[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 4th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 438 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
187/05:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 216
2
191/20:25:31
000 -0
0 0
2 0
2
N/A -0
2 0
0 220
1
000/00:00:58
000 0
0 -0
0 216
0
193/18:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
9
197/12:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 215
7
199/12:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
5
Coasting Arc #1 (Orbit 120)
---------------------------------------
Vector Time (GMT): 2018/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3216089
60 A = 6789227
52 meter
Y = -5885068
48 meter E =
0010393
Z = 1019110
28 I = 51
30805
XDOT = 3824
873052 Wp = 46
84108
YDOT = 3112
607429 meter/sec RA = 291
66525 deg
ZDOT = 5872
984193 TA = 324
25643
MA = 324
32596
Ha = 219
842 n
mi
Hp = 216
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10551475
08 X = 3276708
78
Y = -19307967
46 feet Y = -5848765
10 meter
Z = 3343537
66 Z = 1034879
46
XDOT = 12548
796103 XDOT = 3761
255177
YDOT = 10211
966630 feet/sec YDOT = 3155
023548 meter/sec
ZDOT = 19268
320843 ZDOT = 5891
409688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21027514
47 X = -6409186
41
Y = -6441448
15 feet Y = -1963353
40 meter
Z = 3414946
38 Z = 1040875
66
XDOT = 7044
241863 XDOT = 2147
084920
YDOT = -12683
963695 feet/sec YDOT = -3866
072134 meter/sec
ZDOT = 19350
274399 ZDOT = 5897
963637
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 18185
56229401
00016717 00000-0 10270-3 0 9009
2 25544 51
6412 292
1078 0003727 263
2192 96
8536 15
54006261 1215
Satellite: ISS
Catalog Number: 25544
Epoch time: 18185
56229401 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 292
1078 deg
Eccentricity:
0003727
Arg of perigee: 263
2192 deg
Mean anomaly: 96
8536 deg
Mean motion: 15
54006261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 121
Checksum: 288
Coasting Arc #2 (Orbit 135)
---------------------------------------
Vector Time (GMT): 2018/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3690322
43 A = 6786766
63 meter
Y = 5066506
12 meter E =
0003246
Z = -2597620
78 I = 51
28816
XDOT = -2923
830086 Wp = 174
76220
YDOT = -4800
304927 meter/sec RA = 286
66891 deg
ZDOT = -5212
649427 TA = 34
62073
MA = 34
59960
Ha = 219
789 n
mi
Hp = 216
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12107357
04 X = -3734085
44
Y = 16622395
39 feet Y = 5024993
92 meter
Z = -8522377
90 Z = -2615652
82
XDOT = -9592
618394 XDOT = -2844
614330
YDOT = -15749
031912 feet/sec YDOT = -4832
557837 meter/sec
ZDOT = -17101
868198 ZDOT = -5226
660299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18844334
76 X = 5743753
23
Y = 8147955
23 feet Y = 2483496
76 meter
Z = -8603773
67 Z = -2622430
22
XDOT = -12718
207781 XDOT = -3876
509732
YDOT = 11302
911002 feet/sec YDOT = 3445
127273 meter/sec
ZDOT = -17163
835498 ZDOT = -5231
537060
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 18186
52689914
00016717 00000-0 10270-3 0 9016
2 25544 51
6407 287
3005 0003751 266
8319 93
2404 15
54006523 1364
Satellite: ISS
Catalog Number: 25544
Epoch time: 18186
52689914 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 287
3005 deg
Eccentricity:
0003751
Arg of perigee: 266
8319 deg
Mean anomaly: 93
2404 deg
Mean motion: 15
54006523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 136
Checksum: 304
Coasting Arc #3 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2018/187/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2060945
65 A = 6783034
45 meter
Y = -5125382
68 meter E =
0003068
Z = -3939562
73 I = 51
26572
XDOT = 4402
357494 Wp = 120
12427
YDOT = -4838
288807 meter/sec RA = 282
98701 deg
ZDOT = 3992
402073 TA = 191
77383
MA = 191
78101
Ha = 219
786 n
mi
Hp = 216
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6761632
72 X = -1984342
82
Y = -16815559
98 feet Y = -5148000
94 meter
Z = -12925074
57 Z = -3949388
44
XDOT = 14443
430099 XDOT = 4436
740487
YDOT = -15873
650942 feet/sec YDOT = -4788
866712 meter/sec
ZDOT = 13098
431999 ZDOT = 4013
870186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7981500
98 X = -2432761
50
Y = -16237597
41 feet Y = -4949219
69 meter
Z = -12968282
82 Z = -3952732
60
XDOT = 11875
437042 XDOT = 3619
633210
YDOT = -16373
559587 feet/sec YDOT = -4990
660962 meter/sec
ZDOT = 13195
155377 ZDOT = 4021
883359
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 18187
23427406
00016717 00000-0 10270-3 0 9022
2 25544 51
6371 283
7759 0003793 275
9824 84
0896 15
54016374 1478
Satellite: ISS
Catalog Number: 25544
Epoch time: 18187
23427406 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 283
7759 deg
Eccentricity:
0003793
Arg of perigee: 275
9824 deg
Mean anomaly: 84
0896 deg
Mean motion: 15
54016374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 147
Checksum: 334
Coasting Arc #4 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2018/188/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1271574
85 A = 6786599
27 meter
Y = 6120879
05 meter E =
0009521
Z = 2629888
30 I = 51
27242
XDOT = -4650
933267 Wp = 102
94058
YDOT = 3201
707798 meter/sec RA = 277
98010 deg
ZDOT = -5189
160985 TA = 47
25444
MA = 47
17436
Ha = 219
701 n
mi
Hp = 216
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4171833
49 X = 1190260
40
Y = 20081624
20 feet Y = 6134643
77 meter
Z = 8628242
45 Z = 2635868
25
XDOT = -15258
967412 XDOT = -4661
183822
YDOT = 10504
290675 feet/sec YDOT = 3149
641036 meter/sec
ZDOT = -17024
806380 ZDOT = -5211
778154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6023768
18 X = 1836044
54
Y = 19594459
84 feet Y = 5972391
36 meter
Z = 8654117
70 Z = 2637775
08
XDOT = -12638
477743 XDOT = -3852
208016
YDOT = 11469
393102 feet/sec YDOT = 3495
871018 meter/sec
ZDOT = -17126
426773 ZDOT = -5220
134880
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 18188
26318129
00016717 00000-0 10270-3 0 9038
2 25544 51
6379 278
6473 0004060 281
7338 78
3359 15
54053223 1637
Satellite: ISS
Catalog Number: 25544
Epoch time: 18188
26318129 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 278
6473 deg
Eccentricity:
0004060
Arg of perigee: 281
7338 deg
Mean anomaly: 78
3359 deg
Mean motion: 15
54053223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 163
Checksum: 319
Coasting Arc #5 (Orbit 177)
---------------------------------------
Vector Time (GMT): 2018/189/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -513953
51 A = 6789154
96 meter
Y = -6678736
34 meter E =
0008637
Z = -1073190
22 I = 51
27636
XDOT = 4772
055732 Wp = 14
83967
YDOT = -1305
652395 meter/sec RA = 272
98040 deg
ZDOT = 5858
750485 TA = 333
46127
MA = 333
50547
Ha = 219
855 n
mi
Hp = 216
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1686199
19 X = -434018
86
Y = -21911864
63 feet Y = -6684036
66 meter
Z = -3520965
29 Z = -1075493
42
XDOT = 15656
350827 XDOT = 4757
842515
YDOT = -4283
636468 feet/sec YDOT = -1252
368096 meter/sec
ZDOT = 19221
622327 ZDOT = 5881
896811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4130943
65 X = -1259111
63
Y = -21583381
73 feet Y = -6578614
75 meter
Z = -3530327
65 Z = -1076043
87
XDOT = 13370
594180 XDOT = 4075
357106
YDOT = -5710
042260 feet/sec YDOT = -1740
420881 meter/sec
ZDOT = 19325
339216 ZDOT = 5890
363393
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 18189
22778226
00016717 00000-0 10270-3 0 9044
2 25544 51
6372 273
8385 0003796 283
2763 76
7966 15
54018864 1787
Satellite: ISS
Catalog Number: 25544
Epoch time: 18189
22778226 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 273
8385 deg
Eccentricity:
0003796
Arg of perigee: 283
2763 deg
Mean anomaly: 76
7966 deg
Mean motion: 15
54018864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 178
Checksum: 355
Coasting Arc #6 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2018/190/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -253882
25 A = 6789351
18 meter
Y = 6752575
06 meter E =
0007639
Z = -612420
60 I = 51
27665
XDOT = -4792
377286 Wp = 152
81616
YDOT = -715
796887 meter/sec RA = 267
98587 deg
ZDOT = -5941
802842 TA = 33
82741
MA = 33
77870
Ha = 219
939 n
mi
Hp = 216
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -832947
02 X = -326397
72
Y = 22154117
65 feet Y = 6749330
59 meter
Z = -2009253
94 Z = -613829
12
XDOT = -15723
022591 XDOT = -4755
154724
YDOT = -2348
414983 feet/sec YDOT = -769
179658 meter/sec
ZDOT = -19494
103813 ZDOT = -5964
992242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2071783
89 X = 631479
73
Y = 22072093
16 feet Y = 6727574
00 meter
Z = -2016493
45 Z = -614627
20
XDOT = -14157
136550 XDOT = -4315
095220
YDOT = -450
804016 feet/sec YDOT = -137
405064 meter/sec
ZDOT = -19597
734651 ZDOT = -5973
389522
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 18190
25668508
00016717 00000-0 10270-3 0 9051
2 25544 51
6371 268
7101 0003777 291
1041 68
9708 15
54065213 1946
Satellite: ISS
Catalog Number: 25544
Epoch time: 18190
25668508 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 268
7101 deg
Eccentricity:
0003777
Arg of perigee: 291
1041 deg
Mean anomaly: 68
9708 deg
Mean motion: 15
54065213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 194
Checksum: 311
Coasting Arc #7 (Orbit 209)
---------------------------------------
Vector Time (GMT): 2018/191/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1012845
37 A = 6787534
19 meter
Y = -6328198
75 meter E =
0011233
Z = 2216730
13 I = 51
27153
XDOT = 4716
179943 Wp = 59
78646
YDOT = 2662
747001 meter/sec RA = 262
98850 deg
ZDOT = 5431
485052 TA = 324
98656
MA = 325
06037
Ha = 219
971 n
mi
Hp = 216
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3322983
50 X = 1072766
06
Y = -20761806
92 feet Y = -6316537
71 meter
Z = 7272736
65 Z = 2221794
76
XDOT = 15473
031310 XDOT = 4659
670615
YDOT = 8736
046592 feet/sec YDOT = 2715
169802 meter/sec
ZDOT = 17819
832849 ZDOT = 5454
257734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 182235
82 X = 55545
48
Y = -21017109
38 feet Y = -6406014
94 meter
Z = 7296262
57 Z = 2223900
83
XDOT = 14941
060322 XDOT = 4554
035186
YDOT = 6368
246588 feet/sec YDOT = 1941
041560 meter/sec
ZDOT = 17921
340392 ZDOT = 5462
424552
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 18191
28558851
00016717 00000-0 10270-3 0 9065
2 25544 51
6362 263
5814 0003657 289
9548 70
1210 15
54025534 2108
Satellite: ISS
Catalog Number: 25544
Epoch time: 18191
28558851 = yrday
fracday
Element set: 906
Inclination: 51
6362 deg
RA of node: 263
5814 deg
Eccentricity:
0003657
Arg of perigee: 289
9548 deg
Mean anomaly: 70
1210 deg
Mean motion: 15
54025534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 210
Checksum: 307
Coasting Arc #8 (Orbit 218)
---------------------------------------
Vector Time (GMT): 2018/191/20:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 944252
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4347186
70 A = 6778841
99 meter
Y = -1302961
97 meter E =
0009329
Z = -5043962
58 I = 51
24755
XDOT = 136
880485 Wp = 98
10867
YDOT = -7443
815121 meter/sec RA = 259
82276 deg
ZDOT = 1806
508066 TA = 189
48228
MA = 189
49990
Ha = 220
100 n
mi
Hp = 216
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14262423
56 X = -4307792
72
Y = -4274809
62 feet Y = -1351354
14 meter
Z = -16548433
67 Z = -5064984
16
XDOT = 449
082957 XDOT = 211
334071
YDOT = -24421
965619 feet/sec YDOT = -7441
868422 meter/sec
ZDOT = 5926
863733 ZDOT = 1807
352626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11725832
84 X = 3574033
85
Y = -9004445
17 feet Y = -2744554
89 meter
Z = -16642301
27 Z = -5072573
43
XDOT = 18945
049865 XDOT = 5774
451199
YDOT = 13717
241343 feet/sec YDOT = 4181
015161 meter/sec
ZDOT = 5931
656201 ZDOT = 1807
968810
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 18191
86434566
00016717 00000-0 10270-3 0 9076
2 25544 51
6388 260
7003 0003993 296
5542 63
5201 15
53988785 2196
Satellite: ISS
Catalog Number: 25544
Epoch time: 18191
86434566 = yrday
fracday
Element set: 907
Inclination: 51
6388 deg
RA of node: 260
7003 deg
Eccentricity:
0003993
Arg of perigee: 296
5542 deg
Mean anomaly: 63
5201 deg
Mean motion: 15
53988785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 219
Checksum: 336
Coasting Arc #9 (Orbit 234)
---------------------------------------
Vector Time (GMT): 2018/192/20:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 944252
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4360262
75 A = 6781805
02 meter
Y = 2927358
86 meter E =
0007745
Z = 4288985
45 I = 51
26465
XDOT = -1075
963390 Wp = 48
88609
YDOT = 6738
879186 meter/sec RA = 254
80387 deg
ZDOT = -3496
494893 TA = 76
93016
MA = 76
84372
Ha = 220
173 n
mi
Hp = 216
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14305323
99 X = 4306370
72
Y = 9604195
72 feet Y = 2975816
27 meter
Z = 14071474
58 Z = 4310035
51
XDOT = -3530
063615 XDOT = -1134
255452
YDOT = 22109
183682 feet/sec YDOT = 6726
521677 meter/sec
ZDOT = -11471
439937 ZDOT = -3501
861953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15985326
81 X = -4872327
61
Y = 6221244
60 feet Y = 1896235
35 meter
Z = 14165264
17 Z = 4317572
52
XDOT = -15761
388339 XDOT = -4804
071166
YDOT = -14254
359037 feet/sec YDOT = -4344
728634 meter/sec
ZDOT = -11496
357515 ZDOT = -3504
089771
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 18192
89326853
00016717 00000-0 10270-3 0 9080
2 25544 51
6390 255
5726 0004049 301
8196 58
2562 15
53997650 2351
Satellite: ISS
Catalog Number: 25544
Epoch time: 18192
89326853 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 255
5726 deg
Eccentricity:
0004049
Arg of perigee: 301
8196 deg
Mean anomaly: 58
2562 deg
Mean motion: 15
53997650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 235
Checksum: 335
Coasting Arc #10 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2018/193/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 944252
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3334587
81 A = 6778460
71 meter
Y = 2915436
40 meter E =
0011390
Z = -5141088
78 I = 51
26019
XDOT = -3590
787502 Wp = 64
43670
YDOT = -6615
337724 meter/sec RA = 250
21286 deg
ZDOT = -1420
064802 TA = 191
80016
MA = 191
82687
Ha = 220
362 n
mi
Hp = 215
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10940248
70 X = -3341968
86
Y = 9565080
04 feet Y = 2878106
31 meter
Z = -16867089
16 Z = -5157304
26
XDOT = -11780
798892 XDOT = -3509
648281
YDOT = -21703
863923 feet/sec YDOT = -6655
038477 meter/sec
ZDOT = -4659
005257 ZDOT = -1437
311358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4898187
41 X = 1492967
52
Y = -13591229
83 feet Y = -4142606
85 meter
Z = -16940033
25 Z = -5163322
13
XDOT = 19744
800869 XDOT = 6018
215305
YDOT = 13027
550589 feet/sec YDOT = 3970
797420 meter/sec
ZDOT = -4735
305373 ZDOT = -1443
321078
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 18193
79357484
00016717 00000-0 10270-3 0 9095
2 25544 51
6371 251
0849 0004010 305
3430 54
7347 15
53986730 2499
Satellite: ISS
Catalog Number: 25544
Epoch time: 18193
79357484 = yrday
fracday
Element set: 909
Inclination: 51
6371 deg
RA of node: 251
0849 deg
Eccentricity:
0004010
Arg of perigee: 305
3430 deg
Mean anomaly: 54
7347 deg
Mean motion: 15
53986730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 318
Coasting Arc #11 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2018/194/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 944252
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4057543
26 A = 6777806
87 meter
Y = -1299238
58 meter E =
0003495
Z = 5272097
21 I = 51
27042
XDOT = 2873
441558 Wp = 349
94518
YDOT = 7094
457357 meter/sec RA = 245
18934 deg
ZDOT = -459
803435 TA = 104
48263
MA = 104
44384
Ha = 220
313 n
mi
Hp = 216
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13312149
79 X = 4046161
59
Y = -4262593
76 feet Y = -1253928
74 meter
Z = 17296906
87 Z = 5291779
13
XDOT = 9427
301699 XDOT = 2796
129264
YDOT = 23275
778729 feet/sec YDOT = 7126
157950 meter/sec
ZDOT = -1508
541453 ZDOT = -446
032273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9349526
56 X = -2849735
70
Y = 10242496
70 feet Y = 3121912
99 meter
Z = 17385155
72 Z = 5298995
46
XDOT = -18986
643667 XDOT = -5787
128990
YDOT = -14855
365859 feet/sec YDOT = -4527
915514 meter/sec
ZDOT = -1447
828922 ZDOT = -441
298255
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 18194
82249568
00016717 00000-0 10270-3 0 9105
2 25544 51
6372 245
9574 0004064 309
1538 50
9253 15
53993622 2657
Satellite: ISS
Catalog Number: 25544
Epoch time: 18194
82249568 = yrday
fracday
Element set: 910
Inclination: 51
6372 deg
RA of node: 245
9574 deg
Eccentricity:
0004064
Arg of perigee: 309
1538 deg
Mean anomaly: 50
9253 deg
Mean motion: 15
53993622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 326
Coasting Arc #12 (Orbit 279)
---------------------------------------
Vector Time (GMT): 2018/195/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 944252
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4692373
78 A = 6779457
35 meter
Y = -302332
66 meter E =
0008658
Z = -4891532
36 I = 51
29095
XDOT = -1929
269494 Wp = 94
76370
YDOT = -7052
305272 meter/sec RA = 240
16683 deg
ZDOT = 2289
408930 TA = 197
73708
MA = 197
76733
Ha = 220
488 n
mi
Hp = 215
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15394927
11 X = -4664884
33
Y = -991905
06 feet Y = -354651
74 meter
Z = -16048334
51 Z = -4914259
03
XDOT = -6329
624323 XDOT = -1861
385775
YDOT = -23137
484487 feet/sec YDOT = -7073
500404 meter/sec
ZDOT = 7511
184152 ZDOT = 2280
201461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13652541
50 X = 4161294
65
Y = -6951390
94 feet Y = -2118783
96 meter
Z = -16150014
59 Z = -4922524
45
XDOT = 16790
888933 XDOT = 5117
862947
YDOT = 15641
681965 feet/sec YDOT = 4767
584663 meter/sec
ZDOT = 7470
864118 ZDOT = 2277
119383
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 18195
78710589
00016717 00000-0 10270-3 0 9118
2 25544 51
6373 241
1492 0004130 312
5074 47
5729 15
53994895 2802
Satellite: ISS
Catalog Number: 25544
Epoch time: 18195
78710589 = yrday
fracday
Element set: 911
Inclination: 51
6373 deg
RA of node: 241
1492 deg
Eccentricity:
0004130
Arg of perigee: 312
5074 deg
Mean anomaly: 47
5729 deg
Mean motion: 15
53994895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 280
Checksum: 324
Coasting Arc #13 (Orbit 295)
---------------------------------------
Vector Time (GMT): 2018/196/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 929538
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5164570
78 A = 6782742
51 meter
Y = 1802374
67 meter E =
0009371
Z = 4007770
29 I = 51
31934
XDOT = 752
961410 Wp = 55
54295
YDOT = 6554
979019 meter/sec RA = 235
15298 deg
ZDOT = -3906
447303 TA = 75
24835
MA = 75
14453
Ha = 220
605 n
mi
Hp = 215
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16944129
87 X = 5124565
11
Y = 5913302
73 feet Y = 1859904
42 meter
Z = 13148852
64 Z = 4032760
41
XDOT = 2470
345834 XDOT = 698
580896
YDOT = 21505
836678 feet/sec YDOT = 6563
095444 meter/sec
ZDOT = -12816
428160 ZDOT = -3902
921251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17450476
84 X = -5318905
34
Y = 3821422
16 feet Y = 1164769
47 meter
Z = 13260490
29 Z = 4041797
44
XDOT = -13191
496863 XDOT = -4020
768244
YDOT = -15684
556402 feet/sec YDOT = -4780
652791 meter/sec
ZDOT = -12801
452836 ZDOT = -3901
882824
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 18196
81602174
00016717 00000-0 10270-3 0 9124
2 25544 51
6372 236
0208 0004193 318
0969 41
9862 15
54011940 2967
Satellite: ISS
Catalog Number: 25544
Epoch time: 18196
81602174 = yrday
fracday
Element set: 912
Inclination: 51
6372 deg
RA of node: 236
0208 deg
Eccentricity:
0004193
Arg of perigee: 318
0969 deg
Mean anomaly: 41
9862 deg
Mean motion: 15
54011940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 296
Checksum: 305
Coasting Arc #14 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2018/197/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929538
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -714522
59 A = 6783952
96 meter
Y = -5637226
91 meter E =
0009573
Z = 3695954
39 I = 51
33765
XDOT = 6022
855159 Wp = 78
25943
YDOT = 2051
356137 meter/sec RA = 231
41776 deg
ZDOT = 4285
668025 TA = 326
02930
MA = 326
09056
Ha = 220
797 n
mi
Hp = 215
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2344234
21 X = -669385
08
Y = -18494838
95 feet Y = -5644965
08 meter
Z = 12125834
61 Z = 3692592
78
XDOT = 19760
023487 XDOT = 5978
651628
YDOT = 6730
171052 feet/sec YDOT = 2118
460397 meter/sec
ZDOT = 14060
590632 ZDOT = 4314
817138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13828394
49 X = -4214894
64
Y = 12517115
28 feet Y = 3815216
74 meter
Z = 12111469
69 Z = 3691575
96
XDOT = -4742
332253 XDOT = -1445
462871
YDOT = -18993
974341 feet/sec YDOT = -5789
363379 meter/sec
ZDOT = 14190
826831 ZDOT = 4325
364018
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 18197
58770841
00016717 00000-0 10270-3 0 9137
2 25544 51
6372 232
1738 0003850 322
5466 37
5418 15
53988796 3086
Satellite: ISS
Catalog Number: 25544
Epoch time: 18197
58770841 = yrday
fracday
Element set: 913
Inclination: 51
6372 deg
RA of node: 232
1738 deg
Eccentricity:
0003850
Arg of perigee: 322
5466 deg
Mean anomaly: 37
5418 deg
Mean motion: 15
53988796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 337
Coasting Arc #15 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2018/198/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929538
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -561759
27 A = 6780306
14 meter
Y = 4862927
57 meter E =
0010301
Z = -4701203
75 I = 51
34839
XDOT = -6284
509931 Wp = 49
70314
YDOT = -3398
249991 meter/sec RA = 226
40950 deg
ZDOT = -2761
674881 TA = 192
78852
MA = 192
81466
Ha = 220
808 n
mi
Hp = 215
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1843042
22 X = -593260
55
Y = 15954486
78 feet Y = 4856469
72 meter
Z = -15423896
82 Z = -4704008
77
XDOT = -20618
470903 XDOT = -6232
628167
YDOT = -11149
114144 feet/sec YDOT = -3468
237476 meter/sec
ZDOT = -9060
613128 ZDOT = -2792
076497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13975685
59 X = 4259788
97
Y = -7887794
05 feet Y = -2404199
63 meter
Z = -15437032
20 Z = -4705207
42
XDOT = 2353
294428 XDOT = 717
284142
YDOT = 22183
692092 feet/sec YDOT = 6761
589350 meter/sec
ZDOT = -9196
312471 ZDOT = -2803
036041
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 18198
55231386
00016717 00000-0 10270-3 0 9142
2 25544 51
6385 227
3665 0003936 323
1037 36
9844 15
54010122 3234
Satellite: ISS
Catalog Number: 25544
Epoch time: 18198
55231386 = yrday
fracday
Element set: 914
Inclination: 51
6385 deg
RA of node: 227
3665 deg
Eccentricity:
0003936
Arg of perigee: 323
1037 deg
Mean anomaly: 36
9844 deg
Mean motion: 15
54010122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 300
Coasting Arc #16 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2018/199/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 929538
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3638088
58 A = 6787998
39 meter
Y = -5355884
82 meter E =
0013898
Z = 2011022
28 I = 51
39730
XDOT = 5117
245491 Wp = 51
73524
YDOT = -1387
114997 meter/sec RA = 221
45540 deg
ZDOT = 5545
581528 TA = 330
57102
MA = 330
64920
Ha = 220
979 n
mi
Hp = 215
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11935986
16 X = -3587695
56
Y = -17571800
61 feet Y = -5396286
78 meter
Z = 6597842
12 Z = 1993472
06
XDOT = 16788
863160 XDOT = 5105
439135
YDOT = -4550
902222 feet/sec YDOT = -1329
956727 meter/sec
ZDOT = 18194
165119 ZDOT = 5570
410242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8248826
99 X = -2514242
47
Y = 19601411
22 feet Y = 5974510
14 meter
Z = 6519892
20 Z = 1987263
14
XDOT = -11442
478757 XDOT = -3487
667525
YDOT = -10923
637805 feet/sec YDOT = -3329
524803 meter/sec
ZDOT = 18305
490715 ZDOT = 5579
513570
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 18199
58122499
00016717 00000-0 10270-3 0 9151
2 25544 51
6384 222
2378 0004056 329
3632 30
7283 15
54011594 3391
Satellite: ISS
Catalog Number: 25544
Epoch time: 18199
58122499 = yrday
fracday
Element set: 915
Inclination: 51
6384 deg
RA of node: 222
2378 deg
Eccentricity:
0004056
Arg of perigee: 329
3632 deg
Mean anomaly: 30
7283 deg
Mean motion: 15
54011594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 316
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