[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 10th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14601 2445 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
284/20:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 219
1
289/20:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 219
5
292/20:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
8
000/00:00:00
000 0
0 0
0 220
1
Coasting Arc #1 (Orbit 3299)
---------------------------------------
Vector Time (GMT): 2019/282/13:49:43
769
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1191367
38 A = 6789026
52 meter
Y = -4071150
91 meter E =
0008628
Z = 5293472
77 I = 51
79410
XDOT = 7031
853110 Wp = 112
81599
YDOT = -2976
620251 meter/sec RA = 152
86569 deg
ZDOT = -709
017732 TA = 343
92733
MA = 343
95469
Ha = 229
606 n
mi
Hp = 218
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3908685
62 X = -1171466
92
Y = -13356794
33 feet Y = -4084361
95 meter
Z = 17367036
64 Z = 5287734
17
XDOT = 23070
384218 XDOT = 7068
059950
YDOT = -9765
814472 feet/sec YDOT = -2897
782715 meter/sec
ZDOT = -2326
173660 ZDOT = -674
771297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12224767
61 X = 3726109
17
Y = 6718482
47 feet Y = 2047793
46 meter
Z = 17341072
34 Z = 5285558
85
XDOT = -9157
588009 XDOT = -2791
232825
YDOT = 22243
848884 feet/sec YDOT = 6779
925140 meter/sec
ZDOT = -2169
944839 ZDOT = -661
399187
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 19282
62344783
00016717 00000-0 10270-3 0 9006
2 25544 51
6412 153
8040 0006996 131
1061 229
0694 15
50173013 33009
Satellite: ISS
Catalog Number: 25544
Epoch time: 19282
62344783 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 153
8040 deg
Eccentricity:
0006996
Arg of perigee: 131
1061 deg
Mean anomaly: 229
0694 deg
Mean motion: 15
50173013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3300
Checksum: 279
Coasting Arc #2 (Orbit 3314)
---------------------------------------
Vector Time (GMT): 2019/283/13:49:43
769
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1078200
86 A = 6789267
49 meter
Y = 4193393
20 meter E =
0020270
Z = -5247041
49 I = 51
82236
XDOT = -6841
653519 Wp = 110
85634
YDOT = 3213
303168 meter/sec RA = 147
91874 deg
ZDOT = 1158
771846 TA = 170
27759
MA = 170
23830
Ha = 229
465 n
mi
Hp = 218
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3537404
40 X = 1056716
39
Y = 13757851
71 feet Y = 4205329
81 meter
Z = -17214703
06 Z = -5241856
51
XDOT = -22446
369813 XDOT = -6882
705833
YDOT = 10542
333228 feet/sec YDOT = 3136
565533 meter/sec
ZDOT = 3801
744902 ZDOT = 1125
437423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12362870
73 X = -3768203
00
Y = -7053895
75 feet Y = -2150027
43 meter
Z = -17191268
05 Z = -5239898
50
XDOT = 7749
588197 XDOT = 2362
074483
YDOT = -22504
051387 feet/sec YDOT = -6859
234863 meter/sec
ZDOT = 3649
644405 ZDOT = 1112
411615
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 19283
59043526
00016717 00000-0 10270-3 0 9015
2 25544 51
6393 149
0116 0007020 135
0824 225
0895 15
50189877 33157
Satellite: ISS
Catalog Number: 25544
Epoch time: 19283
59043526 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 149
0116 deg
Eccentricity:
0007020
Arg of perigee: 135
0824 deg
Mean anomaly: 225
0895 deg
Mean motion: 15
50189877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3315
Checksum: 306
Coasting Arc #3 (Orbit 3330)
---------------------------------------
Vector Time (GMT): 2019/284/13:49:43
769
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -991692
77 A = 6789679
20 meter
Y = -4311447
95 meter E =
0008831
Z = 5142601
70 I = 51
85181
XDOT = 6660
764746 Wp = 106
93062
YDOT = -3445
414301 meter/sec RA = 142
97498 deg
ZDOT = -1604
343011 TA = 358
49573
MA = 358
49839
Ha = 229
465 n
mi
Hp = 219
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3253585
19 X = -968387
38
Y = -14145170
43 feet Y = -4322406
95 meter
Z = 16872052
82 Z = 5137841
40
XDOT = 21852
902709 XDOT = 6706
590418
YDOT = -11303
852695 feet/sec YDOT = -3370
672855 meter/sec
ZDOT = -5263
592555 ZDOT = -1571
875527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12565603
78 X = 3829996
03
Y = 7314506
75 feet Y = 2229461
66 meter
Z = 16850561
48 Z = 5136051
14
XDOT = -6372
754404 XDOT = -1942
415542
YDOT = 22730
469799 feet/sec YDOT = 6928
247195 meter/sec
ZDOT = -5115
416330 ZDOT = -1559
178897
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 19284
62188660
00016717 00000-0 10270-3 0 9020
2 25544 51
6398 143
9005 0006949 139
7006 220
4661 15
50175624 33317
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
62188660 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 143
9005 deg
Eccentricity:
0006949
Arg of perigee: 139
7006 deg
Mean anomaly: 220
4661 deg
Mean motion: 15
50175624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3331
Checksum: 311
Coasting Arc #4 (Orbit 3334)
---------------------------------------
Vector Time (GMT): 2019/284/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5077494
47 A = 6792459
52 meter
Y = 480320
33 meter E =
0013350
Z = -4496022
39 I = 51
87088
XDOT = -3449
239339 Wp = 101
34940
YDOT = 6001
097183 meter/sec RA = 141
61984 deg
ZDOT = -3264
989876 TA = 135
86044
MA = 135
75383
Ha = 229
521 n
mi
Hp = 219
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16658446
41 X = 5093585
46
Y = 1575854
11 feet Y = 537189
99 meter
Z = -14750729
62 Z = -4471318
49
XDOT = -11316
402031 XDOT = -3500
229292
YDOT = 19688
639051 feet/sec YDOT = 5962
239931 meter/sec
ZDOT = -10711
909043 ZDOT = -3281
869622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13376588
58 X = 4077184
20
Y = 10215826
31 feet Y = 3113783
86 meter
Z = -14638133
36 Z = -4461703
05
XDOT = -19223
474476 XDOT = -5859
315020
YDOT = 9762
564287 feet/sec YDOT = 2975
629595 meter/sec
ZDOT = -10789
153526 ZDOT = -3288
533995
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 19284
87974932
00016717 00000-0 10270-3 0 9033
2 25544 51
6423 142
6217 0007283 142
7293 217
4364 15
50175322 33356
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
87974932 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 142
6217 deg
Eccentricity:
0007283
Arg of perigee: 142
7293 deg
Mean anomaly: 217
4364 deg
Mean motion: 15
50175322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3335
Checksum: 313
Coasting Arc #5 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2019/285/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4892186
56 A = 6791562
60 meter
Y = -437019
97 meter E =
0014902
Z = 4685087
30 I = 51
89413
XDOT = 3340
966191 Wp = 129
68716
YDOT = -6264
778988 meter/sec RA = 136
67979 deg
ZDOT = 2888
901206 TA = 291
61557
MA = 291
77426
Ha = 229
448 n
mi
Hp = 219
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16050480
83 X = -4909694
00
Y = -1433792
56 feet Y = -491825
29 meter
Z = 15371021
34 Z = 4661280
03
XDOT = 10961
175166 XDOT = 3396
739550
YDOT = -20553
736836 feet/sec YDOT = -6227
105814 meter/sec
ZDOT = 9478
022330 ZDOT = 2905
266708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13106100
26 X = -3994739
36
Y = -9551342
19 feet Y = -2911249
10 meter
Z = 15262502
78 Z = 4652010
85
XDOT = 19232
746071 XDOT = 5862
141002
YDOT = -11044
407283 feet/sec YDOT = -3366
335340 meter/sec
ZDOT = 9552
950371 ZDOT = 2911
739273
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 19285
91119447
00016717 00000-0 10270-3 0 9042
2 25544 51
6426 137
5104 0007211 145
5277 214
6343 15
50223472 33515
Satellite: ISS
Catalog Number: 25544
Epoch time: 19285
91119447 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 137
5104 deg
Eccentricity:
0007211
Arg of perigee: 145
5277 deg
Mean anomaly: 214
6343 deg
Mean motion: 15
50223472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 291
Coasting Arc #6 (Orbit 3365)
---------------------------------------
Vector Time (GMT): 2019/286/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4703991
15 A = 6790918
95 meter
Y = 479664
13 meter E =
0015037
Z = -4886050
15 I = 51
91356
XDOT = -3209
832339 Wp = 100
26649
YDOT = 6495
225938 meter/sec RA = 131
74095 deg
ZDOT = -2461
637740 TA = 145
65696
MA = 145
55966
Ha = 229
367 n
mi
Hp = 219
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15433041
83 X = 4722012
00
Y = 1573701
21 feet Y = 532367
80 meter
Z = -16030348
26 Z = -4863155
73
XDOT = -10530
945995 XDOT = -3270
267763
YDOT = 21309
796384 feet/sec YDOT = 6458
993187 meter/sec
ZDOT = -8076
239304 ZDOT = -2477
377598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12667761
85 X = 3861133
81
Y = 9138825
17 feet Y = 2785513
91 meter
Z = -15925987
10 Z = -4854240
87
XDOT = -19067
573479 XDOT = -5811
796396
YDOT = 12282
619199 feet/sec YDOT = 3743
742332 meter/sec
ZDOT = -8148
343991 ZDOT = -2483
615249
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 19286
87817483
00016717 00000-0 10270-3 0 9054
2 25544 51
6411 132
7190 0007177 148
9094 211
2483 15
50177605 33666
Satellite: ISS
Catalog Number: 25544
Epoch time: 19286
87817483 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 132
7190 deg
Eccentricity:
0007177
Arg of perigee: 148
9094 deg
Mean anomaly: 211
2483 deg
Mean motion: 15
50177605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3366
Checksum: 324
Coasting Arc #7 (Orbit 3381)
---------------------------------------
Vector Time (GMT): 2019/287/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4536401
04 A = 6790175
32 meter
Y = -503603
45 meter E =
0012815
Z = 5023141
48 I = 51
93295
XDOT = 3032
470860 Wp = 139
31724
YDOT = -6734
492422 meter/sec RA = 126
80312 deg
ZDOT = 2051
041696 TA = 290
74513
MA = 290
88241
Ha = 229
311 n
mi
Hp = 219
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14883205
53 X = -4554832
66
Y = -1652242
30 feet Y = -554435
36 meter
Z = 16480122
98 Z = 5001060
10
XDOT = 9949
051379 XDOT = 3097
589468
YDOT = -22094
791411 feet/sec YDOT = -6700
216931 meter/sec
ZDOT = 6729
139421 ZDOT = 2065
931339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12306939
73 X = -3751155
23
Y = -8722760
86 feet Y = -2658697
51 meter
Z = 16379464
04 Z = 4992460
64
XDOT = 18748
186402 XDOT = 5714
447215
YDOT = -13610
856476 feet/sec YDOT = -4148
589054 meter/sec
ZDOT = 6797
400172 ZDOT = 2071
847572
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 19287
90961611
00016717 00000-0 10270-3 0 9063
2 25544 51
6411 127
6077 0007158 152
6872 207
4656 15
50222180 33824
Satellite: ISS
Catalog Number: 25544
Epoch time: 19287
90961611 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 127
6077 deg
Eccentricity:
0007158
Arg of perigee: 152
6872 deg
Mean anomaly: 207
4656 deg
Mean motion: 15
50222180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 311
Coasting Arc #8 (Orbit 3396)
---------------------------------------
Vector Time (GMT): 2019/288/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4381429
90 A = 6789728
85 meter
Y = 607737
91 meter E =
0016479
Z = -5164106
10 I = 51
94971
XDOT = -2833
269936 Wp = 102
95520
YDOT = 6925
269876 meter/sec RA = 121
86545 deg
ZDOT = -1596
733106 TA = 151
72121
MA = 151
63165
Ha = 229
184 n
mi
Hp = 219
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14374770
00 X = 4399393
37
Y = 1993890
78 feet Y = 656834
29 meter
Z = -16942605
32 Z = -5142778
61
XDOT = -9295
505038 XDOT = -2902
743491
YDOT = 22720
701694 feet/sec YDOT = 6893
197706 meter/sec
ZDOT = -5238
625676 ZDOT = -1610
665582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11848561
90 X = 3611441
67
Y = 8573570
12 feet Y = 2613224
17 meter
Z = -16845384
07 Z = -5134473
06
XDOT = -18233
224929 XDOT = -5557
486958
YDOT = 14830
664224 feet/sec YDOT = 4520
386456 meter/sec
ZDOT = -5302
554821 ZDOT = -1616
218709
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 19288
87659126
00016717 00000-0 10270-3 0 9076
2 25544 51
6407 122
8155 0007088 155
9989 204
1493 15
50183400 33970
Satellite: ISS
Catalog Number: 25544
Epoch time: 19288
87659126 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 122
8155 deg
Eccentricity:
0007088
Arg of perigee: 155
9989 deg
Mean anomaly: 204
1493 deg
Mean motion: 15
50183400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3397
Checksum: 340
Coasting Arc #9 (Orbit 3411)
---------------------------------------
Vector Time (GMT): 2019/289/20:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1427298
49 A = 6792263
57 meter
Y = 4914820
48 meter E =
0015032
Z = -4481047
02 I = 51
97550
XDOT = -5207
128191 Wp = 130
84494
YDOT = 4525
975051 meter/sec RA = 117
01614 deg
ZDOT = 3303
219581 TA = 172
40979
MA = 172
38701
Ha = 229
018 n
mi
Hp = 219
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4682737
84 X = 1394000
49
Y = 16124739
09 feet Y = 4930595
18 meter
Z = -14701597
83 Z = -4474194
62
XDOT = -17083
753906 XDOT = -5273
397587
YDOT = 14848
999511 feet/sec YDOT = 4467
374862 meter/sec
ZDOT = 10837
334584 ZDOT = 3277
763489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5566162
88 X = -1696566
44
Y = 15870171
11 feet Y = 4837228
15 meter
Z = -14670641
54 Z = -4471611
54
XDOT = -21445
728382 XDOT = -6536
658011
YDOT = 2395
972238 feet/sec YDOT = 730
292338 meter/sec
ZDOT = 10720
972143 ZDOT = 3267
752309
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 19289
84356185
00016717 00000-0 10270-3 0 9084
2 25544 51
6411 118
0234 0007054 157
6876 202
4582 15
50234375 34123
Satellite: ISS
Catalog Number: 25544
Epoch time: 19289
84356185 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 118
0234 deg
Eccentricity:
0007054
Arg of perigee: 157
6876 deg
Mean anomaly: 202
4582 deg
Mean motion: 15
50234375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3412
Checksum: 311
Coasting Arc #10 (Orbit 3427)
---------------------------------------
Vector Time (GMT): 2019/290/20:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1503826
32 A = 6793101
60 meter
Y = -5087214
07 meter E =
0012440
Z = 4230458
90 I = 51
99284
XDOT = 4956
330269 Wp = 108
23299
YDOT = -4540
209640 meter/sec RA = 112
08311 deg
ZDOT = -3692
747805 TA = 19
46014
MA = 19
41269
Ha = 228
930 n
mi
Hp = 219
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4933813
39 X = -1467377
60
Y = -16690334
89 feet Y = -5103827
05 meter
Z = 13879458
34 Z = 4223242
31
XDOT = 16260
926080 XDOT = 5024
669626
YDOT = -14895
700920 feet/sec YDOT = -4484
402417 meter/sec
ZDOT = -12115
314320 ZDOT = -3668
505114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5414192
14 X = 1650245
77
Y = -16568043
46 feet Y = -5049939
65 meter
Z = 13846863
05 Z = 4220523
86
XDOT = 20715
922502 XDOT = 6314
213179
YDOT = -3277
153839 feet/sec YDOT = -998
876490 meter/sec
ZDOT = -12004
462668 ZDOT = -3658
960221
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 19290
87499475
00016717 00000-0 10270-3 0 9090
2 25544 51
6413 112
9121 0006903 162
4515 197
6875 15
50246790 34280
Satellite: ISS
Catalog Number: 25544
Epoch time: 19290
87499475 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 112
9121 deg
Eccentricity:
0006903
Arg of perigee: 162
4515 deg
Mean anomaly: 197
6875 deg
Mean motion: 15
50246790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3428
Checksum: 334
Coasting Arc #11 (Orbit 3442)
---------------------------------------
Vector Time (GMT): 2019/291/20:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1625209
31 A = 6794021
46 meter
Y = 5272403
68 meter E =
0012069
Z = -3978733
98 I = 52
00670
XDOT = -4690
041614 Wp = 136
56965
YDOT = 4495
454744 meter/sec RA = 107
15171 deg
ZDOT = 4040
137143 TA = 175
51075
MA = 175
49991
Ha = 228
854 n
mi
Hp = 219
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5332051
53 X = 1585457
90
Y = 17297912
35 feet Y = 5290355
65 meter
Z = -13053589
19 Z = -3970935
70
XDOT = -15387
275635 XDOT = -4759
587716
YDOT = 14748
867270 feet/sec YDOT = 4442
618539 meter/sec
ZDOT = 13255
043119 ZDOT = 4017
185223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5141064
40 X = -1566996
43
Y = 17382071
11 feet Y = 5298055
27 meter
Z = -13018363
82 Z = -3967997
29
XDOT = -19802
983515 XDOT = -6035
949375
YDOT = 3994
738503 feet/sec YDOT = 1217
596296 meter/sec
ZDOT = 13150
059835 ZDOT = 4008
138238
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 19291
84196332
00016717 00000-0 10270-3 0 9106
2 25544 51
6407 108
1206 0007050 164
5208 195
6159 15
50242845 34437
Satellite: ISS
Catalog Number: 25544
Epoch time: 19291
84196332 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 108
1206 deg
Eccentricity:
0007050
Arg of perigee: 164
5208 deg
Mean anomaly: 195
6159 deg
Mean motion: 15
50242845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 297
Coasting Arc #12 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2019/292/20:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1762217
13 A = 6794931
44 meter
Y = -5424543
75 meter E =
0014250
Z = 3676774
97 I = 52
01969
XDOT = 4464
897302 Wp = 113
87036
YDOT = -4430
017426 meter/sec RA = 102
22113 deg
ZDOT = -4388
116582 TA = 22
70560
MA = 22
64263
Ha = 228
721 n
mi
Hp = 219
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5781552
27 X = -1719287
42
Y = -17797059
56 feet Y = -5444010
10 meter
Z = 12062909
99 Z = 3668318
84
XDOT = 14648
613197 XDOT = 4535
418647
YDOT = -14534
177907 feet/sec YDOT = -4379
693449 meter/sec
ZDOT = -14396
707946 ZDOT = -4366
256113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4740545
25 X = 1444918
19
Y = -18127580
90 feet Y = -5525286
66 meter
Z = 12024704
35 Z = 3665129
89
XDOT = 18952
908558 XDOT = 5776
846528
YDOT = -4544
127204 feet/sec YDOT = -1385
049972 meter/sec
ZDOT = -14296
687418 ZDOT = -4357
630325
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 19292
87339040
00016717 00000-0 10270-3 0 9116
2 25544 51
6417 103
0090 0006798 169
4200 190
7095 15
50255698 34599
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
87339040 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 103
0090 deg
Eccentricity:
0006798
Arg of perigee: 169
4200 deg
Mean anomaly: 190
7095 deg
Mean motion: 15
50255698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 319
Coasting Arc #13 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2019/292/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4031470
38 A = 6788839
49 meter
Y = 1150078
00 meter E =
0017718
Z = -5353950
43 I = 51
99910
XDOT = -1790
473488 Wp = 113
99433
YDOT = 7433
480981 meter/sec RA = 102
12443 deg
ZDOT = 242
209239 TA = 158
34595
MA = 158
27093
Ha = 228
794 n
mi
Hp = 220
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13226608
84 X = 4044317
26
Y = 3773221
77 feet Y = 1195232
62 meter
Z = -17565454
18 Z = -5334335
47
XDOT = -5874
256849 XDOT = -1874
640296
YDOT = 24388
060962 feet/sec YDOT = 7412
988035 meter/sec
ZDOT = 794
649735 ZDOT = 233
307254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10638950
28 X = 3242752
05
Y = 8895267
32 feet Y = 2711277
48 meter
Z = -17476055
64 Z = -5326701
76
XDOT = -14681
995271 XDOT = -4475
072159
YDOT = 19081
669673 feet/sec YDOT = 5816
092916 meter/sec
ZDOT = 753
536937 ZDOT = 229
678058
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 19292
87339200
00016717 00000-0 10270-3 0 9125
2 25544 51
6419 103
0089 0006852 168
3121 191
8190 15
50200288 34593
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
87339200 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 103
0089 deg
Eccentricity:
0006852
Arg of perigee: 168
3121 deg
Mean anomaly: 191
8190 deg
Mean motion: 15
50200288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 302
Coasting Arc #14 (Orbit 3474)
---------------------------------------
Vector Time (GMT): 2019/293/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4017795
68 A = 6788840
57 meter
Y = -1301097
79 meter E =
0006544
Z = 5311546
18 I = 52
00513
XDOT = 1498
989014 Wp = 144
77248
YDOT = -7484
810803 meter/sec RA = 97
19157 deg
ZDOT = -704
346601 TA = 311
89499
MA = 311
95080
Ha = 228
768 n
mi
Hp = 219
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13181744
35 X = -4028748
74
Y = -4268693
55 feet Y = -1346088
90 meter
Z = 17426332
62 Z = 5292002
33
XDOT = 4917
942958 XDOT = 1585
996307
YDOT = -24556
465888 feet/sec YDOT = -7467
561556 meter/sec
ZDOT = -2310
848428 ZDOT = -696
853696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10553642
43 X = -3216750
21
Y = -9148611
36 feet Y = -2788496
74 meter
Z = 17337264
46 Z = 5284398
21
XDOT = 13515
847492 XDOT = 4119
630316
YDOT = -19875
236708 feet/sec YDOT = -6057
972149 meter/sec
ZDOT = -2276
140364 ZDOT = -693
767583
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 19293
90481624
00016717 00000-0 10270-3 0 9139
2 25544 51
6416 97
8982 0006784 171
1867 188
9404 15
50242272 34757
Satellite: ISS
Catalog Number: 25544
Epoch time: 19293
90481624 = yrday
fracday
Element set: 913
Inclination: 51
6416 deg
RA of node: 97
8982 deg
Eccentricity:
0006784
Arg of perigee: 171
1867 deg
Mean anomaly: 188
9404 deg
Mean motion: 15
50242272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 340
Coasting Arc #15 (Orbit 3489)
---------------------------------------
Vector Time (GMT): 2019/294/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4049645
36 A = 6789247
55 meter
Y = 1488101
04 meter E =
0017053
Z = -5256171
19 I = 52
00976
XDOT = -1211
356440 Wp = 121
56393
YDOT = 7461
828599 meter/sec RA = 92
25794 deg
ZDOT = 1173
392700 TA = 159
69262
MA = 159
62471
Ha = 228
572 n
mi
Hp = 220
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13286238
05 X = 4058235
86
Y = 4882221
25 feet Y = 1533435
05 meter
Z = -17244656
13 Z = -5236478
44
XDOT = -3974
266534 XDOT = -1300
406498
YDOT = 24481
064957 feet/sec YDOT = 7447
784449 meter/sec
ZDOT = 3849
713582 ZDOT = 1167
292009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10573839
57 X = 3222906
30
Y = 9572933
34 feet Y = 2917830
08 meter
Z = -17154918
69 Z = -5228819
22
XDOT = -12234
868630 XDOT = -3729
187958
YDOT = 20396
704092 feet/sec YDOT = 6216
915407 meter/sec
ZDOT = 3821
342124 ZDOT = 1164
745079
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 19294
87177608
00016717 00000-0 10270-3 0 9141
2 25544 51
6421 93
1062 0006747 175
1642 184
9575 15
50209303 34905
Satellite: ISS
Catalog Number: 25544
Epoch time: 19294
87177608 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 93
1062 deg
Eccentricity:
0006747
Arg of perigee: 175
1642 deg
Mean anomaly: 184
9575 deg
Mean motion: 15
50209303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3490
Checksum: 320
Coasting Arc #16 (Orbit 3505)
---------------------------------------
Vector Time (GMT): 2019/295/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4103221
69 A = 6789523
92 meter
Y = -1639951
71 meter E =
0005808
Z = 5150111
79 I = 52
01028
XDOT = 927
543504 Wp = 131
65450
YDOT = -7433
079339 meter/sec RA = 87
32523 deg
ZDOT = -1630
492420 TA = 333
98727
MA = 334
01644
Ha = 228
563 n
mi
Hp = 220
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13462013
41 X = -4109594
94
Y = -5380418
99 feet Y = -1685872
36 meter
Z = 16896692
22 Z = 5130164
24
XDOT = 3043
121733 XDOT = 1018
513522
YDOT = -24386
743237 feet/sec YDOT = -7422
198281 meter/sec
ZDOT = -5349
384581 ZDOT = -1625
765611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10718848
82 X = -3267105
12
Y = -9916865
94 feet Y = -3022660
74 meter
Z = 16805801
72 Z = 5122408
36
XDOT = 10950
832596 XDOT = 3337
813775
YDOT = -20850
014907 feet/sec YDOT = -6355
084544 meter/sec
ZDOT = -5327
269669 ZDOT = -1623
751795
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 19295
90319577
00016717 00000-0 10270-3 0 9150
2 25544 51
6411 87
9950 0006724 177
9760 182
1419 15
50252221 35069
Satellite: ISS
Catalog Number: 25544
Epoch time: 19295
90319577 = yrday
fracday
Element set: 915
Inclination: 51
6411 deg
RA of node: 87
9950 deg
Eccentricity:
0006724
Arg of perigee: 177
9760 deg
Mean anomaly: 182
1419 deg
Mean motion: 15
50252221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3506
Checksum: 323
Coasting Arc #17 (Orbit 3520)
---------------------------------------
Vector Time (GMT): 2019/296/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4203990
43 A = 6790191
54 meter
Y = 1811347
52 meter E =
0015442
Z = -5028555
02 I = 52
01111
XDOT = -661
558153 Wp = 129
88591
YDOT = 7331
923866 meter/sec RA = 82
39196 deg
ZDOT = 2082
590720 TA = 160
34948
MA = 160
28991
Ha = 228
298 n
mi
Hp = 220
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13792619
52 X = 4207849
15
Y = 5942741
20 feet Y = 1858380
87 meter
Z = -16497883
92 Z = -5008124
11
XDOT = -2170
466381 XDOT = -753
612858
YDOT = 24054
868328 feet/sec YDOT = 7324
011234 meter/sec
ZDOT = 6832
646719 ZDOT = 2079
153188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11001716
13 X = 3353323
08
Y = 10371954
04 feet Y = 3161371
59 meter
Z = -16404801
49 Z = -5000183
49
XDOT = -9619
698981 XDOT = -2932
084249
YDOT = 21013
038630 feet/sec YDOT = 6404
774174 meter/sec
ZDOT = 6816
409570 ZDOT = 2077
641637
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 19296
87014862
00016717 00000-0 10270-3 0 9167
2 25544 51
6427 83
2027 0006590 182
6829 177
4287 15
50222112 35213
Satellite: ISS
Catalog Number: 25544
Epoch time: 19296
87014862 = yrday
fracday
Element set: 916
Inclination: 51
6427 deg
RA of node: 83
2027 deg
Eccentricity:
0006590
Arg of perigee: 182
6829 deg
Mean anomaly: 177
4287 deg
Mean motion: 15
50222112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3521
Checksum: 314
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