[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 17th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 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
172/07:16:36
447 1
2 1
2 1
3
N/A 0
1 -0
1 220
4
000/00:03:12
895 0
4 -0
0 216
0
179/14:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
0
180/09:42:42
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
9
Coasting Arc #1 (Orbit 3824)
---------------------------------------
Vector Time (GMT): 2018/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4923129
48 A = 6787493
90 meter
Y = -4216209
77 meter E =
0008585
Z = -2000281
95 I = 51
82821
XDOT = 4532
343729 Wp = 156
38495
YDOT = -2648
050607 meter/sec RA = 26
53708 deg
ZDOT = -5589
455259 TA = 45
64469
MA = 45
57438
Ha = 220
885 n
mi
Hp = 214
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16151999
61 X = -4865900
49
Y = -13832709
22 feet Y = -4270943
25 meter
Z = -6562604
84 Z = -2024058
50
XDOT = 14869
894123 XDOT = 4588
768629
YDOT = -8687
830076 feet/sec YDOT = -2597
050310 meter/sec
ZDOT = -18338
107806 ZDOT = -5567
302214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15731433
67 X = -4794940
98
Y = 14260232
28 feet Y = 4346518
80 meter
Z = -6668319
74 Z = -2032503
86
XDOT = -5715
058841 XDOT = -1741
949935
YDOT = -14809
216581 feet/sec YDOT = -4513
849214 meter/sec
ZDOT = -18238
516168 ZDOT = -5559
099728
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 18166
52817284
00016717 00000-0 10270-3 0 9006
2 25544 51
6411 26
9891 0002986 198
2153 161
8893 15
54156291 38252
Satellite: ISS
Catalog Number: 25544
Epoch time: 18166
52817284 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 26
9891 deg
Eccentricity:
0002986
Arg of perigee: 198
2153 deg
Mean anomaly: 161
8893 deg
Mean motion: 15
54156291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3825
Checksum: 332
Coasting Arc #2 (Orbit 3840)
---------------------------------------
Vector Time (GMT): 2018/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3784634
50 A = 6784037
25 meter
Y = 4431053
12 meter E =
0011600
Z = 3466684
45 I = 51
78564
XDOT = -5969
783503 Wp = 104
19105
YDOT = 1510
252701 meter/sec RA = 21
56943 deg
ZDOT = 4571
352931 TA = 296
40472
MA = 296
52373
Ha = 220
788 n
mi
Hp = 214
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12416779
86 X = 3717964
79
Y = 14537575
84 feet Y = 4473002
16 meter
Z = 11373636
65 Z = 3484907
56
XDOT = -19585
903881 XDOT = -6008
432915
YDOT = 4954
897314 feet/sec YDOT = 1443
277608 meter/sec
ZDOT = 14997
877069 ZDOT = 4542
260403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15780260
91 X = 4809823
52
Y = -10707749
24 feet Y = -3263721
97 meter
Z = 11454458
35 Z = 3491318
91
XDOT = 2031
690235 XDOT = 619
259184
YDOT = 18952
634773 feet/sec YDOT = 5776
763079 meter/sec
ZDOT = 14867
416360 ZDOT = 4531
588506
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 18167
55697055
00016717 00000-0 10270-3 0 9013
2 25544 51
6399 21
8595 0002815 201
4358 158
6677 15
54171331 38411
Satellite: ISS
Catalog Number: 25544
Epoch time: 18167
55697055 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 21
8595 deg
Eccentricity:
0002815
Arg of perigee: 201
4358 deg
Mean anomaly: 158
6677 deg
Mean motion: 15
54171331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3841
Checksum: 328
Coasting Arc #3 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2018/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2265453
22 A = 6780172
57 meter
Y = -4452820
23 meter E =
0008302
Z = -4591359
33 I = 51
74131
XDOT = 7013
853735 Wp = 83
54419
YDOT = -423
397041 meter/sec RA = 16
58935 deg
ZDOT = -3053
961582 TA = 155
96880
MA = 155
93004
Ha = 220
693 n
mi
Hp = 214
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7432589
29 X = -2193190
02
Y = -14608990
25 feet Y = -4477749
38 meter
Z = -15063514
86 Z = -4602189
13
XDOT = 23011
331151 XDOT = 7032
901373
YDOT = -1389
097902 feet/sec YDOT = -344
856357 meter/sec
ZDOT = -10019
558996 ZDOT = -3019
844860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15212779
50 X = -4636855
19
Y = 5983072
70 feet Y = 1823640
56 meter
Z = -15111242
20 Z = -4605906
62
XDOT = 1136
423478 XDOT = 346
381876
YDOT = -21999
077413 feet/sec YDOT = -6705
318796 meter/sec
ZDOT = -9866
797011 ZDOT = -3007
399729
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 18168
52146584
00016717 00000-0 10270-3 0 9028
2 25544 51
6394 17
0506 0002936 206
8757 153
2244 15
54187578 38568
Satellite: ISS
Catalog Number: 25544
Epoch time: 18168
52146584 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 17
0506 deg
Eccentricity:
0002936
Arg of perigee: 206
8757 deg
Mean anomaly: 153
2244 deg
Mean motion: 15
54187578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 330
Coasting Arc #4 (Orbit 3871)
---------------------------------------
Vector Time (GMT): 2018/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 532465
11 A = 6777712
41 meter
Y = 4306163
42 meter E =
0005120
Z = 5205939
06 I = 51
70140
XDOT = -7549
783416 Wp = 157
15899
YDOT = -558
529254 meter/sec RA = 11
59786 deg
ZDOT = 1229
172291 TA = 281
02865
MA = 281
08623
Ha = 220
691 n
mi
Hp = 215
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1746932
76 X = 458985
39
Y = 14127832
75 feet Y = 4311706
34 meter
Z = 17079852
55 Z = 5208347
61
XDOT = -24769
630629 XDOT = -7548
947285
YDOT = -1832
445059 feet/sec YDOT = -642
951607 meter/sec
ZDOT = 4032
717491 ZDOT = 1192
500394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14210876
91 X = 4331475
28
Y = -595450
17 feet Y = -181493
21 meter
Z = 17089915
50 Z = 5209006
24
XDOT = -3685
102321 XDOT = -1123
219187
YDOT = 23558
983239 feet/sec YDOT = 7180
778091 meter/sec
ZDOT = 3868
690842 ZDOT = 1179
176969
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 18169
55025990
00016717 00000-0 10270-3 0 9030
2 25544 51
6400 11
9209 0002855 208
6358 151
4638 15
54161966 38724
Satellite: ISS
Catalog Number: 25544
Epoch time: 18169
55025990 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 11
9209 deg
Eccentricity:
0002855
Arg of perigee: 208
6358 deg
Mean anomaly: 151
4638 deg
Mean motion: 15
54161966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3872
Checksum: 318
Coasting Arc #5 (Orbit 3886)
---------------------------------------
Vector Time (GMT): 2018/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1307791
53 A = 6777358
05 meter
Y = -4053959
71 meter E =
0013586
Z = -5283066
23 I = 51
66606
XDOT = 7483
738704 Wp = 106
72135
YDOT = 1451
850306 meter/sec RA = 6
59941 deg
ZDOT = 736
229914 TA = 170
33104
MA = 170
30487
Ha = 220
612 n
mi
Hp = 215
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4290654
64 X = 1378688
97
Y = -13300392
73 feet Y = -4038938
13 meter
Z = -17332894
47 Z = -5276541
70
XDOT = 24552
948504 XDOT = 7463
371324
YDOT = 4763
288406 feet/sec YDOT = 1535
424676 meter/sec
ZDOT = 2415
452473 ZDOT = 772
533713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13034152
61 X = -3972809
72
Y = -5143502
75 feet Y = -1567739
64 meter
Z = -17303024
01 Z = -5273961
72
XDOT = 5755
231681 XDOT = 1754
194616
YDOT = -23280
622202 feet/sec YDOT = -7095
933647 meter/sec
ZDOT = 2577
673306 ZDOT = 785
674824
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 18170
51475056
00016717 00000-0 10270-3 0 9041
2 25544 51
6382 7
1114 0002893 211
1340 148
9642 15
54198747 38876
Satellite: ISS
Catalog Number: 25544
Epoch time: 18170
51475056 = yrday
fracday
Element set: 904
Inclination: 51
6382 deg
RA of node: 7
1114 deg
Eccentricity:
0002893
Arg of perigee: 211
1340 deg
Mean anomaly: 148
9642 deg
Mean motion: 15
54198747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3887
Checksum: 311
Coasting Arc #6 (Orbit 3902)
---------------------------------------
Vector Time (GMT): 2018/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3060444
56 A = 6779525
30 meter
Y = 3700446
27 meter E =
0004986
Z = 4781972
91 I = 51
64077
XDOT = -6843
011930 Wp = 75
78208
YDOT = -2267
144906 meter/sec RA = 1
60295 deg
ZDOT = -2621
622910 TA = 40
07615
MA = 40
03937
Ha = 220
574 n
mi
Hp = 215
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10040828
61 X = -3124824
70
Y = 12140571
77 feet Y = 3665861
86 meter
Z = 15688887
50 Z = 4766950
37
XDOT = -22450
826542 XDOT = -6804
417107
YDOT = -7438
139456 feet/sec YDOT = -2343
452147 meter/sec
ZDOT = -8601
125033 ZDOT = -2654
770207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11738779
86 X = 3577980
10
Y = 10608330
61 feet Y = 3233419
17 meter
Z = 15621052
53 Z = 4761296
81
XDOT = -7529
134171 XDOT = -2294
880095
YDOT = 21231
630393 feet/sec YDOT = 6471
400944 meter/sec
ZDOT = -8749
074573 ZDOT = -2666
717930
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 18171
54353996
00016717 00000-0 10270-3 0 9054
2 25544 51
6387 1
9828 0003021 217
7469 142
3472 15
54189479 39033
Satellite: ISS
Catalog Number: 25544
Epoch time: 18171
54353996 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 1
9828 deg
Eccentricity:
0003021
Arg of perigee: 217
7469 deg
Mean anomaly: 142
3472 deg
Mean motion: 15
54189479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3903
Checksum: 331
Coasting Arc #7 (Orbit 3914)
---------------------------------------
Vector Time (GMT): 2018/172/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3137512
10 A = 6780709
96 meter
Y = -3818727
78 meter E =
0008715
Z = -4650897
77 I = 51
61976
XDOT = 6788
405717 Wp = 126
52914
YDOT = 2025
602362 meter/sec RA = 357
59396 deg
ZDOT = 2915
045031 TA = 172
51784
MA = 172
50483
Ha = 220
411 n
mi
Hp = 215
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10293674
88 X = 3202572
55
Y = -12528634
44 feet Y = -3783277
76 meter
Z = -15258850
94 Z = -4635499
17
XDOT = 22271
672300 XDOT = 6751
090622
YDOT = 6645
677040 feet/sec YDOT = 2101
306088 meter/sec
ZDOT = 9563
796033 ZDOT = 2947
930253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5981823
70 X = 1823259
86
Y = -15141378
77 feet Y = -4615092
25 meter
Z = -15189318
28 Z = -4629704
21
XDOT = 22069
437831 XDOT = 6726
764651
YDOT = -1026
691568 feet/sec YDOT = -312
935590 meter/sec
ZDOT = 9710
603989 ZDOT = 2959
792096
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 18172
31513167
00016717 00000-0 10270-3 0 9069
2 25544 51
6424 358
1385 0003261 237
8388 122
2448 15
53972724 39154
Satellite: ISS
Catalog Number: 25544
Epoch time: 18172
31513167 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 358
1385 deg
Eccentricity:
0003261
Arg of perigee: 237
8388 deg
Mean anomaly: 122
2448 deg
Mean motion: 15
53972724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3915
Checksum: 317
Coasting Arc #8 (Orbit 3930)
---------------------------------------
Vector Time (GMT): 2018/173/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4557351
80 A = 6784323
36 meter
Y = 3481452
80 meter E =
0009348
Z = 3615739
49 I = 51
59856
XDOT = -5629
122576 Wp = 94
65937
YDOT = -2787
710673 meter/sec RA = 352
60529 deg
ZDOT = -4401
815831 TA = 42
45488
MA = 42
38261
Ha = 220
466 n
mi
Hp = 215
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14951941
61 X = -4613507
03
Y = 11422089
23 feet Y = 3430175
01 meter
Z = 11862662
36 Z = 3593465
37
XDOT = -18468
249921 XDOT = -5576
149534
YDOT = -9146
032392 feet/sec YDOT = -2850
362778 meter/sec
ZDOT = -14441
652990 ZDOT = -4429
031812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10463069
51 X = -3189143
59
Y = 15713589
15 feet Y = 4789501
97 meter
Z = 11762428
80 Z = 3585188
30
XDOT = -19208
348389 XDOT = -5854
704589
YDOT = -1866
510040 feet/sec YDOT = -568
912260 meter/sec
ZDOT = -14562
959073 ZDOT = -4438
789925
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 18173
34406918
00016717 00000-0 10270-3 0 9079
2 25544 51
6420 353
0110 0003086 241
1238 118
9605 15
53974910 39311
Satellite: ISS
Catalog Number: 25544
Epoch time: 18173
34406918 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 353
0110 deg
Eccentricity:
0003086
Arg of perigee: 241
1238 deg
Mean anomaly: 118
9605 deg
Mean motion: 15
53974910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3931
Checksum: 294
Coasting Arc #9 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2018/174/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5628141
98 A = 6787670
52 meter
Y = -3056659
56 meter E =
0003410
Z = -2243045
22 I = 51
57703
XDOT = 4082
885296 Wp = 20
42796
YDOT = 3526
103053 meter/sec RA = 347
62316 deg
ZDOT = 5445
089743 TA = 314
61721
MA = 314
64502
Ha = 220
264 n
mi
Hp = 215
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18465032
75 X = 5672799
66
Y = -10028410
64 feet Y = -2993471
85 meter
Z = -7359072
24 Z = -2215597
44
XDOT = 13395
292966 XDOT = 4016
702536
YDOT = 11568
579570 feet/sec YDOT = 3571
390028 meter/sec
ZDOT = 17864
467660 ZDOT = 5464
762702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13941320
51 X = 4249314
49
Y = -15778644
51 feet Y = -4809330
85 meter
Z = -7235769
38 Z = -2205462
51
XDOT = 15292
742414 XDOT = 4661
227888
YDOT = 5288
229005 feet/sec YDOT = 1611
852201 meter/sec
ZDOT = 17951
897339 ZDOT = 5471
738309
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 18174
30869561
00016717 00000-0 10270-3 0 9084
2 25544 51
6417 348
2033 0003221 246
0691 114
0125 15
53988642 39462
Satellite: ISS
Catalog Number: 25544
Epoch time: 18174
30869561 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 348
2033 deg
Eccentricity:
0003221
Arg of perigee: 246
0691 deg
Mean anomaly: 114
0125 deg
Mean motion: 15
53988642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 310
Coasting Arc #10 (Orbit 3961)
---------------------------------------
Vector Time (GMT): 2018/175/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6279286
68 A = 6789721
77 meter
Y = 2486062
60 meter E =
0011852
Z = 629850
30 I = 51
55170
XDOT = -2284
731431 Wp = 142
19746
YDOT = -4247
024894 meter/sec RA = 342
64713 deg
ZDOT = -5963
951203 TA = 30
99302
MA = 30
92313
Ha = 220
274 n
mi
Hp = 216
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20601334
24 X = -6309679
31
Y = 8156373
35 feet Y = 2415673
27 meter
Z = 2066437
99 Z = 599274
09
XDOT = -7495
838028 XDOT = -2208
100394
YDOT = -13933
808707 feet/sec YDOT = -4272
145092 meter/sec
ZDOT = -19566
769040 ZDOT = -5974
864106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16301858
00 X = -4968806
32
Y = 15024613
81 feet Y = 4579502
29 meter
Z = 1929240
89 Z = 588032
62
XDOT = -10789
290010 XDOT = -3288
575595
YDOT = -9165
109432 feet/sec YDOT = -2793
525355 meter/sec
ZDOT = -19614
886030 ZDOT = -5978
617262
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 18175
33763043
00016717 00000-0 10270-3 0 9097
2 25544 51
6419 343
0757 0003265 247
6428 112
4378 15
53943729 39620
Satellite: ISS
Catalog Number: 25544
Epoch time: 18175
33763043 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 343
0757 deg
Eccentricity:
0003265
Arg of perigee: 247
6428 deg
Mean anomaly: 112
4378 deg
Mean motion: 15
53943729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3962
Checksum: 331
Coasting Arc #11 (Orbit 3977)
---------------------------------------
Vector Time (GMT): 2018/176/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6466431
65 A = 6789228
09 meter
Y = -1776154
24 meter E =
0010549
Z = 1024013
98 I = 51
51937
XDOT = 406
304167 Wp = 50
14794
YDOT = 4894
264318 meter/sec RA = 337
66936 deg
ZDOT = 5889
667988 TA = 320
97020
MA = 321
04627
Ha = 220
064 n
mi
Hp = 216
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21215326
95 X = 6480838
37
Y = -5827277
69 feet Y = -1703761
74 meter
Z = 3359625
92 Z = 1055460
48
XDOT = 1333
018919 XDOT = 322
935990
YDOT = 16057
297630 feet/sec YDOT = 4898
340887 meter/sec
ZDOT = 19323
057705 ZDOT = 5891
439909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17451758
18 X = 5319295
89
Y = -13361000
53 feet Y = -4072432
96 meter
Z = 3500592
88 Z = 1066980
71
XDOT = 6174
718990 XDOT = 1882
054348
YDOT = 13157
579877 feet/sec YDOT = 4010
430346 meter/sec
ZDOT = 19330
175426 ZDOT = 5891
837470
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 18176
36655898
00016717 00000-0 10270-3 0 9101
2 25544 51
6418 337
9465 0003308 256
2991 103
7793 15
53998026 39787
Satellite: ISS
Catalog Number: 25544
Epoch time: 18176
36655898 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 337
9465 deg
Eccentricity:
0003308
Arg of perigee: 256
2991 deg
Mean anomaly: 103
7793 deg
Mean motion: 15
53998026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3978
Checksum: 362
Coasting Arc #12 (Orbit 3992)
---------------------------------------
Vector Time (GMT): 2018/177/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6206113
07 A = 6786862
16 meter
Y = 877317
06 meter E =
0003667
Z = -2598184
59 I = 51
47989
XDOT = 1421
615047 Wp = 168
07458
YDOT = -5420
416730 meter/sec RA = 332
68696 deg
ZDOT = -5230
842952 TA = 41
22907
MA = 41
20138
Ha = 220
026 n
mi
Hp = 216
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20361263
34 X = -6202841
60
Y = 2878336
81 feet Y = 807934
73 meter
Z = -8524227
67 Z = -2628323
67
XDOT = 4664
091363 XDOT = 1507
530661
YDOT = -17783
519455 feet/sec YDOT = -5404
038030 meter/sec
ZDOT = -17161
558240 ZDOT = -5223
729427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17556734
82 X = -5351292
77
Y = 10597535
47 feet Y = 3230128
81 meter
Z = -8659193
36 Z = -2639322
14
XDOT = -1794
126478 XDOT = -546
849751
YDOT = -16955
423355 feet/sec YDOT = -5168
013039 meter/sec
ZDOT = -17128
844448 ZDOT = -5220
871788
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 18177
33118061
00016717 00000-0 10270-3 0 9116
2 25544 51
6406 333
1391 0003365 259
1839 100
8935 15
53960700 39937
Satellite: ISS
Catalog Number: 25544
Epoch time: 18177
33118061 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 333
1391 deg
Eccentricity:
0003365
Arg of perigee: 259
1839 deg
Mean anomaly: 100
8935 deg
Mean motion: 15
53960700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3993
Checksum: 307
Coasting Arc #13 (Orbit 4008)
---------------------------------------
Vector Time (GMT): 2018/178/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5547259
14 A = 6783237
62 meter
Y = 166271
05 meter E =
0007946
Z = 3895335
68 I = 51
43921
XDOT = -3033
264295 Wp = 105
13677
YDOT = 5752
098602 meter/sec RA = 327
69365 deg
ZDOT = 4065
098884 TA = 302
14571
MA = 302
22278
Ha = 219
942 n
mi
Hp = 216
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18199669
11 X = 5526066
14
Y = 545508
68 feet Y = 228185
17 meter
Z = 12779972
69 Z = 3922230
83
XDOT = -9951
654511 XDOT = -3117
106454
YDOT = 18871
714573 feet/sec YDOT = 5717
709080 meter/sec
ZDOT = 13336
938596 ZDOT = 4050
161697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16766600
53 X = 5110459
84
Y = -6878793
59 feet Y = -2096656
29 meter
Z = 12900253
59 Z = 3931997
30
XDOT = -1984
181632 XDOT = -604
778561
YDOT = 20102
974898 feet/sec YDOT = 6127
386749 meter/sec
ZDOT = 13269
178821 ZDOT = 4044
445705
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 18178
36010871
00016717 00000-0 10270-3 0 9121
2 25544 51
6408 328
0107 0003284 265
8269 94
2509 15
53968674 40098
Satellite: ISS
Catalog Number: 25544
Epoch time: 18178
36010871 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 328
0107 deg
Eccentricity:
0003284
Arg of perigee: 265
8269 deg
Mean anomaly: 94
2509 deg
Mean motion: 15
53968674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4009
Checksum: 323
Coasting Arc #14 (Orbit 4023)
---------------------------------------
Vector Time (GMT): 2018/179/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4576037
43 A = 6779738
49 meter
Y = -1354143
21 meter E =
0008530
Z = -4823844
79 I = 51
40005
XDOT = 4339
145855 Wp = 65
34296
YDOT = -5803
343074 meter/sec RA = 322
68766 deg
ZDOT = -2487
113384 TA = 180
11266
MA = 180
11285
Ha = 219
946 n
mi
Hp = 215
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15013246
15 X = -4537123
37
Y = -4442727
07 feet Y = -1405097
23 meter
Z = -15826262
43 Z = -4845979
18
XDOT = 14236
042830 XDOT = 4415
798948
YDOT = -19039
839480 feet/sec YDOT = -5754
390743 meter/sec
ZDOT = -8159
820813 ZDOT = -2465
850235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15388568
57 X = -4690435
70
Y = 2278287
21 feet Y = 694421
94 meter
Z = -15925053
56 Z = -4853956
33
XDOT = 5061
883656 XDOT = 1542
862138
YDOT = -22175
282152 feet/sec YDOT = -6759
026000 meter/sec
ZDOT = -8063
763532 ZDOT = -2457
835125
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 18179
32472431
00016717 00000-0 10270-3 0 9133
2 25544 51
6404 323
2020 0003411 269
3468 90
7294 15
53996588 40241
Satellite: ISS
Catalog Number: 25544
Epoch time: 18179
32472431 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 323
2020 deg
Eccentricity:
0003411
Arg of perigee: 269
3468 deg
Mean anomaly: 90
7294 deg
Mean motion: 15
53996588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4024
Checksum: 308
Coasting Arc #15 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2018/179/14:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 40358
66 A = 6780171
32 meter
Y = 4836687
63 meter E =
0004769
Z = 4749543
10 I = 51
39473
XDOT = -6684
205987 Wp = 49
62936
YDOT = 2664
612556 meter/sec RA = 321
15270 deg
ZDOT = -2651
912828 TA = 66
65966
MA = 66
60949
Ha = 220
078 n
mi
Hp = 216
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 132410
30 X = -36800
12
Y = 15868397
74 feet Y = 4836706
74 meter
Z = 15582490
48 Z = 4749552
55
XDOT = -21929
809668 XDOT = -6700
624132
YDOT = 8742
167179 feet/sec YDOT = 2589
773799 meter/sec
ZDOT = -8700
501403 ZDOT = -2684
421596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11631593
57 X = 3545309
72
Y = -10795958
63 feet Y = -3290608
19 meter
Z = 15581748
85 Z = 4749317
05
XDOT = 20480
239790 XDOT = 6242
377088
YDOT = 9274
881641 feet/sec YDOT = 2826
983924 meter/sec
ZDOT = -8846
350645 ZDOT = -2696
367677
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 18179
64626465
00016717 00000-0 10270-3 0 9147
2 25544 51
6418 321
5964 0003163 260
8487 99
2308 15
53986514 40298
Satellite: ISS
Catalog Number: 25544
Epoch time: 18179
64626465 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 321
5964 deg
Eccentricity:
0003163
Arg of perigee: 260
8487 deg
Mean anomaly: 99
2308 deg
Mean motion: 15
53986514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 339
Coasting Arc #16 (Orbit 4040)
---------------------------------------
Vector Time (GMT): 2018/180/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1472345
54 A = 6778599
84 meter
Y = -4209910
69 meter E =
0010619
Z = -5114282
75 I = 51
36536
XDOT = 6273
357506 Wp = 106
39954
YDOT = -4104
829808 meter/sec RA = 317
14965 deg
ZDOT = 1572
712849 TA = 178
83996
MA = 178
83749
Ha = 220
089 n
mi
Hp = 215
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4830530
00 X = -1400317
49
Y = -13812042
93 feet Y = -4225971
91 meter
Z = -16779142
89 Z = -5121260
57
XDOT = 20581
881581 XDOT = 6311
153257
YDOT = -13467
289395 feet/sec YDOT = -4034
465724 meter/sec
ZDOT = 5159
819057 ZDOT = 1603
277500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14421086
04 X = -4395547
02
Y = -2261226
49 feet Y = -689221
83 meter
Z = -16809679
31 Z = -5123590
25
XDOT = -2505
706689 XDOT = -763
739399
YDOT = -23403
780248 feet/sec YDOT = -7133
472219 meter/sec
ZDOT = 5297
199088 ZDOT = 1614
586282
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 18180
41795601
00016717 00000-0 10270-3 0 9154
2 25544 51
6378 317
7501 0003051 266
1993 93
8811 15
53997681 40414
Satellite: ISS
Catalog Number: 25544
Epoch time: 18180
41795601 = yrday
fracday
Element set: 915
Inclination: 51
6378 deg
RA of node: 317
7501 deg
Eccentricity:
0003051
Arg of perigee: 266
1993 deg
Mean anomaly: 93
8811 deg
Mean motion: 15
53997681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4041
Checksum: 322
Coasting Arc #17 (Orbit 4056)
---------------------------------------
Vector Time (GMT): 2018/181/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 115127
03 A = 6781502
69 meter
Y = 5140135
05 meter E =
0006402
Z = 4419061
09 I = 51
35073
XDOT = -6250
477677 Wp = 60
07200
YDOT = 2979
589720 meter/sec RA = 312
13699 deg
ZDOT = -3296
210347 TA = 63
35207
MA = 63
28652
Ha = 220
066 n
mi
Hp = 216
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 377713
34 X = 36174
86
Y = 16863960
13 feet Y = 5140980
37 meter
Z = 14498231
93 Z = 4419429
35
XDOT = -20506
816525 XDOT = -6267
320662
YDOT = 9775
556825 feet/sec YDOT = 2909
598890 meter/sec
ZDOT = -10814
338409 ZDOT = -3326
613106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15182073
62 X = 4627496
04
Y = 7349580
90 feet Y = 2240152
26 meter
Z = 14499063
73 Z = 4419314
62
XDOT = 51
857624 XDOT = 15
806204
YDOT = 21539
902159 feet/sec YDOT = 6565
362178 meter/sec
ZDOT = -10950
806666 ZDOT = -3337
805872
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 18181
44687688
00016717 00000-0 10270-3 0 9164
2 25544 51
6373 312
6221 0003176 269
4727 90
6061 15
53970766 40575
Satellite: ISS
Catalog Number: 25544
Epoch time: 18181
44687688 = yrday
fracday
Element set: 916
Inclination: 51
6373 deg
RA of node: 312
6221 deg
Eccentricity:
0003176
Arg of perigee: 269
4727 deg
Mean anomaly: 90
6061 deg
Mean motion: 15
53970766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4057
Checksum: 333
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