[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 25th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17491 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 ET - UTC (sec) : 67 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
329/19:38:37
913 5
2 5
8 5
8
N/A -2
1 -0
4 221
6
000/00:15:15
827 -1
6 0
3 215
1
Coasting Arc #1 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2015/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1486290
27 A = 6774138
36 meter
Y = -4085166
51 meter E =
0015040
Z = -5207467
52 I = 51
61993
XDOT = 7471
299136 Wp = 102
05654
YDOT = -1171
461592 meter/sec RA = 358
42646 deg
ZDOT = -1219
481369 TA = 156
26113
MA = 156
19167
Ha = 220
077 n
mi
Hp = 212
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4876280
41 X = -1415201
98
Y = -13402777
27 feet Y = -4101389
47 meter
Z = -17084867
18 Z = -5214515
31
XDOT = 24512
136274 XDOT = 7489
767334
YDOT = -3843
377926 feet/sec YDOT = -1087
809276 meter/sec
ZDOT = -4000
923127 ZDOT = -1183
141633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14116030
70 X = 4302566
16
Y = 1771528
87 feet Y = 539962
00 meter
Z = -17114455
84 Z = -5216486
14
XDOT = -7474
163152 XDOT = -2278
124929
YDOT = 22614
652434 feet/sec YDOT = 6892
946062 meter/sec
ZDOT = -3843
659183 ZDOT = -1171
547319
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 15329
51809983
00016717 00000-0 10270-3 0 9000
2 25544 51
6441 358
8802 0005515 173
0304 187
0927 15
55389118 13140
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
51809983 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 358
8802 deg
Eccentricity:
0005515
Arg of perigee: 173
0304 deg
Mean anomaly: 187
0927 deg
Mean motion: 15
55389118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 314
Coasting Arc #2 (Orbit 1318)
---------------------------------------
Vector Time (GMT): 2015/329/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 69446
59 A = 6777021
14 meter
Y = -4219843
46 meter E =
0013574
Z = -5312348
87 I = 51
60763
XDOT = 7652
739072 Wp = 125
27483
YDOT = -217
571223 meter/sec RA = 356
79575 deg
ZDOT = 265
686606 TA = 147
30346
MA = 147
21937
Ha = 221
593 n
mi
Hp = 215
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 227843
13 X = 142434
70
Y = -13844630
78 feet Y = -4218658
48 meter
Z = -17428966
12 Z = -5311834
45
XDOT = 25107
411653 XDOT = 7653
312600
YDOT = -713
816350 feet/sec YDOT = -131
990053 meter/sec
ZDOT = 871
675218 ZDOT = 302
864306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 301753
74 X = 91974
54
Y = -13847138
82 feet Y = -4220607
91 meter
Z = -17425850
48 Z = -5311399
23
XDOT = 24089
541504 XDOT = 7342
492251
YDOT = -803
867883 feet/sec YDOT = -245
018931 meter/sec
ZDOT = 1032
357189 ZDOT = 314
662471
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 15329
83935194
00016717 00000-0 10270-3 0 9010
2 25544 51
6436 357
2749 0008221 207
5653 152
5065 15
54254430 13196
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
83935194 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 357
2749 deg
Eccentricity:
0008221
Arg of perigee: 207
5653 deg
Mean anomaly: 152
5065 deg
Mean motion: 15
54254430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1319
Checksum: 310
Coasting Arc #3 (Orbit 1334)
---------------------------------------
Vector Time (GMT): 2015/330/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1900671
29 A = 6778519
58 meter
Y = 4232450
85 meter E =
0003698
Z = 4939600
76 I = 51
58083
XDOT = -7311
620358 Wp = 160
11065
YDOT = -712
812112 meter/sec RA = 351
79266 deg
ZDOT = -2205
534369 TA = 311
40464
MA = 311
43642
Ha = 221
355 n
mi
Hp = 215
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6235798
19 X = -1971853
47
Y = 13885993
60 feet Y = 4210797
94 meter
Z = 16206039
24 Z = 4930194
91
XDOT = -23988
255769 XDOT = -7292
392254
YDOT = -2338
622414 feet/sec YDOT = -794
467809 meter/sec
ZDOT = -7236
005147 ZDOT = -2241
006770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6061523
42 X = -1847552
34
Y = 14011014
77 feet Y = 4270557
30 meter
Z = 16164501
36 Z = 4926940
01
XDOT = -22961
608362 XDOT = -6998
698229
YDOT = -1420
029062 feet/sec YDOT = -432
824858 meter/sec
ZDOT = -7389
119746 ZDOT = -2252
203699
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 15330
86809344
00016717 00000-0 10270-3 0 9023
2 25544 51
6432 352
1456 0008170 211
9380 148
1278 15
54300475 13356
Satellite: ISS
Catalog Number: 25544
Epoch time: 15330
86809344 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 352
1456 deg
Eccentricity:
0008170
Arg of perigee: 211
9380 deg
Mean anomaly: 148
1278 deg
Mean motion: 15
54300475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1335
Checksum: 293
Coasting Arc #4 (Orbit 1349)
---------------------------------------
Vector Time (GMT): 2015/331/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3586587
67 A = 6781999
16 meter
Y = -4122919
48 meter E =
0008956
Z = -4024894
58 I = 51
56182
XDOT = 6359
769524 Wp = 167
15452
YDOT = 1701
303233 meter/sec RA = 346
79321 deg
ZDOT = 3917
594397 TA = 143
63416
MA = 143
57327
Ha = 221
173 n
mi
Hp = 215
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11767019
91 X = 3651976
27
Y = -13526638
72 feet Y = -4082445
97 meter
Z = -13205034
71 Z = -4007312
90
XDOT = 20865
385576 XDOT = 6321
242013
YDOT = 5581
703520 feet/sec YDOT = 1772
206646 meter/sec
ZDOT = 12852
999991 ZDOT = 3948
395871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11341081
57 X = 3456761
66
Y = -13958367
57 feet Y = -4254510
43 meter
Z = -13128194
76 Z = -4001473
76
XDOT = 19957
725881 XDOT = 6083
114849
YDOT = 3980
816291 feet/sec YDOT = 1213
352805 meter/sec
ZDOT = 12985
722248 ZDOT = 3958
048141
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 15331
83251955
00016717 00000-0 10270-3 0 9031
2 25544 51
6439 347
3355 0008138 215
1633 144
8983 15
54318016 13501
Satellite: ISS
Catalog Number: 25544
Epoch time: 15331
83251955 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 347
3355 deg
Eccentricity:
0008138
Arg of perigee: 215
1633 deg
Mean anomaly: 144
8983 deg
Mean motion: 15
54318016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1350
Checksum: 306
Coasting Arc #5 (Orbit 1365)
---------------------------------------
Vector Time (GMT): 2015/332/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4922630
04 A = 6785859
03 meter
Y = 3832401
90 meter E =
0012533
Z = 2648644
35 I = 51
54379
XDOT = -4930
862946 Wp = 138
39454
YDOT = -2731
800123 meter/sec RA = 341
80349 deg
ZDOT = -5206
547072 TA = 11
66830
MA = 11
63928
Ha = 221
087 n
mi
Hp = 215
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16150361
01 X = -4977985
26
Y = 12573497
05 feet Y = 3777044
09 meter
Z = 8689778
05 Z = 2624596
80
XDOT = -16177
371869 XDOT = -4874
657150
YDOT = -8962
598829 feet/sec YDOT = -2786
625629 meter/sec
ZDOT = -17081
847349 ZDOT = -5230
364136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15499015
45 X = -4724099
91
Y = 13435639
71 feet Y = 4095182
98 meter
Z = 8585064
77 Z = 2616727
74
XDOT = -15550
997544 XDOT = -4739
944051
YDOT = -6948
398688 feet/sec YDOT = -2117
871920 meter/sec
ZDOT = -17184
173889 ZDOT = -5237
736201
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 15332
86122033
00016717 00000-0 10270-3 0 9040
2 25544 51
6437 342
2057 0008130 218
1674 141
8903 15
54322824 13660
Satellite: ISS
Catalog Number: 25544
Epoch time: 15332
86122033 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 342
2057 deg
Eccentricity:
0008130
Arg of perigee: 218
1674 deg
Mean anomaly: 141
8903 deg
Mean motion: 15
54322824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1366
Checksum: 284
Coasting Arc #6 (Orbit 1380)
---------------------------------------
Vector Time (GMT): 2015/333/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5829788
15 A = 6788189
67 meter
Y = -3336673
36 meter E =
0001889
Z = -972111
63 I = 51
52303
XDOT = 3133
661869 Wp = 21
83235
YDOT = 3758
116029 meter/sec RA = 336
82025 deg
ZDOT = 5898
744714 TA = 327
62563
MA = 327
63722
Ha = 220
728 n
mi
Hp = 215
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19126601
53 X = 5871388
54
Y = -10947091
08 feet Y = -3271248
16 meter
Z = -3189342
62 Z = -943690
68
XDOT = 10281
042878 XDOT = 3062
750758
YDOT = 12329
776998 feet/sec YDOT = 3792
761839 meter/sec
ZDOT = 19352
836989 ZDOT = 5913
795518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18315339
18 X = 5582515
38
Y = -12287658
74 feet Y = -3745278
38 meter
Z = -3065842
30 Z = -934468
73
XDOT = 10116
232379 XDOT = 3083
427629
YDOT = 10238
659587 feet/sec YDOT = 3120
743442 meter/sec
ZDOT = 19417
072248 ZDOT = 5918
323621
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 15333
82560557
00016717 00000-0 10270-3 0 9055
2 25544 51
6444 337
3957 0008134 222
7512 137
3009 15
54391135 13813
Satellite: ISS
Catalog Number: 25544
Epoch time: 15333
82560557 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 337
3957 deg
Eccentricity:
0008134
Arg of perigee: 222
7512 deg
Mean anomaly: 137
3009 deg
Mean motion: 15
54391135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1381
Checksum: 302
Coasting Arc #7 (Orbit 1396)
---------------------------------------
Vector Time (GMT): 2015/334/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6215858
20 A = 6788303
44 meter
Y = 2573799
66 meter E =
0013558
Z = -835030
74 I = 51
49449
XDOT = -1163
489358 Wp = 177
73653
YDOT = -4728
383805 meter/sec RA = 331
83993 deg
ZDOT = -5929
904208 TA = 11
31955
MA = 11
28909
Ha = 220
589 n
mi
Hp = 216
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20393235
58 X = -6240120
80
Y = 8444224
61 feet Y = 2504154
21 meter
Z = -2739602
17 Z = -865285
09
XDOT = -3817
222303 XDOT = -1081
723591
YDOT = -15513
070227 feet/sec YDOT = -4740
937245 meter/sec
ZDOT = -19455
066298 ZDOT = -5935
357859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19546923
61 X = -5957902
32
Y = 10216181
31 feet Y = 3113892
06 meter
Z = -2870857
58 Z = -875037
39
XDOT = -4307
898478 XDOT = -1313
047456
YDOT = -13701
291150 feet/sec YDOT = -4176
153542 meter/sec
ZDOT = -19477
635757 ZDOT = -5936
783379
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 15334
85426396
00016717 00000-0 10270-3 0 9062
2 25544 51
6446 332
2658 0008256 226
0907 133
9565 15
54370757 13970
Satellite: ISS
Catalog Number: 25544
Epoch time: 15334
85426396 = yrday
fracday
Element set: 906
Inclination: 51
6446 deg
RA of node: 332
2658 deg
Eccentricity:
0008256
Arg of perigee: 226
0907 deg
Mean anomaly: 133
9565 deg
Mean motion: 15
54370757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1397
Checksum: 336
Coasting Arc #8 (Orbit 1412)
---------------------------------------
Vector Time (GMT): 2015/335/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6093544
23 A = 6785631
17 meter
Y = -1561291
99 meter E =
0007285
Z = 2541565
72 I = 51
45830
XDOT = -786
287668 Wp = 104
57735
YDOT = 5519
368963 meter/sec RA = 326
85285 deg
ZDOT = 5261
274606 TA = 284
03987
MA = 284
12085
Ha = 220
278 n
mi
Hp = 216
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19991943
01 X = 6098204
08
Y = -5122349
05 feet Y = -1493123
98 meter
Z = 8338470
20 Z = 2571178
33
XDOT = -2579
683949 XDOT = -873
505545
YDOT = 18108
165888 feet/sec YDOT = 5510
088336 meter/sec
ZDOT = 17261
399625 ZDOT = 5257
243299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19284907
98 X = 5878039
95
Y = -7200906
45 feet Y = -2194836
29 meter
Z = 8466734
96 Z = 2580660
82
XDOT = -1285
380703 XDOT = -391
784038
YDOT = 16886
429480 feet/sec YDOT = 5146
983706 meter/sec
ZDOT = 17242
830194 ZDOT = 5255
614643
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 15335
88289951
00016717 00000-0 10270-3 0 9071
2 25544 51
6444 327
1349 0008020 231
1506 128
8932 15
54429868 14137
Satellite: ISS
Catalog Number: 25544
Epoch time: 15335
88289951 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 327
1349 deg
Eccentricity:
0008020
Arg of perigee: 231
1506 deg
Mean anomaly: 128
8932 deg
Mean motion: 15
54429868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1413
Checksum: 322
Coasting Arc #9 (Orbit 1427)
---------------------------------------
Vector Time (GMT): 2015/336/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5489250
99 A = 6781553
47 meter
Y = 284056
00 meter E =
0002602
Z = -3969960
18 I = 51
41843
XDOT = 2558
657529 Wp = 181
49630
YDOT = -6039
121741 meter/sec RA = 321
85466 deg
ZDOT = -3972
446399 TA = 47
00758
MA = 46
98577
Ha = 219
963 n
mi
Hp = 216
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18009353
64 X = -5472734
74
Y = 931942
25 feet Y = 222764
01 meter
Z = -13024803
75 Z = -3996585
89
XDOT = 8394
545700 XDOT = 2645
295041
YDOT = -19813
391539 feet/sec YDOT = -6010
024635 meter/sec
ZDOT = -13032
960626 ZDOT = -3959
806584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17675597
47 X = -5387522
11
Y = 3125270
43 feet Y = 952582
43 meter
Z = -13139892
94 Z = -4005039
37
XDOT = 6207
888563 XDOT = 1892
164434
YDOT = -19416
908472 feet/sec YDOT = -5918
273702 meter/sec
ZDOT = -12977
100009 ZDOT = -3955
420083
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 15336
84722488
00016717 00000-0 10270-3 0 9086
2 25544 51
6440 322
3253 0008211 235
0210 125
0172 15
54461467 14283
Satellite: ISS
Catalog Number: 25544
Epoch time: 15336
84722488 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 322
3253 deg
Eccentricity:
0008211
Arg of perigee: 235
0210 deg
Mean anomaly: 125
0172 deg
Mean motion: 15
54461467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1428
Checksum: 283
Coasting Arc #10 (Orbit 1443)
---------------------------------------
Vector Time (GMT): 2015/337/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4518570
17 A = 6777895
00 meter
Y = 1153308
76 meter E =
0007789
Z = 4922386
48 I = 51
38182
XDOT = -3988
798183 Wp = 190
04768
YDOT = 6161
315690 meter/sec RA = 316
84237 deg
ZDOT = 2210
985193 TA = 238
25069
MA = 238
32661
Ha = 219
810 n
mi
Hp = 216
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14824705
27 X = 4481426
49
Y = 3783821
40 feet Y = 1203630
63 meter
Z = 16149561
93 Z = 4944246
75
XDOT = -13086
608213 XDOT = -4068
139272
YDOT = 20214
290320 feet/sec YDOT = 6116
266654 meter/sec
ZDOT = 7253
888428 ZDOT = 2191
415657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15105784
73 X = 4604243
19
Y = 1689075
06 feet Y = 514830
08 meter
Z = 16243762
94 Z = 4951098
94
XDOT = -10052
988719 XDOT = -3064
150962
YDOT = 20751
620769 feet/sec YDOT = 6325
094010 meter/sec
ZDOT = 7168
075146 ZDOT = 2184
829305
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 15337
87581917
00016717 00000-0 10270-3 0 9091
2 25544 51
6440 317
1945 0008000 238
1746 121
8628 15
54486585 14443
Satellite: ISS
Catalog Number: 25544
Epoch time: 15337
87581917 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 317
1945 deg
Eccentricity:
0008000
Arg of perigee: 238
1746 deg
Mean anomaly: 121
8628 deg
Mean motion: 15
54486585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1444
Checksum: 328
Coasting Arc #11 (Orbit 1458)
---------------------------------------
Vector Time (GMT): 2015/338/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3279475
15 A = 6776111
82 meter
Y = -2683703
38 meter E =
0008479
Z = -5294203
78 I = 51
35260
XDOT = 5008
622429 Wp = 114
20739
YDOT = -5798
317271 meter/sec RA = 311
81901 deg
ZDOT = -166
950770 TA = 154
21543
MA = 154
17314
Ha = 219
515 n
mi
Hp = 216
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10759432
92 X = -3223504
10
Y = -8804801
10 feet Y = -2720063
59 meter
Z = -17369434
97 Z = -5309999
07
XDOT = 16432
488284 XDOT = 5073
899370
YDOT = -19023
350627 feet/sec YDOT = -5741
942560 meter/sec
ZDOT = -547
738746 ZDOT = -142
461189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11897767
40 X = -3626439
50
Y = -7026889
49 feet Y = -2141795
92 meter
Z = -17437119
76 Z = -5314834
10
XDOT = 12735
267012 XDOT = 3881
709385
YDOT = -20498
715146 feet/sec YDOT = -6248
008376 meter/sec
ZDOT = -440
755955 ZDOT = -134
342415
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 15338
84010406
00016717 00000-0 10270-3 0 9101
2 25544 51
6427 312
3834 0008100 242
1775 117
8557 15
54556137 14593
Satellite: ISS
Catalog Number: 25544
Epoch time: 15338
84010406 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 312
3834 deg
Eccentricity:
0008100
Arg of perigee: 242
1775 deg
Mean anomaly: 117
8557 deg
Mean motion: 15
54556137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1459
Checksum: 298
Coasting Arc #12 (Orbit 1474)
---------------------------------------
Vector Time (GMT): 2015/339/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1928396
53 A = 6777261
02 meter
Y = 4127557
16 meter E =
0002703
Z = 5019845
09 I = 51
33632
XDOT = -5572
008105 Wp = 266
47915
YDOT = 4912
165376 meter/sec RA = 306
79468 deg
ZDOT = -1899
554444 TA = 202
01450
MA = 202
02611
Ha = 219
310 n
mi
Hp = 216
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6326760
27 X = 1857713
05
Y = 13541854
21 feet Y = 4148726
44 meter
Z = 16469308
04 Z = 5029041
37
XDOT = -18280
866485 XDOT = -5617
295588
YDOT = 16116
028137 feet/sec YDOT = 4849
602326 meter/sec
ZDOT = -6232
134003 ZDOT = -1926
732374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8480982
22 X = 2585003
38
Y = 12255624
48 feet Y = 3735514
34 meter
Z = 16508192
74 Z = 5031697
15
XDOT = -14267
495852 XDOT = -4348
732736
YDOT = 18422
694003 feet/sec YDOT = 5615
237132 meter/sec
ZDOT = -6350
539611 ZDOT = -1935
644474
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 15339
86865423
00016717 00000-0 10270-3 0 9112
2 25544 51
6430 307
2528 0008182 245
8537 114
1761 15
54584268 14757
Satellite: ISS
Catalog Number: 25544
Epoch time: 15339
86865423 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 307
2528 deg
Eccentricity:
0008182
Arg of perigee: 245
8537 deg
Mean anomaly: 114
1761 deg
Mean motion: 15
54584268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1475
Checksum: 323
Coasting Arc #13 (Orbit 1489)
---------------------------------------
Vector Time (GMT): 2015/340/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -569327
33 A = 6780697
63 meter
Y = -5352865
46 meter E =
0005438
Z = -4126559
38 I = 51
32826
XDOT = 5696
532527 Wp = 184
82529
YDOT = -3499
832963 meter/sec RA = 301
77393 deg
ZDOT = 3748
278790 TA = 123
98287
MA = 123
93119
Ha = 219
167 n
mi
Hp = 216
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1867871
82 X = -489382
42
Y = -17561894
55 feet Y = -5358784
93 meter
Z = -13538580
63 Z = -4129131
08
XDOT = 18689
411179 XDOT = 5717
037163
YDOT = -11482
391610 feet/sec YDOT = -3436
016040 meter/sec
ZDOT = 12297
502592 ZDOT = 3776
001501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5098856
48 X = -1554131
46
Y = -16900865
46 feet Y = -5151383
79 meter
Z = -13548603
63 Z = -4129614
39
XDOT = 14845
937335 XDOT = 4525
041700
YDOT = -14448
716790 feet/sec YDOT = -4403
968878 meter/sec
ZDOT = 12417
967446 ZDOT = 3784
996478
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 15340
83290052
00016717 00000-0 10270-3 0 9122
2 25544 51
6416 302
4408 0008165 249
0077 111
0203 15
54610659 14909
Satellite: ISS
Catalog Number: 25544
Epoch time: 15340
83290052 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 302
4408 deg
Eccentricity:
0008165
Arg of perigee: 249
0077 deg
Mean anomaly: 111
0203 deg
Mean motion: 15
54610659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1490
Checksum: 275
Coasting Arc #14 (Orbit 1505)
---------------------------------------
Vector Time (GMT): 2015/341/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -682483
40 A = 6784619
10 meter
Y = 6175613
94 meter E =
0007308
Z = 2713408
43 I = 51
32651
XDOT = -5445
298681 Wp = 132
64401
YDOT = 1658
808122 meter/sec RA = 296
76573 deg
ZDOT = -5141
020401 TA = 16
51722
MA = 16
49342
Ha = 218
785 n
mi
Hp = 217
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2239118
77 X = -764670
82
Y = 20261200
61 feet Y = 6167522
31 meter
Z = 8902258
64 Z = 2709893
66
XDOT = -17865
153154 XDOT = -5438
469664
YDOT = 5442
283865 feet/sec YDOT = 1597
953606 meter/sec
ZDOT = -16866
864833 ZDOT = -5167
456325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1960771
56 X = 597643
17
Y = 20297229
72 feet Y = 6186595
62 meter
Z = 8885828
74 Z = 2708400
60
XDOT = -14760
198111 XDOT = -4498
908384
YDOT = 8865
808737 feet/sec YDOT = 2702
298503 meter/sec
ZDOT = -16981
395043 ZDOT = -5175
929209
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 15341
86140689
00016717 00000-0 10270-3 0 9137
2 25544 51
6421 297
3098 0008206 254
0347 105
9902 15
54677994 15065
Satellite: ISS
Catalog Number: 25544
Epoch time: 15341
86140689 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 297
3098 deg
Eccentricity:
0008206
Arg of perigee: 254
0347 deg
Mean anomaly: 105
9902 deg
Mean motion: 15
54677994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1506
Checksum: 326
Coasting Arc #15 (Orbit 1520)
---------------------------------------
Vector Time (GMT): 2015/342/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1767361
80 A = 6787415
89 meter
Y = -6479673
81 meter E =
0005992
Z = -951017
43 I = 51
32077
XDOT = 4888
892452 Wp = 343
17083
YDOT = 468
661588 meter/sec RA = 291
76540 deg
ZDOT = 5888
588708 TA = 6
48328
MA = 6
47554
Ha = 218
723 n
mi
Hp = 217
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5798431
09 X = 1844307
49
Y = -21258772
35 feet Y = -6459479
72 meter
Z = -3120135
92 Z = -942245
30
XDOT = 16039
673400 XDOT = 4854
683441
YDOT = 1537
603636 feet/sec YDOT = 523
140779 meter/sec
ZDOT = 19319
516759 ZDOT = 5912
255279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 899018
65 X = 274020
88
Y = -22022534
50 feet Y = -6712468
52 meter
Z = -3080940
24 Z = -939070
58
XDOT = 14249
281621 XDOT = 4343
181038
YDOT = -2137
104065 feet/sec YDOT = -651
389319 meter/sec
ZDOT = 19421
655803 ZDOT = 5919
720689
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 15342
82561387
00016717 00000-0 10270-3 0 9147
2 25544 51
6407 292
4976 0008182 256
0384 103
9859 15
54657238 15211
Satellite: ISS
Catalog Number: 25544
Epoch time: 15342
82561387 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 292
4976 deg
Eccentricity:
0008182
Arg of perigee: 256
0384 deg
Mean anomaly: 103
9859 deg
Mean motion: 15
54657238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1521
Checksum: 332
Coasting Arc #16 (Orbit 1536)
---------------------------------------
Vector Time (GMT): 2015/343/19:46:15
827
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2649180
54 A = 6787237
35 meter
Y = 6170210
72 meter E =
0009277
Z = -944198
29 I = 51
30997
XDOT = -4122
463223 Wp = 191
03695
YDOT = -2671
570562 meter/sec RA = 286
77037 deg
ZDOT = -5891
097157 TA = 359
23923
MA = 359
24065
Ha = 218
295 n
mi
Hp = 217
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8691537
22 X = -2713393
84
Y = 20243473
48 feet Y = 6140226
87 meter
Z = -3097763
43 Z = -957223
15
XDOT = -13525
141808 XDOT = -4063
665560
YDOT = -8764
995282 feet/sec YDOT = -2717
341448 meter/sec
ZDOT = -19327
746578 ZDOT = -5910
980940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3534084
62 X = -1077188
99
Y = 21736875
08 feet Y = 6625399
52 meter
Z = -3155262
84 Z = -961724
11
XDOT = -13534
649368 XDOT = -4125
361127
YDOT = -5018
795976 feet/sec YDOT = -1529
729013 meter/sec
ZDOT = -19413
107075 ZDOT = -5917
115036
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 15343
85407859
00016717 00000-0 10270-3 0 9155
2 25544 51
6409 287
3663 0008093 259
9955 100
0285 15
54713543 15376
Satellite: ISS
Catalog Number: 25544
Epoch time: 15343
85407859 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 287
3663 deg
Eccentricity:
0008093
Arg of perigee: 259
9955 deg
Mean anomaly: 100
0285 deg
Mean motion: 15
54713543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1537
Checksum: 335
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