664)
---------------------------------------
Vector Time (GMT): 2018/027/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3705364
85 A = 6780375
74 meter
Y = 3484800
62 meter E =
0011065
Z = 4474178
61 I = 51
62963
XDOT = -6426
474585 Wp = 94
02024
YDOT = 2665
221864 meter/sec RA = 359
10231 deg
ZDOT = 3238
667897 TA = 323
37484
MA = 323
45043
Ha = 221
871 n
mi
Hp = 213
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12156708
84 X = 3644388
51
Y = 11433072
89 feet Y = 3525895
41 meter
Z = 14679063
67 Z = 4492029
85
XDOT = -21084
234203 XDOT = -6471
531764
YDOT = 8744
166222 feet/sec YDOT = 2593
104553 meter/sec
ZDOT = 10625
550842 ZDOT = 3207
341319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6347234
51 X = 1934637
08
Y = 15358769
73 feet Y = 4681353
01 meter
Z = 14757928
11 Z = 4498216
49
XDOT = -21761
135401 XDOT = -6632
794070
YDOT = -1106
342401 feet/sec YDOT = -337
213164 meter/sec
ZDOT = 10485
619481 ZDOT = 3196
016818
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
63730966
00016717 00000-0 10270-3 0 9038
2 25544 51
6405 359
3830 0003696 48
0593 312
0874 15
54250409 16655
Satellite: ISS
Catalog Number: 25544
Epoch time: 18027
63730966 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 359
3830 deg
Eccentricity:
0003696
Arg of perigee: 48
0593 deg
Mean anomaly: 312
0874 deg
Mean motion: 15
54250409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1665
Checksum: 317
Coasting Arc #5 (Orbit 1679)
---------------------------------------
Vector Time (GMT): 2018/028/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2013631
44 A = 6777692
14 meter
Y = -3913366
26 meter E =
0017467
Z = -5169941
83 I = 51
58720
XDOT = 7285
236134 Wp = 72
96653
YDOT = -1879
467763 meter/sec RA = 354
10345 deg
ZDOT = -1413
816529 TA = 183
39485
MA = 183
40672
Ha = 222
103 n
mi
Hp = 213
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6606402
36 X = -1944608
99
Y = -12839128
14 feet Y = -3935497
86 meter
Z = -16961751
41 Z = -5179555
77
XDOT = 23901
693354 XDOT = 7312
578873
YDOT = -6166
232817 feet/sec YDOT = -1797
846302 meter/sec
ZDOT = -4638
505673 ZDOT = -1378
361595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -939515
67 X = -286364
38
Y = -14358779
38 feet Y = -4376555
96 meter
Z = -17003868
36 Z = -5182779
08
XDOT = 23386
199328 XDOT = 7128
113555
YDOT = 3779
521090 feet/sec YDOT = 1151
998028 meter/sec
ZDOT = -4480
335810 ZDOT = -1365
606355
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
60178455
00016717 00000-0 10270-3 0 9046
2 25544 51
6403 354
5741 0003934 51
3553 308
7951 15
54226902 16805
Satellite: ISS
Catalog Number: 25544
Epoch time: 18028
60178455 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 354
5741 deg
Eccentricity:
0003934
Arg of perigee: 51
3553 deg
Mean anomaly: 308
7951 deg
Mean motion: 15
54226902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1680
Checksum: 305
Coasting Arc #6 (Orbit 1695)
---------------------------------------
Vector Time (GMT): 2018/029/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 175197
00 A = 6777106
38 meter
Y = 4236811
39 meter E =
0006628
Z = 5281999
14 I = 51
55319
XDOT = -7585
879939 Wp = 57
96450
YDOT = 1011
561464 meter/sec RA = 349
09896 deg
ZDOT = -555
826649 TA = 37
36546
MA = 37
31938
Ha = 222
026 n
mi
Hp = 213
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 574793
32 X = 102150
18
Y = 13900299
83 feet Y = 4238361
86 meter
Z = 17329393
51 Z = 5282672
98
XDOT = -24888
057543 XDOT = -7593
927842
YDOT = 3318
771207 feet/sec YDOT = 926
685987 meter/sec
ZDOT = -1823
578244 ZDOT = -592
694964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4803471
24 X = -1464098
03
Y = 13053618
22 feet Y = 3978742
83 meter
Z = 17331656
53 Z = 5282688
91
XDOT = -23344
512053 XDOT = -7115
407274
YDOT = -5933
712517 feet/sec YDOT = -1808
595575 meter/sec
ZDOT = -1987
885801 ZDOT = -605
907592
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
63055360
00016717 00000-0 10270-3 0 9050
2 25544 51
6406 349
4459 0003762 53
1150 307
0347 15
54251838 16963
Satellite: ISS
Catalog Number: 25544
Epoch time: 18029
63055360 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 349
4459 deg
Eccentricity:
0003762
Arg of perigee: 53
1150 deg
Mean anomaly: 307
0347 deg
Mean motion: 15
54251838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1696
Checksum: 307
Coasting Arc #7 (Orbit 1697)
---------------------------------------
Vector Time (GMT): 2018/029/16:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3131761
05 A = 6778502
62 meter
Y = 3383183
59 meter E =
0008319
Z = 4962551
67 I = 51
55559
XDOT = -6699
586304 Wp = 97
56187
YDOT = 3082
245513 meter/sec RA = 348
50242 deg
ZDOT = 2122
545147 TA = 331
73557
MA = 331
78068
Ha = 222
024 n
mi
Hp = 213
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10274806
60 X = 3069591
68
Y = 11099683
70 feet Y = 3417857
23 meter
Z = 16281337
48 Z = 4977613
53
XDOT = -21980
270026 XDOT = -6743
864869
YDOT = 10112
354046 feet/sec YDOT = 3007
078464 meter/sec
ZDOT = 6963
730798 ZDOT = 2089
894182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13657798
81 X = 4162897
08
Y = 6330123
82 feet Y = 1929421
74 meter
Z = 16347802
40 Z = 4982810
17
XDOT = -15971
747942 XDOT = -4868
188773
YDOT = 16818
312427 feet/sec YDOT = 5126
221628 meter/sec
ZDOT = 6817
838654 ZDOT = 2078
077222
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
75914994
00016717 00000-0 10270-3 0 9061
2 25544 51
6425 348
8052 0003820 55
4571 304
6942 15
54221678 16988
Satellite: ISS
Catalog Number: 25544
Epoch time: 18029
75914994 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 348
8052 deg
Eccentricity:
0003820
Arg of perigee: 55
4571 deg
Mean anomaly: 304
6942 deg
Mean motion: 15
54221678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1698
Checksum: 333
Coasting Arc #8 (Orbit 1711)
---------------------------------------
Vector Time (GMT): 2018/030/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1607608
14 A = 6777659
68 meter
Y = -3922567
21 meter E =
0017344
Z = -5303248
55 I = 51
52132
XDOT = 7248
283880 Wp = 80
56393
YDOT = -2431
687659 meter/sec RA = 343
81930 deg
ZDOT = -396
942503 TA = 185
62865
MA = 185
64817
Ha = 222
091 n
mi
Hp = 213
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5274304
92 X = -1537865
74
Y = -12869314
99 feet Y = -3940154
44 meter
Z = -17399109
43 Z = -5310888
31
XDOT = 23780
458923 XDOT = 7276
865053
YDOT = -7977
977885 feet/sec YDOT = -2350
472560 meter/sec
ZDOT = -1302
304801 ZDOT = -361
664436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5224302
95 X = -1592367
54
Y = -12844576
97 feet Y = -3915027
06 meter
Z = -17432443
05 Z = -5313408
64
XDOT = 22811
362140 XDOT = 6952
903180
YDOT = -7716
941059 feet/sec YDOT = -2352
123635 meter/sec
ZDOT = -1144
835842 ZDOT = -348
945965
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 18030
65932046
00016717 00000-0 10270-3 0 9071
2 25544 51
6429 344
3165 0003077 49
4625 310
6795 15
54039113 17126
Satellite: ISS
Catalog Number: 25544
Epoch time: 18030
65932046 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 344
3165 deg
Eccentricity:
0003077
Arg of perigee: 49
4625 deg
Mean anomaly: 310
6795 deg
Mean motion: 15
54039113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1712
Checksum: 301
Coasting Arc #9 (Orbit 1727)
---------------------------------------
Vector Time (GMT): 2018/031/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -103446
26 A = 6778309
39 meter
Y = 4420452
90 meter E =
0007856
Z = 5133167
53 I = 51
49229
XDOT = -7358
098507 Wp = 52
98342
YDOT = 1574
219058 meter/sec RA = 338
81178 deg
ZDOT = -1497
708474 TA = 51
49761
MA = 51
42718
Ha = 222
058 n
mi
Hp = 213
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -339390
63 X = -177802
77
Y = 14502798
22 feet Y = 4418880
29 meter
Z = 16841100
84 Z = 5132484
49
XDOT = -24140
743133 XDOT = -7367
880120
YDOT = 5164
760688 feet/sec YDOT = 1491
881078 meter/sec
ZDOT = -4913
741714 ZDOT = -1533
474270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -127708
90 X = -38925
67
Y = 14510611
77 feet Y = 4422834
47 meter
Z = 16837305
48 Z = 5132010
71
XDOT = -22928
861001 XDOT = -6988
716833
YDOT = 5708
584421 feet/sec YDOT = 1739
976532 meter/sec
ZDOT = -5073
226692 ZDOT = -1546
319496
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 18031
68822171
00016717 00000-0 10270-3 0 9083
2 25544 51
6427 339
1885 0003049 51
3268 308
8158 15
54069836 17283
Satellite: ISS
Catalog Number: 25544
Epoch time: 18031
68822171 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 339
1885 deg
Eccentricity:
0003049
Arg of perigee: 51
3268 deg
Mean anomaly: 308
8158 deg
Mean motion: 15
54069836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1728
Checksum: 330
Coasting Arc #10 (Orbit 1742)
---------------------------------------
Vector Time (GMT): 2018/032/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1706756
37 A = 6781179
08 meter
Y = -4810484
92 meter E =
0011306
Z = -4474892
22 I = 51
47108
XDOT = 6924
233978 Wp = 97
30525
YDOT = -541
226641 meter/sec RA = 333
80744 deg
ZDOT = 3228
381797 TA = 205
27032
MA = 205
32566
Ha = 222
128 n
mi
Hp = 213
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5599594
40 X = 1782157
70
Y = -15782430
83 feet Y = -4790977
29 meter
Z = -14681404
92 Z = -4466418
40
XDOT = 22717
303077 XDOT = 6914
090184
YDOT = -1775
677955 feet/sec YDOT = -463
851759 meter/sec
ZDOT = 10591
803797 ZDOT = 3261
991716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5069405
55 X = 1545154
81
Y = -15995988
07 feet Y = -4875577
17 meter
Z = -14642872
80 Z = -4463147
63
XDOT = 21392
917849 XDOT = 6520
561361
YDOT = -3036
185686 feet/sec YDOT = -925
429397 meter/sec
ZDOT = 10741
507580 ZDOT = 3274
011510
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 18032
65281655
00016717 00000-0 10270-3 0 9098
2 25544 51
6425 334
3815 0003015 54
4883 305
6551 15
54032211 17437
Satellite: ISS
Catalog Number: 25544
Epoch time: 18032
65281655 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 334
3815 deg
Eccentricity:
0003015
Arg of perigee: 54
4883 deg
Mean anomaly: 305
6551 deg
Mean motion: 15
54032211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1743
Checksum: 289
Coasting Arc #11 (Orbit 1758)
---------------------------------------
Vector Time (GMT): 2018/033/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3132450
35 A = 6784910
86 meter
Y = 5002267
00 meter E =
0015308
Z = 3334900
40 I = 51
45500
XDOT = -6056
685924 Wp = 84
83325
YDOT = -673
061306 meter/sec RA = 328
80992 deg
ZDOT = -4659
613470 TA = 56
19186
MA = 56
04620
Ha = 222
200 n
mi
Hp = 213
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10277068
09 X = -3204353
00
Y = 16411637
14 feet Y = 4966835
92 meter
Z = 10941274
27 Z = 3319509
58
XDOT = -19871
016810 XDOT = -6026
076092
YDOT = -2208
206386 feet/sec YDOT = -740
620391 meter/sec
ZDOT = -15287
445767 ZDOT = -4688
959582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9403146
34 X = -2866079
01
Y = 16972134
35 feet Y = 5173106
55 meter
Z = 10871933
56 Z = 3313765
35
XDOT = -18625
537978 XDOT = -5677
063976
YDOT = -400
908023 feet/sec YDOT = -122
196766 meter/sec
ZDOT = -15417
958527 ZDOT = -4699
393759
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 18033
68171324
00016717 00000-0 10270-3 0 9105
2 25544 51
6429 329
2538 0003113 58
4364 301
7092 15
54046792 17596
Satellite: ISS
Catalog Number: 25544
Epoch time: 18033
68171324 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 329
2538 deg
Eccentricity:
0003113
Arg of perigee: 58
4364 deg
Mean anomaly: 301
7092 deg
Mean motion: 15
54046792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1759
Checksum: 305
Coasting Arc #12 (Orbit 1773)
---------------------------------------
Vector Time (GMT): 2018/034/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4222836
15 A = 6788068
39 meter
Y = -4961121
23 meter E =
0010074
Z = -1896004
02 I = 51
43786
XDOT = 4841
650532 Wp = 44
96724
YDOT = 1990
417197 meter/sec RA = 323
81910 deg
ZDOT = 5600
522833 TA = 294
09476
MA = 294
20012
Ha = 222
176 n
mi
Hp = 213
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13854449
32 X = 4287208
48
Y = -16276644
44 feet Y = -4913538
77 meter
Z = -6220485
65 Z = -1875334
77
XDOT = 15884
680223 XDOT = 4791
829551
YDOT = 6530
240149 feet/sec YDOT = 2044
281641 meter/sec
ZDOT = 18374
418744 ZDOT = 5623
920219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12656311
16 X = 3857643
64
Y = -17258006
36 feet Y = -5260240
34 meter
Z = -6127672
17 Z = -1867714
48
XDOT = 14943
669548 XDOT = 4554
830478
YDOT = 4427
968135 feet/sec YDOT = 1349
644687 meter/sec
ZDOT = 18478
230275 ZDOT = 5632
164588
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 18034
64629915
00016717 00000-0 10270-3 0 9117
2 25544 51
6426 324
4457 0003072 60
3746 299
7713 15
54051719 17748
Satellite: ISS
Catalog Number: 25544
Epoch time: 18034
64629915 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 324
4457 deg
Eccentricity:
0003072
Arg of perigee: 60
3746 deg
Mean anomaly: 299
7713 deg
Mean motion: 15
54051719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1774
Checksum: 319
Coasting Arc #13 (Orbit 1789)
---------------------------------------
Vector Time (GMT): 2018/035/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4986671
36 A = 6789664
68 meter
Y = 4594828
03 meter E =
0014007
Z = 221350
59 I = 51
41581
XDOT = -3392
629364 Wp = 121
02198
YDOT = -3380
235108 meter/sec RA = 318
83425 deg
ZDOT = -5988
475786 TA = 56
58591
MA = 56
45202
Ha = 222
230 n
mi
Hp = 213
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16360470
34 X = -5038756
54
Y = 15074895
10 feet Y = 4538772
43 meter
Z = 726215
84 Z = 197000
72
XDOT = -11130
673768 XDOT = -3325
490213
YDOT = -11090
010196 feet/sec YDOT = -3417
798818 meter/sec
ZDOT = -19647
230268 ZDOT = -6004
792394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14926397
09 X = -4549565
83
Y = 16500506
17 feet Y = 5029354
28 meter
Z = 617095
73 Z = 188090
78
XDOT = -10760
596290 XDOT = -3279
829749
YDOT = -8956
940395 feet/sec YDOT = -2730
075433 meter/sec
ZDOT = -19719
298454 ZDOT = -6010
442169
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 18035
67518987
00016717 00000-0 10270-3 0 9128
2 25544 51
6415 319
3178 0003028 67
7914 292
3560 15
54007898 17904
Satellite: ISS
Catalog Number: 25544
Epoch time: 18035
67518987 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 319
3178 deg
Eccentricity:
0003028
Arg of perigee: 67
7914 deg
Mean anomaly: 292
3560 deg
Mean motion: 15
54007898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1790
Checksum: 336
Coasting Arc #14 (Orbit 1805)
---------------------------------------
Vector Time (GMT): 2018/036/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5346719
17 A = 6788593
12 meter
Y = -3917219
58 meter E =
0016776
Z = 1430454
50 I = 51
38855
XDOT = 1882
258062 Wp = 62
02356
YDOT = 4692
264742 meter/sec RA = 313
84728 deg
ZDOT = 5769
946120 TA = 313
63935
MA = 313
77835
Ha = 222
072 n
mi
Hp = 213
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17541729
58 X = 5383176
92
Y = -12851770
28 feet Y = -3857224
97 meter
Z = 4693092
19 Z = 1456515
38
XDOT = 6175
387344 XDOT = 1801
621085
YDOT = 15394
569364 feet/sec YDOT = 4712
862923 meter/sec
ZDOT = 18930
269423 ZDOT = 5778
893198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16019392
19 X = 4882710
74
Y = -14668033
61 feet Y = -4470816
64 meter
Z = 4809704
18 Z = 1465997
84
XDOT = 6608
844883 XDOT = 2014
375920
YDOT = 13484
120979 feet/sec YDOT = 4109
960075 meter/sec
ZDOT = 18969
330207 ZDOT = 5781
851847
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 18036
70407426
00016717 00000-0 10270-3 0 9139
2 25544 51
6412 314
1891 0002916 67
2436 292
9024 15
54070110 18061
Satellite: ISS
Catalog Number: 25544
Epoch time: 18036
70407426 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 314
1891 deg
Eccentricity:
0002916
Arg of perigee: 67
2436 deg
Mean anomaly: 292
9024 deg
Mean motion: 15
54070110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1806
Checksum: 284
Coasting Arc #15 (Orbit 1810)
---------------------------------------
Vector Time (GMT): 2018/037/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4194855
45 A = 6778348
10 meter
Y = -1475021
61 meter E =
0016480
Z = -5130777
71 I = 51
34601
XDOT = 4062
837453 Wp = 78
20257
YDOT = -6311
136801 meter/sec RA = 312
02009 deg
ZDOT = -1508
184208 TA = 177
19076
MA = 177
18150
Ha = 222
127 n
mi
Hp = 213
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13762649
11 X = -4153127
35
Y = -4839309
73 feet Y = -1521698
33 meter
Z = -16833260
19 Z = -5151053
12
XDOT = 13329
519202 XDOT = 4140
434189
YDOT = -20705
829399 feet/sec YDOT = -6265
269580 meter/sec
ZDOT = -4948
110919 ZDOT = -1488
259827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6842863
07 X = 2085704
66
Y = 12765843
67 feet Y = 3891029
15 meter
Z = -16923254
36 Z = -5158207
93
XDOT = -22885
639747 XDOT = -6975
542995
YDOT = 5830
257824 feet/sec YDOT = 1777
062585 meter/sec
ZDOT = -4858
427457 ZDOT = -1480
848689
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 18037
02560126
00016717 00000-0 10270-3 0 9143
2 25544 51
6415 312
5833 0002746 77
5359 282
6101 15
54038093 18113
Satellite: ISS
Catalog Number: 25544
Epoch time: 18037
02560126 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 312
5833 deg
Eccentricity:
0002746
Arg of perigee: 77
5359 deg
Mean anomaly: 282
6101 deg
Mean motion: 15
54038093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1811
Checksum: 290
Coasting Arc #16 (Orbit 1826)
---------------------------------------
Vector Time (GMT): 2018/038/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3107996
86 A = 6777501
56 meter
Y = 2894798
36 meter E =
0005467
Z = 5277068
28 I = 51
32277
XDOT = -4856
773328 Wp = 75
09368
YDOT = 5927
348220 meter/sec RA = 306
99970 deg
ZDOT = -389
338075 TA = 18
64303
MA = 18
62301
Ha = 221
961 n
mi
Hp = 213
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10196840
11 X = 3049762
58
Y = 9497369
96 feet Y = 2929228
74 meter
Z = 17313216
16 Z = 5292024
09
XDOT = -15934
295695 XDOT = -4920
802401
YDOT = 19446
680511 feet/sec YDOT = 5872
678423 meter/sec
ZDOT = -1277
355890 ZDOT = -413
086050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1305950
10 X = -398053
59
Y = -13790471
79 feet Y = -4203335
80 meter
Z = 17379310
12 Z = 5297213
72
XDOT = 23793
255303 XDOT = 7252
184216
YDOT = -4004
442483 feet/sec YDOT = -1220
554069 meter/sec
ZDOT = -1383
980803 ZDOT = -421
837349
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 18038
05448126
00016717 00000-0 10270-3 0 9153
2 25544 51
6418 307
4547 0002820 79
2298 280
9172 15
54094200 18273
Satellite: ISS
Catalog Number: 25544
Epoch time: 18038
05448126 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 307
4547 deg
Eccentricity:
0002820
Arg of perigee: 79
2298 deg
Mean anomaly: 280
9172 deg
Mean motion: 15
54094200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1827
Checksum: 310
Coasting Arc #17 (Orbit 1841)
---------------------------------------
Vector Time (GMT): 2018/039/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1988306
18 A = 6779227
85 meter
Y = -4243901
35 meter E =
0014944
Z = -4912136
09 I = 51
30805
XDOT = 5282
653111 Wp = 101
66223
YDOT = -5068
147249 meter/sec RA = 301
98033 deg
ZDOT = 2243
257937 TA = 190
36931
MA = 190
40017
Ha = 222
158 n
mi
Hp = 213
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6523314
25 X = -1916841
71
Y = -13923560
86 feet Y = -4265736
52 meter
Z = -16115932
06 Z = -4921620
76
XDOT = 17331
539078 XDOT = 5328
037470
YDOT = -16627
779687 feet/sec YDOT = -5008
819168 meter/sec
ZDOT = 7359
770133 ZDOT = 2269
029278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4115592
08 X = -1254432
47
Y = 14769580
88 feet Y = 4501768
25 meter
Z = -16157469
63 Z = -4924796
74
XDOT = -22858
497977 XDOT = -6967
270183
YDOT = 1797
896388 feet/sec YDOT = 547
998819 meter/sec
ZDOT = 7475
252074 ZDOT = 2278
456832
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 18039
01905702
00016717 00000-0 10270-3 0 9169
2 25544 51
6405 302
6477 0002977 82
5792 277
5699 15
54076008 18426
Satellite: ISS
Catalog Number: 25544
Epoch time: 18039
01905702 = yrday
fracday
Element set: 916
Inclination: 51
6405 deg
RA of node: 302
6477 deg
Eccentricity:
0002977
Arg of perigee: 82
5792 deg
Mean anomaly: 277
5699 deg
Mean motion: 15
54076008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1842
Checksum: 329
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