[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 1st 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
7
000/00:00:00
000 0
0 0
0 215
5
061/07:49:02
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
5
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
073/19:14:11
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
5
074/01:07:00
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
Coasting Arc #1 (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 = 6574664
94 A = 6792362
74 meter
Y = 704505
14 meter E =
0010044
Z = -1544823
40 I = 51
68144
XDOT = -1849
303897 Wp = 123
84922
YDOT = 4708
889880 meter/sec RA = 175
47650 deg
ZDOT = -5755
401867 TA = 73
00686
MA = 72
89682
Ha = 224
432 n
mi
Hp = 215
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21570423
03 X = 6573802
07
Y = 2311368
58 feet Y = 778022
74 meter
Z = -5068318
25 Z = -1512888
93
XDOT = -6067
270002 XDOT = -1873
866620
YDOT = 15449
113779 feet/sec YDOT = 4688
072054 meter/sec
ZDOT = -18882
552056 ZDOT = -5764
444792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19186463
37 X = 5848034
04
Y = 10195431
01 feet Y = 3107567
37 meter
Z = -4924046
50 Z = -1500849
37
XDOT = -10526
183405 XDOT = -3208
380702
YDOT = 10722
107270 feet/sec YDOT = 3268
098296 meter/sec
ZDOT = -18923
770558 ZDOT = -5767
965266
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
52930245
00016717 00000-0 10270-3 0 9003
2 25544 51
6392 176
5055 0003485 72
8865 287
2669 15
52756296 38529
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
52930245 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 176
5055 deg
Eccentricity:
0003485
Arg of perigee: 72
8865 deg
Mean anomaly: 287
2669 deg
Mean motion: 15
52756296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3852
Checksum: 336
Coasting Arc #2 (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 = -6115400
64 A = 6790719
51 meter
Y = -1429405
78 meter E =
0017607
Z = 2561088
56 I = 51
68243
XDOT = 3272
690354 Wp = 74
52926
YDOT = -4509
855029 meter/sec RA = 174
35607 deg
ZDOT = 5271
919142 TA = 314
24012
MA = 314
38454
Ha = 224
658 n
mi
Hp = 215
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20063650
41 X = -6111402
20
Y = -4689651
51 feet Y = -1497769
98 meter
Z = 8402521
52 Z = 2531392
65
XDOT = 10737
173079 XDOT = 3297
270081
YDOT = -14796
112299 feet/sec YDOT = -4473
119819 meter/sec
ZDOT = 17296
322644 ZDOT = 5287
876235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14062715
08 X = -4286315
56
Y = 15133360
80 feet Y = 4612648
37 meter
Z = 8268415
96 Z = 2520213
18
XDOT = -6462
156015 XDOT = -1969
665153
YDOT = -15541
377855 feet/sec YDOT = -4737
011970 meter/sec
ZDOT = 17368
776204 ZDOT = 5294
002987
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
78674004
00016717 00000-0 10270-3 0 9010
2 25544 51
6385 175
2278 0003955 68
6659 291
4914 15
52727639 38563
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
78674004 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 175
2278 deg
Eccentricity:
0003955
Arg of perigee: 68
6659 deg
Mean anomaly: 291
4914 deg
Mean motion: 15
52727639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 347
Coasting Arc #3 (Orbit 3864)
---------------------------------------
Vector Time (GMT): 2019/061/07:49:02
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4346269
57 A = 6787384
60 meter
Y = -3638097
87 meter E =
0015028
Z = 3723182
34 I = 51
68957
XDOT = 5823
381087 Wp = 81
18903
YDOT = 2544
376627 meter/sec RA = 171
33163 deg
ZDOT = -4294
655384 TA = 54
40840
MA = 54
26845
Ha = 224
338 n
mi
Hp = 215
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14259414
61 X = 4368544
04
Y = -11936016
65 feet Y = -3589370
09 meter
Z = 12215165
15 Z = 3744348
72
XDOT = 19105
580993 XDOT = 5815
356933
YDOT = 8347
692345 feet/sec YDOT = 2609
452631 meter/sec
ZDOT = -14090
076718 ZDOT = -4266
387847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13394840
56 X = 4082747
40
Y = 12807208
60 feet Y = 3903637
18 meter
Z = 12311105
23 Z = 3752424
87
XDOT = -5293
105353 XDOT = -1613
338512
YDOT = 19010
986803 feet/sec YDOT = 5794
548777 meter/sec
ZDOT = -13962
497793 ZDOT = -4255
769327
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
36597037
00016717 00000-0 10270-3 0 9026
2 25544 51
6365 172
3432 0003502 70
6740 289
4790 15
52746658 38654
Satellite: ISS
Catalog Number: 25544
Epoch time: 19061
36597037 = yrday
fracday
Element set: 902
Inclination: 51
6365 deg
RA of node: 172
3432 deg
Eccentricity:
0003502
Arg of perigee: 70
6740 deg
Mean anomaly: 289
4790 deg
Mean motion: 15
52746658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3865
Checksum: 324
Coasting Arc #4 (Orbit 3879)
---------------------------------------
Vector Time (GMT): 2019/062/07:49:02
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5144765
39 A = 6790030
41 meter
Y = 3478269
52 meter E =
0008418
Z = -2747513
84 I = 51
73189
XDOT = -4790
316119 Wp = 67
39088
YDOT = -3024
184096 meter/sec RA = 166
36438 deg
ZDOT = 5157
190934 TA = 261
59016
MA = 261
68560
Ha = 224
473 n
mi
Hp = 215
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16879151
54 X = -5169932
43
Y = 11411645
39 feet Y = 3420596
24 meter
Z = -9014153
01 Z = -2772565
96
XDOT = -15716
260234 XDOT = -4781
192998
YDOT = -9921
863833 feet/sec YDOT = -3077
701381 meter/sec
ZDOT = 16919
917763 ZDOT = 5133
944295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13423129
14 X = -4091369
76
Y = -15260793
14 feet Y = -4651489
75 meter
Z = -9127659
00 Z = -2782110
46
XDOT = 6752
228778 XDOT = 2058
079331
YDOT = -15965
862608 feet/sec YDOT = -4866
394923 meter/sec
ZDOT = 16815
052900 ZDOT = 5125
228124
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
33135564
00016717 00000-0 10270-3 0 9038
2 25544 51
6371 167
5404 0003765 76
6326 283
5245 15
52760026 38805
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
33135564 = yrday
fracday
Element set: 903
Inclination: 51
6371 deg
RA of node: 167
5404 deg
Eccentricity:
0003765
Arg of perigee: 76
6326 deg
Mean anomaly: 283
5245 deg
Mean motion: 15
52760026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3880
Checksum: 307
Coasting Arc #5 (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 = -6326912
83 A = 6792990
58 meter
Y = 2306480
87 meter E =
0013099
Z = -855749
51 I = 51
74883
XDOT = -2339
846732 Wp = 49
55559
YDOT = -4238
851372 meter/sec RA = 165
72028 deg
ZDOT = 5942
670892 TA = 301
20703
MA = 301
33535
Ha = 224
456 n
mi
Hp = 215
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20757588
04 X = -6348077
67
Y = 7567194
46 feet Y = 2235610
51 meter
Z = -2807577
13 Z = -886534
13
XDOT = -7676
662505 XDOT = -2321
138314
YDOT = -13906
992691 feet/sec YDOT = -4264
912134 meter/sec
ZDOT = 19496
951747 ZDOT = 5931
350811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21333112
21 X = -6502332
60
Y = -5677711
61 feet Y = -1730566
50 meter
Z = -2946913
10 Z = -898219
11
XDOT = 1152
891393 XDOT = 351
401297
YDOT = -14314
496463 feet/sec YDOT = -4363
058522 meter/sec
ZDOT = 19446
090005 ZDOT = 5927
168234
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
46007331
00016717 00000-0 10270-3 0 9043
2 25544 51
6401 166
9005 0003666 77
2253 282
9308 15
52751228 38824
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
46007331 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 166
9005 deg
Eccentricity:
0003666
Arg of perigee: 77
2253 deg
Mean anomaly: 282
9308 deg
Mean motion: 15
52751228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3882
Checksum: 301
Coasting Arc #6 (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 = 6500781
83 A = 6793229
57 meter
Y = -1906538
39 meter E =
0013641
Z = -433651
57 I = 51
78126
XDOT = 977
226863 Wp = 125
61870
YDOT = 4665
587066 meter/sec RA = 160
76546 deg
ZDOT = -6003
002915 TA = 59
04511
MA = 58
91113
Ha = 224
475 n
mi
Hp = 215
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21328024
36 X = 6523724
52
Y = -6255047
22 feet Y = -1833713
86 meter
Z = -1422741
37 Z = -402018
06
XDOT = 3206
124879 XDOT = 954
140895
YDOT = 15307
044180 feet/sec YDOT = 4676
385484 meter/sec
ZDOT = -19694
891455 ZDOT = -5998
312511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21191300
47 X = 6459108
38
Y = 6732450
63 feet Y = 2052050
95 meter
Z = -1279579
89 Z = -390015
95
XDOT = -5291
553836 XDOT = -1612
865609
YDOT = 13013
861410 feet/sec YDOT = 3966
624958 meter/sec
ZDOT = -19674
027754 ZDOT = -5996
643659
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
48981407
00016717 00000-0 10270-3 0 9052
2 25544 51
6397 161
7781 0003584 82
4070 277
7488 15
52764977 38989
Satellite: ISS
Catalog Number: 25544
Epoch time: 19063
48981407 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 161
7781 deg
Eccentricity:
0003584
Arg of perigee: 82
4070 deg
Mean anomaly: 277
7488 deg
Mean motion: 15
52764977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3898
Checksum: 365
Coasting Arc #7 (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 = -6416986
92 A = 6792190
58 meter
Y = 1459101
01 meter E =
0017370
Z = 1650425
13 I = 51
81021
XDOT = 327
470701 Wp = 67
97025
YDOT = -5087
707441 meter/sec RA = 155
81168 deg
ZDOT = 5729
284318 TA = 310
05917
MA = 310
21139
Ha = 224
502 n
mi
Hp = 215
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21053106
68 X = -6440842
75
Y = 4787076
80 feet Y = 1387208
56 meter
Z = 5414780
61 Z = 1619196
41
XDOT = 1074
378941 XDOT = 356
509475
YDOT = -16691
953548 feet/sec YDOT = -5083
882472 meter/sec
ZDOT = 18796
864560 ZDOT = 5730
946071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20296861
31 X = -6186483
33
Y = -7463057
52 feet Y = -2274739
93 meter
Z = 5273466
39 Z = 1607352
56
XDOT = 9336
628155 XDOT = 2845
804262
YDOT = -12005
031384 feet/sec YDOT = -3659
133566 meter/sec
ZDOT = 18804
751831 ZDOT = 5731
688358
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
51955171
00016717 00000-0 10270-3 0 9067
2 25544 51
6411 156
6558 0003657 84
5870 275
5699 15
52770773 39143
Satellite: ISS
Catalog Number: 25544
Epoch time: 19064
51955171 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 156
6558 deg
Eccentricity:
0003657
Arg of perigee: 84
5870 deg
Mean anomaly: 275
5699 deg
Mean motion: 15
52770773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3914
Checksum: 344
Coasting Arc #8 (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 = 6115001
86 A = 6790010
33 meter
Y = -867899
89 meter E =
0008040
Z = -2824342
98 I = 51
83254
XDOT = -1577
227457 Wp = 106
90474
YDOT = 5481
233431 meter/sec RA = 150
85679 deg
ZDOT = -5113
512731 TA = 105
03018
MA = 104
94119
Ha = 224
508 n
mi
Hp = 215
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20062342
06 X = 6137971
31
Y = -2847440
58 feet Y = -799389
56 meter
Z = -9266217
13 Z = -2794583
28
XDOT = -5174
630763 XDOT = -1613
564811
YDOT = 17983
049313 feet/sec YDOT = 5463
391999 meter/sec
ZDOT = -16776
616571 ZDOT = -5121
263056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18576321
30 X = 5662062
73
Y = 8246386
26 feet Y = 2513498
53 meter
Z = -9131575
30 Z = -2783304
15
XDOT = -13219
066648 XDOT = -4029
171514
YDOT = 11214
107006 feet/sec YDOT = 3418
059815 meter/sec
ZDOT = -16812
068155 ZDOT = -5124
318374
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
48492770
00016717 00000-0 10270-3 0 9076
2 25544 51
6409 151
8537 0003631 87
8243 272
3324 15
52766373 39293
Satellite: ISS
Catalog Number: 25544
Epoch time: 19065
48492770 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 151
8537 deg
Eccentricity:
0003631
Arg of perigee: 87
8243 deg
Mean anomaly: 272
3324 deg
Mean motion: 15
52766373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3929
Checksum: 333
Coasting Arc #9 (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 = -5615112
75 A = 6787212
98 meter
Y = 201569
26 meter E =
0015220
Z = 3795538
83 I = 51
85184
XDOT = 2662
716218 Wp = 95
48360
YDOT = -5817
367151 meter/sec RA = 145
89882 deg
ZDOT = 4232
173715 TA = 309
89747
MA = 310
03118
Ha = 224
542 n
mi
Hp = 215
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18422285
94 X = -5635385
76
Y = 661316
47 feet Y = 138664
26 meter
Z = 12452555
20 Z = 3768213
89
XDOT = 8735
945596 XDOT = 2707
012540
YDOT = -19085
850232 feet/sec YDOT = -5787
342591 meter/sec
ZDOT = 13885
084368 ZDOT = 4245
216299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16201969
99 X = -4938360
45
Y = -8965319
71 feet Y = -2732629
45 meter
Z = 12328961
87 Z = 3757867
58
XDOT = 16585
529693 XDOT = 5055
269450
YDOT = -10723
982448 feet/sec YDOT = -3268
669850 meter/sec
ZDOT = 13944
501559 ZDOT = 4250
284075
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
51465873
00016717 00000-0 10270-3 0 9086
2 25544 51
6408 146
7315 0003649 91
2222 268
9348 15
52799222 39458
Satellite: ISS
Catalog Number: 25544
Epoch time: 19066
51465873 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 146
7315 deg
Eccentricity:
0003649
Arg of perigee: 91
2222 deg
Mean anomaly: 268
9348 deg
Mean motion: 15
52799222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3945
Checksum: 338
Coasting Arc #10 (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 = -4276221
71 A = 6782829
80 meter
Y = -1691595
53 meter E =
0009617
Z = 4979121
99 I = 51
85073
XDOT = 4739
971142 Wp = 109
33532
YDOT = -5635
997165 meter/sec RA = 143
31917 deg
ZDOT = 2149
587112 TA = 319
75542
MA = 319
82658
Ha = 224
617 n
mi
Hp = 215
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14029598
79 X = -4281173
47
Y = -5549854
11 feet Y = -1739442
29 meter
Z = 16335702
06 Z = 4958338
18
XDOT = 15551
086425 XDOT = 4792
200819
YDOT = -18490
804348 feet/sec YDOT = -5582
699186 meter/sec
ZDOT = 7052
451155 ZDOT = 2172
739365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10730798
53 X = 3270747
39
Y = 10748890
65 feet Y = 3276261
87 meter
Z = 16241828
63 Z = 4950509
37
XDOT = -20829
467254 XDOT = -6348
821619
YDOT = 9946
801291 feet/sec YDOT = 3031
785033 meter/sec
ZDOT = 7157
583295 ZDOT = 2181
631388
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
02952560
00016717 00000-0 10270-3 0 9098
2 25544 51
6402 144
1734 0003747 85
7755 274
3825 15
52787936 39536
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
02952560 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 144
1734 deg
Eccentricity:
0003747
Arg of perigee: 85
7755 deg
Mean anomaly: 274
3825 deg
Mean motion: 15
52787936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3953
Checksum: 338
Coasting Arc #11 (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 = -5924207
86 A = 6790840
34 meter
Y = 2269572
02 meter E =
0017324
Z = 2401788
56 I = 51
88374
XDOT = 103
166612 Wp = 78
17688
YDOT = -5460
373434 meter/sec RA = 141
75912 deg
ZDOT = 5384
944525 TA = 308
56857
MA = 308
72366
Ha = 224
513 n
mi
Hp = 215
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19436377
49 X = -5960812
97
Y = 7446102
42 feet Y = 2203119
02 meter
Z = 7879883
71 Z = 2372922
14
XDOT = 338
473138 XDOT = 138
061641
YDOT = -17914
611003 feet/sec YDOT = -5459
023954 meter/sec
ZDOT = 17667
140831 ZDOT = 5385
531114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7383403
47 X = -2250461
38
Y = -19512706
77 feet Y = -5947473
02 meter
Z = 7749155
21 Z = 2361942
51
XDOT = 16489
737255 XDOT = 5026
071915
YDOT = 816
722543 feet/sec YDOT = 248
937031 meter/sec
ZDOT = 17670
203045 ZDOT = 5385
877888
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
35131539
00016717 00000-0 10270-3 0 9101
2 25544 51
6380 142
5675 0003731 94
6506 265
5072 15
52798721 39588
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
35131539 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 142
5675 deg
Eccentricity:
0003731
Arg of perigee: 94
6506 deg
Mean anomaly: 265
5072 deg
Mean motion: 15
52798721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 323
Coasting Arc #12 (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 = 5625011
79 A = 6788215
86 meter
Y = -1535003
20 meter E =
0008699
Z = -3483230
86 I = 51
90070
XDOT = -1181
063454 Wp = 92
04588
YDOT = 6028
234831 meter/sec RA = 136
80537 deg
ZDOT = -4573
979824 TA = 128
62405
MA = 128
54614
Ha = 224
527 n
mi
Hp = 215
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18454763
09 X = 5658678
03
Y = -5036099
75 feet Y = -1471912
58 meter
Z = -11427922
77 Z = -3455824
94
XDOT = -3874
880098 XDOT = -1226
167436
YDOT = 19777
673330 feet/sec YDOT = 6014
774588 meter/sec
ZDOT = -15006
495485 ZDOT = -4579
827241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5295052
35 X = 1613931
95
Y = 18458698
18 feet Y = 5626211
21 meter
Z = -11303843
70 Z = -3445411
56
XDOT = -18481
406738 XDOT = -5633
132774
YDOT = -3884
049191 feet/sec YDOT = -1183
858194 meter/sec
ZDOT = -15033
404027 ZDOT = -4582
181547
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
31668537
00016717 00000-0 10270-3 0 9112
2 25544 51
6384 137
7644 0003783 95
7003 264
4580 15
52784843 39734
Satellite: ISS
Catalog Number: 25544
Epoch time: 19068
31668537 = yrday
fracday
Element set: 911
Inclination: 51
6384 deg
RA of node: 137
7644 deg
Eccentricity:
0003783
Arg of perigee: 95
7003 deg
Mean anomaly: 264
4580 deg
Mean motion: 15
52784843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3973
Checksum: 340
Coasting Arc #13 (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 = -5173436
76 A = 6785359
44 meter
Y = 694602
57 meter E =
0013567
Z = 4326211
31 I = 51
91489
XDOT = 2091
869239 Wp = 105
52809
YDOT = -6481
583473 meter/sec RA = 131
84810 deg
ZDOT = 3529
465207 TA = 308
63919
MA = 308
76055
Ha = 224
572 n
mi
Hp = 215
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16973217
72 X = -5201833
73
Y = 2278879
81 feet Y = 636591
31 meter
Z = 14193606
66 Z = 4301011
77
XDOT = 6863
088055 XDOT = 2147
048570
YDOT = -21265
037640 feet/sec YDOT = -6457
881791 meter/sec
ZDOT = 11579
610259 ZDOT = 3539
761445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2810503
08 X = -856641
34
Y = -16988492
77 feet Y = -5178092
60 meter
Z = 14079562
09 Z = 4291450
52
XDOT = 20226
537599 XDOT = 6165
048660
YDOT = 6324
556709 feet/sec YDOT = 1927
724885 meter/sec
ZDOT = 11626
690626 ZDOT = 3543
815303
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
34640922
00016717 00000-0 10270-3 0 9125
2 25544 51
6384 132
6415 0003758 100
0199 260
1377 15
52809154 39899
Satellite: ISS
Catalog Number: 25544
Epoch time: 19069
34640922 = yrday
fracday
Element set: 912
Inclination: 51
6384 deg
RA of node: 132
6415 deg
Eccentricity:
0003758
Arg of perigee: 100
0199 deg
Mean anomaly: 260
1377 deg
Mean motion: 15
52809154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 318
Coasting Arc #14 (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 = 4632935
87 A = 6782984
48 meter
Y = 298647
61 meter E =
0015570
Z = -4959389
94 I = 51
92784
XDOT = -2846
178014 Wp = 80
56169
YDOT = 6737
448356 meter/sec RA = 126
88724 deg
ZDOT = -2256
656083 TA = 167
46372
MA = 167
42495
Ha = 224
482 n
mi
Hp = 215
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15199920
84 X = 4653341
89
Y = 979814
99 feet Y = 350569
93 meter
Z = -16270964
37 Z = -4936835
40
XDOT = -9337
854377 XDOT = -2910
344979
YDOT = 22104
489356 feet/sec YDOT = 6705
261394 meter/sec
ZDOT = -7403
727306 ZDOT = -2270
638249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -237489
82 X = -72386
90
Y = 15337874
98 feet Y = 4674984
29 meter
Z = -16168954
89 Z = -4928297
45
XDOT = -21408
731480 XDOT = -6525
381355
YDOT = -8191
284311 feet/sec YDOT = -2496
703458 meter/sec
ZDOT = -7467
519416 ZDOT = -2276
099918
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
31177553
00016717 00000-0 10270-3 0 9130
2 25544 51
6381 127
8394 0003775 102
8826 257
2748 15
52785958 40047
Satellite: ISS
Catalog Number: 25544
Epoch time: 19070
31177553 = yrday
fracday
Element set: 913
Inclination: 51
6381 deg
RA of node: 127
8394 deg
Eccentricity:
0003775
Arg of perigee: 102
8826 deg
Mean anomaly: 257
2748 deg
Mean motion: 15
52785958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 331
Coasting Arc #15 (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 = -4028957
12 A = 6781417
24 meter
Y = -1350157
65 meter E =
0007008
Z = 5279908
78 I = 51
94316
XDOT = 3432
012860 Wp = 113
47035
YDOT = -6804
688450 meter/sec RA = 121
92251 deg
ZDOT = 875
172462 TA = 328
17773
MA = 328
22005
Ha = 224
511 n
mi
Hp = 215
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13218363
26 X = -4039206
66
Y = -4429651
07 feet Y = -1395269
13 meter
Z = 17322535
36 Z = 5260312
86
XDOT = 11259
884712 XDOT = 3503
598644
YDOT = -22325
093339 feet/sec YDOT = -6765
908948 meter/sec
ZDOT = 2871
300728 ZDOT = 892
018307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3545340
97 X = 1080619
93
Y = -13595488
28 feet Y = -4143904
83 meter
Z = 17233990
33 Z = 5252920
25
XDOT = 22022
000342 XDOT = 6712
305704
YDOT = 9495
006794 feet/sec YDOT = 2894
078071 meter/sec
ZDOT = 2948
074597 ZDOT = 898
573137
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
34149522
00016717 00000-0 10270-3 0 9140
2 25544 51
6392 122
7156 0003652 106
3809 253
7745 15
52822537 40204
Satellite: ISS
Catalog Number: 25544
Epoch time: 19071
34149522 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 122
7156 deg
Eccentricity:
0003652
Arg of perigee: 106
3809 deg
Mean anomaly: 253
7745 deg
Mean motion: 15
52822537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 298
Coasting Arc #16 (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 = 3424321
21 A = 6781291
00 meter
Y = 2460711
72 meter E =
0018476
Z = -5326802
25 I = 51
95982
XDOT = -3850
136960 Wp = 97
24546
YDOT = 6589
109649 meter/sec RA = 116
95887 deg
ZDOT = 568
205151 TA = 178
16757
MA = 178
16079
Ha = 224
438 n
mi
Hp = 215
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11234649
64 X = 3422424
92
Y = 8073201
17 feet Y = 2498993
92 meter
Z = -17476385
32 Z = -5310172
99
XDOT = -12631
682938 XDOT = -3926
292119
YDOT = 21617
813810 feet/sec YDOT = 6545
628954 meter/sec
ZDOT = 1864
190128 ZDOT = 549
317275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7105933
51 X = -2165888
54
Y = 11979841
66 feet Y = 3651455
74 meter
Z = -17401352
71 Z = -5303932
31
XDOT = -21715
670934 XDOT = -6618
936501
YDOT = -10295
159824 feet/sec YDOT = -3137
964714 meter/sec
ZDOT = 1778
172486 ZDOT = 541
986974
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
30685715
00016717 00000-0 10270-3 0 9157
2 25544 51
6397 117
9138 0003852 107
8848 252
2724 15
52813204 40354
Satellite: ISS
Catalog Number: 25544
Epoch time: 19072
30685715 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 117
9138 deg
Eccentricity:
0003852
Arg of perigee: 107
8848 deg
Mean anomaly: 252
2724 deg
Mean motion: 15
52813204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 315
Coasting Arc #17 (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 = -2822127
70 A = 6782513
97 meter
Y = -3541217
08 meter E =
0008639
Z = 5042813
10 I = 51
97767
XDOT = 4151
871819 Wp = 77
87575
YDOT = -6138
913299 meter/sec RA = 111
99611 deg
ZDOT = -1982
780423 TA = 31
30226
MA = 31
25085
Ha = 224
592 n
mi
Hp = 215
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9258949
14 X = -2806814
12
Y = -11618166
26 feet Y = -3572690
20 meter
Z = 16544662
40 Z = 5029141
71
XDOT = 13621
626704 XDOT = 4229
841510
YDOT = -20140
791662 feet/sec YDOT = -6092
048312 meter/sec
ZDOT = -6505
185115 ZDOT = -1962
422599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10623940
13 X = 3238176
95
Y = -10482121
18 feet Y = -3194950
53 meter
Z = 16483106
87 Z = 5024050
98
XDOT = 20640
108371 XDOT = 6291
105031
YDOT = 10811
723708 feet/sec YDOT = 3295
413386 meter/sec
ZDOT = -6412
532096 ZDOT = -1954
539783
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
33657476
00016717 00000-0 10270-3 0 9165
2 25544 51
6395 112
7905 0003892 111
0323 249
1245 15
52788789 40516
Satellite: ISS
Catalog Number: 25544
Epoch time: 19073
33657476 = yrday
fracday
Element set: 916
Inclination: 51
6395 deg
RA of node: 112
7905 deg
Eccentricity:
0003892
Arg of perigee: 111
0323 deg
Mean anomaly: 249
1245 deg
Mean motion: 15
52788789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 325
Coasting Arc #18 (Orbit 4058)
---------------------------------------
Vector Time (GMT): 2019/073/19:14:11
000
Vector Time (MET): N/A
Weight (LBS) : 910513
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4238704
53 A = 6781418
20 meter
Y = -384227
92 meter E =
0006976
Z = 5274443
59 I = 51
97984
XDOT = 1839
631220 Wp = 114
35839
YDOT = -7388
225616 meter/sec RA = 109
50000 deg
ZDOT = 936
400592 TA = 326
70588
MA = 326
74974
Ha = 224
453 n
mi
Hp = 215
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13906510
92 X = -4259713
10
Y = -1260590
29 feet Y = -431745
30 meter
Z = 17304604
97 Z = 5253802
69
XDOT = 6035
535498 XDOT = 1917
563243
YDOT = -24239
585353 feet/sec YDOT = -7367
217785 meter/sec
ZDOT = 3072
180419 ZDOT = 945
526395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1139811
63 X = 347414
59
Y = 14032239
38 feet Y = 4277026
56 meter
Z = 17211233
96 Z = 5245984
11
XDOT = -23885
461651 XDOT = -7280
288711
YDOT = -1894
724375 feet/sec YDOT = -577
511989 meter/sec
ZDOT = 3114
126923 ZDOT = 949
185886
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
85143134
00016717 00000-0 10270-3 0 9174
2 25544 51
6388 110
2335 0003523 107
1229 253
0309 15
52832948 40590
Satellite: ISS
Catalog Number: 25544
Epoch time: 19073
85143134 = yrday
fracday
Element set: 917
Inclination: 51
6388 deg
RA of node: 110
2335 deg
Eccentricity:
0003523
Arg of perigee: 107
1229 deg
Mean anomaly: 253
0309 deg
Mean motion: 15
52832948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4059
Checksum: 298
Coasting Arc #19 (Orbit 4062)
---------------------------------------
Vector Time (GMT): 2019/074/01:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 925785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2877278
61 A = 6792739
70 meter
Y = 6053183
17 meter E =
0015961
Z = 1066367
81 I = 52
01855
XDOT = -3906
420853 Wp = 66
58768
YDOT = -2911
099652 meter/sec RA = 108
28730 deg
ZDOT = 5920
580171 TA = 304
91131
MA = 305
06119
Ha = 224
349 n
mi
Hp = 215
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9439890
45 X = -2949932
96
Y = 19859524
83 feet Y = 6020601
24 meter
Z = 3498582
07 Z = 1052214
45
XDOT = -12816
341382 XDOT = -3902
336451
YDOT = -9550
851877 feet/sec YDOT = -2954
760876 meter/sec
ZDOT = 19424
475628 ZDOT = 5901
614442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6525724
84 X = 1989040
93
Y = -21008924
54 feet Y = -6403520
20 meter
Z = 3433997
63 Z = 1046682
48
XDOT = 12646
654328 XDOT = 3854
700239
YDOT = 7124
150773 feet/sec YDOT = 2171
441156 meter/sec
ZDOT = 19338
906913 ZDOT = 5894
498827
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 19074
10885969
00016717 00000-0 10270-3 0 9183
2 25544 51
6374 108
9510 0003509 109
1972 250
9560 15
52797937 40633
Satellite: ISS
Catalog Number: 25544
Epoch time: 19074
10885969 = yrday
fracday
Element set: 918
Inclination: 51
6374 deg
RA of node: 108
9510 deg
Eccentricity:
0003509
Arg of perigee: 109
1972 deg
Mean anomaly: 250
9560 deg
Mean motion: 15
52797937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4063
Checksum: 340
Coasting Arc #20 (Orbit 4077)
---------------------------------------
Vector Time (GMT): 2019/075/01:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 925785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3165093
46 A = 6790955
79 meter
Y = -5547226
36 meter E =
0009201
Z = -2304597
60 I = 52
02219
XDOT = 3382
357260 Wp = 126
57934
YDOT = 4187
188733 meter/sec RA = 103
34630 deg
ZDOT = -5453
784320 TA = 78
92655
MA = 78
82309
Ha = 224
344 n
mi
Hp = 215
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10384164
90 X = 3238083
21
Y = -18199561
54 feet Y = -5511424
06 meter
Z = -7561015
76 Z = -2289045
42
XDOT = 11096
972638 XDOT = 3361
774696
YDOT = 13737
495842 feet/sec YDOT = 4224
897287 meter/sec
ZDOT = -17892
993176 ZDOT = -5437
404467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7387874
41 X = -2251824
12
Y = 19635201
91 feet Y = 5984809
54 meter
Z = -7490129
38 Z = -2282991
43
XDOT = -11838
099471 XDOT = -3608
252719
YDOT = -11225
818551 feet/sec YDOT = -3421
629494 meter/sec
ZDOT = -17819
240674 ZDOT = -5431
304557
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 19075
07421640
00016717 00000-0 10270-3 0 9193
2 25544 51
6375 104
1475 0003513 110
7330 249
4198 15
52809413 40782
Satellite: ISS
Catalog Number: 25544
Epoch time: 19075
07421640 = yrday
fracday
Element set: 919
Inclination: 51
6375 deg
RA of node: 104
1475 deg
Eccentricity:
0003513
Arg of perigee: 110
7330 deg
Mean anomaly: 249
4198 deg
Mean motion: 15
52809413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4078
Checksum: 299
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