[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 19th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13747 6664 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 995 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
141/07:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 216
9
143/14:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
5
000/00:00:00
000 0
0 0
0 216
7
143/16:03:00
458 -2
1 7
1 7
1
N/A 6
7 -0
7 223
7
000/00:20:00
916 -1
1 -0
1 221
4
143/19:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 221
4
143/21:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
6
000/00:00:00
000 0
0 0
0 221
5
144/08:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
7
000/00:00:00
000 0
0 0
0 221
3
147/06:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
0
000/00:00:00
000 0
0 0
0 221
5
Coasting Arc #1 (Orbit 1047)
---------------------------------------
Vector Time (GMT): 2019/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2447628
59 A = 6786552
02 meter
Y = 4868517
89 meter E =
0006785
Z = -4051581
44 I = 51
80915
XDOT = -6580
108569 Wp = 95
90013
YDOT = -49
846368 meter/sec RA = 152
48695 deg
ZDOT = 3920
219467 TA = 214
70937
MA = 214
75366
Ha = 223
321 n
mi
Hp = 216
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8030277
54 X = -2482207
14
Y = 15972827
74 feet Y = 4840953
69 meter
Z = -13292590
02 Z = -4063555
02
XDOT = -21588
282706 XDOT = -6598
104721
YDOT = -163
537952 feet/sec YDOT = -123
530602 meter/sec
ZDOT = 12861
612425 ZDOT = 3888
211465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8257417
21 X = 2516860
77
Y = 15810637
61 feet Y = 4819082
34 meter
Z = -13347221
88 Z = -4068233
23
XDOT = -11714
568314 XDOT = -3570
600422
YDOT = 16839
709534 feet/sec YDOT = 5132
743466 meter/sec
ZDOT = 12716
569137 ZDOT = 3876
010273
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 19137
50891694
00016717 00000-0 10270-3 0 9000
2 25544 51
6392 153
6273 0001647 356
3755 3
7385 15
52677341 10487
Satellite: ISS
Catalog Number: 25544
Epoch time: 19137
50891694 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 153
6273 deg
Eccentricity:
0001647
Arg of perigee: 356
3755 deg
Mean anomaly: 3
7385 deg
Mean motion: 15
52677341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1048
Checksum: 321
Coasting Arc #2 (Orbit 1063)
---------------------------------------
Vector Time (GMT): 2019/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3319414
70 A = 6789256
87 meter
Y = -5023721
52 meter E =
0012979
Z = 3126109
76 I = 51
84598
XDOT = 5855
492506 Wp = 87
07245
YDOT = 819
759913 meter/sec RA = 147
52608 deg
ZDOT = -4882
087050 TA = 57
05636
MA = 56
93161
Ha = 223
334 n
mi
Hp = 216
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10890468
16 X = 3360159
49
Y = -16482026
00 feet Y = -4986373
95 meter
Z = 10256265
61 Z = 3142333
08
XDOT = 19210
933419 XDOT = 5869
605435
YDOT = 2689
501028 feet/sec YDOT = 885
319448 meter/sec
ZDOT = -16017
345964 ZDOT = -4853
608377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7293168
58 X = -2222957
78
Y = -18317952
84 feet Y = -5583312
03 meter
Z = 10330186
73 Z = 3148640
91
XDOT = 11947
239567 XDOT = 3641
518620
YDOT = -13750
020746 feet/sec YDOT = -4191
006323 meter/sec
ZDOT = -15888
340194 ZDOT = -4842
766091
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 19138
53870721
00016717 00000-0 10270-3 0 9013
2 25544 51
6377 148
5043 0001775 3
1674 356
9489 15
52711291 10646
Satellite: ISS
Catalog Number: 25544
Epoch time: 19138
53870721 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 148
5043 deg
Eccentricity:
0001775
Arg of perigee: 3
1674 deg
Mean anomaly: 356
9489 deg
Mean motion: 15
52711291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1064
Checksum: 313
Coasting Arc #3 (Orbit 1078)
---------------------------------------
Vector Time (GMT): 2019/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3989680
84 A = 6791605
95 meter
Y = 5090855
35 meter E =
0007898
Z = -2062190
99 I = 51
88073
XDOT = -4999
360474 Wp = 35
03228
YDOT = -1671
116172 meter/sec RA = 142
57320 deg
ZDOT = 5563
587481 TA = 302
25481
MA = 302
33133
Ha = 223
376 n
mi
Hp = 216
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13089504
07 X = -4036294
56
Y = 16702281
33 feet Y = 5045979
54 meter
Z = -6765718
48 Z = -2081684
37
XDOT = -16402
101294 XDOT = -5007
327294
YDOT = -5482
664606 feet/sec YDOT = -1727
067667 meter/sec
ZDOT = 18253
239766 ZDOT = 5539
282509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6546671
90 X = 1995425
59
Y = 20155231
17 feet Y = 6143314
46 meter
Z = -6854488
20 Z = -2089248
00
XDOT = -12317
778217 XDOT = -3754
458801
YDOT = 10152
645696 feet/sec YDOT = 3094
526408 meter/sec
ZDOT = 18143
205089 ZDOT = 5530
048911
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 19139
50413528
00016717 00000-0 10270-3 0 9020
2 25544 51
6371 143
7026 0001642 8
2035 351
9143 15
52709337 10794
Satellite: ISS
Catalog Number: 25544
Epoch time: 19139
50413528 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 143
7026 deg
Eccentricity:
0001642
Arg of perigee: 8
2035 deg
Mean anomaly: 351
9143 deg
Mean motion: 15
52709337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1079
Checksum: 288
Coasting Arc #4 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2019/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4501558
16 A = 6793161
17 meter
Y = -5008856
35 meter E =
0012694
Z = 850086
34 I = 51
91104
XDOT = 4052
936475 Wp = 118
55236
YDOT = 2621
240351 meter/sec RA = 137
62465 deg
ZDOT = -5955
742004 TA = 52
29183
MA = 52
17681
Ha = 223
454 n
mi
Hp = 216
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14768891
59 X = 4553104
74
Y = -16433255
75 feet Y = -4958228
67 meter
Z = 2788997
18 Z = 872078
09
XDOT = 13297
035680 XDOT = 4052
253883
YDOT = 8599
869917 feet/sec YDOT = 2666
560065 meter/sec
ZDOT = -19539
835970 ZDOT = -5936
055403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5737150
67 X = -1748683
53
Y = -21323430
92 feet Y = -6499381
74 meter
Z = 2889109
62 Z = 880600
61
XDOT = 12973
232132 XDOT = 3954
241154
YDOT = -6152
244637 feet/sec YDOT = -1875
204165 meter/sec
ZDOT = -19450
804608 ZDOT = -5928
605245
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 19140
53392331
00016717 00000-0 10270-3 0 9034
2 25544 51
6365 138
5790 0001820 8
5357 351
5826 15
52698792 10959
Satellite: ISS
Catalog Number: 25544
Epoch time: 19140
53392331 = yrday
fracday
Element set: 903
Inclination: 51
6365 deg
RA of node: 138
5790 deg
Eccentricity:
0001820
Arg of perigee: 8
5357 deg
Mean anomaly: 351
5826 deg
Mean motion: 15
52698792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 317
Coasting Arc #5 (Orbit 1107)
---------------------------------------
Vector Time (GMT): 2019/141/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2729710
92 A = 6781504
64 meter
Y = -3188825
28 meter E =
0003419
Z = 5324179
15 I = 51
89469
XDOT = 5489
868417 Wp = 48
01371
YDOT = -5340
549424 meter/sec RA = 133
55062 deg
ZDOT = -381
584340 TA = 45
62594
MA = 45
59794
Ha = 223
422 n
mi
Hp = 216
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8955744
49 X = -2719711
87
Y = -10462025
19 feet Y = -3219295
63 meter
Z = 17467779
36 Z = 5310942
94
XDOT = 18011
379320 XDOT = 5551
033488
YDOT = -17521
487611 feet/sec YDOT = -5278
815826 meter/sec
ZDOT = -1251
917125 ZDOT = -354
768497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7935562
64 X = -2418759
49
Y = -11347677
65 feet Y = -3458772
15 meter
Z = 17408035
60 Z = 5305969
25
XDOT = 18916
433148 XDOT = 5765
728824
YDOT = -14973
841917 feet/sec YDOT = -4564
027016 meter/sec
ZDOT = -1129
884498 ZDOT = -344
388795
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 19141
37062276
00016717 00000-0 10270-3 0 9040
2 25544 51
6392 134
4163 0001612 1
6190 358
4966 15
52714907 11089
Satellite: ISS
Catalog Number: 25544
Epoch time: 19141
37062276 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 134
4163 deg
Eccentricity:
0001612
Arg of perigee: 1
6190 deg
Mean anomaly: 358
4966 deg
Mean motion: 15
52714907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1108
Checksum: 293
Coasting Arc #6 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2019/142/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1897224
10 A = 6782554
51 meter
Y = 4046545
49 meter E =
0013359
Z = -5113672
18 I = 51
91993
XDOT = -5644
069509 Wp = 95
62626
YDOT = 4864
915611 meter/sec RA = 128
58505 deg
ZDOT = 1758
363184 TA = 191
32293
MA = 191
35302
Ha = 223
498 n
mi
Hp = 216
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6224488
50 X = 1876673
00
Y = 13276067
87 feet Y = 4067647
37 meter
Z = -16777139
71 Z = -5104505
48
XDOT = -18517
288416 XDOT = -5706
592110
YDOT = 15961
009224 feet/sec YDOT = 4801
449848 meter/sec
ZDOT = 5768
908084 ZDOT = 1730
795039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5159626
99 X = 1572654
31
Y = 13775262
47 feet Y = 4198700
00 meter
Z = -16735920
81 Z = -5101108
66
XDOT = -18867
590666 XDOT = -5750
841635
YDOT = 13912
733435 feet/sec YDOT = 4240
601151 meter/sec
ZDOT = 5643
478462 ZDOT = 1720
132235
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 19142
33604601
00016717 00000-0 10270-3 0 9052
2 25544 51
6390 129
6141 0001774 10
2288 349
8900 15
52680529 11233
Satellite: ISS
Catalog Number: 25544
Epoch time: 19142
33604601 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 129
6141 deg
Eccentricity:
0001774
Arg of perigee: 10
2288 deg
Mean anomaly: 349
8900 deg
Mean motion: 15
52680529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 289
Coasting Arc #7 (Orbit 1138)
---------------------------------------
Vector Time (GMT): 2019/143/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1097296
25 A = 6784464
17 meter
Y = -4857345
46 meter E =
0009588
Z = 4603305
60 I = 51
94641
XDOT = 5654
302607 Wp = 57
84621
YDOT = -4182
571673 meter/sec RA = 123
62433 deg
ZDOT = -3055
956491 TA = 62
60642
MA = 62
50890
Ha = 223
462 n
mi
Hp = 216
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3600053
31 X = -1065258
84
Y = -15936172
78 feet Y = -4869437
67 meter
Z = 15102708
66 Z = 4598052
51
XDOT = 18550
861571 XDOT = 5715
497262
YDOT = -13722
348010 feet/sec YDOT = -4118
998744 meter/sec
ZDOT = -10026
103974 ZDOT = -3028
341832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2581137
02 X = -786730
56
Y = -16154438
96 feet Y = -4923873
00 meter
Z = 15079311
29 Z = 4596174
08
XDOT = 18351
271157 XDOT = 5593
467449
YDOT = -12203
218372 feet/sec YDOT = -3719
540960 meter/sec
ZDOT = -9900
499251 ZDOT = -3017
672172
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 19143
36582722
00016717 00000-0 10270-3 0 9066
2 25544 51
6387 124
4922 0001707 11
9325 348
1867 15
52723804 11390
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
36582722 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 124
4922 deg
Eccentricity:
0001707
Arg of perigee: 11
9325 deg
Mean anomaly: 348
1867 deg
Mean motion: 15
52723804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1139
Checksum: 310
Coasting Arc #8 (Orbit 1142)
---------------------------------------
Vector Time (GMT): 2019/143/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 251925
72 A = 6787853
54 meter
Y = -5719916
10 meter E =
0012601
Z = 3638037
28 I = 51
96186
XDOT = 5716
586342 Wp = 77
41783
YDOT = -2568
316722 meter/sec RA = 122
33160 deg
ZDOT = -4418
365287 TA = 59
66544
MA = 59
54087
Ha = 223
516 n
mi
Hp = 216
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 826527
94 X = 298197
12
Y = -18766128
94 feet Y = -5716840
64 meter
Z = 11935817
84 Z = 3639372
70
XDOT = 18755
204535 XDOT = 5766
343140
YDOT = -8426
235966 feet/sec YDOT = -2504
111080 meter/sec
ZDOT = -14495
949103 ZDOT = -4390
475657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18765418
69 X = -5719699
62
Y = -743734
16 feet Y = -226690
17 meter
Z = 11942378
83 Z = 3640037
07
XDOT = -8484
174879 XDOT = -2585
976503
YDOT = -17482
410390 feet/sec YDOT = -5328
638687 meter/sec
ZDOT = -14369
234038 ZDOT = -4379
742535
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 19143
62327393
00016717 00000-0 10270-3 0 9077
2 25544 51
6382 123
2118 0001996 12
4452 347
6749 15
52707566 11431
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
62327393 = yrday
fracday
Element set: 907
Inclination: 51
6382 deg
RA of node: 123
2118 deg
Eccentricity:
0001996
Arg of perigee: 12
4452 deg
Mean anomaly: 347
6749 deg
Mean motion: 15
52707566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1143
Checksum: 312
Coasting Arc #9 (Orbit 1143)
---------------------------------------
Vector Time (GMT): 2019/143/16:13:00
916
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1821178
75 A = 6787892
85 meter
Y = 4335630
51 meter E =
0006744
Z = -4901325
95 I = 51
94970
XDOT = -5310
769273 Wp = 118
99128
YDOT = 4960
875478 meter/sec RA = 121
87949 deg
ZDOT = 2414
319642 TA = 174
61304
MA = 174
60578
Ha = 223
690 n
mi
Hp = 221
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5974995
89 X = 1796369
11
Y = 14224509
54 feet Y = 4355858
10 meter
Z = -16080465
70 Z = -4892539
03
XDOT = -17423
783704 XDOT = -5377
575939
YDOT = 16275
838184 feet/sec YDOT = 4901
112893 meter/sec
ZDOT = 7920
996200 ZDOT = 2388
360219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8536514
36 X = 2601929
58
Y = -12900890
27 feet Y = -3932191
35 meter
Z = -16040996
77 Z = -4889295
82
XDOT = 22263
424728 XDOT = 6785
891857
YDOT = 5026
903114 feet/sec YDOT = 1532
200069 meter/sec
ZDOT = 7802
822323 ZDOT = 2378
300244
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 19143
68764208
00016717 00000-0 10270-3 0 9084
2 25544 51
6394 122
8903 0005477 272
8726 87
1798 15
51156907 11442
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
68764208 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 122
8903 deg
Eccentricity:
0005477
Arg of perigee: 272
8726 deg
Mean anomaly: 87
1798 deg
Mean motion: 15
51156907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1144
Checksum: 340
Coasting Arc #10 (Orbit 1146)
---------------------------------------
Vector Time (GMT): 2019/143/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4367420
96 A = 6786910
52 meter
Y = -587496
07 meter E =
0002885
Z = 5163555
58 I = 51
94902
XDOT = 2783
649929 Wp = 212
75524
YDOT = -6965
887978 meter/sec RA = 121
14979 deg
ZDOT = 1559
942414 TA = 222
24982
MA = 222
27205
Ha = 223
850 n
mi
Hp = 221
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14328808
91 X = -4385608
54
Y = -1927480
55 feet Y = -636437
97 meter
Z = 16940799
13 Z = 5142295
99
XDOT = 9132
709740 XDOT = 2853
760240
YDOT = -22853
963181 feet/sec YDOT = -6934
367439 meter/sec
ZDOT = 5117
921306 ZDOT = 1573
633786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14406357
61 X = 4391057
80
Y = 2177769
45 feet Y = 663784
13 meter
Z = 16844429
40 Z = 5134182
08
XDOT = -9336
336297 XDOT = -2845
715303
YDOT = 21641
021894 feet/sec YDOT = 6596
183473 meter/sec
ZDOT = 5180
634791 ZDOT = 1579
057484
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 19143
88091779
00016717 00000-0 10270-3 0 9093
2 25544 51
6396 121
9317 0005565 274
0294 86
0221 15
51133851 11470
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
88091779 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 121
9317 deg
Eccentricity:
0005565
Arg of perigee: 274
0294 deg
Mean anomaly: 86
0221 deg
Mean motion: 15
51133851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1147
Checksum: 317
Coasting Arc #11 (Orbit 1146)
---------------------------------------
Vector Time (GMT): 2019/143/21:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2560980
92 A = 6797330
77 meter
Y = 6168023
87 meter E =
0007404
Z = -1238416
99 I = 51
98309
XDOT = -4850
468125 Wp = 358
65942
YDOT = -835
914720 meter/sec RA = 120
88352 deg
ZDOT = 5873
665744 TA = 347
95957
MA = 347
97726
Ha = 223
593 n
mi
Hp = 221
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8402168
39 X = -2623747
64
Y = 20236298
79 feet Y = 6139034
39 meter
Z = -4063047
87 Z = -1251008
98
XDOT = -15913
609333 XDOT = -4869
291247
YDOT = -2742
502363 feet/sec YDOT = -890
262027 meter/sec
ZDOT = 19270
556902 ZDOT = 5850
058119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2263820
88 X = 690012
60
Y = -21783192
67 feet Y = -6639517
12 meter
Z = -4120705
34 Z = -1255990
99
XDOT = 14570
311406 XDOT = 4441
030916
YDOT = -2106
961017 feet/sec YDOT = -642
201718 meter/sec
ZDOT = 19163
559081 ZDOT = 5841
052808
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 19143
88091654
00016717 00000-0 10270-3 0 9107
2 25544 51
6378 121
9300 0005739 272
9359 87
1135 15
51150669 11476
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
88091654 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 121
9300 deg
Eccentricity:
0005739
Arg of perigee: 272
9359 deg
Mean anomaly: 87
1135 deg
Mean motion: 15
51150669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1147
Checksum: 317
Coasting Arc #12 (Orbit 1154)
---------------------------------------
Vector Time (GMT): 2019/144/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 477235
42 A = 6793769
37 meter
Y = -6006915
81 meter E =
0007609
Z = 3130202
57 I = 51
98070
XDOT = 5504
087808 Wp = 95
45315
YDOT = -2117
867427 meter/sec RA = 118
50448 deg
ZDOT = -4893
884893 TA = 48
73376
MA = 48
66825
Ha = 223
723 n
mi
Hp = 221
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1565733
01 X = 529166
20
Y = -19707729
05 feet Y = -6001289
04 meter
Z = 10269693
48 Z = 3132646
23
XDOT = 18058
030867 XDOT = 5551
133128
YDOT = -6948
383948 feet/sec YDOT = -2056
053239 meter/sec
ZDOT = -16056
052798 ZDOT = -4867
034051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1783684
26 X = -543666
96
Y = -19683133
84 feet Y = -5999419
20 meter
Z = 10281314
15 Z = 3133744
55
XDOT = 15330
210311 XDOT = 4672
648103
YDOT = -9728
515698 feet/sec YDOT = -2965
251585 meter/sec
ZDOT = -15934
075822 ZDOT = -4856
706311
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 19144
39632047
00016717 00000-0 10270-3 0 9112
2 25544 51
6389 119
3728 0005312 274
3480 85
7064 15
51178687 11555
Satellite: ISS
Catalog Number: 25544
Epoch time: 19144
39632047 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 119
3728 deg
Eccentricity:
0005312
Arg of perigee: 274
3480 deg
Mean anomaly: 85
7064 deg
Mean motion: 15
51178687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1155
Checksum: 321
Coasting Arc #13 (Orbit 1169)
---------------------------------------
Vector Time (GMT): 2019/145/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -593990
10 A = 6795184
30 meter
Y = 6280563
22 meter E =
0004252
Z = -2517518
97 I = 52
00196
XDOT = -5256
377228 Wp = 344
44915
YDOT = 1638
086969 meter/sec RA = 113
56803 deg
ZDOT = 5328
712396 TA = 347
49475
MA = 347
50529
Ha = 223
792 n
mi
Hp = 221
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1948786
41 X = -651948
29
Y = 20605522
39 feet Y = 6273597
01 meter
Z = -8259576
68 Z = -2520544
47
XDOT = -17245
332114 XDOT = -5300
188053
YDOT = 5374
301081 feet/sec YDOT = 1579
060960 meter/sec
ZDOT = 17482
652217 ZDOT = 5303
072635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1895862
06 X = 577858
75
Y = 20604724
69 feet Y = 6280320
09 meter
Z = -8273871
86 Z = -2521876
14
XDOT = -14588
333525 XDOT = -4446
524058
YDOT = 8313
219905 feet/sec YDOT = 2533
869427 meter/sec
ZDOT = 17366
197854 ZDOT = 5293
217106
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 19145
36270033
00016717 00000-0 10270-3 0 9124
2 25544 51
6404 114
5769 0005235 277
7379 82
3177 15
51193844 11700
Satellite: ISS
Catalog Number: 25544
Epoch time: 19145
36270033 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 114
5769 deg
Eccentricity:
0005235
Arg of perigee: 277
7379 deg
Mean anomaly: 82
3177 deg
Mean motion: 15
51193844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1170
Checksum: 308
Coasting Arc #14 (Orbit 1185)
---------------------------------------
Vector Time (GMT): 2019/146/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 673366
98 A = 6796501
33 meter
Y = -6502071
38 meter E =
0008849
Z = 1843609
24 I = 52
01635
XDOT = 5039
450512 Wp = 120
45782
YDOT = -1090
150391 meter/sec RA = 108
63449 deg
ZDOT = -5669
543648 TA = 39
39756
MA = 39
33324
Ha = 223
946 n
mi
Hp = 221
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2209209
24 X = 737069
71
Y = -21332255
20 feet Y = -6494185
31 meter
Z = 6048586
75 Z = 1847034
34
XDOT = 16533
630288 XDOT = 5078
805865
YDOT = -3576
608894 feet/sec YDOT = -1033
575156 meter/sec
ZDOT = -18600
864987 ZDOT = -5644
968370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2125106
79 X = -647732
55
Y = -21336216
49 feet Y = -6503278
79 meter
Z = 6064726
38 Z = 1848528
60
XDOT = 14055
336013 XDOT = 4284
066417
YDOT = -6670
158473 feet/sec YDOT = -2033
064303 meter/sec
ZDOT = -18489
279038 ZDOT = -5635
532251
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 19146
39350429
00016717 00000-0 10270-3 0 9137
2 25544 51
6383 109
4615 0005234 282
7664 77
2902 15
51169597 11865
Satellite: ISS
Catalog Number: 25544
Epoch time: 19146
39350429 = yrday
fracday
Element set: 913
Inclination: 51
6383 deg
RA of node: 109
4615 deg
Eccentricity:
0005234
Arg of perigee: 282
7664 deg
Mean anomaly: 77
2902 deg
Mean motion: 15
51169597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1186
Checksum: 326
Coasting Arc #15 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2019/147/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4379682
50 A = 6788039
96 meter
Y = -1761452
96 meter E =
0007681
Z = -4884818
22 I = 51
99798
XDOT = 161
583457 Wp = 50
55541
YDOT = 7247
414598 meter/sec RA = 104
13919 deg
ZDOT = -2466
364101 TA = 195
30638
MA = 195
32963
Ha = 223
996 n
mi
Hp = 221
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14369037
08 X = 4422781
86
Y = -5779045
13 feet Y = -1712234
89 meter
Z = -16026306
49 Z = -4863438
77
XDOT = 530
129451 XDOT = 92
509049
YDOT = 23777
606948 feet/sec YDOT = 7248
835520 meter/sec
ZDOT = -8091
745738 ZDOT = -2465
746362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15541328
25 X = 4736996
85
Y = -1199348
18 feet Y = -365561
33 meter
Z = -15929148
41 Z = -4855204
44
XDOT = -6621
417324 XDOT = -2018
208000
YDOT = 21735
842873 feet/sec YDOT = 6625
084908 meter/sec
ZDOT = -8089
625626 ZDOT = -2465
717891
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 19147
29545710
00016717 00000-0 10270-3 0 9147
2 25544 51
6395 104
9844 0005392 284
5813 75
4739 15
51155468 12000
Satellite: ISS
Catalog Number: 25544
Epoch time: 19147
29545710 = yrday
fracday
Element set: 914
Inclination: 51
6395 deg
RA of node: 104
9844 deg
Eccentricity:
0005392
Arg of perigee: 284
5813 deg
Mean anomaly: 75
4739 deg
Mean motion: 15
51155468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 321
Coasting Arc #16 (Orbit 1215)
---------------------------------------
Vector Time (GMT): 2019/148/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4263766
94 A = 6786909
16 meter
Y = 1236495
59 meter E =
0001359
Z = 5134519
63 I = 52
00123
XDOT = -128
966977 Wp = 215
11551
YDOT = -7472
628282 meter/sec RA = 99
19631 deg
ZDOT = 1691
604014 TA = 218
61117
MA = 218
62090
Ha = 224
337 n
mi
Hp = 221
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13988736
70 X = -4302217
68
Y = 4056744
06 feet Y = 1188599
78 meter
Z = 16845536
84 Z = 5113714
44
XDOT = -423
120004 XDOT = -53
613247
YDOT = -24516
496989 feet/sec YDOT = -7473
649279 meter/sec
ZDOT = 5549
881937 ZDOT = 1691
159997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14673468
47 X = -4472473
19
Y = -80331
52 feet Y = -24485
05 meter
Z = 16751027
07 Z = 5105713
05
XDOT = 6461
054367 XDOT = 1969
329371
YDOT = -22582
289390 feet/sec YDOT = -6883
081806 meter/sec
ZDOT = 5548
585705 ZDOT = 1691
208923
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 19148
32625633
00016717 00000-0 10270-3 0 9156
2 25544 51
6393 99
8684 0005332 290
2896 69
7682 15
51175327 12167
Satellite: ISS
Catalog Number: 25544
Epoch time: 19148
32625633 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 99
8684 deg
Eccentricity:
0005332
Arg of perigee: 290
2896 deg
Mean anomaly: 69
7682 deg
Mean motion: 15
51175327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1216
Checksum: 337
Coasting Arc #17 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2019/149/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4199024
69 A = 6786263
38 meter
Y = -686489
78 meter E =
0010153
Z = -5295378
80 I = 52
00440
XDOT = 126
322003 Wp = 67
48583
YDOT = 7604
262354 meter/sec RA = 94
25317 deg
ZDOT = -883
214990 TA = 194
08279
MA = 194
11112
Ha = 224
368 n
mi
Hp = 221
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13776327
73 X = 4232111
36
Y = -2252263
04 feet Y = -639347
94 meter
Z = -17373290
03 Z = -5274901
03
XDOT = 414
442266 XDOT = 45
569787
YDOT = 24948
367303 feet/sec YDOT = 7605
223527 meter/sec
ZDOT = -2897
686976 ZDOT = -882
796924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13992666
45 X = 4264964
73
Y = 1512323
60 feet Y = 460956
23 meter
Z = -17280314
34 Z = -5267039
81
XDOT = -6088
949876 XDOT = -1855
911922
YDOT = 23149
226890 feet/sec YDOT = 7055
884356 meter/sec
ZDOT = -2896
537911 ZDOT = -882
864755
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 19149
29262904
00016717 00000-0 10270-3 0 9162
2 25544 51
6405 95
0726 0005424 293
7602 66
2980 15
51162564 12310
Satellite: ISS
Catalog Number: 25544
Epoch time: 19149
29262904 = yrday
fracday
Element set: 916
Inclination: 51
6405 deg
RA of node: 95
0726 deg
Eccentricity:
0005424
Arg of perigee: 293
7602 deg
Mean anomaly: 66
2980 deg
Mean motion: 15
51162564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 306
Coasting Arc #18 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2019/150/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4177287
40 A = 6785964
82 meter
Y = 110629
80 meter E =
0003300
Z = 5348618
14 I = 52
00320
XDOT = -135
401457 Wp = 317
40868
YDOT = -7661
046879 meter/sec RA = 89
30929 deg
ZDOT = 55
092805 TA = 132
08260
MA = 132
05453
Ha = 224
649 n
mi
Hp = 221
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13705011
17 X = -4204194
95
Y = 362958
65 feet Y = 63765
55 meter
Z = 17547959
78 Z = 5328260
86
XDOT = -444
230501 XDOT = -49
990994
YDOT = -25134
668237 feet/sec YDOT = -7662
083477 meter/sec
ZDOT = 180
750673 ZDOT = 54
641881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13478941
26 X = -4108381
30
Y = -3083934
23 feet Y = -939983
15 meter
Z = 17455585
20 Z = 5320462
37
XDOT = 5592
849979 XDOT = 1704
700674
YDOT = -23473
251003 feet/sec YDOT = -7154
646906 meter/sec
ZDOT = 179
477129 ZDOT = 54
704629
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 19150
32342553
00016717 00000-0 10270-3 0 9178
2 25544 51
6388 89
9566 0005296 298
8148 61
2471 15
51174785 12477
Satellite: ISS
Catalog Number: 25544
Epoch time: 19150
32342553 = yrday
fracday
Element set: 917
Inclination: 51
6388 deg
RA of node: 89
9566 deg
Eccentricity:
0005296
Arg of perigee: 298
8148 deg
Mean anomaly: 61
2471 deg
Mean motion: 15
51174785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1247
Checksum: 339
Coasting Arc #19 (Orbit 1261)
---------------------------------------
Vector Time (GMT): 2019/151/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4212474
72 A = 6786204
85 meter
Y = 452905
36 meter E =
0009851
Z = -5309432
55 I = 52
00349
XDOT = 147
503419 Wp = 82
03822
YDOT = 7616
549676 meter/sec RA = 84
36600 deg
ZDOT = 769
279658 TA = 195
27169
MA = 195
30144
Ha = 224
715 n
mi
Hp = 221
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13820455
13 X = 4232887
77
Y = 1485909
98 feet Y = 500126
87 meter
Z = -17419398
13 Z = -5288920
01
XDOT = 483
935102 XDOT = 58
585238
YDOT = 24988
680040 feet/sec YDOT = 7617
701914 meter/sec
ZDOT = 2523
883393 ZDOT = 769
780968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13212642
44 X = 4027213
41
Y = 4676658
09 feet Y = 1425445
39 meter
Z = -17326375
52 Z = -5281079
26
XDOT = -5000
382816 XDOT = -1524
116682
YDOT = 23452
295747 feet/sec YDOT = 7148
259744 meter/sec
ZDOT = 2525
369224 ZDOT = 769
732539
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 19151
28979502
00016717 00000-0 10270-3 0 9185
2 25544 51
6399 85
1611 0005511 301
3385 58
7227 15
51160575 12620
Satellite: ISS
Catalog Number: 25544
Epoch time: 19151
28979502 = yrday
fracday
Element set: 918
Inclination: 51
6399 deg
RA of node: 85
1611 deg
Eccentricity:
0005511
Arg of perigee: 301
3385 deg
Mean anomaly: 58
7227 deg
Mean motion: 15
51160575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1262
Checksum: 309
Coasting Arc #20 (Orbit 1277)
---------------------------------------
Vector Time (GMT): 2019/152/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4291284
57 A = 6786771
30 meter
Y = -1020838
82 meter E =
0006082
Z = 5159552
37 I = 52
00089
XDOT = -135
883036 Wp = 356
58173
YDOT = -7494
175805 meter/sec RA = 79
42189 deg
ZDOT = -1589
962293 TA = 108
71889
MA = 108
65288
Ha = 224
916 n
mi
Hp = 220
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14079017
61 X = -4304612
95
Y = -3349208
74 feet Y = -1068902
11 meter
Z = 16927665
25 Z = 5138674
09
XDOT = -445
810487 XDOT = -44
347650
YDOT = -24587
190962 feet/sec YDOT = -7495
183348 meter/sec
ZDOT = -5216
411722 ZDOT = -1590
400943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13139494
41 X = -4004917
89
Y = -6323300
52 feet Y = -1927342
00 meter
Z = 16833043
22 Z = 5130711
57
XDOT = 4428
062605 XDOT = 1349
673482
YDOT = -23141
901296 feet/sec YDOT = -7053
651515 meter/sec
ZDOT = -5217
604124 ZDOT = -1590
325737
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 19152
32058617
00016717 00000-0 10270-3 0 9197
2 25544 51
6395 80
0448 0005456 306
7326 53
3324 15
51186500 12782
Satellite: ISS
Catalog Number: 25544
Epoch time: 19152
32058617 = yrday
fracday
Element set: 919
Inclination: 51
6395 deg
RA of node: 80
0448 deg
Eccentricity:
0005456
Arg of perigee: 306
7326 deg
Mean anomaly: 53
3324 deg
Mean motion: 15
51186500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1278
Checksum: 303
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