[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 29th 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
154/16:09:12
500 -0
0 -0
0 0
0
N/A 0
0 -0
0 227
4
000/00:00:25
000 0
0 0
0 218
6
155/08:40:30
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 218
3
157/09:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
7
000/00:00:00
000 0
0 0
0 218
1
161/12:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
0
000/00:00:00
000 0
0 0
0 217
6
Coasting Arc #1 (Orbit 1234)
---------------------------------------
Vector Time (GMT): 2019/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4162228
57 A = 6786388
69 meter
Y = 1103738
75 meter E =
0005486
Z = 5242906
37 I = 52
00566
XDOT = -513
718113 Wp = 17
82321
YDOT = -7555
951762 meter/sec RA = 93
14639 deg
ZDOT = 1187
604847 TA = 60
86716
MA = 60
81226
Ha = 226
919 n
mi
Hp = 219
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13655605
54 X = -4199728
90
Y = 3621190
12 feet Y = 1056983
72 meter
Z = 17201136
38 Z = 5222596
64
XDOT = -1685
426880 XDOT = -434
955901
YDOT = -24789
867986 feet/sec YDOT = -7561
256221 meter/sec
ZDOT = 3896
341363 ZDOT = 1185
300101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2331149
47 X = -710534
36
Y = 14047049
74 feet Y = 4281540
76 meter
Z = 17108881
00 Z = 5214786
93
XDOT = -22294
335384 XDOT = -6795
313425
YDOT = -8414
517571 feet/sec YDOT = -2564
744956 meter/sec
ZDOT = 3886
631604 ZDOT = 1184
645313
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 19149
55037642
00016717 00000-0 10270-3 0 9003
2 25544 51
6403 93
7954 0007624 347
8071 12
2894 15
51185904 12353
Satellite: ISS
Catalog Number: 25544
Epoch time: 19149
55037642 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 93
7954 deg
Eccentricity:
0007624
Arg of perigee: 347
8071 deg
Mean anomaly: 12
2894 deg
Mean motion: 15
51185904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1235
Checksum: 310
Coasting Arc #2 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2019/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4159351
97 A = 6786086
35 meter
Y = -562214
54 meter E =
0016002
Z = -5344655
11 I = 52
00509
XDOT = 535
040278 Wp = 58
77296
YDOT = 7625
096168 meter/sec RA = 88
20294 deg
ZDOT = -378
494985 TA = 207
58651
MA = 207
67152
Ha = 227
002 n
mi
Hp = 219
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13646167
88 X = 4191291
37
Y = -1844535
89 feet Y = -515522
71 meter
Z = -17534957
70 Z = -5324372
75
XDOT = 1755
381490 XDOT = 451
573052
YDOT = 25016
719712 feet/sec YDOT = 7630
612701 meter/sec
ZDOT = -1241
781447 ZDOT = -376
098002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3719618
97 X = 1133739
86
Y = -13379291
25 feet Y = -4078007
97 meter
Z = -17442876
83 Z = -5316588
86
XDOT = 22716
476840 XDOT = 6923
982141
YDOT = 7952
296394 feet/sec YDOT = 2423
859941 meter/sec
ZDOT = -1231
679251 ZDOT = -375
415836
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 19150
51675975
00016717 00000-0 10270-3 0 9019
2 25544 51
6404 88
9994 0007611 351
9784 8
1244 15
51152049 12501
Satellite: ISS
Catalog Number: 25544
Epoch time: 19150
51675975 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 88
9994 deg
Eccentricity:
0007611
Arg of perigee: 351
9784 deg
Mean anomaly: 8
1244 deg
Mean motion: 15
51152049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1250
Checksum: 314
Coasting Arc #3 (Orbit 1265)
---------------------------------------
Vector Time (GMT): 2019/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4196692
31 A = 6786014
14 meter
Y = -23346
64 meter E =
0008760
Z = 5331660
43 I = 52
00401
XDOT = -544
933776 Wp = 11
86898
YDOT = -7632
111824 meter/sec RA = 83
26006 deg
ZDOT = -453
881049 TA = 82
49008
MA = 82
39056
Ha = 227
148 n
mi
Hp = 218
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13768675
54 X = -4222017
95
Y = -76596
60 feet Y = -70419
15 meter
Z = 17492324
24 Z = 5311212
65
XDOT = -1787
840473 XDOT = -457
344089
YDOT = -25039
736956 feet/sec YDOT = -7637
715864 meter/sec
ZDOT = -1489
111054 ZDOT = -456
316218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5313945
95 X = -1619690
72
Y = 12828924
98 feet Y = 3910256
33 meter
Z = 17399550
66 Z = 5303383
04
XDOT = -22921
383839 XDOT = -6986
437794
YDOT = -7422
958797 feet/sec YDOT = -2262
517841 meter/sec
ZDOT = -1499
364727 ZDOT = -457
006369
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 19151
54756514
00016717 00000-0 10270-3 0 9023
2 25544 51
6414 83
8845 0007691 354
6496 5
4572 15
51180753 12663
Satellite: ISS
Catalog Number: 25544
Epoch time: 19151
54756514 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 83
8845 deg
Eccentricity:
0007691
Arg of perigee: 354
6496 deg
Mean anomaly: 5
4572 deg
Mean motion: 15
51180753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1266
Checksum: 320
Coasting Arc #4 (Orbit 1280)
---------------------------------------
Vector Time (GMT): 2019/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4293095
57 A = 6786538
72 meter
Y = 554335
73 meter E =
0014764
Z = -5237602
68 I = 52
00123
XDOT = 553
169574 Wp = 68
43275
YDOT = 7529
938777 meter/sec RA = 78
31614 deg
ZDOT = 1258
482087 TA = 213
56307
MA = 213
65669
Ha = 227
274 n
mi
Hp = 218
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14084959
22 X = 4312019
52
Y = 1818686
79 feet Y = 602450
60 meter
Z = -17183735
82 Z = -5216702
06
XDOT = 1814
860808 XDOT = 462
813434
YDOT = 24704
523547 feet/sec YDOT = 7535
619337 meter/sec
ZDOT = 4128
878237 ZDOT = 1260
950698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6830300
43 X = 2081875
57
Y = -12581288
71 feet Y = -3834776
80 meter
Z = -17088962
67 Z = -5208715
82
XDOT = 22761
276603 XDOT = 6937
637109
YDOT = 6771
008108 feet/sec YDOT = 2063
803271 meter/sec
ZDOT = 4139
272385 ZDOT = 1261
650223
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 19152
51394471
00016717 00000-0 10270-3 0 9032
2 25544 51
6421 79
0882 0007751 359
3573
7567 15
51158684 12811
Satellite: ISS
Catalog Number: 25544
Epoch time: 19152
51394471 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 79
0882 deg
Eccentricity:
0007751
Arg of perigee: 359
3573 deg
Mean anomaly:
7567 deg
Mean motion: 15
51158684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1281
Checksum: 317
Coasting Arc #5 (Orbit 1296)
---------------------------------------
Vector Time (GMT): 2019/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4426994
12 A = 6787407
36 meter
Y = -1107762
81 meter E =
0012386
Z = 5023066
06 I = 51
99635
XDOT = -514
828241 Wp = 26
17539
YDOT = -7363
000733 meter/sec RA = 73
37418 deg
ZDOT = -2064
785016 TA = 83
88737
MA = 83
74626
Ha = 227
425 n
mi
Hp = 218
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14524258
94 X = -4438677
42
Y = -3634392
42 feet Y = -1157334
62 meter
Z = 16479875
51 Z = 5001532
50
XDOT = -1689
069031 XDOT = -422
425071
YDOT = -24156
826552 feet/sec YDOT = -7368
240941 meter/sec
ZDOT = -6774
229055 ZDOT = -2067
062545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8466933
32 X = -2580721
28
Y = 12477211
14 feet Y = 3803053
95 meter
Z = 16382290
60 Z = 4993322
17
XDOT = -22327
014128 XDOT = -6805
273906
YDOT = -6188
764552 feet/sec YDOT = -1886
335436 meter/sec
ZDOT = -6783
752573 ZDOT = -2067
687784
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 19153
54474821
00016717 00000-0 10270-3 0 9045
2 25544 51
6420 73
9739 0007789 3
1060 357
0138 15
51168188 12979
Satellite: ISS
Catalog Number: 25544
Epoch time: 19153
54474821 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 73
9739 deg
Eccentricity:
0007789
Arg of perigee: 3
1060 deg
Mean anomaly: 357
0138 deg
Mean motion: 15
51168188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1297
Checksum: 318
Coasting Arc #6 (Orbit 1311)
---------------------------------------
Vector Time (GMT): 2019/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4605429
84 A = 6788581
19 meter
Y = 1570659
58 meter E =
0011796
Z = -4741307
96 I = 51
99059
XDOT = 453
076024 Wp = 69
24615
YDOT = 7109
906217 meter/sec RA = 68
43175 deg
ZDOT = 2805
086982 TA = 228
41190
MA = 228
51306
Ha = 227
473 n
mi
Hp = 218
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15109677
94 X = 4610554
92
Y = 5153082
61 feet Y = 1622190
17 meter
Z = -15555472
31 Z = -4718923
51
XDOT = 1486
469894 XDOT = 359
911622
YDOT = 23326
463966 feet/sec YDOT = 7114
451449 meter/sec
ZDOT = 9203
041278 ZDOT = 2807
062785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9875837
59 X = 3010155
30
Y = -12667621
49 feet Y = -3861091
03 meter
Z = -15454078
58 Z = -4710403
15
XDOT = 21570
800251 XDOT = 6574
779917
YDOT = 5618
531290 feet/sec YDOT = 1712
528337 meter/sec
ZDOT = 9211
203889 ZDOT = 2807
574945
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 19154
51112617
00016717 00000-0 10270-3 0 9056
2 25544 51
6429 69
1782 0007752 6
4610 353
6639 15
51169541 13120
Satellite: ISS
Catalog Number: 25544
Epoch time: 19154
51112617 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 69
1782 deg
Eccentricity:
0007752
Arg of perigee: 6
4610 deg
Mean anomaly: 353
6639 deg
Mean motion: 15
51169541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1312
Checksum: 300
Coasting Arc #7 (Orbit 1314)
---------------------------------------
Vector Time (GMT): 2019/154/16:09:25
000
Vector Time (MET): N/A
Weight (LBS) : 945426
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2191113
00 A = 6797886
30 meter
Y = -6412975
03 meter E =
0007924
Z = -534997
41 I = 52
01889
XDOT = 4624
376252 Wp = 93
97200
YDOT = -1085
400224 meter/sec RA = 67
60261 deg
ZDOT = -6005
850538 TA = 91
75821
MA = 91
66745
Ha = 227
379 n
mi
Hp = 218
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7188690
95 X = -2116639
68
Y = -21039944
31 feet Y = -6437061
09 meter
Z = -1755240
86 Z = -545461
35
XDOT = 15171
838098 XDOT = 4665
343252
YDOT = -3561
024357 feet/sec YDOT = -1033
457134 meter/sec
ZDOT = -19704
234050 ZDOT = -5983
287453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10392928
15 X = -3167764
50
Y = 19651393
41 feet Y = 5989744
71 meter
Z = -1801995
10 Z = -549248
11
XDOT = -11654
074919 XDOT = -3552
162035
YDOT = -7938
287288 feet/sec YDOT = -2419
589965 meter/sec
ZDOT = -19601
728611 ZDOT = -5974
606881
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 19154
70440006
00016717 00000-0 10270-3 0 9064
2 25544 51
6424 68
2192 0007652 5
5142 354
6092 15
51143163 13158
Satellite: ISS
Catalog Number: 25544
Epoch time: 19154
70440006 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 68
2192 deg
Eccentricity:
0007652
Arg of perigee: 5
5142 deg
Mean anomaly: 354
6092 deg
Mean motion: 15
51143163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1315
Checksum: 276
Coasting Arc #8 (Orbit 1325)
---------------------------------------
Vector Time (GMT): 2019/155/08:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2633113
78 A = 6787071
80 meter
Y = 3659309
01 meter E =
0007284
Z = 5067272
47 I = 51
97328
XDOT = -4512
938304 Wp = 52
06972
YDOT = -5896
874795 meter/sec RA = 64
21314 deg
ZDOT = 1915
826917 TA = 19
45388
MA = 19
42609
Ha = 227
511 n
mi
Hp = 218
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8638824
73 X = -2698451
74
Y = 12005607
00 feet Y = 3629497
46 meter
Z = 16624909
69 Z = 5054323
63
XDOT = -14806
228033 XDOT = -4455
968465
YDOT = -19346
702084 feet/sec YDOT = -5947
023435 meter/sec
ZDOT = 6285
521381 ZDOT = 1894
041860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3680109
00 X = -1121697
22
Y = 14393918
36 feet Y = 4387266
31 meter
Z = 16565730
49 Z = 5049234
65
XDOT = -19908
566857 XDOT = -6068
131178
YDOT = -12201
532444 feet/sec YDOT = -3719
027089 meter/sec
ZDOT = 6187
345500 ZDOT = 1885
902908
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 19155
41307553
00016717 00000-0 10270-3 0 9073
2 25544 51
6415 64
7018 0007698 8
5858 351
5423 15
51194927 13263
Satellite: ISS
Catalog Number: 25544
Epoch time: 19155
41307553 = yrday
fracday
Element set: 907
Inclination: 51
6415 deg
RA of node: 64
7018 deg
Eccentricity:
0007698
Arg of perigee: 8
5858 deg
Mean anomaly: 351
5423 deg
Mean motion: 15
51194927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1326
Checksum: 320
Coasting Arc #9 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2019/156/08:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2892182
40 A = 6786409
48 meter
Y = -3190490
81 meter E =
0018557
Z = -5260329
51 I = 51
95511
XDOT = 4593
140945 Wp = 58
26764
YDOT = 6015
658640 meter/sec RA = 59
26703 deg
ZDOT = -1116
666211 TA = 201
01343
MA = 201
08978
Ha = 227
608 n
mi
Hp = 218
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9488787
39 X = 2953196
29
Y = -10467489
53 feet Y = -3157806
27 meter
Z = -17258298
91 Z = -5246132
71
XDOT = 15069
360057 XDOT = 4530
954929
YDOT = 19736
412862 feet/sec YDOT = 6066
674862 meter/sec
ZDOT = -3663
603053 ZDOT = -1094
504274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4814080
63 X = 1467331
78
Y = -13366466
65 feet Y = -4074099
03 meter
Z = -17193501
73 Z = -5240579
33
XDOT = 20571
988847 XDOT = 6270
342200
YDOT = 12021
244567 feet/sec YDOT = 3664
075344 meter/sec
ZDOT = -3563
739836 ZDOT = -1086
227902
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 19156
37945073
00016717 00000-0 10270-3 0 9085
2 25544 51
6414 59
9054 0007818 12
9744 347
1606 15
51160852 13416
Satellite: ISS
Catalog Number: 25544
Epoch time: 19156
37945073 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 59
9054 deg
Eccentricity:
0007818
Arg of perigee: 12
9744 deg
Mean anomaly: 347
1606 deg
Mean motion: 15
51160852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 315
Coasting Arc #10 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2019/157/08:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3206706
32 A = 6785950
92 meter
Y = 2695863
44 meter E =
0008439
Z = 5334144
50 I = 51
93565
XDOT = -4650
740385 Wp = 32
99924
YDOT = -6089
696280 meter/sec RA = 54
32054 deg
ZDOT = 288
529427 TA = 54
30064
MA = 54
22214
Ha = 227
785 n
mi
Hp = 217
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10520690
01 X = -3262524
18
Y = 8844696
34 feet Y = 2659690
74 meter
Z = 17500474
09 Z = 5318432
46
XDOT = -15258
334596 XDOT = -4583
699525
YDOT = -19979
318504 feet/sec YDOT = -6141
329319 meter/sec
ZDOT = 946
618855 ZDOT = 266
099609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6182315
30 X = -1884369
70
Y = 12377166
15 feet Y = 3772560
24 meter
Z = 17428852
54 Z = 5312314
26
XDOT = -21107
843521 XDOT = -6433
670705
YDOT = -11702
915526 feet/sec YDOT = -3567
048652 meter/sec
ZDOT = 845
555828 ZDOT = 257
725416
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 19157
41024875
00016717 00000-0 10270-3 0 9090
2 25544 51
6412 54
7909 0007875 16
2499 343
8903 15
51184206 13572
Satellite: ISS
Catalog Number: 25544
Epoch time: 19157
41024875 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 54
7909 deg
Eccentricity:
0007875
Arg of perigee: 16
2499 deg
Mean anomaly: 343
8903 deg
Mean motion: 15
51184206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 326
Coasting Arc #11 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2019/157/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3989050
89 A = 6786325
75 meter
Y = -1542467
33 meter E =
0017409
Z = -5282383
33 I = 51
93629
XDOT = 3809
966541 Wp = 70
79116
YDOT = 6565
288739 meter/sec RA = 54
14001 deg
ZDOT = 968
228104 TA = 208
40928
MA = 208
50430
Ha = 227
735 n
mi
Hp = 218
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13087437
30 X = 4031661
58
Y = -5060588
37 feet Y = -1497619
76 meter
Z = -17330653
98 Z = -5262902
82
XDOT = 12499
890228 XDOT = 3731
565337
YDOT = 21539
661216 feet/sec YDOT = 6607
455907 meter/sec
ZDOT = 3176
601392 ZDOT = 986
546251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7681324
65 X = 2341267
75
Y = -11872256
67 feet Y = -3618663
83 meter
Z = -17242068
03 Z = -5255382
34
XDOT = 21911
677617 XDOT = 6678
679338
YDOT = 9482
957082 feet/sec YDOT = 2890
405319 meter/sec
ZDOT = 3258
948858 ZDOT = 993
327612
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 19157
41024934
00016717 00000-0 10270-3 0 9108
2 25544 51
6415 54
7907 0007878 16
6686 343
4723 15
51164212 13579
Satellite: ISS
Catalog Number: 25544
Epoch time: 19157
41024934 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 54
7907 deg
Eccentricity:
0007878
Arg of perigee: 16
6686 deg
Mean anomaly: 343
4723 deg
Mean motion: 15
51164212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 311
Coasting Arc #12 (Orbit 1372)
---------------------------------------
Vector Time (GMT): 2019/158/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4342938
98 A = 6787059
94 meter
Y = 1083241
52 meter E =
0012693
Z = 5098627
43 I = 51
91883
XDOT = -3724
561492 Wp = 33
96394
YDOT = -6457
759754 meter/sec RA = 49
19245 deg
ZDOT = -1788
129301 TA = 73
34243
MA = 73
20313
Ha = 227
882 n
mi
Hp = 217
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14248487
46 X = -4379495
49
Y = 3553942
00 feet Y = 1034470
49 meter
Z = 16727780
29 Z = 5077442
56
XDOT = -12219
689933 XDOT = -3643
386469
YDOT = -21186
875834 feet/sec YDOT = -6498
956233 meter/sec
ZDOT = -5866
565948 ZDOT = -1806
025655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9307677
69 X = -2836980
16
Y = 11499063
80 feet Y = 3504914
64 meter
Z = 16631512
26 Z = 5069284
94
XDOT = -21657
688895 XDOT = -6601
263575
YDOT = -8869
813280 feet/sec YDOT = -2703
519088 meter/sec
ZDOT = -5947
005461 ZDOT = -1812
647264
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 19158
44104679
00016717 00000-0 10270-3 0 9118
2 25544 51
6419 49
6759 0007864 19
8905 340
2551 15
51173731 13733
Satellite: ISS
Catalog Number: 25544
Epoch time: 19158
44104679 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 49
6759 deg
Eccentricity:
0007864
Arg of perigee: 19
8905 deg
Mean anomaly: 340
2551 deg
Mean motion: 15
51173731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1373
Checksum: 325
Coasting Arc #13 (Orbit 1387)
---------------------------------------
Vector Time (GMT): 2019/159/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4706180
07 A = 6788130
70 meter
Y = -723416
93 meter E =
0014514
Z = -4848671
45 I = 51
90054
XDOT = 3576
685564 Wp = 74
89538
YDOT = 6270
140958 meter/sec RA = 44
24316 deg
ZDOT = 2546
107808 TA = 220
05564
MA = 220
16276
Ha = 227
901 n
mi
Hp = 217
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15440223
33 X = 4737471
74
Y = -2373415
11 feet Y = -670613
47 meter
Z = -15907714
73 Z = -4825734
84
XDOT = 11734
532690 XDOT = 3493
937740
YDOT = 20571
328601 feet/sec YDOT = 6309
674924 meter/sec
ZDOT = 8353
372074 ZDOT = 2563
281811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10770413
07 X = 3282821
90
Y = -11460160
38 feet Y = -3493056
88 meter
Z = -15803541
05 Z = -4816919
31
XDOT = 21046
837285 XDOT = 6415
076004
YDOT = 8200
072625 feet/sec YDOT = 2499
382136 meter/sec
ZDOT = 8430
549856 ZDOT = 2569
631596
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 19159
40741691
00016717 00000-0 10270-3 0 9127
2 25544 51
6426 44
8793 0007925 23
6131 336
5382 15
51179707 13883
Satellite: ISS
Catalog Number: 25544
Epoch time: 19159
40741691 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 44
8793 deg
Eccentricity:
0007925
Arg of perigee: 23
6131 deg
Mean anomaly: 336
5382 deg
Mean motion: 15
51179707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1388
Checksum: 324
Coasting Arc #14 (Orbit 1403)
---------------------------------------
Vector Time (GMT): 2019/160/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5092615
63 A = 6789622
86 meter
Y = 365394
74 meter E =
0016082
Z = 4470788
22 I = 51
88055
XDOT = -3338
267668 Wp = 49
82315
YDOT = -6066
403534 meter/sec RA = 39
29497 deg
ZDOT = -3288
855773 TA = 73
31353
MA = 73
13706
Ha = 228
074 n
mi
Hp = 217
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16708056
53 X = -5118039
56
Y = 1198801
63 feet Y = 308302
86 meter
Z = 14667940
35 Z = 4445988
64
XDOT = -10952
321746 XDOT = -3254
207967
YDOT = -19902
898734 feet/sec YDOT = -6103
263985 meter/sec
ZDOT = -10790
209228 ZDOT = -3304
868287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12289921
87 X = -3745968
19
Y = 11525800
84 feet Y = 3513064
10 meter
Z = 14555359
42 Z = 4436473
55
XDOT = -20152
205831 XDOT = -6142
392337
YDOT = -7696
170902 feet/sec YDOT = -2345
792891 meter/sec
ZDOT = -10862
133958 ZDOT = -3310
778430
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 19160
43821069
00016717 00000-0 10270-3 0 9131
2 25544 51
6423 39
7643 0007984 27
6936 332
4639 15
51170054 14044
Satellite: ISS
Catalog Number: 25544
Epoch time: 19160
43821069 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 39
7643 deg
Eccentricity:
0007984
Arg of perigee: 27
6936 deg
Mean anomaly: 332
4639 deg
Mean motion: 15
51170054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1404
Checksum: 309
Coasting Arc #15 (Orbit 1418)
---------------------------------------
Vector Time (GMT): 2019/161/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5455190
20 A = 6791094
51 meter
Y = -122630
61 meter E =
0011688
Z = -4048508
92 I = 51
85985
XDOT = 3041
748706 Wp = 65
82225
YDOT = 5821
781100 meter/sec RA = 34
34616 deg
ZDOT = 3935
892548 TA = 244
92457
MA = 245
04592
Ha = 228
058 n
mi
Hp = 217
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17897605
64 X = 5475821
40
Y = -402331
38 feet Y = -61511
08 meter
Z = -13282509
59 Z = -4021959
63
XDOT = 9979
490505 XDOT = 2957
303496
YDOT = 19100
331694 feet/sec YDOT = 5855
323507 meter/sec
ZDOT = 12913
033294 ZDOT = 3950
463667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13505804
15 X = 4116569
11
Y = -11885519
66 feet Y = -3622706
39 meter
Z = -13162024
76 Z = -4011785
15
XDOT = 18998
769068 XDOT = 5790
824812
YDOT = 7266
344973 feet/sec YDOT = 2214
781948 meter/sec
ZDOT = 12978
438887 ZDOT = 3955
828173
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 19161
40457884
00016717 00000-0 10270-3 0 9140
2 25544 51
6430 34
9683 0007943 30
8805 329
2812 15
51187732 14193
Satellite: ISS
Catalog Number: 25544
Epoch time: 19161
40457884 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 34
9683 deg
Eccentricity:
0007943
Arg of perigee: 30
8805 deg
Mean anomaly: 329
2812 deg
Mean motion: 15
51187732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1419
Checksum: 317
Coasting Arc #16 (Orbit 1420)
---------------------------------------
Vector Time (GMT): 2019/161/12:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3415406
50 A = 6786429
58 meter
Y = -2667283
34 meter E =
0018385
Z = -5237202
53 I = 51
84066
XDOT = 5705
771111 Wp = 75
36311
YDOT = 4952
748896 meter/sec RA = 33
74973 deg
ZDOT = 1206
631062 TA = 206
16042
MA = 206
25342
Ha = 227
972 n
mi
Hp = 217
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11205401
90 X = 3470418
34
Y = -8750929
59 feet Y = -2628781
76 meter
Z = -17182423
01 Z = -5220478
46
XDOT = 18719
721494 XDOT = 5644
102866
YDOT = 16249
176169 feet/sec YDOT = 5016
209899 meter/sec
ZDOT = 3958
763328 ZDOT = 1234
198207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7666111
47 X = -2336630
78
Y = -12082374
47 feet Y = -3682707
74 meter
Z = -17106210
07 Z = -5213972
83
XDOT = 17029
665008 XDOT = 5190
641894
YDOT = -16548
535921 feet/sec YDOT = -5043
993749 meter/sec
ZDOT = 4083
244451 ZDOT = 1244
572909
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 19161
53342622
00016717 00000-0 10270-3 0 9158
2 25544 51
6427 34
3290 0007905 30
1351 330
0253 15
51192337 14213
Satellite: ISS
Catalog Number: 25544
Epoch time: 19161
53342622 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 34
3290 deg
Eccentricity:
0007905
Arg of perigee: 30
1351 deg
Mean anomaly: 330
0253 deg
Mean motion: 15
51192337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1421
Checksum: 265
Coasting Arc #17 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2019/162/12:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3903691
08 A = 6787259
89 meter
Y = 2360214
61 meter E =
0013610
Z = 5020808
56 I = 51
81623
XDOT = -5563
804616 Wp = 42
59490
YDOT = -4872
879205 meter/sec RA = 28
79486 deg
ZDOT = -2022
217592 TA = 67
08183
MA = 66
93824
Ha = 228
068 n
mi
Hp = 217
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12807385
45 X = -3954181
89
Y = 7743486
27 feet Y = 2316278
02 meter
Z = 16472469
03 Z = 5001723
45
XDOT = -18253
952153 XDOT = -5499
078350
YDOT = -15987
136499 feet/sec YDOT = -4934
735468 meter/sec
ZDOT = -6634
572153 ZDOT = -2049
087776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6747654
96 X = 2056685
23
Y = 13465315
72 feet Y = 4104228
23 meter
Z = 16385584
00 Z = 4994326
00
XDOT = -16334
280156 XDOT = -4978
688591
YDOT = 16458
484780 feet/sec YDOT = 5016
546161 meter/sec
ZDOT = -6755
887520 ZDOT = -2059
194516
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 19162
56421647
00016717 00000-0 10270-3 0 9168
2 25544 51
6436 29
2134 0007861 32
6313 327
5322 15
51213355 14378
Satellite: ISS
Catalog Number: 25544
Epoch time: 19162
56421647 = yrday
fracday
Element set: 916
Inclination: 51
6436 deg
RA of node: 29
2134 deg
Eccentricity:
0007861
Arg of perigee: 32
6313 deg
Mean anomaly: 327
5322 deg
Mean motion: 15
51213355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 290
Coasting Arc #18 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2019/163/12:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4365945
16 A = 6788505
85 meter
Y = -2152974
94 meter E =
0015184
Z = -4743069
00 I = 51
78951
XDOT = 5333
751308 Wp = 78
96703
YDOT = 4739
537316 meter/sec RA = 23
83835 deg
ZDOT = 2768
643875 TA = 218
39080
MA = 218
49895
Ha = 228
114 n
mi
Hp = 217
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14323967
06 X = 4412735
18
Y = -7063566
08 feet Y = -2103889
77 meter
Z = -15561249
99 Z = -4721747
33
XDOT = 17499
184083 XDOT = 5266
907424
YDOT = 15549
663111 feet/sec YDOT = 4798
809027 meter/sec
ZDOT = 9083
477279 ZDOT = 2794
391527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6211388
56 X = -1893231
23
Y = -14815472
07 feet Y = -4515755
89 meter
Z = -15464247
11 Z = -4713502
52
XDOT = 15460
165324 XDOT = 4712
258391
YDOT = -16048
557961 feet/sec YDOT = -4891
600467 meter/sec
ZDOT = 9199
702032 ZDOT = 2804
069179
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 19163
53058236
00016717 00000-0 10270-3 0 9177
2 25544 51
6426 24
4165 0007924 36
8022 323
3672 15
51194193 14528
Satellite: ISS
Catalog Number: 25544
Epoch time: 19163
53058236 = yrday
fracday
Element set: 917
Inclination: 51
6426 deg
RA of node: 24
4165 deg
Eccentricity:
0007924
Arg of perigee: 36
8022 deg
Mean anomaly: 323
3672 deg
Mean motion: 15
51194193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 299
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