[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 8th 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) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
283/18:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
6
284/08:40:17
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
6
284/14:44:01
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
7
287/02:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
6
291/16:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 216
4
295/18:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 216
2
Coasting Arc #1 (Orbit 1612)
---------------------------------------
Vector Time (GMT): 2018/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1429894
34 A = 6778528
16 meter
Y = 4023821
21 meter E =
0010630
Z = -5273557
49 I = 51
66458
XDOT = -7450
970565 Wp = 83
80993
YDOT = 1580
511727 meter/sec RA = 172
87528 deg
ZDOT = -814
620601 TA = 178
39987
MA = 178
39646
Ha = 220
109 n
mi
Hp = 216
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4691254
39 X = 1410409
06
Y = 13201513
16 feet Y = 4039701
68 meter
Z = -17301697
79 Z = -5266659
29
XDOT = -24445
441487 XDOT = -7464
133466
YDOT = 5185
405929 feet/sec YDOT = 1497
116101 meter/sec
ZDOT = -2672
639768 ZDOT = -850
847452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8296586
68 X = -2528799
62
Y = -11336386
60 feet Y = -3455330
64 meter
Z = -17271061
12 Z = -5264219
43
XDOT = 21185
543577 XDOT = 6457
353682
YDOT = -11186
254538 feet/sec YDOT = -3409
570383 meter/sec
ZDOT = -2835
530358 ZDOT = -864
269653
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 18281
51757136
00016717 00000-0 10270-3 0 9002
2 25544 51
6416 173
9613 0003857 263
4035 96
6678 15
53810265 16130
Satellite: ISS
Catalog Number: 25544
Epoch time: 18281
51757136 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 173
9613 deg
Eccentricity:
0003857
Arg of perigee: 263
4035 deg
Mean anomaly: 96
6678 deg
Mean motion: 15
53810265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1613
Checksum: 316
Coasting Arc #2 (Orbit 1628)
---------------------------------------
Vector Time (GMT): 2018/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 231499
36 A = 6778506
68 meter
Y = -4287615
28 meter E =
0001928
Z = 5246160
93 I = 51
69793
XDOT = 7558
152716 Wp = 329
98360
YDOT = -815
915436 meter/sec RA = 167
88189 deg
ZDOT = -998
885403 TA = 129
58081
MA = 129
56378
Ha = 220
006 n
mi
Hp = 216
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 759512
34 X = 253943
93
Y = -14066979
26 feet Y = -4284900
38 meter
Z = 17211814
07 Z = 5247340
51
XDOT = 24797
088964 XDOT = 7571
566913
YDOT = -2676
887915 feet/sec YDOT = -731
320038 meter/sec
ZDOT = -3277
183082 ZDOT = -962
137209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3537884
77 X = 1078347
28
Y = 13628814
96 feet Y = 4154062
80 meter
Z = 17217493
50 Z = 5247892
02
XDOT = -21926
787118 XDOT = -6683
284713
YDOT = 9629
484683 feet/sec YDOT = 2935
066931 meter/sec
ZDOT = -3112
001329 ZDOT = -948
538005
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 18282
54662647
00016717 00000-0 10270-3 0 9019
2 25544 51
6420 168
8341 0003974 267
7204 92
3494 15
53833024 16295
Satellite: ISS
Catalog Number: 25544
Epoch time: 18282
54662647 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 168
8341 deg
Eccentricity:
0003974
Arg of perigee: 267
7204 deg
Mean anomaly: 92
3494 deg
Mean motion: 15
53833024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1629
Checksum: 318
Coasting Arc #3 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2018/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1832314
20 A = 6780656
71 meter
Y = 4484882
77 meter E =
0007504
Z = -4751292
82 I = 51
73606
XDOT = -7161
448186 Wp = 117
54303
YDOT = -42
161441 meter/sec RA = 162
89340 deg
ZDOT = 2721
890404 TA = 179
36052
MA = 179
35956
Ha = 220
074 n
mi
Hp = 216
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6011529
52 X = -1859249
46
Y = 14714182
30 feet Y = 4464241
47 meter
Z = -15588231
02 Z = -4760259
63
XDOT = -23495
564914 XDOT = -7173
666254
YDOT = -138
324937 feet/sec YDOT = -122
313766 meter/sec
ZDOT = 8930
086626 ZDOT = 2687
072178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1026884
89 X = 312994
51
Y = -15821530
02 feet Y = -4822402
35 meter
Z = -15628924
78 Z = -4763696
27
XDOT = 21269
954391 XDOT = 6483
082098
YDOT = -7286
614933 feet/sec YDOT = -2220
960232 meter/sec
ZDOT = 8773
636268 ZDOT = 2674
204334
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 18283
51136537
00016717 00000-0 10270-3 0 9022
2 25544 51
6409 164
0272 0003894 272
4296 87
6410 15
53807222 16441
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
51136537 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 164
0272 deg
Eccentricity:
0003894
Arg of perigee: 272
4296 deg
Mean anomaly: 87
6410 deg
Mean motion: 15
53807222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1644
Checksum: 307
Coasting Arc #4 (Orbit 1647)
---------------------------------------
Vector Time (GMT): 2018/283/18:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1770316
29 A = 6778360
05 meter
Y = 3829840
84 meter E =
0011106
Z = -5314748
54 I = 51
73319
XDOT = -7148
408634 Wp = 87
19603
YDOT = 2719
754587 meter/sec RA = 161
66096 deg
ZDOT = -421
457505 TA = 178
78682
MA = 178
78412
Ha = 220
172 n
mi
Hp = 216
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5808124
32 X = 1753175
18
Y = 12565094
64 feet Y = 3849541
39 meter
Z = -17436839
04 Z = -5306190
78
XDOT = -23452
784233 XDOT = -7176
243137
YDOT = 8923
079353 feet/sec YDOT = 2639
660445 meter/sec
ZDOT = -1382
734598 ZDOT = -456
250606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9944519
86 X = -3031089
65
Y = 9697939
92 feet Y = 2955932
09 meter
Z = -17398728
50 Z = -5303132
45
XDOT = -15374
226192 XDOT = -4686
064143
YDOT = -18525
420752 feet/sec YDOT = -5646
548245 meter/sec
ZDOT = -1539
324571 ZDOT = -469
186129
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 18283
76862961
00016717 00000-0 10270-3 0 9037
2 25544 51
6379 162
7411 0003654 265
2884 94
7851 15
53808623 16482
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
76862961 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 162
7411 deg
Eccentricity:
0003654
Arg of perigee: 265
2884 deg
Mean anomaly: 94
7851 deg
Mean motion: 15
53808623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1648
Checksum: 343
Coasting Arc #5 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2018/284/08:40:17
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2811879
55 A = 6778773
03 meter
Y = -3307326
22 meter E =
0002149
Z = 5207195
89 I = 51
75482
XDOT = 6623
772740 Wp = 192
50023
YDOT = -3652
611307 meter/sec RA = 158
63987 deg
ZDOT = 1254
938853 TA = 245
46007
MA = 245
48247
Ha = 220
118 n
mi
Hp = 216
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9225326
61 X = -2799981
50
Y = -10850807
82 feet Y = -3338703
65 meter
Z = 17083976
03 Z = 5193565
63
XDOT = 21731
537860 XDOT = 6658
028992
YDOT = -11983
632898 feet/sec YDOT = -3578
348038 meter/sec
ZDOT = 4117
253456 ZDOT = 1287
199072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2437386
21 X = 742915
32
Y = 14106194
98 feet Y = 4299568
23 meter
Z = 17023023
53 Z = 5188617
57
XDOT = -23748
197784 XDOT = -7238
450685
YDOT = -1048
297198 feet/sec YDOT = -319
520986 meter/sec
ZDOT = 4262
558687 ZDOT = 1299
227888
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 18284
41178599
00016717 00000-0 10270-3 0 9048
2 25544 51
6389 159
5404 0003957 274
6913 85
3788 15
53831703 16583
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
41178599 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 159
5404 deg
Eccentricity:
0003957
Arg of perigee: 274
6913 deg
Mean anomaly: 85
3788 deg
Mean motion: 15
53831703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 355
Coasting Arc #6 (Orbit 1661)
---------------------------------------
Vector Time (GMT): 2018/284/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5138791
00 A = 6783005
29 meter
Y = -1431778
23 meter E =
0006376
Z = 4185838
17 I = 51
77450
XDOT = 4438
159519 Wp = 110
20406
YDOT = -5024
377638 meter/sec RA = 157
39588 deg
ZDOT = 3723
208431 TA = 301
59103
MA = 301
65325
Ha = 220
187 n
mi
Hp = 216
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16859550
52 X = -5142731
58
Y = -4697435
14 feet Y = -1489265
46 meter
Z = 13733064
86 Z = 4160865
69
XDOT = 14560
890812 XDOT = 4475
927861
YDOT = -16484
178601 feet/sec YDOT = -4974
535589 meter/sec
ZDOT = 12215
250759 ZDOT = 3744
860084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12485248
29 X = 3805503
68
Y = -12389317
88 feet Y = -3776264
09 meter
Z = 13620968
72 Z = 4151671
27
XDOT = 6228
030827 XDOT = 1898
303796
YDOT = 19837
859006 feet/sec YDOT = 6046
579425 meter/sec
ZDOT = 12313
011654 ZDOT = 3753
005952
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 18284
66904867
00016717 00000-0 10270-3 0 9051
2 25544 51
6371 158
2565 0004064 275
7951 84
2738 15
53789888 16626
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
66904867 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 158
2565 deg
Eccentricity:
0004064
Arg of perigee: 275
7951 deg
Mean anomaly: 84
2738 deg
Mean motion: 15
53789888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1662
Checksum: 361
Coasting Arc #7 (Orbit 1676)
---------------------------------------
Vector Time (GMT): 2018/285/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3950821
85 A = 6779858
84 meter
Y = 2363255
26 meter E =
0009029
Z = -4985503
14 I = 51
79376
XDOT = -5570
246615 Wp = 64
20248
YDOT = 4806
233953 meter/sec RA = 152
41529 deg
ZDOT = -2135
107387 TA = 185
01872
MA = 185
02778
Ha = 220
127 n
mi
Hp = 216
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12962013
96 X = 3948319
12
Y = 7753462
13 feet Y = 2407421
81 meter
Z = -16356637
59 Z = -4966317
21
XDOT = -18275
087318 XDOT = -5613
205810
YDOT = 15768
484098 feet/sec YDOT = 4743
703266 meter/sec
ZDOT = -7004
945497 ZDOT = -2162
270930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13083270
34 X = -3987780
80
Y = 7730743
11 feet Y = 2356330
50 meter
Z = -16270624
52 Z = -4959286
35
XDOT = -4493
378873 XDOT = -1369
581881
YDOT = -22611
134876 feet/sec YDOT = -6891
873910 meter/sec
ZDOT = -7127
479759 ZDOT = -2172
455831
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 18285
63378274
00016717 00000-0 10270-3 0 9067
2 25544 51
6365 153
4486 0003884 278
6958 81
3754 15
53805808 16779
Satellite: ISS
Catalog Number: 25544
Epoch time: 18285
63378274 = yrday
fracday
Element set: 906
Inclination: 51
6365 deg
RA of node: 153
4486 deg
Eccentricity:
0003884
Arg of perigee: 278
6958 deg
Mean anomaly: 81
3754 deg
Mean motion: 15
53805808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1677
Checksum: 360
Coasting Arc #8 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2018/286/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2589673
09 A = 6778460
13 meter
Y = -3309850
47 meter E =
0001205
Z = 5319493
71 I = 51
81739
XDOT = 6299
567689 Wp = 272
76838
YDOT = -4356
422225 meter/sec RA = 147
43112 deg
ZDOT = 356
309572 TA = 173
84310
MA = 173
84162
Ha = 220
347 n
mi
Hp = 216
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8496302
79 X = -2578308
77
Y = -10859089
47 feet Y = -3338746
23 meter
Z = 17452407
19 Z = 5306941
47
XDOT = 20667
872996 XDOT = 6346
083417
YDOT = -14292
723834 feet/sec YDOT = -4285
715986 meter/sec
ZDOT = 1168
994659 ZDOT = 387
024470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13619606
90 X = 4151256
18
Y = -2562948
58 feet Y = -781186
73 meter
Z = 17396295
71 Z = 5302390
93
XDOT = 2836
661559 XDOT = 864
614443
YDOT = 23945
930495 feet/sec YDOT = 7298
719615 meter/sec
ZDOT = 1307
473982 ZDOT = 398
518070
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 18286
66283119
00016717 00000-0 10270-3 0 9075
2 25544 51
6363 148
3205 0003813 283
0169 77
0558 15
53765195 16931
Satellite: ISS
Catalog Number: 25544
Epoch time: 18286
66283119 = yrday
fracday
Element set: 907
Inclination: 51
6363 deg
RA of node: 148
3205 deg
Eccentricity:
0003813
Arg of perigee: 283
0169 deg
Mean anomaly: 77
0558 deg
Mean motion: 15
53765195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 330
Coasting Arc #9 (Orbit 1699)
---------------------------------------
Vector Time (GMT): 2018/287/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 624361
57 A = 6779385
46 meter
Y = 4445216
98 meter E =
0009504
Z = -5088948
99 I = 51
83572
XDOT = -6801
061849 Wp = 102
86137
YDOT = 3025
889308 meter/sec RA = 145
00129 deg
ZDOT = 1809
488309 TA = 184
61741
MA = 184
62618
Ha = 220
291 n
mi
Hp = 216
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2048430
36 X = 599327
42
Y = 14584045
20 feet Y = 4452058
86 meter
Z = -16696026
86 Z = -5085976
97
XDOT = -22313
195043 XDOT = -6843
182421
YDOT = 9927
458359 feet/sec YDOT = 2949
599671 meter/sec
ZDOT = 5936
641435 ZDOT = 1776
348065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13481420
85 X = 4109137
08
Y = 5964357
66 feet Y = 1817936
22 meter
Z = -16683089
76 Z = -5085005
76
XDOT = -3112
471869 XDOT = -948
681426
YDOT = 23216
073716 feet/sec YDOT = 7076
259269 meter/sec
ZDOT = 5787
373619 ZDOT = 1763
991479
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 18287
11303746
00016717 00000-0 10270-3 0 9086
2 25544 51
6378 146
0803 0003754 285
2649 74
8088 15
53784780 17000
Satellite: ISS
Catalog Number: 25544
Epoch time: 18287
11303746 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 146
0803 deg
Eccentricity:
0003754
Arg of perigee: 285
2649 deg
Mean anomaly: 74
8088 deg
Mean motion: 15
53784780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1700
Checksum: 330
Coasting Arc #10 (Orbit 1715)
---------------------------------------
Vector Time (GMT): 2018/288/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 772136
06 A = 6782082
11 meter
Y = -5125378
77 meter E =
0006897
Z = 4371912
51 I = 51
87080
XDOT = 6559
251073 Wp = 50
75300
YDOT = -1963
184767 meter/sec RA = 140
02459 deg
ZDOT = -3452
082025 TA = 74
19790
MA = 74
12186
Ha = 220
244 n
mi
Hp = 216
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2533254
79 X = 808155
29
Y = -16815547
16 feet Y = -5116542
67 meter
Z = 14343544
98 Z = 4375750
99
XDOT = 21519
852603 XDOT = 6597
485120
YDOT = -6440
894904 feet/sec YDOT = -1889
621001 meter/sec
ZDOT = -11325
728429 ZDOT = -3420
126013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13100293
57 X = -3992969
48
Y = -10819089
02 feet Y = -3297658
33 meter
Z = 14361299
03 Z = 4377323
94
XDOT = 4926
822890 XDOT = 1501
695617
YDOT = -20842
814178 feet/sec YDOT = -6352
889761 meter/sec
ZDOT = -11181
863769 ZDOT = -3408
232077
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 18288
14208208
00016717 00000-0 10270-3 0 9098
2 25544 51
6369 140
9525 0003874 289
5517 70
5217 15
53826817 17160
Satellite: ISS
Catalog Number: 25544
Epoch time: 18288
14208208 = yrday
fracday
Element set: 909
Inclination: 51
6369 deg
RA of node: 140
9525 deg
Eccentricity:
0003874
Arg of perigee: 289
5517 deg
Mean anomaly: 70
5217 deg
Mean motion: 15
53826817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1716
Checksum: 332
Coasting Arc #11 (Orbit 1730)
---------------------------------------
Vector Time (GMT): 2018/289/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1987879
36 A = 6785704
49 meter
Y = 5603706
72 meter E =
0002430
Z = -3268765
38 I = 51
90810
XDOT = -5961
896262 Wp = 31
96424
YDOT = 666
024608 meter/sec RA = 135
05890 deg
ZDOT = 4771
094534 TA = 290
29262
MA = 290
31873
Ha = 220
439 n
mi
Hp = 216
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6521913
91 X = -2034515
67
Y = 18384864
57 feet Y = 5581216
00 meter
Z = -10724295
87 Z = -3278535
40
XDOT = -19560
027107 XDOT = -5992
076613
YDOT = 2185
120105 feet/sec YDOT = 599
185957 meter/sec
ZDOT = 15653
197289 ZDOT = 4742
059988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12613858
18 X = 3844703
97
Y = 14848337
51 feet Y = 4525773
27 meter
Z = -10768778
17 Z = -3282323
59
XDOT = -6955
964381 XDOT = -2120
177943
YDOT = 17158
362450 feet/sec YDOT = 5229
868875 meter/sec
ZDOT = 15522
576003 ZDOT = 4731
281166
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 18289
10681033
00016717 00000-0 10270-3 0 9108
2 25544 51
6376 136
1460 0003698 295
1424 64
9344 15
53804129 17314
Satellite: ISS
Catalog Number: 25544
Epoch time: 18289
10681033 = yrday
fracday
Element set: 910
Inclination: 51
6376 deg
RA of node: 136
1460 deg
Eccentricity:
0003698
Arg of perigee: 295
1424 deg
Mean anomaly: 64
9344 deg
Mean motion: 15
53804129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1731
Checksum: 306
Coasting Arc #12 (Orbit 1746)
---------------------------------------
Vector Time (GMT): 2018/290/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2996181
39 A = 6788702
14 meter
Y = -5800337
97 meter E =
0010065
Z = 1845047
15 I = 51
94052
XDOT = 5101
679408 Wp = 111
08524
YDOT = 826
779320 meter/sec RA = 130
10274 deg
ZDOT = -5664
160505 TA = 48
70817
MA = 48
62156
Ha = 220
477 n
mi
Hp = 216
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9829991
44 X = 3051857
33
Y = -19029980
20 feet Y = -5766521
21 meter
Z = 6053304
29 Z = 1859737
18
XDOT = 16737
793333 XDOT = 5119
568793
YDOT = 2712
530577 feet/sec YDOT = 883
929646 meter/sec
ZDOT = -18583
203756 ZDOT = -5639
334607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11794419
25 X = -3594938
99
Y = -17856352
44 feet Y = -5442616
22 meter
Z = 6119944
69 Z = 1865359
14
XDOT = 9321
113678 XDOT = 2841
075449
YDOT = -12511
274437 feet/sec YDOT = -3813
436448 meter/sec
ZDOT = -18471
642129 ZDOT = -5630
156521
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 18290
13585019
00016717 00000-0 10270-3 0 9111
2 25544 51
6370 131
0180 0003926 300
7045 59
3720 15
53837399 17475
Satellite: ISS
Catalog Number: 25544
Epoch time: 18290
13585019 = yrday
fracday
Element set: 911
Inclination: 51
6370 deg
RA of node: 131
0180 deg
Eccentricity:
0003926
Arg of perigee: 300
7045 deg
Mean anomaly: 59
3720 deg
Mean motion: 15
53837399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1747
Checksum: 300
Coasting Arc #13 (Orbit 1761)
---------------------------------------
Vector Time (GMT): 2018/291/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3726685
73 A = 6790104
62 meter
Y = 5661331
40 meter E =
0011329
Z = -272072
22 I = 51
96531
XDOT = -4081
193911 Wp = 24
58522
YDOT = -2401
391947 meter/sec RA = 125
15517 deg
ZDOT = 6033
114192 TA = 332
49582
MA = 332
55573
Ha = 220
511 n
mi
Hp = 216
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12226659
22 X = -3788393
74
Y = 18573921
90 feet Y = 5619311
96 meter
Z = -892625
40 Z = -290325
52
XDOT = -13389
743801 XDOT = -4083
343556
YDOT = -7878
582502 feet/sec YDOT = -2447
042418 meter/sec
ZDOT = 19793
681731 ZDOT = 6013
283851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10544580
71 X = 3213988
20
Y = 19573941
19 feet Y = 5966137
27 meter
Z = -975292
10 Z = -297269
03
XDOT = -11925
061398 XDOT = -3634
758714
YDOT = 7390
946996 feet/sec YDOT = 2252
760644 meter/sec
ZDOT = 19704
736846 ZDOT = 6006
003791
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 18291
10057515
00016717 00000-0 10270-3 0 9125
2 25544 51
6365 126
2119 0003722 301
1615 58
9173 15
53848886 17626
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
10057515 = yrday
fracday
Element set: 912
Inclination: 51
6365 deg
RA of node: 126
2119 deg
Eccentricity:
0003722
Arg of perigee: 301
1615 deg
Mean anomaly: 58
9173 deg
Mean motion: 15
53848886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1762
Checksum: 305
Coasting Arc #14 (Orbit 1770)
---------------------------------------
Vector Time (GMT): 2018/291/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 517139
98 A = 6782832
73 meter
Y = 5314197
82 meter E =
0004109
Z = -4187183
47 I = 51
95388
XDOT = -5688
881236 Wp = 101
84989
YDOT = 3506
602169 meter/sec RA = 122
30061 deg
ZDOT = 3750
106751 TA = 206
55904
MA = 206
58010
Ha = 220
508 n
mi
Hp = 216
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1696653
46 X = 478016
04
Y = 17435032
22 feet Y = 5319761
85 meter
Z = -13737478
57 Z = -4184766
68
XDOT = -18664
308516 XDOT = -5745
886461
YDOT = 11504
600292 feet/sec YDOT = 3442
666620 meter/sec
ZDOT = 12303
499840 ZDOT = 3722
333199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17496043
03 X = -5332793
91
Y = 1015450
56 feet Y = 309509
33 meter
Z = -13727149
66 Z = -4184035
22
XDOT = -10591
379271 XDOT = -3228
252402
YDOT = -17960
276849 feet/sec YDOT = -5474
292384 meter/sec
ZDOT = 12178
224216 ZDOT = 3711
922741
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 18291
67940915
00016717 00000-0 10270-3 0 9133
2 25544 51
6390 123
3237 0003804 298
4363 61
6406 15
53812167 17715
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
67940915 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 123
3237 deg
Eccentricity:
0003804
Arg of perigee: 298
4363 deg
Mean anomaly: 61
6406 deg
Mean motion: 15
53812167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1771
Checksum: 312
Coasting Arc #15 (Orbit 1786)
---------------------------------------
Vector Time (GMT): 2018/292/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 505096
76 A = 6786453
54 meter
Y = -6067053
17 meter E =
0009938
Z = 2990494
51 I = 51
98326
XDOT = 5447
960209 Wp = 88
02711
YDOT = -2019
981881 meter/sec RA = 117
34102 deg
ZDOT = -5003
621382 TA = 57
94307
MA = 57
84659
Ha = 220
601 n
mi
Hp = 216
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1657141
59 X = 558376
29
Y = -19905030
08 feet Y = -6061106
71 meter
Z = 9811333
70 Z = 2993077
95
XDOT = 17873
885201 XDOT = 5494
448533
YDOT = -6627
237144 feet/sec YDOT = -1958
799422 meter/sec
ZDOT = -16416
080651 ZDOT = -4977
043733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19854037
33 X = 6051510
58
Y = 2129101
02 feet Y = 648949
99 meter
Z = 9823580
82 Z = 2994227
44
XDOT = 6295
325313 XDOT = 1918
815155
YDOT = 16707
471853 feet/sec YDOT = 5092
437421 meter/sec
ZDOT = -16296
323515 ZDOT = -4967
119407
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 18292
70844455
00016717 00000-0 10270-3 0 9141
2 25544 51
6395 118
1958 0003703 302
6696 57
4099 15
53811120 17873
Satellite: ISS
Catalog Number: 25544
Epoch time: 18292
70844455 = yrday
fracday
Element set: 914
Inclination: 51
6395 deg
RA of node: 118
1958 deg
Eccentricity:
0003703
Arg of perigee: 302
6696 deg
Mean anomaly: 57
4099 deg
Mean motion: 15
53811120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1787
Checksum: 328
Coasting Arc #16 (Orbit 1801)
---------------------------------------
Vector Time (GMT): 2018/293/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1364317
79 A = 6789214
30 meter
Y = 6464882
92 meter E =
0009037
Z = -1537905
14 I = 52
00691
XDOT = -5019
566510 Wp = 13
18962
YDOT = 314
105918 meter/sec RA = 112
39157 deg
ZDOT = 5788
629494 TA = 330
09255
MA = 330
14415
Ha = 220
744 n
mi
Hp = 216
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4476108
23 X = -1429038
08
Y = 21210245
80 feet Y = 6449264
17 meter
Z = -5045620
53 Z = -1544690
34
XDOT = -16468
394062 XDOT = -5050
824347
YDOT = 1030
531227 feet/sec YDOT = 257
799345 meter/sec
ZDOT = 18991
566582 ZDOT = 5764
169915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21165218
64 X = -6451158
64
Y = -4650566
77 feet Y = -1417492
75 meter
Z = -5076820
56 Z = -1547414
91
XDOT = -1207
966047 XDOT = -368
188051
YDOT = -15060
325558 feet/sec YDOT = -4590
387230 meter/sec
ZDOT = 18881
506110 ZDOT = 5755
083062
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 18293
67316266
00016717 00000-0 10270-3 0 9153
2 25544 51
6396 113
3892 0003775 308
7793 51
3022 15
53818137 18024
Satellite: ISS
Catalog Number: 25544
Epoch time: 18293
67316266 = yrday
fracday
Element set: 915
Inclination: 51
6396 deg
RA of node: 113
3892 deg
Eccentricity:
0003775
Arg of perigee: 308
7793 deg
Mean anomaly: 51
3022 deg
Mean motion: 15
53818137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1802
Checksum: 321
Coasting Arc #17 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2018/294/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2094987
28 A = 6790177
00 meter
Y = -6454155
27 meter E =
0008221
Z = -81192
67 I = 52
02141
XDOT = 4466
472742 Wp = 137
17146
YDOT = 1521
231095 meter/sec RA = 107
44796 deg
ZDOT = -6042
257519 TA = 43
69825
MA = 43
63319
Ha = 220
758 n
mi
Hp = 216
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6873317
84 X = 2167398
13
Y = -21175050
08 feet Y = -6430322
80 meter
Z = -266380
15 Z = -70839
32
XDOT = 14653
781962 XDOT = 4478
480536
YDOT = 4990
915665 feet/sec YDOT = 1571
244885 meter/sec
ZDOT = -19823
679523 ZDOT = -6020
531565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21225220
51 X = 6469447
21
Y = 6718497
20 feet Y = 2047797
95 meter
Z = -219116
91 Z = -66786
83
XDOT = -4390
332709 XDOT = -1338
173410
YDOT = 13273
995682 feet/sec YDOT = 4045
913884 meter/sec
ZDOT = -19726
107028 ZDOT = -6012
517422
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 18294
70219402
00016717 00000-0 10270-3 0 9163
2 25544 51
6391 108
2617 0003771 310
7844 49
2981 15
53835579 18189
Satellite: ISS
Catalog Number: 25544
Epoch time: 18294
70219402 = yrday
fracday
Element set: 916
Inclination: 51
6391 deg
RA of node: 108
2617 deg
Eccentricity:
0003771
Arg of perigee: 310
7844 deg
Mean anomaly: 49
2981 deg
Mean motion: 15
53835579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 326
Coasting Arc #18 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2018/295/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2667855
92 A = 6789013
34 meter
Y = 6006236
80 meter E =
0013323
Z = 1670896
42 I = 52
02771
XDOT = -3855
977589 Wp = 48
08843
YDOT = -3316
178068 meter/sec RA = 102
50430 deg
ZDOT = 5743
071157 TA = 330
12582
MA = 330
20180
Ha = 220
953 n
mi
Hp = 216
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8752808
14 X = -2742937
55
Y = 19705501
31 feet Y = 5975983
32 meter
Z = 5481943
63 Z = 1657753
73
XDOT = -12650
845107 XDOT = -3846
505954
YDOT = -10879
849305 feet/sec YDOT = -3359
244808 meter/sec
ZDOT = 18842
096973 ZDOT = 5724
363085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19915965
52 X = -6070386
29
Y = -8302082
38 feet Y = -2530474
71 meter
Z = 5422165
95 Z = 1652676
18
XDOT = 9955
793394 XDOT = 3034
525826
YDOT = -11587
151895 feet/sec YDOT = -3531
763898 meter/sec
ZDOT = 18758
296594 ZDOT = 5717
528802
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 18295
73122273
00016717 00000-0 10270-3 0 9177
2 25544 51
6404 103
1340 0003782 316
9458 43
1398 15
53840322 18347
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
73122273 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 103
1340 deg
Eccentricity:
0003782
Arg of perigee: 316
9458 deg
Mean anomaly: 43
1398 deg
Mean motion: 15
53840322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 298
Coasting Arc #19 (Orbit 1834)
---------------------------------------
Vector Time (GMT): 2018/295/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4030210
37 A = 6783257
70 meter
Y = -3631392
45 meter E =
0006566
Z = -4079498
17 I = 52
00798
XDOT = 1767
200445 Wp = 38
68881
YDOT = 6349
584871 meter/sec RA = 102
01036 deg
ZDOT = -3904
676916 TA = 191
00707
MA = 191
02144
Ha = 220
922 n
mi
Hp = 216
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13222474
96 X = 4090334
54
Y = -11914017
21 feet Y = -3585988
03 meter
Z = -13384180
35 Z = -4059774
04
XDOT = 5797
901723 XDOT = 1715
033530
YDOT = 20831
971360 feet/sec YDOT = 6369
054898 meter/sec
ZDOT = -12810
619802 ZDOT = -3896
219572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17598419
35 X = 5363998
22
Y = 3074272
52 feet Y = 937038
27 meter
Z = -13295052
42 Z = -4052331
98
XDOT = -12489
904645 XDOT = -3806
922936
YDOT = 16235
105732 feet/sec YDOT = 4948
460227 meter/sec
ZDOT = -12773
265245 ZDOT = -3893
291247
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 18295
79553666
00016717 00000-0 10270-3 0 9188
2 25544 51
6393 102
8157 0003956 316
8971 43
1872 15
53826163 18353
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
79553666 = yrday
fracday
Element set: 918
Inclination: 51
6393 deg
RA of node: 102
8157 deg
Eccentricity:
0003956
Arg of perigee: 316
8971 deg
Mean anomaly: 43
1872 deg
Mean motion: 15
53826163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1835
Checksum: 345
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