[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 28th 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 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
060/17:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 224
6
000/00:00:00
000 0
0 0
0 215
5
061/07:48:58
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 215
6
062/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
4
000/00:00:00
000 0
0 0
0 215
5
066/23:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 224
6
000/00:00:00
000 0
0 0
0 215
4
067/07:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 3820)
---------------------------------------
Vector Time (GMT): 2019/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6718887
75 A = 6792940
41 meter
Y = -121820
32 meter E =
0015511
Z = 951842
02 I = 51
61646
XDOT = 934
310663 Wp = 113
49067
YDOT = 4791
867796 meter/sec RA = 185
40337 deg
ZDOT = -5911
451862 TA = 56
20298
MA = 56
05537
Ha = 224
354 n
mi
Hp = 215
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22043594
97 X = 6715127
17
Y = -399672
98 feet Y = -46706
01 meter
Z = 3122841
28 Z = 984470
24
XDOT = 3065
323697 XDOT = 909
371325
YDOT = 15721
351037 feet/sec YDOT = 4802
176203 meter/sec
ZDOT = -19394
527105 ZDOT = -5906
974184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20303051
27 X = 6188370
03
Y = 8539521
59 feet Y = 2602846
18 meter
Z = 3270265
33 Z = 996776
87
XDOT = -2811
661611 XDOT = -856
994459
YDOT = 14188
956529 feet/sec YDOT = 4324
793950 meter/sec
ZDOT = -19374
656011 ZDOT = -5905
395152
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 19058
53416106
00016717 00000-0 10270-3 0 9006
2 25544 51
6388 186
4305 0003449 63
4578 296
6927 15
52743321 38211
Satellite: ISS
Catalog Number: 25544
Epoch time: 19058
53416106 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 186
4305 deg
Eccentricity:
0003449
Arg of perigee: 63
4578 deg
Mean anomaly: 296
6927 deg
Mean motion: 15
52743321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3821
Checksum: 321
Coasting Arc #2 (Orbit 3836)
---------------------------------------
Vector Time (GMT): 2019/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6775063
91 A = 6793345
54 meter
Y = -272620
46 meter E =
0015939
Z = 278912
94 I = 51
65125
XDOT = 447
515819 Wp = 52
34559
YDOT = -4747
413149 meter/sec RA = 180
43938 deg
ZDOT = 6004
925164 TA = 310
65844
MA = 310
79689
Ha = 224
406 n
mi
Hp = 215
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22227899
97 X = -6772866
64
Y = -894424
08 feet Y = -348371
66 meter
Z = 915068
70 Z = 246008
16
XDOT = 1468
227751 XDOT = 471
401403
YDOT = -15575
502457 feet/sec YDOT = -4742
274901 meter/sec
ZDOT = 19701
198046 ZDOT = 6007
157208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20138912
13 X = -6138340
42
Y = -9463283
15 feet Y = -2884408
70 meter
Z = 766402
13 Z = 233599
37
XDOT = 6592
894910 XDOT = 2009
514368
YDOT = -12362
530242 feet/sec YDOT = -3768
099218 meter/sec
ZDOT = 19711
638459 ZDOT = 6008
107402
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 19059
56391281
00016717 00000-0 10270-3 0 9017
2 25544 51
6391 181
3083 0003560 66
6629 293
4897 15
52741033 38374
Satellite: ISS
Catalog Number: 25544
Epoch time: 19059
56391281 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 181
3083 deg
Eccentricity:
0003560
Arg of perigee: 66
6629 deg
Mean anomaly: 293
4897 deg
Mean motion: 15
52741033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3837
Checksum: 325
Coasting Arc #3 (Orbit 3851)
---------------------------------------
Vector Time (GMT): 2019/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6574599
13 A = 6792356
44 meter
Y = 704886
29 meter E =
0009922
Z = -1545234
49 I = 51
68157
XDOT = -1849
965801 Wp = 123
39639
YDOT = 4708
741751 meter/sec RA = 175
47699 deg
ZDOT = -5755
201407 TA = 73
46410
MA = 73
35512
Ha = 224
414 n
mi
Hp = 215
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21570207
12 X = 6573734
00
Y = 2312619
07 feet Y = 778403
14 meter
Z = -5069666
98 Z = -1513300
35
XDOT = -6069
441604 XDOT = -1874
527792
YDOT = 15448
627793 feet/sec YDOT = 4687
916527 meter/sec
ZDOT = -18881
894381 ZDOT = -5764
247546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19185805
43 X = 5847833
49
Y = 10196514
24 feet Y = 3107897
54 meter
Z = -4925396
73 Z = -1501260
92
XDOT = -10527
942539 XDOT = -3208
916886
YDOT = 10720
893421 feet/sec YDOT = 3267
728315 meter/sec
ZDOT = -18923
127394 ZDOT = -5767
769230
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 19060
52930132
00016717 00000-0 10270-3 0 9020
2 25544 51
6394 176
5059 0003472 70
5348 289
6179 15
52758268 38525
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
52930132 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 176
5059 deg
Eccentricity:
0003472
Arg of perigee: 70
5348 deg
Mean anomaly: 289
6179 deg
Mean motion: 15
52758268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3852
Checksum: 329
Coasting Arc #4 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2019/060/17:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6114897
17 A = 6790711
32 meter
Y = -1430029
49 meter E =
0017591
Z = 2561759
25 I = 51
68256
XDOT = 3273
709606 Wp = 74
07242
YDOT = -4509
635379 meter/sec RA = 174
35656 deg
ZDOT = 5271
581189 TA = 314
70547
MA = 314
84860
Ha = 224
644 n
mi
Hp = 215
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20061998
58 X = -6110895
05
Y = -4691697
79 feet Y = -1498388
03 meter
Z = 8404721
94 Z = 2532065
79
XDOT = 10740
517079 XDOT = 3298
288442
YDOT = -14795
391664 feet/sec YDOT = -4472
888776 meter/sec
ZDOT = 17295
213876 ZDOT = 5287
543231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14063677
89 X = -4286609
02
Y = 15130923
67 feet Y = 4611905
53 meter
Z = 8270627
52 Z = 2520887
27
XDOT = -6460
043792 XDOT = -1969
021348
YDOT = -15543
858504 feet/sec YDOT = -4737
768072 meter/sec
ZDOT = 17367
689785 ZDOT = 5293
671846
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 19060
78673855
00016717 00000-0 10270-3 0 9035
2 25544 51
6387 175
2282 0003955 66
5842 293
5726 15
52729939 38560
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
78673855 = yrday
fracday
Element set: 903
Inclination: 51
6387 deg
RA of node: 175
2282 deg
Eccentricity:
0003955
Arg of perigee: 66
5842 deg
Mean anomaly: 293
5726 deg
Mean motion: 15
52729939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 359
Coasting Arc #5 (Orbit 3864)
---------------------------------------
Vector Time (GMT): 2019/061/07:48:58
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4324312
77 A = 6787323
82 meter
Y = -3647673
14 meter E =
0014963
Z = 3739423
75 I = 51
68954
XDOT = 5844
233709 Wp = 80
40217
YDOT = 2526
783800 meter/sec RA = 171
33235 deg
ZDOT = -4276
529298 TA = 54
95030
MA = 54
81002
Ha = 224
323 n
mi
Hp = 215
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14187377
87 X = 4346617
06
Y = -11967431
55 feet Y = -3599190
72 meter
Z = 12268450
62 Z = 3760483
55
XDOT = 19173
995107 XDOT = 5836
316689
YDOT = 8289
973098 feet/sec YDOT = 2592
093594 meter/sec
ZDOT = -14030
607932 ZDOT = -4248
160208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13414545
52 X = 4088753
48
Y = 12735764
43 feet Y = 3881861
00 meter
Z = 12363909
66 Z = 3768519
66
XDOT = -5239
447834 XDOT = -1596
983700
YDOT = 19069
143744 feet/sec YDOT = 5812
275013 meter/sec
ZDOT = -13902
568693 ZDOT = -4237
502938
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 19061
36596774
00016717 00000-0 10270-3 0 9045
2 25544 51
6366 172
3436 0003504 68
3199 291
8325 15
52749935 38655
Satellite: ISS
Catalog Number: 25544
Epoch time: 19061
36596774 = yrday
fracday
Element set: 904
Inclination: 51
6366 deg
RA of node: 172
3436 deg
Eccentricity:
0003504
Arg of perigee: 68
3199 deg
Mean anomaly: 291
8325 deg
Mean motion: 15
52749935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3865
Checksum: 344
Coasting Arc #6 (Orbit 3879)
---------------------------------------
Vector Time (GMT): 2019/062/07:48:58
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5127765
88 A = 6789970
51 meter
Y = 3488804
67 meter E =
0008418
Z = -2765649
42 I = 51
73188
XDOT = -4813
413698 Wp = 66
84101
YDOT = -3008
626068 meter/sec RA = 166
36498 deg
ZDOT = 5144
873191 TA = 261
91188
MA = 262
00740
Ha = 224
454 n
mi
Hp = 215
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16823378
87 X = -5152963
90
Y = 11446209
55 feet Y = 3431321
32 meter
Z = -9073652
94 Z = -2790619
04
XDOT = -15792
039692 XDOT = -4804
403003
YDOT = -9870
820434 feet/sec YDOT = -3062
402276 meter/sec
ZDOT = 16879
505220 ZDOT = 5121
514081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13445965
41 X = -4098330
26
Y = -15204668
05 feet Y = -4634382
82 meter
Z = -9186786
76 Z = -2800132
60
XDOT = 6701
208120 XDOT = 2042
528235
YDOT = -16030
457879 feet/sec YDOT = -4886
083561 meter/sec
ZDOT = 16774
130780 ZDOT = 5112
755062
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 19062
33135000
00016717 00000-0 10270-3 0 9055
2 25544 51
6373 167
5408 0003762 74
3769 285
7798 15
52765976 38800
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
33135000 = yrday
fracday
Element set: 905
Inclination: 51
6373 deg
RA of node: 167
5408 deg
Eccentricity:
0003762
Arg of perigee: 74
3769 deg
Mean anomaly: 285
7798 deg
Mean motion: 15
52765976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3880
Checksum: 339
Coasting Arc #7 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2019/062/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 935961
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6328051
81 A = 6792975
05 meter
Y = 2304155
58 meter E =
0013173
Z = -852611
56 I = 51
74897
XDOT = -2335
610557 Wp = 48
97746
YDOT = -4240
468397 meter/sec RA = 165
72077 deg
ZDOT = 5943
351204 TA = 301
81918
MA = 301
94738
Ha = 224
437 n
mi
Hp = 215
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20761324
85 X = -6349205
81
Y = 7559565
55 feet Y = 2233272
54 meter
Z = -2797282
03 Z = -883401
69
XDOT = -7662
764294 XDOT = -2316
887676
YDOT = -13912
297892 feet/sec YDOT = -4266
481706 meter/sec
ZDOT = 19499
183741 ZDOT = 5932
051735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21331861
64 X = -6501951
43
Y = -5686144
20 feet Y = -1733136
75 meter
Z = -2936642
71 Z = -895088
70
XDOT = 1166
694768 XDOT = 355
608565
YDOT = -14310
983051 feet/sec YDOT = -4361
987634 meter/sec
ZDOT = 19448
415300 ZDOT = 5927
876983
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 19062
46006716
00016717 00000-0 10270-3 0 9061
2 25544 51
6402 166
9009 0003663 74
9022 285
2535 15
52757416 38827
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
46006716 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 166
9009 deg
Eccentricity:
0003663
Arg of perigee: 74
9022 deg
Mean anomaly: 285
2535 deg
Mean motion: 15
52757416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3882
Checksum: 312
Coasting Arc #8 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2019/063/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 935961
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6501766
20 A = 6793202
95 meter
Y = -1902202
26 meter E =
0013518
Z = -439193
73 I = 51
78139
XDOT = 969
490703 Wp = 125
19868
YDOT = 4667
771710 meter/sec RA = 160
76593 deg
ZDOT = -6002
420766 TA = 59
52480
MA = 59
39137
Ha = 224
454 n
mi
Hp = 215
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21331253
94 X = 6524687
25
Y = -6240821
05 feet Y = -1829366
84 meter
Z = -1440924
30 Z = -407555
49
XDOT = 3180
743776 XDOT = 946
378052
YDOT = 15314
211647 feet/sec YDOT = 4678
483468 meter/sec
ZDOT = -19692
981517 ZDOT = -5997
768005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21186132
84 X = 6457533
29
Y = 6746120
85 feet Y = 2056217
63 meter
Z = -1297741
76 Z = -395551
69
XDOT = -5315
622258 XDOT = -1620
201664
YDOT = 13005
996460 feet/sec YDOT = 3964
227721 meter/sec
ZDOT = -19672
288170 ZDOT = -5996
113434
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 19063
48980308
00016717 00000-0 10270-3 0 9073
2 25544 51
6398 161
7785 0003578 79
9887 280
1669 15
52773444 38982
Satellite: ISS
Catalog Number: 25544
Epoch time: 19063
48980308 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 161
7785 deg
Eccentricity:
0003578
Arg of perigee: 79
9887 deg
Mean anomaly: 280
1669 deg
Mean motion: 15
52773444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3898
Checksum: 379
Coasting Arc #9 (Orbit 3913)
---------------------------------------
Vector Time (GMT): 2019/064/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 935961
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6416389
18 A = 6792148
47 meter
Y = 1451562
72 meter E =
0017416
Z = 1658799
55 I = 51
81031
XDOT = 339
501147 Wp = 67
56902
YDOT = -5090
491711 meter/sec RA = 155
81211 deg
ZDOT = 5726
289958 TA = 310
55542
MA = 310
70692
Ha = 224
482 n
mi
Hp = 215
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21051145
61 X = -6440201
44
Y = 4762344
87 feet Y = 1379677
20 meter
Z = 5442255
73 Z = 1627573
84
XDOT = 1113
848906 XDOT = 368
584705
YDOT = -16701
088290 feet/sec YDOT = -5086
531959 meter/sec
ZDOT = 18787
040543 ZDOT = 5728
010257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20281909
35 X = -6181925
97
Y = -7482835
65 feet Y = -2280768
31 meter
Z = 5300955
68 Z = 1615731
29
XDOT = 9373
323334 XDOT = 2856
988952
YDOT = -11992
265512 feet/sec YDOT = -3655
242528 meter/sec
ZDOT = 18795
192750 ZDOT = 5728
774750
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 19064
51953441
00016717 00000-0 10270-3 0 9087
2 25544 51
6413 156
6562 0003657 82
1875 277
9692 15
52781324 39142
Satellite: ISS
Catalog Number: 25544
Epoch time: 19064
51953441 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 156
6562 deg
Eccentricity:
0003657
Arg of perigee: 82
1875 deg
Mean anomaly: 277
9692 deg
Mean motion: 15
52781324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3914
Checksum: 333
Coasting Arc #10 (Orbit 3928)
---------------------------------------
Vector Time (GMT): 2019/065/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 935961
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6111744
98 A = 6789948
27 meter
Y = -856439
06 meter E =
0007983
Z = -2835021
21 I = 51
83260
XDOT = -1593
538341 Wp = 105
56406
YDOT = 5483
452108 meter/sec RA = 150
85714 deg
ZDOT = -5105
913344 TA = 106
50562
MA = 106
41790
Ha = 224
485 n
mi
Hp = 215
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20051656
76 X = 6134638
38
Y = -2809839
42 feet Y = -787965
58 meter
Z = -9301250
69 Z = -2805277
52
XDOT = -5228
144164 XDOT = -1629
936206
YDOT = 17990
328437 feet/sec YDOT = 5465
427939 meter/sec
ZDOT = -16751
684200 ZDOT = -5113
743047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18547537
67 X = 5653289
48
Y = 8272737
54 feet Y = 2521530
40 meter
Z = -9166682
09 Z = -2794004
70
XDOT = -13266
528545 XDOT = -4043
637900
YDOT = 11193
941127 feet/sec YDOT = 3411
913256 meter/sec
ZDOT = -16787
494905 ZDOT = -5116
828447
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 19065
48490315
00016717 00000-0 10270-3 0 9091
2 25544 51
6410 151
8540 0003633 85
3693 274
7874 15
52779039 39292
Satellite: ISS
Catalog Number: 25544
Epoch time: 19065
48490315 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 151
8540 deg
Eccentricity:
0003633
Arg of perigee: 85
3693 deg
Mean anomaly: 274
7874 deg
Mean motion: 15
52779039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3929
Checksum: 337
Coasting Arc #11 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2019/066/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 935961
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5607305
43 A = 6787130
34 meter
Y = 184768
70 meter E =
0015174
Z = 3807657
00 I = 51
85185
XDOT = 2683
391905 Wp = 95
06783
YDOT = -5818
134638 meter/sec RA = 145
89902 deg
ZDOT = 4218
250197 TA = 310
50017
MA = 310
63230
Ha = 224
520 n
mi
Hp = 215
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18396671
37 X = -5627450
02
Y = 606196
52 feet Y = 121951
73 meter
Z = 12492313
00 Z = 3780370
30
XDOT = 8803
779215 XDOT = 2727
762905
YDOT = -19088
368235 feet/sec YDOT = -5787
878452 meter/sec
ZDOT = 13839
403533 ZDOT = 4231
393395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16151850
83 X = -4923084
13
Y = -8999503
09 feet Y = -2743048
54 meter
Z = 12368893
84 Z = 3770038
84
XDOT = 16642
736820 XDOT = 5072
706183
YDOT = -10694
697210 feet/sec YDOT = -3259
743710 meter/sec
ZDOT = 13899
275815 ZDOT = 4236
499268
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 19066
51462506
00016717 00000-0 10270-3 0 9109
2 25544 51
6409 146
7318 0003652 88
7589 271
3981 15
52814139 39459
Satellite: ISS
Catalog Number: 25544
Epoch time: 19066
51462506 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 146
7318 deg
Eccentricity:
0003652
Arg of perigee: 88
7589 deg
Mean anomaly: 271
3981 deg
Mean motion: 15
52814139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3945
Checksum: 332
Coasting Arc #12 (Orbit 3952)
---------------------------------------
Vector Time (GMT): 2019/066/23:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 935961
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4260329
82 A = 6782751
82 meter
Y = -1710348
99 meter E =
0009519
Z = 4986189
18 I = 51
85077
XDOT = 4758
140668 Wp = 108
44918
YDOT = -5628
812267 meter/sec RA = 143
31919 deg
ZDOT = 2128
438186 TA = 320
85777
MA = 320
92659
Ha = 224
597 n
mi
Hp = 215
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13977460
04 X = -4265107
39
Y = -5611381
19 feet Y = -1758017
05 meter
Z = 16358888
37 Z = 4965482
99
XDOT = 15610
697731 XDOT = 4810
391379
YDOT = -18467
231846 feet/sec YDOT = -5575
310988 meter/sec
ZDOT = 6983
064915 ZDOT = 2151
678749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10658519
40 X = 3248716
71
Y = 10784433
43 feet Y = 3287095
31 meter
Z = 16265367
40 Z = 4957683
98
XDOT = -20872
473564 XDOT = -6361
929942
YDOT = 9906
408268 feet/sec YDOT = 3019
473240 meter/sec
ZDOT = 7088
595920 ZDOT = 2160
604036
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 19067
02948682
00016717 00000-0 10270-3 0 9111
2 25544 51
6403 144
1737 0003769 83
3950 276
7631 15
52804188 39535
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
02948682 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 144
1737 deg
Eccentricity:
0003769
Arg of perigee: 83
3950 deg
Mean anomaly: 276
7631 deg
Mean motion: 15
52804188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3953
Checksum: 330
Coasting Arc #13 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2019/067/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910513
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5923668
14 A = 6790754
20 meter
Y = 2249829
79 meter E =
0017362
Z = 2421094
35 I = 51
88374
XDOT = 130
398915 Wp = 77
89544
YDOT = -5470
835100 meter/sec RA = 141
75936 deg
ZDOT = 5373
952601 TA = 309
08314
MA = 309
23745
Ha = 224
492 n
mi
Hp = 215
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19434606
76 X = -5960146
30
Y = 7381331
33 feet Y = 2183383
54 meter
Z = 7943222
93 Z = 2392230
87
XDOT = 427
817961 XDOT = 165
462296
YDOT = -17948
934056 feet/sec YDOT = -5469
180150 meter/sec
ZDOT = 17631
078088 ZDOT = 5374
671883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7318641
30 X = -2230721
87
Y = -19511149
95 feet Y = -5946998
51 meter
Z = 7812509
17 Z = 2381252
80
XDOT = 16523
885611 XDOT = 5036
480334
YDOT = 901
694945 feet/sec YDOT = 274
836619 meter/sec
ZDOT = 17634
741236 ZDOT = 5375
069129
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 19067
35127327
00016717 00000-0 10270-3 0 9123
2 25544 51
6381 142
5678 0003734 92
1992 267
9588 15
52814952 39580
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
35127327 = yrday
fracday
Element set: 912
Inclination: 51
6381 deg
RA of node: 142
5678 deg
Eccentricity:
0003734
Arg of perigee: 92
1992 deg
Mean anomaly: 267
9588 deg
Mean motion: 15
52814952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 347
Coasting Arc #14 (Orbit 3972)
---------------------------------------
Vector Time (GMT): 2019/068/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910513
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5619619
92 A = 6788102
82 meter
Y = -1507651
21 meter E =
0008764
Z = -3503941
68 I = 51
90064
XDOT = -1213
544802 Wp = 90
48392
YDOT = 6036
944787 meter/sec RA = 136
80543 deg
ZDOT = -4553
718806 TA = 130
47895
MA = 130
40253
Ha = 224
504 n
mi
Hp = 215
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18437073
22 X = 5653081
30
Y = -4946362
22 feet Y = -1444622
03 meter
Z = -11495871
66 Z = -3476562
45
XDOT = -3981
446200 XDOT = -1258
842183
YDOT = 19806
249300 feet/sec YDOT = 6023
120236 meter/sec
ZDOT = -14940
022330 ZDOT = -4559
724475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5205087
50 X = 1586510
67
Y = 18442717
74 feet Y = 5621340
37 meter
Z = -11371915
41 Z = -3466159
82
XDOT = -18512
643455 XDOT = -5642
653725
YDOT = -3984
087954 feet/sec YDOT = -1214
350009 meter/sec
ZDOT = -14967
647338 ZDOT = -4562
138909
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 19068
31663250
00016717 00000-0 10270-3 0 9131
2 25544 51
6385 137
7646 0003794 93
2818 266
8768 15
52802916 39732
Satellite: ISS
Catalog Number: 25544
Epoch time: 19068
31663250 = yrday
fracday
Element set: 913
Inclination: 51
6385 deg
RA of node: 137
7646 deg
Eccentricity:
0003794
Arg of perigee: 93
2818 deg
Mean anomaly: 266
8768 deg
Mean motion: 15
52802916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3973
Checksum: 347
Coasting Arc #15 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2019/069/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910513
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5161462
33 A = 6785228
59 meter
Y = 658128
34 meter E =
0013477
Z = 4345882
45 I = 51
91479
XDOT = 2128
973316 Wp = 105
14830
YDOT = -6486
524311 meter/sec RA = 131
84788 deg
ZDOT = 3498
358418 TA = 309
38367
MA = 309
50296
Ha = 224
551 n
mi
Hp = 215
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16933931
53 X = -5189547
88
Y = 2159213
73 feet Y = 600252
73 meter
Z = 14258144
51 Z = 4320741
83
XDOT = 6984
820589 XDOT = 2184
356237
YDOT = -21281
247740 feet/sec YDOT = -6462
406571 meter/sec
ZDOT = 11477
553864 ZDOT = 3508
835388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2689688
82 X = -819817
15
Y = -16953386
55 feet Y = -5167392
22 meter
Z = 14144369
34 Z = 4311203
78
XDOT = 20249
120642 XDOT = 6171
931972
YDOT = 6437
594794 feet/sec YDOT = 1962
178893 meter/sec
ZDOT = 11525
452159 ZDOT = 3512
957818
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 19069
34634375
00016717 00000-0 10270-3 0 9142
2 25544 51
6385 132
6417 0003768 97
5741 262
5839 15
52829132 39893
Satellite: ISS
Catalog Number: 25544
Epoch time: 19069
34634375 = yrday
fracday
Element set: 914
Inclination: 51
6385 deg
RA of node: 132
6417 deg
Eccentricity:
0003768
Arg of perigee: 97
5741 deg
Mean anomaly: 262
5839 deg
Mean motion: 15
52829132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 349
Coasting Arc #16 (Orbit 4003)
---------------------------------------
Vector Time (GMT): 2019/070/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910513
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4613640
31 A = 6782857
82 meter
Y = 343989
00 meter E =
0015748
Z = -4974448
52 I = 51
92777
XDOT = -2885
718592 Wp = 80
18339
YDOT = 6734
652942 meter/sec RA = 126
88671 deg
ZDOT = -2214
051329 TA = 168
27692
MA = 168
24021
Ha = 224
459 n
mi
Hp = 215
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15136615
19 X = 4633613
89
Y = 1128572
83 feet Y = 395693
12 meter
Z = -16320369
15 Z = -4951988
76
XDOT = -9467
580684 XDOT = -2950
058309
YDOT = 22095
318050 feet/sec YDOT = 6702
022848 meter/sec
ZDOT = -7263
947929 ZDOT = -2228
225987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -389114
93 X = -118602
23
Y = 15282166
66 feet Y = 4658004
40 meter
Z = -16218792
09 Z = -4943487
83
XDOT = -21409
959291 XDOT = -6525
755592
YDOT = -8311
176534 feet/sec YDOT = -2533
246608 meter/sec
ZDOT = -7328
610623 ZDOT = -2233
760518
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 19070
31169719
00016717 00000-0 10270-3 0 9157
2 25544 51
6383 127
8395 0003789 100
4177 259
7402 15
52807823 40048
Satellite: ISS
Catalog Number: 25544
Epoch time: 19070
31169719 = yrday
fracday
Element set: 915
Inclination: 51
6383 deg
RA of node: 127
8395 deg
Eccentricity:
0003789
Arg of perigee: 100
4177 deg
Mean anomaly: 259
7402 deg
Mean motion: 15
52807823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 319
Coasting Arc #17 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2019/071/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910513
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4001190
11 A = 6781320
49 meter
Y = -1404636
52 meter E =
0006911
Z = 5286625
11 I = 51
94319
XDOT = 3473
102633 Wp = 111
55116
YDOT = -6790
693841 meter/sec RA = 121
92166 deg
ZDOT = 821
028512 TA = 330
61749
MA = 330
65633
Ha = 224
490 n
mi
Hp = 215
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13127264
12 X = -4010865
14
Y = -4608387
53 feet Y = -1449434
28 meter
Z = 17344570
57 Z = 5267165
48
XDOT = 11394
693679 XDOT = 3544
791872
YDOT = -22279
179270 feet/sec YDOT = -6751
454271 meter/sec
ZDOT = 2693
663098 ZDOT = 838
074206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3729650
89 X = 1136797
59
Y = -13516444
80 feet Y = -4119812
37 meter
Z = 17256646
59 Z = 5259825
88
XDOT = 21990
871027 XDOT = 6702
817489
YDOT = 9620
276645 feet/sec YDOT = 2932
260321 meter/sec
ZDOT = 2771
339975 ZDOT = 844
704425
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 19071
34140212
00016717 00000-0 10270-3 0 9169
2 25544 51
6393 122
7156 0003669 103
7886 256
3675 15
52844943 40205
Satellite: ISS
Catalog Number: 25544
Epoch time: 19071
34140212 = yrday
fracday
Element set: 916
Inclination: 51
6393 deg
RA of node: 122
7156 deg
Eccentricity:
0003669
Arg of perigee: 103
7886 deg
Mean anomaly: 256
3675 deg
Mean motion: 15
52844943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 308
Coasting Arc #18 (Orbit 4034)
---------------------------------------
Vector Time (GMT): 2019/072/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910513
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3388355
79 A = 6781242
89 meter
Y = 2521741
59 meter E =
0018494
Z = -5321215
68 I = 51
96003
XDOT = -3890
279476 Wp = 97
15475
YDOT = 6559
748153 meter/sec RA = 116
95779 deg
ZDOT = 631
137591 TA = 178
85823
MA = 178
85400
Ha = 224
417 n
mi
Hp = 215
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11116652
86 X = 3385752
58
Y = 8273430
43 feet Y = 2559617
65 meter
Z = -17458056
69 Z = -5304762
85
XDOT = -12763
384106 XDOT = -3966
409013
YDOT = 21521
483440 feet/sec YDOT = 6515
818703 meter/sec
ZDOT = 2070
661387 ZDOT = 612
054782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7315243
74 X = -2229686
29
Y = 11878683
23 feet Y = 3620622
65 meter
Z = -17383827
51 Z = -5298590
62
XDOT = -21638
062983 XDOT = -6595
281597
YDOT = -10420
483951 feet/sec YDOT = -3176
163508 meter/sec
ZDOT = 1983
764233 ZDOT = 604
651338
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 19072
30674926
00016717 00000-0 10270-3 0 9171
2 25544 51
6398 117
9137 0003876 105
5015 254
6565 15
52837844 40356
Satellite: ISS
Catalog Number: 25544
Epoch time: 19072
30674926 = yrday
fracday
Element set: 917
Inclination: 51
6398 deg
RA of node: 117
9137 deg
Eccentricity:
0003876
Arg of perigee: 105
5015 deg
Mean anomaly: 254
6565 deg
Mean motion: 15
52837844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 331
Coasting Arc #19 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2019/073/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910513
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2777281
20 A = 6782533
18 meter
Y = -3606839
29 meter E =
0008923
Z = 5021082
24 I = 51
97810
XDOT = 4190
248778 Wp = 76
95317
YDOT = -6090
005885 meter/sec RA = 111
99490 deg
ZDOT = -2051
943304 TA = 32
92219
MA = 32
86665
Ha = 224
572 n
mi
Hp = 215
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9111814
97 X = -2761131
60
Y = -11833462
24 feet Y = -3637806
23 meter
Z = 16473366
93 Z = 5007630
73
XDOT = 13747
535361 XDOT = 4268
004673
YDOT = -19980
334269 feet/sec YDOT = -6042
712940 meter/sec
ZDOT = -6732
097453 ZDOT = -2031
399581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10852897
83 X = 3307963
26
Y = -10356738
26 feet Y = -3156733
82 meter
Z = 16412812
07 Z = 5002625
12
XDOT = 20502
327851 XDOT = 6249
109529
YDOT = 10937
828937 feet/sec YDOT = 3333
850260 meter/sec
ZDOT = -6638
607487 ZDOT = -2023
447562
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 19073
33645022
00016717 00000-0 10270-3 0 9181
2 25544 51
6397 112
7903 0003922 108
7026 251
4552 15
52813438 40510
Satellite: ISS
Catalog Number: 25544
Epoch time: 19073
33645022 = yrday
fracday
Element set: 918
Inclination: 51
6397 deg
RA of node: 112
7903 deg
Eccentricity:
0003922
Arg of perigee: 108
7026 deg
Mean anomaly: 251
4552 deg
Mean motion: 15
52813438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 295
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