[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 22nd 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
175/23:25:30
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
180/21:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 216
3
Coasting Arc #1 (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 = 4505386
01 A = 6790951
88 meter
Y = 3106700
25 meter E =
0017085
Z = 4004354
03 I = 51
63398
XDOT = -5738
275637 Wp = 81
90002
YDOT = 3210
720061 meter/sec RA = 359
19172 deg
ZDOT = 3953
199730 TA = 326
96290
MA = 327
06952
Ha = 228
183 n
mi
Hp = 216
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14781450
15 X = 4450860
20
Y = 10192586
12 feet Y = 3156776
99 meter
Z = 13137644
47 Z = 4026107
70
XDOT = -18826
363638 XDOT = -5792
954809
YDOT = 10533
858469 feet/sec YDOT = 3146
244158 meter/sec
ZDOT = 12969
815386 ZDOT = 3925
193114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11538984
24 X = 3517082
40
Y = -13661631
64 feet Y = -4164065
32 meter
Z = 13235915
01 Z = 4034306
89
XDOT = 7700
282295 XDOT = 2347
046044
YDOT = 18984
171806 feet/sec YDOT = 5786
375566 meter/sec
ZDOT = 12842
365135 ZDOT = 3914
352893
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
55560996
00016717 00000-0 10270-3 0 9007
2 25544 51
6396 359
4756 0007810 55
3822 304
8065 15
51203720 15303
Satellite: ISS
Catalog Number: 25544
Epoch time: 19168
55560996 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 359
4756 deg
Eccentricity:
0007810
Arg of perigee: 55
3822 deg
Mean anomaly: 304
8065 deg
Mean motion: 15
51203720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1530
Checksum: 314
Coasting Arc #2 (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 = -4039044
62 A = 6789303
08 meter
Y = -3154022
42 meter E =
0017361
Z = -4471203
77 I = 51
59505
XDOT = 6123
351375 Wp = 64
64802
YDOT = -3219
383405 meter/sec RA = 354
22454 deg
ZDOT = -3263
209820 TA = 172
38141
MA = 172
35500
Ha = 228
353 n
mi
Hp = 216
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13251458
72 X = -3981756
70
Y = -10347842
60 feet Y = -3198868
67 meter
Z = -14669303
70 Z = -4490685
34
XDOT = 20089
735481 XDOT = 6174
747147
YDOT = -10562
281512 feet/sec YDOT = -3150
619802 meter/sec
ZDOT = -10706
068964 ZDOT = -3233
340755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11337720
35 X = -3455737
16
Y = 12310436
04 feet Y = 3752220
90 meter
Z = -14757260
50 Z = -4498013
00
XDOT = -8069
936788 XDOT = -2459
716733
YDOT = -20092
902282 feet/sec YDOT = -6124
316615 meter/sec
ZDOT = -10570
173589 ZDOT = -3221
788910
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
52196145
00016717 00000-0 10270-3 0 9017
2 25544 51
6394 354
6787 0007943 59
9642 300
2296 15
51212475 15458
Satellite: ISS
Catalog Number: 25544
Epoch time: 19169
52196145 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 354
6787 deg
Eccentricity:
0007943
Arg of perigee: 59
9642 deg
Mean anomaly: 300
2296 deg
Mean motion: 15
51212475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1545
Checksum: 329
Coasting Arc #3 (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 = 3528246
42 A = 6787971
10 meter
Y = 3218503
56 meter E =
0013252
Z = 4812269
89 I = 51
55767
XDOT = -6457
124426 Wp = 89
22167
YDOT = 3275
727828 meter/sec RA = 349
25346 deg
ZDOT = 2537
498597 TA = 335
76922
MA = 335
83149
Ha = 228
324 n
mi
Hp = 216
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11575611
62 X = 3468618
80
Y = 10559394
88 feet Y = 3257624
59 meter
Z = 15788287
04 Z = 4829264
44
XDOT = -21184
791424 XDOT = -6505
600315
YDOT = 10747
138544 feet/sec YDOT = 3203
248226 meter/sec
ZDOT = 8325
126632 ZDOT = 2506
015390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11233867
53 X = 3424082
82
Y = -10810598
38 feet Y = -3295070
39 meter
Z = 15864954
93 Z = 4835638
26
XDOT = 8657
014810 XDOT = 2638
658114
YDOT = 21031
353624 feet/sec YDOT = 6410
356585 meter/sec
ZDOT = 8181
908576 ZDOT = 2493
845734
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
55273396
00016717 00000-0 10270-3 0 9027
2 25544 51
6397 349
5620 0007935 63
0841 297
1120 15
51190386 15612
Satellite: ISS
Catalog Number: 25544
Epoch time: 19170
55273396 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 349
5620 deg
Eccentricity:
0007935
Arg of perigee: 63
0841 deg
Mean anomaly: 297
1120 deg
Mean motion: 15
51190386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1561
Checksum: 313
Coasting Arc #4 (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 = -2998958
06 A = 6786815
80 meter
Y = -3362683
75 meter E =
0021376
Z = -5094762
71 I = 51
52134
XDOT = 6669
284481 Wp = 73
35418
YDOT = -3313
213552 meter/sec RA = 344
27932 deg
ZDOT = -1739
057207 TA = 179
75896
MA = 179
75793
Ha = 228
474 n
mi
Hp = 216
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9839101
24 X = -2936385
40
Y = -11032426
99 feet Y = -3395869
46 meter
Z = -16715100
75 Z = -5109178
98
XDOT = 21880
854598 XDOT = 6714
285400
YDOT = -10870
123203 feet/sec YDOT = -3238
381028 meter/sec
ZDOT = -5705
568266 ZDOT = -1706
551903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11443591
13 X = -3488006
58
Y = 9240716
93 feet Y = 2816570
52 meter
Z = -16780057
33 Z = -5114561
48
XDOT = -9239
323669 XDOT = -2816
145854
YDOT = -21533
483171 feet/sec YDOT = -6563
405671 meter/sec
ZDOT = -5557
717932 ZDOT = -1693
992426
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
51908121
00016717 00000-0 10270-3 0 9036
2 25544 51
6396 344
7661 0008086 68
2884 291
9127 15
51213593 15766
Satellite: ISS
Catalog Number: 25544
Epoch time: 19171
51908121 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 344
7661 deg
Eccentricity:
0008086
Arg of perigee: 68
2884 deg
Mean anomaly: 291
9127 deg
Mean motion: 15
51213593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1576
Checksum: 326
Coasting Arc #5 (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 = 2447678
76 A = 6786205
00 meter
Y = 3534273
28 meter E =
0010579
Z = 5241486
73 I = 51
48652
XDOT = -6832
862177 Wp = 84
94434
YDOT = 3365
234398 meter/sec RA = 339
30152 deg
ZDOT = 920
993730 TA = 356
22655
MA = 356
23453
Ha = 228
472 n
mi
Hp = 216
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8030442
12 X = 2382515
64
Y = 11595384
77 feet Y = 3561279
78 meter
Z = 17196478
77 Z = 5253218
78
XDOT = -22417
526828 XDOT = -6874
458987
YDOT = 11040
795268 feet/sec YDOT = 3288
591820 meter/sec
ZDOT = 3021
632971 ZDOT = 887
702097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11798593
70 X = 3596211
36
Y = -7610300
31 feet Y = -2319619
53 meter
Z = 17249241
91 Z = 5257568
93
XDOT = 9898
441306 XDOT = 3017
044910
YDOT = 21856
660509 feet/sec YDOT = 6661
910123 meter/sec
ZDOT = 2870
220499 ZDOT = 874
843208
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
54985197
00016717 00000-0 10270-3 0 9049
2 25544 51
6390 339
6499 0008053 71
7729 288
4298 15
51175528 15926
Satellite: ISS
Catalog Number: 25544
Epoch time: 19172
54985197 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 339
6499 deg
Eccentricity:
0008053
Arg of perigee: 71
7729 deg
Mean anomaly: 288
4298 deg
Mean motion: 15
51175528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1592
Checksum: 359
Coasting Arc #6 (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 = -1917927
54 A = 6785839
05 meter
Y = -3779693
44 meter E =
0022741
Z = -5319021
86 I = 51
45684
XDOT = 6863
936744 Wp = 84
37570
YDOT = -3369
668773 meter/sec RA = 334
32181 deg
ZDOT = -78
618875 TA = 184
86006
MA = 184
88218
Ha = 228
488 n
mi
Hp = 216
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6292413
19 X = -1849682
82
Y = -12400569
04 feet Y = -3800758
74 meter
Z = -17450859
11 Z = -5328173
10
XDOT = 22519
477507 XDOT = 6901
489088
YDOT = -11055
343743 feet/sec YDOT = -3292
701442 meter/sec
ZDOT = -257
935943 ZDOT = -45
186060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12455758
43 X = -3796515
17
Y = 6065386
04 feet Y = 1848729
66 meter
Z = -17491890
53 Z = -5331528
23
XDOT = -10413
937904 XDOT = -3174
168273
YDOT = -21709
072742 feet/sec YDOT = -6616
925372 meter/sec
ZDOT = -105
895457 ZDOT = -32
276935
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
51619553
00016717 00000-0 10270-3 0 9058
2 25544 51
6409 334
8544 0008050 75
7779 284
4266 15
51222563 16071
Satellite: ISS
Catalog Number: 25544
Epoch time: 19173
51619553 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 334
8544 deg
Eccentricity:
0008050
Arg of perigee: 75
7779 deg
Mean anomaly: 284
4266 deg
Mean motion: 15
51222563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1607
Checksum: 323
Coasting Arc #7 (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 = 1385737
80 A = 6786154
64 meter
Y = 4051280
53 meter E =
0011300
Z = 5255809
07 I = 51
42725
XDOT = -6858
089317 Wp = 73
64011
YDOT = 3351
379013 meter/sec RA = 329
33829 deg
ZDOT = -770
614119 TA = 23
76755
MA = 23
71540
Ha = 228
567 n
mi
Hp = 216
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4546383
87 X = 1314802
68
Y = 13291602
77 feet Y = 4066379
54 meter
Z = 17243468
09 Z = 5262368
62
XDOT = -22500
293035 XDOT = -6891
312512
YDOT = 10995
337969 feet/sec YDOT = 3274
501383 meter/sec
ZDOT = -2528
261546 ZDOT = -804
008113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13255186
16 X = 4040180
74
Y = -4541671
00 feet Y = -1384301
32 meter
Z = 17272717
41 Z = 5264724
27
XDOT = 10851
980661 XDOT = 3307
683705
YDOT = 21423
293605 feet/sec YDOT = 6529
819891 meter/sec
ZDOT = -2680
109522 ZDOT = -816
897382
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
54696190
00016717 00000-0 10270-3 0 9065
2 25544 51
6402 329
7375 0008164 79
5169 280
6902 15
51182114 16230
Satellite: ISS
Catalog Number: 25544
Epoch time: 19174
54696190 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 329
7375 deg
Eccentricity:
0008164
Arg of perigee: 79
5169 deg
Mean anomaly: 280
6902 deg
Mean motion: 15
51182114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1623
Checksum: 319
Coasting Arc #8 (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 = -914390
04 A = 6786722
90 meter
Y = -4377369
19 meter E =
0021260
Z = -5123944
11 I = 51
40172
XDOT = 6730
810845 Wp = 94
77085
YDOT = -3263
765938 meter/sec RA = 324
35591 deg
ZDOT = 1591
077270 TA = 190
64490
MA = 190
68998
Ha = 228
525 n
mi
Hp = 216
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2999967
33 X = -840483
99
Y = -14361447
46 feet Y = -4387180
72 meter
Z = -16810840
25 Z = -5128206
83
XDOT = 22082
712747 XDOT = 6759
078450
YDOT = -10707
893499 feet/sec YDOT = -3188
339418 meter/sec
ZDOT = 5220
069783 ZDOT = 1623
841086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14284045
02 X = -4353776
92
Y = 3253397
22 feet Y = 991635
47 meter
Z = -16829640
27 Z = -5129674
35
XDOT = -11030
728011 XDOT = -3362
165898
YDOT = -20724
434336 feet/sec YDOT = -6316
807586 meter/sec
ZDOT = 5369
034808 ZDOT = 1636
481809
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
51330199
00016717 00000-0 10270-3 0 9078
2 25544 51
6406 324
9430 0008086 83
2055 277
0016 15
51222240 16389
Satellite: ISS
Catalog Number: 25544
Epoch time: 19175
51330199 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 324
9430 deg
Eccentricity:
0008086
Arg of perigee: 83
2055 deg
Mean anomaly: 277
0016 deg
Mean motion: 15
51222240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1638
Checksum: 291
Coasting Arc #9 (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 = 5573158
11 A = 6797558
07 meter
Y = -3847611
13 meter E =
0020280
Z = 491453
11 I = 51
42468
XDOT = 2355
768056 Wp = 62
75588
YDOT = 4197
460106 meter/sec RA = 322
06139 deg
ZDOT = 5966
485918 TA = 302
55614
MA = 302
75186
Ha = 228
467 n
mi
Hp = 216
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18284639
45 X = 5613381
79
Y = -12623396
09 feet Y = -3785063
32 meter
Z = 1612378
97 Z = 518622
54
XDOT = 7728
897821 XDOT = 2279
674066
YDOT = 13771
194575 feet/sec YDOT = 4223
377833 meter/sec
ZDOT = 19575
085033 ZDOT = 5977
744936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9055057
00 X = 2759981
37
Y = 20279793
94 feet Y = 6181281
19 meter
Z = 1736040
08 Z = 529145
02
XDOT = -13454
099228 XDOT = -4100
809445
YDOT = 4280
125842 feet/sec YDOT = 1304
582357 meter/sec
ZDOT = 19625
633830 ZDOT = 5981
893191
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
02868124
00016717 00000-0 10270-3 0 9080
2 25544 51
6393 322
3888 0008103 83
5231 276
6842 15
51262839 16461
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
02868124 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 322
3888 deg
Eccentricity:
0008103
Arg of perigee: 83
5231 deg
Mean anomaly: 276
6842 deg
Mean motion: 15
51262839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 325
Coasting Arc #10 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2019/175/23:25:30
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4579948
67 A = 6787762
75 meter
Y = 1311341
86 meter E =
0014135
Z = 4823876
60 I = 51
39178
XDOT = -4292
425205 Wp = 99
24746
YDOT = 5857
781862 meter/sec RA = 322
02179 deg
ZDOT = 2474
528344 TA = 326
33011
MA = 326
41983
Ha = 228
323 n
mi
Hp = 216
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15026078
33 X = 4541512
91
Y = 4302302
70 feet Y = 1362342
62 meter
Z = 15826366
81 Z = 4846030
95
XDOT = -14082
759859 XDOT = -4369
629392
YDOT = 19218
444429 feet/sec YDOT = 5809
349006 meter/sec
ZDOT = 8118
531313 ZDOT = 2453
490598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6012173
89 X = -1832510
60
Y = 14316485
85 feet Y = 4363664
89 meter
Z = 15926667
04 Z = 4854448
11
XDOT = -16397
207627 XDOT = -4997
868885
YDOT = -15841
297265 feet/sec YDOT = -4828
427406 meter/sec
ZDOT = 8022
432533 ZDOT = 2445
237436
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
02868248
00016717 00000-0 10270-3 0 9098
2 25544 51
6396 322
3886 0007963 81
7618 278
4436 15
51235575 16460
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
02868248 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 322
3886 deg
Eccentricity:
0007963
Arg of perigee: 81
7618 deg
Mean anomaly: 278
4436 deg
Mean motion: 15
51235575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 352
Coasting Arc #11 (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 = 3784598
51 A = 6786236
46 meter
Y = 2174921
59 meter E =
0011311
Z = 5186659
47 I = 51
36875
XDOT = -4954
107624 Wp = 97
96117
YDOT = 5732
464806 meter/sec RA = 318
15062 deg
ZDOT = 1207
314773 TA = 340
39576
MA = 340
43921
Ha = 228
326 n
mi
Hp = 216
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12416661
78 X = 3734802
81
Y = 7135569
53 feet Y = 2216964
64 meter
Z = 17016599
32 Z = 5204922
87
XDOT = -16253
633936 XDOT = -5023
705932
YDOT = 18807
299231 feet/sec YDOT = 5676
675221 meter/sec
ZDOT = 3961
006474 ZDOT = 1183
081230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12681158
76 X = -3865217
19
Y = -6439077
88 feet Y = -1962630
94 meter
Z = 17099151
54 Z = 5211821
39
XDOT = 14735
388100 XDOT = 4491
346293
YDOT = -18762
042065 feet/sec YDOT = -5718
670421 meter/sec
ZDOT = 3850
443797 ZDOT = 1173
615269
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
80175353
00016717 00000-0 10270-3 0 9104
2 25544 51
6417 318
5509 0007915 86
0538 274
1518 15
51234439 16584
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
80175353 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 318
5509 deg
Eccentricity:
0007915
Arg of perigee: 86
0538 deg
Mean anomaly: 274
1518 deg
Mean motion: 15
51234439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 322
Coasting Arc #12 (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 = -3374092
16 A = 6785924
70 meter
Y = -2601452
40 meter E =
0022793
Z = -5301588
97 I = 51
34396
XDOT = 5010
833452 Wp = 87
54683
YDOT = -5764
865898 meter/sec RA = 313
16178 deg
ZDOT = -360
661334 TA = 178
99280
MA = 178
98820
Ha = 228
531 n
mi
Hp = 216
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11069856
17 X = -3318999
04
Y = -8534948
81 feet Y = -2638875
22 meter
Z = -17393664
61 Z = -5317845
53
XDOT = 16439
742297 XDOT = 5076
677310
YDOT = -18913
602029 feet/sec YDOT = -5708
463048 meter/sec
ZDOT = -1183
272094 ZDOT = -336
161315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11546446
97 X = 3519357
04
Y = 7714128
08 feet Y = 2351266
24 meter
Z = -17467066
89 Z = -5323961
99
XDOT = -14460
774349 XDOT = -4407
644022
YDOT = 19221
469078 feet/sec YDOT = 5858
703775 meter/sec
ZDOT = -1071
511913 ZDOT = -326
596831
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
76809148
00016717 00000-0 10270-3 0 9117
2 25544 51
6424 313
7546 0008002 88
7363 271
4705 15
51205071 16738
Satellite: ISS
Catalog Number: 25544
Epoch time: 19177
76809148 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 313
7546 deg
Eccentricity:
0008002
Arg of perigee: 88
7363 deg
Mean anomaly: 271
4705 deg
Mean motion: 15
51205071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 309
Coasting Arc #13 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2019/178/18:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2975634
78 A = 6785833
90 meter
Y = 3046410
05 meter E =
0010683
Z = 5274035
39 I = 51
32132
XDOT = -5034
270997 Wp = 85
53162
YDOT = 5768
878065 meter/sec RA = 308
17200 deg
ZDOT = -490
206967 TA = 9
17274
MA = 9
15324
Ha = 228
386 n
mi
Hp = 216
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9762581
31 X = 2915729
41
Y = 9994783
64 feet Y = 3079350
07 meter
Z = 17303265
72 Z = 5288344
83
XDOT = -16516
637128 XDOT = -5096
024927
YDOT = 18926
765306 feet/sec YDOT = 5712
236091 meter/sec
ZDOT = -1608
290575 ZDOT = -514
810886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10507662
38 X = -3202735
49
Y = -9086012
44 feet Y = -2769416
59 meter
Z = 17367789
37 Z = 5293702
20
XDOT = 14070
125937 XDOT = 4288
574385
YDOT = -19570
830990 feet/sec YDOT = -5965
189286 meter/sec
ZDOT = -1720
509629 ZDOT = -524
411335
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 19178
79884824
00016717 00000-0 10270-3 0 9126
2 25544 51
6416 308
6392 0008072 92
0634 268
1441 15
51246770 16895
Satellite: ISS
Catalog Number: 25544
Epoch time: 19178
79884824 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 308
6392 deg
Eccentricity:
0008072
Arg of perigee: 92
0634 deg
Mean anomaly: 268
1441 deg
Mean motion: 15
51246770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 335
Coasting Arc #14 (Orbit 1703)
---------------------------------------
Vector Time (GMT): 2019/179/18:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2644201
79 A = 6786488
09 meter
Y = -3532101
09 meter E =
0021894
Z = -5175917
36 I = 51
30397
XDOT = 4969
125363 Wp = 98
24289
YDOT = -5659
505570 meter/sec RA = 303
18025 deg
ZDOT = 1325
307441 TA = 184
57681
MA = 184
59686
Ha = 228
529 n
mi
Hp = 216
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8675202
71 X = -2579366
49
Y = -11588258
18 feet Y = -3561307
14 meter
Z = -16981356
17 Z = -5188604
99
XDOT = 16302
904735 XDOT = 5025
604631
YDOT = -18567
931660 feet/sec YDOT = -5603
621724 meter/sec
ZDOT = 4348
121526 ZDOT = 1349
582029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9754335
26 X = 2973121
39
Y = 10604559
01 feet Y = 3232269
59 meter
Z = -17038474
08 Z = -5193326
90
XDOT = -13415
088594 XDOT = -4088
919003
YDOT = 19494
334469 feet/sec YDOT = 5941
873146 meter/sec
ZDOT = 4458
824537 ZDOT = 1359
049719
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 19179
76518338
00016717 00000-0 10270-3 0 9139
2 25544 51
6422 303
8429 0008026 95
3549 264
8518 15
51209075 17043
Satellite: ISS
Catalog Number: 25544
Epoch time: 19179
76518338 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 303
8429 deg
Eccentricity:
0008026
Arg of perigee: 95
3549 deg
Mean anomaly: 264
8518 deg
Mean motion: 15
51209075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1704
Checksum: 326
Coasting Arc #15 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2019/180/18:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2334141
94 A = 6787288
05 meter
Y = 4018830
36 meter E =
0013580
Z = 4935635
87 I = 51
28937
XDOT = -4901
458330 Wp = 80
39039
YDOT = 5496
884166 meter/sec RA = 298
18836 deg
ZDOT = -2150
548687 TA = 30
70113
MA = 30
62175
Ha = 228
397 n
mi
Hp = 216
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7657946
00 X = 2265054
11
Y = 13185138
99 feet Y = 4044545
26 meter
Z = 16193031
06 Z = 4946807
16
XDOT = -16080
900033 XDOT = -4952
115576
YDOT = 18034
396871 feet/sec YDOT = 5441
789740 meter/sec
ZDOT = -7055
605929 ZDOT = -2174
480330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9129732
59 X = -2782742
49
Y = -12145449
17 feet Y = -3701932
91 meter
Z = 16243224
11 Z = 4950934
71
XDOT = 12781
084532 XDOT = 3895
674565
YDOT = -19221
510620 feet/sec YDOT = -5858
716437 meter/sec
ZDOT = -7164
727640 ZDOT = -2183
808985
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 19180
79593677
00016717 00000-0 10270-3 0 9144
2 25544 51
6417 298
7271 0008124 98
6214 261
5858 15
51260040 17206
Satellite: ISS
Catalog Number: 25544
Epoch time: 19180
79593677 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 298
7271 deg
Eccentricity:
0008124
Arg of perigee: 98
6214 deg
Mean anomaly: 261
5858 deg
Mean motion: 15
51260040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 324
Coasting Arc #16 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2019/180/21:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4169883
21 A = 6786037
31 meter
Y = 1081230
43 meter E =
0011173
Z = 5234342
11 I = 51
28096
XDOT = -2908
480013 Wp = 104
32494
YDOT = 7047
408999 meter/sec RA = 297
59643 deg
ZDOT = 857
005379 TA = 337
41910
MA = 337
46822
Ha = 228
355 n
mi
Hp = 216
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13680719
18 X = 4132057
07
Y = 3547343
94 feet Y = 1127648
60 meter
Z = 17173038
41 Z = 5254506
21
XDOT = -9542
257261 XDOT = -2991
232860
YDOT = 23121
420600 feet/sec YDOT = 7014
421492 meter/sec
ZDOT = 2811
697439 ZDOT = 842
677232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11182755
99 X = -3408504
03
Y = 8458585
73 feet Y = 2578176
93 meter
Z = 17264335
21 Z = 5262169
37
XDOT = -11626
964701 XDOT = -3543
898841
YDOT = -21004
490133 feet/sec YDOT = -6402
168592 meter/sec
ZDOT = 2745
941163 ZDOT = 836
962866
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 19180
92478201
00016717 00000-0 10270-3 0 9155
2 25544 51
6397 298
0876 0008036 98
6129 261
5932 15
51226119 17228
Satellite: ISS
Catalog Number: 25544
Epoch time: 19180
92478201 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 298
0876 deg
Eccentricity:
0008036
Arg of perigee: 98
6129 deg
Mean anomaly: 261
5932 deg
Mean motion: 15
51226119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 327
Coasting Arc #17 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2019/181/21:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3928825
90 A = 6785839
47 meter
Y = -1635322
50 meter E =
0022803
Z = -5305413
65 I = 51
26620
XDOT = 2938
025652 Wp = 93
91440
YDOT = -7059
845175 meter/sec RA = 292
60191 deg
ZDOT = -1
128262 TA = 176
08370
MA = 176
06582
Ha = 228
503 n
mi
Hp = 216
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12889848
75 X = -3884476
51
Y = -5365231
29 feet Y = -1679008
42 meter
Z = -17406212
75 Z = -5324391
01
XDOT = 9639
191773 XDOT = 3016
757982
YDOT = -23162
221702 feet/sec YDOT = -7026
549893 meter/sec
ZDOT = -3
701647 ZDOT = 13
333478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12002977
08 X = 3658507
41
Y = -6918535
48 feet Y = -2108769
62 meter
Z = -17492071
29 Z = -5331583
33
XDOT = 12097
859767 XDOT = 3687
427657
YDOT = 20817
561041 feet/sec YDOT = 6345
192605 meter/sec
ZDOT = 62
652067 ZDOT = 19
096350
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 19181
89111138
00016717 00000-0 10270-3 0 9166
2 25544 51
6402 293
2915 0008057 101
4719 258
7337 15
51222450 17374
Satellite: ISS
Catalog Number: 25544
Epoch time: 19181
89111138 = yrday
fracday
Element set: 916
Inclination: 51
6402 deg
RA of node: 293
2915 deg
Eccentricity:
0008057
Arg of perigee: 101
4719 deg
Mean anomaly: 258
7337 deg
Mean motion: 15
51222450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 304
Coasting Arc #18 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2019/182/21:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3710723
51 A = 6786034
58 meter
Y = 2190230
21 meter E =
0010609
Z = 5233224
32 I = 51
25468
XDOT = -2948
233981 Wp = 91
79571
YDOT = 7031
756347 meter/sec RA = 287
60699 deg
ZDOT = -851
282020 TA = 6
38994
MA = 6
37642
Ha = 228
306 n
mi
Hp = 216
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12174289
73 X = 3660535
96
Y = 7185794
64 feet Y = 2231444
47 meter
Z = 17169371
11 Z = 5251128
08
XDOT = -9672
683665 XDOT = -3022
510938
YDOT = 23070
066755 feet/sec YDOT = 6998
371988 meter/sec
ZDOT = -2792
920012 ZDOT = -865
782392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12927748
88 X = -3940377
86
Y = 5471421
65 feet Y = 1667689
32 meter
Z = 17250308
22 Z = 5257893
94
XDOT = -12491
515265 XDOT = -3807
413853
YDOT = -20487
363480 feet/sec YDOT = -6244
548389 meter/sec
ZDOT = -2859
435277 ZDOT = -871
555872
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 19182
92186209
00016717 00000-0 10270-3 0 9173
2 25544 51
6396 288
1760 0007970 105
0785 255
1249 15
51233196 17533
Satellite: ISS
Catalog Number: 25544
Epoch time: 19182
92186209 = yrday
fracday
Element set: 917
Inclination: 51
6396 deg
RA of node: 288
1760 deg
Eccentricity:
0007970
Arg of perigee: 105
0785 deg
Mean anomaly: 255
1249 deg
Mean motion: 15
51233196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 330
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