[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 26th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 161 4587 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
269/10:12:00
354 -0
2 -1
2 1
2
003/16:19:33
354 0
9 0
0 206
3
000/00:00:24
975 -0
9 -0
0 194
0
269/15:12:52
991 0
8 0
0 1
3
003/21:20:25
991 -0
6 1
3 206
1
000/00:00:26
262 -0
8 -0
0 194
2
269/17:52:00
090 1
8 10
4 10
4
003/23:59:33
090 -7
1 -0
0 206
1
000/00:00:53
198 7
3 -0
0 200
2
269/18:39:12
990 -3
9 14
5 14
5
004/00:46:45
990 8
9 -0
0 214
5
000/00:01:14
073 -10
7 0
6 200
3
269/19:30:35
153 8
8 18
9 18
9
004/01:38:08
153 -7
6 -0
2 214
8
000/00:01:36
806 14
9 -0
5 209
6
269/23:54:29
358 0
3 0
0 0
4
004/06:02:02
358 -0
2 0
4 215
0
000/00:00:08
716 -0
3 -0
0 209
3
270/02:33:28
204 0
0 0
0 0
0
004/08:41:01
204 0
0 0
0 215
0
000/00:00:00
000 0
0 0
0 209
6
270/03:19:51
153 0
0 0
0 0
0
004/09:27:24
153 0
0 0
0 215
0
000/00:00:00
000 0
0 0
0 209
5
270/04:06:15
989 -6
2 8
0 8
1
004/10:13:48
989 -0
8 -0
0 218
8
000/00:02:39
998 -5
1 0
7 211
8
270/04:52:36
808 6
1 8
0 8
0
004/11:00:09
808 0
8 -0
0 219
6
000/00:02:39
865 5
2 0
6 214
3
270/05:38:34
827 0
0 0
0 0
0
004/11:46:07
827 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 214
2
270/06:25:12
857 0
0 0
0 0
0
004/12:32:45
857 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 214
2
270/07:11:37
999 -2
3 3
0 3
0
004/13:19:10
999 -0
2 -0
0 220
9
000/00:00:59
673 -2
0 0
1 215
3
270/07:34:41
670 0
0 0
0 0
0
004/13:42:14
670 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 215
2
270/07:57:59
998 2
5 3
0 3
1
004/14:05:32
998 0
1 0
3 221
4
000/00:01:00
490 1
8 0
1 215
9
270/11:54:38
000 0
0 0
0 0
0
004/18:02:11
000 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 216
0
Coasting Arc #1 (Orbit 12)
---------------------------------------
Vector Time (GMT): 2018/269/08:04:55
241
Vector Time (MET): N/A
Weight (LBS) : 35533
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2974648
95 A = 6754988
77 meter
Y = 5892687
62 meter E =
0021588
Z = -1370038
83 I = 51
34925
XDOT = -4922
874810 Wp = 171
58763
YDOT = 1142
925361 meter/sec RA = 233
66056 deg
ZDOT = -5805
304372 TA = 23
49533
MA = 23
39685
Ha = 206
329 n
mi
Hp = 194
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9759346
95 X = 2915189
20
Y = 19332964
62 feet Y = 5925619
58 meter
Z = -4494878
06 Z = -1355734
02
XDOT = -16151
164074 XDOT = -4907
090022
YDOT = 3749
755122 feet/sec YDOT = 1087
961895 meter/sec
ZDOT = -19046
274186 ZDOT = -5829
180050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10076580
30 X = 3071341
68
Y = -19184331
02 feet Y = -5847384
10 meter
Z = -4431283
73 Z = -1350655
28
XDOT = 10945
445852 XDOT = 3336
171896
YDOT = 10148
256227 feet/sec YDOT = 3093
188498 meter/sec
ZDOT = -19153
499781 ZDOT = -5837
986733
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 18269
36607468
00016717 00000-0 10270-3 0 9003
2 25544 51
6413 234
5559 0014521 188
2985 171
7936 15
65745928 139
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
36607468 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 234
5559 deg
Eccentricity:
0014521
Arg of perigee: 188
2985 deg
Mean anomaly: 171
7936 deg
Mean motion: 15
65745928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 13
Checksum: 336
Coasting Arc #2 (Orbit 13)
---------------------------------------
Vector Time (GMT): 2018/269/10:12:12
842
Vector Time (MET): N/A
Weight (LBS) : 35528
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5132087
33 A = 6752613
50 meter
Y = -3721883
45 meter E =
0011538
Z = -2347170
23 I = 51
34300
XDOT = 1390
602083 Wp = 167
58622
YDOT = -5306
200219 meter/sec RA = 233
17748 deg
ZDOT = 5367
264807 TA = 166
01458
MA = 165
98260
Ha = 206
297 n
mi
Hp = 193
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16837556
85 X = -5078685
32
Y = -12210903
72 feet Y = -3778975
72 meter
Z = -7700689
72 Z = -2371970
24
XDOT = 4562
342793 XDOT = 1423
762497
YDOT = -17408
793368 feet/sec YDOT = -5290
463466 meter/sec
ZDOT = 17609
136506 ZDOT = 5374
101142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10787023
36 X = 3287884
72
Y = 17734976
77 feet Y = 5405620
92 meter
Z = -7811583
62 Z = -2380970
69
XDOT = -9514
103219 XDOT = -2899
898661
YDOT = 13565
490236 feet/sec YDOT = 4134
761424 meter/sec
ZDOT = 17640
328807 ZDOT = 5376
772220
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 18269
42989902
00016717 00000-0 10270-3 0 9017
2 25544 51
6387 234
2331 0015230 185
7404 174
3583 15
65994557 142
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
42989902 = yrday
fracday
Element set: 901
Inclination: 51
6387 deg
RA of node: 234
2331 deg
Eccentricity:
0015230
Arg of perigee: 185
7404 deg
Mean anomaly: 174
3583 deg
Mean motion: 15
65994557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 14
Checksum: 323
Coasting Arc #3 (Orbit 17)
---------------------------------------
Vector Time (GMT): 2018/269/15:13:06
122
Vector Time (MET): N/A
Weight (LBS) : 35523
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1899702
46 A = 6744131
64 meter
Y = -4095608
47 meter E =
0018369
Z = 5012940
07 I = 51
31997
XDOT = 5647
773160 Wp = 172
29253
YDOT = 4880
951510 meter/sec RA = 232
14553 deg
ZDOT = 1828
786491 TA = 259
85662
MA = 260
06387
Ha = 206
133 n
mi
Hp = 194
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6232619
61 X = 1921008
98
Y = -13437035
66 feet Y = -4074244
93 meter
Z = 16446653
78 Z = 5022220
53
XDOT = 18529
439502 XDOT = 5583
889860
YDOT = 16013
620440 feet/sec YDOT = 4943
751858 meter/sec
ZDOT = 5999
955680 ZDOT = 1856
065985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6993766
91 X = 2131700
16
Y = 13003929
35 feet Y = 3963597
67 meter
Z = 16488691
30 Z = 5025753
11
XDOT = -22988
355271 XDOT = -7006
850687
YDOT = 4523
575520 feet/sec YDOT = 1378
785819 meter/sec
ZDOT = 6121
862138 ZDOT = 1865
943580
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 18269
68515712
00016717 00000-0 10270-3 0 9020
2 25544 51
6399 232
9346 0015152 188
0116 172
0803 15
66013520 182
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
68515712 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 232
9346 deg
Eccentricity:
0015152
Arg of perigee: 188
0116 deg
Mean anomaly: 172
0803 deg
Mean motion: 15
66013520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 18
Checksum: 296
Coasting Arc #4 (Orbit 18)
---------------------------------------
Vector Time (GMT): 2018/269/17:52:26
689
Vector Time (MET): N/A
Weight (LBS) : 35487
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5170920
29 A = 6758646
91 meter
Y = -3816007
16 meter E =
0003087
Z = -2096575
12 I = 51
35369
XDOT = 1548
817367 Wp = 210
42287
YDOT = -5125
620943 meter/sec RA = 231
54771 deg
ZDOT = 5503
097757 TA = 126
17945
MA = 126
15089
Ha = 206
149 n
mi
Hp = 200
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16964961
58 X = -5117680
14
Y = -12519708
52 feet Y = -3873534
54 meter
Z = -6878527
31 Z = -2121564
20
XDOT = 5081
421807 XDOT = 1579
286888
YDOT = -16816
341675 feet/sec YDOT = -5108
129963 meter/sec
ZDOT = 18054
782666 ZDOT = 5510
696091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11704062
71 X = 3567398
31
Y = -17493378
32 feet Y = -5331981
71 meter
Z = -6990264
08 Z = -2130632
49
XDOT = 15755
698393 XDOT = 4802
336870
YDOT = 3305
074935 feet/sec YDOT = 1007
386840 meter/sec
ZDOT = 18089
373949 ZDOT = 5513
641180
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 18269
74896986
00016717 00000-0 10270-3 0 9033
2 25544 51
6413 232
6112 0009395 217
8098 142
2401 15
64065014 196
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
74896986 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 232
6112 deg
Eccentricity:
0009395
Arg of perigee: 217
8098 deg
Mean anomaly: 142
2401 deg
Mean motion: 15
64065014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 19
Checksum: 313
Coasting Arc #5 (Orbit 19)
---------------------------------------
Vector Time (GMT): 2018/269/18:39:50
026
Vector Time (MET): N/A
Weight (LBS) : 35436
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5022825
47 A = 6767242
80 meter
Y = 4204489
47 meter E =
0026687
Z = 1626663
68 I = 51
35654
XDOT = -2088
082836 Wp = 156
63139
YDOT = 4709
228093 meter/sec RA = 231
38415 deg
ZDOT = -5716
502333 TA = 5
39508
MA = 5
36638
Ha = 214
498 n
mi
Hp = 200
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16479086
18 X = 4967534
81
Y = 13794256
79 feet Y = 4260349
24 meter
Z = 5336823
10 Z = 1650928
33
XDOT = -6850
665472 XDOT = -2112
819434
YDOT = 15450
223403 feet/sec YDOT = 4685
738704 meter/sec
ZDOT = -18754
928914 ZDOT = -5726
706289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9205416
40 X = -2805810
92
Y = 19388986
62 feet Y = 5909763
12 meter
Z = 5445272
16 Z = 1659718
96
XDOT = -15231
382599 XDOT = -4642
525416
YDOT = -1944
084687 feet/sec YDOT = -592
557013 meter/sec
ZDOT = -18801
169097 ZDOT = -5730
596341
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 18269
81293266
00016717 00000-0 10270-3 0 9044
2 25544 51
6409 232
2881 0018369 185
9104 174
1839 15
61351961 201
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
81293266 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 232
2881 deg
Eccentricity:
0018369
Arg of perigee: 185
9104 deg
Mean anomaly: 174
1839 deg
Mean motion: 15
61351961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 20
Checksum: 319
Coasting Arc #6 (Orbit 20)
---------------------------------------
Vector Time (GMT): 2018/269/19:31:23
556
Vector Time (MET): N/A
Weight (LBS) : 35371
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4045169
98 A = 6778478
42 meter
Y = -5425799
11 meter E =
0008860
Z = 306386
15 I = 51
35984
XDOT = 4009
987303 Wp = 54
38244
YDOT = -2645
189476 meter/sec RA = 231
21978 deg
ZDOT = 5982
675661 TA = 308
93686
MA = 309
01581
Ha = 214
832 n
mi
Hp = 209
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13271555
05 X = -3985684
82
Y = -17801178
19 feet Y = -5470702
37 meter
Z = 1005203
90 Z = 286881
00
XDOT = 13156
126321 XDOT = 4010
207457
YDOT = -8678
443163 feet/sec YDOT = -2600
345068 meter/sec
ZDOT = 19628
200986 ZDOT = 6002
155886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9651060
66 X = 2941643
29
Y = -20001010
98 feet Y = -6096308
15 meter
Z = 918227
03 Z = 279875
60
XDOT = 12255
438320 XDOT = 3735
457600
YDOT = 6838
004748 feet/sec YDOT = 2084
223847 meter/sec
ZDOT = 19715
856091 ZDOT = 6009
392936
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 18269
87707947
00016717 00000-0 10270-3 0 9057
2 25544 51
6398 231
9652 0003938 214
9395 145
1502 15
57857283 210
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
87707947 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 231
9652 deg
Eccentricity:
0003938
Arg of perigee: 214
9395 deg
Mean anomaly: 145
1502 deg
Mean motion: 15
57857283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 21
Checksum: 341
Coasting Arc #7 (Orbit 22)
---------------------------------------
Vector Time (GMT): 2018/269/23:54:33
716
Vector Time (MET): N/A
Weight (LBS) : 35369
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5256603
25 A = 6771238
56 meter
Y = -1178850
81 meter E =
0008146
Z = -4111115
59 I = 51
33822
XDOT = -1489
101507 Wp = 140
74082
YDOT = -6508
201369 meter/sec RA = 230
26922 deg
ZDOT = 3768
128180 TA = 168
27927
MA = 168
26030
Ha = 215
044 n
mi
Hp = 209
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17246073
64 X = -5223060
42
Y = -3867620
77 feet Y = -1237446
73 meter
Z = -13487912
05 Z = -4136569
08
XDOT = -4885
503632 XDOT = -1434
518146
YDOT = -21352
366696 feet/sec YDOT = -6524
547898 meter/sec
ZDOT = 12362
625261 ZDOT = 3761
027885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17359916
95 X = -5291302
69
Y = -2815739
13 feet Y = -858237
29 meter
Z = -13601993
03 Z = -4145887
48
XDOT = -6465
058333 XDOT = -1970
549780
YDOT = -19743
102747 feet/sec YDOT = -6017
697717 meter/sec
ZDOT = 12331
405571 ZDOT = 3758
612418
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 18270
00537823
00016717 00000-0 10270-3 0 9069
2 25544 51
6386 231
3196 0004253 208
7780 151
3140 15
57844359 233
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
00537823 = yrday
fracday
Element set: 906
Inclination: 51
6386 deg
RA of node: 231
3196 deg
Eccentricity:
0004253
Arg of perigee: 208
7780 deg
Mean anomaly: 151
3140 deg
Mean motion: 15
57844359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 23
Checksum: 296
Coasting Arc #8 (Orbit 24)
---------------------------------------
Vector Time (GMT): 2018/270/02:33:28
204
Vector Time (MET): N/A
Weight (LBS) : 35369
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2312410
10 A = 6775874
66 meter
Y = 5846697
77 meter E =
0007463
Z = -2516079
07 I = 51
35776
XDOT = -5574
490429 Wp = 166
11661
YDOT = -60
322692 meter/sec RA = 229
76142 deg
ZDOT = -5273
792841 TA = 42
28699
MA = 42
22947
Ha = 215
018 n
mi
Hp = 209
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7586647
30 X = 2259080
79
Y = 19182079
30 feet Y = 5872258
27 meter
Z = -8254852
58 Z = -2504976
24
XDOT = -18289
010595 XDOT = -5547
783913
YDOT = -197
909095 feet/sec YDOT = -122
511801 meter/sec
ZDOT = -17302
469952 ZDOT = -5300
807281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18720779
46 X = 5706093
58
Y = 8709325
81 feet Y = 2654602
51 meter
Z = -8205609
96 Z = -2501069
92
XDOT = -12721
239147 XDOT = -3877
433692
YDOT = 10960
719695 feet/sec YDOT = 3340
827363 meter/sec
ZDOT = -17423
664060 ZDOT = -5310
732805
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 18270
13367422
00016717 00000-0 10270-3 0 9070
2 25544 51
6404 230
6774 0004374 210
3420 149
7481 15
57846743 252
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
13367422 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 230
6774 deg
Eccentricity:
0004374
Arg of perigee: 210
3420 deg
Mean anomaly: 149
7481 deg
Mean motion: 15
57846743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 25
Checksum: 296
Coasting Arc #9 (Orbit 25)
---------------------------------------
Vector Time (GMT): 2018/270/03:19:51
153
Vector Time (MET): N/A
Weight (LBS) : 35369
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2277698
29 A = 6775742
24 meter
Y = -5839587
48 meter E =
0011090
Z = 2564405
94 I = 51
35860
XDOT = 5605
334895 Wp = 92
31123
YDOT = 123
324884 meter/sec RA = 229
60024 deg
ZDOT = 5239
404237 TA = 296
68773
MA = 296
80123
Ha = 214
974 n
mi
Hp = 209
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7472763
42 X = -2224685
82
Y = -19158751
57 feet Y = -5864761
57 meter
Z = 8413405
33 Z = 2553470
96
XDOT = 18390
206348 XDOT = 5578
088619
YDOT = 404
609200 feet/sec YDOT = 185
855893 meter/sec
ZDOT = 17189
646448 ZDOT = 5266
567195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20008048
10 X = -6098453
06
Y = -4836481
91 feet Y = -1474159
69 meter
Z = 8364914
72 Z = 2549626
01
XDOT = 10473
100638 XDOT = 3192
201074
YDOT = -13270
610255 feet/sec YDOT = -4044
882006 meter/sec
ZDOT = 17311
501004 ZDOT = 5276
545506
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 18270
19782173
00016717 00000-0 10270-3 0 9081
2 25544 51
6410 230
3565 0004281 211
2741 148
8159 15
57858618 264
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
19782173 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 230
3565 deg
Eccentricity:
0004281
Arg of perigee: 211
2741 deg
Mean anomaly: 148
8159 deg
Mean motion: 15
57858618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 26
Checksum: 309
Coasting Arc #10 (Orbit 25)
---------------------------------------
Vector Time (GMT): 2018/270/04:07:35
988
Vector Time (MET): N/A
Weight (LBS) : 35337
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1742148
46 A = 6778949
49 meter
Y = 5789034
32 meter E =
0010554
Z = -3052863
91 I = 51
35443
XDOT = -5853
360083 Wp = 187
95650
YDOT = -816
644667 meter/sec RA = 229
43671 deg
ZDOT = -4897
086490 TA = 27
29380
MA = 27
23838
Ha = 218
799 n
mi
Hp = 211
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5715710
16 X = 1692113
80
Y = 18992894
76 feet Y = 5808236
12 meter
Z = -10015957
71 Z = -3044523
24
XDOT = -19203
937279 XDOT = -5820
005298
YDOT = -2679
280405 feet/sec YDOT = -881
915069 meter/sec
ZDOT = -16066
556727 ZDOT = -4925
439372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19738978
27 X = 6016440
58
Y = 2123459
03 feet Y = 647230
31 meter
Z = -9979101
24 Z = -3041630
06
XDOT = -9795
237721 XDOT = -2985
588457
YDOT = 15079
221418 feet/sec YDOT = 4596
146688 meter/sec
ZDOT = -16193
682624 ZDOT = -4935
834464
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 18270
19784030
00016717 00000-0 10270-3 0 9096
2 25544 51
6400 230
3577 0010692 212
2822 147
7678 15
56346516 262
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
19784030 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 230
3577 deg
Eccentricity:
0010692
Arg of perigee: 212
2822 deg
Mean anomaly: 147
7678 deg
Mean motion: 15
56346516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 26
Checksum: 302
Coasting Arc #11 (Orbit 26)
---------------------------------------
Vector Time (GMT): 2018/270/04:53:56
741
Vector Time (MET): N/A
Weight (LBS) : 35305
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1735372
53 A = 6783180
74 meter
Y = -5787085
13 meter E =
0010942
Z = 3077231
32 I = 51
35499
XDOT = 5863
352455 Wp = 101
97637
YDOT = 840
976436 meter/sec RA = 229
27531 deg
ZDOT = 4871
187414 TA = 293
55143
MA = 293
66633
Ha = 219
605 n
mi
Hp = 214
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5693479
42 X = -1685478
54
Y = -18986499
78 feet Y = -5806211
95 meter
Z = 10095903
28 Z = 3068923
22
XDOT = 19236
720654 XDOT = 5829
850647
YDOT = 2759
109042 feet/sec YDOT = 906
357752 meter/sec
ZDOT = 15981
586005 ZDOT = 4899
588480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19751612
00 X = -6020291
34
Y = 1875264
34 feet Y = 571580
57 meter
Z = 10059192
43 Z = 3066041
85
XDOT = 6641
155363 XDOT = 2024
224155
YDOT = -16760
523824 feet/sec YDOT = -5108
607662 meter/sec
ZDOT = 16108
926019 ZDOT = 4910
000651
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 18270
26211242
00016717 00000-0 10270-3 0 9106
2 25544 51
6401 230
0369 0004204 212
8538 147
2354 15
54872555 273
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
26211242 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 230
0369 deg
Eccentricity:
0004204
Arg of perigee: 212
8538 deg
Mean anomaly: 147
2354 deg
Mean motion: 15
54872555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 27
Checksum: 273
Coasting Arc #12 (Orbit 26)
---------------------------------------
Vector Time (GMT): 2018/270/05:38:34
827
Vector Time (MET): N/A
Weight (LBS) : 35305
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2302670
43 A = 6784365
73 meter
Y = 5827255
64 meter E =
0006888
Z = -2592995
76 I = 51
35905
XDOT = -5612
949045 Wp = 164
24456
YDOT = -102
403494 meter/sec RA = 229
11805 deg
ZDOT = -5224
400150 TA = 45
06753
MA = 45
01167
Ha = 219
617 n
mi
Hp = 214
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7554693
02 X = 2249932
89
Y = 19118292
79 feet Y = 5852710
53 meter
Z = -8507203
95 Z = -2581938
79
XDOT = -18415
187154 XDOT = -5586
009026
YDOT = -335
969470 feet/sec YDOT = -165
021354 meter/sec
ZDOT = -17140
420441 ZDOT = -5251
600851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19152753
57 X = 5837759
29
Y = -7522401
23 feet Y = -2292827
89 meter
Z = -8458163
82 Z = -2578048
33
XDOT = -970
564235 XDOT = -295
827979
YDOT = 16902
425280 feet/sec YDOT = 5151
859225 meter/sec
ZDOT = -17262
447180 ZDOT = -5261
593901
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 18270
26211356
00016717 00000-0 10270-3 0 9113
2 25544 51
6396 230
0375 0004042 211
7962 148
2947 15
54864921 279
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
26211356 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 230
0375 deg
Eccentricity:
0004042
Arg of perigee: 211
7962 deg
Mean anomaly: 148
2947 deg
Mean motion: 15
54864921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 27
Checksum: 296
Coasting Arc #13 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2018/270/06:25:12
857
Vector Time (MET): N/A
Weight (LBS) : 35305
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2212092
37 A = 6784210
01 meter
Y = -5817374
33 meter E =
0011257
Z = 2691137
03 I = 51
35874
XDOT = 5672
154238 Wp = 92
93589
YDOT = 237
297007 meter/sec RA = 228
95656 deg
ZDOT = 5156
158095 TA = 297
60332
MA = 297
71758
Ha = 219
657 n
mi
Hp = 214
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7257520
88 X = -2159948
78
Y = -19085873
77 feet Y = -5841819
62 meter
Z = 8829189
71 Z = 2680518
61
XDOT = 18609
429916 XDOT = 5644
032889
YDOT = 778
533488 feet/sec YDOT = 300
570325 meter/sec
ZDOT = 16916
529183 ZDOT = 5183
643517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17257894
72 X = -5260206
31
Y = 10951542
75 feet Y = 3338030
23 meter
Z = 8782115
89 Z = 2676788
92
XDOT = -2100
932299 XDOT = -640
364165
YDOT = -17026
041311 feet/sec YDOT = -5189
537392 meter/sec
ZDOT = 17039
820483 ZDOT = 5193
737283
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 18270
32638577
00016717 00000-0 10270-3 0 9129
2 25544 51
6393 229
7169 0003888 211
3361 148
7561 15
54844899 288
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
32638577 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 229
7169 deg
Eccentricity:
0003888
Arg of perigee: 211
3361 deg
Mean anomaly: 148
7561 deg
Mean motion: 15
54844899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 28
Checksum: 341
Coasting Arc #14 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2018/270/07:12:07
836
Vector Time (MET): N/A
Weight (LBS) : 35294
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1993532
21 A = 6785244
93 meter
Y = 5796566
67 meter E =
0007462
Z = -2900351
57 I = 51
35909
XDOT = -5780
007514 Wp = 173
87490
YDOT = -516
589155 meter/sec RA = 228
79456 deg
ZDOT = -5013
755137 TA = 39
32588
MA = 39
27172
Ha = 220
864 n
mi
Hp = 215
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6540460
01 X = 1942653
81
Y = 19017607
18 feet Y = 5818574
92 meter
Z = -9515589
13 Z = -2890791
77
XDOT = -18963
279244 XDOT = -5749
446751
YDOT = -1694
846308 feet/sec YDOT = -581
054904 meter/sec
ZDOT = -16449
327877 ZDOT = -5041
758526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14881009
56 X = 4535731
71
Y = -13557517
77 feet Y = -4132331
42 meter
Z = -9473262
52 Z = -2887450
42
XDOT = 4875
277103 XDOT = 1485
984461
YDOT = 16913
348491 feet/sec YDOT = 5155
188620 meter/sec
ZDOT = -16574
916182 ZDOT = -5052
034452
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 18270
32639187
00016717 00000-0 10270-3 0 9138
2 25544 51
6406 229
7172 0006332 211
6038 148
4735 15
54315855 283
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
32639187 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 229
7172 deg
Eccentricity:
0006332
Arg of perigee: 211
6038 deg
Mean anomaly: 148
4735 deg
Mean motion: 15
54315855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 28
Checksum: 305
Coasting Arc #15 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2018/270/07:34:41
670
Vector Time (MET): N/A
Weight (LBS) : 35294
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5033039
94 A = 6779961
44 meter
Y = -214467
47 meter E =
0010666
Z = -4547469
88 I = 51
34168
XDOT = -2498
270637 Wp = 145
62422
YDOT = -6558
627757 meter/sec RA = 228
67020 deg
ZDOT = 3069
243346 TA = 155
27249
MA = 155
22133
Ha = 220
845 n
mi
Hp = 215
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16512598
24 X = -5008178
11
Y = -703633
44 feet Y = -270611
92 meter
Z = -14919520
60 Z = -4571858
58
XDOT = -8196
425975 XDOT = -2439
653547
YDOT = -21517
807602 feet/sec YDOT = -6586
237056 meter/sec
ZDOT = 10069
696016 ZDOT = 3057
250555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7300403
87 X = 2225163
10
Y = 14716953
82 feet Y = 4485727
53 meter
Z = -15028921
09 Z = -4580815
15
XDOT = -13788
519759 XDOT = -4202
740823
YDOT = 17085
686907 feet/sec YDOT = 5207
717369 meter/sec
ZDOT = 10016
527502 ZDOT = 3053
037583
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 18270
32639177
00016717 00000-0 10270-3 0 9148
2 25544 51
6405 229
7173 0006285 212
2949 147
7819 15
54295813 284
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
32639177 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 229
7173 deg
Eccentricity:
0006285
Arg of perigee: 212
2949 deg
Mean anomaly: 147
7819 deg
Mean motion: 15
54295813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 28
Checksum: 326
Coasting Arc #16 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2018/270/07:58:30
243
Vector Time (MET): N/A
Weight (LBS) : 35282
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1997105
37 A = 6786933
85 meter
Y = -5791642
17 meter E =
0011289
Z = 2912789
19 I = 51
35766
XDOT = 5789
665577 Wp = 96
79332
YDOT = 526
896069 meter/sec RA = 228
63292 deg
ZDOT = 4999
218122 TA = 296
55706
MA = 296
67274
Ha = 221
417 n
mi
Hp = 215
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6552182
96 X = -1946342
19
Y = -19001450
70 feet Y = -5813691
03 meter
Z = 9556394
98 Z = 2903211
76
XDOT = 18994
965803 XDOT = 5759
059453
YDOT = 1728
661643 feet/sec YDOT = 591
469564 meter/sec
ZDOT = 16401
634260 ZDOT = 5027
268320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11823705
84 X = -3603865
54
Y = 16278664
55 feet Y = 4961736
95 meter
Z = 9513988
43 Z = 2899863
67
XDOT = -8173
893595 XDOT = -2491
402768
YDOT = -15631
047828 feet/sec YDOT = -4764
343378 meter/sec
ZDOT = 16527
431879 ZDOT = 5037
561237
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 18270
39071092
00016717 00000-0 10270-3 0 9152
2 25544 51
6386 229
3962 0003770 210
7945 149
2986 15
53727720 298
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
39071092 = yrday
fracday
Element set: 915
Inclination: 51
6386 deg
RA of node: 229
3962 deg
Eccentricity:
0003770
Arg of perigee: 210
7945 deg
Mean anomaly: 149
2986 deg
Mean motion: 15
53727720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 29
Checksum: 324
Coasting Arc #17 (Orbit 30)
---------------------------------------
Vector Time (GMT): 2018/270/11:54:38
000
Vector Time (MET): N/A
Weight (LBS) : 35282
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 395751
12 A = 6783208
67 meter
Y = 5363908
44 meter E =
0005034
Z = -4137146
93 I = 51
34768
XDOT = -6233
546900 Wp = 97
28316
YDOT = -2422
229566 meter/sec RA = 227
81410 deg
ZDOT = -3741
315717 TA = 134
04257
MA = 134
00109
Ha = 221
261 n
mi
Hp = 215
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1298396
08 X = 355837
38
Y = 17598124
81 feet Y = 5368110
38 meter
Z = -13573316
70 Z = -4135322
02
XDOT = -20451
269358 XDOT = -6187
823948
YDOT = -7946
947396 feet/sec YDOT = -2491
682176 meter/sec
ZDOT = -12274
657864 ZDOT = -3771
485258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2614284
78 X = -796834
00
Y = -17457188
22 feet Y = -5320950
97 meter
Z = -13565649
63 Z = -4134810
01
XDOT = 19601
584069 XDOT = 5974
562824
YDOT = 6696
383704 feet/sec YDOT = 2041
057753 meter/sec
ZDOT = -12409
781812 ZDOT = -3782
501496
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 18270
51934729
00016717 00000-0 10270-3 0 9162
2 25544 51
6373 228
7552 0003781 214
8401 145
2504 15
53742660 311
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
51934729 = yrday
fracday
Element set: 916
Inclination: 51
6373 deg
RA of node: 228
7552 deg
Eccentricity:
0003781
Arg of perigee: 214
8401 deg
Mean anomaly: 145
2504 deg
Mean motion: 15
53742660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 31
Checksum: 297
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