[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 3rd 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15438 0847 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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
227/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
6
000/00:00:00
000 0
0 0
0 223
7
234/03:38:33
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
3
235/16:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
9
000/00:00:00
000 0
0 0
0 222
2
236/05:30:59
000 0
0 0
0 0
0
N/A 0
0 0
0 227
1
000/00:00:00
000 0
0 0
0 221
9
239/14:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
6
000/00:00:00
000 0
0 0
0 221
4
Coasting Arc #1 (Orbit 2443)
---------------------------------------
Vector Time (GMT): 2019/227/10:00:23
369
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -544904
31 A = 6797599
85 meter
Y = -6278087
01 meter E =
0003468
Z = -2543959
17 I = 52
00926
XDOT = 5250
952789 Wp = 248
94848
YDOT = 1698
409551 meter/sec RA = 66
66079 deg
ZDOT = -5311
519210 TA = 319
41004
MA = 319
43589
Ha = 225
432 n
mi
Hp = 223
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1787743
81 X = -462303
59
Y = -20597398
34 feet Y = -6283718
63 meter
Z = -8346322
73 Z = -2546405
52
XDOT = 17227
535396 XDOT = 5257
370228
YDOT = 5572
209814 feet/sec YDOT = 1757
165355 meter/sec
ZDOT = -17426
244126 ZDOT = -5285
997040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18328661
03 X = -5586575
88
Y = 9556819
82 feet Y = 2912918
68 meter
Z = -8356873
17 Z = -2547174
94
XDOT = -867
356487 XDOT = -264
370257
YDOT = -16813
434020 feet/sec YDOT = -5124
734689 meter/sec
ZDOT = -17310
193193 ZDOT = -5276
146885
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 19227
44405919
00016717 00000-0 10270-3 0 9004
2 25544 51
6429 67
2790 0007558 285
9510 74
0808 15
50348959 24445
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
44405919 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 67
2790 deg
Eccentricity:
0007558
Arg of perigee: 285
9510 deg
Mean anomaly: 74
0808 deg
Mean motion: 15
50348959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2444
Checksum: 333
Coasting Arc #2 (Orbit 2444)
---------------------------------------
Vector Time (GMT): 2019/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4676022
17 A = 6793731
44 meter
Y = 2930441
08 meter E =
0000937
Z = -3961636
01 I = 51
99292
XDOT = -614
186785 Wp = 283
19346
YDOT = 6467
722569 meter/sec RA = 66
20191 deg
ZDOT = 4058
666877 TA = 29
06353
MA = 29
05832
Ha = 225
552 n
mi
Hp = 223
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15341280
08 X = 4662148
58
Y = 9614308
00 feet Y = 2982654
12 meter
Z = -12997493
48 Z = -3938955
84
XDOT = -2015
048508 XDOT = -706
179360
YDOT = 21219
562235 feet/sec YDOT = 6460
339888 meter/sec
ZDOT = 13315
836212 ZDOT = 4055
460111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6452471
43 X = -1966713
29
Y = -16994767
91 feet Y = -5180005
26 meter
Z = -12894499
04 Z = -3930243
31
XDOT = 13289
462020 XDOT = 4050
628024
YDOT = -15138
794356 feet/sec YDOT = -4614
304520 meter/sec
ZDOT = 13300
627881 ZDOT = 4054
031378
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 19227
50851632
00016717 00000-0 10270-3 0 9019
2 25544 51
6403 66
9568 0007518 285
9401 74
0921 15
50378683 24455
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
50851632 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 66
9568 deg
Eccentricity:
0007518
Arg of perigee: 285
9401 deg
Mean anomaly: 74
0921 deg
Mean motion: 15
50378683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2445
Checksum: 318
Coasting Arc #3 (Orbit 2460)
---------------------------------------
Vector Time (GMT): 2019/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4888515
05 A = 6794729
25 meter
Y = -3016100
65 meter E =
0005804
Z = 3628651
96 I = 51
98291
XDOT = 541
773129 Wp = 54
56329
YDOT = -6222
444780 meter/sec RA = 61
26807 deg
ZDOT = -4433
903522 TA = 82
75591
MA = 82
68994
Ha = 225
646 n
mi
Hp = 223
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16038435
21 X = -4872050
41
Y = -9895343
35 feet Y = -3070675
39 meter
Z = 11905026
12 Z = 3604945
92
XDOT = 1777
470895 XDOT = 632
850999
YDOT = -20414
845080 feet/sec YDOT = -6215
877070 meter/sec
ZDOT = -14546
927567 ZDOT = -4431
050606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7133382
25 X = 2174254
91
Y = 17516155
10 feet Y = 5338924
08 meter
Z = 11797374
24 Z = 3595839
67
XDOT = -12319
677127 XDOT = -3755
037588
YDOT = 14823
960861 feet/sec YDOT = 4518
343270 meter/sec
ZDOT = -14533
347092 ZDOT = -4429
764194
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 19228
53984226
00016717 00000-0 10270-3 0 9020
2 25544 51
6413 61
8440 0007715 290
4484 69
5838 15
50402076 24618
Satellite: ISS
Catalog Number: 25544
Epoch time: 19228
53984226 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 61
8440 deg
Eccentricity:
0007715
Arg of perigee: 290
4484 deg
Mean anomaly: 69
5838 deg
Mean motion: 15
50402076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2461
Checksum: 312
Coasting Arc #4 (Orbit 2475)
---------------------------------------
Vector Time (GMT): 2019/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5109923
56 A = 6795821
92 meter
Y = 3050637
17 meter E =
0004301
Z = -3275052
36 I = 51
96785
XDOT = -507
191503 Wp = 327
92394
YDOT = 5972
430130 meter/sec RA = 56
33327 deg
ZDOT = 4772
508801 TA = 354
33475
MA = 354
33961
Ha = 225
947 n
mi
Hp = 223
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16764841
09 X = 5091338
76
Y = 10008652
13 feet Y = 3107675
95 meter
Z = -10744922
43 Z = -3250275
95
XDOT = -1664
014118 XDOT = -597
120991
YDOT = 19594
587040 feet/sec YDOT = 5966
255632 meter/sec
ZDOT = 15657
837273 ZDOT = 4769
826557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7954467
48 X = -2424521
69
Y = -17898735
10 feet Y = -5455534
46 meter
Z = -10632408
06 Z = -3240757
98
XDOT = 11465
267071 XDOT = 3494
613403
YDOT = -14387
658794 feet/sec YDOT = -4385
358401 meter/sec
ZDOT = 15645
051654 ZDOT = 4768
611744
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 19229
50671135
00016717 00000-0 10270-3 0 9031
2 25544 51
6398 57
0502 0007438 293
6657 66
3712 15
50376747 24762
Satellite: ISS
Catalog Number: 25544
Epoch time: 19229
50671135 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 57
0502 deg
Eccentricity:
0007438
Arg of perigee: 293
6657 deg
Mean anomaly: 66
3712 deg
Mean motion: 15
50376747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2476
Checksum: 327
Coasting Arc #5 (Orbit 2491)
---------------------------------------
Vector Time (GMT): 2019/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5335353
60 A = 6796759
61 meter
Y = -3061820
53 meter E =
0006499
Z = 2886906
97 I = 51
95174
XDOT = 524
692209 Wp = 77
75636
YDOT = -5711
549238 meter/sec RA = 51
39936 deg
ZDOT = -5076
929853 TA = 69
59472
MA = 69
52493
Ha = 226
001 n
mi
Hp = 223
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17504440
94 X = -5314741
68
Y = -10045342
94 feet Y = -3121368
87 meter
Z = 9471479
55 Z = 2861040
39
XDOT = 1721
431131 XDOT = 613
181918
YDOT = -18738
678603 feet/sec YDOT = -5705
187149 meter/sec
ZDOT = -16656
594006 ZDOT = -5074
166028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8844137
37 X = 2695693
07
Y = 18201839
85 feet Y = 5547920
79 meter
Z = 9354012
66 Z = 2851103
06
XDOT = -10754
173211 XDOT = -3277
871995
YDOT = 13797
267731 feet/sec YDOT = 4205
407205 meter/sec
ZDOT = -16643
456054 ZDOT = -5072
925405
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 19230
53803541
00016717 00000-0 10270-3 0 9045
2 25544 51
6398 51
9381 0007644 297
5205 62
5169 15
50400312 24929
Satellite: ISS
Catalog Number: 25544
Epoch time: 19230
53803541 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 51
9381 deg
Eccentricity:
0007644
Arg of perigee: 297
5205 deg
Mean anomaly: 62
5169 deg
Mean motion: 15
50400312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2492
Checksum: 298
Coasting Arc #6 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2019/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5554096
14 A = 6797729
87 meter
Y = 3017244
78 meter E =
0007718
Z = -2487405
40 I = 51
93272
XDOT = -577
911427 Wp = 342
40664
YDOT = 5464
767819 meter/sec RA = 46
46396 deg
ZDOT = 5341
238136 TA = 349
87436
MA = 349
88990
Ha = 226
248 n
mi
Hp = 222
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18222100
18 X = 5532025
94
Y = 9899097
05 feet Y = 3079231
10 meter
Z = -8160778
87 Z = -2460479
72
XDOT = -1896
034864 XDOT = -664
921546
YDOT = 17929
028279 feet/sec YDOT = 5457
818906 meter/sec
ZDOT = 17523
747166 ZDOT = 5338
219355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9828419
36 X = -2995702
22
Y = -18314477
86 feet Y = -5582252
85 meter
Z = -8038497
55 Z = -2450134
05
XDOT = 10201
530983 XDOT = 3109
426644
YDOT = -13155
644251 feet/sec YDOT = -4009
840368 meter/sec
ZDOT = 17509
466380 ZDOT = 5336
885353
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 19231
50490459
00016717 00000-0 10270-3 0 9054
2 25544 51
6395 47
1448 0007350 300
4827 59
5597 15
50373703 25076
Satellite: ISS
Catalog Number: 25544
Epoch time: 19231
50490459 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 47
1448 deg
Eccentricity:
0007350
Arg of perigee: 300
4827 deg
Mean anomaly: 59
5597 deg
Mean motion: 15
50373703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 314
Coasting Arc #7 (Orbit 2522)
---------------------------------------
Vector Time (GMT): 2019/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5765332
47 A = 6798455
67 meter
Y = -2953520
97 meter E =
0006757
Z = 2055848
93 I = 51
91239
XDOT = 684
293827 Wp = 96
21869
YDOT = -5219
252120 meter/sec RA = 41
52836 deg
ZDOT = -5564
212327 TA = 61
17884
MA = 61
11102
Ha = 226
330 n
mi
Hp = 222
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18915132
77 X = -5741862
95
Y = -9690029
44 feet Y = -3017861
68 meter
Z = 6744911
18 Z = 2027900
44
XDOT = 2245
058488 XDOT = 769
633790
YDOT = -17123
530577 feet/sec YDOT = -5211
122902 meter/sec
ZDOT = -18255
289787 ZDOT = -5560
680847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10831209
33 X = 3301352
60
Y = 18331938
98 feet Y = 5587575
00 meter
Z = 6617980
27 Z = 2017160
38
XDOT = -9827
881158 XDOT = -2995
538177
YDOT = 12409
095213 feet/sec YDOT = 3782
292221 meter/sec
ZDOT = -18238
692994 ZDOT = -5559
153625
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 19232
53622703
00016717 00000-0 10270-3 0 9068
2 25544 51
6402 42
0325 0007578 304
9129 55
1309 15
50405619 25232
Satellite: ISS
Catalog Number: 25544
Epoch time: 19232
53622703 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 42
0325 deg
Eccentricity:
0007578
Arg of perigee: 304
9129 deg
Mean anomaly: 55
1309 deg
Mean motion: 15
50405619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2523
Checksum: 284
Coasting Arc #8 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2019/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5954426
67 A = 6799190
54 meter
Y = 2836786
62 meter E =
0010876
Z = -1621332
13 I = 51
88949
XDOT = -821
607908 Wp = 355
87533
YDOT = 5004
540215 meter/sec RA = 36
59125 deg
ZDOT = 5747
031858 TA = 346
46348
MA = 346
49263
Ha = 226
555 n
mi
Hp = 222
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19535520
57 X = 5930137
86
Y = 9307042
71 feet Y = 2903237
36 meter
Z = -5319331
15 Z = -1592466
97
XDOT = -2695
564003 XDOT = -905
424814
YDOT = 16419
095194 feet/sec YDOT = 4994
883926 meter/sec
ZDOT = 18855
091399 ZDOT = 5742
837101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11865755
83 X = -3616682
38
Y = -18133918
74 feet Y = -5527218
43 meter
Z = -5188229
15 Z = -1581372
24
XDOT = 9635
058599 XDOT = 2936
765861
YDOT = -11685
703285 feet/sec YDOT = -3561
802361 meter/sec
ZDOT = 18835
490675 ZDOT = 5741
057558
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 19233
50309358
00016717 00000-0 10270-3 0 9075
2 25544 51
6408 37
2395 0007213 308
7346 51
3159 15
50380280 25383
Satellite: ISS
Catalog Number: 25544
Epoch time: 19233
50309358 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 37
2395 deg
Eccentricity:
0007213
Arg of perigee: 308
7346 deg
Mean anomaly: 51
3159 deg
Mean motion: 15
50380280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2538
Checksum: 302
Coasting Arc #9 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2019/234/03:38:33
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4351309
94 A = 6798447
14 meter
Y = 4794173
06 meter E =
0012603
Z = 2046392
13 I = 51
87097
XDOT = -4860
784475 Wp = 36
12939
YDOT = 2031
096812 meter/sec RA = 33
40769 deg
ZDOT = 5569
773397 TA = 346
39826
MA = 346
43219
Ha = 226
739 n
mi
Hp = 222
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14275951
26 X = 4287436
52
Y = 15728914
24 feet Y = 4842475
37 meter
Z = 6713884
95 Z = 2067373
87
XDOT = -15947
455626 XDOT = -4910
190299
YDOT = 6663
703453 feet/sec YDOT = 1976
463958 meter/sec
ZDOT = 18273
534768 ZDOT = 5546
041572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19384494
09 X = 5908393
80
Y = 8611509
96 feet Y = 2624788
24 meter
Z = 6808895
94 Z = 2075351
48
XDOT = -11361
592453 XDOT = -3463
013380
YDOT = 11192
828877 feet/sec YDOT = 3411
574242 meter/sec
ZDOT = 18165
308512 ZDOT = 5536
786034
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 19234
21212823
00016717 00000-0 10270-3 0 9085
2 25544 51
6423 33
7294 0007575 313
7521 46
3002 15
50374763 25493
Satellite: ISS
Catalog Number: 25544
Epoch time: 19234
21212823 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 33
7294 deg
Eccentricity:
0007575
Arg of perigee: 313
7521 deg
Mean anomaly: 46
3002 deg
Mean motion: 15
50374763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 292
Coasting Arc #10 (Orbit 2563)
---------------------------------------
Vector Time (GMT): 2019/235/03:38:33
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4369982
49 A = 6797582
96 meter
Y = -4582088
14 meter E =
0002424
Z = -2475275
40 I = 51
84076
XDOT = 5116
292088 Wp = 330
39003
YDOT = -1994
890125 meter/sec RA = 28
46808 deg
ZDOT = -5335
462373 TA = 237
19391
MA = 237
21725
Ha = 226
905 n
mi
Hp = 222
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14337212
90 X = -4306395
99
Y = -15033097
56 feet Y = -4630600
83 meter
Z = -8120982
27 Z = -2496348
63
XDOT = 16785
735198 XDOT = 5164
135921
YDOT = -6544
915109 feet/sec YDOT = -1937
408645 meter/sec
ZDOT = -17504
797812 ZDOT = -5310
493199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19283835
02 X = -5877712
91
Y = -7623923
90 feet Y = -2323772
01 meter
Z = -8216418
95 Z = -2504364
50
XDOT = 12020
682327 XDOT = 3663
903973
YDOT = -11647
464863 feet/sec YDOT = -3550
147290 meter/sec
ZDOT = -17390
947402 ZDOT = -5300
760768
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 19235
17899266
00016717 00000-0 10270-3 0 9094
2 25544 51
6433 28
9375 0007632 316
9988 43
0565 15
50386035 25646
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
17899266 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 28
9375 deg
Eccentricity:
0007632
Arg of perigee: 316
9988 deg
Mean anomaly: 43
0565 deg
Mean motion: 15
50386035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2564
Checksum: 344
Coasting Arc #11 (Orbit 2571)
---------------------------------------
Vector Time (GMT): 2019/235/16:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4351881
93 A = 6790618
22 meter
Y = -2078050
93 meter E =
0005634
Z = -4784589
93 I = 51
80224
XDOT = 5263
238693 Wp = 71
71381
YDOT = 4879
422799 meter/sec RA = 25
79649 deg
ZDOT = 2672
309192 TA = 224
62332
MA = 224
66869
Ha = 226
854 n
mi
Hp = 222
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14277827
86 X = 4398036
67
Y = -6817752
38 feet Y = -2029127
02 meter
Z = -15697473
52 Z = -4763338
09
XDOT = 17267
843481 XDOT = 5195
303849
YDOT = 16008
604984 feet/sec YDOT = 4937
900171 meter/sec
ZDOT = 8767
418610 ZDOT = 2697
710997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7436658
16 X = -2266693
41
Y = 14073671
07 feet Y = 4289654
94 meter
Z = -15600534
89 Z = -4755043
03
XDOT = -22342
166061 XDOT = -6809
892215
YDOT = -1975
372451 feet/sec YDOT = -602
093523 meter/sec
ZDOT = 8882
518451 ZDOT = 2707
391624
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 19235
69465175
00016717 00000-0 10270-3 0 9101
2 25544 51
6438 26
3795 0007352 316
1126 43
9440 15
50410718 25720
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
69465175 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 26
3795 deg
Eccentricity:
0007352
Arg of perigee: 316
1126 deg
Mean anomaly: 43
9440 deg
Mean motion: 15
50410718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2572
Checksum: 305
Coasting Arc #12 (Orbit 2580)
---------------------------------------
Vector Time (GMT): 2019/236/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3574562
34 A = 6789436
74 meter
Y = 2799154
45 meter E =
0009241
Z = 5051055
68 I = 51
78310
XDOT = -6073
360653 Wp = 358
52133
YDOT = -4247
379196 meter/sec RA = 23
10119 deg
ZDOT = -1935
324533 TA = 110
28725
MA = 110
18790
Ha = 227
080 n
mi
Hp = 221
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11727566
72 X = -3630132
75
Y = 9183577
60 feet Y = 2758870
39 meter
Z = 16571704
98 Z = 5033556
93
XDOT = -19925
723927 XDOT = -6016
013153
YDOT = -13934
971114 feet/sec YDOT = -4314
975107 meter/sec
ZDOT = -6349
489937 ZDOT = -1964
687320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 489446
48 X = 149183
29
Y = 14975887
44 feet Y = 4564650
49 meter
Z = 16491772
56 Z = 5026692
28
XDOT = -21859
204869 XDOT = -6662
685644
YDOT = 7885
691946 feet/sec YDOT = 2403
558905 meter/sec
ZDOT = -6482
676718 ZDOT = -1975
919864
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 19236
27476858
00016717 00000-0 10270-3 0 9117
2 25544 51
6449 23
5068 0007827 320
1401 39
9174 15
50431330 25814
Satellite: ISS
Catalog Number: 25544
Epoch time: 19236
27476858 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 23
5068 deg
Eccentricity:
0007827
Arg of perigee: 320
1401 deg
Mean anomaly: 39
9174 deg
Mean motion: 15
50431330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2581
Checksum: 305
Coasting Arc #13 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2019/237/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3796070
04 A = 6790228
04 meter
Y = -2807436
64 meter E =
0007190
Z = -4884711
58 I = 51
75379
XDOT = 6066
017318 Wp = 66
54413
YDOT = 3997
720532 meter/sec RA = 18
15051 deg
ZDOT = 2422
073188 TA = 227
17408
MA = 227
23453
Ha = 227
301 n
mi
Hp = 221
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12454298
02 X = 3850908
54
Y = -9210750
14 feet Y = -2764679
56 meter
Z = -16025956
64 Z = -4866138
70
XDOT = 19901
631621 XDOT = 6009
097804
YDOT = 13115
881011 feet/sec YDOT = 4065
236681 meter/sec
ZDOT = 7946
434345 ZDOT = 2451
401313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -355053
64 X = -108220
35
Y = -15573466
80 feet Y = -4746792
68 meter
Z = -15941135
85 Z = -4858858
21
XDOT = 20984
697993 XDOT = 6396
135948
YDOT = -8729
676195 feet/sec YDOT = -2660
805304 meter/sec
ZDOT = 8079
480283 ZDOT = 2462
625590
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 19237
24163111
00016717 00000-0 10270-3 0 9121
2 25544 51
6444 18
7140 0007807 324
4610 35
6020 15
50400561 25964
Satellite: ISS
Catalog Number: 25544
Epoch time: 19237
24163111 = yrday
fracday
Element set: 912
Inclination: 51
6444 deg
RA of node: 18
7140 deg
Eccentricity:
0007807
Arg of perigee: 324
4610 deg
Mean anomaly: 35
6020 deg
Mean motion: 15
50400561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 269
Coasting Arc #14 (Orbit 2611)
---------------------------------------
Vector Time (GMT): 2019/238/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4043647
64 A = 6791017
83 meter
Y = 2832600
33 meter E =
0010736
Z = 4665045
74 I = 51
72408
XDOT = -6004
187256 Wp = 17
59150
YDOT = -3764
217880 meter/sec RA = 13
19859 deg
ZDOT = -2907
049737 TA = 101
37986
MA = 101
25923
Ha = 227
409 n
mi
Hp = 221
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13266560
51 X = -4097682
04
Y = 9293308
15 feet Y = 2787079
13 meter
Z = 15305268
17 Z = 4645272
27
XDOT = -19698
777086 XDOT = -5947
527753
YDOT = -12349
796194 feet/sec YDOT = -3831
044028 meter/sec
ZDOT = -9537
564753 ZDOT = -2936
078047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 240286
31 X = 73239
27
Y = 16280816
83 feet Y = 4962392
97 meter
Z = 15214982
87 Z = 4637526
78
XDOT = -20024
608161 XDOT = -6103
500568
YDOT = 9368
013071 feet/sec YDOT = 2855
370384 meter/sec
ZDOT = -9669
264604 ZDOT = -2947
191851
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 19238
27294864
00016717 00000-0 10270-3 0 9136
2 25544 51
6438 13
6021 0007917 328
0714 31
9956 15
50434107 26125
Satellite: ISS
Catalog Number: 25544
Epoch time: 19238
27294864 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 13
6021 deg
Eccentricity:
0007917
Arg of perigee: 328
0714 deg
Mean anomaly: 31
9956 deg
Mean motion: 15
50434107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 305
Coasting Arc #15 (Orbit 2626)
---------------------------------------
Vector Time (GMT): 2019/239/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4247763
03 A = 6792027
33 meter
Y = -2917409
22 meter E =
0005924
Z = -4426283
81 I = 51
69427
XDOT = 5912
116346 Wp = 49
95730
YDOT = 3532
264088 meter/sec RA = 8
24464 deg
ZDOT = 3352
209455 TA = 253
90881
MA = 253
97404
Ha = 227
593 n
mi
Hp = 221
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13936230
42 X = 4301570
76
Y = -9571552
55 feet Y = -2869606
77 meter
Z = -14521928
51 Z = -4405519
46
XDOT = 19396
707173 XDOT = 5855
895216
YDOT = 11588
792938 feet/sec YDOT = 3598
063092 meter/sec
ZDOT = 10998
062515 ZDOT = 3380
791432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -392068
06 X = -119502
35
Y = -16983044
17 feet Y = -5176431
86 meter
Z = -14427128
53 Z = -4397388
78
XDOT = 19000
721565 XDOT = 5791
419933
YDOT = -9872
920475 feet/sec YDOT = -3009
266161 meter/sec
ZDOT = 11127
751838 ZDOT = 3391
738760
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 19239
23981049
00016717 00000-0 10270-3 0 9142
2 25544 51
6437 8
8092 0007883 331
1924 28
8790 15
50399878 26270
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
23981049 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 8
8092 deg
Eccentricity:
0007883
Arg of perigee: 331
1924 deg
Mean anomaly: 28
8790 deg
Mean motion: 15
50399878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 346
Coasting Arc #16 (Orbit 2632)
---------------------------------------
Vector Time (GMT): 2019/239/14:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 928585
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6326510
38 A = 6798291
86 meter
Y = -1069726
66 meter E =
0011250
Z = -2225947
40 I = 51
70215
XDOT = 2704
290336 Wp = 2
01293
YDOT = 4642
159184 meter/sec RA = 6
30287 deg
ZDOT = 5466
960103 TA = 333
30193
MA = 333
35981
Ha = 227
597 n
mi
Hp = 221
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20756267
65 X = 6348814
42
Y = -3509601
90 feet Y = -998854
41 meter
Z = -7302977
02 Z = -2195161
93
XDOT = 8872
343621 XDOT = 2625
624358
YDOT = 15230
181051 feet/sec YDOT = 4671
960499 meter/sec
ZDOT = 17936
220809 ZDOT = 5479
905355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18587371
69 X = -5665430
89
Y = 9983872
59 feet Y = 3043084
37 meter
Z = -7162773
70 Z = -2183213
43
XDOT = -12437
630704 XDOT = -3790
989839
YDOT = -10273
999460 feet/sec YDOT = -3131
515035 meter/sec
ZDOT = 17994
635957 ZDOT = 5484
765040
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 19239
62655438
00016717 00000-0 10270-3 0 9156
2 25544 51
6440 6
8895 0007632 331
1091 28
9636 15
50359846 26338
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
62655438 = yrday
fracday
Element set: 915
Inclination: 51
6440 deg
RA of node: 6
8895 deg
Eccentricity:
0007632
Arg of perigee: 331
1091 deg
Mean anomaly: 28
9636 deg
Mean motion: 15
50359846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2633
Checksum: 328
Coasting Arc #17 (Orbit 2648)
---------------------------------------
Vector Time (GMT): 2019/240/14:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 928585
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6442095
17 A = 6798936
72 meter
Y = 1249821
35 meter E =
0009570
Z = 1772732
18 I = 51
67141
XDOT = -2446
420924 Wp = 83
80649
YDOT = -4536
937428 meter/sec RA = 1
35186 deg
ZDOT = -5664
265948 TA = 76
77612
MA = 76
66938
Ha = 227
622 n
mi
Hp = 221
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21135482
83 X = -6464203
02
Y = 4100463
73 feet Y = 1177657
69 meter
Z = 5816050
45 Z = 1741385
81
XDOT = -8026
315368 XDOT = -2367
992440
YDOT = -14884
965314 feet/sec YDOT = -4563
856516 meter/sec
ZDOT = -18583
549697 ZDOT = -5675
959019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18561906
49 X = 5657669
10
Y = -10982639
24 feet Y = -3347508
44 meter
Z = 5673283
26 Z = 1729216
74
XDOT = 11645
962771 XDOT = 3549
689453
YDOT = 10008
564301 feet/sec YDOT = 3050
610399 meter/sec
ZDOT = -18636
279611 ZDOT = -5680
338025
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 19240
65787037
00016717 00000-0 10270-3 0 9163
2 25544 51
6440 1
7777 0007544 336
2471 23
8330 15
50396664 26492
Satellite: ISS
Catalog Number: 25544
Epoch time: 19240
65787037 = yrday
fracday
Element set: 916
Inclination: 51
6440 deg
RA of node: 1
7777 deg
Eccentricity:
0007544
Arg of perigee: 336
2471 deg
Mean anomaly: 23
8330 deg
Mean motion: 15
50396664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2649
Checksum: 319
Coasting Arc #18 (Orbit 2663)
---------------------------------------
Vector Time (GMT): 2019/241/14:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 928585
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6495694
79 A = 6799632
29 meter
Y = -1464767
78 meter E =
0014598
Z = -1331542
57 I = 51
63961
XDOT = 2198
251115 Wp = 10
41162
YDOT = 4478
249239 meter/sec RA = 356
39878 deg
ZDOT = 5821
458860 TA = 335
10674
MA = 335
17708
Ha = 227
930 n
mi
Hp = 220
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21311334
61 X = 6518059
24
Y = -4805668
56 feet Y = -1392003
34 meter
Z = -4368577
97 Z = -1299935
21
XDOT = 7212
109956 XDOT = 2119
733833
YDOT = 14692
418762 feet/sec YDOT = 4502
392794 meter/sec
ZDOT = 19099
274474 ZDOT = 5831
946079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18277174
17 X = -5570882
69
Y = 12018713
30 feet Y = 3663303
81 meter
Z = -4224611
40 Z = -1287661
56
XDOT = -10930
960496 XDOT = -3331
756759
YDOT = -9921
553835 feet/sec YDOT = -3024
089609 meter/sec
ZDOT = 19146
526434 ZDOT = 5835
861257
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 19241
62472784
00016717 00000-0 10270-3 0 9172
2 25544 51
6437 356
9854 0007784 339
6979 20
3861 15
50351195 26643
Satellite: ISS
Catalog Number: 25544
Epoch time: 19241
62472784 = yrday
fracday
Element set: 917
Inclination: 51
6437 deg
RA of node: 356
9854 deg
Eccentricity:
0007784
Arg of perigee: 339
6979 deg
Mean anomaly: 20
3861 deg
Mean motion: 15
50351195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2664
Checksum: 349
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