[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 29th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19909 6822 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
184/00:03:16
781 0
4 1
7 1
7
N/A -1
6 -0
2 228
4
000/00:00:33
561 0
3 0
1 217
2
184/09:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 217
3
187/16:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 217
5
194/07:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
9
000/00:00:00
000 0
0 0
0 218
1
Coasting Arc #1 (Orbit 1699)
---------------------------------------
Vector Time (GMT): 2019/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 512988
11 A = 6792479
78 meter
Y = -5775996
63 meter E =
0013246
Z = -3550043
27 I = 51
32783
XDOT = 5825
142418 Wp = 95
68877
YDOT = -2207
043238 meter/sec RA = 304
41492 deg
ZDOT = 4445
740224 TA = 222
33894
MA = 222
44125
Ha = 228
521 n
mi
Hp = 216
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1683031
85 X = 594783
02
Y = -18950120
18 feet Y = -5769802
19 meter
Z = -11647123
58 Z = -3547353
50
XDOT = 19111
359639 XDOT = 5827
794268
YDOT = -7240
955505 feet/sec YDOT = -2141
888208 meter/sec
ZDOT = 14585
761889 ZDOT = 4474
042809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19032549
48 X = -5801121
08
Y = 32721
02 feet Y = 9973
37 meter
Z = -11634265
26 Z = -3546124
05
XDOT = -8997
317621 XDOT = -2742
382411
YDOT = -16858
047587 feet/sec YDOT = -5138
332904 meter/sec
ZDOT = 14714
332503 ZDOT = 4484
928547
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 19179
50747543
00016717 00000-0 10270-3 0 9009
2 25544 51
6414 305
1180 0008071 96
4269 263
7801 15
51223747 17005
Satellite: ISS
Catalog Number: 25544
Epoch time: 19179
50747543 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 305
1180 deg
Eccentricity:
0008071
Arg of perigee: 96
4269 deg
Mean anomaly: 263
7801 deg
Mean motion: 15
51223747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1700
Checksum: 298
Coasting Arc #2 (Orbit 1715)
---------------------------------------
Vector Time (GMT): 2019/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -743287
45 A = 6794178
65 meter
Y = 6077867
23 meter E =
0021369
Z = 2921382
32 I = 51
31621
XDOT = -5563
271695 Wp = 99
03185
YDOT = 1731
163850 meter/sec RA = 299
43064 deg
ZDOT = -4989
089335 TA = 47
48927
MA = 47
30896
Ha = 228
515 n
mi
Hp = 216
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2438607
12 X = -825387
16
Y = 19940509
27 feet Y = 6069095
75 meter
Z = 9584587
66 Z = 2917573
27
XDOT = -18252
203724 XDOT = -5557
982292
YDOT = 5679
671425 feet/sec YDOT = 1668
981827 meter/sec
ZDOT = -16368
403330 ZDOT = -5016
100589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20095858
19 X = 6125217
58
Y = 266712
97 feet Y = 81294
11 meter
Z = 9566628
63 Z = 2915908
41
XDOT = 7682
971504 XDOT = 2341
769715
YDOT = 15931
182837 feet/sec YDOT = 4855
824529 meter/sec
ZDOT = -16491
061460 ZDOT = -5026
475533
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 19180
53822396
00016717 00000-0 10270-3 0 9015
2 25544 51
6421 300
0015 0008132 101
0244 259
1822 15
51229254 17166
Satellite: ISS
Catalog Number: 25544
Epoch time: 19180
53822396 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 300
0015 deg
Eccentricity:
0008132
Arg of perigee: 101
0244 deg
Mean anomaly: 259
1822 deg
Mean motion: 15
51229254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1716
Checksum: 265
Coasting Arc #3 (Orbit 1730)
---------------------------------------
Vector Time (GMT): 2019/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 868265
80 A = 6795568
12 meter
Y = -6341122
33 meter E =
0012253
Z = -2289694
54 I = 51
30668
XDOT = 5297
018087 Wp = 78
13089
YDOT = -1212
565059 meter/sec RA = 294
44786 deg
ZDOT = 5393
828970 TA = 256
30184
MA = 256
43829
Ha = 228
502 n
mi
Hp = 216
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2848641
08 X = 950231
59
Y = -20804207
14 feet Y = -6330954
06 meter
Z = -7512121
18 Z = -2285278
89
XDOT = 17378
668266 XDOT = 5283
983396
YDOT = -3978
231820 feet/sec YDOT = -1153
403947 meter/sec
ZDOT = 17696
289273 ZDOT = 5419
528061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21004752
81 X = -6402248
66
Y = -202904
99 feet Y = -61845
44 meter
Z = -7491391
33 Z = -2283376
08
XDOT = -6175
650210 XDOT = -1882
338184
YDOT = -15073
915331 feet/sec YDOT = -4594
529393 meter/sec
ZDOT = 17812
939557 ZDOT = 5429
383977
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 19181
50454742
00016717 00000-0 10270-3 0 9020
2 25544 51
6433 295
2059 0008077 102
5614 257
6441 15
51226841 17313
Satellite: ISS
Catalog Number: 25544
Epoch time: 19181
50454742 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 295
2059 deg
Eccentricity:
0008077
Arg of perigee: 102
5614 deg
Mean anomaly: 257
6441 deg
Mean motion: 15
51226841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1731
Checksum: 297
Coasting Arc #4 (Orbit 1746)
---------------------------------------
Vector Time (GMT): 2019/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -993049
03 A = 6796751
72 meter
Y = 6532916
84 meter E =
0022004
Z = 1548583
18 I = 51
29715
XDOT = -5072
738950 Wp = 113
64091
YDOT = 598
193026 meter/sec RA = 289
46586 deg
ZDOT = -5720
481457 TA = 49
35889
MA = 49
16776
Ha = 228
496 n
mi
Hp = 216
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3258034
86 X = -1073550
30
Y = 21433454
20 feet Y = 6521361
46 meter
Z = 5080653
47 Z = 1543565
08
XDOT = -16642
844325 XDOT = -5051
264251
YDOT = 1962
575545 feet/sec YDOT = 541
587290 meter/sec
ZDOT = -18767
983783 ZDOT = -5745
070594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21684704
47 X = 6609497
92
Y = 138914
01 feet Y = 42340
99 meter
Z = 5057181
48 Z = 1541428
91
XDOT = 4353
331744 XDOT = 1326
895516
YDOT = 14474
033851 feet/sec YDOT = 4411
685518 meter/sec
ZDOT = -18879
536115 ZDOT = -5754
482608
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 19182
53529182
00016717 00000-0 10270-3 0 9036
2 25544 51
6425 290
0902 0008212 107
4004 252
8046 15
51236448 17471
Satellite: ISS
Catalog Number: 25544
Epoch time: 19182
53529182 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 290
0902 deg
Eccentricity:
0008212
Arg of perigee: 107
4004 deg
Mean anomaly: 252
8046 deg
Mean motion: 15
51236448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1747
Checksum: 291
Coasting Arc #5 (Orbit 1761)
---------------------------------------
Vector Time (GMT): 2019/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1026510
16 A = 6797441
31 meter
Y = -6664798
43 meter E =
0015009
Z = -839878
48 I = 51
29020
XDOT = 4881
233048 Wp = 69
93319
YDOT = 19
418538 meter/sec RA = 284
48452 deg
ZDOT = 5903
109686 TA = 280
95349
MA = 281
12231
Ha = 228
454 n
mi
Hp = 216
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3367815
49 X = 1105041
18
Y = -21866136
60 feet Y = -6652880
02 meter
Z = -2755506
84 Z = -834702
71
XDOT = 16014
544122 XDOT = 4851
979320
YDOT = 63
709114 feet/sec YDOT = 73
839161 meter/sec
ZDOT = 19367
157764 ZDOT = 5926
749664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22125959
91 X = -6743992
58
Y = 211483
68 feet Y = 64460
22 meter
Z = -2731318
61 Z = -832505
91
XDOT = -2501
173019 XDOT = -762
357536
YDOT = -14070
080279 feet/sec YDOT = -4288
560469 meter/sec
ZDOT = 19474
344574 ZDOT = 5935
780226
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 19183
50161281
00016717 00000-0 10270-3 0 9047
2 25544 51
6432 285
2952 0008105 109
7501 250
4525 15
51239221 17623
Satellite: ISS
Catalog Number: 25544
Epoch time: 19183
50161281 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 285
2952 deg
Eccentricity:
0008105
Arg of perigee: 109
7501 deg
Mean anomaly: 250
4525 deg
Mean motion: 15
51239221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1762
Checksum: 284
Coasting Arc #6 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2019/184/00:03:33
561
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3892444
11 A = 6786943
31 meter
Y = -1913364
06 meter E =
0020924
Z = -5238637
86 I = 51
24752
XDOT = 2299
916977 Wp = 101
30463
YDOT = -7233
714140 meter/sec RA = 281
97997 deg
ZDOT = 932
311370 TA = 177
69371
MA = 177
68405
Ha = 228
389 n
mi
Hp = 217
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12770485
91 X = -3845312
91
Y = -6277441
14 feet Y = -1956627
53 meter
Z = -17187132
08 Z = -5257431
61
XDOT = 7545
659373 XDOT = 2376
106903
YDOT = -23732
657938 feet/sec YDOT = -7207
569036 meter/sec
ZDOT = 3058
764337 ZDOT = 943
667007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3811422
47 X = 1161721
57
Y = -13602761
80 feet Y = -4146121
80 meter
Z = -17272145
70 Z = -5264550
01
XDOT = 23726
861622 XDOT = 7231
947422
YDOT = 2694
433281 feet/sec YDOT = 821
263264 meter/sec
ZDOT = 3111
027456 ZDOT = 948
241168
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 19184
01698455
00016717 00000-0 10270-3 0 9053
2 25544 51
6425 282
7396 0006663 110
3342 249
8525 15
50945969 17700
Satellite: ISS
Catalog Number: 25544
Epoch time: 19184
01698455 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 282
7396 deg
Eccentricity:
0006663
Arg of perigee: 110
3342 deg
Mean anomaly: 249
8525 deg
Mean motion: 15
50945969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 337
Coasting Arc #7 (Orbit 1776)
---------------------------------------
Vector Time (GMT): 2019/184/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3323538
31 A = 6794690
25 meter
Y = -5116171
91 meter E =
0019209
Z = 2976297
53 I = 51
27087
XDOT = 3154
514406 Wp = 94
40195
YDOT = 4940
642930 meter/sec RA = 279
97635 deg
ZDOT = 4941
159219 TA = 299
79489
MA = 299
98577
Ha = 228
310 n
mi
Hp = 217
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10903997
10 X = 3366044
79
Y = -16785340
92 feet Y = -5078768
69 meter
Z = 9764755
68 Z = 2992544
08
XDOT = 10349
456711 XDOT = 3075
031177
YDOT = 16209
458432 feet/sec YDOT = 4975
473540 meter/sec
ZDOT = 16211
152293 ZDOT = 4956
290390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11430269
77 X = -3483946
23
Y = -16387158
15 feet Y = -4994805
80 meter
Z = 9838966
25 Z = 2998916
91
XDOT = 17686
188160 XDOT = 5390
750151
YDOT = -2505
259703 feet/sec YDOT = -763
603157 meter/sec
ZDOT = 16279
242388 ZDOT = 4961
913080
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 19184
46802082
00016717 00000-0 10270-3 0 9066
2 25544 51
6423 280
4975 0006860 117
0903 243
0949 15
50984011 17776
Satellite: ISS
Catalog Number: 25544
Epoch time: 19184
46802082 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 280
4975 deg
Eccentricity:
0006860
Arg of perigee: 117
0903 deg
Mean anomaly: 243
0949 deg
Mean motion: 15
50984011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1777
Checksum: 316
Coasting Arc #8 (Orbit 1791)
---------------------------------------
Vector Time (GMT): 2019/185/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3258532
85 A = 6793282
13 meter
Y = 4812267
70 meter E =
0011552
Z = -3524410
81 I = 51
26096
XDOT = -3126
404991 Wp = 104
41001
YDOT = -5376
051487 meter/sec RA = 274
99081 deg
ZDOT = -4465
136186 TA = 117
25576
MA = 117
13803
Ha = 228
371 n
mi
Hp = 217
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10690724
58 X = -3294983
50
Y = 15788279
85 feet Y = 4775625
32 meter
Z = -11563027
59 Z = -3540326
94
XDOT = -10257
234224 XDOT = -3044
367316
YDOT = -17637
964195 feet/sec YDOT = -5410
553640 meter/sec
ZDOT = -14649
396937 ZDOT = -4480
124538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10862929
04 X = 3311020
77
Y = 15616410
69 feet Y = 4759881
98 meter
Z = -11635698
06 Z = -3546560
77
XDOT = -18983
643520 XDOT = -5786
214545
YDOT = 2276
649797 feet/sec YDOT = 693
922858 meter/sec
ZDOT = -14716
814202 ZDOT = -4485
684969
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 19185
43453122
00016717 00000-0 10270-3 0 9072
2 25544 51
6421 275
7030 0006907 119
2862 240
8980 15
50947367 17923
Satellite: ISS
Catalog Number: 25544
Epoch time: 19185
43453122 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 275
7030 deg
Eccentricity:
0006907
Arg of perigee: 119
2862 deg
Mean anomaly: 240
8980 deg
Mean motion: 15
50947367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1792
Checksum: 319
Coasting Arc #9 (Orbit 1807)
---------------------------------------
Vector Time (GMT): 2019/186/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3183034
33 A = 6791756
67 meter
Y = -4492998
29 meter E =
0017472
Z = 3966173
88 I = 51
25397
XDOT = 3171
574442 Wp = 109
39338
YDOT = 5753
794030 meter/sec RA = 270
00377 deg
ZDOT = 3952
732347 TA = 299
14388
MA = 299
31864
Ha = 228
238 n
mi
Hp = 217
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10443026
03 X = 3213774
68
Y = -14740808
03 feet Y = -4457232
10 meter
Z = 13012381
49 Z = 3981709
53
XDOT = 10405
427958 XDOT = 3087
798361
YDOT = 18877
277000 feet/sec YDOT = 5788
791769 meter/sec
ZDOT = 12968
281977 ZDOT = 3967
935775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10236564
20 X = -3120104
77
Y = -14822642
76 feet Y = -4517941
51 meter
Z = 13083283
26 Z = 3987784
74
XDOT = 20203
410171 XDOT = 6157
999420
YDOT = -2388
054198 feet/sec YDOT = -727
878920 meter/sec
ZDOT = 13036
658978 ZDOT = 3973
573657
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 19186
46547169
00016717 00000-0 10270-3 0 9082
2 25544 51
6416 270
5890 0006882 123
3323 236
8488 15
50986513 18086
Satellite: ISS
Catalog Number: 25544
Epoch time: 19186
46547169 = yrday
fracday
Element set: 908
Inclination: 51
6416 deg
RA of node: 270
5890 deg
Eccentricity:
0006882
Arg of perigee: 123
3323 deg
Mean anomaly: 236
8488 deg
Mean motion: 15
50986513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1808
Checksum: 342
Coasting Arc #10 (Orbit 1822)
---------------------------------------
Vector Time (GMT): 2019/187/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3182695
37 A = 6790387
58 meter
Y = 4095585
53 meter E =
0013956
Z = -4394027
31 I = 51
25018
XDOT = -3224
411383 Wp = 93
91936
YDOT = -6082
257993 meter/sec RA = 265
01477 deg
ZDOT = -3343
807113 TA = 142
05820
MA = 141
95979
Ha = 228
285 n
mi
Hp = 217
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10441913
95 X = -3206913
52
Y = 13436960
39 feet Y = 4059859
54 meter
Z = -14416100
10 Z = -4409545
65
XDOT = -10578
777504 XDOT = -3139
916155
YDOT = -19954
914676 feet/sec YDOT = -6117
842759 meter/sec
ZDOT = -10970
495776 ZDOT = -3359
265335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9262817
00 X = 2823306
62
Y = 14203525
06 feet Y = 4329234
44 meter
Z = -14486873
75 Z = -4415599
12
XDOT = -21270
178449 XDOT = -6483
150391
YDOT = 2644
938581 feet/sec YDOT = 806
177280 meter/sec
ZDOT = -11040
019629 ZDOT = -3364
997983
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 19187
43198014
00016717 00000-0 10270-3 0 9092
2 25544 51
6417 265
7945 0006847 126
9818 233
1961 15
50942713 18230
Satellite: ISS
Catalog Number: 25544
Epoch time: 19187
43198014 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 265
7945 deg
Eccentricity:
0006847
Arg of perigee: 126
9818 deg
Mean anomaly: 233
1961 deg
Mean motion: 15
50942713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1823
Checksum: 336
Coasting Arc #11 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2019/187/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4200122
04 A = 6786600
81 meter
Y = -632999
18 meter E =
0008974
Z = 5286150
91 I = 51
23587
XDOT = 972
414829 Wp = 116
88193
YDOT = 7606
767313 meter/sec RA = 263
51953 deg
ZDOT = 134
083291 TA = 331
80910
MA = 331
85765
Ha = 228
140 n
mi
Hp = 217
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13779927
95 X = 4181211
57
Y = -2076768
95 feet Y = -586136
83 meter
Z = 17343014
79 Z = 5306507
13
XDOT = 3190
337367 XDOT = 886
630217
YDOT = 24956
585671 feet/sec YDOT = 7617
161870 meter/sec
ZDOT = 439
905810 ZDOT = 138
599377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13740671
87 X = -4188156
79
Y = 1476610
88 feet Y = 450071
00 meter
Z = 17435397
97 Z = 5314309
30
XDOT = -1986
112912 XDOT = -605
367216
YDOT = -24070
064428 feet/sec YDOT = -7336
555638 meter/sec
ZDOT = 459
665040 ZDOT = 140
105904
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 19187
75414772
00016717 00000-0 10270-3 0 9101
2 25544 51
6390 264
1989 0006736 124
1670 236
0120 15
50956323 18280
Satellite: ISS
Catalog Number: 25544
Epoch time: 19187
75414772 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 264
1989 deg
Eccentricity:
0006736
Arg of perigee: 124
1670 deg
Mean anomaly: 236
0120 deg
Mean motion: 15
50956323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 315
Coasting Arc #12 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2019/188/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4290194
03 A = 6786798
92 meter
Y = 151218
88 meter E =
0020688
Z = -5274516
30 I = 51
24152
XDOT = -1028
148372 Wp = 104
75648
YDOT = -7553
465760 meter/sec RA = 258
52556 deg
ZDOT = 616
592462 TA = 171
19601
MA = 171
15967
Ha = 228
292 n
mi
Hp = 217
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14075439
73 X = -4265945
89
Y = 496124
95 feet Y = 103379
02 meter
Z = -17304843
50 Z = -5295297
21
XDOT = -3373
190197 XDOT = -946
601955
YDOT = -24781
711810 feet/sec YDOT = -7564
507341 meter/sec
ZDOT = 2022
941149 ZDOT = 611
795507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13967001
25 X = 4257141
98
Y = -124829
35 feet Y = -38047
99 meter
Z = -17399110
49 Z = -5303248
88
XDOT = 2719
623884 XDOT = 828
941360
YDOT = 23844
142297 feet/sec YDOT = 7267
694572 meter/sec
ZDOT = 2001
878866 ZDOT = 610
172678
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 19188
72065282
00016717 00000-0 10270-3 0 9118
2 25544 51
6393 259
4040 0006748 126
6955 233
4817 15
50936056 18436
Satellite: ISS
Catalog Number: 25544
Epoch time: 19188
72065282 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 259
4040 deg
Eccentricity:
0006748
Arg of perigee: 126
6955 deg
Mean anomaly: 233
4817 deg
Mean motion: 15
50936056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 328
Coasting Arc #13 (Orbit 1858)
---------------------------------------
Vector Time (GMT): 2019/189/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4400212
81 A = 6787193
80 meter
Y = 301965
07 meter E =
0008804
Z = 5150911
59 I = 51
24953
XDOT = 1074
340684 Wp = 101
85856
YDOT = 7472
605530 meter/sec RA = 253
53220 deg
ZDOT = -1355
644039 TA = 1
24111
MA = 1
23893
Ha = 228
018 n
mi
Hp = 217
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14436393
75 X = 4371489
16
Y = 990699
06 feet Y = 351010
29 meter
Z = 16899316
24 Z = 5172216
19
XDOT = 3524
739778 XDOT = 997
284908
YDOT = 24516
422343 feet/sec YDOT = 7484
188834 meter/sec
ZDOT = -4447
651045 ZDOT = -1350
611855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14312607
85 X = -4362482
87
Y = -1125052
07 feet Y = -342915
87 meter
Z = 16995921
65 Z = 5180356
92
XDOT = -3408
343274 XDOT = -1038
863030
YDOT = -23504
445960 feet/sec YDOT = -7164
155129 meter/sec
ZDOT = -4425
493450 ZDOT = -1348
890404
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 19189
75158989
00016717 00000-0 10270-3 0 9120
2 25544 51
6380 254
2890 0006608 130
3981 229
7748 15
50956978 18597
Satellite: ISS
Catalog Number: 25544
Epoch time: 19189
75158989 = yrday
fracday
Element set: 912
Inclination: 51
6380 deg
RA of node: 254
2890 deg
Eccentricity:
0006608
Arg of perigee: 130
3981 deg
Mean anomaly: 229
7748 deg
Mean motion: 15
50956978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1859
Checksum: 371
Coasting Arc #14 (Orbit 1873)
---------------------------------------
Vector Time (GMT): 2019/190/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4577658
30 A = 6788089
60 meter
Y = -735182
23 meter E =
0018715
Z = -4975415
13 I = 51
26285
XDOT = -1080
237713 Wp = 115
03195
YDOT = -7283
962015 meter/sec RA = 248
54055 deg
ZDOT = 2068
560048 TA = 175
26353
MA = 175
24580
Ha = 228
169 n
mi
Hp = 217
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15018563
98 X = -4544929
45
Y = -2412015
19 feet Y = -786189
37 meter
Z = -16323540
46 Z = -4997572
08
XDOT = -3544
086986 XDOT = -1008
753914
YDOT = -23897
513171 feet/sec YDOT = -7295
642486 meter/sec
ZDOT = 6786
614331 ZDOT = 2063
485660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14927074
64 X = 4549772
35
Y = 2295294
39 feet Y = 699605
73 meter
Z = -16423980
05 Z = -5006029
12
XDOT = 3945
629179 XDOT = 1202
627774
YDOT = 22779
466526 feet/sec YDOT = 6943
181397 meter/sec
ZDOT = 6764
230981 ZDOT = 2061
737603
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 19190
71809403
00016717 00000-0 10270-3 0 9133
2 25544 51
6381 249
4942 0006609 133
5132 226
6569 15
50934226 18742
Satellite: ISS
Catalog Number: 25544
Epoch time: 19190
71809403 = yrday
fracday
Element set: 913
Inclination: 51
6381 deg
RA of node: 249
4942 deg
Eccentricity:
0006609
Arg of perigee: 133
5132 deg
Mean anomaly: 226
6569 deg
Mean motion: 15
50934226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1874
Checksum: 319
Coasting Arc #15 (Orbit 1889)
---------------------------------------
Vector Time (GMT): 2019/191/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4763956
99 A = 6789088
96 meter
Y = 1128987
48 meter E =
0011408
Z = 4692942
68 I = 51
28011
XDOT = 1048
045892 Wp = 96
47804
YDOT = 7078
726997 meter/sec RA = 243
55034 deg
ZDOT = -2762
310025 TA = 21
03356
MA = 20
98668
Ha = 227
883 n
mi
Hp = 217
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15629780
17 X = 4728182
67
Y = 3704027
17 feet Y = 1182060
88 meter
Z = 15396793
57 Z = 4715997
32
XDOT = 3438
470773 XDOT = 982
229346
YDOT = 23224
169939 feet/sec YDOT = 7090
079264 meter/sec
ZDOT = -9062
696934 ZDOT = -2757
378160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15614008
17 X = -4759149
69
Y = -3314237
45 feet Y = -1010179
58 meter
Z = 15501279
83 Z = 4724790
09
XDOT = -4322
748977 XDOT = -1317
573888
YDOT = -21989
835103 feet/sec YDOT = -6702
501739 meter/sec
ZDOT = -9040
927556 ZDOT = -2755
674719
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 19191
74902971
00016717 00000-0 10270-3 0 9142
2 25544 51
6384 244
3792 0006516 137
6747 222
4908 15
50963587 18907
Satellite: ISS
Catalog Number: 25544
Epoch time: 19191
74902971 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 244
3792 deg
Eccentricity:
0006516
Arg of perigee: 137
6747 deg
Mean anomaly: 222
4908 deg
Mean motion: 15
50963587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1890
Checksum: 343
Coasting Arc #16 (Orbit 1904)
---------------------------------------
Vector Time (GMT): 2019/192/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5001149
69 A = 6790460
70 meter
Y = -1475545
20 meter E =
0014897
Z = -4365668
23 I = 51
30086
XDOT = -961
010863 Wp = 123
10742
YDOT = -6787
661413 meter/sec RA = 238
56281 deg
ZDOT = 3395
530888 TA = 181
55103
MA = 181
55565
Ha = 228
019 n
mi
Hp = 217
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16407971
41 X = -4963072
11
Y = -4841027
55 feet Y = -1531258
13 meter
Z = -14323058
48 Z = -4389869
54
XDOT = -3152
922778 XDOT = -901
531402
YDOT = -22269
230357 feet/sec YDOT = -6798
075952 meter/sec
ZDOT = 11140
193201 ZDOT = 3391
006315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16501473
73 X = 5029649
19
Y = 4147864
79 feet Y = 1264269
19 meter
Z = -14432728
78 Z = -4399095
73
XDOT = 4469
055814 XDOT = 1362
168212
YDOT = 20908
757696 feet/sec YDOT = 6372
989346 meter/sec
ZDOT = 11120
233996 ZDOT = 3389
447322
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 19192
71553055
00016717 00000-0 10270-3 0 9156
2 25544 51
6390 239
5843 0006473 140
0103 220
1526 15
50942135 19057
Satellite: ISS
Catalog Number: 25544
Epoch time: 19192
71553055 = yrday
fracday
Element set: 915
Inclination: 51
6390 deg
RA of node: 239
5843 deg
Eccentricity:
0006473
Arg of perigee: 140
0103 deg
Mean anomaly: 220
1526 deg
Mean motion: 15
50942135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1905
Checksum: 287
Coasting Arc #17 (Orbit 1920)
---------------------------------------
Vector Time (GMT): 2019/193/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5228877
35 A = 6791846
74 meter
Y = 1776257
82 meter E =
0014853
Z = 3938735
38 I = 51
32335
XDOT = 813
597772 Wp = 102
49123
YDOT = 6494
822953 meter/sec RA = 233
57803 deg
ZDOT = -3999
438923 TA = 29
45276
MA = 29
36915
Ha = 227
744 n
mi
Hp = 218
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17155109
41 X = 5189494
01
Y = 5827617
52 feet Y = 1834510
04 meter
Z = 12922360
18 Z = 3964039
78
XDOT = 2669
284028 XDOT = 760
337289
YDOT = 21308
474255 feet/sec YDOT = 6503
623934 meter/sec
ZDOT = -13121
518776 ZDOT = -3995
615241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17384242
58 X = -5298717
14
Y = -4803165
10 feet Y = -1464004
72 meter
Z = 13037024
67 Z = 3973685
12
XDOT = -4369
968495 XDOT = -1331
966397
YDOT = -19838
221619 feet/sec YDOT = -6046
689950 meter/sec
ZDOT = -13104
703311 ZDOT = -3994
313569
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 19193
74646411
00016717 00000-0 10270-3 0 9160
2 25544 51
6382 234
4697 0006368 144
0017 216
1564 15
50968590 19218
Satellite: ISS
Catalog Number: 25544
Epoch time: 19193
74646411 = yrday
fracday
Element set: 916
Inclination: 51
6382 deg
RA of node: 234
4697 deg
Eccentricity:
0006368
Arg of perigee: 144
0017 deg
Mean anomaly: 216
1564 deg
Mean motion: 15
50968590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1921
Checksum: 322
Coasting Arc #18 (Orbit 1929)
---------------------------------------
Vector Time (GMT): 2019/194/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5152000
27 A = 6797310
52 meter
Y = -4089565
26 meter E =
0008086
Z = -1720044
73 I = 51
35711
XDOT = 1918
067257 Wp = 88
88754
YDOT = -4786
598885 meter/sec RA = 230
50959 deg
ZDOT = 5658
756867 TA = 252
21334
MA = 252
30159
Ha = 227
928 n
mi
Hp = 218
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16902888
01 X = -5097531
70
Y = -13417208
84 feet Y = -4146873
73 meter
Z = -5643191
36 Z = -1744939
38
XDOT = 6292
871578 XDOT = 1943
962903
YDOT = -15704
064582 feet/sec YDOT = -4765
005763 meter/sec
ZDOT = 18565
475284 ZDOT = 5668
136243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21353546
65 X = -6508561
02
Y = 2910552
68 feet Y = 887136
46 meter
Z = -5755819
10 Z = -1754373
66
XDOT = -6870
492361 XDOT = -2094
126072
YDOT = -13754
838721 feet/sec YDOT = -4192
474842 meter/sec
ZDOT = 18608
422835 ZDOT = 5671
847280
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 19194
32636392
00016717 00000-0 10270-3 0 9173
2 25544 51
6416 231
5906 0006635 148
8926 211
2619 15
50938699 19309
Satellite: ISS
Catalog Number: 25544
Epoch time: 19194
32636392 = yrday
fracday
Element set: 917
Inclination: 51
6416 deg
RA of node: 231
5906 deg
Eccentricity:
0006635
Arg of perigee: 148
8926 deg
Mean anomaly: 211
2619 deg
Mean motion: 15
50938699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1930
Checksum: 336
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