[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 16th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
349/15:36:09
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
6
351/06:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
6
351/07:21:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
6
351/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 215
8
353/08:43:02
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
6
361/06:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
5
362/01:04:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
5
364/11:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 996)
---------------------------------------
Vector Time (GMT): 2017/349/15:34:47
651
Vector Time (MET): N/A
Weight (LBS) : 903628
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6115030
18 A = 6786486
99 meter
Y = 1562196
23 meter E =
0011377
Z = 2477806
73 I = 51
44016
XDOT = 750
470511 Wp = 114
35327
YDOT = 5493
380197 meter/sec RA = 212
56789 deg
ZDOT = -5300
924258 TA = 37
78516
MA = 37
70534
Ha = 219
877 n
mi
Hp = 215
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20062434
99 X = 6085070
72
Y = 5125315
70 feet Y = 1630410
94 meter
Z = 8129287
19 Z = 2507439
31
XDOT = 2462
173592 XDOT = 714
735815
YDOT = 18022
900908 feet/sec YDOT = 5501
573128 meter/sec
ZDOT = -17391
483786 ZDOT = -5297
364986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11231581
96 X = 3423386
18
Y = 17334037
03 feet Y = 5283414
49 meter
Z = 8260641
36 Z = 2517843
49
XDOT = -9061
013626 XDOT = -2761
796953
YDOT = 14174
428541 feet/sec YDOT = 4320
365819 meter/sec
ZDOT = -17376
455091 ZDOT = -5296
343512
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 17349
68638641
00016717 00000-0 10270-3 0 9003
2 25544 51
6369 213
5241 0003111 247
0362 113
0463 15
54181843 9973
Satellite: ISS
Catalog Number: 25544
Epoch time: 17349
68638641 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 213
5241 deg
Eccentricity:
0003111
Arg of perigee: 247
0362 deg
Mean anomaly: 113
0463 deg
Mean motion: 15
54181843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 997
Checksum: 300
Coasting Arc #2 (Orbit 996)
---------------------------------------
Vector Time (GMT): 2017/349/15:36:09
000
Vector Time (MET): N/A
Weight (LBS) : 903628
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6150126
74 A = 6787324
58 meter
Y = 2001838
21 meter E =
0011853
Z = 2036680
10 I = 51
44307
XDOT = 111
772405 Wp = 121
35905
YDOT = 5307
774834 meter/sec RA = 212
56614 deg
ZDOT = -5536
692422 TA = 36
05331
MA = 35
97343
Ha = 219
877 n
mi
Hp = 215
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20177581
18 X = 6117391
27
Y = 6567710
68 feet Y = 2070429
92 meter
Z = 6682021
34 Z = 2066476
47
XDOT = 366
707364 XDOT = 79
305924
YDOT = 17413
959428 feet/sec YDOT = 5308
843701 meter/sec
ZDOT = -18165
001386 ZDOT = -5536
227856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10454760
06 X = 3186610
86
Y = 18416999
10 feet Y = 5613501
33 meter
Z = 6814040
73 Z = 2076919
61
XDOT = -10027
526913 XDOT = -3056
390203
YDOT = 12433
821688 feet/sec YDOT = 3789
828851 meter/sec
ZDOT = -18163
687607 ZDOT = -5536
291983
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 17349
68638625
00016717 00000-0 10270-3 0 9016
2 25544 51
6369 213
5241 0003099 247
6416 112
4408 15
54189543 9971
Satellite: ISS
Catalog Number: 25544
Epoch time: 17349
68638625 = yrday
fracday
Element set: 901
Inclination: 51
6369 deg
RA of node: 213
5241 deg
Eccentricity:
0003099
Arg of perigee: 247
6416 deg
Mean anomaly: 112
4408 deg
Mean motion: 15
54189543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 997
Checksum: 331
Coasting Arc #3 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2017/350/15:36:09
000
Vector Time (MET): N/A
Weight (LBS) : 903628
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6135022
39 A = 6789135
47 meter
Y = -2873318
05 meter E =
0008625
Z = -369083
78 I = 51
47658
XDOT = 1737
012814 Wp = 35
14912
YDOT = -4467
674603 meter/sec RA = 207
58173 deg
ZDOT = 5984
384976 TA = 320
86365
MA = 320
92600
Ha = 220
040 n
mi
Hp = 215
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20128026
21 X = -6100643
36
Y = -9426896
49 feet Y = -2941731
80 meter
Z = -1210904
78 Z = -398802
84
XDOT = 5698
860938 XDOT = 1757
773025
YDOT = -14657
725076 feet/sec YDOT = -4448
134670 meter/sec
ZDOT = 19633
808977 ZDOT = 5992
872881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8870685
80 X = -2703785
03
Y = -20371028
29 feet Y = -6209089
42 meter
Z = -1342477
81 Z = -409187
24
XDOT = 12379
895783 XDOT = 3773
392235
YDOT = -6672
364479 feet/sec YDOT = -2033
736693 meter/sec
ZDOT = 19672
130180 ZDOT = 5996
065279
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 17350
65089537
00016717 00000-0 10270-3 0 9028
2 25544 51
6365 208
7155 0002916 244
7749 115
3102 15
54169779 10122
Satellite: ISS
Catalog Number: 25544
Epoch time: 17350
65089537 = yrday
fracday
Element set: 902
Inclination: 51
6365 deg
RA of node: 208
7155 deg
Eccentricity:
0002916
Arg of perigee: 244
7749 deg
Mean anomaly: 115
3102 deg
Mean motion: 15
54169779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
Checksum: 314
Coasting Arc #4 (Orbit 1021)
---------------------------------------
Vector Time (GMT): 2017/351/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 903628
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -62796
08 A = 6778101
45 meter
Y = 4452567
82 meter E =
0010690
Z = -5119708
87 I = 51
45937
XDOT = -7246
549061 Wp = 78
49871
YDOT = -1917
166906 meter/sec RA = 204
47996 deg
ZDOT = -1579
176526 TA = 176
22392
MA = 176
21584
Ha = 219
949 n
mi
Hp = 215
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -206023
87 X = -87712
04
Y = 14608162
15 feet Y = 4451726
84 meter
Z = -16796945
11 Z = -5120073
95
XDOT = -23774
767259 XDOT = -7216
901296
YDOT = -6289
917672 feet/sec YDOT = -1998
036828 meter/sec
ZDOT = -5181
025348 ZDOT = -1614
306431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -978260
48 X = -298173
79
Y = -14574237
56 feet Y = -4442227
61 meter
Z = -16799190
99 Z = -5120393
41
XDOT = 23075
507378 XDOT = 7033
414649
YDOT = 4599
913984 feet/sec YDOT = 1402
053782 meter/sec
ZDOT = -5336
776446 ZDOT = -1626
649461
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 17351
29389999
00016717 00000-0 10270-3 0 9035
2 25544 51
6380 205
5137 0002811 256
4363 103
6477 15
54173129 10220
Satellite: ISS
Catalog Number: 25544
Epoch time: 17351
29389999 = yrday
fracday
Element set: 903
Inclination: 51
6380 deg
RA of node: 205
5137 deg
Eccentricity:
0002811
Arg of perigee: 256
4363 deg
Mean anomaly: 103
6477 deg
Mean motion: 15
54173129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 309
Coasting Arc #5 (Orbit 1022)
---------------------------------------
Vector Time (GMT): 2017/351/07:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 903628
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -519609
40 A = 6778659
50 meter
Y = -4579415
79 meter E =
0004755
Z = 4970142
80 I = 51
46284
XDOT = 7236
192845 Wp = 150
61508
YDOT = 1448
212541 meter/sec RA = 204
32846 deg
ZDOT = 2085
966679 TA = 279
00872
MA = 279
06253
Ha = 219
880 n
mi
Hp = 215
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1704755
27 X = -492505
19
Y = -15024330
02 feet Y = -4585075
41 meter
Z = 16306242
80 Z = 4967684
02
XDOT = 23740
790173 XDOT = 7209
328072
YDOT = 4751
353482 feet/sec YDOT = 1528
982158 meter/sec
ZDOT = 6843
722701 ZDOT = 2121
052983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5759707
74 X = 1755558
92
Y = 13992767
11 feet Y = 4264995
42 meter
Z = 16295964
91 Z = 4967010
11
XDOT = -23083
140694 XDOT = -7035
741284
YDOT = 1331
280687 feet/sec YDOT = 405
774353 meter/sec
ZDOT = 6999
346672 ZDOT = 2133
400866
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 17351
35819933
00016717 00000-0 10270-3 0 9049
2 25544 51
6384 205
1940 0002973 255
7050 104
3773 15
54197130 10232
Satellite: ISS
Catalog Number: 25544
Epoch time: 17351
35819933 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 205
1940 deg
Eccentricity:
0002973
Arg of perigee: 255
7050 deg
Mean anomaly: 104
3773 deg
Mean motion: 15
54197130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1023
Checksum: 295
Coasting Arc #6 (Orbit 1024)
---------------------------------------
Vector Time (GMT): 2017/351/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5186760
83 A = 6787795
53 meter
Y = 3928979
25 meter E =
0006431
Z = -1919841
81 I = 51
49841
XDOT = -4318
509891 Wp = 166
99869
YDOT = 2971
843877 meter/sec RA = 203
56972 deg
ZDOT = -5595
021599 TA = 34
20003
MA = 34
15863
Ha = 219
965 n
mi
Hp = 215
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17016931
86 X = 5151766
14
Y = 12890351
88 feet Y = 3986785
70 meter
Z = -6298693
61 Z = -1894730
56
XDOT = -14168
339537 XDOT = -4324
242868
YDOT = 9750
143952 feet/sec YDOT = 2923
519910 meter/sec
ZDOT = -18356
370076 ZDOT = -5616
013297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17866016
36 X = -5445561
79
Y = 11744288
39 feet Y = 3579659
10 meter
Z = -6187716
26 Z = -1886015
92
XDOT = -3613
807131 XDOT = -1101
488414
YDOT = -15201
052555 feet/sec YDOT = -4633
280819 meter/sec
ZDOT = -18450
018016 ZDOT = -5623
565491
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 17351
48680055
00016717 00000-0 10270-3 0 9055
2 25544 51
6395 204
5538 0003070 255
9739 104
1072 15
54136511 10253
Satellite: ISS
Catalog Number: 25544
Epoch time: 17351
48680055 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 204
5538 deg
Eccentricity:
0003070
Arg of perigee: 255
9739 deg
Mean anomaly: 104
1072 deg
Mean motion: 15
54136511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1025
Checksum: 292
Coasting Arc #7 (Orbit 1040)
---------------------------------------
Vector Time (GMT): 2017/352/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4075123
91 A = 6784411
82 meter
Y = -4220636
02 meter E =
0009496
Z = 3399040
00 I = 51
51763
XDOT = 5827
006959 Wp = 91
39365
YDOT = -1905
750571 meter/sec RA = 198
58213 deg
ZDOT = 4608
252083 TA = 308
42786
MA = 308
51307
Ha = 219
908 n
mi
Hp = 215
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13369829
12 X = -4044135
66
Y = -13847231
02 feet Y = -4266033
97 meter
Z = 11151706
04 Z = 3379319
04
XDOT = 19117
476899 XDOT = 5825
499822
YDOT = -6252
462502 feet/sec YDOT = -1840
597960 meter/sec
ZDOT = 15118
937281 ZDOT = 4636
554062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17413557
46 X = 5307652
31
Y = -8318609
10 feet Y = -2535512
06 meter
Z = 11064693
59 Z = 3372518
61
XDOT = -754
411362 XDOT = -229
944583
YDOT = 18748
274634 feet/sec YDOT = 5714
474108 meter/sec
ZDOT = 15244
922050 ZDOT = 4646
652241
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 17352
51560558
00016717 00000-0 10270-3 0 9066
2 25544 51
6394 199
4241 0003017 264
5030 95
5779 15
54161089 10419
Satellite: ISS
Catalog Number: 25544
Epoch time: 17352
51560558 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 199
4241 deg
Eccentricity:
0003017
Arg of perigee: 264
5030 deg
Mean anomaly: 95
5779 deg
Mean motion: 15
54161089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1041
Checksum: 309
Coasting Arc #8 (Orbit 1054)
---------------------------------------
Vector Time (GMT): 2017/353/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1731294
10 A = 6779264
06 meter
Y = -4406734
97 meter E =
0005044
Z = 4850586
15 I = 51
52968
XDOT = 7270
767082 Wp = 139
10690
YDOT = -172
514664 meter/sec RA = 194
05772 deg
ZDOT = 2433
218380 TA = 286
95907
MA = 287
01435
Ha = 219
938 n
mi
Hp = 215
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5680098
75 X = -1705449
88
Y = -14457791
89 feet Y = -4425951
55 meter
Z = 15913996
57 Z = 4842238
33
XDOT = 23854
222709 XDOT = 7260
336440
YDOT = -565
992991 feet/sec YDOT = -91
266583 meter/sec
ZDOT = 7982
999936 ZDOT = 2468
512132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13462927
59 X = 4103500
33
Y = 7823069
97 feet Y = 2384471
73 meter
Z = 15877522
22 Z = 4839468
77
XDOT = -17828
849131 XDOT = -5434
233215
YDOT = 14127
238869 feet/sec YDOT = 4305
982407 meter/sec
ZDOT = 8139
823514 ZDOT = 2481
018207
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 17353
41580868
00016717 00000-0 10270-3 0 9073
2 25544 51
6401 194
9359 0002840 265
5225 94
5603 15
54171814 10555
Satellite: ISS
Catalog Number: 25544
Epoch time: 17353
41580868 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 194
9359 deg
Eccentricity:
0002840
Arg of perigee: 265
5225 deg
Mean anomaly: 94
5603 deg
Mean motion: 15
54171814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1055
Checksum: 312
Coasting Arc #9 (Orbit 1069)
---------------------------------------
Vector Time (GMT): 2017/354/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -61284
67 A = 6777271
62 meter
Y = 4245148
70 meter E =
0011788
Z = -5292893
44 I = 51
55471
XDOT = -7601
312014 Wp = 84
59850
YDOT = -779
397120 meter/sec RA = 189
05290 deg
ZDOT = -537
046279 TA = 180
26534
MA = 180
26596
Ha = 219
818 n
mi
Hp = 215
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -201065
18 X = -83040
33
Y = 13927653
21 feet Y = 4244342
32 meter
Z = -17365135
95 Z = -5293243
50
XDOT = -24938
687711 XDOT = -7589
422946
YDOT = -2557
077165 feet/sec YDOT = -864
333650 meter/sec
ZDOT = -1761
962859 ZDOT = -573
942159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8699765
25 X = -2651688
45
Y = -10874723
66 feet Y = -3314615
77 meter
Z = -17367278
64 Z = -5293546
53
XDOT = 20183
862209 XDOT = 6152
041201
YDOT = -13071
220982 feet/sec YDOT = -3984
108155 meter/sec
ZDOT = -1925
799083 ZDOT = -586
983560
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 17354
38030970
00016717 00000-0 10270-3 0 9085
2 25544 51
6395 190
1279 0002926 270
8621 89
2197 15
54196549 10708
Satellite: ISS
Catalog Number: 25544
Epoch time: 17354
38030970 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 190
1279 deg
Eccentricity:
0002926
Arg of perigee: 270
8621 deg
Mean anomaly: 89
2197 deg
Mean motion: 15
54196549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1070
Checksum: 327
Coasting Arc #10 (Orbit 1085)
---------------------------------------
Vector Time (GMT): 2017/355/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1883099
49 A = 6777707
93 meter
Y = -3969202
69 meter E =
0002771
Z = 5161187
08 I = 51
58956
XDOT = 7355
148046 Wp = 11
00932
YDOT = 1645
526068 meter/sec RA = 184
04821 deg
ZDOT = -1415
306132 TA = 92
62936
MA = 92
59764
Ha = 219
660 n
mi
Hp = 215
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6178147
93 X = 1902273
88
Y = -13022318
54 feet Y = -3948037
91 meter
Z = 16933028
47 Z = 5170380
69
XDOT = 24131
063142 XDOT = 7343
075498
YDOT = 5398
707572 feet/sec YDOT = 1727
709007 meter/sec
ZDOT = -4643
392822 ZDOT = -1379
606495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3722975
15 X = 1134762
83
Y = 13873926
95 feet Y = 4228772
94 meter
Z = 16974432
31 Z = 5173806
97
XDOT = -20966
250343 XDOT = -6390
513105
YDOT = 11124
568876 feet/sec YDOT = 3390
768593 meter/sec
ZDOT = -4484
965402 ZDOT = -1367
017455
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 17355
40910921
00016717 00000-0 10270-3 0 9093
2 25544 51
6400 184
9990 0003110 274
0448 86
0349 15
54217798 10866
Satellite: ISS
Catalog Number: 25544
Epoch time: 17355
40910921 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 184
9990 deg
Eccentricity:
0003110
Arg of perigee: 274
0448 deg
Mean anomaly: 86
0349 deg
Mean motion: 15
54217798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1086
Checksum: 313
Coasting Arc #11 (Orbit 1100)
---------------------------------------
Vector Time (GMT): 2017/356/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3571684
00 A = 6780497
51 meter
Y = 3617374
12 meter E =
0006651
Z = -4493730
67 I = 51
63170
XDOT = -6513
541230 Wp = 115
96200
YDOT = -2437
929317 meter/sec RA = 179
04971 deg
ZDOT = 3215
426698 TA = 186
39413
MA = 186
40262
Ha = 219
776 n
mi
Hp = 215
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11718123
35 X = -3590040
85
Y = 11868025
32 feet Y = 3577330
88 meter
Z = -14743210
86 Z = -4511124
91
XDOT = -21369
885925 XDOT = -6501
414380
YDOT = -7998
455765 feet/sec YDOT = -2510
700676 meter/sec
ZDOT = 10549
300190 ZDOT = 3183
815437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 988516
24 X = 301299
75
Y = -16579713
54 feet Y = -5053496
69 meter
Z = -14821020
24 Z = -4517446
97
XDOT = 20219
631313 XDOT = 6162
943624
YDOT = -8096
942679 feet/sec YDOT = -2467
948128 meter/sec
ZDOT = 10409
128056 ZDOT = 3172
702231
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 17356
37360851
00016717 00000-0 10270-3 0 9103
2 25544 51
6402 180
1900 0003103 279
4571 80
6230 15
54192988 11015
Satellite: ISS
Catalog Number: 25544
Epoch time: 17356
37360851 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 180
1900 deg
Eccentricity:
0003103
Arg of perigee: 279
4571 deg
Mean anomaly: 80
6230 deg
Mean motion: 15
54192988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1101
Checksum: 282
Coasting Arc #12 (Orbit 1116)
---------------------------------------
Vector Time (GMT): 2017/357/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4985330
74 A = 6784276
97 meter
Y = -3165849
92 meter E =
0009601
Z = 3331557
10 I = 51
67707
XDOT = 5165
339253 Wp = 86
44502
YDOT = 3188
039564 meter/sec RA = 174
06364 deg
ZDOT = -4687
690175 TA = 54
77800
MA = 54
68817
Ha = 219
769 n
mi
Hp = 215
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16356071
99 X = 5004178
69
Y = -10386646
72 feet Y = -3109995
41 meter
Z = 10930305
43 Z = 3355819
60
XDOT = 16946
651091 XDOT = 5152
076125
YDOT = 10459
447387 feet/sec YDOT = 3245
728117 meter/sec
ZDOT = -15379
560943 ZDOT = -4662
630762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5160357
70 X = -1572877
03
Y = 18611696
17 feet Y = 5672844
99 meter
Z = 11038594
66 Z = 3364563
65
XDOT = -18311
102150 XDOT = -5581
223935
YDOT = 4002
362868 feet/sec YDOT = 1219
920202 meter/sec
ZDOT = -15268
595513 ZDOT = -4653
867912
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 17357
40240499
00016717 00000-0 10270-3 0 9114
2 25544 51
6399 175
0609 0003056 286
3136 73
7681 15
54215101 11173
Satellite: ISS
Catalog Number: 25544
Epoch time: 17357
40240499 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 175
0609 deg
Eccentricity:
0003056
Arg of perigee: 286
3136 deg
Mean anomaly: 73
7681 deg
Mean motion: 15
54215101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1117
Checksum: 301
Coasting Arc #13 (Orbit 1131)
---------------------------------------
Vector Time (GMT): 2017/358/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5980686
98 A = 6787708
73 meter
Y = 2625669
92 meter E =
0006721
Z = -1832615
35 I = 51
72005
XDOT = -3432
546849 Wp = 13
19083
YDOT = -3880
980029 meter/sec RA = 169
09004 deg
ZDOT = 5652
036826 TA = 326
68029
MA = 326
72258
Ha = 219
843 n
mi
Hp = 215
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19621676
45 X = -6000701
56
Y = 8614402
62 feet Y = 2558677
99 meter
Z = -6012517
56 Z = -1861715
87
XDOT = -11261
636643 XDOT = -3416
348156
YDOT = -12732
874110 feet/sec YDOT = -3919
274892 meter/sec
ZDOT = 18543
427906 ZDOT = 5635
401825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8460434
27 X = 2578740
37
Y = -19648466
23 feet Y = -5988852
51 meter
Z = -6142256
37 Z = -1872159
74
XDOT = 15574
148677 XDOT = 4747
000517
YDOT = 942
730584 feet/sec YDOT = 287
344282 meter/sec
ZDOT = 18469
996022 ZDOT = 5629
654788
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 17358
36690165
00016717 00000-0 10270-3 0 9120
2 25544 51
6394 170
2525 0003175 288
5576 71
5232 15
54173626 11326
Satellite: ISS
Catalog Number: 25544
Epoch time: 17358
36690165 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 170
2525 deg
Eccentricity:
0003175
Arg of perigee: 288
5576 deg
Mean anomaly: 71
5232 deg
Mean motion: 15
54173626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1132
Checksum: 310
Coasting Arc #14 (Orbit 1147)
---------------------------------------
Vector Time (GMT): 2017/359/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6499266
82 A = 6789222
64 meter
Y = -1941698
78 meter E =
0009605
Z = 114081
76 I = 51
75767
XDOT = 1460
253795 Wp = 140
85932
YDOT = 4518
210124 meter/sec RA = 164
12561 deg
ZDOT = -6021
073012 TA = 37
91384
MA = 37
84624
Ha = 219
950 n
mi
Hp = 215
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21323053
88 X = 6519942
23
Y = -6370402
82 feet Y = -1868903
93 meter
Z = 374284
01 Z = 145703
09
XDOT = 4790
858906 XDOT = 1438
868645
YDOT = 14823
524029 feet/sec YDOT = 4534
420415 meter/sec
ZDOT = -19754
176548 ZDOT = -6014
031310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10929825
23 X = -3331410
73
Y = 19382164
06 feet Y = 5907683
61 meter
Z = 515154
42 Z = 157019
07
XDOT = -12415
484786 XDOT = -3784
239763
YDOT = -6459
969583 feet/sec YDOT = -1968
998729 meter/sec
ZDOT = -19723
479312 ZDOT = -6011
716494
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 17359
39569639
00016717 00000-0 10270-3 0 9136
2 25544 51
6402 165
1234 0003130 289
8372 70
2443 15
54161447 11480
Satellite: ISS
Catalog Number: 25544
Epoch time: 17359
39569639 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 165
1234 deg
Eccentricity:
0003130
Arg of perigee: 289
8372 deg
Mean anomaly: 70
2443 deg
Mean motion: 15
54161447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1148
Checksum: 310
Coasting Arc #15 (Orbit 1163)
---------------------------------------
Vector Time (GMT): 2017/360/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6493599
32 A = 6788050
84 meter
Y = 1126948
15 meter E =
0012205
Z = 1595984
74 I = 51
78412
XDOT = 542
013876 Wp = 51
08195
YDOT = -5049
525243 meter/sec RA = 159
16272 deg
ZDOT = 5748
820492 TA = 326
34893
MA = 326
42637
Ha = 219
947 n
mi
Hp = 215
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21304459
72 X = -6513471
02
Y = 3697336
45 feet Y = 1054221
10 meter
Z = 5236170
42 Z = 1564392
76
XDOT = 1778
260748 XDOT = 570
513906
YDOT = -16566
683868 feet/sec YDOT = -5043
304982 meter/sec
ZDOT = 18860
959621 ZDOT = 5751
522408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12495301
50 X = 3808567
90
Y = -17688155
61 feet Y = -5391349
83 meter
Z = 5095524
77 Z = 1553115
95
XDOT = 9238
200182 XDOT = 2815
803415
YDOT = 11984
494603 feet/sec YDOT = 3652
873955 meter/sec
ZDOT = 18873
663341 ZDOT = 5752
692586
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 17360
42448642
00016717 00000-0 10270-3 0 9143
2 25544 51
6388 159
9932 0003178 294
6467 65
4355 15
54217620 11641
Satellite: ISS
Catalog Number: 25544
Epoch time: 17360
42448642 = yrday
fracday
Element set: 914
Inclination: 51
6388 deg
RA of node: 159
9932 deg
Eccentricity:
0003178
Arg of perigee: 294
6467 deg
Mean anomaly: 65
4355 deg
Mean motion: 15
54217620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1164
Checksum: 328
Coasting Arc #16 (Orbit 1177)
---------------------------------------
Vector Time (GMT): 2017/361/06:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 940029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 792163
91 A = 6778872
92 meter
Y = -4634142
20 meter E =
0005919
Z = 4882957
76 I = 51
78300
XDOT = 7163
704233 Wp = 30
93167
YDOT = -1312
600354 meter/sec RA = 154
56733 deg
ZDOT = -2401
638184 TA = 82
59291
MA = 82
52565
Ha = 219
924 n
mi
Hp = 215
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2598962
95 X = 820206
28
Y = -15203878
60 feet Y = -4625127
12 meter
Z = 16020202
63 Z = 4886873
73
XDOT = 23502
966645 XDOT = 7189
515626
YDOT = -4306
431606 feet/sec YDOT = -1232
346477 meter/sec
ZDOT = -7879
390366 ZDOT = -2366
776548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1813898
26 X = 552876
19
Y = 15298483
98 feet Y = 4662977
92 meter
Z = 16038253
84 Z = 4888459
77
XDOT = -20324
897112 XDOT = -6195
028640
YDOT = 10529
000220 feet/sec YDOT = 3209
239267 meter/sec
ZDOT = -7724
162139 ZDOT = -2354
324620
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 17361
32467922
00016717 00000-0 10270-3 0 9156
2 25544 51
6402 155
5071 0003233 299
6407 60
4423 15
54236899 11780
Satellite: ISS
Catalog Number: 25544
Epoch time: 17361
32467922 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 155
5071 deg
Eccentricity:
0003233
Arg of perigee: 299
6407 deg
Mean anomaly: 60
4423 deg
Mean motion: 15
54236899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1178
Checksum: 310
Coasting Arc #17 (Orbit 1189)
---------------------------------------
Vector Time (GMT): 2017/362/01:04:30
000
Vector Time (MET): N/A
Weight (LBS) : 925596
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3750215
08 A = 6778230
83 meter
Y = -2476894
83 meter E =
0002443
Z = 5072773
33 I = 51
80070
XDOT = 5672
180601 Wp = 129
15479
YDOT = -4824
870390 meter/sec RA = 150
79822 deg
ZDOT = 1835
399508 TA = 303
10427
MA = 303
12771
Ha = 220
123 n
mi
Hp = 215
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12303855
26 X = -3746880
11
Y = -8126295
37 feet Y = -2518813
93 meter
Z = 16642957
10 Z = 5054563
90
XDOT = 18609
516408 XDOT = 5716
796557
YDOT = -15829
627265 feet/sec YDOT = -4761
190824 meter/sec
ZDOT = 6021
651928 ZDOT = 1863
061318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2894753
96 X = -882321
01
Y = 14550602
16 feet Y = 4435023
54 meter
Z = 16562304
44 Z = 5048190
39
XDOT = -20562
741643 XDOT = -6267
523653
YDOT = -11093
684106 feet/sec YDOT = -3381
354916 meter/sec
ZDOT = 6145
354440 ZDOT = 1873
104033
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 17362
09627261
00016717 00000-0 10270-3 0 9166
2 25544 51
6379 151
6590 0003163 301
1143 58
9699 15
54224567 11904
Satellite: ISS
Catalog Number: 25544
Epoch time: 17362
09627261 = yrday
fracday
Element set: 916
Inclination: 51
6379 deg
RA of node: 151
6590 deg
Eccentricity:
0003163
Arg of perigee: 301
1143 deg
Mean anomaly: 58
9699 deg
Mean motion: 15
54224567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1190
Checksum: 314
Coasting Arc #18 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2017/363/01:04:30
000
Vector Time (MET): N/A
Weight (LBS) : 925596
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2253341
43 A = 6777172
80 meter
Y = 3538462
98 meter E =
0012509
Z = -5333425
91 I = 51
82530
XDOT = -6384
071370 Wp = 82
26766
YDOT = 4230
969950 meter/sec RA = 145
80922 deg
ZDOT = 111
669112 TA = 188
78401
MA = 188
80592
Ha = 220
194 n
mi
Hp = 215
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7392852
46 X = 2239513
13
Y = 11609130
50 feet Y = 3563584
45 meter
Z = -17498116
52 Z = -5322513
19
XDOT = -20945
116044 XDOT = -6431
451171
YDOT = 13881
135008 feet/sec YDOT = 4159
313972 meter/sec
ZDOT = 366
368479 ZDOT = 80
542432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7763275
85 X = 2366246
48
Y = -11438402
34 feet Y = -3486425
03 meter
Z = -17450064
76 Z = -5318779
74
XDOT = 20113
769592 XDOT = 6130
676972
YDOT = 13313
844267 feet/sec YDOT = 4058
059733 meter/sec
ZDOT = 227
313620 ZDOT = 69
285191
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 17363
06076187
00016717 00000-0 10270-3 0 9170
2 25544 51
6381 146
8494 0003137 307
5170 52
5697 15
54192084 12050
Satellite: ISS
Catalog Number: 25544
Epoch time: 17363
06076187 = yrday
fracday
Element set: 917
Inclination: 51
6381 deg
RA of node: 146
8494 deg
Eccentricity:
0003137
Arg of perigee: 307
5170 deg
Mean anomaly: 52
5697 deg
Mean motion: 15
54192084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 314
Coasting Arc #19 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2017/364/01:04:30
000
Vector Time (MET): N/A
Weight (LBS) : 925596
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -694356
07 A = 6778503
37 meter
Y = -4510821
50 meter E =
0006027
Z = 5011202
95 I = 51
85630
XDOT = 6608
496750 Wp = 26
44689
YDOT = -3305
121095 meter/sec RA = 140
82406 deg
ZDOT = -2053
207081 TA = 83
49021
MA = 83
42160
Ha = 220
307 n
mi
Hp = 215
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2278071
08 X = -668205
24
Y = -14799283
14 feet Y = -4518440
52 meter
Z = 16440954
57 Z = 5007893
08
XDOT = 21681
419782 XDOT = 6654
937833
YDOT = -10843
573147 feet/sec YDOT = -3230
960505 meter/sec
ZDOT = -6736
243704 ZDOT = -2020
992506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12558568
62 X = -3827851
72
Y = 8182532
20 feet Y = 2494035
81 meter
Z = 16426865
12 Z = 5006908
49
XDOT = -18126
403007 XDOT = -5524
927636
YDOT = -14544
801642 feet/sec YDOT = -4433
255540 meter/sec
ZDOT = -6592
453911 ZDOT = -2009
379952
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 17364
08954826
00016717 00000-0 10270-3 0 9189
2 25544 51
6380 141
7209 0003131 313
0844 47
0047 15
54192632 12216
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
08954826 = yrday
fracday
Element set: 918
Inclination: 51
6380 deg
RA of node: 141
7209 deg
Eccentricity:
0003131
Arg of perigee: 313
0844 deg
Mean anomaly: 47
0047 deg
Mean motion: 15
54192632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 289
Coasting Arc #20 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2017/364/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 925596
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3592066
53 A = 6777483
77 meter
Y = -2331643
21 meter E =
0000885
Z = 5252415
06 I = 51
86382
XDOT = 5138
569074 Wp = 111
81033
YDOT = -5600
006184 meter/sec RA = 138
63427 deg
ZDOT = 1027
804330 TA = 328
37708
MA = 328
38240
Ha = 220
294 n
mi
Hp = 215
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11784995
19 X = -3591240
17
Y = -7649748
06 feet Y = -2371808
08 meter
Z = 17232332
86 Z = 5234967
66
XDOT = 16858
822422 XDOT = 5195
815368
YDOT = -18372
723701 feet/sec YDOT = -5542
223213 meter/sec
ZDOT = 3372
061449 ZDOT = 1052
904388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6693532
28 X = 2040188
64
Y = -12460315
25 feet Y = -3797904
09 meter
Z = 17155034
90 Z = 5228854
64
XDOT = 18725
238951 XDOT = 5707
452832
YDOT = 14858
471345 feet/sec YDOT = 4528
862066 meter/sec
ZDOT = 3484
533713 ZDOT = 1062
085876
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 17364
53964146
00016717 00000-0 10270-3 0 9196
2 25544 51
6376 139
4724 0002875 306
5492 53
5396 15
54210039 12285
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
53964146 = yrday
fracday
Element set: 919
Inclination: 51
6376 deg
RA of node: 139
4724 deg
Eccentricity:
0002875
Arg of perigee: 306
5492 deg
Mean anomaly: 53
5396 deg
Mean motion: 15
54210039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1228
Checksum: 325
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