[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 11th 2019
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) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
107/20:48:33
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 217
3
109/09:19:21
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
4
114/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
2
Coasting Arc #1 (Orbit 473)
---------------------------------------
Vector Time (GMT): 2019/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6385498
98 A = 6793832
69 meter
Y = -2243100
63 meter E =
0012379
Z = 526928
94 I = 51
51526
XDOT = 1140
325399 Wp = 56
40653
YDOT = 4670
913841 meter/sec RA = 337
09601 deg
ZDOT = 5970
370828 TA = 309
28434
MA = 309
39407
Ha = 223
654 n
mi
Hp = 217
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20949799
81 X = 6407547
83
Y = -7359254
03 feet Y = -2171570
22 meter
Z = 1728769
49 Z = 558001
21
XDOT = 3741
225062 XDOT = 1059
008120
YDOT = 15324
520476 feet/sec YDOT = 4683
211177 meter/sec
ZDOT = 19587
830802 ZDOT = 5975
712579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17745338
58 X = 5408779
20
Y = -13328511
67 feet Y = -4062530
36 meter
Z = 1869521
66 Z = 569830
20
XDOT = 7090
094788 XDOT = 2161
060891
YDOT = 12230
652727 feet/sec YDOT = 3727
902951 meter/sec
ZDOT = 19611
426309 ZDOT = 5977
562739
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 19100
56327200
00016717 00000-0 10270-3 0 9003
2 25544 51
6425 337
3821 0001431 171
7268 188
3908 15
52533859 4741
Satellite: ISS
Catalog Number: 25544
Epoch time: 19100
56327200 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 337
3821 deg
Eccentricity:
0001431
Arg of perigee: 171
7268 deg
Mean anomaly: 188
3908 deg
Mean motion: 15
52533859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 474
Checksum: 298
Coasting Arc #2 (Orbit 488)
---------------------------------------
Vector Time (GMT): 2019/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6318247
47 A = 6792802
99 meter
Y = 1809521
49 meter E =
0008827
Z = -1701945
89 I = 51
48058
XDOT = 51
687487 Wp = 147
36074
YDOT = -5143
786457 meter/sec RA = 332
12292 deg
ZDOT = -5681
853847 TA = 51
32713
MA = 51
24819
Ha = 223
615 n
mi
Hp = 217
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20729158
35 X = -6329745
30
Y = 5936750
30 feet Y = 1738802
13 meter
Z = -5583811
96 Z = -1732665
69
XDOT = 169
578371 XDOT = 136
802391
YDOT = -16875
939821 feet/sec YDOT = -5142
732573 meter/sec
ZDOT = -18641
252779 ZDOT = -5681
396011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17731931
41 X = -5404692
69
Y = 12204459
66 feet Y = 3719919
30 meter
Z = -5722913
52 Z = -1744344
04
XDOT = -4194
583953 XDOT = -1278
509189
YDOT = -14802
722539 feet/sec YDOT = -4511
869830 meter/sec
ZDOT = -18638
574109 ZDOT = -5681
037388
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 19101
52880299
00016717 00000-0 10270-3 0 9013
2 25544 51
6418 332
5811 0001559 178
6639 181
4518 15
52490930 4897
Satellite: ISS
Catalog Number: 25544
Epoch time: 19101
52880299 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 332
5811 deg
Eccentricity:
0001559
Arg of perigee: 178
6639 deg
Mean anomaly: 181
4518 deg
Mean motion: 15
52490930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 489
Checksum: 324
Coasting Arc #3 (Orbit 504)
---------------------------------------
Vector Time (GMT): 2019/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6062109
09 A = 6790672
62 meter
Y = -1298593
07 meter E =
0013137
Z = 2757905
98 I = 51
44509
XDOT = -1139
891318 Wp = 85
08929
YDOT = 5593
193585 meter/sec RA = 327
14352 deg
ZDOT = 5119
222283 TA = 306
22595
MA = 306
34733
Ha = 223
480 n
mi
Hp = 217
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19888809
34 X = 6062783
37
Y = -4260475
95 feet Y = -1230798
54 meter
Z = 9048247
96 Z = 2787355
14
XDOT = -3739
800912 XDOT = -1227
217670
YDOT = 18350
372653 feet/sec YDOT = 5579
958276 meter/sec
ZDOT = 16795
348696 ZDOT = 5113
472978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17265521
38 X = 5262530
92
Y = -10638998
37 feet Y = -3242766
70 meter
Z = 9181539
56 Z = 2798533
26
XDOT = 1723
993803 XDOT = 525
473311
YDOT = 17325
049204 feet/sec YDOT = 5280
674997 meter/sec
ZDOT = 16768
700746 ZDOT = 5111
099988
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 19102
55869748
00016717 00000-0 10270-3 0 9024
2 25544 51
6419 327
4589 0001332 184
2628 175
8512 15
52528501 5059
Satellite: ISS
Catalog Number: 25544
Epoch time: 19102
55869748 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 327
4589 deg
Eccentricity:
0001332
Arg of perigee: 184
2628 deg
Mean anomaly: 175
8512 deg
Mean motion: 15
52528501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 505
Checksum: 317
Coasting Arc #4 (Orbit 519)
---------------------------------------
Vector Time (GMT): 2019/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5651724
49 A = 6788047
08 meter
Y = 642255
25 meter E =
0005470
Z = -3709173
46 I = 51
40845
XDOT = 2128
154969 Wp = 90
55777
YDOT = -5982
753845 meter/sec RA = 322
15756 deg
ZDOT = -4284
176090 TA = 133
77609
MA = 133
73082
Ha = 223
441 n
mi
Hp = 217
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18542403
19 X = -5640469
24
Y = 2107136
64 feet Y = 579116
58 meter
Z = -12169204
26 Z = -3736600
06
XDOT = 6982
135725 XDOT = 2215
707777
YDOT = -19628
457496 feet/sec YDOT = -5958
465856 meter/sec
ZDOT = -14055
695832 ZDOT = -4273
625579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16553524
35 X = -5045514
22
Y = 8438400
14 feet Y = 2572024
36 meter
Z = -12293270
84 Z = -3746988
95
XDOT = 368
392502 XDOT = 112
286034
YDOT = -19657
305701 feet/sec YDOT = -5991
546778 meter/sec
ZDOT = -14007
307208 ZDOT = -4269
427237
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 19103
52421976
00016717 00000-0 10270-3 0 9030
2 25544 51
6414 322
6568 0001340 190
7072 169
4052 15
52528275 5205
Satellite: ISS
Catalog Number: 25544
Epoch time: 19103
52421976 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 322
6568 deg
Eccentricity:
0001340
Arg of perigee: 190
7072 deg
Mean anomaly: 169
4052 deg
Mean motion: 15
52528275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 520
Checksum: 289
Coasting Arc #5 (Orbit 535)
---------------------------------------
Vector Time (GMT): 2019/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5120448
45 A = 6785530
06 meter
Y = 97951
89 meter E =
0009434
Z = 4446700
16 I = 51
37338
XDOT = -2953
950051 Wp = 118
42061
YDOT = 6283
738965 meter/sec RA = 317
16546 deg
ZDOT = 3253
424185 TA = 298
63638
MA = 298
73123
Ha = 223
415 n
mi
Hp = 217
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16799371
56 X = 5097373
02
Y = 321364
46 feet Y = 155083
46 meter
Z = 14588911
27 Z = 4471517
26
XDOT = -9691
437174 XDOT = -3039
800347
YDOT = 20615
941487 feet/sec YDOT = 6250
225921 meter/sec
ZDOT = 10673
963860 ZDOT = 3238
866314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15658589
35 X = 4772738
03
Y = -5817643
01 feet Y = -1773217
59 meter
Z = 14701091
85 Z = 4480892
80
XDOT = -1956
670389 XDOT = -596
393134
YDOT = 21617
954874 feet/sec YDOT = 6589
152646 meter/sec
ZDOT = 10607
438715 ZDOT = 3233
147320
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 19104
55410932
00016717 00000-0 10270-3 0 9045
2 25544 51
6405 317
5352 0001245 186
8466 173
2669 15
52511270 5367
Satellite: ISS
Catalog Number: 25544
Epoch time: 19104
55410932 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 317
5352 deg
Eccentricity:
0001245
Arg of perigee: 186
8466 deg
Mean anomaly: 173
2669 deg
Mean motion: 15
52511270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 536
Checksum: 296
Coasting Arc #6 (Orbit 550)
---------------------------------------
Vector Time (GMT): 2019/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4511150
28 A = 6783310
66 meter
Y = -959695
33 meter E =
0012055
Z = -4985084
87 I = 51
34144
XDOT = 3620
850549 Wp = 80
20579
YDOT = -6430
136564 meter/sec RA = 312
16634 deg
ZDOT = -2040
946605 TA = 169
84662
MA = 169
82225
Ha = 223
375 n
mi
Hp = 217
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14800361
80 X = -4475868
69
Y = -3148606
73 feet Y = -1009945
17 meter
Z = -16355265
33 Z = -5006912
55
XDOT = 11879
430936 XDOT = 3702
398820
YDOT = -21096
248568 feet/sec YDOT = -6389
189826 meter/sec
ZDOT = -6696
019045 ZDOT = -2023
159490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14778845
35 X = -4504592
06
Y = 2704862
78 feet Y = 824442
18 meter
Z = -16453831
92 Z = -5015127
97
XDOT = 3151
635992 XDOT = 960
618650
YDOT = -22974
834406 feet/sec YDOT = -7002
729527 meter/sec
ZDOT = -6614
896671 ZDOT = -2016
220505
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 19105
51962570
00016717 00000-0 10270-3 0 9053
2 25544 51
6393 312
7332 0001373 198
2501 161
8601 15
52546704 5513
Satellite: ISS
Catalog Number: 25544
Epoch time: 19105
51962570 = yrday
fracday
Element set: 905
Inclination: 51
6393 deg
RA of node: 312
7332 deg
Eccentricity:
0001373
Arg of perigee: 198
2501 deg
Mean anomaly: 161
8601 deg
Mean motion: 15
52546704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 551
Checksum: 290
Coasting Arc #7 (Orbit 566)
---------------------------------------
Vector Time (GMT): 2019/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3858367
74 A = 6782192
47 meter
Y = 1871917
71 meter E =
0003515
Z = 5252517
60 I = 51
31624
XDOT = -4125
059028 Wp = 138
83629
YDOT = 6421
278072 meter/sec RA = 307
16242 deg
ZDOT = 738
836406 TA = 304
05651
MA = 304
08988
Ha = 223
280 n
mi
Hp = 217
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12658686
81 X = 3811634
83
Y = 6141462
31 feet Y = 1914803
76 meter
Z = 17232669
30 Z = 5271146
48
XDOT = -13533
658228 XDOT = -4200
145862
YDOT = 21067
185276 feet/sec YDOT = 6374
728991 meter/sec
ZDOT = 2424
003958 ZDOT = 718
615566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13951550
19 X = 4252432
50
Y = 641752
85 feet Y = 195606
27 meter
Z = 17316674
12 Z = 5278122
27
XDOT = -3996
325182 XDOT = -1218
079915
YDOT = 23702
616637 feet/sec YDOT = 7224
557551 meter/sec
ZDOT = 2331
899947 ZDOT = 710
763104
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 19106
54950835
00016717 00000-0 10270-3 0 9069
2 25544 51
6396 307
6110 0001333 199
4376 160
6725 15
52523234 5676
Satellite: ISS
Catalog Number: 25544
Epoch time: 19106
54950835 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 307
6110 deg
Eccentricity:
0001333
Arg of perigee: 199
4376 deg
Mean anomaly: 160
6725 deg
Mean motion: 15
52523234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 567
Checksum: 309
Coasting Arc #8 (Orbit 581)
---------------------------------------
Vector Time (GMT): 2019/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3208023
13 A = 6782065
11 meter
Y = -2835136
43 meter E =
0014369
Z = -5272471
01 I = 51
29477
XDOT = 4466
088438 Wp = 99
85891
YDOT = -6187
712685 meter/sec RA = 302
15461 deg
ZDOT = 608
912168 TA = 175
99696
MA = 175
98545
Ha = 223
360 n
mi
Hp = 217
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10525010
27 X = -3150470
53
Y = -9301628
69 feet Y = -2870689
42 meter
Z = -17298133
23 Z = -5287914
45
XDOT = 14652
521122 XDOT = 4531
991499
YDOT = -20300
894635 feet/sec YDOT = -6137
401220 meter/sec
ZDOT = 1997
743333 ZDOT = 630
767433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13325437
21 X = -4061593
26
Y = -4161669
46 feet Y = -1268476
85 meter
Z = -17367636
03 Z = -5293655
46
XDOT = 4622
636160 XDOT = 1408
979502
YDOT = -23567
016319 feet/sec YDOT = -7183
226574 meter/sec
ZDOT = 2097
191908 ZDOT = 639
224094
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 19107
51501834
00016717 00000-0 10270-3 0 9079
2 25544 51
6375 302
8079 0001339 199
5877 160
5223 15
52559976 5828
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
51501834 = yrday
fracday
Element set: 907
Inclination: 51
6375 deg
RA of node: 302
8079 deg
Eccentricity:
0001339
Arg of perigee: 199
5877 deg
Mean anomaly: 160
5223 deg
Mean motion: 15
52559976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 582
Checksum: 331
Coasting Arc #9 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2019/107/20:48:33
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2650851
88 A = 6793425
16 meter
Y = 6161859
96 meter E =
0013995
Z = 1027297
14 I = 51
32890
XDOT = -4810
895747 Wp = 129
35874
YDOT = -1083
141654 meter/sec RA = 300
31786 deg
ZDOT = -5872
272713 TA = 39
46106
MA = 39
35921
Ha = 223
334 n
mi
Hp = 217
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8697020
59 X = -2724548
60
Y = 20216075
99 feet Y = 6131804
30 meter
Z = 3370397
46 Z = 1014240
71
XDOT = -15783
778697 XDOT = -4769
901748
YDOT = -3553
614349 feet/sec YDOT = -1136
711726 meter/sec
ZDOT = -19265
986592 ZDOT = -5895
542750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15940408
68 X = 4858636
57
Y = -15186504
63 feet Y = -4628846
61 meter
Z = 3310728
39 Z = 1009110
01
XDOT = 11904
207389 XDOT = 3628
402412
YDOT = 8239
418068 feet/sec YDOT = 2511
374627 meter/sec
ZDOT = -19371
051958 ZDOT = -5904
296637
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 19107
90122239
00016717 00000-0 10270-3 0 9081
2 25544 51
6400 300
8885 0001406 198
3352 161
7749 15
52573522 5885
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
90122239 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 300
8885 deg
Eccentricity:
0001406
Arg of perigee: 198
3352 deg
Mean anomaly: 161
7749 deg
Mean motion: 15
52573522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 310
Coasting Arc #10 (Orbit 603)
---------------------------------------
Vector Time (GMT): 2019/108/20:48:33
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3009575
60 A = 6794008
95 meter
Y = -6083597
72 meter E =
0011214
Z = 146379
38 I = 51
31373
XDOT = 4235
482838 Wp = 49
49824
YDOT = 2246
332001 meter/sec RA = 295
33223 deg
ZDOT = 5981
007383 TA = 312
08461
MA = 312
17993
Ha = 223
391 n
mi
Hp = 217
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9873935
71 X = 3076669
41
Y = -19959310
12 feet Y = -6049567
39 meter
Z = 480247
31 Z = 161162
36
XDOT = 13895
941069 XDOT = 4180
996159
YDOT = 7369
855645 feet/sec YDOT = 2293
391924 meter/sec
ZDOT = 19622
727633 ZDOT = 6001
449511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16646985
66 X = -5074001
23
Y = 14787738
11 feet Y = 4507302
57 meter
Z = 547699
10 Z = 166938
69
XDOT = -8907
430215 XDOT = -2714
984730
YDOT = -10789
042326 feet/sec YDOT = -3288
500101 meter/sec
ZDOT = 19714
886869 ZDOT = 6009
097518
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 19108
93109901
00016717 00000-0 10270-3 0 9097
2 25544 51
6393 295
7664 0001306 204
5352 155
5738 15
52516166 6041
Satellite: ISS
Catalog Number: 25544
Epoch time: 19108
93109901 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 295
7664 deg
Eccentricity:
0001306
Arg of perigee: 204
5352 deg
Mean anomaly: 155
5738 deg
Mean motion: 15
52516166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 604
Checksum: 312
Coasting Arc #11 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2019/109/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4468629
76 A = 6789390
81 meter
Y = -3947239
78 meter E =
0011934
Z = 3237521
02 I = 51
29282
XDOT = 1680
552449 Wp = 91
56915
YDOT = 5795
445271 meter/sec RA = 292
75132 deg
ZDOT = 4730
822556 TA = 306
12898
MA = 306
23938
Ha = 223
162 n
mi
Hp = 217
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14660858
79 X = 4496710
50
Y = -12950261
75 feet Y = -3897111
21 meter
Z = 10621788
14 Z = 3259296
72
XDOT = 5513
623520 XDOT = 1592
641193
YDOT = 19013
928055 feet/sec YDOT = 5813
747152 meter/sec
ZDOT = 15521
071377 ZDOT = 4738
772263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17266206
93 X = 5262739
87
Y = -9078485
43 feet Y = -2767122
36 meter
Z = 10720617
70 Z = 3267644
28
XDOT = 35
956264 XDOT = 10
959469
YDOT = 18498
064048 feet/sec YDOT = 5638
209922 meter/sec
ZDOT = 15556
400180 ZDOT = 4741
590775
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 19109
44603299
00016717 00000-0 10270-3 0 9105
2 25544 51
6406 293
2069 0001190 219
4608 140
6457 15
52554473 6123
Satellite: ISS
Catalog Number: 25544
Epoch time: 19109
44603299 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 293
2069 deg
Eccentricity:
0001190
Arg of perigee: 219
4608 deg
Mean anomaly: 140
6457 deg
Mean motion: 15
52554473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 302
Coasting Arc #12 (Orbit 626)
---------------------------------------
Vector Time (GMT): 2019/110/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4444564
35 A = 6786638
14 meter
Y = 3080997
56 meter E =
0006456
Z = -4106812
31 I = 51
27148
XDOT = -1073
678823 Wp = 75
27498
YDOT = -6576
971012 meter/sec RA = 287
75219 deg
ZDOT = -3775
556682 TA = 155
55148
MA = 155
52085
Ha = 223
124 n
mi
Hp = 217
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14581904
03 X = -4458737
66
Y = 10108259
70 feet Y = 3031215
91 meter
Z = -13473793
67 Z = -4128437
25
XDOT = -3522
568318 XDOT = -981
713601
YDOT = -21577
988886 feet/sec YDOT = -6588
463590 meter/sec
ZDOT = -12386
996989 ZDOT = -3780
548652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16378751
12 X = -4992243
34
Y = 6625213
37 feet Y = 2019365
03 meter
Z = -13571846
41 Z = -4136698
79
XDOT = 1937
056396 XDOT = 590
414790
YDOT = -20608
427657 feet/sec YDOT = -6281
448750 meter/sec
ZDOT = -12408
884484 ZDOT = -3782
227991
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 19110
41153390
00016717 00000-0 10270-3 0 9117
2 25544 51
6401 288
4040 0001246 226
0210 134
0839 15
52567005 6270
Satellite: ISS
Catalog Number: 25544
Epoch time: 19110
41153390 = yrday
fracday
Element set: 911
Inclination: 51
6401 deg
RA of node: 288
4040 deg
Eccentricity:
0001246
Arg of perigee: 226
0210 deg
Mean anomaly: 134
0839 deg
Mean motion: 15
52567005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 627
Checksum: 261
Coasting Arc #13 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2019/111/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4374728
37 A = 6784290
78 meter
Y = -2089047
55 meter E =
0007313
Z = 4742707
95 I = 51
25387
XDOT = 552
165125 Wp = 126
37685
YDOT = 7176
014540 meter/sec RA = 282
74831 deg
ZDOT = 2644
415857 TA = 297
34198
MA = 297
41640
Ha = 223
104 n
mi
Hp = 217
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14352783
36 X = 4374725
72
Y = -6853830
54 feet Y = -2040126
22 meter
Z = 15560065
45 Z = 4763959
12
XDOT = 1811
565372 XDOT = 459
034532
YDOT = 23543
354789 feet/sec YDOT = 7181
668550 meter/sec
ZDOT = 8675
905042 ZDOT = 2646
871806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15354159
14 X = 4679947
71
Y = -3771246
03 feet Y = -1149475
79 meter
Z = 15656325
26 Z = 4772047
94
XDOT = -3408
388363 XDOT = -1038
876773
YDOT = 22280
637492 feet/sec YDOT = 6791
138308 meter/sec
ZDOT = 8686
278064 ZDOT = 2647
577554
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 19111
44140109
00016717 00000-0 10270-3 0 9126
2 25544 51
6396 283
2819 0001084 224
4424 135
6641 15
52544292 6438
Satellite: ISS
Catalog Number: 25544
Epoch time: 19111
44140109 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 283
2819 deg
Eccentricity:
0001084
Arg of perigee: 224
4424 deg
Mean anomaly: 135
6641 deg
Mean motion: 15
52544292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 288
Coasting Arc #14 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2019/112/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4310357
64 A = 6782470
39 meter
Y = 977508
62 meter E =
0012790
Z = -5156008
79 I = 51
24102
XDOT = -80
111720 Wp = 82
17520
YDOT = -7533
715929 meter/sec RA = 277
73911 deg
ZDOT = -1362
523364 TA = 174
63958
MA = 174
62588
Ha = 223
077 n
mi
Hp = 217
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14141593
32 X = -4295922
67
Y = 3207049
27 feet Y = 929387
94 meter
Z = -16916039
33 Z = -5176912
14
XDOT = -262
833727 XDOT = 10
756868
YDOT = -24716
915777 feet/sec YDOT = -7534
103703 meter/sec
ZDOT = -4470
221012 ZDOT = -1362
691888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14381090
49 X = -4383356
38
Y = 495376
78 feet Y = 150990
84 meter
Z = -17010615
85 Z = -5184835
71
XDOT = 4481
486543 XDOT = 1365
957098
YDOT = -23266
611512 feet/sec YDOT = -7091
663189 meter/sec
ZDOT = -4470
229578 ZDOT = -1362
525975
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 19112
40689657
00016717 00000-0 10270-3 0 9130
2 25544 51
6388 278
4794 0001266 231
9746 128
1292 15
52584586 6584
Satellite: ISS
Catalog Number: 25544
Epoch time: 19112
40689657 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 278
4794 deg
Eccentricity:
0001266
Arg of perigee: 231
9746 deg
Mean anomaly: 128
1292 deg
Mean motion: 15
52584586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 348
Coasting Arc #15 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2019/113/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4241808
99 A = 6781915
84 meter
Y = 180810
09 meter E =
0001580
Z = 5287341
31 I = 51
23638
XDOT = -350
223536 Wp = 118
35785
YDOT = 7659
463120 meter/sec RA = 272
72778 deg
ZDOT = 18
298227 TA = 331
46246
MA = 331
47111
Ha = 222
951 n
mi
Hp = 217
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13916696
16 X = 4213788
59
Y = 593208
96 feet Y = 228088
16 meter
Z = 17346920
32 Z = 5307878
62
XDOT = -1149
027349 XDOT = -435
936684
YDOT = 25129
472177 feet/sec YDOT = 7655
067422 meter/sec
ZDOT = 60
033552 ZDOT = 16
388964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13491718
33 X = 4112275
75
Y = 2961635
49 feet Y = 902706
50 meter
Z = 17439731
23 Z = 5315630
08
XDOT = -5243
107010 XDOT = -1598
099017
YDOT = 23572
434319 feet/sec YDOT = 7184
877980 meter/sec
ZDOT = 50
650184 ZDOT = 15
438176
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 19113
43675690
00016717 00000-0 10270-3 0 9147
2 25544 51
6396 273
3572 0001247 234
9815 125
1220 15
52560557 6748
Satellite: ISS
Catalog Number: 25544
Epoch time: 19113
43675690 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 273
3572 deg
Eccentricity:
0001247
Arg of perigee: 234
9815 deg
Mean anomaly: 125
1220 deg
Mean motion: 15
52560557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 309
Coasting Arc #16 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2019/114/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4202217
55 A = 6782424
22 meter
Y = -1347224
20 meter E =
0013124
Z = -5162212
54 I = 51
23614
XDOT = 769
912593 Wp = 103
83779
YDOT = -7500
187025 meter/sec RA = 267
71519 deg
ZDOT = 1330
427472 TA = 179
04074
MA = 179
03822
Ha = 223
075 n
mi
Hp = 217
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13786802
97 X = -4161764
82
Y = -4420026
91 feet Y = -1393989
99 meter
Z = -16936392
86 Z = -5182527
30
XDOT = 2525
959952 XDOT = 847
262065
YDOT = -24606
912812 feet/sec YDOT = -7491
144877 meter/sec
ZDOT = 4364
919526 ZDOT = 1334
355083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12821097
79 X = -3907870
61
Y = -6489803
15 feet Y = -1978092
00 meter
Z = -17028091
02 Z = -5190162
14
XDOT = 5812
393660 XDOT = 1771
617588
YDOT = -22985
976803 feet/sec YDOT = -7006
125730 meter/sec
ZDOT = 4383
397068 ZDOT = 1336
059426
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 19114
40224631
00016717 00000-0 10270-3 0 9151
2 25544 51
6378 268
5542 0001177 235
4089 124
6952 15
52592800 6890
Satellite: ISS
Catalog Number: 25544
Epoch time: 19114
40224631 = yrday
fracday
Element set: 915
Inclination: 51
6378 deg
RA of node: 268
5542 deg
Eccentricity:
0001177
Arg of perigee: 235
4089 deg
Mean anomaly: 124
6952 deg
Mean motion: 15
52592800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 315
Coasting Arc #17 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2019/114/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4038374
64 A = 6782573
44 meter
Y = 1873635
32 meter E =
0012802
Z = -5128497
74 I = 51
23664
XDOT = -1524
495856 Wp = 81
79502
YDOT = -7354
027195 meter/sec RA = 267
44036 deg
ZDOT = -1487
667071 TA = 173
78311
MA = 173
76721
Ha = 223
155 n
mi
Hp = 217
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13249260
64 X = -4034114
43
Y = 6147097
49 feet Y = 1828499
37 meter
Z = -16825780
00 Z = -5148104
41
XDOT = -5001
626823 XDOT = -1434
921411
YDOT = -24127
385812 feet/sec YDOT = -7370
574286 meter/sec
ZDOT = -4880
797477 ZDOT = -1494
855229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11488122
62 X = -3501579
78
Y = 8851911
06 feet Y = 2698062
49 meter
Z = -16914588
29 Z = -5155566
51
XDOT = -9444
227009 XDOT = -2878
600392
YDOT = -21635
219407 feet/sec YDOT = -6594
414875 meter/sec
ZDOT = -4912
581241 ZDOT = -1497
354762
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 19114
46661347
00016717 00000-0 10270-3 0 9167
2 25544 51
6377 268
2332 0001152 221
1289 138
9776 15
52593111 6900
Satellite: ISS
Catalog Number: 25544
Epoch time: 19114
46661347 = yrday
fracday
Element set: 916
Inclination: 51
6377 deg
RA of node: 268
2332 deg
Eccentricity:
0001152
Arg of perigee: 221
1289 deg
Mean anomaly: 138
9776 deg
Mean motion: 15
52593111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 311
Coasting Arc #18 (Orbit 705)
---------------------------------------
Vector Time (GMT): 2019/115/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4185751
11 A = 6781958
36 meter
Y = -722036
23 meter E =
0001952
Z = 5285702
88 I = 51
23571
XDOT = 1124
678923 Wp = 125
00895
YDOT = 7583
302806 meter/sec RA = 262
42891 deg
ZDOT = 144
119212 TA = 323
60313
MA = 323
61640
Ha = 223
049 n
mi
Hp = 217
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13732779
24 X = 4167838
90
Y = -2368885
28 feet Y = -675328
54 meter
Z = 17341544
89 Z = 5305992
27
XDOT = 3689
891481 XDOT = 1039
096632
YDOT = 24879
602383 feet/sec YDOT = 7595
401229 meter/sec
ZDOT = 472
832062 ZDOT = 149
374855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12684673
68 X = 3866288
54
Y = -5487074
26 feet Y = -1672460
23 meter
Z = 17433332
79 Z = 5313679
84
XDOT = 9003
951357 XDOT = 2744
404374
YDOT = 22402
062560 feet/sec YDOT = 6828
148668 meter/sec
ZDOT = 495
876246 ZDOT = 151
143080
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 19115
49646790
00016717 00000-0 10270-3 0 9177
2 25544 51
6366 263
1108 0001158 225
6131 134
4926 15
52548861 7062
Satellite: ISS
Catalog Number: 25544
Epoch time: 19115
49646790 = yrday
fracday
Element set: 917
Inclination: 51
6366 deg
RA of node: 263
1108 deg
Eccentricity:
0001158
Arg of perigee: 225
6131 deg
Mean anomaly: 134
4926 deg
Mean motion: 15
52548861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 706
Checksum: 313
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