[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 19th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15476 3504 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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
199/15:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
4
201/19:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 215
3
203/18:49:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 215
1
206/03:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
8
207/15:56:37
527 -1
2 1
2 1
2
N/A 0
2 0
0 221
8
000/00:03:15
055 -0
3 0
0 215
4
209/20:18:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 215
3
212/23:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 214
9
Coasting Arc #1 (Orbit 337)
---------------------------------------
Vector Time (GMT): 2018/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2336008
30 A = 6777903
41 meter
Y = 3568154
52 meter E =
0013347
Z = -5279218
57 I = 51
36408
XDOT = -5996
108872 Wp = 70
35235
YDOT = -4733
796712 meter/sec RA = 221
54731 deg
ZDOT = -543
008083 TA = 194
42090
MA = 194
45903
Ha = 220
987 n
mi
Hp = 215
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7664069
22 X = -2350091
47
Y = 11706543
71 feet Y = 3541953
20 meter
Z = -17320270
90 Z = -5290599
95
XDOT = -19672
273201 XDOT = -5940
091003
YDOT = -15530
829109 feet/sec YDOT = -4800
536099 meter/sec
ZDOT = -1781
522581 ZDOT = -571
998888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13810858
53 X = 4209549
68
Y = 1805281
71 feet Y = 550249
87 meter
Z = -17371645
04 Z = -5294877
41
XDOT = -5477
123435 XDOT = -1669
427223
YDOT = 23411
526786 feet/sec YDOT = 7135
833364 meter/sec
ZDOT = -1910
766832 ZDOT = -582
401731
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18199
51708513
00016717 00000-0 10270-3 0 9005
2 25544 51
6398 222
5590 0004007 328
2925 31
7985 15
53979603 3386
Satellite: ISS
Catalog Number: 25544
Epoch time: 18199
51708513 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 222
5590 deg
Eccentricity:
0004007
Arg of perigee: 328
2925 deg
Mean anomaly: 31
7985 deg
Mean motion: 15
53979603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 338
Checksum: 325
Coasting Arc #2 (Orbit 339)
---------------------------------------
Vector Time (GMT): 2018/199/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5109573
65 A = 6781261
86 meter
Y = 288034
61 meter E =
0006843
Z = -4454930
60 I = 51
37551
XDOT = -3174
274364 Wp = 87
88767
YDOT = -6172
508933 meter/sec RA = 220
84209 deg
ZDOT = 3246
217596 TA = 214
92815
MA = 214
97307
Ha = 221
011 n
mi
Hp = 215
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16763693
07 X = -5090775
36
Y = 944995
44 feet Y = 231001
17 meter
Z = -14615914
04 Z = -4479705
13
XDOT = -10414
285972 XDOT = -3120
783953
YDOT = -20251
013560 feet/sec YDOT = -6207
706948 meter/sec
ZDOT = 10650
320197 ZDOT = 3230
927872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16297172
01 X = 4967378
03
Y = 3613980
58 feet Y = 1101541
28 meter
Z = -14726869
78 Z = -4488749
91
XDOT = 4859
984578 XDOT = 1481
323299
YDOT = 21147
029316 feet/sec YDOT = 6445
614535 meter/sec
ZDOT = 10582
584525 ZDOT = 3225
571763
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18199
64570141
00016717 00000-0 10270-3 0 9014
2 25544 51
6366 221
9182 0004166 330
3167 29
7748 15
53967485 3401
Satellite: ISS
Catalog Number: 25544
Epoch time: 18199
64570141 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 221
9182 deg
Eccentricity:
0004166
Arg of perigee: 330
3167 deg
Mean anomaly: 29
7748 deg
Mean motion: 15
53967485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 340
Checksum: 319
Coasting Arc #3 (Orbit 355)
---------------------------------------
Vector Time (GMT): 2018/200/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5833704
70 A = 6784905
49 meter
Y = 935468
50 meter E =
0011216
Z = 3330438
21 I = 51
41320
XDOT = 1733
207754 Wp = 71
37645
YDOT = 5837
889424 meter/sec RA = 215
83965 deg
ZDOT = -4659
296470 TA = 69
70515
MA = 69
58464
Ha = 221
086 n
mi
Hp = 215
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19139451
11 X = 5806633
11
Y = 3069122
39 feet Y = 1000553
46 meter
Z = 10926634
55 Z = 3358710
34
XDOT = 5686
377145 XDOT = 1690
430227
YDOT = 19153
180525 feet/sec YDOT = 5857
032434 meter/sec
ZDOT = -15286
405740 ZDOT = -4650
980794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17655374
58 X = -5381358
17
Y = -7825964
61 feet Y = -2385354
01 meter
Z = 11053120
37 Z = 3368991
09
XDOT = -1288
341795 XDOT = -392
686579
YDOT = -18707
064755 feet/sec YDOT = -5701
913337 meter/sec
ZDOT = -15249
843896 ZDOT = -4648
152420
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 18200
67462652
00016717 00000-0 10270-3 0 9028
2 25544 51
6362 216
7898 0004263 333
6751 26
4184 15
53995791 3562
Satellite: ISS
Catalog Number: 25544
Epoch time: 18200
67462652 = yrday
fracday
Element set: 902
Inclination: 51
6362 deg
RA of node: 216
7898 deg
Eccentricity:
0004263
Arg of perigee: 333
6751 deg
Mean anomaly: 26
4184 deg
Mean motion: 15
53995791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 356
Checksum: 324
Coasting Arc #4 (Orbit 370)
---------------------------------------
Vector Time (GMT): 2018/201/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6213343
71 A = 6788131
43 meter
Y = -1947655
96 meter E =
0009629
Z = -1899998
12 I = 51
45157
XDOT = -65
905772 Wp = 17
22341
YDOT = -5237
760005 meter/sec RA = 210
84895 deg
ZDOT = 5600
957051 TA = 321
78922
MA = 321
85743
Ha = 221
153 n
mi
Hp = 215
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20384985
94 X = -6181873
59
Y = -6389947
37 feet Y = -2016961
77 meter
Z = -6233589
65 Z = -1930103
85
XDOT = -216
226285 XDOT = -34
537077
YDOT = -17184
251984 feet/sec YDOT = -5238
321997 meter/sec
ZDOT = 18375
843344 ZDOT = 5600
712738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18236766
69 X = 5558566
49
Y = 11050035
02 feet Y = 3368050
67 meter
Z = -6368185
44 Z = -1941022
92
XDOT = -2956
735878 XDOT = -901
213095
YDOT = 15439
380276 feet/sec YDOT = 4705
923108 meter/sec
ZDOT = 18375
347685 ZDOT = 5600
805974
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 18201
63924192
00016717 00000-0 10270-3 0 9038
2 25544 51
6364 211
9824 0004205 337
3242 22
7724 15
53990000 3716
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
63924192 = yrday
fracday
Element set: 903
Inclination: 51
6364 deg
RA of node: 211
9824 deg
Eccentricity:
0004205
Arg of perigee: 337
3242 deg
Mean anomaly: 22
7724 deg
Mean motion: 15
53990000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 371
Checksum: 278
Coasting Arc #5 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2018/201/19:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1692289
86 A = 6777756
19 meter
Y = 3896832
62 meter E =
0013898
Z = -5292593
31 I = 51
42573
XDOT = -6785
940555 Wp = 69
78595
YDOT = -3525
104218 meter/sec RA = 209
97249 deg
ZDOT = -421
880428 TA = 196
15142
MA = 196
19577
Ha = 221
188 n
mi
Hp = 215
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5552132
07 X = -1710031
11
Y = 12784883
93 feet Y = 3877809
44 meter
Z = -17364151
27 Z = -5300856
62
XDOT = -22263
584497 XDOT = -6743
968269
YDOT = -11565
302554 feet/sec YDOT = -3600
754581 meter/sec
ZDOT = -1384
122138 ZDOT = -454
742229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6546099
95 X = -1995251
27
Y = -12252592
72 feet Y = -3734590
26 meter
Z = -17401601
19 Z = -5304008
04
XDOT = 22072
401021 XDOT = 6727
667831
YDOT = -9600
558902 feet/sec YDOT = -2926
250353 meter/sec
ZDOT = -1530
883386 ZDOT = -466
613256
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 18201
83216446
00016717 00000-0 10270-3 0 9047
2 25544 51
6401 211
0221 0004321 336
5314 23
5640 15
54016393 3744
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
83216446 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 211
0221 deg
Eccentricity:
0004321
Arg of perigee: 336
5314 deg
Mean anomaly: 23
5640 deg
Mean motion: 15
54016393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 255
Coasting Arc #6 (Orbit 389)
---------------------------------------
Vector Time (GMT): 2018/202/19:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3233321
31 A = 6778266
12 meter
Y = -3011459
44 meter E =
0007072
Z = 5139748
01 I = 51
45717
XDOT = 6249
295854 Wp = 18
22458
YDOT = 4196
491347 meter/sec RA = 204
96017 deg
ZDOT = -1465
393571 TA = 85
95675
MA = 85
87592
Ha = 221
139 n
mi
Hp = 215
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10608009
53 X = 3241789
97
Y = -9880116
28 feet Y = -2975255
29 meter
Z = 16862690
32 Z = 5155474
57
XDOT = 20502
939153 XDOT = 6209
023130
YDOT = 13768
016230 feet/sec YDOT = 4266
150233 meter/sec
ZDOT = -4807
721691 ZDOT = -1435
134341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1357615
21 X = 413801
12
Y = 14349614
35 feet Y = 4373762
45 meter
Z = 16933467
98 Z = 5161321
04
XDOT = -22426
063403 XDOT = -6835
464125
YDOT = 7663
283109 feet/sec YDOT = 2335
768692 meter/sec
ZDOT = -4672
672002 ZDOT = -1424
230426
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 18202
86108194
00016717 00000-0 10270-3 0 9052
2 25544 51
6402 205
8937 0004416 339
5755 20
5220 15
54045154 3903
Satellite: ISS
Catalog Number: 25544
Epoch time: 18202
86108194 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 205
8937 deg
Eccentricity:
0004416
Arg of perigee: 339
5755 deg
Mean anomaly: 20
5220 deg
Mean motion: 15
54045154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 390
Checksum: 289
Coasting Arc #7 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2018/203/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5020633
00 A = 6781999
18 meter
Y = -1732292
92 meter E =
0011074
Z = 4214779
74 I = 51
49772
XDOT = 4728
822847 Wp = 50
71432
YDOT = 4815
432547 meter/sec RA = 200
10954 deg
ZDOT = -3640
504449 TA = 76
69422
MA = 76
57075
Ha = 221
359 n
mi
Hp = 215
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16471893
04 X = 5019157
83
Y = -5683375
73 feet Y = -1676157
39 meter
Z = 13828017
53 Z = 4239164
29
XDOT = 15514
510653 XDOT = 4692
307400
YDOT = 15798
663213 feet/sec YDOT = 4868
109689 meter/sec
ZDOT = -11943
912235 ZDOT = -3617
621884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8411585
03 X = -2563851
12
Y = 15160180
05 feet Y = 4620822
88 meter
Z = 13937441
19 Z = 4248132
07
XDOT = -21049
783913 XDOT = -6415
974137
YDOT = -752
794917 feet/sec YDOT = -229
451891 meter/sec
ZDOT = -11841
954729 ZDOT = -3609
427801
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 18203
82569314
00016717 00000-0 10270-3 0 9065
2 25544 51
6391 201
0863 0004407 345
8281 14
2747 15
54017696 4051
Satellite: ISS
Catalog Number: 25544
Epoch time: 18203
82569314 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 201
0863 deg
Eccentricity:
0004407
Arg of perigee: 345
8281 deg
Mean anomaly: 14
2747 deg
Mean motion: 15
54017696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 300
Coasting Arc #8 (Orbit 419)
---------------------------------------
Vector Time (GMT): 2018/204/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6013936
23 A = 6785682
01 meter
Y = 859157
78 meter E =
0006570
Z = -3019047
68 I = 51
54183
XDOT = -3179
021100 Wp = 30
73144
YDOT = -4924
296267 meter/sec RA = 195
11757 deg
ZDOT = 4941
536531 TA = 294
63483
MA = 294
70326
Ha = 221
396 n
mi
Hp = 214
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19730761
91 X = -6008431
82
Y = 2818759
14 feet Y = 791936
89 meter
Z = -9905012
07 Z = -3048247
53
XDOT = -10429
859251 XDOT = -3147
723113
YDOT = -16155
827648 feet/sec YDOT = -4959
671801 meter/sec
ZDOT = 16212
390195 ZDOT = 4926
169608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12505799
15 X = 3811767
58
Y = -15435116
13 feet Y = -4704623
40 meter
Z = -10035925
98 Z = -3058950
24
XDOT = 17584
437675 XDOT = 5359
736603
YDOT = 3771
964934 feet/sec YDOT = 1149
694912 meter/sec
ZDOT = 16144
097413 ZDOT = 4920
720891
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 18204
79030034
00016717 00000-0 10270-3 0 9075
2 25544 51
6395 196
2783 0004428 347
0480 13
0558 15
54017125 4200
Satellite: ISS
Catalog Number: 25544
Epoch time: 18204
79030034 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 196
2783 deg
Eccentricity:
0004428
Arg of perigee: 347
0480 deg
Mean anomaly: 13
0558 deg
Mean motion: 15
54017125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 420
Checksum: 289
Coasting Arc #9 (Orbit 435)
---------------------------------------
Vector Time (GMT): 2018/205/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6619475
98 A = 6788735
95 meter
Y = -16396
15 meter E =
0011897
Z = 1489531
08 I = 51
58406
XDOT = 1317
568092 Wp = 101
09888
YDOT = 4879
737663 meter/sec RA = 190
13769 deg
ZDOT = -5764
682861 TA = 62
62974
MA = 62
50872
Ha = 221
614 n
mi
Hp = 214
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21717440
88 X = 6611932
10
Y = -53793
13 feet Y = 57585
06 meter
Z = 4886912
99 Z = 1521667
44
XDOT = 4322
729961 XDOT = 1290
905005
YDOT = 16009
638001 feet/sec YDOT = 4894
323168 meter/sec
ZDOT = -18913
001513 ZDOT = -5758
346883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15609990
86 X = -4757925
21
Y = 15051583
76 feet Y = 4587722
73 meter
Z = 5030910
69 Z = 1533421
58
XDOT = -13195
141703 XDOT = -4021
879191
YDOT = -7333
133891 feet/sec YDOT = -2235
139210 meter/sec
ZDOT = -18885
155616 ZDOT = -5756
195432
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 18205
81921217
00016717 00000-0 10270-3 0 9082
2 25544 51
6397 191
1502 0004327 352
1536 7
9548 15
53990083 4362
Satellite: ISS
Catalog Number: 25544
Epoch time: 18205
81921217 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 191
1502 deg
Eccentricity:
0004327
Arg of perigee: 352
1536 deg
Mean anomaly: 7
9548 deg
Mean motion: 15
53990083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 436
Checksum: 308
Coasting Arc #10 (Orbit 440)
---------------------------------------
Vector Time (GMT): 2018/206/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -899757
93 A = 6777646
21 meter
Y = 4128802
38 meter E =
0014790
Z = -5311385
47 I = 51
55752
XDOT = -7538
662378 Wp = 76
70767
YDOT = -1322
245492 meter/sec RA = 188
44382 deg
ZDOT = 253
135077 TA = 195
68819
MA = 195
73407
Ha = 221
497 n
mi
Hp = 214
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2951961
71 X = -920060
93
Y = 13545939
58 feet Y = 4118627
73 meter
Z = -17425805
36 Z = -5315804
98
XDOT = -24733
144284 XDOT = -7524
545958
YDOT = -4338
075760 feet/sec YDOT = -1406
469118 meter/sec
ZDOT = 830
495659 ZDOT = 216
549540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5831998
98 X = -1777593
29
Y = 12549410
95 feet Y = 3825060
46 meter
Z = -17446068
97 Z = -5317561
82
XDOT = -22196
266855 XDOT = -6765
422137
YDOT = -9406
126254 feet/sec YDOT = -2866
987282 meter/sec
ZDOT = 666
702329 ZDOT = 203
210870
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 18206
14074523
00016717 00000-0 10270-3 0 9099
2 25544 51
6387 189
5428 0003956 353
0502 7
0595 15
54033988 4411
Satellite: ISS
Catalog Number: 25544
Epoch time: 18206
14074523 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 189
5428 deg
Eccentricity:
0003956
Arg of perigee: 353
0502 deg
Mean anomaly: 7
0595 deg
Mean motion: 15
54033988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 441
Checksum: 314
Coasting Arc #11 (Orbit 456)
---------------------------------------
Vector Time (GMT): 2018/207/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2628780
43 A = 6779123
69 meter
Y = -3787415
88 meter E =
0008813
Z = 4968098
78 I = 51
59494
XDOT = 7062
574174 Wp = 34
59611
YDOT = 2108
731468 meter/sec RA = 183
44130 deg
ZDOT = -2120
499442 TA = 76
11253
MA = 76
01451
Ha = 221
562 n
mi
Hp = 214
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8624607
70 X = 2646805
00
Y = -12425905
11 feet Y = -3757918
78 meter
Z = 16299536
69 Z = 4980911
65
XDOT = 23171
175112 XDOT = 7048
768942
YDOT = 6918
410329 feet/sec YDOT = 2187
633081 meter/sec
ZDOT = -6957
019167 ZDOT = -2086
225815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10933795
27 X = 3332620
80
Y = -10360990
48 feet Y = -3158029
90 meter
Z = 16357379
66 Z = 4985729
32
XDOT = 20492
784020 XDOT = 6246
200569
YDOT = 10838
294843 feet/sec YDOT = 3303
512268 meter/sec
ZDOT = -6803
647152 ZDOT = -2073
751652
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 18207
16965271
00016717 00000-0 10270-3 0 9103
2 25544 51
6385 184
4138 0003965 357
8953 2
2182 15
54009978 4571
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
16965271 = yrday
fracday
Element set: 910
Inclination: 51
6385 deg
RA of node: 184
4138 deg
Eccentricity:
0003965
Arg of perigee: 357
8953 deg
Mean anomaly: 2
2182 deg
Mean motion: 15
54009978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 457
Checksum: 328
Coasting Arc #12 (Orbit 464)
---------------------------------------
Vector Time (GMT): 2018/207/15:58:15
055
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1569778
47 A = 6779030
85 meter
Y = 4114708
52 meter E =
0014255
Z = -5165969
30 I = 51
61045
XDOT = -7450
099655 Wp = 61
80595
YDOT = 1035
839056 meter/sec RA = 180
77982 deg
ZDOT = -1435
249381 TA = 194
33864
MA = 194
37913
Ha = 221
790 n
mi
Hp = 215
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5150191
84 X = 1548743
07
Y = 13499699
88 feet Y = 4132145
77 meter
Z = -16948718
17 Z = -5158394
69
XDOT = -24442
584169 XDOT = -7454
157439
YDOT = 3398
422099 feet/sec YDOT = 952
504350 meter/sec
ZDOT = -4708
823428 ZDOT = -1471
448448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5957787
09 X = -1815933
51
Y = -13206266
35 feet Y = -4025269
98 meter
Z = -16915221
63 Z = -5155759
55
XDOT = 23237
902451 XDOT = 7082
912667
YDOT = -4229
165489 feet/sec YDOT = -1289
049641 meter/sec
ZDOT = -4871
186036 ZDOT = -1484
737504
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 18207
68410615
00016717 00000-0 10270-3 0 9118
2 25544 51
6387 181
8539 0004261 347
1927 12
9117 15
53805718 4652
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
68410615 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 181
8539 deg
Eccentricity:
0004261
Arg of perigee: 347
1927 deg
Mean anomaly: 12
9117 deg
Mean motion: 15
53805718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 465
Checksum: 314
Coasting Arc #13 (Orbit 480)
---------------------------------------
Vector Time (GMT): 2018/208/15:58:15
055
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 115234
12 A = 6778241
11 meter
Y = -4217492
20 meter E =
0005096
Z = 5303976
77 I = 51
64168
XDOT = 7655
684321 Wp = 18
24322
YDOT = -267
512108 meter/sec RA = 175
78310 deg
ZDOT = -374
209773 TA = 75
35245
MA = 75
29596
Ha = 221
737 n
mi
Hp = 215
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 378064
69 X = 136623
34
Y = -13836916
67 feet Y = -4216084
44 meter
Z = 17401498
58 Z = 5304588
11
XDOT = 25117
074543 XDOT = 7659
924409
YDOT = -877
664396 feet/sec YDOT = -181
877218 meter/sec
ZDOT = -1227
722352 ZDOT = -337
011623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 695527
40 X = 211996
75
Y = 13820563
22 feet Y = 4212507
67 meter
Z = 17404701
17 Z = 5304952
92
XDOT = -23995
879269 XDOT = -7313
944001
YDOT = 2563
643261 feet/sec YDOT = 781
398466 meter/sec
ZDOT = -1060
941113 ZDOT = -323
374851
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 18208
71316027
00016717 00000-0 10270-3 0 9126
2 25544 51
6391 176
7267 0004302 347
7946 12
3102 15
53833501 4818
Satellite: ISS
Catalog Number: 25544
Epoch time: 18208
71316027 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 176
7267 deg
Eccentricity:
0004302
Arg of perigee: 347
7946 deg
Mean anomaly: 12
3102 deg
Mean motion: 15
53833501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 481
Checksum: 288
Coasting Arc #14 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2018/209/15:58:15
055
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1755714
60 A = 6779745
35 meter
Y = 4268514
95 meter E =
0011686
Z = -4975883
70 I = 51
68062
XDOT = -7335
037302 Wp = 85
64930
YDOT = -525
765344 meter/sec RA = 170
78930 deg
ZDOT = 2142
311753 TA = 205
20705
MA = 205
26413
Ha = 221
944 n
mi
Hp = 215
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5760218
52 X = -1779146
15
Y = 14004314
15 feet Y = 4248750
68 meter
Z = -16325077
76 Z = -4984468
77
XDOT = -24065
083012 XDOT = -7339
018887
YDOT = -1724
951917 feet/sec YDOT = -607
813211 meter/sec
ZDOT = 7028
581868 ZDOT = 2106
671768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4421423
63 X = 1347649
92
Y = -14438785
40 feet Y = -4400941
79 meter
Z = -16364033
28 Z = -4987757
34
XDOT = 23117
150159 XDOT = 7046
107368
YDOT = -686
524750 feet/sec YDOT = -209
252744 meter/sec
ZDOT = 6868
849065 ZDOT = 2093
625195
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 18209
67789730
00016717 00000-0 10270-3 0 9138
2 25544 51
6403 171
9197 0004364 353
4347 6
6748 15
53804391 4961
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
67789730 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 171
9197 deg
Eccentricity:
0004364
Arg of perigee: 353
4347 deg
Mean anomaly: 6
6748 deg
Mean motion: 15
53804391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 333
Coasting Arc #15 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2018/209/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5552587
13 A = 6785278
08 meter
Y = 1796816
75 meter E =
0006196
Z = -3469453
07 I = 51
70122
XDOT = -4280
543799 Wp = 45
26231
YDOT = 4419
553161 meter/sec RA = 169
93138 deg
ZDOT = -4562
555036 TA = 175
36504
MA = 175
35930
Ha = 221
941 n
mi
Hp = 215
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18217149
39 X = 5548934
35
Y = 5895068
09 feet Y = 1858889
43 meter
Z = -11382720
03 Z = -3442489
87
XDOT = -14043
778868 XDOT = -4307
484334
YDOT = 14499
846330 feet/sec YDOT = 4371
534835 meter/sec
ZDOT = -14969
012586 ZDOT = -4583
413108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11776803
95 X = -3589569
84
Y = 15187375
32 feet Y = 4629112
00 meter
Z = -11262024
44 Z = -3432665
05
XDOT = -7769
368555 XDOT = -2368
103535
YDOT = -17192
588355 feet/sec YDOT = -5240
300931 meter/sec
ZDOT = -15063
011620 ZDOT = -4591
205942
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 18209
87084268
00016717 00000-0 10270-3 0 9145
2 25544 51
6368 170
9564 0004362 352
9728 7
1362 15
53806160 4990
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
87084268 = yrday
fracday
Element set: 914
Inclination: 51
6368 deg
RA of node: 170
9564 deg
Eccentricity:
0004362
Arg of perigee: 352
9728 deg
Mean anomaly: 7
1362 deg
Mean motion: 15
53806160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 329
Coasting Arc #16 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2018/210/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4394676
33 A = 6781800
33 meter
Y = -2504059
70 meter E =
0008100
Z = 4510213
39 I = 51
72165
XDOT = 5628
716894 Wp = 83
36083
YDOT = -4121
770634 meter/sec RA = 164
95181 deg
ZDOT = 3192
130020 TA = 334
61260
MA = 334
65237
Ha = 222
137 n
mi
Hp = 215
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14418229
44 X = -4388256
39
Y = -8215418
97 feet Y = -2553168
33 meter
Z = 14797288
02 Z = 4488881
51
XDOT = 18466
918943 XDOT = 5658
883991
YDOT = -13522
869535 feet/sec YDOT = -4058
657915 meter/sec
ZDOT = 10472
867519 ZDOT = 3219
544844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12482220
27 X = 3804580
74
Y = -11062837
81 feet Y = -3371952
96 meter
Z = 14701903
90 Z = 4481140
31
XDOT = 6009
898857 XDOT = 1831
817172
YDOT = 20880
362734 feet/sec YDOT = 6364
334561 meter/sec
ZDOT = 10596
245739 ZDOT = 3229
735701
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 18210
89989259
00016717 00000-0 10270-3 0 9154
2 25544 51
6367 165
8287 0004334 355
4857 4
6256 15
53785371 5157
Satellite: ISS
Catalog Number: 25544
Epoch time: 18210
89989259 = yrday
fracday
Element set: 915
Inclination: 51
6367 deg
RA of node: 165
8287 deg
Eccentricity:
0004334
Arg of perigee: 355
4857 deg
Mean anomaly: 4
6256 deg
Mean motion: 15
53785371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 345
Coasting Arc #17 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2018/211/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3004057
26 A = 6779089
19 meter
Y = 3233894
47 meter E =
0015067
Z = -5158380
09 I = 51
74453
XDOT = -6551
275248 Wp = 62
83440
YDOT = 3661
578789 meter/sec RA = 159
96586 deg
ZDOT = -1516
409856 TA = 192
53860
MA = 192
57612
Ha = 222
069 n
mi
Hp = 215
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9855830
90 X = 2992727
87
Y = 10609890
00 feet Y = 3267424
74 meter
Z = -16923819
20 Z = -5143815
13
XDOT = -21493
685197 XDOT = -6584
367361
YDOT = 12013
053771 feet/sec YDOT = 3588
132921 meter/sec
ZDOT = -4975
097953 ZDOT = -1548
313292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13165284
17 X = -4012778
62
Y = 6211064
20 feet Y = 1893132
37 meter
Z = -16858849
28 Z = -5138577
26
XDOT = -4357
135940 XDOT = -1328
055035
YDOT = -23158
578984 feet/sec YDOT = -7058
734874 meter/sec
ZDOT = -5118
569916 ZDOT = -1560
140110
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 18211
86462300
00016717 00000-0 10270-3 0 9166
2 25544 51
6367 161
0213 0004197
5965 359
5191 15
53812272 5307
Satellite: ISS
Catalog Number: 25544
Epoch time: 18211
86462300 = yrday
fracday
Element set: 916
Inclination: 51
6367 deg
RA of node: 161
0213 deg
Eccentricity:
0004197
Arg of perigee:
5965 deg
Mean anomaly: 359
5191 deg
Mean motion: 15
53812272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 287
Coasting Arc #18 (Orbit 545)
---------------------------------------
Vector Time (GMT): 2018/212/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1462820
38 A = 6778384
85 meter
Y = -3938894
93 meter E =
0005501
Z = 5316743
06 I = 51
77294
XDOT = 7041
787722 Wp = 31
21090
YDOT = -3026
334418 meter/sec RA = 154
97746 deg
ZDOT = -299
879052 TA = 61
66948
MA = 61
61400
Ha = 222
250 n
mi
Hp = 214
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4799279
47 X = -1444491
33
Y = -12922883
62 feet Y = -3955150
81 meter
Z = 17443382
75 Z = 5309681
76
XDOT = 23102
978092 XDOT = 7076
562301
YDOT = -9928
918695 feet/sec YDOT = -2947
393838 meter/sec
ZDOT = -983
855158 ZDOT = -265
588687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13793512
28 X = 4204262
54
Y = -928496
12 feet Y = -283005
62 meter
Z = 17412137
15 Z = 5307219
40
XDOT = 2682
247491 XDOT = 817
549035
YDOT = 23995
127017 feet/sec YDOT = 7313
714715 meter/sec
ZDOT = -829
730493 ZDOT = -252
901854
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 18212
89366603
00016717 00000-0 10270-3 0 9170
2 25544 51
6369 155
8933 0004231 5
1067 355
0127 15
53779352 5460
Satellite: ISS
Catalog Number: 25544
Epoch time: 18212
89366603 = yrday
fracday
Element set: 917
Inclination: 51
6369 deg
RA of node: 155
8933 deg
Eccentricity:
0004231
Arg of perigee: 5
1067 deg
Mean anomaly: 355
0127 deg
Mean motion: 15
53779352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 546
Checksum: 314
Coasting Arc #19 (Orbit 547)
---------------------------------------
Vector Time (GMT): 2018/212/23:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1811499
66 A = 6778242
21 meter
Y = -3780904
94 meter E =
0004793
Z = 5323697
32 I = 51
77922
XDOT = 6914
785825 Wp = 36
26966
YDOT = -3320
388659 meter/sec RA = 154
34162 deg
ZDOT = -1
475073 TA = 53
76651
MA = 53
72222
Ha = 222
154 n
mi
Hp = 214
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5943240
36 X = -1794945
18
Y = -12404543
78 feet Y = -3801069
92 meter
Z = 17466198
54 Z = 5314937
97
XDOT = 22686
305199 XDOT = 6951
408574
YDOT = -10893
663578 feet/sec YDOT = -3242
857973 meter/sec
ZDOT = -4
839479 ZDOT = 32
202873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7855817
52 X = 2394453
18
Y = -11350663
87 feet Y = -3459682
35 meter
Z = 17427319
49 Z = 5311846
98
XDOT = 19768
573082 XDOT = 6025
461075
YDOT = 13887
859852 feet/sec YDOT = 4233
019683 meter/sec
ZDOT = 146
572229 ZDOT = 44
675215
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 18213
02229595
00016717 00000-0 10270-3 0 9185
2 25544 51
6395 155
2510 0003993 5
8977 354
2222 15
53820684 5489
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
02229595 = yrday
fracday
Element set: 918
Inclination: 51
6395 deg
RA of node: 155
2510 deg
Eccentricity:
0003993
Arg of perigee: 5
8977 deg
Mean anomaly: 354
2222 deg
Mean motion: 15
53820684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 548
Checksum: 318
Coasting Arc #20 (Orbit 562)
---------------------------------------
Vector Time (GMT): 2018/213/23:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 298275
93 A = 6779226
04 meter
Y = 4478658
98 meter E =
0013648
Z = -5091974
34 I = 51
81160
XDOT = -7008
901465 Wp = 86
98697
YDOT = 2506
974625 meter/sec RA = 149
35795 deg
ZDOT = 1799
309051 TA = 200
37912
MA = 200
43363
Ha = 222
152 n
mi
Hp = 214
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 978595
57 X = 272905
95
Y = 14693763
06 feet Y = 4481852
72 meter
Z = -16705952
55 Z = -5090587
00
XDOT = -22995
083548 XDOT = -7045
154209
YDOT = 8224
982366 feet/sec YDOT = 2428
393521 meter/sec
ZDOT = 5903
244918 ZDOT = 1765
174682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12141205
95 X = -3700639
57
Y = 8345483
47 feet Y = 2543703
36 meter
Z = -16700215
46 Z = -5090225
67
XDOT = -18104
136314 XDOT = -5518
140749
YDOT = -14864
142963 feet/sec YDOT = -4530
590775 meter/sec
ZDOT = 5749
857699 ZDOT = 1752
556627
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 18213
98701957
00016717 00000-0 10270-3 0 9198
2 25544 51
6390 150
4456 0003902 10
2739 349
8492 15
53834562 5632
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
98701957 = yrday
fracday
Element set: 919
Inclination: 51
6390 deg
RA of node: 150
4456 deg
Eccentricity:
0003902
Arg of perigee: 10
2739 deg
Mean anomaly: 349
8492 deg
Mean motion: 15
53834562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 563
Checksum: 324
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