[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 13th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16989 6378 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
175/23:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 216
2
175/23:24:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 216
3
176/18:02:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 216
3
Coasting Arc #1 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2019/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5865209
59 A = 6797615
95 meter
Y = -3331756
26 meter E =
0011229
Z = -842384
43 I = 51
82172
XDOT = 2993
953730 Wp = 97
17655
YDOT = -3784
940828 meter/sec RA = 23
96365 deg
ZDOT = -5945
129145 TA = 91
89336
MA = 91
76476
Ha = 228
105 n
mi
Hp = 217
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19242813
60 X = -5823425
16
Y = -10930958
85 feet Y = -3397111
42 meter
Z = -2763728
43 Z = -870774
44
XDOT = 9822
682841 XDOT = 3064
933796
YDOT = -12417
784869 feet/sec YDOT = -3751
062851 meter/sec
ZDOT = -19505
016881 ZDOT = -5930
413550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14210494
10 X = -4331358
60
Y = 16944245
28 feet Y = 5164605
96 meter
Z = -2892117
01 Z = -881517
27
XDOT = -9190
762871 XDOT = -2801
344523
YDOT = -10988
557341 feet/sec YDOT = -3349
312278 meter/sec
ZDOT = -19437
781822 ZDOT = -5924
635899
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 19163
53056419
00016717 00000-0 10270-3 0 9000
2 25544 51
6438 24
4170 0007896 37
2549 322
9149 15
51166890 14521
Satellite: ISS
Catalog Number: 25544
Epoch time: 19163
53056419 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 24
4170 deg
Eccentricity:
0007896
Arg of perigee: 37
2549 deg
Mean anomaly: 322
9149 deg
Mean motion: 15
51166890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 315
Coasting Arc #2 (Orbit 1467)
---------------------------------------
Vector Time (GMT): 2019/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5747147
80 A = 6796762
16 meter
Y = 3262125
63 meter E =
0021443
Z = 1538717
55 I = 51
78703
XDOT = -3582
090509 Wp = 54
29729
YDOT = 3569
084715 meter/sec RA = 19
01673 deg
ZDOT = 5768
530381 TA = 322
47824
MA = 322
62770
Ha = 228
079 n
mi
Hp = 217
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18855471
78 X = 5702768
34
Y = 10702511
92 feet Y = 3326145
94 meter
Z = 5048285
93 Z = 1566527
87
XDOT = -11752
265448 XDOT = -3649
755347
YDOT = 11709
595521 feet/sec YDOT = 3528
648236 meter/sec
ZDOT = 18925
624609 ZDOT = 5750
965867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13626086
56 X = 4153231
18
Y = -16826076
12 feet Y = -5128588
00 meter
Z = 5174040
57 Z = 1577047
57
XDOT = 8392
200544 XDOT = 2557
942726
YDOT = 12634
594549 feet/sec YDOT = 3851
024419 meter/sec
ZDOT = 18845
491806 ZDOT = 5744
105902
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 19164
56134486
00016717 00000-0 10270-3 0 9016
2 25544 51
6424 19
3011 0007931 40
8474 319
3270 15
51217208 14682
Satellite: ISS
Catalog Number: 25544
Epoch time: 19164
56134486 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 19
3011 deg
Eccentricity:
0007931
Arg of perigee: 40
8474 deg
Mean anomaly: 319
3270 deg
Mean motion: 15
51217208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1468
Checksum: 292
Coasting Arc #3 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2019/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5544513
47 A = 6795665
70 meter
Y = -3223923
67 meter E =
0009658
Z = -2257449
32 I = 51
75087
XDOT = 4177
849036 Wp = 80
63444
YDOT = -3381
989868 meter/sec RA = 14
06739 deg
ZDOT = -5449
678132 TA = 124
37486
MA = 124
28348
Ha = 228
164 n
mi
Hp = 217
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18190660
99 X = -5497085
03
Y = -10577177
38 feet Y = -3285660
79 meter
Z = -7406329
79 Z = -2284267
99
XDOT = 13706
853794 XDOT = 4241
828646
YDOT = -11095
767282 feet/sec YDOT = -3334
911727 meter/sec
ZDOT = -17879
521432 ZDOT = -5429
228610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13111491
12 X = -3996382
49
Y = 16402892
97 feet Y = 4999601
78 meter
Z = -7527579
47 Z = -2294406
22
XDOT = -7764
555674 XDOT = -2366
636570
YDOT = -14341
743068 feet/sec YDOT = -4371
363287 meter/sec
ZDOT = -17786
324883 ZDOT = -5421
271824
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 19165
52770273
00016717 00000-0 10270-3 0 9024
2 25544 51
6419 14
5056 0007866 43
7959 316
3814 15
51186751 14835
Satellite: ISS
Catalog Number: 25544
Epoch time: 19165
52770273 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 14
5056 deg
Eccentricity:
0007866
Arg of perigee: 43
7959 deg
Mean anomaly: 316
3814 deg
Mean motion: 15
51186751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 323
Coasting Arc #4 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2019/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5269701
23 A = 6794198
47 meter
Y = 3150499
53 meter E =
0020167
Z = 2883492
87 I = 51
71357
XDOT = -4742
504757 Wp = 68
49088
YDOT = 3283
367355 meter/sec RA = 9
11270 deg
ZDOT = 5058
516084 TA = 324
30067
MA = 324
43536
Ha = 228
088 n
mi
Hp = 216
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17289046
04 X = 5220073
28
Y = 10336284
55 feet Y = 3209151
06 meter
Z = 9460278
44 Z = 2908971
28
XDOT = -15559
398810 XDOT = -4803
439480
YDOT = 10772
202607 feet/sec YDOT = 3229
991810 meter/sec
ZDOT = 16596
181379 ZDOT = 5035
331131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12470682
51 X = 3801064
03
Y = -15749273
50 feet Y = -4800378
56 meter
Z = 9575448
88 Z = 2918596
82
XDOT = 7515
446768 XDOT = 2290
708175
YDOT = 16018
876127 feet/sec YDOT = 4882
553443 meter/sec
ZDOT = 16490
589503 ZDOT = 5026
331681
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 19166
55847999
00016717 00000-0 10270-3 0 9039
2 25544 51
6418 9
3888 0007827 47
2081 312
9727 15
51219658 14996
Satellite: ISS
Catalog Number: 25544
Epoch time: 19166
55847999 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 9
3888 deg
Eccentricity:
0007827
Arg of perigee: 47
2081 deg
Mean anomaly: 312
9727 deg
Mean motion: 15
51219658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 359
Coasting Arc #5 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2019/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4917799
78 A = 6792566
76 meter
Y = -3131722
30 meter E =
0012634
Z = -3500568
33 I = 51
67339
XDOT = 5264
134551 Wp = 63
88572
YDOT = -3209
283780 meter/sec RA = 4
15444 deg
ZDOT = -4531
538886 TA = 157
12232
MA = 157
06598
Ha = 228
298 n
mi
Hp = 216
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16134513
72 X = -4865410
57
Y = -10274679
45 feet Y = -3186423
02 meter
Z = -11484804
25 Z = -3524330
60
XDOT = 17270
782646 XDOT = 5321
642238
YDOT = -10529
146260 feet/sec YDOT = -3150
094175 meter/sec
ZDOT = -14867
253562 ZDOT = -4505
828470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12006253
30 X = -3659506
01
Y = 14807545
29 feet Y = 4513339
81 meter
Z = -11592186
31 Z = -3533298
39
XDOT = -7442
342554 XDOT = -2268
426011
YDOT = -17563
106198 feet/sec YDOT = -5353
234769 meter/sec
ZDOT = -14750
216740 ZDOT = -4495
866062
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 19167
52483304
00016717 00000-0 10270-3 0 9044
2 25544 51
6402 4
5922 0008044 51
3336 308
8534 15
51208418 15146
Satellite: ISS
Catalog Number: 25544
Epoch time: 19167
52483304 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 4
5922 deg
Eccentricity:
0008044
Arg of perigee: 51
3336 deg
Mean anomaly: 308
8534 deg
Mean motion: 15
51208418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1514
Checksum: 284
Coasting Arc #6 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2019/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4504168
73 A = 6790943
06 meter
Y = 3107356
09 meter E =
0017103
Z = 4005129
79 I = 51
63410
XDOT = -5739
473622 Wp = 81
63191
YDOT = 3209
900882 meter/sec RA = 359
19222 deg
ZDOT = 3952
225744 TA = 327
24409
MA = 327
35001
Ha = 228
195 n
mi
Hp = 216
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14777456
48 X = 4449631
92
Y = 10194737
82 feet Y = 3157419
16 meter
Z = 13140189
60 Z = 4026877
51
XDOT = -18830
294035 XDOT = -5794
138813
YDOT = 10531
170872 feet/sec YDOT = 3145
411660 meter/sec
ZDOT = 12966
619896 ZDOT = 3924
213343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11540746
67 X = 3517619
58
Y = -13657435
22 feet Y = -4162786
26 meter
Z = 13238433
11 Z = 4035074
41
XDOT = 7697
542427 XDOT = 2346
210932
YDOT = 18987
680059 feet/sec YDOT = 5787
444882 meter/sec
ZDOT = 12839
143507 ZDOT = 3913
370941
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 19168
55560771
00016717 00000-0 10270-3 0 9053
2 25544 51
6397 359
4760 0007866 54
9218 305
2670 15
51205806 15308
Satellite: ISS
Catalog Number: 25544
Epoch time: 19168
55560771 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 359
4760 deg
Eccentricity:
0007866
Arg of perigee: 54
9218 deg
Mean anomaly: 305
2670 deg
Mean motion: 15
51205806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1530
Checksum: 325
Coasting Arc #7 (Orbit 1544)
---------------------------------------
Vector Time (GMT): 2019/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4037137
13 A = 6789291
92 meter
Y = -3155059
93 meter E =
0017415
Z = -4472243
38 I = 51
59517
XDOT = 6124
959809 Wp = 64
42201
YDOT = -3218
045349 meter/sec RA = 354
22504 deg
ZDOT = -3261
410676 TA = 172
62738
MA = 172
60174
Ha = 228
365 n
mi
Hp = 216
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13245200
54 X = -3979832
70
Y = -10351246
49 feet Y = -3199884
76 meter
Z = -14672714
51 Z = -4491715
65
XDOT = 20095
012496 XDOT = 6176
331759
YDOT = -10557
891564 feet/sec YDOT = -3149
263892 meter/sec
ZDOT = -10700
166260 ZDOT = -3231
533855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11340627
11 X = -3456623
14
Y = 12303910
02 feet Y = 3750231
77 meter
Z = -14760628
97 Z = -4499039
71
XDOT = -8065
629373 XDOT = -2458
403833
YDOT = -20097
571309 feet/sec YDOT = -6125
739735 meter/sec
ZDOT = -10564
235879 ZDOT = -3219
979096
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 19169
52195775
00016717 00000-0 10270-3 0 9060
2 25544 51
6395 354
6791 0007999 59
5002 300
6938 15
51215024 15451
Satellite: ISS
Catalog Number: 25544
Epoch time: 19169
52195775 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 354
6791 deg
Eccentricity:
0007999
Arg of perigee: 59
5002 deg
Mean anomaly: 300
6938 deg
Mean motion: 15
51215024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1545
Checksum: 335
Coasting Arc #8 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2019/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3525053
15 A = 6787957
56 meter
Y = 3220095
04 meter E =
0013264
Z = 4813480
16 I = 51
55779
XDOT = -6459
354211 Wp = 88
86095
YDOT = 3273
709849 meter/sec RA = 349
25393 deg
ZDOT = 2534
560884 TA = 336
16149
MA = 336
22286
Ha = 228
336 n
mi
Hp = 216
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11565135
02 X = 3465402
10
Y = 10564616
27 feet Y = 3259180
23 meter
Z = 15792257
74 Z = 4830459
14
XDOT = -21192
106993 XDOT = -6507
793100
YDOT = 10740
517876 feet/sec YDOT = 3201
205518 meter/sec
ZDOT = 8315
488463 ZDOT = 2503
066934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11238445
35 X = 3425478
14
Y = -10799799
18 feet Y = -3291778
79 meter
Z = 15868854
81 Z = 4836826
95
XDOT = 8650
755167 XDOT = 2636
750175
YDOT = 21037
857360 feet/sec YDOT = 6412
338923 meter/sec
ZDOT = 8172
221943 ZDOT = 2490
893248
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 19170
55272843
00016717 00000-0 10270-3 0 9078
2 25544 51
6398 349
5624 0007991 62
6204 297
5759 15
51193301 15619
Satellite: ISS
Catalog Number: 25544
Epoch time: 19170
55272843 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 349
5624 deg
Eccentricity:
0007991
Arg of perigee: 62
6204 deg
Mean anomaly: 297
5759 deg
Mean motion: 15
51193301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1561
Checksum: 331
Coasting Arc #9 (Orbit 1575)
---------------------------------------
Vector Time (GMT): 2019/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2994673
42 A = 6786801
27 meter
Y = -3364825
33 meter E =
0021429
Z = -5095897
84 I = 51
52146
XDOT = 6671
732450 Wp = 73
18153
YDOT = -3310
393886 meter/sec RA = 344
27978 deg
ZDOT = -1734
888714 TA = 179
97279
MA = 179
97268
Ha = 228
484 n
mi
Hp = 216
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9825044
01 X = -2932071
61
Y = -11039453
17 feet Y = -3397962
96 meter
Z = -16718824
94 Z = -5110293
23
XDOT = 21888
885990 XDOT = 6716
681408
YDOT = -10860
872331 feet/sec YDOT = -3235
534278 meter/sec
ZDOT = -5691
892105 ZDOT = -1702
371643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11450002
47 X = -3489960
75
Y = 9226344
53 feet Y = 2812189
81 meter
Z = -16783686
54 Z = -5115667
66
XDOT = -9230
785464 XDOT = -2813
543409
YDOT = -21540
547776 feet/sec YDOT = -6565
558962 meter/sec
ZDOT = -5543
988766 ZDOT = -1689
807776
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 19171
51907370
00016717 00000-0 10270-3 0 9086
2 25544 51
6397 344
7665 0008140 67
8174 292
3840 15
51216993 15763
Satellite: ISS
Catalog Number: 25544
Epoch time: 19171
51907370 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 344
7665 deg
Eccentricity:
0008140
Arg of perigee: 67
8174 deg
Mean anomaly: 292
3840 deg
Mean motion: 15
51216993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1576
Checksum: 333
Coasting Arc #10 (Orbit 1591)
---------------------------------------
Vector Time (GMT): 2019/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2441708
95 A = 6786190
53 meter
Y = 3537176
75 meter E =
0010609
Z = 5242261
95 I = 51
48665
XDOT = -6835
607663 Wp = 84
46564
YDOT = 3361
309520 meter/sec RA = 339
30195 deg
ZDOT = 915
235577 TA = 356
76148
MA = 356
76834
Ha = 228
483 n
mi
Hp = 216
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8010856
14 X = 2376510
05
Y = 11604910
60 feet Y = 3564116
29 meter
Z = 17199022
15 Z = 5253964
92
XDOT = -22426
534329 XDOT = -6877
132410
YDOT = 11027
918372 feet/sec YDOT = 3284
636644 meter/sec
ZDOT = 3002
741393 ZDOT = 881
930783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11807606
38 X = 3598958
42
Y = -7590456
43 feet Y = -2313571
12 meter
Z = 17251653
02 Z = 5258303
84
XDOT = 9886
783429 XDOT = 3013
491589
YDOT = 21864
545568 feet/sec YDOT = 6664
313489 meter/sec
ZDOT = 2851
269720 ZDOT = 869
067011
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 19172
54984205
00016717 00000-0 10270-3 0 9093
2 25544 51
6390 339
6503 0008106 71
2994 288
9037 15
51179312 15921
Satellite: ISS
Catalog Number: 25544
Epoch time: 19172
54984205 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 339
6503 deg
Eccentricity:
0008106
Arg of perigee: 71
2994 deg
Mean anomaly: 288
9037 deg
Mean motion: 15
51179312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1592
Checksum: 328
Coasting Arc #11 (Orbit 1606)
---------------------------------------
Vector Time (GMT): 2019/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1910584
70 A = 6785826
45 meter
Y = -3783288
68 meter E =
0022780
Z = -5319120
08 I = 51
45697
XDOT = 6866
540815 Wp = 84
22182
YDOT = -3364
480650 meter/sec RA = 334
32221 deg
ZDOT = -71
400237 TA = 185
08257
MA = 185
10574
Ha = 228
498 n
mi
Hp = 216
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6268322
51 X = -1842299
84
Y = -12412364
42 feet Y = -3804271
64 meter
Z = -17451181
36 Z = -5328235
55
XDOT = 22528
021046 XDOT = 6903
999886
YDOT = -11038
322342 feet/sec YDOT = -3287
484721 meter/sec
ZDOT = -234
252746 ZDOT = -37
954998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12467340
81 X = -3800045
48
Y = 6041190
61 feet Y = 1841354
90 meter
Z = -17492050
12 Z = -5331576
88
XDOT = -10398
605935 XDOT = -3169
495089
YDOT = -21716
461879 feet/sec YDOT = -6619
177581 meter/sec
ZDOT = -82
156562 ZDOT = -25
041320
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 19173
51618309
00016717 00000-0 10270-3 0 9102
2 25544 51
6410 334
8548 0008103 75
2949 284
9099 15
51226828 16077
Satellite: ISS
Catalog Number: 25544
Epoch time: 19173
51618309 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 334
8548 deg
Eccentricity:
0008103
Arg of perigee: 75
2949 deg
Mean anomaly: 284
9099 deg
Mean motion: 15
51226828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1607
Checksum: 323
Coasting Arc #12 (Orbit 1622)
---------------------------------------
Vector Time (GMT): 2019/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1376481
49 A = 6786145
74 meter
Y = 4055756
83 meter E =
0011372
Z = 5254753
46 I = 51
42740
XDOT = -6860
496599 Wp = 73
25392
YDOT = 3344
427495 meter/sec RA = 329
33866 deg
ZDOT = -779
595080 TA = 24
24087
MA = 24
18741
Ha = 228
578 n
mi
Hp = 216
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4516015
39 X = 1305502
13
Y = 13306288
82 feet Y = 4070752
09 meter
Z = 17240004
79 Z = 5261267
94
XDOT = -22508
190940 XDOT = -6893
598256
YDOT = 10972
531152 feet/sec YDOT = 3267
523626 meter/sec
ZDOT = -2557
726639 ZDOT = -813
000472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13270125
72 X = 4044734
32
Y = -4511450
60 feet Y = -1375090
14 meter
Z = 17269049
17 Z = 5263606
19
XDOT = 10831
440863 XDOT = 3301
423175
YDOT = 21430
094832 feet/sec YDOT = 6531
892905 meter/sec
ZDOT = -2709
625457 ZDOT = -825
893839
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 19174
54694648
00016717 00000-0 10270-3 0 9117
2 25544 51
6402 329
7379 0008216 79
0388 281
1687 15
51186842 16238
Satellite: ISS
Catalog Number: 25544
Epoch time: 19174
54694648 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 329
7379 deg
Eccentricity:
0008216
Arg of perigee: 79
0388 deg
Mean anomaly: 281
1687 deg
Mean motion: 15
51186842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1623
Checksum: 339
Coasting Arc #13 (Orbit 1637)
---------------------------------------
Vector Time (GMT): 2019/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -903664
63 A = 6786719
23 meter
Y = -4382537
39 meter E =
0021276
Z = -5121420
51 I = 51
40189
XDOT = 6732
662683 Wp = 94
59855
YDOT = -3254
883105 meter/sec RA = 324
35625 deg
ZDOT = 1601
427621 TA = 190
91952
MA = 190
96578
Ha = 228
535 n
mi
Hp = 216
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2964778
97 X = -829713
84
Y = -14378403
50 feet Y = -4392228
73 meter
Z = -16802560
74 Z = -5125631
03
XDOT = 22088
788329 XDOT = 6760
780544
YDOT = -10678
750345 feet/sec YDOT = -3179
436715 meter/sec
ZDOT = 5254
027627 ZDOT = 1634
200070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14301893
56 X = -4359217
16
Y = 3218710
47 feet Y = 981062
95 meter
Z = -16821123
40 Z = -5127078
41
XDOT = -11004
271052 XDOT = -3354
101817
YDOT = -20729
723708 feet/sec YDOT = -6318
419786 meter/sec
ZDOT = 5403
030724 ZDOT = 1646
843765
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 19175
51328351
00016717 00000-0 10270-3 0 9121
2 25544 51
6406 324
9433 0008138 82
7152 277
4924 15
51227313 16380
Satellite: ISS
Catalog Number: 25544
Epoch time: 19175
51328351 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 324
9433 deg
Eccentricity:
0008138
Arg of perigee: 82
7152 deg
Mean anomaly: 277
4924 deg
Mean motion: 15
51227313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1638
Checksum: 305
Coasting Arc #14 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2019/175/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5577200
37 A = 6797537
62 meter
Y = -3840253
66 meter E =
0020372
Z = 501771
88 I = 51
42480
XDOT = 2343
420711 Wp = 62
68467
YDOT = 4206
003224 meter/sec RA = 322
06190 deg
ZDOT = 5965
449640 TA = 302
73928
MA = 302
93548
Ha = 228
476 n
mi
Hp = 216
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18297901
49 X = 5617291
37
Y = -12599257
43 feet Y = -3777661
39 meter
Z = 1646233
19 Z = 528960
63
XDOT = 7688
388161 XDOT = 2267
237141
YDOT = 13799
223175 feet/sec YDOT = 4231
782373 meter/sec
ZDOT = 19571
685172 ZDOT = 5976
648464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9028933
87 X = 2752019
04
Y = 20288176
13 feet Y = 6183836
08 meter
Z = 1769981
00 Z = 539490
21
XDOT = -13473
609681 XDOT = -4106
756231
YDOT = 4237
088426 feet/sec YDOT = 1291
464552 meter/sec
ZDOT = 19621
959990 ZDOT = 5980
773405
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 19176
02866102
00016717 00000-0 10270-3 0 9130
2 25544 51
6394 322
3891 0008156 83
0450 277
1628 15
51268287 16463
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
02866102 = yrday
fracday
Element set: 913
Inclination: 51
6394 deg
RA of node: 322
3891 deg
Eccentricity:
0008156
Arg of perigee: 83
0450 deg
Mean anomaly: 277
1628 deg
Mean motion: 15
51268287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 317
Coasting Arc #15 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2019/175/23:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4819836
07 A = 6788349
60 meter
Y = 967545
60 meter E =
0015167
Z = 4669326
03 I = 51
39403
XDOT = -3942
954841 Wp = 98
46931
YDOT = 5942
522833 meter/sec RA = 322
02779 deg
ZDOT = 2828
603940 TA = 323
32805
MA = 323
43175
Ha = 228
315 n
mi
Hp = 216
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15813110
47 X = 4785977
62
Y = 3174362
19 feet Y = 1021254
55 meter
Z = 15319311
11 Z = 4692656
72
XDOT = -12936
203548 XDOT = -4022
852492
YDOT = 19496
465986 feet/sec YDOT = 5897
982900 meter/sec
ZDOT = 9280
196655 ZDOT = 2809
257248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5050563
23 X = -1539411
67
Y = 15210980
40 feet Y = 4636306
83 meter
Z = 15424986
79 Z = 4701535
97
XDOT = -16674
255279 XDOT = -5082
313009
YDOT = -14890
798361 feet/sec YDOT = -4538
715340 meter/sec
ZDOT = 9191
755673 ZDOT = 2801
647129
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 19176
02866199
00016717 00000-0 10270-3 0 9147
2 25544 51
6396 322
3890 0007997 81
4456 278
7601 15
51247340 16469
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
02866199 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 322
3890 deg
Eccentricity:
0007997
Arg of perigee: 81
4456 deg
Mean anomaly: 278
7601 deg
Mean motion: 15
51247340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 340
Coasting Arc #16 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2019/176/18:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3774678
25 A = 6786209
32 meter
Y = 2186320
10 meter E =
0011325
Z = 5189012
54 I = 51
36885
XDOT = -4963
759252 Wp = 97
47207
YDOT = 5726
943910 meter/sec RA = 318
15090 deg
ZDOT = 1194
161568 TA = 341
01394
MA = 341
05613
Ha = 228
336 n
mi
Hp = 216
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12384115
00 X = 3724744
40
Y = 7172966
21 feet Y = 2228251
44 meter
Z = 17024319
34 Z = 5207227
41
XDOT = -16285
299383 XDOT = -5033
231216
YDOT = 18789
186056 feet/sec YDOT = 5671
047102 meter/sec
ZDOT = 3917
852915 ZDOT = 1169
881447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12650698
64 X = -3855932
94
Y = -6478235
95 feet Y = -1974566
32 meter
Z = 17106650
19 Z = 5214106
98
XDOT = 14764
869553 XDOT = 4500
332240
YDOT = -18747
926273 feet/sec YDOT = -5714
367928 meter/sec
ZDOT = 3807
079699 ZDOT = 1160
397892
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 19176
80173056
00016717 00000-0 10270-3 0 9157
2 25544 51
6417 318
5513 0007968 85
5612 274
6449 15
51240185 16587
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
80173056 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 318
5513 deg
Eccentricity:
0007968
Arg of perigee: 85
5612 deg
Mean anomaly: 274
6449 deg
Mean motion: 15
51240185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 328
Coasting Arc #17 (Orbit 1672)
---------------------------------------
Vector Time (GMT): 2019/177/18:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3362557
59 A = 6785903
65 meter
Y = -2614704
14 meter E =
0022853
Z = -5302424
47 I = 51
34409
XDOT = 5020
654125 Wp = 87
45293
YDOT = -5757
216290 meter/sec RA = 313
16200 deg
ZDOT = -345
202921 TA = 179
23473
MA = 179
23123
Ha = 228
541 n
mi
Hp = 216
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11032013
09 X = -3307313
08
Y = -8578425
65 feet Y = -2651997
12 meter
Z = -17396405
75 Z = -5318624
63
XDOT = 16471
962351 XDOT = 5086
336624
YDOT = -18888
504890 feet/sec YDOT = -5700
704523 meter/sec
ZDOT = -1132
555514 ZDOT = -320
655587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11511859
88 X = 3508814
89
Y = 7760251
95 feet Y = 2365324
80 meter
Z = -17469550
77 Z = -5324719
07
XDOT = -14491
036186 XDOT = -4416
867830
YDOT = 19201
283790 feet/sec YDOT = 5852
551299 meter/sec
ZDOT = -1020
581707 ZDOT = -311
073304
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 19177
76806482
00016717 00000-0 10270-3 0 9160
2 25544 51
6425 313
7549 0008055 88
2440 271
9634 15
51211174 16738
Satellite: ISS
Catalog Number: 25544
Epoch time: 19177
76806482 = yrday
fracday
Element set: 916
Inclination: 51
6425 deg
RA of node: 313
7549 deg
Eccentricity:
0008055
Arg of perigee: 88
2440 deg
Mean anomaly: 271
9634 deg
Mean motion: 15
51211174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 322
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