[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 15th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14504 3693 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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
201/16:28:21
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 218
5
201/22:50:29
000 0
0 -0
0 0
0
N/A -0
0 0
0 227
4
000/00:00:58
000 0
0 -0
0 218
6
202/23:35:13
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
7
203/20:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 219
0
204/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
9
210/10:44:30
000 0
0 0
0 0
0
N/A 0
0 0
0 226
6
000/00:00:00
000 0
0 0
0 219
9
Coasting Arc #1 (Orbit 1963)
---------------------------------------
Vector Time (GMT): 2019/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2280408
69 A = 6786671
46 meter
Y = 3605233
87 meter E =
0019319
Z = -5294302
02 I = 51
37197
XDOT = -6114
732095 Wp = 104
06656
YDOT = -4570
910827 meter/sec RA = 219
68847 deg
ZDOT = -484
929669 TA = 161
31458
MA = 161
24356
Ha = 228
070 n
mi
Hp = 217
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7481655
81 X = -2294837
55
Y = 11828195
11 feet Y = 3579652
92 meter
Z = -17369757
29 Z = -5305413
70
XDOT = -20061
457004 XDOT = -6060
808918
YDOT = -14996
426597 feet/sec YDOT = -4638
988469 meter/sec
ZDOT = -1590
976604 ZDOT = -514
502100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13731474
38 X = 4185353
39
Y = 2358729
91 feet Y = 718940
88 meter
Z = -17420472
05 Z = -5309759
88
XDOT = -6152
431363 XDOT = -1875
261079
YDOT = 23224
962624 feet/sec YDOT = 7078
968608 meter/sec
ZDOT = -1724
848415 ZDOT = -525
733797
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 19196
51704459
00016717 00000-0 10270-3 0 9008
2 25544 51
6413 220
7240 0006953 143
9130 216
2492 15
50967091 19642
Satellite: ISS
Catalog Number: 25544
Epoch time: 19196
51704459 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 220
7240 deg
Eccentricity:
0006953
Arg of perigee: 143
9130 deg
Mean anomaly: 216
2492 deg
Mean motion: 15
50967091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1964
Checksum: 304
Coasting Arc #2 (Orbit 1979)
---------------------------------------
Vector Time (GMT): 2019/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2649329
91 A = 6786531
58 meter
Y = -3307633
20 meter E =
0008325
Z = 5295025
26 I = 51
39589
XDOT = 6178
610195 Wp = 130
61348
YDOT = 4535
017450 meter/sec RA = 214
70471 deg
ZDOT = -263
589874 TA = 321
87794
MA = 321
93680
Ha = 227
968 n
mi
Hp = 217
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8692027
27 X = 2660400
08
Y = -10851814
95 feet Y = -3277945
45 meter
Z = 17372130
10 Z = 5307920
86
XDOT = 20271
030825 XDOT = 6128
719477
YDOT = 14878
666174 feet/sec YDOT = 4603
832088 meter/sec
ZDOT = -864
796176 ZDOT = -233
697508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13348060
71 X = -4068488
91
Y = -3618892
34 feet Y = -1103038
39 meter
Z = 17430921
48 Z = 5312944
87
XDOT = 5445
568911 XDOT = 1659
809404
YDOT = -23519
647584 feet/sec YDOT = -7168
788584 meter/sec
ZDOT = -729
440438 ZDOT = -222
333446
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 19197
54796818
00016717 00000-0 10270-3 0 9013
2 25544 51
6390 215
6092 0007012 146
2241 213
9357 15
50983447 19805
Satellite: ISS
Catalog Number: 25544
Epoch time: 19197
54796818 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 215
6092 deg
Eccentricity:
0007012
Arg of perigee: 146
2241 deg
Mean anomaly: 213
9357 deg
Mean motion: 15
50983447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1980
Checksum: 322
Coasting Arc #3 (Orbit 1994)
---------------------------------------
Vector Time (GMT): 2019/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3081047
38 A = 6786919
40 meter
Y = 3051073
28 meter E =
0019222
Z = -5237520
47 I = 51
42542
XDOT = -6142
350329 Wp = 114
76522
YDOT = -4443
456255 meter/sec RA = 209
72285 deg
ZDOT = 1019
905824 TA = 165
08272
MA = 165
02594
Ha = 227
928 n
mi
Hp = 218
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10108423
16 X = -3089495
93
Y = 10010082
95 feet Y = 3016572
34 meter
Z = -17183466
11 Z = -5252506
83
XDOT = -20152
068009 XDOT = -6097
159852
YDOT = -14578
268553 feet/sec YDOT = -4511
891792 meter/sec
ZDOT = 3346
147717 ZDOT = 990
178340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13219842
76 X = 4029408
07
Y = 5026622
97 feet Y = 1532114
68 meter
Z = -17251733
42 Z = -5258328
35
XDOT = -4688
285799 XDOT = -1428
989511
YDOT = 23407
357479 feet/sec YDOT = 7134
562560 meter/sec
ZDOT = 3211
504660 ZDOT = 978
866620
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 19198
51445802
00016717 00000-0 10270-3 0 9026
2 25544 51
6394 210
8144 0006877 151
4326 208
7203 15
50961286 19959
Satellite: ISS
Catalog Number: 25544
Epoch time: 19198
51445802 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 210
8144 deg
Eccentricity:
0006877
Arg of perigee: 151
4326 deg
Mean anomaly: 208
7203 deg
Mean motion: 15
50961286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1995
Checksum: 319
Coasting Arc #4 (Orbit 2010)
---------------------------------------
Vector Time (GMT): 2019/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3495190
97 A = 6787467
63 meter
Y = -2838349
83 meter E =
0007943
Z = 5071933
99 I = 51
45661
XDOT = 6073
639785 Wp = 114
04964
YDOT = 4340
639849 meter/sec RA = 204
74278 deg
ZDOT = -1757
381224 TA = 352
98077
MA = 352
99188
Ha = 227
734 n
mi
Hp = 218
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11467161
98 X = 3502034
36
Y = -9312171
36 feet Y = -2799226
50 meter
Z = 16640203
38 Z = 5088928
22
XDOT = 19926
639716 XDOT = 6033
186295
YDOT = 14240
944388 feet/sec YDOT = 4408
333574 meter/sec
ZDOT = -5765
686429 ZDOT = -1727
976139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13250836
42 X = -4038854
94
Y = -6328243
60 feet Y = -1928848
65 meter
Z = 16717576
83 Z = 5095517
42
XDOT = 3956
625929 XDOT = 1205
979583
YDOT = -23155
805807 feet/sec YDOT = -7057
889610 meter/sec
ZDOT = -5632
471840 ZDOT = -1716
777417
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 19199
54537830
00016717 00000-0 10270-3 0 9034
2 25544 51
6389 205
6988 0006848 154
1200 206
0295 15
50990837 20116
Satellite: ISS
Catalog Number: 25544
Epoch time: 19199
54537830 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 205
6988 deg
Eccentricity:
0006848
Arg of perigee: 154
1200 deg
Mean anomaly: 206
0295 deg
Mean motion: 15
50990837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2011
Checksum: 324
Coasting Arc #5 (Orbit 2025)
---------------------------------------
Vector Time (GMT): 2019/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3941495
21 A = 6788554
17 meter
Y = 2682830
93 meter E =
0016941
Z = -4848169
68 I = 51
49047
XDOT = -5897
292697 Wp = 125
60608
YDOT = -4203
367242 meter/sec RA = 199
76661 deg
ZDOT = 2464
842309 TA = 168
72832
MA = 168
69033
Ha = 227
779 n
mi
Hp = 218
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12931414
72 X = -3947653
27
Y = 8801938
76 feet Y = 2638720
43 meter
Z = -15906068
50 Z = -4867330
24
XDOT = -19348
073153 XDOT = -5861
823709
YDOT = -13790
574942 feet/sec YDOT = -4269
116840 meter/sec
ZDOT = 8086
752981 ZDOT = 2436
281828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13546074
77 X = 4128843
59
Y = 7643143
63 feet Y = 2329630
18 meter
Z = -15993274
88 Z = -4874750
18
XDOT = -3288
308481 XDOT = -1002
276425
YDOT = 22502
951048 feet/sec YDOT = 6858
899480 meter/sec
ZDOT = 7957
338351 ZDOT = 2425
396729
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 19200
51186532
00016717 00000-0 10270-3 0 9044
2 25544 51
6387 200
9041 0006749 157
2695 202
8756 15
50960508 20268
Satellite: ISS
Catalog Number: 25544
Epoch time: 19200
51186532 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 200
9041 deg
Eccentricity:
0006749
Arg of perigee: 157
2695 deg
Mean anomaly: 202
8756 deg
Mean motion: 15
50960508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2026
Checksum: 306
Coasting Arc #6 (Orbit 2041)
---------------------------------------
Vector Time (GMT): 2019/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4352254
69 A = 6789671
49 meter
Y = -2568992
18 meter E =
0010482
Z = 4523763
28 I = 51
52520
XDOT = 5680
672572 Wp = 106
70679
YDOT = 4083
721679 meter/sec RA = 194
79338 deg
ZDOT = -3143
113767 TA = 14
87289
MA = 14
84209
Ha = 227
492 n
mi
Hp = 218
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14279050
82 X = 4358684
97
Y = -8428452
02 feet Y = -2520286
63 meter
Z = 14841743
05 Z = 4544919
86
XDOT = 18637
377206 XDOT = 5649
852207
YDOT = 13398
037006 feet/sec YDOT = 4147
074885 meter/sec
ZDOT = -10312
053042 ZDOT = -3115
594281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13960079
83 X = -4255032
33
Y = -8785176
24 feet Y = -2677721
72 meter
Z = 14938014
66 Z = 4553106
87
XDOT = 2767
627971 XDOT = 843
573006
YDOT = -21737
227010 feet/sec YDOT = -6625
506793 meter/sec
ZDOT = -10187
335041 ZDOT = -3105
099720
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 19201
54278369
00016717 00000-0 10270-3 0 9059
2 25544 51
6375 195
7890 0006670 162
0976 198
0411 15
50996024 20421
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
54278369 = yrday
fracday
Element set: 905
Inclination: 51
6375 deg
RA of node: 195
7890 deg
Eccentricity:
0006670
Arg of perigee: 162
0976 deg
Mean anomaly: 198
0411 deg
Mean motion: 15
50996024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2042
Checksum: 324
Coasting Arc #7 (Orbit 2044)
---------------------------------------
Vector Time (GMT): 2019/201/16:28:21
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 166230
39 A = 6786627
26 meter
Y = -4271797
08 meter E =
0009163
Z = 5267778
81 I = 51
52340
XDOT = 7527
242192 Wp = 149
75616
YDOT = 1240
311209 meter/sec RA = 193
89787 deg
ZDOT = 759
945032 TA = 292
92123
MA = 293
01791
Ha = 227
498 n
mi
Hp = 218
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 545375
29 X = 188399
08
Y = -14015082
29 feet Y = -4269814
65 meter
Z = 17282738
88 Z = 5268639
78
XDOT = 24695
676483 XDOT = 7509
121927
YDOT = 4069
262498 feet/sec YDOT = 1324
384739 meter/sec
ZDOT = 2493
257979 ZDOT = 796
464890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 638206
46 X = 194525
33
Y = 14005977
65 feet Y = 4269021
99 meter
Z = 17286940
49 Z = 5269059
46
XDOT = -23895
074727 XDOT = -7283
218777
YDOT = -2226
852799 feet/sec YDOT = -678
744733 meter/sec
ZDOT = 2659
055314 ZDOT = 810
480060
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 19201
73608130
00016717 00000-0 10270-3 0 9064
2 25544 51
6398 194
8310 0006555 163
8985 196
2376 15
51021709 20457
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
73608130 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 194
8310 deg
Eccentricity:
0006555
Arg of perigee: 163
8985 deg
Mean anomaly: 196
2376 deg
Mean motion: 15
51021709 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2045
Checksum: 315
Coasting Arc #8 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2019/201/22:50:58
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4746938
37 A = 6790793
98 meter
Y = -2378479
17 meter E =
0011739
Z = 4221614
57 I = 51
54443
XDOT = 5323
404075 Wp = 108
26618
YDOT = 4148
862344 meter/sec RA = 192
54392 deg
ZDOT = -3643
611334 TA = 19
10260
MA = 19
05861
Ha = 227
380 n
mi
Hp = 218
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15573944
77 X = 4752676
56
Y = -7803409
34 feet Y = -2325363
81 meter
Z = 13850441
51 Z = 4244686
71
XDOT = 17465
236465 XDOT = 5294
312945
YDOT = 13611
753097 feet/sec YDOT = 4208
230008 meter/sec
ZDOT = -11954
105428 ZDOT = -3617
823087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10439584
18 X = 3181985
26
Y = 13839704
92 feet Y = 4218342
06 meter
Z = 13955405
15 Z = 4253607
49
XDOT = -9252
558236 XDOT = -2820
179750
YDOT = 18931
135994 feet/sec YDOT = 5770
210251 meter/sec
ZDOT = -11837
246197 ZDOT = -3607
992641
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 19201
99380974
00016717 00000-0 10270-3 0 9076
2 25544 51
6384 193
5495 0006597 166
0713 194
0621 15
50994736 20493
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
99380974 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 193
5495 deg
Eccentricity:
0006597
Arg of perigee: 166
0713 deg
Mean anomaly: 194
0621 deg
Mean motion: 15
50994736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 343
Coasting Arc #9 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2019/202/22:50:58
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5128808
60 A = 6792280
63 meter
Y = 2353288
75 meter E =
0010926
Z = -3793823
69 I = 51
58194
XDOT = -4962
005121 Wp = 138
24517
YDOT = -4027
412649 meter/sec RA = 187
57552 deg
ZDOT = 4208
915652 TA = 176
34752
MA = 176
33954
Ha = 227
492 n
mi
Hp = 218
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16826799
88 X = -5136314
60
Y = 7720763
62 feet Y = 2295893
09 meter
Z = -12446928
12 Z = -3818755
17
XDOT = -16279
544360 XDOT = -4937
044873
YDOT = -13213
296091 feet/sec YDOT = -4082
761985 meter/sec
ZDOT = 13808
778385 ZDOT = 4184
872868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10841708
71 X = -3304552
81
Y = -14912157
67 feet Y = -4545225
66 meter
Z = -12560346
76 Z = -3828393
69
XDOT = 8672
369489 XDOT = 2643
338220
YDOT = -17846
970888 feet/sec YDOT = -5439
756727 meter/sec
ZDOT = 13699
821829 ZDOT = 4175
705694
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 19202
96029514
00016717 00000-0 10270-3 0 9085
2 25544 51
6381 188
7532 0006744 168
1186 192
0125 15
50993802 20646
Satellite: ISS
Catalog Number: 25544
Epoch time: 19202
96029514 = yrday
fracday
Element set: 908
Inclination: 51
6381 deg
RA of node: 188
7532 deg
Eccentricity:
0006744
Arg of perigee: 168
1186 deg
Mean anomaly: 192
0125 deg
Mean motion: 15
50993802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 315
Coasting Arc #10 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2019/202/23:35:13
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4422459
40 A = 6790651
18 meter
Y = -2849253
43 meter E =
0011278
Z = 4282158
43 I = 51
57714
XDOT = 5765
169614 Wp = 109
78186
YDOT = 3596
634013 meter/sec RA = 187
42373 deg
ZDOT = -3557
044239 TA = 16
53323
MA = 16
49648
Ha = 227
438 n
mi
Hp = 218
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14509381
24 X = 4433191
90
Y = -9347944
31 feet Y = -2799738
65 meter
Z = 14049076
21 Z = 4303666
59
XDOT = 18914
598472 XDOT = 5741
800391
YDOT = 11799
980357 feet/sec YDOT = 3660
973752 meter/sec
ZDOT = -11670
092647 ZDOT = -3529
096212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14127415
67 X = 4306036
29
Y = 9775578
65 feet Y = 2979596
37 meter
Z = 14146976
27 Z = 4311998
37
XDOT = -2974
979793 XDOT = -906
773841
YDOT = 21023
004684 feet/sec YDOT = 6407
811828 meter/sec
ZDOT = -11543
365623 ZDOT = -3518
417842
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 19203
02472781
00016717 00000-0 10270-3 0 9092
2 25544 51
6380 188
4330 0006818 168
7021 191
4284 15
50971056 20651
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
02472781 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 188
4330 deg
Eccentricity:
0006818
Arg of perigee: 168
7021 deg
Mean anomaly: 191
4284 deg
Mean motion: 15
50971056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2065
Checksum: 307
Coasting Arc #11 (Orbit 2078)
---------------------------------------
Vector Time (GMT): 2019/203/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4016572
74 A = 6791237
49 meter
Y = -3532408
20 meter E =
0014096
Z = 4181101
51 I = 51
61049
XDOT = 6176
362213 Wp = 129
18787
YDOT = -2612
331517 meter/sec RA = 183
06417 deg
ZDOT = 3709
174429 TA = 282
59931
MA = 282
75691
Ha = 227
397 n
mi
Hp = 218
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13177732
07 X = -3997082
99
Y = -11589265
74 feet Y = -3577215
60 meter
Z = 13717524
64 Z = 4161637
91
XDOT = 20263
655555 XDOT = 6187
098164
YDOT = -8570
641460 feet/sec YDOT = -2543
203284 meter/sec
ZDOT = 12169
207443 ZDOT = 3739
202381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14932562
21 X = 4551444
96
Y = -9348488
48 feet Y = -2849419
29 meter
Z = 13629326
26 Z = 4154218
64
XDOT = 1681
352073 XDOT = 512
476112
YDOT = 20708
904861 feet/sec YDOT = 6312
074202 meter/sec
ZDOT = 12305
808933 ZDOT = 3750
810563
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 19203
92677798
00016717 00000-0 10270-3 0 9108
2 25544 51
6402 183
9606 0006349 171
5382 188
5877 15
50970384 20796
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
92677798 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 183
9606 deg
Eccentricity:
0006349
Arg of perigee: 171
5382 deg
Mean anomaly: 188
5877 deg
Mean motion: 15
50970384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2079
Checksum: 348
Coasting Arc #12 (Orbit 2087)
---------------------------------------
Vector Time (GMT): 2019/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 67419
38 A = 6786509
62 meter
Y = -4212579
30 meter E =
0007298
Z = 5317513
64 I = 51
61251
XDOT = 7665
916189 Wp = 153
64518
YDOT = 60
897589 meter/sec RA = 180
12760 deg
ZDOT = -55
317566 TA = 296
84498
MA = 296
91958
Ha = 227
370 n
mi
Hp = 218
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 221192
20 X = 88691
43
Y = -13820798
22 feet Y = -4211706
73 meter
Z = 17445910
88 Z = 5317892
56
XDOT = 25150
643665 XDOT = 7664
934170
YDOT = 199
795238 feet/sec YDOT = 146
617760 meter/sec
ZDOT = -181
488077 ZDOT = -18
082249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13375184
20 X = -4076756
15
Y = 3478233
44 feet Y = 1060165
55 meter
Z = 17447909
21 Z = 5318122
73
XDOT = -6066
162770 XDOT = -1848
966412
YDOT = -23369
844641 feet/sec YDOT = -7123
128647 meter/sec
ZDOT = -12
305058 ZDOT = -3
750582
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 19204
50666699
00016717 00000-0 10270-3 0 9112
2 25544 51
6381 181
0839 0006573 172
4480 187
6771 15
50986571 20885
Satellite: ISS
Catalog Number: 25544
Epoch time: 19204
50666699 = yrday
fracday
Element set: 911
Inclination: 51
6381 deg
RA of node: 181
0839 deg
Eccentricity:
0006573
Arg of perigee: 172
4480 deg
Mean anomaly: 187
6771 deg
Mean motion: 15
50986571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2088
Checksum: 341
Coasting Arc #13 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2019/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -578001
37 A = 6786768
70 meter
Y = 4241830
78 meter E =
0016970
Z = -5280069
86 I = 51
64656
XDOT = -7607
403716 Wp = 118
79416
YDOT = -7
635484 meter/sec RA = 175
16080 deg
ZDOT = 820
664792 TA = 159
10156
MA = 159
03211
Ha = 227
271 n
mi
Hp = 219
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1896329
96 X = -599744
37
Y = 13916767
66 feet Y = 4235245
92 meter
Z = -17323063
84 Z = -5282930
10
XDOT = -24958
673609 XDOT = -7610
739237
YDOT = -25
050800 feet/sec YDOT = -92
725517 meter/sec
ZDOT = 2692
469791 ZDOT = 783
703100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13867389
00 X = 4226780
17
Y = -2123175
84 feet Y = -647144
00 meter
Z = -17336339
79 Z = -5284116
37
XDOT = 6702
712256 XDOT = 2042
986696
YDOT = 23005
153155 feet/sec YDOT = 7011
970682 meter/sec
ZDOT = 2524
506609 ZDOT = 769
469614
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 19205
47314920
00016717 00000-0 10270-3 0 9127
2 25544 51
6381 176
2890 0006554 175
8117 184
3090 15
50970714 21039
Satellite: ISS
Catalog Number: 25544
Epoch time: 19205
47314920 = yrday
fracday
Element set: 912
Inclination: 51
6381 deg
RA of node: 176
2890 deg
Eccentricity:
0006554
Arg of perigee: 175
8117 deg
Mean anomaly: 184
3090 deg
Mean motion: 15
50970714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 300
Coasting Arc #14 (Orbit 2118)
---------------------------------------
Vector Time (GMT): 2019/206/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1045815
51 A = 6787238
18 meter
Y = -4302663
18 meter E =
0005399
Z = 5139734
00 I = 51
68183
XDOT = 7505
475165 Wp = 135
01495
YDOT = -41
836302 meter/sec RA = 170
19658 deg
ZDOT = -1564
937701 TA = 330
04895
MA = 330
07983
Ha = 227
107 n
mi
Hp = 219
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3431153
26 X = 1068885
59
Y = -14116349
01 feet Y = -4290839
52 meter
Z = 16862644
34 Z = 5144869
86
XDOT = 24624
262353 XDOT = 7512
986719
YDOT = -137
258210 feet/sec YDOT = 42
137308 meter/sec
ZDOT = -5134
310043 ZDOT = -1528
460910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14468811
29 X = -4410093
68
Y = 948836
21 feet Y = 289205
28 meter
Z = 16886269
74 Z = 5146935
02
XDOT = -7262
979365 XDOT = -2213
756110
YDOT = -22488
224742 feet/sec YDOT = -6854
410901 meter/sec
ZDOT = -4968
526411 ZDOT = -1514
406850
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 19206
50406123
00016717 00000-0 10270-3 0 9130
2 25544 51
6383 171
1740 0006501 180
3542 179
7605 15
50995879 21190
Satellite: ISS
Catalog Number: 25544
Epoch time: 19206
50406123 = yrday
fracday
Element set: 913
Inclination: 51
6383 deg
RA of node: 171
1740 deg
Eccentricity:
0006501
Arg of perigee: 180
3542 deg
Mean anomaly: 179
7605 deg
Mean motion: 15
50995879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2119
Checksum: 304
Coasting Arc #15 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2019/207/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1515914
11 A = 6788210
73 meter
Y = 4425362
97 meter E =
0015014
Z = -4932444
51 I = 51
71794
XDOT = -7301
364263 Wp = 131
25998
YDOT = 55
981722 meter/sec RA = 165
23515 deg
ZDOT = 2289
075116 TA = 161
16931
MA = 161
11372
Ha = 227
006 n
mi
Hp = 219
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4973471
48 X = -1541328
18
Y = 14518907
39 feet Y = 4408269
31 meter
Z = -16182560
73 Z = -4939869
53
XDOT = -23954
607161 XDOT = -7312
566608
YDOT = 183
667068 feet/sec YDOT = -25
730105 meter/sec
ZDOT = 7510
088962 ZDOT = 2253
580816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15310410
00 X = 4666612
97
Y = 149693
81 feet Y = 45626
67 meter
Z = -16216605
68 Z = -4942821
41
XDOT = 7589
669089 XDOT = 2313
331138
YDOT = 21661
097119 feet/sec YDOT = 6602
302402 meter/sec
ZDOT = 7348
747946 ZDOT = 2239
898374
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 19207
47053950
00016717 00000-0 10270-3 0 9144
2 25544 51
6387 166
3787 0006375 183
3466 176
7643 15
50979602 21340
Satellite: ISS
Catalog Number: 25544
Epoch time: 19207
47053950 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 166
3787 deg
Eccentricity:
0006375
Arg of perigee: 183
3466 deg
Mean anomaly: 176
7643 deg
Mean motion: 15
50979602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 338
Coasting Arc #16 (Orbit 2149)
---------------------------------------
Vector Time (GMT): 2019/208/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1928850
25 A = 6789306
56 meter
Y = -4568525
77 meter E =
0007152
Z = 4630043
26 I = 51
75324
XDOT = 7064
997934 Wp = 113
17209
YDOT = -37
759310 meter/sec RA = 160
27749 deg
ZDOT = -2979
588908 TA = 6
48891
MA = 6
47965
Ha = 226
815 n
mi
Hp = 219
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6328248
84 X = 1957303
43
Y = -14988601
62 feet Y = -4546797
43 meter
Z = 15190430
63 Z = 4639481
44
XDOT = 23179
127081 XDOT = 7079
368182
YDOT = -123
882251 feet/sec YDOT = 41
327133 meter/sec
ZDOT = -9775
554161 ZDOT = -2945
235111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16197125
32 X = -4936883
80
Y = -1021394
87 feet Y = -311321
16 meter
Z = 15233646
27 Z = 4643215
38
XDOT = -7740
640260 XDOT = -2359
347151
YDOT = -20763
051498 feet/sec YDOT = -6328
578097 meter/sec
ZDOT = -9619
375660 ZDOT = -2931
985701
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 19208
50144876
00016717 00000-0 10270-3 0 9158
2 25544 51
6381 161
2639 0006332 188
0337 172
0713 15
51002541 21501
Satellite: ISS
Catalog Number: 25544
Epoch time: 19208
50144876 = yrday
fracday
Element set: 915
Inclination: 51
6381 deg
RA of node: 161
2639 deg
Eccentricity:
0006332
Arg of perigee: 188
0337 deg
Mean anomaly: 172
0713 deg
Mean motion: 15
51002541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2150
Checksum: 283
Coasting Arc #17 (Orbit 2164)
---------------------------------------
Vector Time (GMT): 2019/209/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2312583
45 A = 6790753
77 meter
Y = 4759572
92 meter E =
0011147
Z = -4267393
85 I = 51
78932
XDOT = -6745
604762 Wp = 144
83345
YDOT = -32
552649 meter/sec RA = 155
32295 deg
ZDOT = 3615
094454 TA = 162
13923
MA = 162
10003
Ha = 226
746 n
mi
Hp = 219
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7587216
05 X = -2344906
05
Y = 15615396
73 feet Y = 4733531
80 meter
Z = -14000635
98 Z = -4278705
32
XDOT = -22131
249219 XDOT = -6762
299368
YDOT = -106
800030 feet/sec YDOT = -108
080534 meter/sec
ZDOT = 11860
546108 ZDOT = 3582
286567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17233583
73 X = 5252796
32
Y = 1719911
82 feet Y = 524229
12 meter
Z = -14052393
59 Z = -4283169
57
XDOT = 7598
688168 XDOT = 2316
080154
YDOT = 19659
091629 feet/sec YDOT = 5992
091128 meter/sec
ZDOT = 11711
376840 ZDOT = 3569
627661
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 19209
46792562
00016717 00000-0 10270-3 0 9166
2 25544 51
6385 156
4686 0006330 191
8132 168
2872 15
50984672 21658
Satellite: ISS
Catalog Number: 25544
Epoch time: 19209
46792562 = yrday
fracday
Element set: 916
Inclination: 51
6385 deg
RA of node: 156
4686 deg
Eccentricity:
0006330
Arg of perigee: 191
8132 deg
Mean anomaly: 168
2872 deg
Mean motion: 15
50984672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2165
Checksum: 338
Coasting Arc #18 (Orbit 2180)
---------------------------------------
Vector Time (GMT): 2019/210/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3615448
80 A = 6787346
04 meter
Y = -2588318
09 meter E =
0009342
Z = 5128277
00 I = 51
80909
XDOT = 5769
858658 Wp = 165
40825
YDOT = -4764
296268 meter/sec RA = 150
46482 deg
ZDOT = 1653
681638 TA = 268
60216
MA = 268
70918
Ha = 226
633 n
mi
Hp = 219
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11861708
66 X = -3611146
77
Y = -8491857
26 feet Y = -2628725
20 meter
Z = 16825055
77 Z = 5110724
83
XDOT = 18929
982473 XDOT = 5814
673000
YDOT = -15630
893269 feet/sec YDOT = -4699
523304 meter/sec
ZDOT = 5425
464690 ZDOT = 1681
817305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4610073
24 X = -1405150
32
Y = 13936733
32 feet Y = 4247916
32 meter
Z = 16745416
17 Z = 5104002
85
XDOT = -19463
413756 XDOT = -5932
448513
YDOT = -13148
734049 feet/sec YDOT = -4007
734138 meter/sec
ZDOT = 5553
744349 ZDOT = 1692
781278
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 19210
49883102
00016717 00000-0 10270-3 0 9173
2 25544 51
6399 151
3539 0006339 196
8568 163
2373 15
51028583 21811
Satellite: ISS
Catalog Number: 25544
Epoch time: 19210
49883102 = yrday
fracday
Element set: 917
Inclination: 51
6399 deg
RA of node: 151
3539 deg
Eccentricity:
0006339
Arg of perigee: 196
8568 deg
Mean anomaly: 163
2373 deg
Mean motion: 15
51028583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2181
Checksum: 328
Coasting Arc #19 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2019/211/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3180771
24 A = 6786768
86 meter
Y = 2852389
88 meter E =
0012866
Z = -5283191
88 I = 51
83553
XDOT = -5840
900270 Wp = 108
81350
YDOT = 4866
282014 meter/sec RA = 145
51014 deg
ZDOT = -895
063952 TA = 152
66787
MA = 152
60011
Ha = 226
491 n
mi
Hp = 220
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10435601
19 X = 3174300
94
Y = 9358234
51 feet Y = 2887924
00 meter
Z = -17333306
69 Z = -5267756
51
XDOT = -19163
058630 XDOT = -5890
534685
YDOT = 15965
492173 feet/sec YDOT = 4800
687558 meter/sec
ZDOT = -2936
561522 ZDOT = -923
556268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5633625
76 X = 1717129
13
Y = -12929134
14 feet Y = -3940800
08 meter
Z = -17263302
04 Z = -5261854
46
XDOT = 20161
442349 XDOT = 6145
207628
YDOT = 12853
819215 feet/sec YDOT = 3917
844097 meter/sec
ZDOT = -3066
495361 ZDOT = -934
667786
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 19211
46530475
00016717 00000-0 10270-3 0 9184
2 25544 51
6401 146
5579 0006221 199
5754 160
5159 15
50999338 21964
Satellite: ISS
Catalog Number: 25544
Epoch time: 19211
46530475 = yrday
fracday
Element set: 918
Inclination: 51
6401 deg
RA of node: 146
5579 deg
Eccentricity:
0006221
Arg of perigee: 199
5754 deg
Mean anomaly: 160
5159 deg
Mean motion: 15
50999338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 332
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