[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 29th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
121/07:59:48
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
3
124/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 217
4
128/05:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
2
131/09:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
3
Coasting Arc #1 (Orbit 768)
---------------------------------------
Vector Time (GMT): 2019/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2620752
51 A = 6782819
88 meter
Y = -3698289
71 meter E =
0004916
Z = 5044077
66 I = 51
28197
XDOT = 4690
504802 Wp = 138
67176
YDOT = 5790
838209 meter/sec RA = 242
18392 deg
ZDOT = 1804
126076 TA = 293
75036
MA = 293
80192
Ha = 222
800 n
mi
Hp = 217
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8598269
39 X = 2637411
63
Y = -12133496
41 feet Y = -3668889
40 meter
Z = 16548811
23 Z = 5056848
87
XDOT = 15388
795281 XDOT = 4616
637913
YDOT = 18998
813022 feet/sec YDOT = 5842
877728 meter/sec
ZDOT = 5919
048806 ZDOT = 1826
731394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -335102
44 X = -102139
22
Y = -14802520
97 feet Y = -4511808
39 meter
Z = 16606872
19 Z = 5061774
64
XDOT = 22535
280818 XDOT = 6868
753593
YDOT = 6261
531068 feet/sec YDOT = 1908
514670 meter/sec
ZDOT = 6020
776856 ZDOT = 1835
132786
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 19119
55146691
00016717 00000-0 10270-3 0 9005
2 25544 51
6399 242
9409 0001396 246
2119 113
8887 15
52634111 7696
Satellite: ISS
Catalog Number: 25544
Epoch time: 19119
55146691 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 242
9409 deg
Eccentricity:
0001396
Arg of perigee: 246
2119 deg
Mean anomaly: 113
8887 deg
Mean motion: 15
52634111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 769
Checksum: 325
Coasting Arc #2 (Orbit 783)
---------------------------------------
Vector Time (GMT): 2019/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3275074
57 A = 6781833
55 meter
Y = 2733444
51 meter E =
0013566
Z = -5283959
45 I = 51
29600
XDOT = -4446
963627 Wp = 87
61426
YDOT = -6215
230920 meter/sec RA = 237
17716 deg
ZDOT = -459
379437 TA = 177
97881
MA = 177
97332
Ha = 222
950 n
mi
Hp = 217
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10744995
31 X = -3279730
59
Y = 8967993
79 feet Y = 2696794
18 meter
Z = -17335824
98 Z = -5299880
01
XDOT = -14589
775680 XDOT = -4374
901213
YDOT = -20391
177559 feet/sec YDOT = -6264
557065 meter/sec
ZDOT = -1507
150384 ZDOT = -480
806110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3031126
09 X = -923887
23
Y = 13571401
67 feet Y = 4136563
23 meter
Z = -17408044
00 Z = -5305971
81
XDOT = -22959
181114 XDOT = -6997
958404
YDOT = -7182
730862 feet/sec YDOT = -2189
296367 meter/sec
ZDOT = -1603
532563 ZDOT = -488
756725
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 19120
51694566
00016717 00000-0 10270-3 0 9013
2 25544 51
6408 238
1398 0001207 253
2980 106
8040 15
52619378 7844
Satellite: ISS
Catalog Number: 25544
Epoch time: 19120
51694566 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 238
1398 deg
Eccentricity:
0001207
Arg of perigee: 253
2980 deg
Mean anomaly: 106
8040 deg
Mean motion: 15
52619378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 784
Checksum: 311
Coasting Arc #3 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2019/121/07:59:48
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1417518
46 A = 6783806
68 meter
Y = 4553722
20 meter E =
0010721
Z = -4834518
74 I = 51
31491
XDOT = -5768
428052 Wp = 71
21862
YDOT = -4398
106143 meter/sec RA = 233
03013 deg
ZDOT = -2452
402848 TA = 174
56371
MA = 174
55207
Ha = 223
016 n
mi
Hp = 217
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4650651
12 X = -1444850
49
Y = 14940033
45 feet Y = 4537717
58 meter
Z = -15861281
97 Z = -4841471
07
XDOT = -18925
288884 XDOT = -5706
905927
YDOT = -14429
482096 feet/sec YDOT = -4462
268809 meter/sec
ZDOT = -8045
941103 ZDOT = -2480
274456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9803597
73 X = -2988136
59
Y = 12153706
35 feet Y = 3704449
70 meter
Z = -15893090
15 Z = -4844213
88
XDOT = -11215
070948 XDOT = -3418
353625
YDOT = -19727
611758 feet/sec YDOT = -6012
976064 meter/sec
ZDOT = -8171
630957 ZDOT = -2490
713116
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 19121
35369116
00016717 00000-0 10270-3 0 9027
2 25544 51
6375 233
9781 0000952 267
0602 93
0441 15
52619842 7978
Satellite: ISS
Catalog Number: 25544
Epoch time: 19121
35369116 = yrday
fracday
Element set: 902
Inclination: 51
6375 deg
RA of node: 233
9781 deg
Eccentricity:
0000952
Arg of perigee: 267
0602 deg
Mean anomaly: 93
0441 deg
Mean motion: 15
52619842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 309
Coasting Arc #4 (Orbit 812)
---------------------------------------
Vector Time (GMT): 2019/122/07:59:48
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2215588
05 A = 6782332
01 meter
Y = -3753400
31 meter E =
0003196
Z = 5194842
70 I = 51
32976
XDOT = 5718
378575 Wp = 134
06095
YDOT = 4976
022615 meter/sec RA = 228
02595 deg
ZDOT = 1153
796427 TA = 304
81171
MA = 304
84178
Ha = 222
972 n
mi
Hp = 217
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7268989
68 X = 2232160
98
Y = -12314305
48 feet Y = -3728531
30 meter
Z = 17043447
19 Z = 5205645
66
XDOT = 18761
084564 XDOT = 5656
705693
YDOT = 16325
533513 feet/sec YDOT = 5039
624714 meter/sec
ZDOT = 3785
421350 ZDOT = 1181
424659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11089878
78 X = 3380195
05
Y = -8934033
69 feet Y = -2723093
47 meter
Z = 17092602
29 Z = 5209825
18
XDOT = 10994
097359 XDOT = 3351
000875
YDOT = 21144
065585 feet/sec YDOT = 6444
711190 meter/sec
ZDOT = 3909
980370 ZDOT = 1191
762017
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 19122
38353126
00016717 00000-0 10270-3 0 9036
2 25544 51
6367 228
8555 0001019 271
9291 88
1745 15
52579839 8136
Satellite: ISS
Catalog Number: 25544
Epoch time: 19122
38353126 = yrday
fracday
Element set: 903
Inclination: 51
6367 deg
RA of node: 228
8555 deg
Eccentricity:
0001019
Arg of perigee: 271
9291 deg
Mean anomaly: 88
1745 deg
Mean motion: 15
52579839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 813
Checksum: 326
Coasting Arc #5 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2019/123/07:59:48
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3068804
47 A = 6781744
77 meter
Y = 2933539
61 meter E =
0013847
Z = -5300594
85 I = 51
35342
XDOT = -5477
287207 Wp = 91
74112
YDOT = -5344
797888 meter/sec RA = 223
02233 deg
ZDOT = 213
169772 TA = 180
30154
MA = 180
30238
Ha = 222
992 n
mi
Hp = 217
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10068256
13 X = -3075632
28
Y = 9624473
77 feet Y = 2899183
88 meter
Z = -17390403
05 Z = -5315518
80
XDOT = -17970
102386 XDOT = -5418
148549
YDOT = -17535
426141 feet/sec YDOT = -5405
718083 meter/sec
ZDOT = 699
375892 ZDOT = 186
706380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12642748
21 X = -3853509
65
Y = 5639228
99 feet Y = 1718837
00 meter
Z = -17458133
04 Z = -5321238
95
XDOT = -10481
519332 XDOT = -3194
767093
YDOT = -21703
650535 feet/sec YDOT = -6615
272683 meter/sec
ZDOT = 580
098602 ZDOT = 176
814054
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 19123
34900192
00016717 00000-0 10270-3 0 9045
2 25544 51
6388 224
0543 0000998 271
2567 88
8470 15
52626573 8284
Satellite: ISS
Catalog Number: 25544
Epoch time: 19123
34900192 = yrday
fracday
Element set: 904
Inclination: 51
6388 deg
RA of node: 224
0543 deg
Eccentricity:
0000998
Arg of perigee: 271
2567 deg
Mean anomaly: 88
8470 deg
Mean motion: 15
52626573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 323
Coasting Arc #6 (Orbit 843)
---------------------------------------
Vector Time (GMT): 2019/124/07:59:48
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3919625
36 A = 6782629
09 meter
Y = -2118949
17 meter E =
0004159
Z = 5111798
34 I = 51
38074
XDOT = 5054
777938 Wp = 47
03189
YDOT = 5546
943587 meter/sec RA = 218
01903 deg
ZDOT = -1572
982331 TA = 58
21061
MA = 58
17011
Ha = 222
959 n
mi
Hp = 217
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12859663
26 X = 3918197
97
Y = -6951932
97 feet Y = -2075125
22 meter
Z = 16770991
93 Z = 5130835
29
XDOT = 16583
917118 XDOT = 5000
015577
YDOT = 18198
633816 feet/sec YDOT = 5603
163477 meter/sec
ZDOT = -5160
703187 ZDOT = -1548
560573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14316090
27 X = 4363544
31
Y = -2418380
04 feet Y = -737122
23 meter
Z = 16857267
83 Z = 5138095
24
XDOT = 9605
732643 XDOT = 2927
827310
YDOT = 21575
760108 feet/sec YDOT = 6576
291681 meter/sec
ZDOT = -5050
661425 ZDOT = -1539
441602
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 19124
37883620
00016717 00000-0 10270-3 0 9056
2 25544 51
6383 218
9311 0000906 276
4802 83
6246 15
52585828 8441
Satellite: ISS
Catalog Number: 25544
Epoch time: 19124
37883620 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 218
9311 deg
Eccentricity:
0000906
Arg of perigee: 276
4802 deg
Mean anomaly: 83
6246 deg
Mean motion: 15
52585828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 844
Checksum: 321
Coasting Arc #7 (Orbit 845)
---------------------------------------
Vector Time (GMT): 2019/124/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2104385
95 A = 6781724
92 meter
Y = -3698957
47 meter E =
0001721
Z = 5279108
81 I = 51
38494
XDOT = 6314
787728 Wp = 125
41251
YDOT = 4319
306930 meter/sec RA = 217
41285 deg
ZDOT = 508
115571 TA = 319
71590
MA = 319
72865
Ha = 222
784 n
mi
Hp = 217
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6904153
37 X = 2119948
85
Y = -12135687
24 feet Y = -3675337
82 meter
Z = 17319910
79 Z = 5289369
08
XDOT = 20717
807507 XDOT = 6263
550486
YDOT = 14170
954495 feet/sec YDOT = 4389
636815 meter/sec
ZDOT = 1667
045835 ZDOT = 538
666670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 743126
93 X = 226505
09
Y = -13884171
80 feet Y = -4231895
56 meter
Z = 17366608
31 Z = 5293342
21
XDOT = 23820
348214 XDOT = 7260
442135
YDOT = 3537
047419 feet/sec YDOT = 1078
092053 meter/sec
ZDOT = 1804
910042 ZDOT = 550
136581
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 19124
50756214
00016717 00000-0 10270-3 0 9060
2 25544 51
6416 218
2918 0001201 275
2243 84
8772 15
52660260 8462
Satellite: ISS
Catalog Number: 25544
Epoch time: 19124
50756214 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 218
2918 deg
Eccentricity:
0001201
Arg of perigee: 275
2243 deg
Mean anomaly: 84
8772 deg
Mean motion: 15
52660260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 846
Checksum: 296
Coasting Arc #8 (Orbit 860)
---------------------------------------
Vector Time (GMT): 2019/125/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3074503
87 A = 6781911
60 meter
Y = 3012587
55 meter E =
0013406
Z = -5252560
47 I = 51
41209
XDOT = -6025
783471 Wp = 96
29456
YDOT = -4643
214934 meter/sec RA = 212
41381 deg
ZDOT = 864
463910 TA = 182
00827
MA = 182
01366
Ha = 222
936 n
mi
Hp = 217
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10086954
96 X = -3082448
42
Y = 9883817
41 feet Y = 2978162
06 meter
Z = -17232809
95 Z = -5267514
76
XDOT = -19769
630811 XDOT = -5977
613043
YDOT = -15233
644798 feet/sec YDOT = -4710
330157 meter/sec
ZDOT = 2836
167684 ZDOT = 835
309124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4364267
08 X = -1330228
61
Y = 13343365
43 feet Y = 4067057
78 meter
Z = -17300694
13 Z = -5273251
57
XDOT = -23585
705925 XDOT = -7188
923166
YDOT = -4209
485881 feet/sec YDOT = -1283
051296 meter/sec
ZDOT = 2704
627804 ZDOT = 824
370555
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 19125
47302961
00016717 00000-0 10270-3 0 9074
2 25544 51
6412 213
4915 0001111 282
2163 77
8864 15
52642556 8610
Satellite: ISS
Catalog Number: 25544
Epoch time: 19125
47302961 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 213
4915 deg
Eccentricity:
0001111
Arg of perigee: 282
2163 deg
Mean anomaly: 77
8864 deg
Mean motion: 15
52642556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 861
Checksum: 298
Coasting Arc #9 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2019/126/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4020207
03 A = 6783213
59 meter
Y = -2343631
93 meter E =
0005631
Z = 4932917
89 I = 51
44528
XDOT = 5525
678354 Wp = 48
64334
YDOT = 4840
101638 meter/sec RA = 207
41626 deg
ZDOT = -2198
474578 TA = 62
89416
MA = 62
83673
Ha = 222
798 n
mi
Hp = 217
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13189655
60 X = 4022153
53
Y = -7689081
12 feet Y = -2298664
56 meter
Z = 16184113
82 Z = 4952451
54
XDOT = 18128
865992 XDOT = 5481
823465
YDOT = 15879
598550 feet/sec YDOT = 4901
648562 meter/sec
ZDOT = -7212
843103 ZDOT = -2171
738584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7911167
34 X = 2411323
80
Y = -12947123
73 feet Y = -3946283
31 meter
Z = 16272674
70 Z = 4959911
25
XDOT = 22572
197361 XDOT = 6880
005756
YDOT = 4856
843357 feet/sec YDOT = 1480
365855 meter/sec
ZDOT = -7092
243714 ZDOT = -2161
715884
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 19126
50285859
00016717 00000-0 10270-3 0 9086
2 25544 51
6412 208
3691 0001169 287
9094 72
1930 15
52647323 8778
Satellite: ISS
Catalog Number: 25544
Epoch time: 19126
50285859 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 208
3691 deg
Eccentricity:
0001169
Arg of perigee: 287
9094 deg
Mean anomaly: 72
1930 deg
Mean motion: 15
52647323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 877
Checksum: 328
Coasting Arc #10 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2019/127/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4895885
03 A = 6785415
07 meter
Y = 1743009
51 meter E =
0007836
Z = -4370826
61 I = 51
48251
XDOT = -4788
466848 Wp = 110
64652
YDOT = -4910
418088 meter/sec RA = 202
42554 deg
ZDOT = 3407
764095 TA = 194
00194
MA = 194
02368
Ha = 222
909 n
mi
Hp = 217
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16062614
94 X = -4893780
56
Y = 5718535
15 feet Y = 1688272
41 meter
Z = -14339982
30 Z = -4394604
16
XDOT = -15710
193071 XDOT = -4749
754588
YDOT = -16110
295563 feet/sec YDOT = -4963
749891 meter/sec
ZDOT = 11180
328395 ZDOT = 3384
596733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11166712
67 X = -3403614
02
Y = 12763714
06 feet Y = 3890380
05 meter
Z = -14447714
94 Z = -4403663
51
XDOT = -20697
905511 XDOT = -6308
721600
YDOT = -5579
320901 feet/sec YDOT = -1700
577011 meter/sec
ZDOT = 11075
864158 ZDOT = 3375
923395
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 19127
46832091
00016717 00000-0 10270-3 0 9099
2 25544 51
6408 203
5681 0001153 292
9007 67
2023 15
52656579 8920
Satellite: ISS
Catalog Number: 25544
Epoch time: 19127
46832091 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 203
5681 deg
Eccentricity:
0001153
Arg of perigee: 292
9007 deg
Mean anomaly: 67
2023 deg
Mean motion: 15
52656579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 313
Coasting Arc #11 (Orbit 903)
---------------------------------------
Vector Time (GMT): 2019/128/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5279984
10 A = 6786873
71 meter
Y = 1560710
90 meter E =
0006022
Z = -3974571
16 I = 51
50744
XDOT = -4420
423492 Wp = 104
99844
YDOT = -4824
628065 meter/sec RA = 198
56671 deg
ZDOT = 3981
296975 TA = 206
59960
MA = 206
63051
Ha = 223
037 n
mi
Hp = 217
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17322782
47 X = -5277737
44
Y = 5120442
58 feet Y = 1501679
35 meter
Z = -13039931
61 Z = -4000214
13
XDOT = -14502
701746 XDOT = -4385
483810
YDOT = -15828
832235 feet/sec YDOT = -4873
865338 meter/sec
ZDOT = 13061
997950 ZDOT = 3959
908312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14713617
59 X = -4484710
64
Y = -10332660
36 feet Y = -3149394
88 meter
Z = -13156106
12 Z = -4009981
15
XDOT = 2596
544664 XDOT = 791
426814
YDOT = -20191
300353 feet/sec YDOT = -6154
308348 meter/sec
ZDOT = 12965
562985 ZDOT = 3951
903598
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 19128
24069042
00016717 00000-0 10270-3 0 9106
2 25544 51
6370 199
7243 0000996 306
9156 53
1904 15
52635407 9046
Satellite: ISS
Catalog Number: 25544
Epoch time: 19128
24069042 = yrday
fracday
Element set: 910
Inclination: 51
6370 deg
RA of node: 199
7243 deg
Eccentricity:
0000996
Arg of perigee: 306
9156 deg
Mean anomaly: 53
1904 deg
Mean motion: 15
52635407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 904
Checksum: 306
Coasting Arc #12 (Orbit 919)
---------------------------------------
Vector Time (GMT): 2019/129/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5967495
84 A = 6789659
77 meter
Y = -1051108
36 meter E =
0012056
Z = 3051984
21 I = 51
54709
XDOT = 3370
732142 Wp = 93
29816
YDOT = 4827
552671 meter/sec RA = 193
58679 deg
ZDOT = -4912
018786 TA = 51
64262
MA = 51
53435
Ha = 222
976 n
mi
Hp = 217
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19578398
42 X = 5963981
12
Y = -3448518
24 feet Y = -984395
60 meter
Z = 10013071
56 Z = 3080963
73
XDOT = 11058
832487 XDOT = 3340
358655
YDOT = 15838
427398 feet/sec YDOT = 4865
077214 meter/sec
ZDOT = -16115
547199 ZDOT = -4895
718157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15040130
44 X = 4584231
76
Y = 12897853
05 feet Y = 3931265
61 meter
Z = 10144329
83 Z = 3091991
73
XDOT = -4221
666263 XDOT = -1286
763877
YDOT = 17581
222006 feet/sec YDOT = 5358
756467 meter/sec
ZDOT = -16042
125408 ZDOT = -4889
639824
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 19129
27051420
00016717 00000-0 10270-3 0 9112
2 25544 51
6356 194
6022 0001100 305
7560 54
3489 15
52624283 9202
Satellite: ISS
Catalog Number: 25544
Epoch time: 19129
27051420 = yrday
fracday
Element set: 911
Inclination: 51
6356 deg
RA of node: 194
6022 deg
Eccentricity:
0001100
Arg of perigee: 305
7560 deg
Mean anomaly: 54
3489 deg
Mean motion: 15
52624283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 920
Checksum: 278
Coasting Arc #13 (Orbit 934)
---------------------------------------
Vector Time (GMT): 2019/130/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6459783
91 A = 6791891
73 meter
Y = 621127
05 meter E =
0006722
Z = -1994729
58 I = 51
58955
XDOT = -2176
111369 Wp = 32
24504
YDOT = -4795
035591 meter/sec RA = 188
61353 deg
ZDOT = 5568
305484 TA = 305
73336
MA = 305
79587
Ha = 223
024 n
mi
Hp = 217
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21193516
77 X = -6456560
09
Y = 2037818
41 feet Y = 548907
44 meter
Z = -6544388
38 Z = -2026101
08
XDOT = -7139
472997 XDOT = -2149
378070
YDOT = -15731
744066 feet/sec YDOT = -4819
221444 meter/sec
ZDOT = 18268
718779 ZDOT = 5557
799165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15245553
22 X = -4646844
62
Y = -14799025
72 feet Y = -4510743
04 meter
Z = -6686465
53 Z = -2038034
69
XDOT = 6207
711766 XDOT = 1892
110546
YDOT = -14607
179434 feet/sec YDOT = -4452
268292 meter/sec
ZDOT = 18221
512001 ZDOT = 5553
916858
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 19130
23597313
00016717 00000-0 10270-3 0 9127
2 25544 51
6378 189
7998 0001024 311
6130 48
4934 15
52642062 9357
Satellite: ISS
Catalog Number: 25544
Epoch time: 19130
23597313 = yrday
fracday
Element set: 912
Inclination: 51
6378 deg
RA of node: 189
7998 deg
Eccentricity:
0001024
Arg of perigee: 311
6130 deg
Mean anomaly: 48
4934 deg
Mean motion: 15
52642062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 935
Checksum: 308
Coasting Arc #14 (Orbit 950)
---------------------------------------
Vector Time (GMT): 2019/131/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6737281
52 A = 6793312
09 meter
Y = -204443
12 meter E =
0012271
Z = 798758
93 I = 51
62693
XDOT = 855
966295 Wp = 125
08666
YDOT = 4768
731906 meter/sec RA = 183
64611 deg
ZDOT = -5941
520428 TA = 46
28033
MA = 46
17877
Ha = 223
073 n
mi
Hp = 217
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22103942
01 X = 6735187
00
Y = -670745
14 feet Y = -129113
90 meter
Z = 2620600
16 Z = 831481
10
XDOT = 2808
288369 XDOT = 831
438035
YDOT = 15645
445885 feet/sec YDOT = 4778
167246 meter/sec
ZDOT = -19493
177257 ZDOT = -5937
421649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15090226
91 X = 4599501
16
Y = 16140649
86 feet Y = 4919670
08 meter
Z = 2768785
00 Z = 843925
67
XDOT = -8628
616063 XDOT = -2630
002176
YDOT = 11438
578829 feet/sec YDOT = 3486
478827 meter/sec
ZDOT = -19474
971331 ZDOT = -5935
971262
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 19131
26579279
00016717 00000-0 10270-3 0 9133
2 25544 51
6373 184
6769 0001148 320
3880 39
7188 15
52656261 9516
Satellite: ISS
Catalog Number: 25544
Epoch time: 19131
26579279 = yrday
fracday
Element set: 913
Inclination: 51
6373 deg
RA of node: 184
6769 deg
Eccentricity:
0001148
Arg of perigee: 320
3880 deg
Mean anomaly: 39
7188 deg
Mean motion: 15
52656261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 951
Checksum: 333
Coasting Arc #15 (Orbit 952)
---------------------------------------
Vector Time (GMT): 2019/131/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -313217
30 A = 6781685
28 meter
Y = 4207745
89 meter E =
0014024
Z = -5321356
79 I = 51
59607
XDOT = -7641
515626 Wp = 87
13248
YDOT = -459
808875 meter/sec RA = 182
92681 deg
ZDOT = 87
083077 TA = 183
69402
MA = 183
70438
Ha = 223
049 n
mi
Hp = 217
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1027615
82 X = -334397
98
Y = 13804940
59 feet Y = 4204125
25 meter
Z = -17458519
66 Z = -5322929
41
XDOT = -25070
589325 XDOT = -7636
228982
YDOT = -1508
559301 feet/sec YDOT = -545
232099 meter/sec
ZDOT = 285
705634 ZDOT = 49
976179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 109872
01 X = 33488
99
Y = 13833318
94 feet Y = 4216395
61 meter
Z = -17465952
67 Z = -5323622
37
XDOT = -24106
180981 XDOT = -7347
563963
YDOT = 336
427318 feet/sec YDOT = 102
543046 meter/sec
ZDOT = 117
711683 ZDOT = 35
878521
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 19131
39451972
00016717 00000-0 10270-3 0 9147
2 25544 51
6406 184
0391 0001241 316
0144 44
0909 15
52643407 9537
Satellite: ISS
Catalog Number: 25544
Epoch time: 19131
39451972 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 184
0391 deg
Eccentricity:
0001241
Arg of perigee: 316
0144 deg
Mean anomaly: 44
0909 deg
Mean motion: 15
52643407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 953
Checksum: 288
Coasting Arc #16 (Orbit 968)
---------------------------------------
Vector Time (GMT): 2019/132/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1502951
11 A = 6782236
16 meter
Y = -4139063
60 meter E =
0004556
Z = 5156566
96 I = 51
63174
XDOT = 7474
594130 Wp = 39
25273
YDOT = 888
733392 meter/sec RA = 177
94113 deg
ZDOT = -1461
047728 TA = 64
83636
MA = 64
78912
Ha = 222
961 n
mi
Hp = 217
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4930941
95 X = 1524075
81
Y = -13579604
99 feet Y = -4122138
72 meter
Z = 16917870
61 Z = 5163918
83
XDOT = 24522
946621 XDOT = 7471
197503
YDOT = 2915
791969 feet/sec YDOT = 972
300625 meter/sec
ZDOT = -4793
463673 ZDOT = -1424
747091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3563357
97 X = 1086111
51
Y = -13960098
20 feet Y = -4255037
93 meter
Z = 16951470
28 Z = 5166808
14
XDOT = 23699
901850 XDOT = 7223
730084
YDOT = 411
887414 feet/sec YDOT = 125
543284 meter/sec
ZDOT = -4629
127691 ZDOT = -1410
958120
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 19132
42433810
00016717 00000-0 10270-3 0 9154
2 25544 51
6406 178
9167 0001284 319
6086 40
4971 15
52677419 9697
Satellite: ISS
Catalog Number: 25544
Epoch time: 19132
42433810 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 178
9167 deg
Eccentricity:
0001284
Arg of perigee: 319
6086 deg
Mean anomaly: 40
4971 deg
Mean motion: 15
52677419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 969
Checksum: 325
Coasting Arc #17 (Orbit 983)
---------------------------------------
Vector Time (GMT): 2019/133/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2624676
69 A = 6784024
01 meter
Y = 4097356
86 meter E =
0010152
Z = -4736788
25 I = 51
67045
XDOT = -7023
433610 Wp = 105
22335
YDOT = -1323
102220 meter/sec RA = 172
96145 deg
ZDOT = 2749
544765 TA = 192
00448
MA = 192
02870
Ha = 223
077 n
mi
Hp = 217
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8611143
99 X = -2647290
66
Y = 13442771
86 feet Y = 4067879
62 meter
Z = -15540643
87 Z = -4749592
77
XDOT = -23042
761189 XDOT = -7021
472116
YDOT = -4340
886550 feet/sec YDOT = -1401
632303 meter/sec
ZDOT = 9020
816159 ZDOT = 2715
432156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7005236
32 X = -2135196
03
Y = 14281850
06 feet Y = 4353107
90 meter
Z = -15598940
70 Z = -4754557
12
XDOT = -22394
907397 XDOT = -6825
967775
YDOT = -1308
896673 feet/sec YDOT = -398
951706 meter/sec
ZDOT = 8866
400607 ZDOT = 2702
478905
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 19133
38979370
00016717 00000-0 10270-3 0 9167
2 25544 51
6401 174
1158 0001193 326
2286 33
8790 15
52669173 9845
Satellite: ISS
Catalog Number: 25544
Epoch time: 19133
38979370 = yrday
fracday
Element set: 916
Inclination: 51
6401 deg
RA of node: 174
1158 deg
Eccentricity:
0001193
Arg of perigee: 326
2286 deg
Mean anomaly: 33
8790 deg
Mean motion: 15
52669173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 984
Checksum: 326
Coasting Arc #18 (Orbit 999)
---------------------------------------
Vector Time (GMT): 2019/134/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3650887
34 A = 6786556
41 meter
Y = -4040652
55 meter E =
0010352
Z = 4043979
00 I = 51
71266
XDOT = 6343
473376 Wp = 70
56743
YDOT = 1806
248357 meter/sec RA = 167
98700 deg
ZDOT = -3910
573482 TA = 60
00703
MA = 59
90433
Ha = 223
035 n
mi
Hp = 217
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11977976
85 X = 3676156
19
Y = -13256734
09 feet Y = -3999684
58 meter
Z = 13267647
65 Z = 4061775
05
XDOT = 20811
920525 XDOT = 6341
799459
YDOT = 5926
011670 feet/sec YDOT = 1877
176255 meter/sec
ZDOT = -12829
965491 ZDOT = -3879
763070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10137217
75 X = 3089823
97
Y = -14638859
18 feet Y = -4461924
28 meter
Z = 13348558
73 Z = 4068640
70
XDOT = 20407
029358 XDOT = 6220
062548
YDOT = 2525
373577 feet/sec YDOT = 769
733866 meter/sec
ZDOT = -12690
526038 ZDOT = -3868
072336
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 19134
41960954
00016717 00000-0 10270-3 0 9171
2 25544 51
6409 168
9933 0001393 331
6386 28
4690 15
52671859 10001
Satellite: ISS
Catalog Number: 25544
Epoch time: 19134
41960954 = yrday
fracday
Element set: 917
Inclination: 51
6409 deg
RA of node: 168
9933 deg
Eccentricity:
0001393
Arg of perigee: 331
6386 deg
Mean anomaly: 28
4690 deg
Mean motion: 15
52671859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1000
Checksum: 326
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