[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 3rd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24007 8258 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
307/06:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 214
8
311/16:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
2
319/09:49:40
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
5
320/04:47:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
5
320/18:14:08
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
4
Coasting Arc #1 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2018/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5274969
93 A = 6788716
98 meter
Y = -3860706
48 meter E =
0013025
Z = 1816970
63 I = 51
94612
XDOT = 1616
692038 Wp = 97
28968
YDOT = -4895
400354 meter/sec RA = 48
76738 deg
ZDOT = -5675
083838 TA = 62
82736
MA = 62
69464
Ha = 222
010 n
mi
Hp = 214
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17306331
79 X = -5240232
38
Y = -12666359
84 feet Y = -3919500
57 meter
Z = 5961189
74 Z = 1791430
85
XDOT = 5304
107737 XDOT = 1698
880513
YDOT = -16061
024784 feet/sec YDOT = -4876
862028 meter/sec
ZDOT = -18619
041464 ZDOT = -5667
030626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21405742
89 X = 6524470
43
Y = -1758065
71 feet Y = -535858
43 meter
Z = 5846789
82 Z = 1782101
54
XDOT = 6267
276917 XDOT = 1910
266004
YDOT = 14141
305778 feet/sec YDOT = 4310
270001 meter/sec
ZDOT = -18582
152749 ZDOT = -5663
840158
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 18306
53569403
00016717 00000-0 10270-3 0 9000
2 25544 51
6414 49
2918 0004090 3
3209 356
7970 15
53876756 20020
Satellite: ISS
Catalog Number: 25544
Epoch time: 18306
53569403 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 49
2918 deg
Eccentricity:
0004090
Arg of perigee: 3
3209 deg
Mean anomaly: 356
7970 deg
Mean motion: 15
53876756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2002
Checksum: 304
Coasting Arc #2 (Orbit 2013)
---------------------------------------
Vector Time (GMT): 2018/307/06:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 57215
45 A = 6781446
60 meter
Y = 5060042
78 meter E =
0008622
Z = 4506443
17 I = 51
90181
XDOT = -6371
415127 Wp = 81
22781
YDOT = -2804
830181 meter/sec RA = 45
06742 deg
ZDOT = 3226
316237 TA = 336
45427
MA = 336
49371
Ha = 222
178 n
mi
Hp = 214
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 187714
73 X = -21261
85
Y = 16601190
22 feet Y = 5060244
01 meter
Z = 14784918
52 Z = 4506530
26
XDOT = -20903
592935 XDOT = -6355
249160
YDOT = -9202
198756 feet/sec YDOT = -2875
989237 meter/sec
ZDOT = 10585
027024 ZDOT = 3195
405066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12115937
27 X = 3692937
68
Y = -11351093
92 feet Y = -3459813
43 meter
Z = 14784630
54 Z = 4506355
39
XDOT = 6680
689898 XDOT = 2036
274281
YDOT = 20753
989453 feet/sec YDOT = 6325
815985 meter/sec
ZDOT = 10446
325400 ZDOT = 3184
039982
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 18307
30743718
00016717 00000-0 10270-3 0 9010
2 25544 51
6381 45
4471 0004632 3
6602 356
4584 15
53873060 20143
Satellite: ISS
Catalog Number: 25544
Epoch time: 18307
30743718 = yrday
fracday
Element set: 901
Inclination: 51
6381 deg
RA of node: 45
4471 deg
Eccentricity:
0004632
Arg of perigee: 3
6602 deg
Mean anomaly: 356
4584 deg
Mean motion: 15
53873060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2014
Checksum: 287
Coasting Arc #3 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2018/308/06:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1300534
05 A = 6778755
40 meter
Y = -4207317
12 meter E =
0015867
Z = -5167312
31 I = 51
86877
XDOT = 6435
788580 Wp = 62
93420
YDOT = 3859
139060 meter/sec RA = 40
09101 deg
ZDOT = -1518
946007 TA = 192
43767
MA = 192
47687
Ha = 222
182 n
mi
Hp = 214
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4266844
00 X = 1372585
32
Y = -13803533
85 feet Y = -4192371
04 meter
Z = -16953124
38 Z = -5160819
43
XDOT = 21114
791929 XDOT = 6399
534659
YDOT = 12661
217387 feet/sec YDOT = 3930
905732 meter/sec
ZDOT = -4983
418659 ZDOT = -1487
770872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12993843
51 X = -3960523
50
Y = 6396284
37 feet Y = 1949587
48 meter
Z = -16923342
09 Z = -5158234
67
XDOT = -5037
047065 XDOT = -1535
291945
YDOT = -23077
998783 feet/sec YDOT = -7034
174029 meter/sec
ZDOT = -4843
685011 ZDOT = -1476
355191
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 18308
27211439
00016717 00000-0 10270-3 0 9028
2 25544 51
6380 40
6395 0004508 9
0636 351
0597 15
53897954 20292
Satellite: ISS
Catalog Number: 25544
Epoch time: 18308
27211439 = yrday
fracday
Element set: 902
Inclination: 51
6380 deg
RA of node: 40
6395 deg
Eccentricity:
0004508
Arg of perigee: 9
0636 deg
Mean anomaly: 351
0597 deg
Mean motion: 15
53897954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2029
Checksum: 314
Coasting Arc #4 (Orbit 2044)
---------------------------------------
Vector Time (GMT): 2018/309/06:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2712211
71 A = 6778156
08 meter
Y = 3202907
09 meter E =
0006276
Z = 5319716
42 I = 51
84098
XDOT = -6115
811604 Wp = 33
70942
YDOT = -4618
522850 meter/sec RA = 35
10808 deg
ZDOT = -332
082230 TA = 59
47763
MA = 59
41569
Ha = 222
436 n
mi
Hp = 214
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8898332
37 X = -2773666
88
Y = 10508225
37 feet Y = 3172233
90 meter
Z = 17453137
87 Z = 5306391
72
XDOT = -20064
998700 XDOT = -6062
098334
YDOT = -15152
634021 feet/sec YDOT = -4686
613791 meter/sec
ZDOT = -1089
508628 ZDOT = -361
660693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13809084
43 X = 4209008
94
Y = -1008169
02 feet Y = -307289
92 meter
Z = 17392754
91 Z = 5301311
70
XDOT = 3306
010919 XDOT = 1007
672128
YDOT = 23902
445092 feet/sec YDOT = 7285
465264 meter/sec
ZDOT = -1221
939213 ZDOT = -372
447072
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 18309
30110030
00016717 00000-0 10270-3 0 9039
2 25544 51
6386 35
5111 0004563 13
0944 347
0326 15
53866144 20455
Satellite: ISS
Catalog Number: 25544
Epoch time: 18309
30110030 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 35
5111 deg
Eccentricity:
0004563
Arg of perigee: 13
0944 deg
Mean anomaly: 347
0326 deg
Mean motion: 15
53866144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2045
Checksum: 268
Coasting Arc #5 (Orbit 2059)
---------------------------------------
Vector Time (GMT): 2018/310/06:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4052958
16 A = 6779560
14 meter
Y = -2183412
52 meter E =
0013419
Z = -4988050
05 I = 51
81825
XDOT = 5346
489083 Wp = 85
94132
YDOT = 5048
340926 meter/sec RA = 30
12501 deg
ZDOT = 2140
283009 TA = 204
85241
MA = 204
91710
Ha = 222
382 n
mi
Hp = 214
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13297106
81 X = 4101302
40
Y = -7163426
91 feet Y = -2137819
40 meter
Z = -16364993
60 Z = -4968244
17
XDOT = 17540
974682 XDOT = 5279
243125
YDOT = 16562
798315 feet/sec YDOT = 5107
753165 meter/sec
ZDOT = 7021
925883 ZDOT = 2166
091551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14604311
65 X = -4451394
19
Y = -4214236
60 feet Y = -1284499
32 meter
Z = -16275596
50 Z = -4960801
81
XDOT = -1293
866693 XDOT = -394
370568
YDOT = -23005
867170 feet/sec YDOT = -7012
188313 meter/sec
ZDOT = 7137
320794 ZDOT = 2175
455378
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 18310
26577003
00016717 00000-0 10270-3 0 9044
2 25544 51
6386 30
7038 0004503 18
8417 341
2902 15
53908069 20608
Satellite: ISS
Catalog Number: 25544
Epoch time: 18310
26577003 = yrday
fracday
Element set: 904
Inclination: 51
6386 deg
RA of node: 30
7038 deg
Eccentricity:
0004503
Arg of perigee: 18
8417 deg
Mean anomaly: 341
2902 deg
Mean motion: 15
53908069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2060
Checksum: 286
Coasting Arc #6 (Orbit 2075)
---------------------------------------
Vector Time (GMT): 2018/311/06:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5231461
40 A = 6782825
59 meter
Y = 1155630
40 meter E =
0013494
Z = 4154191
31 I = 51
79906
XDOT = -4159
159489 Wp = 60
31626
YDOT = -5227
846264 meter/sec RA = 25
14656 deg
ZDOT = -3767
712613 TA = 68
44628
MA = 68
30252
Ha = 222
498 n
mi
Hp = 214
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17163587
26 X = -5264174
60
Y = 3791438
32 feet Y = 1096945
73 meter
Z = 13629236
60 Z = 4128698
50
XDOT = -13645
536382 XDOT = -4082
089057
YDOT = -17151
726587 feet/sec YDOT = -5273
926015 meter/sec
ZDOT = -12361
261854 ZDOT = -3787
729645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15168541
81 X = 4623371
54
Y = 9055163
95 feet Y = 2760013
97 meter
Z = 13514405
94 Z = 4119190
93
XDOT = -1206
856754 XDOT = -367
849939
YDOT = 20681
051779 feet/sec YDOT = 6303
584582 meter/sec
ZDOT = -12450
564201 ZDOT = -3794
931968
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 18311
29474890
00016717 00000-0 10270-3 0 9059
2 25544 51
6380 25
5763 0004429 21
1935 338
9400 15
53890469 20765
Satellite: ISS
Catalog Number: 25544
Epoch time: 18311
29474890 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 25
5763 deg
Eccentricity:
0004429
Arg of perigee: 21
1935 deg
Mean anomaly: 338
9400 deg
Mean motion: 15
53890469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2076
Checksum: 318
Coasting Arc #7 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2018/311/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4212492
23 A = 6780324
12 meter
Y = 2307116
67 meter E =
0011643
Z = 4782023
09 I = 51
77912
XDOT = -5536
558145 Wp = 46
35193
YDOT = -4603
103655 meter/sec RA = 22
92767 deg
ZDOT = -2644
497699 TA = 69
74044
MA = 69
61531
Ha = 222
556 n
mi
Hp = 214
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13820512
57 X = -4261207
18
Y = 7569280
40 feet Y = 2259737
31 meter
Z = 15689052
15 Z = 4761441
34
XDOT = -18164
560843 XDOT = -5471
827521
YDOT = -15102
046113 feet/sec YDOT = -4664
655384 meter/sec
ZDOT = -8676
173553 ZDOT = -2671
235886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13291109
92 X = -4051130
30
Y = -8634432
17 feet Y = -2631774
92 meter
Z = 15596150
45 Z = 4753706
66
XDOT = 4019
781353 XDOT = 1225
229356
YDOT = -22146
075419 feet/sec YDOT = -6750
123788 meter/sec
ZDOT = -8795
789069 ZDOT = -2680
956508
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 18311
74492428
00016717 00000-0 10270-3 0 9067
2 25544 51
6395 23
3366 0004731 21
8460 338
2893 15
53927048 20833
Satellite: ISS
Catalog Number: 25544
Epoch time: 18311
74492428 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 23
3366 deg
Eccentricity:
0004731
Arg of perigee: 21
8460 deg
Mean anomaly: 338
2893 deg
Mean motion: 15
53927048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 314
Coasting Arc #8 (Orbit 2097)
---------------------------------------
Vector Time (GMT): 2018/312/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5394725
91 A = 6783804
75 meter
Y = -1445869
60 meter E =
0008663
Z = -3855078
81 I = 51
75986
XDOT = 4258
051155 Wp = 69
93976
YDOT = 4824
977691 meter/sec RA = 17
94935 deg
ZDOT = 4159
484840 TA = 243
73657
MA = 243
82562
Ha = 222
686 n
mi
Hp = 214
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17699231
97 X = 5429219
54
Y = -4743666
66 feet Y = -1385349
10 meter
Z = -12647896
35 Z = -3828788
60
XDOT = 13969
984105 XDOT = 4183
575284
YDOT = 15829
979301 feet/sec YDOT = 4872
177695 meter/sec
ZDOT = 13646
603807 ZDOT = 4179
988738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12873557
76 X = 3923860
40
Y = 13153669
06 feet Y = 4009238
33 meter
Z = -12529444
07 Z = -3818974
55
XDOT = -6004
357066 XDOT = -1830
128034
YDOT = 18929
595072 feet/sec YDOT = 5769
740578 meter/sec
ZDOT = 13738
133680 ZDOT = 4187
383146
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 18312
70958715
00016717 00000-0 10270-3 0 9071
2 25544 51
6398 18
5301 0004917 26
6953 333
4452 15
53902672 20987
Satellite: ISS
Catalog Number: 25544
Epoch time: 18312
70958715 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 18
5301 deg
Eccentricity:
0004917
Arg of perigee: 26
6953 deg
Mean anomaly: 333
4452 deg
Mean motion: 15
53902672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2098
Checksum: 322
Coasting Arc #9 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2018/313/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6268936
01 A = 6787254
16 meter
Y = 595262
49 meter E =
0015613
Z = 2520503
84 I = 51
73861
XDOT = -2607
125419 Wp = 86
32582
YDOT = -4890
367110 meter/sec RA = 12
97706 deg
ZDOT = -5300
148144 TA = 65
42809
MA = 65
26546
Ha = 222
642 n
mi
Hp = 213
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20567375
37 X = -6287370
08
Y = 1952960
94 feet Y = 525055
74 meter
Z = 8269369
56 Z = 2490005
97
XDOT = -8553
561085 XDOT = -2526
500200
YDOT = -16044
511517 feet/sec YDOT = -4919
070809 meter/sec
ZDOT = -17388
937480 ZDOT = -5312
617329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12129248
41 X = -3696994
92
Y = -16791766
62 feet Y = -5118130
47 meter
Z = 8132119
37 Z = 2478669
98
XDOT = 8337
406114 XDOT = 2541
241384
YDOT = -14517
837392 feet/sec YDOT = -4425
036837 meter/sec
ZDOT = -17444
311143 ZDOT = -5317
026036
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 18313
73855622
00016717 00000-0 10270-3 0 9089
2 25544 51
6384 13
4017 0004993 28
0153 332
1267 15
53947658 21144
Satellite: ISS
Catalog Number: 25544
Epoch time: 18313
73855622 = yrday
fracday
Element set: 908
Inclination: 51
6384 deg
RA of node: 13
4017 deg
Eccentricity:
0004993
Arg of perigee: 28
0153 deg
Mean anomaly: 332
1267 deg
Mean motion: 15
53947658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 307
Coasting Arc #10 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2018/314/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6708691
16 A = 6789469
65 meter
Y = 157572
68 meter E =
0014750
Z = -986832
13 I = 51
71324
XDOT = 748
678391 Wp = 36
95384
YDOT = 4822
197540 meter/sec RA = 8
01163 deg
ZDOT = 5917
051925 TA = 312
36407
MA = 312
48886
Ha = 222
698 n
mi
Hp = 213
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22010141
60 X = 6711224
15
Y = 516970
73 feet Y = 232608
13 meter
Z = -3237638
23 Z = -954236
72
XDOT = 2456
293934 XDOT = 665
957006
YDOT = 15820
858070 feet/sec YDOT = 4830
106971 meter/sec
ZDOT = 19412
900015 ZDOT = 5920
488142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11042680
24 X = 3365808
94
Y = 19070930
77 feet Y = 5812819
70 meter
Z = -3091068
73 Z = -942157
75
XDOT = -10899
242656 XDOT = -3322
089162
YDOT = 9427
930556 feet/sec YDOT = 2873
633234 meter/sec
ZDOT = 19427
652425 ZDOT = 5921
548459
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 18314
70321373
00016717 00000-0 10270-3 0 9099
2 25544 51
6381 8
5952 0004856 34
4467 325
6999 15
53950215 21299
Satellite: ISS
Catalog Number: 25544
Epoch time: 18314
70321373 = yrday
fracday
Element set: 909
Inclination: 51
6381 deg
RA of node: 8
5952 deg
Eccentricity:
0004856
Arg of perigee: 34
4467 deg
Mean anomaly: 325
6999 deg
Mean motion: 15
53950215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2129
Checksum: 322
Coasting Arc #11 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2018/315/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6692332
57 A = 6789637
09 meter
Y = -901671
47 meter E =
0010428
Z = -689406
30 I = 51
68189
XDOT = 1233
425019 Wp = 111
56876
YDOT = -4653
575397 meter/sec RA = 3
04573 deg
ZDOT = -5963
231309 TA = 75
86905
MA = 75
75319
Ha = 222
729 n
mi
Hp = 213
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21956471
67 X = -6678403
60
Y = -2958239
74 feet Y = -976431
86 meter
Z = -2261831
70 Z = -721882
19
XDOT = 4046
670009 XDOT = 1314
337729
YDOT = -15267
635816 feet/sec YDOT = -4639
329649 meter/sec
ZDOT = -19564
407181 ZDOT = -5957
043364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9259171
64 X = -2822195
51
Y = -20110300
71 feet Y = -6129619
66 meter
Z = -2407749
84 Z = -733882
15
XDOT = 13663
592156 XDOT = 4164
662889
YDOT = -3980
155005 feet/sec YDOT = -1213
151246 meter/sec
ZDOT = -19535
899505 ZDOT = -5954
542169
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 18315
73217680
00016717 00000-0 10270-3 0 9100
2 25544 51
6391 3
4662 0005040 35
8496 324
2994 15
53942239 21450
Satellite: ISS
Catalog Number: 25544
Epoch time: 18315
73217680 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 3
4662 deg
Eccentricity:
0005040
Arg of perigee: 35
8496 deg
Mean anomaly: 324
2994 deg
Mean motion: 15
53942239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2145
Checksum: 304
Coasting Arc #12 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2018/316/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6194597
44 A = 6787539
34 meter
Y = 1576825
10 meter E =
0018096
Z = 2254028
32 I = 51
64175
XDOT = -3115
873668 Wp = 63
52947
YDOT = 4417
687275 meter/sec RA = 358
07660 deg
ZDOT = 5446
796446 TA = 321
56415
MA = 321
69292
Ha = 222
615 n
mi
Hp = 213
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20323482
41 X = 6165555
48
Y = 5173310
69 feet Y = 1645934
89 meter
Z = 7395106
02 Z = 2284049
57
XDOT = -10222
682638 XDOT = -3191
500002
YDOT = 14493
724656 feet/sec YDOT = 4382
420273 meter/sec
ZDOT = 17870
067080 ZDOT = 5431
476907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6836475
41 X = 2083757
70
Y = 19775190
56 feet Y = 6027478
08 meter
Z = 7529881
54 Z = 2295107
89
XDOT = -16351
743774 XDOT = -4984
011502
YDOT = -1156
829007 feet/sec YDOT = -352
601481 meter/sec
ZDOT = 17800
529570 ZDOT = 5425
601413
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 18316
76113476
00016717 00000-0 10270-3 0 9113
2 25544 51
6388 358
3390 0004849 39
6199 320
5307 15
53977435 21615
Satellite: ISS
Catalog Number: 25544
Epoch time: 18316
76113476 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 358
3390 deg
Eccentricity:
0004849
Arg of perigee: 39
6199 deg
Mean anomaly: 320
5307 deg
Mean motion: 15
53977435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2161
Checksum: 332
Coasting Arc #13 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2018/317/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5263761
09 A = 6784141
76 meter
Y = -2269601
94 meter E =
0010065
Z = -3640647
94 I = 51
59703
XDOT = 4782
088169 Wp = 61
43924
YDOT = -4074
903946 meter/sec RA = 353
09637 deg
ZDOT = -4378
282638 TA = 161
72822
MA = 161
69203
Ha = 222
819 n
mi
Hp = 213
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17269557
37 X = -5220305
95
Y = -7446200
58 feet Y = -2328221
83 meter
Z = -11944383
02 Z = -3666112
39
XDOT = 15689
265647 XDOT = 4848
567155
YDOT = -13369
107435 feet/sec YDOT = -4021
055406 meter/sec
ZDOT = -14364
444352 ZDOT = -4354
891303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3558111
62 X = -1084512
42
Y = -18392464
27 feet Y = -5606023
11 meter
Z = -12058561
29 Z = -3675449
48
XDOT = 18605
852290 XDOT = 5671
063778
YDOT = 5739
332194 feet/sec YDOT = 1749
348453 meter/sec
ZDOT = -14258
663609 ZDOT = -4346
040668
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 18317
72578388
00016717 00000-0 10270-3 0 9128
2 25544 51
6387 353
5309 0005057 41
9631 318
1908 15
53946403 21767
Satellite: ISS
Catalog Number: 25544
Epoch time: 18317
72578388 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 353
5309 deg
Eccentricity:
0005057
Arg of perigee: 41
9631 deg
Mean anomaly: 318
1908 deg
Mean motion: 15
53946403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2176
Checksum: 329
Coasting Arc #14 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2018/318/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3973445
76 A = 6780483
26 meter
Y = 2927669
24 meter E =
0010671
Z = 4640004
60 I = 51
55342
XDOT = -6093
160648 Wp = 90
01113
YDOT = 3645
774135 meter/sec RA = 348
10564 deg
ZDOT = 2911
707750 TA = 330
98362
MA = 331
04290
Ha = 222
615 n
mi
Hp = 213
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13036239
36 X = 3917873
44
Y = 9605214
04 feet Y = 2971792
17 meter
Z = 15223112
21 Z = 4659171
60
XDOT = -19990
684542 XDOT = -6147
619575
YDOT = 11961
201230 feet/sec YDOT = 3577
331575 meter/sec
ZDOT = 9552
846949 ZDOT = 2881
976772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -349368
81 X = -106487
61
Y = 16107859
70 feet Y = 4909675
64 meter
Z = 15308873
76 Z = 4666144
72
XDOT = -20185
831972 XDOT = -6152
641585
YDOT = -9407
227289 feet/sec YDOT = -2867
322878 meter/sec
ZDOT = 9418
629340 ZDOT = 2870
798223
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 18318
75473612
00016717 00000-0 10270-3 0 9137
2 25544 51
6397 348
4037 0004835 44
6188 315
5353 15
53988186 21926
Satellite: ISS
Catalog Number: 25544
Epoch time: 18318
75473612 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 348
4037 deg
Eccentricity:
0004835
Arg of perigee: 44
6188 deg
Mean anomaly: 315
5353 deg
Mean motion: 15
53988186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 337
Coasting Arc #15 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2018/319/09:49:40
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3782938
02 A = 6779888
58 meter
Y = 2915517
30 meter E =
0009802
Z = 4803717
33 I = 51
52983
XDOT = -6163
982707 Wp = 91
85580
YDOT = 3798
419846 meter/sec RA = 344
56912 deg
ZDOT = 2543
976973 TA = 333
06930
MA = 333
12014
Ha = 222
675 n
mi
Hp = 213
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12411213
97 X = 3726720
52
Y = 9565345
48 feet Y = 2957506
28 meter
Z = 15760227
47 Z = 4821957
30
XDOT = -20223
040377 XDOT = -6218
357029
YDOT = 12462
007369 feet/sec YDOT = 3729
185812 meter/sec
ZDOT = 8346
381144 ZDOT = 2513
902150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14914818
85 X = -4546036
78
Y = -4528103
93 feet Y = -1380166
08 meter
Z = 15841820
92 Z = 4828587
02
XDOT = 14143
857067 XDOT = 4311
047634
YDOT = -17807
443818 feet/sec YDOT = -5427
708876 meter/sec
ZDOT = 8210
602838 ZDOT = 2502
591745
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 18319
46213940
00016717 00000-0 10270-3 0 9143
2 25544 51
6413 344
8769 0004776 48
7498 311
4066 15
53966939 22031
Satellite: ISS
Catalog Number: 25544
Epoch time: 18319
46213940 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 344
8769 deg
Eccentricity:
0004776
Arg of perigee: 48
7498 deg
Mean anomaly: 311
4066 deg
Mean motion: 15
53966939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 338
Coasting Arc #16 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2018/320/04:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5892263
44 A = 6789217
34 meter
Y = 3123335
99 meter E =
0016159
Z = 1243650
00 I = 51
53424
XDOT = -3243
738607 Wp = 105
65170
YDOT = -3772
434778 meter/sec RA = 340
59314 deg
ZDOT = -5835
287932 TA = 60
80751
MA = 60
64596
Ha = 222
849 n
mi
Hp = 213
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19331572
95 X = -5932792
60
Y = 10247165
33 feet Y = 3057217
97 meter
Z = 4080216
53 Z = 1214928
68
XDOT = -10642
187031 XDOT = -3172
967994
YDOT = -12376
754522 feet/sec YDOT = -3808
312708 meter/sec
ZDOT = -19144
645446 ZDOT = -5850
873267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19683118
97 X = 5999414
66
Y = 9608830
52 feet Y = 2928771
54 meter
Z = 3950630
42 Z = 1204152
15
XDOT = -3109
900225 XDOT = -947
897589
YDOT = 14352
414573 feet/sec YDOT = 4374
615962 meter/sec
ZDOT = -19214
178216 ZDOT = -5856
481520
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 18320
23385241
00016717 00000-0 10270-3 0 9155
2 25544 51
6399 341
0280 0004739 54
7435 305
4160 15
53956360 22156
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
23385241 = yrday
fracday
Element set: 915
Inclination: 51
6399 deg
RA of node: 341
0280 deg
Eccentricity:
0004739
Arg of perigee: 54
7435 deg
Mean anomaly: 305
4160 deg
Mean motion: 15
53956360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 295
Coasting Arc #17 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2018/320/18:14:08
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4181977
00 A = 6779991
94 meter
Y = 2389148
44 meter E =
0010391
Z = 4763112
04 I = 51
48682
XDOT = -5598
285655 Wp = 92
28275
YDOT = 4542
359626 meter/sec RA = 337
83132 deg
ZDOT = 2631
461329 TA = 331
69945
MA = 331
75586
Ha = 222
735 n
mi
Hp = 213
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13720396
97 X = 4131813
06
Y = 7838413
51 feet Y = 2435633
67 meter
Z = 15627008
00 Z = 4783305
09
XDOT = -18367
078922 XDOT = -5661
445935
YDOT = 14902
754678 feet/sec YDOT = 4479
402527 meter/sec
ZDOT = 8633
403311 ZDOT = 2604
113075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7494232
92 X = 2284242
19
Y = 13809108
34 feet Y = 4209016
22 meter
Z = 15717455
21 Z = 4790680
35
XDOT = -22493
459970 XDOT = -6856
006599
YDOT = 2501
502869 feet/sec YDOT = 762
458075 meter/sec
ZDOT = 8509
794024 ZDOT = 2593
785219
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 18320
81263425
00016717 00000-0 10270-3 0 9169
2 25544 51
6403 338
1486 0004973 51
9529 308
2071 15
53984520 22241
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
81263425 = yrday
fracday
Element set: 916
Inclination: 51
6403 deg
RA of node: 338
1486 deg
Eccentricity:
0004973
Arg of perigee: 51
9529 deg
Mean anomaly: 308
2071 deg
Mean motion: 15
53984520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 304
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