[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 3rd 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 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
033/17:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 216
5
034/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 216
4
037/01:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 216
1
039/16:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 215
6
040/11:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 215
5
044/15:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
7
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 3417)
---------------------------------------
Vector Time (GMT): 2019/032/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5157316
06 A = 6783581
05 meter
Y = 169470
41 meter E =
0010513
Z = -4413918
84 I = 51
36568
XDOT = 2631
284943 Wp = 38
86550
YDOT = -6381
540030 meter/sec RA = 314
98515 deg
ZDOT = -3315
746806 TA = 197
45391
MA = 197
49007
Ha = 222
645 n
mi
Hp = 216
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16920328
29 X = -5137387
94
Y = 556005
29 feet Y = 111909
31 meter
Z = -14481361
01 Z = -4438922
18
XDOT = 8632
824615 XDOT = 2718
555260
YDOT = -20936
811122 feet/sec YDOT = -6351
627079 meter/sec
ZDOT = -10878
434403 ZDOT = -3302
753583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16052789
29 X = -4892890
18
Y = -5063055
58 feet Y = -1543219
34 meter
Z = -14594173
23 Z = -4448304
00
XDOT = 14794
963212 XDOT = 4509
504787
YDOT = -15688
041069 feet/sec YDOT = -4781
714918 meter/sec
ZDOT = -10818
998261 ZDOT = -3297
630670
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 19032
60538886
00016717 00000-0 10270-3 0 9006
2 25544 51
6422 315
5198 0005298 337
7898 22
3024 15
53229580 34182
Satellite: ISS
Catalog Number: 25544
Epoch time: 19032
60538886 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 315
5198 deg
Eccentricity:
0005298
Arg of perigee: 337
7898 deg
Mean anomaly: 22
3024 deg
Mean motion: 15
53229580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3418
Checksum: 322
Coasting Arc #2 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2019/033/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4449560
78 A = 6781127
53 meter
Y = 951063
97 meter E =
0003432
Z = 5024934
27 I = 51
33520
XDOT = -3523
920157 Wp = 57
62149
YDOT = 6546
706655 meter/sec RA = 309
97923 deg
ZDOT = 1882
192715 TA = 14
06432
MA = 14
05477
Ha = 222
618 n
mi
Hp = 216
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14598296
54 X = 4414187
30
Y = 3120288
62 feet Y = 1000624
12 meter
Z = 16486004
81 Z = 5046462
14
XDOT = -11561
417837 XDOT = -3606
007789
YDOT = 21478
696376 feet/sec YDOT = 6506
840685 meter/sec
ZDOT = 6175
172949 ZDOT = 1864
876094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12760615
78 X = 3889435
69
Y = 7536958
76 feet Y = 2297265
03 meter
Z = 16582995
96 Z = 5054497
17
XDOT = -17242
186838 XDOT = -5255
418548
YDOT = 15785
394035 feet/sec YDOT = 4811
388102 meter/sec
ZDOT = 6096
227412 ZDOT = 1858
130115
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 19033
63482565
00016717 00000-0 10270-3 0 9013
2 25544 51
6428 310
3950 0005231 341
5761 18
5201 15
53221754 34343
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
63482565 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 310
3950 deg
Eccentricity:
0005231
Arg of perigee: 341
5761 deg
Mean anomaly: 18
5201 deg
Mean motion: 15
53221754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 280
Coasting Arc #3 (Orbit 3435)
---------------------------------------
Vector Time (GMT): 2019/033/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1929265
24 A = 6788603
41 meter
Y = 5881174
93 meter E =
0011595
Z = 2782313
19 I = 51
35458
XDOT = -5703
372020 Wp = 76
59203
YDOT = 547
850003 meter/sec RA = 309
22682 deg
ZDOT = -5092
187256 TA = 71
74304
MA = 71
61689
Ha = 222
693 n
mi
Hp = 216
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6329610
37 X = -2008401
40
Y = 19295193
36 feet Y = 5859157
99 meter
Z = 9128324
10 Z = 2772749
75
XDOT = -18711
850458 XDOT = -5684
339967
YDOT = 1797
408146 feet/sec YDOT = 484
177484 meter/sec
ZDOT = -16706
651104 ZDOT = -5119
845152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5143311
94 X = 1567681
48
Y = 19665046
54 feet Y = 5993906
19 meter
Z = 9084439
55 Z = 2768937
17
XDOT = -13190
594674 XDOT = -4020
493257
YDOT = 11256
738181 feet/sec YDOT = 3431
053798 meter/sec
ZDOT = -16831
484409 ZDOT = -5130
236448
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 19033
76350230
00016717 00000-0 10270-3 0 9021
2 25544 51
6400 309
7516 0005449 339
5414 20
5519 15
53262533 34363
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
76350230 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 309
7516 deg
Eccentricity:
0005449
Arg of perigee: 339
5414 deg
Mean anomaly: 20
5519 deg
Mean motion: 15
53262533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3436
Checksum: 288
Coasting Arc #4 (Orbit 3447)
---------------------------------------
Vector Time (GMT): 2019/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2576009
44 A = 6790734
51 meter
Y = 6033961
30 meter E =
0011321
Z = 1740102
91 I = 51
34721
XDOT = -5147
088227 Wp = 94
26344
YDOT = -558
451845 meter/sec RA = 305
36559 deg
ZDOT = -5652
108243 TA = 66
57264
MA = 66
45365
Ha = 222
896 n
mi
Hp = 216
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8451474
53 X = -2651743
66
Y = 19796460
95 feet Y = 6004731
07 meter
Z = 5708999
03 Z = 1727406
13
XDOT = -16886
772397 XDOT = -5113
006872
YDOT = -1832
191091 feet/sec YDOT = -615
819510 meter/sec
ZDOT = -18543
662215 ZDOT = -5677
027420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20331861
66 X = -6197151
43
Y = 7113498
86 feet Y = 2168194
45 meter
Z = 5650972
78 Z = 1722416
50
XDOT = -9452
675146 XDOT = -2881
175384
YDOT = -12115
619714 feet/sec YDOT = -3692
840889 meter/sec
ZDOT = -18656
001839 ZDOT = -5686
349360
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 19034
53558055
00016717 00000-0 10270-3 0 9033
2 25544 51
6418 305
9106 0005242 345
7096 14
3907 15
53213627 34486
Satellite: ISS
Catalog Number: 25544
Epoch time: 19034
53558055 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 305
9106 deg
Eccentricity:
0005242
Arg of perigee: 345
7096 deg
Mean anomaly: 14
3907 deg
Mean motion: 15
53213627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3448
Checksum: 303
Coasting Arc #5 (Orbit 3462)
---------------------------------------
Vector Time (GMT): 2019/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3166789
67 A = 6791921
37 meter
Y = -5986944
84 meter E =
0015216
Z = -369383
99 I = 51
33264
XDOT = 4392
533463 Wp = 25
88821
YDOT = 1961
357353 meter/sec RA = 300
37790 deg
ZDOT = 5975
057208 TA = 330
11233
MA = 330
19913
Ha = 222
993 n
mi
Hp = 216
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10389729
89 X = 3235296
23
Y = -19642207
47 feet Y = -5951148
54 meter
Z = -1211889
72 Z = -353834
98
XDOT = 14411
199024 XDOT = 4341
251879
YDOT = 6434
899452 feet/sec YDOT = 2010
190983 meter/sec
ZDOT = 19603
206062 ZDOT = 5996
269328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21407332
18 X = 6524954
85
Y = -5971237
76 feet Y = -1820033
27 meter
Z = -1141019
99 Z = -347782
89
XDOT = 4720
275449 XDOT = 1438
739957
YDOT = 13229
423967 feet/sec YDOT = 4032
328425 meter/sec
ZDOT = 19698
653295 ZDOT = 6004
149524
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 19035
50067236
00016717 00000-0 10270-3 0 9048
2 25544 51
6415 301
1065 0005389 349
2115 10
8921 15
53220326 34636
Satellite: ISS
Catalog Number: 25544
Epoch time: 19035
50067236 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 301
1065 deg
Eccentricity:
0005389
Arg of perigee: 349
2115 deg
Mean anomaly: 10
8921 deg
Mean motion: 15
53220326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3463
Checksum: 278
Coasting Arc #6 (Orbit 3478)
---------------------------------------
Vector Time (GMT): 2019/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3619348
59 A = 6791510
44 meter
Y = 5647261
26 meter E =
0005612
Z = -1059347
48 I = 51
31541
XDOT = -3584
751798 Wp = 113
93725
YDOT = -3391
852277 meter/sec RA = 295
39093 deg
ZDOT = -5860
895978 TA = 77
59074
MA = 77
52793
Ha = 223
054 n
mi
Hp = 216
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11874503
26 X = -3677083
29
Y = 18527760
04 feet Y = 5606464
35 meter
Z = -3475549
48 Z = -1077068
73
XDOT = -11760
996714 XDOT = -3518
088572
YDOT = -11128
124270 feet/sec YDOT = -3431
566831 meter/sec
ZDOT = -19228
661344 ZDOT = -5878
146892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21523948
79 X = -6560499
59
Y = 4520456
07 feet Y = 1377835
01 meter
Z = -3556159
32 Z = -1083917
36
XDOT = 124
297956 XDOT = 37
886017
YDOT = -14527
992856 feet/sec YDOT = -4428
132222 meter/sec
ZDOT = -19306
074798 ZDOT = -5884
491599
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 19036
53010343
00016717 00000-0 10270-3 0 9050
2 25544 51
6416 295
9827 0005219 351
5812 8
5252 15
53205540 34794
Satellite: ISS
Catalog Number: 25544
Epoch time: 19036
53010343 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 295
9827 deg
Eccentricity:
0005219
Arg of perigee: 351
5812 deg
Mean anomaly: 8
5252 deg
Mean motion: 15
53205540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3479
Checksum: 298
Coasting Arc #7 (Orbit 3487)
---------------------------------------
Vector Time (GMT): 2019/037/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4325389
41 A = 6780314
15 meter
Y = 458145
62 meter E =
0003948
Z = 5198620
16 I = 51
26905
XDOT = -2085
918865 Wp = 40
23246
YDOT = 7298
922539 meter/sec RA = 292
59139 deg
ZDOT = 1094
794560 TA = 39
23832
MA = 39
20970
Ha = 222
872 n
mi
Hp = 216
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14190910
13 X = 4294693
53
Y = 1503102
43 feet Y = 506343
65 meter
Z = 17055840
42 Z = 5219556
12
XDOT = -6843
565831 XDOT = -2172
700200
YDOT = 23946
596257 feet/sec YDOT = 7275
111143 meter/sec
ZDOT = 3591
845670 ZDOT = 1084
451277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12280631
46 X = -3743136
47
Y = -7042640
60 feet Y = -2146596
86 meter
Z = 17150225
77 Z = 5227388
82
XDOT = 15411
237247 XDOT = 4697
345113
YDOT = -18262
087423 feet/sec YDOT = -5566
284246 meter/sec
ZDOT = 3544
333084 ZDOT = 1080
312724
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 19037
10915520
00016717 00000-0 10270-3 0 9066
2 25544 51
6400 293
0979 0005096 353
4285 6
6799 15
53241374 34882
Satellite: ISS
Catalog Number: 25544
Epoch time: 19037
10915520 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 293
0979 deg
Eccentricity:
0005096
Arg of perigee: 353
4285 deg
Mean anomaly: 6
6799 deg
Mean motion: 15
53241374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3488
Checksum: 322
Coasting Arc #8 (Orbit 3502)
---------------------------------------
Vector Time (GMT): 2019/038/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3866957
18 A = 6780114
72 meter
Y = -1815294
13 meter E =
0015120
Z = -5277409
33 I = 51
25646
XDOT = 2685
092876 Wp = 73
64123
YDOT = -7153
040650 meter/sec RA = 287
57486 deg
ZDOT = 498
367441 TA = 201
11459
MA = 201
17707
Ha = 223
185 n
mi
Hp = 215
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12686867
39 X = -3820736
61
Y = -5955689
39 feet Y = -1858278
92 meter
Z = -17314335
06 Z = -5296080
72
XDOT = 8809
359831 XDOT = 2762
459907
YDOT = -23467
981135 feet/sec YDOT = -7122
581461 meter/sec
ZDOT = 1635
063783 ZDOT = 511
598472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9289629
72 X = 2831479
14
Y = 10354381
57 feet Y = 3156015
50 meter
Z = -17398350
52 Z = -5303017
24
XDOT = -16433
258084 XDOT = -5008
857064
YDOT = 17562
967934 feet/sec YDOT = 5353
192626 meter/sec
ZDOT = 1695
563305 ZDOT = 516
807695
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 19038
07424398
00016717 00000-0 10270-3 0 9072
2 25544 51
6402 288
2936 0005248 358
1319 1
9813 15
53211806 35032
Satellite: ISS
Catalog Number: 25544
Epoch time: 19038
07424398 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 288
2936 deg
Eccentricity:
0005248
Arg of perigee: 358
1319 deg
Mean anomaly: 1
9813 deg
Mean motion: 15
53211806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3503
Checksum: 308
Coasting Arc #9 (Orbit 3518)
---------------------------------------
Vector Time (GMT): 2019/039/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3372517
32 A = 6781348
62 meter
Y = 3163172
53 meter E =
0010126
Z = 4958696
02 I = 51
25090
XDOT = -3186
582648 Wp = 31
71208
YDOT = 6660
288261 meter/sec RA = 282
55922 deg
ZDOT = -2070
954903 TA = 78
60519
MA = 78
49145
Ha = 223
171 n
mi
Hp = 215
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11064689
36 X = 3312809
16
Y = 10377862
61 feet Y = 3200552
79 meter
Z = 16268687
73 Z = 4974932
87
XDOT = -10454
667481 XDOT = -3250
763729
YDOT = 21851
339438 feet/sec YDOT = 6624
294699 meter/sec
ZDOT = -6794
471466 ZDOT = -2086
589997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6326809
44 X = -1928411
52
Y = -13701166
75 feet Y = -4176115
62 meter
Z = 16341575
67 Z = 4980912
26
XDOT = 16769
371731 XDOT = 5111
304504
YDOT = -15973
021022 feet/sec YDOT = -4868
576808 meter/sec
ZDOT = -6865
738728 ZDOT = -2092
677164
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 19039
10366930
00016717 00000-0 10270-3 0 9085
2 25544 51
6391 283
1694 0005260 2
2526 357
8649 15
53255718 35192
Satellite: ISS
Catalog Number: 25544
Epoch time: 19039
10366930 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 283
1694 deg
Eccentricity:
0005260
Arg of perigee: 2
2526 deg
Mean anomaly: 357
8649 deg
Mean motion: 15
53255718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3519
Checksum: 321
Coasting Arc #10 (Orbit 3527)
---------------------------------------
Vector Time (GMT): 2019/039/16:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2556072
11 A = 6784689
80 meter
Y = -4752930
81 meter E =
0007999
Z = -4116660
70 I = 51
25494
XDOT = 3956
100925 Wp = 70
72161
YDOT = -5376
897724 meter/sec RA = 279
47193 deg
ZDOT = 3760
165782 TA = 238
23445
MA = 238
31241
Ha = 223
253 n
mi
Hp = 215
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8386063
34 X = -2482737
50
Y = -15593605
03 feet Y = -4781104
80 meter
Z = -13506104
67 Z = -4128898
48
XDOT = 12979
333742 XDOT = 3997
668487
YDOT = -17640
740565 feet/sec YDOT = -5332
425203 meter/sec
ZDOT = 12336
501910 ZDOT = 3779
483893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13148223
94 X = -4007578
66
Y = -11795370
63 feet Y = -3595228
97 meter
Z = -13560784
58 Z = -4133327
14
XDOT = 5191
200095 XDOT = 1582
277789
YDOT = -20038
073472 feet/sec YDOT = -6107
604794 meter/sec
ZDOT = 12424
229677 ZDOT = 3786
905205
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 19039
68272204
00016717 00000-0 10270-3 0 9099
2 25544 51
6363 280
2834 0005134 4
6640 355
4559 15
53236639 35283
Satellite: ISS
Catalog Number: 25544
Epoch time: 19039
68272204 = yrday
fracday
Element set: 909
Inclination: 51
6363 deg
RA of node: 280
2834 deg
Eccentricity:
0005134
Arg of perigee: 4
6640 deg
Mean anomaly: 355
4559 deg
Mean motion: 15
53236639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3528
Checksum: 316
Coasting Arc #11 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2019/040/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3836973
08 A = 6780885
25 meter
Y = 2407063
82 meter E =
0009860
Z = 5044275
93 I = 51
24377
XDOT = -2125
331592 Wp = 29
69750
YDOT = 7148
805658 meter/sec RA = 275
48154 deg
ZDOT = -1784
737962 TA = 77
72194
MA = 77
61155
Ha = 223
232 n
mi
Hp = 215
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12588494
35 X = 3785269
61
Y = 7897191
01 feet Y = 2449682
75 meter
Z = 16549461
71 Z = 5062788
43
XDOT = -6972
872678 XDOT = -2196
444493
YDOT = 23454
086806 feet/sec YDOT = 7124
640990 meter/sec
ZDOT = -5855
439507 ZDOT = -1795
234988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1716114
34 X = 523071
65
Y = 14667259
90 feet Y = 4470580
82 meter
Z = 16632706
87 Z = 5069649
05
XDOT = -21519
601802 XDOT = -6559
174629
YDOT = 9249
259726 feet/sec YDOT = 2819
174365 meter/sec
ZDOT = -5903
557158 ZDOT = -1799
404222
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 19040
51912777
00016717 00000-0 10270-3 0 9101
2 25544 51
6411 276
1240 0005503 4
6478 355
4725 15
53284242 35414
Satellite: ISS
Catalog Number: 25544
Epoch time: 19040
51912777 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 276
1240 deg
Eccentricity:
0005503
Arg of perigee: 4
6478 deg
Mean anomaly: 355
4725 deg
Mean motion: 15
53284242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 289
Coasting Arc #12 (Orbit 3555)
---------------------------------------
Vector Time (GMT): 2019/041/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3547858
44 A = 6783385
50 meter
Y = -3690386
36 meter E =
0009941
Z = -4457822
14 I = 51
24947
XDOT = 2641
557074 Wp = 77
14787
YDOT = -6426
181852 meter/sec RA = 270
46746 deg
ZDOT = 3225
816390 TA = 225
49305
MA = 225
57434
Ha = 223
445 n
mi
Hp = 215
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11639955
50 X = -3484674
52
Y = -12107566
80 feet Y = -3729707
97 meter
Z = -14625400
71 Z = -4474902
36
XDOT = 8666
525833 XDOT = 2697
551143
YDOT = -21083
273792 feet/sec YDOT = -6396
328845 meter/sec
ZDOT = 10583
387106 ZDOT = 3238
784260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1858744
59 X = 566545
35
Y = -16624641
07 feet Y = -5067190
60 meter
Z = -14702056
37 Z = -4481186
78
XDOT = 20463
848059 XDOT = 6237
380888
YDOT = -7099
900617 feet/sec YDOT = -2164
049708 meter/sec
ZDOT = 10642
557001 ZDOT = 3243
851374
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 19041
48421202
00016717 00000-0 10270-3 0 9117
2 25544 51
6408 271
3190 0005580 8
7638 351
3611 15
53250463 35562
Satellite: ISS
Catalog Number: 25544
Epoch time: 19041
48421202 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 271
3190 deg
Eccentricity:
0005580
Arg of perigee: 8
7638 deg
Mean anomaly: 351
3611 deg
Mean motion: 15
53250463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 283
Coasting Arc #13 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2019/042/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3215734
21 A = 6786501
49 meter
Y = 4825750
31 meter E =
0014697
Z = 3519534
67 I = 51
26035
XDOT = -3162
586316 Wp = 65
70892
YDOT = 5375
272197 meter/sec RA = 265
46020 deg
ZDOT = -4459
901746 TA = 72
59510
MA = 72
43445
Ha = 223
559 n
mi
Hp = 215
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10550309
09 X = 3144436
58
Y = 15832514
15 feet Y = 4861312
42 meter
Z = 11547029
75 Z = 3534981
90
XDOT = -10375
939356 XDOT = -3200
795625
YDOT = 17635
407470 feet/sec YDOT = 5339
692087 meter/sec
ZDOT = -14632
223575 ZDOT = -4475
357277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5085560
29 X = -1550078
78
Y = 18289672
59 feet Y = 5574692
21 meter
Z = 11616211
76 Z = 3540621
34
XDOT = -18719
451567 XDOT = -5705
688838
YDOT = 4175
751603 feet/sec YDOT = 1272
769088 meter/sec
ZDOT = -14702
493611 ZDOT = -4481
320053
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 19042
51363275
00016717 00000-0 10270-3 0 9128
2 25544 51
6403 266
1940 0005711 12
9840 347
1458 15
53275939 35725
Satellite: ISS
Catalog Number: 25544
Epoch time: 19042
51363275 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 266
1940 deg
Eccentricity:
0005711
Arg of perigee: 12
9840 deg
Mean anomaly: 347
1458 deg
Mean motion: 15
53275939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 307
Coasting Arc #14 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2019/043/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2875919
92 A = 6789523
17 meter
Y = -5672968
68 meter E =
0010839
Z = -2364300
11 I = 51
27347
XDOT = 3667
449275 Wp = 30
65233
YDOT = -4082
152028 meter/sec RA = 260
46027 deg
ZDOT = 5353
798525 TA = 302
82013
MA = 302
92446
Ha = 223
625 n
mi
Hp = 215
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9435432
82 X = -2800785
12
Y = -18612101
98 feet Y = -5704709
20 meter
Z = -7756890
13 Z = -2378087
41
XDOT = 12032
313895 XDOT = 3686
818994
YDOT = -13392
887230 feet/sec YDOT = -4041
031559 meter/sec
ZDOT = 17564
955790 ZDOT = 5371
660604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7565322
46 X = 2305910
29
Y = -19422766
58 feet Y = -5920059
25 meter
Z = -7818510
82 Z = -2383082
10
XDOT = 16508
102382 XDOT = 5031
669606
YDOT = -646
979861 feet/sec YDOT = -197
199462 meter/sec
ZDOT = 17645
942878 ZDOT = 5378
483389
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 19043
47871464
00016717 00000-0 10270-3 0 9139
2 25544 51
6399 261
3895 0005639 14
8830 345
2487 15
53233033 35870
Satellite: ISS
Catalog Number: 25544
Epoch time: 19043
47871464 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 261
3895 deg
Eccentricity:
0005639
Arg of perigee: 14
8830 deg
Mean anomaly: 345
2487 deg
Mean motion: 15
53233033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 333
Coasting Arc #15 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2019/044/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2445482
82 A = 6791494
82 meter
Y = 6253725
84 meter E =
0013324
Z = 995435
52 I = 51
28725
XDOT = -4192
625614 Wp = 100
09667
YDOT = 2584
638482 meter/sec RA = 255
46629 deg
ZDOT = -5872
713112 TA = 69
07126
MA = 68
92871
Ha = 223
768 n
mi
Hp = 215
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8023237
60 X = 2370534
93
Y = 20517473
23 feet Y = 6280653
89 meter
Z = 3265864
57 Z = 1007132
48
XDOT = -13755
333378 XDOT = -4192
690120
YDOT = 8479
785046 feet/sec YDOT = 2537
753148 meter/sec
ZDOT = -19267
431469 ZDOT = -5893
079282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9566244
21 X = -2915791
24
Y = 19836398
06 feet Y = 6046134
13 meter
Z = 3318012
08 Z = 1011330
08
XDOT = -14043
621403 XDOT = -4280
495804
YDOT = -3499
265001 feet/sec YDOT = -1066
575972 meter/sec
ZDOT = -19359
563565 ZDOT = -5900
794975
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 19044
50813331
00016717 00000-0 10270-3 0 9144
2 25544 51
6406 256
2640 0005607 19
8365 340
3004 15
53234790 36034
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
50813331 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 256
2640 deg
Eccentricity:
0005607
Arg of perigee: 19
8365 deg
Mean anomaly: 340
3004 deg
Mean motion: 15
53234790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 282
Coasting Arc #16 (Orbit 3605)
---------------------------------------
Vector Time (GMT): 2019/044/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4438716
00 A = 6783115
62 meter
Y = 2374531
98 meter E =
0012985
Z = 4541860
35 I = 51
25755
XDOT = -605
657035 Wp = 51
09926
YDOT = 7007
211286 meter/sec RA = 254
52522 deg
ZDOT = -3057
603032 TA = 69
71142
MA = 69
57190
Ha = 223
669 n
mi
Hp = 215
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14562716
55 X = 4389771
85
Y = 7790459
25 feet Y = 2423895
20 meter
Z = 14901116
63 Z = 4563302
80
XDOT = -1987
063762 XDOT = -669
116674
YDOT = 22989
538339 feet/sec YDOT = 7000
083535 meter/sec
ZDOT = -10031
506012 ZDOT = -3060
699289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16234338
83 X = 4948226
48
Y = 2514963
09 feet Y = 766560
75 meter
Z = 14997614
77 Z = 4571272
98
XDOT = 6049
967383 XDOT = 1844
030058
YDOT = 21126
625386 feet/sec YDOT = 6439
395418 meter/sec
ZDOT = -10046
166119 ZDOT = -3062
071433
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 19044
70115064
00016717 00000-0 10270-3 0 9155
2 25544 51
6374 255
2977 0005221 25
0778 335
0627 15
53218925 36066
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
70115064 = yrday
fracday
Element set: 915
Inclination: 51
6374 deg
RA of node: 255
2977 deg
Eccentricity:
0005221
Arg of perigee: 25
0778 deg
Mean anomaly: 335
0627 deg
Mean motion: 15
53218925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3606
Checksum: 305
Coasting Arc #17 (Orbit 3620)
---------------------------------------
Vector Time (GMT): 2019/045/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4471355
34 A = 6786077
98 meter
Y = -3544166
95 meter E =
0008832
Z = -3677630
74 I = 51
27818
XDOT = 1373
372960 Wp = 66
38755
YDOT = -6187
434998 meter/sec RA = 249
51921 deg
ZDOT = 4304
820017 TA = 249
63241
MA = 249
72731
Ha = 223
733 n
mi
Hp = 214
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14669800
99 X = -4413527
51
Y = -11627844
33 feet Y = -3593845
43 meter
Z = -12065717
65 Z = -3699210
15
XDOT = 4505
816797 XDOT = 1421
550404
YDOT = -20299
983588 feet/sec YDOT = -6171
807607 meter/sec
ZDOT = 14123
425252 ZDOT = 4311
608264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17736580
07 X = -5406109
60
Y = -5785586
79 feet Y = -1763446
85 meter
Z = -12162733
26 Z = -3707201
10
XDOT = -3396
028266 XDOT = -1035
109415
YDOT = -19265
403403 feet/sec YDOT = -5872
094957 meter/sec
ZDOT = 14154
650520 ZDOT = 4314
337479
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 19045
66622783
00016717 00000-0 10270-3 0 9163
2 25544 51
6379 250
4941 0005270 28
0900 332
0536 15
53244968 36212
Satellite: ISS
Catalog Number: 25544
Epoch time: 19045
66622783 = yrday
fracday
Element set: 916
Inclination: 51
6379 deg
RA of node: 250
4941 deg
Eccentricity:
0005270
Arg of perigee: 28
0900 deg
Mean anomaly: 332
0536 deg
Mean motion: 15
53244968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3621
Checksum: 309
Coasting Arc #18 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2019/046/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4384152
92 A = 6789187
03 meter
Y = 4530305
99 meter E =
0015972
Z = 2507440
06 I = 51
30055
XDOT = -2242
460011 Wp = 86
27814
YDOT = 5101
606825 meter/sec RA = 244
51988 deg
ZDOT = -5266
335116 TA = 65
45698
MA = 65
29057
Ha = 223
790 n
mi
Hp = 214
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14383703
81 X = 4320988
39
Y = 14863208
62 feet Y = 4578979
45 meter
Z = 8226509
38 Z = 2528582
88
XDOT = -7357
152266 XDOT = -2273
760486
YDOT = 16737
555201 feet/sec YDOT = 5076
355111 meter/sec
ZDOT = -17278
002349 ZDOT = -5277
303923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18775637
81 X = 5722814
40
Y = 8585439
31 feet Y = 2616841
90 meter
Z = 8321479
40 Z = 2536386
92
XDOT = 15
322475 XDOT = 4
670290
YDOT = 16856
417519 feet/sec YDOT = 5137
836060 meter/sec
ZDOT = -17327
977963 ZDOT = -5281
567683
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 19046
69564348
00016717 00000-0 10270-3 0 9170
2 25544 51
6373 245
3686 0005175 31
3196 328
8263 15
53241803 36375
Satellite: ISS
Catalog Number: 25544
Epoch time: 19046
69564348 = yrday
fracday
Element set: 917
Inclination: 51
6373 deg
RA of node: 245
3686 deg
Eccentricity:
0005175
Arg of perigee: 31
3196 deg
Mean anomaly: 328
8263 deg
Mean motion: 15
53241803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 329
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