[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 8th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14730 1961 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 995 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
131/09:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
3
134/06:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
2
134/18:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
1
Coasting Arc #1 (Orbit 908)
---------------------------------------
Vector Time (GMT): 2019/128/13:13:49
819
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4123635
83 A = 6784209
05 meter
Y = 2648563
30 meter E =
0009818
Z = -4700513
28 I = 51
51060
XDOT = -5825
953188 Wp = 106
31305
YDOT = -4106
556706 meter/sec RA = 196
98317 deg
ZDOT = 2799
233984 TA = 191
51631
MA = 191
53879
Ha = 223
033 n
mi
Hp = 217
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13528988
96 X = -4130113
55
Y = 8689512
15 feet Y = 2602414
15 meter
Z = -15421631
48 Z = -4720560
11
XDOT = -19114
019645 XDOT = -5793
196811
YDOT = -13472
955071 feet/sec YDOT = -4171
523704 meter/sec
ZDOT = 9183
838529 ZDOT = 2771
012470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1826873
00 X = 556830
89
Y = 15886809
36 feet Y = 4842299
49 meter
Z = -15512566
02 Z = -4728230
12
XDOT = -19425
015683 XDOT = -5920
744780
YDOT = 11069
906161 feet/sec YDOT = 3374
107398 meter/sec
ZDOT = 9056
417318 ZDOT = 2760
395999
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19128
56248153
00016717 00000-0 10270-3 0 9002
2 25544 51
6390 198
1271 0001239 315
7000 44
4052 15
52641749 9097
Satellite: ISS
Catalog Number: 25544
Epoch time: 19128
56248153 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 198
1271 deg
Eccentricity:
0001239
Arg of perigee: 315
7000 deg
Mean anomaly: 44
4052 deg
Mean motion: 15
52641749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 909
Checksum: 293
Coasting Arc #2 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2019/129/13:13:49
819
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5029006
08 A = 6786677
41 meter
Y = -2176374
49 meter E =
0010093
Z = 3997885
35 I = 51
55075
XDOT = 4996
710763 Wp = 72
51387
YDOT = 4268
634575 meter/sec RA = 191
99845 deg
ZDOT = -3950
469756 TA = 58
67197
MA = 58
57322
Ha = 222
873 n
mi
Hp = 217
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16499363
78 X = 5033549
48
Y = -7140336
26 feet Y = -2120111
62 meter
Z = 13116421
77 Z = 4022325
42
XDOT = 16393
408014 XDOT = 4967
795663
YDOT = 14004
706610 feet/sec YDOT = 4324
350008 meter/sec
ZDOT = -12960
858779 ZDOT = -3926
267201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 578837
36 X = 176429
63
Y = -17887410
70 feet Y = -5452082
78 meter
Z = 13227222
41 Z = 4031657
39
XDOT = 18409
073382 XDOT = 5611
085567
YDOT = -8934
650484 feet/sec YDOT = -2723
281467 meter/sec
ZDOT = -12851
619117 ZDOT = -3917
173507
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19129
59229738
00016717 00000-0 10270-3 0 9015
2 25544 51
6384 193
0051 0001324 314
4746 45
6297 15
52673873 9253
Satellite: ISS
Catalog Number: 25544
Epoch time: 19129
59229738 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 193
0051 deg
Eccentricity:
0001324
Arg of perigee: 314
4746 deg
Mean anomaly: 45
6297 deg
Mean motion: 15
52673873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 925
Checksum: 322
Coasting Arc #3 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2019/130/13:13:49
819
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5772665
72 A = 6789355
37 meter
Y = 1769785
25 meter E =
0004286
Z = -3105649
77 I = 51
59354
XDOT = -3963
513197 Wp = 62
34794
YDOT = -4383
259531 meter/sec RA = 187
02050 deg
ZDOT = 4876
495585 TA = 261
94078
MA = 261
98941
Ha = 223
036 n
mi
Hp = 217
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18939191
99 X = -5776941
34
Y = 5806382
05 feet Y = 1705207
64 meter
Z = -10189139
65 Z = -3133701
56
XDOT = -13003
652220 XDOT = -3937
891175
YDOT = -14380
772739 feet/sec YDOT = -4427
439491 meter/sec
ZDOT = 15999
001263 ZDOT = 4857
304068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2501052
63 X = -762320
84
Y = 19584298
34 feet Y = 5969294
13 meter
Z = -10316279
69 Z = -3144402
05
XDOT = -17081
067566 XDOT = -5206
309394
YDOT = 6188
572361 feet/sec YDOT = 1886
276856 meter/sec
ZDOT = 15912
436871 ZDOT = 4850
110758
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19130
55774931
00016717 00000-0 10270-3 0 9024
2 25544 51
6393 188
2026 0001166 327
4361 32
6719 15
52680578 9404
Satellite: ISS
Catalog Number: 25544
Epoch time: 19130
55774931 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 188
2026 deg
Eccentricity:
0001166
Arg of perigee: 327
4361 deg
Mean anomaly: 32
6719 deg
Mean motion: 15
52680578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 940
Checksum: 312
Coasting Arc #4 (Orbit 952)
---------------------------------------
Vector Time (GMT): 2019/131/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -345209
03 A = 6781649
54 meter
Y = 4205761
56 meter E =
0014021
Z = -5320895
85 I = 51
59597
XDOT = -7639
787278 Wp = 87
24471
YDOT = -482
136462 meter/sec RA = 182
92586 deg
ZDOT = 115
483857 TA = 183
85283
MA = 183
86364
Ha = 223
032 n
mi
Hp = 217
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1132575
55 X = -366367
38
Y = 13798430
30 feet Y = 4201783
29 meter
Z = -17457007
38 Z = -5322623
82
XDOT = -25064
918891 XDOT = -7634
389045
YDOT = -1581
812540 feet/sec YDOT = -567
539736 meter/sec
ZDOT = 378
884045 ZDOT = 78
385624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4710
21 X = 1435
67
Y = 13834567
07 feet Y = 4216776
04 meter
Z = -17465143
71 Z = -5323375
80
XDOT = -24106
459583 XDOT = -7347
648881
YDOT = 270
676271 feet/sec YDOT = 82
502127 meter/sec
ZDOT = 210
930983 ZDOT = 64
291764
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19131
39447105
00016717 00000-0 10270-3 0 9038
2 25544 51
6404 184
0391 0001262 316
9658 43
1395 15
52655989 9534
Satellite: ISS
Catalog Number: 25544
Epoch time: 19131
39447105 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 184
0391 deg
Eccentricity:
0001262
Arg of perigee: 316
9658 deg
Mean anomaly: 43
1395 deg
Mean motion: 15
52655989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 953
Checksum: 316
Coasting Arc #5 (Orbit 968)
---------------------------------------
Vector Time (GMT): 2019/132/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1539535
98 A = 6782229
94 meter
Y = -4134645
21 meter E =
0004653
Z = 5149289
75 I = 51
63174
XDOT = 7465
112983 Wp = 39
24392
YDOT = 914
518780 meter/sec RA = 177
94006 deg
ZDOT = -1493
341295 TA = 65
16323
MA = 65
11484
Ha = 222
943 n
mi
Hp = 217
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5050971
07 X = 1560643
91
Y = -13565108
97 feet Y = -4117311
31 meter
Z = 16893995
24 Z = 5156819
29
XDOT = 24491
840497 XDOT = 7461
585586
YDOT = 3000
389699 feet/sec YDOT = 997
979259 meter/sec
ZDOT = -4899
413699 ZDOT = -1457
087031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3684364
40 X = 1122994
27
Y = -13956587
08 feet Y = -4253967
74 meter
Z = 16928399
25 Z = 5159776
09
XDOT = 23677
576805 XDOT = 7216
925410
YDOT = 490
066442 feet/sec YDOT = 149
372251 meter/sec
ZDOT = -4735
289621 ZDOT = -1443
316277
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19132
42428106
00016717 00000-0 10270-3 0 9044
2 25544 51
6405 178
9166 0001306 320
5547 39
5510 15
52690087 9697
Satellite: ISS
Catalog Number: 25544
Epoch time: 19132
42428106 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 178
9166 deg
Eccentricity:
0001306
Arg of perigee: 320
5547 deg
Mean anomaly: 39
5510 deg
Mean motion: 15
52690087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 969
Checksum: 305
Coasting Arc #6 (Orbit 983)
---------------------------------------
Vector Time (GMT): 2019/133/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2664165
93 A = 6784044
66 meter
Y = 4089821
12 meter E =
0010051
Z = -4721148
11 I = 51
67056
XDOT = -7004
525951 Wp = 105
19530
YDOT = -1352
372733 meter/sec RA = 172
96033 deg
ZDOT = 2783
536539 TA = 192
39718
MA = 192
42193
Ha = 223
058 n
mi
Hp = 217
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8740701
88 X = -2686768
68
Y = 13418048
29 feet Y = 4059902
34 meter
Z = -15489331
06 Z = -4734144
43
XDOT = -22980
728185 XDOT = -7002
403664
YDOT = -4436
918414 feet/sec YDOT = -1430
690479 meter/sec
ZDOT = 9132
337725 ZDOT = 2749
516166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7137045
39 X = -2175371
44
Y = 14271304
03 feet Y = 4349893
47 meter
Z = -15548496
08 Z = -4739181
61
XDOT = -22345
122018 XDOT = -6810
793191
YDOT = -1401
366486 feet/sec YDOT = -427
136505 meter/sec
ZDOT = 8978
342088 ZDOT = 2736
598668
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19133
38972831
00016717 00000-0 10270-3 0 9050
2 25544 51
6400 174
1156 0001215 327
0728 33
0348 15
52683122 9848
Satellite: ISS
Catalog Number: 25544
Epoch time: 19133
38972831 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 174
1156 deg
Eccentricity:
0001215
Arg of perigee: 327
0728 deg
Mean anomaly: 33
0348 deg
Mean motion: 15
52683122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 984
Checksum: 292
Coasting Arc #7 (Orbit 997)
---------------------------------------
Vector Time (GMT): 2019/134/06:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6177190
49 A = 6790648
15 meter
Y = 904988
06 meter E =
0004038
Z = -2671349
79 I = 51
72138
XDOT = -2948
995817 Wp = 120
21558
YDOT = 4785
490476 meter/sec RA = 168
60014 deg
ZDOT = -5205
872459 TA = 89
85888
MA = 89
81261
Ha = 223
166 n
mi
Hp = 217
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20266373
00 X = 6179587
57
Y = 2969120
92 feet Y = 974079
20 meter
Z = -8764270
98 Z = -2641337
28
XDOT = -9675
183127 XDOT = -2977
001957
YDOT = 15700
428072 feet/sec YDOT = 4752
356278 meter/sec
ZDOT = -17079
634052 ZDOT = -5220
265572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15147133
72 X = 4616846
36
Y = 13873332
80 feet Y = 4228591
84 meter
Z = -8628382
02 Z = -2629930
84
XDOT = -15716
851682 XDOT = -4790
496393
YDOT = 6512
941474 feet/sec YDOT = 1985
144561 meter/sec
ZDOT = -17145
183126 ZDOT = -5225
851817
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19134
29081054
00016717 00000-0 10270-3 0 9060
2 25544 51
6400 169
6311 0001124 332
1176 27
9915 15
52668252 9987
Satellite: ISS
Catalog Number: 25544
Epoch time: 19134
29081054 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 169
6311 deg
Eccentricity:
0001124
Arg of perigee: 332
1176 deg
Mean anomaly: 27
9915 deg
Mean motion: 15
52668252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 998
Checksum: 301
Coasting Arc #8 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2019/134/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1256493
13 A = 6781568
88 meter
Y = -4014504
44 meter E =
0002156
Z = 5317611
17 I = 51
70638
XDOT = 7395
831980 Wp = 60
79239
YDOT = -2012
126801 meter/sec RA = 166
13486 deg
ZDOT = 229
466538 TA = 27
02810
MA = 27
01688
Ha = 223
185 n
mi
Hp = 217
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4122352
78 X = -1237338
63
Y = -13170946
31 feet Y = -4028448
45 meter
Z = 17446230
88 Z = 5311553
98
XDOT = 24264
540617 XDOT = 7416
667851
YDOT = -6601
465884 feet/sec YDOT = -1929
304933 meter/sec
ZDOT = 752
842973 ZDOT = 265
443590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4355207
91 X = -1327467
37
Y = 13131879
45 feet Y = 4002596
86 meter
Z = 17419084
28 Z = 5309336
89
XDOT = -22518
635888 XDOT = -6863
680219
YDOT = -8679
178420 feet/sec YDOT = -2645
413582 meter/sec
ZDOT = 915
973073 ZDOT = 279
188593
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19134
80571250
00016717 00000-0 10270-3 0 9070
2 25544 51
6389 167
0742 0001730 340
3656 19
7429 15
52688234 10062
Satellite: ISS
Catalog Number: 25544
Epoch time: 19134
80571250 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 167
0742 deg
Eccentricity:
0001730
Arg of perigee: 340
3656 deg
Mean anomaly: 19
7429 deg
Mean motion: 15
52688234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 306
Coasting Arc #9 (Orbit 1020)
---------------------------------------
Vector Time (GMT): 2019/135/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 100186
35 A = 6782040
04 meter
Y = 4326877
72 meter E =
0013726
Z = -5233449
72 I = 51
73916
XDOT = -7404
821318 Wp = 92
19547
YDOT = 1565
174977 meter/sec RA = 161
15609 deg
ZDOT = 1154
395323 TA = 188
86381
MA = 188
88807
Ha = 223
283 n
mi
Hp = 217
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 328695
37 X = 77216
05
Y = 14195793
04 feet Y = 4327869
78 meter
Z = -17170110
64 Z = -5233018
72
XDOT = -24294
033196 XDOT = -7427
380693
YDOT = 5135
088508 feet/sec YDOT = 1482
242909 meter/sec
ZDOT = 3787
386230 ZDOT = 1118
370257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7820721
35 X = 2383755
87
Y = -11854154
10 feet Y = -3613146
17 meter
Z = -17168477
75 Z = -5232952
02
XDOT = 21966
859007 XDOT = 6695
498625
YDOT = 9253
780867 feet/sec YDOT = 2820
552408 meter/sec
ZDOT = 3624
052334 ZDOT = 1104
611151
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 19135
77115525
00016717 00000-0 10270-3 0 9087
2 25544 51
6383 162
2717 0001720 348
1786 11
9325 15
52659963 10217
Satellite: ISS
Catalog Number: 25544
Epoch time: 19135
77115525 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 162
2717 deg
Eccentricity:
0001720
Arg of perigee: 348
1786 deg
Mean anomaly: 11
9325 deg
Mean motion: 15
52659963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1021
Checksum: 308
Coasting Arc #10 (Orbit 1036)
---------------------------------------
Vector Time (GMT): 2019/136/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1024481
51 A = 6783599
38 meter
Y = -4627744
20 meter E =
0007765
Z = 4850032
20 I = 51
77572
XDOT = 7179
755582 Wp = 48
19849
YDOT = -1026
708106 meter/sec RA = 156
18272 deg
ZDOT = -2488
628213 TA = 66
24381
MA = 66
16239
Ha = 223
269 n
mi
Hp = 217
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3361159
83 X = 1052594
97
Y = -15182887
81 feet Y = -4616130
75 meter
Z = 15912179
13 Z = 4855076
92
XDOT = 23555
628550 XDOT = 7202
791484
YDOT = -3368
464915 feet/sec YDOT = -946
290143 meter/sec
ZDOT = -8164
790726 ZDOT = -2453
695162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11228806
92 X = -3422540
35
Y = 10723445
99 feet Y = 3268506
34 meter
Z = 15935385
90 Z = 4857105
62
XDOT = -20635
300170 XDOT = -6289
639492
YDOT = -9672
886991 feet/sec YDOT = -2948
295955 meter/sec
ZDOT = -8006
425213 ZDOT = -2440
358405
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 19136
80095878
00016717 00000-0 10270-3 0 9091
2 25544 51
6384 157
1502 0001712 349
8953 10
2164 15
52661831 10375
Satellite: ISS
Catalog Number: 25544
Epoch time: 19136
80095878 = yrday
fracday
Element set: 909
Inclination: 51
6384 deg
RA of node: 157
1502 deg
Eccentricity:
0001712
Arg of perigee: 349
8953 deg
Mean anomaly: 10
2164 deg
Mean motion: 15
52661831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1037
Checksum: 310
Coasting Arc #11 (Orbit 1051)
---------------------------------------
Vector Time (GMT): 2019/137/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2031039
97 A = 6785945
02 meter
Y = 4910133
01 meter E =
0007501
Z = -4227859
58 I = 51
81421
XDOT = -6708
111883 Wp = 98
35756
YDOT = 386
690912 meter/sec RA = 151
21353 deg
ZDOT = 3676
145121 TA = 209
25716
MA = 209
29919
Ha = 223
308 n
mi
Hp = 216
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6663516
96 X = -2065258
55
Y = 16109360
27 feet Y = 4887229
45 meter
Z = -13870930
39 Z = -4237808
59
XDOT = -22008
241087 XDOT = -6729
794412
YDOT = 1268
670971 feet/sec YDOT = 311
554635 meter/sec
ZDOT = 12060
843574 ZDOT = 3643
506379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14324123
66 X = 4365992
89
Y = -9872694
45 feet Y = -3009197
27 meter
Z = -13916394
73 Z = -4241717
11
XDOT = 18451
557266 XDOT = 5624
034655
YDOT = 9999
607881 feet/sec YDOT = 3047
880482 meter/sec
ZDOT = 11912
903761 ZDOT = 3631
053066
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 19137
76639619
00016717 00000-0 10270-3 0 9106
2 25544 51
6388 152
3470 0001753 353
9031 6
2100 15
52676982 10523
Satellite: ISS
Catalog Number: 25544
Epoch time: 19137
76639619 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 152
3470 deg
Eccentricity:
0001753
Arg of perigee: 353
9031 deg
Mean anomaly: 6
2100 deg
Mean motion: 15
52676982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1052
Checksum: 303
Coasting Arc #12 (Orbit 1067)
---------------------------------------
Vector Time (GMT): 2019/138/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2927185
68 A = 6788766
67 meter
Y = -5121268
31 meter E =
0012585
Z = 3351157
81 I = 51
85197
XDOT = 6055
506762 Wp = 82
93198
YDOT = 382
679884 meter/sec RA = 146
25283 deg
ZDOT = -4687
994147 TA = 58
15676
MA = 58
03431
Ha = 223
367 n
mi
Hp = 216
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9603627
56 X = 2967957
24
Y = -16802061
39 feet Y = -5088306
80 meter
Z = 10994612
24 Z = 3365475
81
XDOT = 19867
148168 XDOT = 6073
549560
YDOT = 1255
511432 feet/sec YDOT = 450
498106 meter/sec
ZDOT = -15380
558226 ZDOT = -4658
534357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17024728
16 X = -5189137
14
Y = 9124551
04 feet Y = 2781163
16 meter
Z = 11059910
79 Z = 3371060
81
XDOT = -15554
545098 XDOT = -4741
025346
YDOT = -10475
305708 feet/sec YDOT = -3192
873180 meter/sec
ZDOT = -15247
067168 ZDOT = -4647
306073
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 19138
79619441
00016717 00000-0 10270-3 0 9112
2 25544 51
6385 147
2249 0001796 359
6919
4232 15
52668656 10680
Satellite: ISS
Catalog Number: 25544
Epoch time: 19138
79619441 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 147
2249 deg
Eccentricity:
0001796
Arg of perigee: 359
6919 deg
Mean anomaly:
4232 deg
Mean motion: 15
52668656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1068
Checksum: 336
Coasting Arc #13 (Orbit 1082)
---------------------------------------
Vector Time (GMT): 2019/139/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3630560
88 A = 6791195
85 meter
Y = 5244745
03 meter E =
0007094
Z = -2323954
20 I = 51
88761
XDOT = -5262
573847 Wp = 35
70643
YDOT = -1242
644326 meter/sec RA = 141
29857 deg
ZDOT = 5430
900617 TA = 298
50355
MA = 298
57497
Ha = 223
363 n
mi
Hp = 216
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11911288
96 X = -3677650
61
Y = 17207168
74 feet Y = 5203882
53 meter
Z = -7624521
64 Z = -2341704
17
XDOT = -17265
662228 XDOT = -5274
667849
YDOT = -4076
917081 feet/sec YDOT = -1301
562350 meter/sec
ZDOT = 17817
915409 ZDOT = 5405
307064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19067455
96 X = 5811760
58
Y = -8553222
57 feet Y = -2607022
24 meter
Z = -7705407
08 Z = -2348608
08
XDOT = 12121
514007 XDOT = 3694
637469
YDOT = 11115
610975 feet/sec YDOT = 3388
038225 meter/sec
ZDOT = 17702
001762 ZDOT = 5395
570137
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 19139
76162891
00016717 00000-0 10270-3 0 9123
2 25544 51
6388 142
4224 0001784
7020 359
4134 15
52682954 10839
Satellite: ISS
Catalog Number: 25544
Epoch time: 19139
76162891 = yrday
fracday
Element set: 912
Inclination: 51
6388 deg
RA of node: 142
4224 deg
Eccentricity:
0001784
Arg of perigee:
7020 deg
Mean anomaly: 359
4134 deg
Mean motion: 15
52682954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1083
Checksum: 306
Coasting Arc #14 (Orbit 1098)
---------------------------------------
Vector Time (GMT): 2019/140/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4184854
22 A = 6793026
52 meter
Y = -5221904
50 meter E =
0012937
Z = 1135760
44 I = 51
91955
XDOT = 4373
080019 Wp = 115
96761
YDOT = 2212
271080 meter/sec RA = 136
35098 deg
ZDOT = -5895
261808 TA = 51
75896
MA = 51
64260
Ha = 223
442 n
mi
Hp = 216
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13729836
68 X = 4237419
05
Y = -17132232
62 feet Y = -5174812
77 meter
Z = 3726248
17 Z = 1156216
15
XDOT = 14347
375392 XDOT = 4376
653032
YDOT = 7258
107218 feet/sec YDOT = 2261
194671 meter/sec
ZDOT = -19341
410130 ZDOT = -5874
009777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20472887
20 X = -6240136
02
Y = 7885407
39 feet Y = 2403472
17 meter
Z = 3819420
81 Z = 1164159
46
XDOT = -8268
256122 XDOT = -2520
164466
YDOT = -12073
027131 feet/sec YDOT = -3679
858670 meter/sec
ZDOT = -19245
245719 ZDOT = -5865
950895
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 19140
79142412
00016717 00000-0 10270-3 0 9136
2 25544 51
6396 137
3001 0001713 3
5099 356
6064 15
52660987 10993
Satellite: ISS
Catalog Number: 25544
Epoch time: 19140
79142412 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 137
3001 deg
Eccentricity:
0001713
Arg of perigee: 3
5099 deg
Mean anomaly: 356
6064 deg
Mean motion: 15
52660987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1099
Checksum: 303
Coasting Arc #15 (Orbit 1114)
---------------------------------------
Vector Time (GMT): 2019/141/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4534730
97 A = 6793539
21 meter
Y = 5048306
66 meter E =
0013728
Z = 79572
95 I = 51
94572
XDOT = -3464
629874 Wp = 41
15740
YDOT = -3216
468447 meter/sec RA = 131
40638 deg
ZDOT = 6037
154423 TA = 319
69581
MA = 319
79748
Ha = 223
470 n
mi
Hp = 216
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14877726
29 X = -4591232
07
Y = 16562685
89 feet Y = 4997280
20 meter
Z = 261066
09 Z = 57408
19
XDOT = -11366
895911 XDOT = -3457
730306
YDOT = -10552
718001 feet/sec YDOT = -3255
174619 meter/sec
ZDOT = 19806
937084 ZDOT = 6020
340712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21080116
30 X = 6425219
45
Y = -7165229
40 feet Y = -2183961
92 meter
Z = 160135
82 Z = 48809
40
XDOT = 4344
314585 XDOT = 1324
147086
YDOT = 13291
292508 feet/sec YDOT = 4051
185956 meter/sec
ZDOT = 19730
973070 ZDOT = 6014
000592
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 19141
82121546
00016717 00000-0 10270-3 0 9147
2 25544 51
6406 132
1772 0001932 6
1875 353
9300 15
52681990 11156
Satellite: ISS
Catalog Number: 25544
Epoch time: 19141
82121546 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 132
1772 deg
Eccentricity:
0001932
Arg of perigee: 6
1875 deg
Mean anomaly: 353
9300 deg
Mean motion: 15
52681990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1115
Checksum: 287
Coasting Arc #16 (Orbit 1129)
---------------------------------------
Vector Time (GMT): 2019/142/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4744982
41 A = 6792896
05 meter
Y = -4672185
08 meter E =
0007806
Z = -1328418
81 I = 51
96452
XDOT = 2550
656857 Wp = 133
02369
YDOT = 4245
378194 meter/sec RA = 126
46485 deg
ZDOT = -5847
558570 TA = 61
35812
MA = 61
27964
Ha = 223
538 n
mi
Hp = 216
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15567527
60 X = 4803328
21
Y = -15328691
21 feet Y = -4618796
95 meter
Z = -4358329
42 Z = -1305228
26
XDOT = 8368
296776 XDOT = 2531
398588
YDOT = 13928
406148 feet/sec YDOT = 4273
794537 meter/sec
ZDOT = -19184
903446 ZDOT = -5835
214571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21000240
89 X = -6400873
42
Y = 6100463
89 feet Y = 1859421
39 meter
Z = -4252757
71 Z = -1296240
55
XDOT = -431
940984 XDOT = -131
655612
YDOT = -14759
456697 feet/sec YDOT = -4498
682401 meter/sec
ZDOT = -19129
293661 ZDOT = -5830
608708
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 19142
78664456
00016717 00000-0 10270-3 0 9156
2 25544 51
6406 127
3760 0001756 9
5587 350
5598 15
52656625 11306
Satellite: ISS
Catalog Number: 25544
Epoch time: 19142
78664456 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 127
3760 deg
Eccentricity:
0001756
Arg of perigee: 9
5587 deg
Mean anomaly: 350
5598 deg
Mean motion: 15
52656625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1130
Checksum: 326
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