[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 17th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
200/11:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 212
7
201/17:45:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 212
7
209/14:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 212
4
212/23:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 212
2
Coasting Arc #1 (Orbit 2645)
---------------------------------------
Vector Time (GMT): 2017/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4073830
98 A = 6777354
37 meter
Y = 1261016
42 meter E =
0018945
Z = -5283439
54 I = 51
27478
XDOT = -2759
159706 Wp = 79
39606
YDOT = -7127
389960 meter/sec RA = 246
24520 deg
ZDOT = 431
092960 TA = 194
71581
MA = 194
77103
Ha = 222
749 n
mi
Hp = 212
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13365587
21 X = -4061964
94
Y = 4137192
99 feet Y = 1215526
80 meter
Z = -17334119
22 Z = -5303199
99
XDOT = -9052
361240 XDOT = -2681
348319
YDOT = -23383
825327 feet/sec YDOT = -7157
809717 meter/sec
ZDOT = 1414
346982 ZDOT = 417
878335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9283612
71 X = 2829645
16
Y = 10321355
55 feet Y = 3145949
17 meter
Z = -17421570
86 Z = -5310094
80
XDOT = -16724
694407 XDOT = -5097
686855
YDOT = 17307
735470 feet/sec YDOT = 5275
397771 meter/sec
ZDOT = 1357
135935 ZDOT = 413
655033
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 17198
51539231
00016717 00000-0 10270-3 0 9002
2 25544 51
6401 247
1538 0005822 41
3984 318
7609 15
54149706 26469
Satellite: ISS
Catalog Number: 25544
Epoch time: 17198
51539231 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 247
1538 deg
Eccentricity:
0005822
Arg of perigee: 41
3984 deg
Mean anomaly: 318
7609 deg
Mean motion: 15
54149706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2646
Checksum: 315
Coasting Arc #2 (Orbit 2661)
---------------------------------------
Vector Time (GMT): 2017/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4694022
57 A = 6778947
17 meter
Y = 449460
82 meter E =
0012471
Z = 4864314
15 I = 51
29386
XDOT = 1757
096513 Wp = 52
66306
YDOT = 7093
110430 meter/sec RA = 241
22230 deg
ZDOT = -2339
403972 TA = 60
39759
MA = 60
27340
Ha = 222
609 n
mi
Hp = 212
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15400336
53 X = 4665019
32
Y = 1474608
98 feet Y = 501789
97 meter
Z = 15959035
91 Z = 4887045
80
XDOT = 5764
752338 XDOT = 1689
012544
YDOT = 23271
359677 feet/sec YDOT = 7112
379002 meter/sec
ZDOT = -7675
209881 ZDOT = -2331
033296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5283782
22 X = -1610496
82
Y = -14429651
13 feet Y = -4398157
66 meter
Z = 16059342
39 Z = 4894887
56
XDOT = 17415
256584 XDOT = 5308
170207
YDOT = -14921
219026 feet/sec YDOT = -4547
987559 meter/sec
ZDOT = -7639
368230 ZDOT = -2328
479437
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 17199
54419415
00016717 00000-0 10270-3 0 9018
2 25544 51
6392 242
0255 0005827 45
3567 314
8060 15
54197938 26620
Satellite: ISS
Catalog Number: 25544
Epoch time: 17199
54419415 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 242
0255 deg
Eccentricity:
0005827
Arg of perigee: 45
3567 deg
Mean anomaly: 314
8060 deg
Mean motion: 15
54197938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2662
Checksum: 322
Coasting Arc #3 (Orbit 2676)
---------------------------------------
Vector Time (GMT): 2017/200/11:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4617083
06 A = 6778651
12 meter
Y = 256713
78 meter E =
0016685
Z = -4970807
56 I = 51
30977
XDOT = -2609
573565 Wp = 88
20792
YDOT = -6892
568222 meter/sec RA = 236
23512 deg
ZDOT = 2074
478924 TA = 202
06785
MA = 202
13977
Ha = 222
839 n
mi
Hp = 212
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15147910
31 X = -4595464
90
Y = 842236
81 feet Y = 205203
83 meter
Z = -16308423
74 Z = -4993183
31
XDOT = -8561
593060 XDOT = -2542
381866
YDOT = -22613
412802 feet/sec YDOT = -6921
374773 meter/sec
ZDOT = 6806
033214 ZDOT = 2061
964934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7171865
61 X = 2185984
64
Y = 13247593
87 feet Y = 4037866
61 meter
Z = -16407279
94 Z = -5000938
92
XDOT = -15821
212291 XDOT = -4822
305506
YDOT = 16900
866104 feet/sec YDOT = 5151
383989 meter/sec
ZDOT = 6751
849226 ZDOT = 2057
963644
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 17200
50869503
00016717 00000-0 10270-3 0 9025
2 25544 51
6400 237
2168 0005924 48
5888 311
5773 15
54164339 26778
Satellite: ISS
Catalog Number: 25544
Epoch time: 17200
50869503 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 237
2168 deg
Eccentricity:
0005924
Arg of perigee: 48
5888 deg
Mean anomaly: 311
5773 deg
Mean motion: 15
54164339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2677
Checksum: 317
Coasting Arc #4 (Orbit 2692)
---------------------------------------
Vector Time (GMT): 2017/201/11:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5242499
39 A = 6781852
13 meter
Y = 1295898
71 meter E =
0016125
Z = 4093860
91 I = 51
33931
XDOT = 1358
689922 Wp = 67
70031
YDOT = 6531
416819 meter/sec RA = 231
22039 deg
ZDOT = -3789
401662 TA = 61
61666
MA = 61
45419
Ha = 222
762 n
mi
Hp = 212
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17199801
14 X = 5207732
85
Y = 4251636
19 feet Y = 1354329
02 meter
Z = 13431302
21 Z = 4119242
89
XDOT = 4457
644101 XDOT = 1303
959840
YDOT = 21428
532872 feet/sec YDOT = 6546
305047 meter/sec
ZDOT = -12432
420151 ZDOT = -3782
933768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3743739
70 X = -1141091
86
Y = -17230072
85 feet Y = -5251726
20 meter
Z = 13543206
84 Z = 4127969
44
XDOT = 15961
796513 XDOT = 4865
155577
YDOT = -13264
704529 feet/sec YDOT = -4043
081941 meter/sec
ZDOT = -12404
867649 ZDOT = -3781
003660
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 17201
53749030
00016717 00000-0 10270-3 0 9032
2 25544 51
6394 232
0882 0006023 52
1764 307
9931 15
54212424 26933
Satellite: ISS
Catalog Number: 25544
Epoch time: 17201
53749030 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 232
0882 deg
Eccentricity:
0006023
Arg of perigee: 52
1764 deg
Mean anomaly: 307
9931 deg
Mean motion: 15
54212424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2693
Checksum: 289
Coasting Arc #5 (Orbit 2696)
---------------------------------------
Vector Time (GMT): 2017/201/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 50278
77 A = 6781325
86 meter
Y = -5258377
01 meter E =
0014153
Z = 4269007
65 I = 51
34164
XDOT = 6148
225238 Wp = 87
02791
YDOT = 2936
306435 meter/sec RA = 230
05026 deg
ZDOT = 3534
972437 TA = 326
78797
MA = 326
87673
Ha = 222
798 n
mi
Hp = 212
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 164956
60 X = 88339
02
Y = -17251893
06 feet Y = -5257602
46 meter
Z = 14005930
62 Z = 4269343
70
XDOT = 20171
342645 XDOT = 6097
762718
YDOT = 9633
551295 feet/sec YDOT = 3004
777483 meter/sec
ZDOT = 11597
678600 ZDOT = 3564
716161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7006289
70 X = 2135517
10
Y = 15763962
63 feet Y = 4804855
81 meter
Z = 14008229
88 Z = 4269708
47
XDOT = -21129
030418 XDOT = -6440
128471
YDOT = -1059
004948 feet/sec YDOT = -322
784708 meter/sec
ZDOT = 11728
598474 ZDOT = 3574
876815
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 17201
79468917
00016717 00000-0 10270-3 0 9043
2 25544 51
6387 230
8063 0005932 51
7991 308
3695 15
54215848 26976
Satellite: ISS
Catalog Number: 25544
Epoch time: 17201
79468917 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 230
8063 deg
Eccentricity:
0005932
Arg of perigee: 51
7991 deg
Mean anomaly: 308
3695 deg
Mean motion: 15
54215848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2697
Checksum: 343
Coasting Arc #6 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2017/202/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1439004
93 A = 6778261
94 meter
Y = 4289774
10 meter E =
0018958
Z = -5064197
56 I = 51
35223
XDOT = -6169
470025 Wp = 69
92676
YDOT = -4167
342194 meter/sec RA = 225
03535 deg
ZDOT = -1776
049156 TA = 182
78388
MA = 182
79445
Ha = 222
949 n
mi
Hp = 212
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4721144
78 X = -1462268
31
Y = 14074061
99 feet Y = 4273552
70 meter
Z = -16614821
39 Z = -5071243
69
XDOT = -20241
043390 XDOT = -6113
784121
YDOT = -13672
382526 feet/sec YDOT = -4236
021821 meter/sec
ZDOT = -5826
932925 ZDOT = -1805
883388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1816379
52 X = -553632
48
Y = -14697346
94 feet Y = -4479751
35 meter
Z = -16646605
57 Z = -5073885
38
XDOT = 23029
093691 XDOT = 7019
267757
YDOT = 3905
737092 feet/sec YDOT = 1190
468666 meter/sec
ZDOT = -5958
087593 ZDOT = -1816
025098
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 17202
75918419
00016717 00000-0 10270-3 0 9058
2 25544 51
6380 225
9977 0006098 54
9009 305
2715 15
54195156 27123
Satellite: ISS
Catalog Number: 25544
Epoch time: 17202
75918419 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 225
9977 deg
Eccentricity:
0006098
Arg of perigee: 54
9009 deg
Mean anomaly: 305
2715 deg
Mean motion: 15
54195156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 325
Coasting Arc #7 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2017/203/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2860773
08 A = 6777065
80 meter
Y = -3115979
27 meter E =
0008141
Z = 5288505
83 I = 51
37258
XDOT = 5791
460661 Wp = 65
20012
YDOT = 5033
305916 meter/sec RA = 220
01695 deg
ZDOT = -163
673514 TA = 26
38487
MA = 26
34344
Ha = 222
745 n
mi
Hp = 212
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9385738
47 X = 2869715
68
Y = -10223029
09 feet Y = -3083938
74 meter
Z = 17350740
92 Z = 5302423
71
XDOT = 19000
855186 XDOT = 5735
541507
YDOT = 16513
470853 feet/sec YDOT = 5097
757315 meter/sec
ZDOT = -536
986595 ZDOT = -135
676167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3811731
57 X = -1161815
78
Y = 13263448
06 feet Y = 4042698
97 meter
Z = 17412704
25 Z = 5307392
25
XDOT = -23372
518207 XDOT = -7123
943550
YDOT = -6158
109510 feet/sec YDOT = -1876
991779 meter/sec
ZDOT = -414
051177 ZDOT = -126
202799
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 17203
78797372
00016717 00000-0 10270-3 0 9066
2 25544 51
6382 220
8694 0005900 57
2705 302
9016 15
54225249 27287
Satellite: ISS
Catalog Number: 25544
Epoch time: 17203
78797372 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 220
8694 deg
Eccentricity:
0005900
Arg of perigee: 57
2705 deg
Mean anomaly: 302
9016 deg
Mean motion: 15
54225249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 317
Coasting Arc #8 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2017/204/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4209942
93 A = 6778535
63 meter
Y = 1901202
71 meter E =
0017592
Z = -4976299
87 I = 51
40333
XDOT = -4926
739875 Wp = 91
60085
YDOT = -5477
549132 meter/sec RA = 214
99894 deg
ZDOT = 2081
217427 TA = 198
72200
MA = 198
78678
Ha = 222
978 n
mi
Hp = 212
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13812148
73 X = -4206717
90
Y = 6237541
69 feet Y = 1854142
75 meter
Z = -16326443
13 Z = -4996742
02
XDOT = -16163
844733 XDOT = -4875
231624
YDOT = -17970
961718 feet/sec YDOT = -5532
355469 meter/sec
ZDOT = 6828
141164 ZDOT = 2057
409983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9346547
51 X = 2848827
68
Y = -11804974
46 feet Y = -3598156
21 meter
Z = -16417056
74 Z = -5003918
89
XDOT = 21763
680501 XDOT = 6633
569817
YDOT = 7907
463961 feet/sec YDOT = 2410
195015 meter/sec
ZDOT = 6723
758072 ZDOT = 2049
401460
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 17204
75246224
00016717 00000-0 10270-3 0 9070
2 25544 51
6386 216
0598 0006094 61
1448 299
0316 15
54200760 27431
Satellite: ISS
Catalog Number: 25544
Epoch time: 17204
75246224 = yrday
fracday
Element set: 907
Inclination: 51
6386 deg
RA of node: 216
0598 deg
Eccentricity:
0006094
Arg of perigee: 61
1448 deg
Mean anomaly: 299
0316 deg
Mean motion: 15
54200760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 305
Coasting Arc #9 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2017/205/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5356573
04 A = 6781890
14 meter
Y = -676321
92 meter E =
0016477
Z = 4094011
80 I = 51
44160
XDOT = 3625
808593 Wp = 72
46182
YDOT = 5592
300577 meter/sec RA = 209
99127 deg
ZDOT = -3802
620924 TA = 56
94332
MA = 56
78517
Ha = 222
929 n
mi
Hp = 212
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17574058
54 X = 5343851
50
Y = -2218903
93 feet Y = -616492
48 meter
Z = 13431797
24 Z = 4120000
83
XDOT = 11895
697485 XDOT = 3581
475378
YDOT = 18347
442837 feet/sec YDOT = 5632
599194 meter/sec
ZDOT = -12475
790432 ZDOT = -3785
115589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14371425
66 X = -4380410
54
Y = 10204502
75 feet Y = 3110332
44 meter
Z = 13546752
15 Z = 4129050
05
XDOT = -18471
501552 XDOT = -5630
113673
YDOT = -9478
174758 feet/sec YDOT = -2888
947666 meter/sec
ZDOT = -12399
250070 ZDOT = -3779
291421
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 17205
78124664
00016717 00000-0 10270-3 0 9088
2 25544 51
6383 210
9312 0006116 65
1568 295
0220 15
54197320 27591
Satellite: ISS
Catalog Number: 25544
Epoch time: 17205
78124664 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 210
9312 deg
Eccentricity:
0006116
Arg of perigee: 65
1568 deg
Mean anomaly: 295
0220 deg
Mean motion: 15
54197320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 303
Coasting Arc #10 (Orbit 2773)
---------------------------------------
Vector Time (GMT): 2017/206/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6162758
94 A = 6785623
48 meter
Y = -402200
50 meter E =
0010662
Z = -2813779
78 I = 51
48379
XDOT = -1962
950860 Wp = 66
27931
YDOT = -5383
346391 meter/sec RA = 204
99506 deg
ZDOT = 5088
264841 TA = 261
72252
MA = 261
84343
Ha = 222
951 n
mi
Hp = 212
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20219025
40 X = -6144135
74
Y = -1319555
44 feet Y = -471012
41 meter
Z = -9231560
97 Z = -2843670
69
XDOT = -6440
127493 XDOT = -1927
322724
YDOT = -17661
897609 feet/sec YDOT = -5405
098435 meter/sec
ZDOT = 16693
782287 ZDOT = 5078
815961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18250609
87 X = 5562785
89
Y = -8660822
19 feet Y = -2639818
60 meter
Z = -9363617
42 Z = -2854030
59
XDOT = 13687
233341 XDOT = 4171
868722
YDOT = 10906
657492 feet/sec YDOT = 3324
349204 meter/sec
ZDOT = 16652
800124 ZDOT = 5075
773478
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 17206
74572948
00016717 00000-0 10270-3 0 9098
2 25544 51
6391 206
1224 0006026 68
5034 291
6761 15
54213673 27743
Satellite: ISS
Catalog Number: 25544
Epoch time: 17206
74572948 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 206
1224 deg
Eccentricity:
0006026
Arg of perigee: 68
5034 deg
Mean anomaly: 291
6761 deg
Mean motion: 15
54213673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2774
Checksum: 315
Coasting Arc #11 (Orbit 2789)
---------------------------------------
Vector Time (GMT): 2017/207/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6534305
11 A = 6788503
57 meter
Y = 1385230
98 meter E =
0018257
Z = 1175765
55 I = 51
52413
XDOT = 15
052022 Wp = 107
60961
YDOT = 4956
271825 meter/sec RA = 200
01096 deg
ZDOT = -5853
293977 TA = 59
59666
MA = 59
41635
Ha = 223
040 n
mi
Hp = 212
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21438008
89 X = 6512618
27
Y = 4544721
08 feet Y = 1458180
74 meter
Z = 3857498
52 Z = 1207453
93
XDOT = 49
383275 XDOT = -11
939550
YDOT = 16260
734334 feet/sec YDOT = 4956
289353 meter/sec
ZDOT = -19203
720396 ZDOT = -5853
286311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20801920
65 X = -6340425
41
Y = 6813523
72 feet Y = 2076762
03 meter
Z = 3997374
34 Z = 1218399
70
XDOT = -7813
578957 XDOT = -2381
578866
YDOT = -12458
960977 feet/sec YDOT = -3797
491306 meter/sec
ZDOT = -19204
397342 ZDOT = -5853
500310
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 17207
77450794
00016717 00000-0 10270-3 0 9108
2 25544 51
6401 200
9931 0006030 72
6283 287
5529 15
54197222 27904
Satellite: ISS
Catalog Number: 25544
Epoch time: 17207
77450794 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 200
9931 deg
Eccentricity:
0006030
Arg of perigee: 72
6283 deg
Mean anomaly: 287
5529 deg
Mean motion: 15
54197222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2790
Checksum: 306
Coasting Arc #12 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2017/208/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6405873
58 A = 6788996
59 meter
Y = -2159840
70 meter E =
0018674
Z = 534566
24 I = 51
55711
XDOT = 1987
214696 Wp = 58
42346
YDOT = -4378
887880 meter/sec RA = 195
03346 deg
ZDOT = 5976
831944 TA = 307
35297
MA = 307
52293
Ha = 223
054 n
mi
Hp = 212
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21016645
61 X = -6383842
20
Y = -7086091
53 feet Y = -2231352
35 meter
Z = 1753826
23 Z = 503502
46
XDOT = 6519
733255 XDOT = 2007
000822
YDOT = -14366
430051 feet/sec YDOT = -4356
554934 meter/sec
ZDOT = 19609
028687 ZDOT = 5986
533070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21664982
71 X = 6603486
73
Y = -4796087
51 feet Y = -1461847
47 meter
Z = 1616805
78 Z = 492802
40
XDOT = 1599
021390 XDOT = 487
381720
YDOT = 14021
296405 feet/sec YDOT = 4273
691144 meter/sec
ZDOT = 19652
538454 ZDOT = 5990
093721
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 17208
80328277
00016717 00000-0 10270-3 0 9114
2 25544 51
6405 195
8639 0006089 74
6137 285
5688 15
54209143 28067
Satellite: ISS
Catalog Number: 25544
Epoch time: 17208
80328277 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 195
8639 deg
Eccentricity:
0006089
Arg of perigee: 74
6137 deg
Mean anomaly: 285
5688 deg
Mean motion: 15
54209143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 335
Coasting Arc #13 (Orbit 2818)
---------------------------------------
Vector Time (GMT): 2017/209/14:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3208823
83 A = 6781121
69 meter
Y = 4114988
57 meter E =
0014620
Z = -4345268
50 I = 51
55686
XDOT = -6653
748882 Wp = 73
48537
YDOT = 1540
751787 meter/sec RA = 190
67545 deg
ZDOT = -3460
070207 TA = 161
30121
MA = 161
24744
Ha = 223
055 n
mi
Hp = 212
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10527637
25 X = 3183677
37
Y = 13500618
68 feet Y = 4150731
27 meter
Z = -14256130
24 Z = -4329742
26
XDOT = -21829
884783 XDOT = -6653
676349
YDOT = 5054
959931 feet/sec YDOT = 1466
345489 meter/sec
ZDOT = -11351
936374 ZDOT = -3492
391450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7472727
64 X = -2277687
39
Y = -15465839
05 feet Y = -4713987
74 meter
Z = -14188067
67 Z = -4324523
03
XDOT = 21205
100316 XDOT = 6463
314576
YDOT = 282
558509 feet/sec YDOT = 86
123833 meter/sec
ZDOT = -11495
054106 ZDOT = -3503
692492
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 17209
63916032
00016717 00000-0 10270-3 0 9129
2 25544 51
6386 191
6957 0006102 77
9323 282
2513 15
54231156 28195
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
63916032 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 191
6957 deg
Eccentricity:
0006102
Arg of perigee: 77
9323 deg
Mean anomaly: 282
2513 deg
Mean motion: 15
54231156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2819
Checksum: 308
Coasting Arc #14 (Orbit 2834)
---------------------------------------
Vector Time (GMT): 2017/210/14:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1504106
22 A = 6777956
53 meter
Y = -4206244
05 meter E =
0010333
Z = 5089490
48 I = 51
57953
XDOT = 7461
043349 Wp = 102
67703
YDOT = -609
993661 meter/sec RA = 185
67657 deg
ZDOT = 1695
716918 TA = 330
91581
MA = 330
97333
Ha = 222
952 n
mi
Hp = 212
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4934731
71 X = -1481681
10
Y = -13800013
30 feet Y = -4222938
69 meter
Z = 16697803
42 Z = 5082238
47
XDOT = 24478
488677 XDOT = 7459
073063
YDOT = -2001
291540 feet/sec YDOT = -526
570249 meter/sec
ZDOT = 5563
375715 ZDOT = 1731
955193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2212026
09 X = 674225
55
Y = 14524081
27 feet Y = 4426939
97 meter
Z = 16666330
94 Z = 5079897
67
XDOT = -23294
701257 XDOT = -7100
224943
YDOT = -3039
456263 feet/sec YDOT = -926
426269 meter/sec
ZDOT = 5723
696880 ZDOT = 1744
582809
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 17210
66792859
00016717 00000-0 10270-3 0 9134
2 25544 51
6392 186
5674 0005825 81
9981 278
1833 15
54264317 28359
Satellite: ISS
Catalog Number: 25544
Epoch time: 17210
66792859 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 186
5674 deg
Eccentricity:
0005825
Arg of perigee: 81
9981 deg
Mean anomaly: 278
1833 deg
Mean motion: 15
54264317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2835
Checksum: 347
Coasting Arc #15 (Orbit 2849)
---------------------------------------
Vector Time (GMT): 2017/211/14:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -354177
35 A = 6777087
52 meter
Y = 4209393
21 meter E =
0020868
Z = -5317535
86 I = 51
60905
XDOT = -7642
406034 Wp = 90
04909
YDOT = -303
417239 meter/sec RA = 180
67230 deg
ZDOT = 269
739430 TA = 182
52297
MA = 182
53352
Ha = 223
052 n
mi
Hp = 212
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1161999
17 X = -375391
80
Y = 13810345
17 feet Y = 4205314
08 meter
Z = -17445983
78 Z = -5319307
74
XDOT = -25073
510609 XDOT = -7639
755396
YDOT = -995
463381 feet/sec YDOT = -388
865003 meter/sec
ZDOT = 884
971882 ZDOT = 232
621729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3531289
97 X = 1076337
18
Y = -13390730
68 feet Y = -4081494
71 meter
Z = -17454413
45 Z = -5320105
22
XDOT = 23507
311695 XDOT = 7165
028605
YDOT = 5263
359836 feet/sec YDOT = 1604
272078 meter/sec
ZDOT = 720
872086 ZDOT = 219
721812
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 17211
63239795
00016717 00000-0 10270-3 0 9148
2 25544 51
6394 181
7581 0006055 84
3911 275
7932 15
54228484 28506
Satellite: ISS
Catalog Number: 25544
Epoch time: 17211
63239795 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 181
7581 deg
Eccentricity:
0006055
Arg of perigee: 84
3911 deg
Mean anomaly: 275
7932 deg
Mean motion: 15
54228484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2850
Checksum: 328
Coasting Arc #16 (Orbit 2865)
---------------------------------------
Vector Time (GMT): 2017/212/14:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2192257
83 A = 6778578
19 meter
Y = -4083955
97 meter E =
0011915
Z = 4937528
41 I = 51
64649
XDOT = 7249
799327 Wp = 72
72338
YDOT = 1207
186928 meter/sec RA = 175
67313 deg
ZDOT = -2212
541247 TA = 38
88648
MA = 38
80083
Ha = 222
975 n
mi
Hp = 212
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7192446
95 X = 2213778
87
Y = -13398805
68 feet Y = -4059320
50 meter
Z = 16199240
21 Z = 4948229
76
XDOT = 23785
430864 XDOT = 7246
508782
YDOT = 3960
587034 feet/sec YDOT = 1288
240794 meter/sec
ZDOT = -7258
993591 ZDOT = -2177
332188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9189442
42 X = -2800942
05
Y = 12052345
66 feet Y = 3673554
96 meter
Z = 16247146
89 Z = 4952130
37
XDOT = -21980
171294 XDOT = -6699
556210
YDOT = -7148
542931 feet/sec YDOT = -2178
875885 meter/sec
ZDOT = -7103
442601 ZDOT = -2165
129305
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 17212
66116107
00016717 00000-0 10270-3 0 9154
2 25544 51
6390 176
6301 0006033 87
9619 272
2225 15
54238803 28665
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
66116107 = yrday
fracday
Element set: 915
Inclination: 51
6390 deg
RA of node: 176
6301 deg
Eccentricity:
0006033
Arg of perigee: 87
9619 deg
Mean anomaly: 272
2225 deg
Mean motion: 15
54238803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2866
Checksum: 303
Coasting Arc #17 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2017/212/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2600366
67 A = 6779329
17 meter
Y = 4072981
67 meter E =
0017291
Z = -4771116
96 I = 51
65909
XDOT = -7041
537191 Wp = 103
97654
YDOT = -1371
755046 meter/sec RA = 173
89887 deg
ZDOT = 2670
821692 TA = 192
41509
MA = 192
45774
Ha = 223
062 n
mi
Hp = 212
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8531386
71 X = -2622543
00
Y = 13362800
74 feet Y = 4043778
80 meter
Z = -15653270
86 Z = -4783802
33
XDOT = -23102
156139 XDOT = -7038
647964
YDOT = -4500
508682 feet/sec YDOT = -1450
482254 meter/sec
ZDOT = 8762
538361 ZDOT = 2636
623315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15764558
40 X = -4805037
40
Y = -1024664
21 feet Y = -312317
65 meter
Z = -15709953
95 Z = -4788393
96
XDOT = -7180
924549 XDOT = -2188
745803
YDOT = -21346
888793 feet/sec YDOT = -6506
531704 meter/sec
ZDOT = 8611
473783 ZDOT = 2624
777209
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 17212
98264874
00016717 00000-0 10270-3 0 9165
2 25544 51
6375 175
0227 0006118 94
3323 265
8529 15
54235071 28711
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
98264874 = yrday
fracday
Element set: 916
Inclination: 51
6375 deg
RA of node: 175
0227 deg
Eccentricity:
0006118
Arg of perigee: 94
3323 deg
Mean anomaly: 265
8529 deg
Mean motion: 15
54235071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 320
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