[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 28th 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
5
Coasting Arc #1 (Orbit 1203)
---------------------------------------
Vector Time (GMT): 2019/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4320664
76 A = 6788394
18 meter
Y = 2158020
64 meter E =
0005453
Z = 4765274
04 I = 52
00186
XDOT = -544
982110 Wp = 51
68064
YDOT = -7139
636810 meter/sec RA = 103
03142 deg
ZDOT = 2740
320743 TA = 11
35279
MA = 11
34050
Ha = 226
591 n
mi
Hp = 219
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14175409
32 X = -4367622
37
Y = 7080120
20 feet Y = 2109441
00 meter
Z = 15634101
18 Z = 4744171
92
XDOT = -1787
999048 XDOT = -478
415148
YDOT = -23424
005282 feet/sec YDOT = -7145
359202 meter/sec
ZDOT = 8990
553618 ZDOT = 2737
834523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 68029
84 X = 20735
50
Y = 15939145
04 feet Y = 4858251
41 meter
Z = 15538162
00 Z = 4736031
78
XDOT = -20680
939575 XDOT = -6303
550382
YDOT = -8662
002761 feet/sec YDOT = -2640
178442 meter/sec
ZDOT = 8979
949478 ZDOT = 2737
088601
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 19147
55318521
00016717 00000-0 10270-3 0 9009
2 25544 51
6399 103
7073 0007430 339
6270 20
4584 15
51189247 12043
Satellite: ISS
Catalog Number: 25544
Epoch time: 19147
55318521 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 103
7073 deg
Eccentricity:
0007430
Arg of perigee: 339
6270 deg
Mean anomaly: 20
4584 deg
Mean motion: 15
51189247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1204
Checksum: 296
Coasting Arc #2 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2019/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4225883
37 A = 6787331
24 meter
Y = -1662065
49 meter E =
0014765
Z = -5056632
46 I = 52
00492
XDOT = 517
654573 Wp = 44
66451
YDOT = 7373
359607 meter/sec RA = 98
08881 deg
ZDOT = -1984
253163 TA = 206
09032
MA = 206
16481
Ha = 226
718 n
mi
Hp = 219
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13864446
74 X = 4268717
44
Y = -5452970
77 feet Y = -1614568
83 meter
Z = -16590001
50 Z = -5036000
66
XDOT = 1698
341774 XDOT = 444
803546
YDOT = 24190
812360 feet/sec YDOT = 7378
741195 meter/sec
ZDOT = -6510
016939 ZDOT = -1981
914969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1001284
91 X = 305191
64
Y = -14968552
02 feet Y = -4562414
66 meter
Z = -16496236
00 Z = -5028052
73
XDOT = 21546
518662 XDOT = 6567
378888
YDOT = 8629
142273 feet/sec YDOT = 2630
162565 meter/sec
ZDOT = -6500
120890 ZDOT = -1981
236847
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 19148
51956931
00016717 00000-0 10270-3 0 9010
2 25544 51
6404 98
9107 0007535 344
5707 15
5214 15
51156719 12198
Satellite: ISS
Catalog Number: 25544
Epoch time: 19148
51956931 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 98
9107 deg
Eccentricity:
0007535
Arg of perigee: 344
5707 deg
Mean anomaly: 15
5214 deg
Mean motion: 15
51156719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1219
Checksum: 312
Coasting Arc #3 (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 = -4162293
32 A = 6786384
98 meter
Y = 1102890
23 meter E =
0005481
Z = 5243038
48 I = 52
00565
XDOT = -513
096860 Wp = 17
72918
YDOT = -7556
102816 meter/sec RA = 93
14669 deg
ZDOT = 1186
870640 TA = 60
96829
MA = 60
91339
Ha = 226
915 n
mi
Hp = 219
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13655817
99 X = -4199784
81
Y = 3618406
28 feet Y = 1056134
53 meter
Z = 17201569
82 Z = 5222728
46
XDOT = -1683
388649 XDOT = -434
329439
YDOT = -24790
363571 feet/sec YDOT = -7561
400299 meter/sec
ZDOT = 3893
932547 ZDOT = 1184
568924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2333777
57 X = -711335
40
Y = 14046106
85 feet Y = 4281253
37 meter
Z = 17109313
19 Z = 5214918
66
XDOT = -22294
015641 XDOT = -6795
215967
YDOT = -8416
403227 feet/sec YDOT = -2565
319703 meter/sec
ZDOT = 3884
236552 ZDOT = 1183
915301
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
55037510
00016717 00000-0 10270-3 0 9029
2 25544 51
6404 93
7957 0007623 347
7342 12
3622 15
51186978 12358
Satellite: ISS
Catalog Number: 25544
Epoch time: 19149
55037510 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 93
7957 deg
Eccentricity:
0007623
Arg of perigee: 347
7342 deg
Mean anomaly: 12
3622 deg
Mean motion: 15
51186978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1235
Checksum: 311
Coasting Arc #4 (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 = 4159444
35 A = 6786082
09 meter
Y = -560831
44 meter E =
0015991
Z = -5344713
74 I = 52
00509
XDOT = 534
062540 Wp = 58
77420
YDOT = 7625
235363 meter/sec RA = 88
20322 deg
ZDOT = -377
286274 TA = 207
59679
MA = 207
68177
Ha = 226
997 n
mi
Hp = 219
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13646470
95 X = 4191368
55
Y = -1839998
17 feet Y = -514138
66 meter
Z = -17535150
06 Z = -5324430
97
XDOT = 1752
173689 XDOT = 450
587960
YDOT = 25017
176389 feet/sec YDOT = 7630
740922 meter/sec
ZDOT = -1237
815859 ZDOT = -374
894058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3723910
32 X = 1135047
86
Y = -13377785
31 feet Y = -4077548
96 meter
Z = -17443067
46 Z = -5316646
96
XDOT = 22715
733908 XDOT = 6923
755695
YDOT = 7955
136646 feet/sec YDOT = 2424
725650 meter/sec
ZDOT = -1227
735307 ZDOT = -374
213721
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
51675766
00016717 00000-0 10270-3 0 9039
2 25544 51
6404 88
9996 0007609 351
9026 8
2001 15
51153393 12504
Satellite: ISS
Catalog Number: 25544
Epoch time: 19150
51675766 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 88
9996 deg
Eccentricity:
0007609
Arg of perigee: 351
9026 deg
Mean anomaly: 8
2001 deg
Mean motion: 15
51153393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1250
Checksum: 307
Coasting Arc #5 (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 = -4196836
06 A = 6786009
93 meter
Y = -25362
99 meter E =
0008758
Z = 5331542
54 I = 52
00400
XDOT = -543
496722 Wp = 11
81232
YDOT = -7632
101854 meter/sec RA = 83
26033 deg
ZDOT = -455
661132 TA = 82
56367
MA = 82
46416
Ha = 227
142 n
mi
Hp = 218
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13769147
17 X = -4222138
57
Y = -83211
89 feet Y = -72436
97 meter
Z = 17491937
45 Z = 5311094
12
XDOT = -1783
125727 XDOT = -455
898606
YDOT = -25039
704247 feet/sec YDOT = -7637
689777 meter/sec
ZDOT = -1494
951219 ZDOT = -458
089299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5320248
49 X = -1621611
74
Y = 12826860
91 feet Y = 3909627
20 meter
Z = 17399161
16 Z = 5303264
32
XDOT = -22919
709092 XDOT = -6985
927331
YDOT = -7426
888779 feet/sec YDOT = -2263
715700 meter/sec
ZDOT = -1505
173128 ZDOT = -458
776769
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
54756204
00016717 00000-0 10270-3 0 9041
2 25544 51
6414 83
8848 0007688 354
5739 5
5328 15
51182377 12665
Satellite: ISS
Catalog Number: 25544
Epoch time: 19151
54756204 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 83
8848 deg
Eccentricity:
0007688
Arg of perigee: 354
5739 deg
Mean anomaly: 5
5328 deg
Mean motion: 15
51182377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1266
Checksum: 330
Coasting Arc #6 (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 = 4293286
80 A = 6786534
94 meter
Y = 557100
03 meter E =
0014748
Z = -5237133
74 I = 52
00123
XDOT = 551
152917 Wp = 68
43749
YDOT = 7529
695712 meter/sec RA = 78
31639 deg
ZDOT = 1260
905696 TA = 213
58188
MA = 213
67544
Ha = 227
268 n
mi
Hp = 218
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14085586
61 X = 4312177
55
Y = 1827756
00 feet Y = 605216
85 meter
Z = -17182197
31 Z = -5216232
27
XDOT = 1808
244478 XDOT = 460
787872
YDOT = 24703
726089 feet/sec YDOT = 7535
353670 meter/sec
ZDOT = 4136
829710 ZDOT = 1263
364489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6838978
95 X = 2084520
78
Y = -12578583
80 feet Y = -3833952
34 meter
Z = -17087420
60 Z = -5208245
80
XDOT = 22758
318648 XDOT = 6936
735524
YDOT = 6776
305058 feet/sec YDOT = 2065
417782 meter/sec
ZDOT = 4147
179338 ZDOT = 1264
060262
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
51394047
00016717 00000-0 10270-3 0 9053
2 25544 51
6421 79
0884 0007748 359
2793
8345 15
51160656 12819
Satellite: ISS
Catalog Number: 25544
Epoch time: 19152
51394047 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 79
0884 deg
Eccentricity:
0007748
Arg of perigee: 359
2793 deg
Mean anomaly:
8345 deg
Mean motion: 15
51160656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1281
Checksum: 316
Coasting Arc #7 (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 = -4427235
88 A = 6787405
12 meter
Y = -1111323
03 meter E =
0012384
Z = 5022072
21 I = 51
99636
XDOT = -512
081869 Wp = 26
16306
YDOT = -7362
320798 meter/sec RA = 73
37440 deg
ZDOT = -2067
867693 TA = 83
93083
MA = 83
78973
Ha = 227
418 n
mi
Hp = 218
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14525052
09 X = -4438874
51
Y = -3646072
93 feet Y = -1160897
29 meter
Z = 16476614
86 Z = 5000537
59
XDOT = -1680
058626 XDOT = -419
671533
YDOT = -24154
595793 feet/sec YDOT = -7367
530253 meter/sec
ZDOT = -6784
342824 ZDOT = -2070
131864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8478160
89 X = -2584143
44
Y = 12473898
14 feet Y = 3802044
15 meter
Z = 16379025
50 Z = 4992326
97
XDOT = -22322
025771 XDOT = -6803
753455
YDOT = -6195
693872 feet/sec YDOT = -1888
447492 meter/sec
ZDOT = -6793
805804 ZDOT = -2070
752009
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
54474255
00016717 00000-0 10270-3 0 9068
2 25544 51
6421 73
9742 0007785 3
0279 357
0918 15
51170397 12972
Satellite: ISS
Catalog Number: 25544
Epoch time: 19153
54474255 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 73
9742 deg
Eccentricity:
0007785
Arg of perigee: 3
0279 deg
Mean anomaly: 357
0918 deg
Mean motion: 15
51170397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1297
Checksum: 324
Coasting Arc #8 (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 = 4605693
13 A = 6788580
36 meter
Y = 1575080
03 meter E =
0011774
Z = -4739559
79 I = 51
99061
XDOT = 449
429687 Wp = 69
21663
YDOT = 7108
684559 meter/sec RA = 68
43196 deg
ZDOT = 2808
821135 TA = 228
48144
MA = 228
58252
Ha = 227
466 n
mi
Hp = 218
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15110541
77 X = 4610760
27
Y = 5167585
40 feet Y = 1626613
24 meter
Z = -15549736
86 Z = -4717174
20
XDOT = 1474
506846 XDOT = 356
261079
YDOT = 23322
455902 feet/sec YDOT = 7113
188991 meter/sec
ZDOT = 9215
292439 ZDOT = 2810
779216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9889803
23 X = 3014412
02
Y = -12663623
45 feet Y = -3859872
43 meter
Z = -15448338
45 Z = -4708653
56
XDOT = 21563
340627 XDOT = 6572
506223
YDOT = 5627
565719 feet/sec YDOT = 1715
282031 meter/sec
ZDOT = 9223
374768 ZDOT = 2811
284629
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
51111899
00016717 00000-0 10270-3 0 9079
2 25544 51
6429 69
1784 0007748 6
3784 353
7464 15
51172175 13122
Satellite: ISS
Catalog Number: 25544
Epoch time: 19154
51111899 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 69
1784 deg
Eccentricity:
0007748
Arg of perigee: 6
3784 deg
Mean anomaly: 353
7464 deg
Mean motion: 15
51172175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1312
Checksum: 325
Coasting Arc #9 (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 = -2188113
26 A = 6797876
67 meter
Y = -6413669
82 meter E =
0007902
Z = -538848
75 I = 52
01888
XDOT = 4626
173596 Wp = 93
97587
YDOT = -1080
145195 meter/sec RA = 67
60287 deg
ZDOT = -6005
416231 TA = 91
79574
MA = 91
70523
Ha = 227
371 n
mi
Hp = 218
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7178849
28 X = -2113613
69
Y = -21042223
81 feet Y = -6437722
19 meter
Z = -1767876
46 Z = -549298
05
XDOT = 15177
734896 XDOT = 4667
079590
YDOT = -3543
783447 feet/sec YDOT = -1028
182346 meter/sec
ZDOT = -19702
809157 ZDOT = -5982
844562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10401394
61 X = -3170345
08
Y = 19645732
20 feet Y = 5988019
18 meter
Z = -1814564
22 Z = -553079
17
XDOT = -11645
975649 XDOT = -3549
693378
YDOT = -7953
777502 feet/sec YDOT = -2424
311382 meter/sec
ZDOT = -19600
265365 ZDOT = -5974
160883
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
70439254
00016717 00000-0 10270-3 0 9089
2 25544 51
6425 68
2194 0007649 5
4268 354
6965 15
51145854 13153
Satellite: ISS
Catalog Number: 25544
Epoch time: 19154
70439254 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 68
2194 deg
Eccentricity:
0007649
Arg of perigee: 5
4268 deg
Mean anomaly: 354
6965 deg
Mean motion: 15
51145854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1315
Checksum: 326
Coasting Arc #10 (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 = -2636520
18 A = 6787057
41 meter
Y = 3654865
54 meter E =
0007268
Z = 5068709
49 I = 51
97325
XDOT = -4510
387521 Wp = 51
94254
YDOT = -5900
392147 meter/sec RA = 64
21331 deg
ZDOT = 1910
960400 TA = 19
62979
MA = 19
60182
Ha = 227
503 n
mi
Hp = 218
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8650000
60 X = -2701815
18
Y = 11991028
67 feet Y = 3625016
13 meter
Z = 16629624
30 Z = 5055744
20
XDOT = -14797
859320 XDOT = -4453
354900
YDOT = -19358
241952 feet/sec YDOT = -5950
511910 meter/sec
ZDOT = 6269
555118 ZDOT = 1889
187885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3695919
08 X = -1126516
13
Y = 14384528
86 feet Y = 4384404
40 meter
Z = 16570370
99 Z = 5050649
08
XDOT = -19905
653898 XDOT = -6067
243308
YDOT = -12214
239133 feet/sec YDOT = -3722
900088 meter/sec
ZDOT = 6171
436556 ZDOT = 1881
053862
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
41306672
00016717 00000-0 10270-3 0 9096
2 25544 51
6416 64
7020 0007694 8
5008 351
6272 15
51197784 13267
Satellite: ISS
Catalog Number: 25544
Epoch time: 19155
41306672 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 64
7020 deg
Eccentricity:
0007694
Arg of perigee: 8
5008 deg
Mean anomaly: 351
6272 deg
Mean motion: 15
51197784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1326
Checksum: 307
Coasting Arc #11 (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 = 2896432
82 A = 6786395
49 meter
Y = -3184907
82 meter E =
0018547
Z = -5261344
27 I = 51
95509
XDOT = 4589
740030 Wp = 58
29346
YDOT = 6019
417925 meter/sec RA = 59
26717 deg
ZDOT = -1110
498140 TA = 201
04727
MA = 201
12370
Ha = 227
599 n
mi
Hp = 218
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9502732
34 X = 2957388
89
Y = -10449172
63 feet Y = -3152176
07 meter
Z = -17261628
17 Z = -5247126
96
XDOT = 15058
202197 XDOT = 4527
482267
YDOT = 19748
746474 feet/sec YDOT = 6070
395713 meter/sec
ZDOT = -3643
366600 ZDOT = -1088
352897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4834039
74 X = 1473415
31
Y = -13354968
35 feet Y = -4070594
35 meter
Z = -17196738
58 Z = -5241565
92
XDOT = 20567
176414 XDOT = 6268
875371
YDOT = 12035
529557 feet/sec YDOT = 3668
429409 meter/sec
ZDOT = -3543
579578 ZDOT = -1080
083055
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
37943998
00016717 00000-0 10270-3 0 9102
2 25544 51
6415 59
9056 0007813 12
8867 347
2483 15
51164117 13411
Satellite: ISS
Catalog Number: 25544
Epoch time: 19156
37943998 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 59
9056 deg
Eccentricity:
0007813
Arg of perigee: 12
8867 deg
Mean anomaly: 347
2483 deg
Mean motion: 15
51164117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 327
Coasting Arc #12 (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 = -3211911
42 A = 6785939
48 meter
Y = 2689042
95 meter E =
0008442
Z = 5334461
00 I = 51
93564
XDOT = -4646
145734 Wp = 32
86308
YDOT = -6093
544095 meter/sec RA = 54
32063 deg
ZDOT = 280
914202 TA = 54
50927
MA = 54
43053
Ha = 227
776 n
mi
Hp = 217
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10537767
11 X = -3267654
17
Y = 8822319
38 feet Y = 2652812
45 meter
Z = 17501512
46 Z = 5318723
85
XDOT = -15243
260281 XDOT = -4579
025198
YDOT = -19991
942569 feet/sec YDOT = -6145
125306 meter/sec
ZDOT = 921
634521 ZDOT = 258
506896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6206955
66 X = -1891880
09
Y = 12363548
87 feet Y = 3768409
69 meter
Z = 17429777
80 Z = 5312596
27
XDOT = -21099
959241 XDOT = -6431
267577
YDOT = -11718
808074 feet/sec YDOT = -3571
892701 meter/sec
ZDOT = 820
674110 ZDOT = 250
141469
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
41023568
00016717 00000-0 10270-3 0 9111
2 25544 51
6412 54
7911 0007870 16
1647 343
9754 15
51187695 13574
Satellite: ISS
Catalog Number: 25544
Epoch time: 19157
41023568 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 54
7911 deg
Eccentricity:
0007870
Arg of perigee: 16
1647 deg
Mean anomaly: 343
9754 deg
Mean motion: 15
51187695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 319
Coasting Arc #13 (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 = 3993330
69 A = 6786319
86 meter
Y = -1535057
51 meter E =
0017383
Z = -5281273
88 I = 51
93630
XDOT = 3804
264014 Wp = 70
81287
YDOT = 6567
508964 meter/sec RA = 54
14011 deg
ZDOT = 975
774232 TA = 208
46024
MA = 208
55528
Ha = 227
725 n
mi
Hp = 218
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13101478
63 X = 4035852
81
Y = -5036277
91 feet Y = -1490162
57 meter
Z = -17327014
05 Z = -5261772
80
XDOT = 12481
181149 XDOT = 3725
801752
YDOT = 21546
945421 feet/sec YDOT = 6609
612020 meter/sec
ZDOT = 3201
359030 ZDOT = 994
064530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7706978
07 X = 2349086
91
Y = -11860882
25 feet Y = -3615196
91 meter
Z = -17238335
62 Z = -5254244
70
XDOT = 21901
555745 XDOT = 6675
594191
YDOT = 9498
098540 feet/sec YDOT = 2895
020435 meter/sec
ZDOT = 3283
579856 ZDOT = 1000
835140
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
41023627
00016717 00000-0 10270-3 0 9128
2 25544 51
6416 54
7909 0007873 16
5801 343
5606 15
51167900 13573
Satellite: ISS
Catalog Number: 25544
Epoch time: 19157
41023627 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 54
7909 deg
Eccentricity:
0007873
Arg of perigee: 16
5801 deg
Mean anomaly: 343
5606 deg
Mean motion: 15
51167900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 305
Coasting Arc #14 (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 = -4347918
76 A = 6787059
09 meter
Y = 1074585
84 meter E =
0012702
Z = 5096227
01 I = 51
91886
XDOT = -3717
133730 Wp = 33
96554
YDOT = -6459
608839 meter/sec RA = 49
19252 deg
ZDOT = -1796
837225 TA = 73
42752
MA = 73
28805
Ha = 227
872 n
mi
Hp = 217
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14264825
32 X = -4384366
45
Y = 3525544
11 feet Y = 1025759
73 meter
Z = 16719904
90 Z = 5075018
21
XDOT = -12195
320637 XDOT = -3635
896284
YDOT = -21192
942385 feet/sec YDOT = -6500
721905 meter/sec
ZDOT = -5895
135252 ZDOT = -1814
697347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9337797
92 X = -2846160
81
Y = 11486240
69 feet Y = 3501006
16 meter
Z = 16623529
33 Z = 5066851
74
XDOT = -21642
698084 XDOT = -6596
694376
YDOT = -8887
274252 feet/sec YDOT = -2708
841192 meter/sec
ZDOT = -5975
410119 ZDOT = -1821
305004
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
44103117
00016717 00000-0 10270-3 0 9136
2 25544 51
6419 49
6760 0007858 19
8023 340
3432 15
51177606 13733
Satellite: ISS
Catalog Number: 25544
Epoch time: 19158
44103117 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 49
6760 deg
Eccentricity:
0007858
Arg of perigee: 19
8023 deg
Mean anomaly: 340
3432 deg
Mean motion: 15
51177606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1373
Checksum: 303
Coasting Arc #15 (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 = 4711787
70 A = 6788134
19 meter
Y = -713533
77 meter E =
0014474
Z = -4844642
46 I = 51
90059
XDOT = 3567
286933 Wp = 74
86145
YDOT = 6271
598839 meter/sec RA = 44
24321 deg
ZDOT = 2555
800761 TA = 220
19119
MA = 220
29831
Ha = 227
891 n
mi
Hp = 217
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15458621
06 X = 4742948
87
Y = -2340990
06 feet Y = -660668
33 meter
Z = -15894496
27 Z = -4821678
93
XDOT = 11703
697286 XDOT = 3484
476422
YDOT = 20576
111677 feet/sec YDOT = 6311
027352 meter/sec
ZDOT = 8385
173100 ZDOT = 2572
928957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10804827
05 X = 3293311
28
Y = -11445936
26 feet Y = -3488721
37 meter
Z = -15790201
61 Z = -4812853
45
XDOT = 21026
391584 XDOT = 6408
844155
YDOT = 8220
484116 feet/sec YDOT = 2505
603559 meter/sec
ZDOT = 8462
142835 ZDOT = 2579
261136
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
40739866
00016717 00000-0 10270-3 0 9140
2 25544 51
6426 44
8794 0007919 23
5206 336
6305 15
51184104 13882
Satellite: ISS
Catalog Number: 25544
Epoch time: 19159
40739866 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 44
8794 deg
Eccentricity:
0007919
Arg of perigee: 23
5206 deg
Mean anomaly: 336
6305 deg
Mean motion: 15
51184104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1388
Checksum: 326
Coasting Arc #16 (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 = -5098688
50 A = 6789632
08 meter
Y = 354319
03 meter E =
0016088
Z = 4464778
81 I = 51
88062
XDOT = -3326
415738 Wp = 49
89588
YDOT = -6067
247975 meter/sec RA = 39
29500 deg
ZDOT = -3299
259382 TA = 73
35889
MA = 73
18231
Ha = 228
062 n
mi
Hp = 217
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16727980
65 X = -5123958
94
Y = 1162464
00 feet Y = 297160
09 meter
Z = 14648224
45 Z = 4439950
10
XDOT = -10913
437460 XDOT = -3242
296940
YDOT = -19905
669209 feet/sec YDOT = -6103
975558 meter/sec
ZDOT = -10824
341804 ZDOT = -3315
214181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12328193
16 X = -3757633
28
Y = 11510067
89 feet Y = 3508268
69 meter
Z = 14535512
70 Z = 4430424
27
XDOT = -20124
738782 XDOT = -6134
020381
YDOT = -7720
188724 feet/sec YDOT = -2353
113523 meter/sec
ZDOT = -10896
004528 ZDOT = -3321
102180
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
43818943
00016717 00000-0 10270-3 0 9150
2 25544 51
6424 39
7644 0007977 27
5999 332
5574 15
51174679 14042
Satellite: ISS
Catalog Number: 25544
Epoch time: 19160
43818943 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 39
7644 deg
Eccentricity:
0007977
Arg of perigee: 27
5999 deg
Mean anomaly: 332
5574 deg
Mean motion: 15
51174679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1404
Checksum: 346
Coasting Arc #17 (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 = 5461537
92 A = 6791107
81 meter
Y = -110403
39 meter E =
0011655
Z = -4040226
95 I = 51
85993
XDOT = 3027
210874 Wp = 65
60761
YDOT = 5822
112949 meter/sec RA = 34
34617 deg
ZDOT = 3946
697565 TA = 245
27475
MA = 245
39611
Ha = 228
046 n
mi
Hp = 217
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17918431
48 X = 5481991
69
Y = -362215
85 feet Y = -49213
88 meter
Z = -13255337
76 Z = -4013647
25
XDOT = 9931
794205 XDOT = 2942
710548
YDOT = 19101
420437 feet/sec YDOT = 5855
492474 meter/sec
ZDOT = 12948
482824 ZDOT = 3961
197931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13547424
16 X = 4129254
88
Y = -11868103
82 feet Y = -3617398
05 meter
Z = -13134716
45 Z = -4003461
58
XDOT = 18964
057086 XDOT = 5780
244600
YDOT = 7294
997254 feet/sec YDOT = 2223
515163 meter/sec
ZDOT = 13013
567328 ZDOT = 3966
535322
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
40455453
00016717 00000-0 10270-3 0 9162
2 25544 51
6430 34
9684 0007936 30
7805 329
3810 15
51192767 14198
Satellite: ISS
Catalog Number: 25544
Epoch time: 19161
40455453 = yrday
fracday
Element set: 916
Inclination: 51
6430 deg
RA of node: 34
9684 deg
Eccentricity:
0007936
Arg of perigee: 30
7805 deg
Mean anomaly: 329
3810 deg
Mean motion: 15
51192767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1419
Checksum: 314
Coasting Arc #18 (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 = 3427551
95 A = 6786426
41 meter
Y = -2656701
35 meter E =
0018343
Z = -5234595
82 I = 51
84070
XDOT = 5696
546087 Wp = 75
39812
YDOT = 4959
955979 meter/sec RA = 33
74964 deg
ZDOT = 1220
795490 TA = 206
26300
MA = 206
35612
Ha = 227
960 n
mi
Hp = 217
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11245249
19 X = 3482431
90
Y = -8716211
78 feet Y = -2618064
69 meter
Z = -17173870
82 Z = -5217813
07
XDOT = 18689
455665 XDOT = 5634
729133
YDOT = 16272
821454 feet/sec YDOT = 5023
312988 meter/sec
ZDOT = 4005
234547 ZDOT = 1248
317463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7627857
48 X = -2324970
96
Y = -12118777
24 feet Y = -3693803
30 meter
Z = -17097392
92 Z = -5211285
36
XDOT = 17047
725590 XDOT = 5196
146760
YDOT = -16518
689667 feet/sec YDOT = -5034
896611 meter/sec
ZDOT = 4129
509817 ZDOT = 1258
674592
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
53340149
00016717 00000-0 10270-3 0 9172
2 25544 51
6427 34
3291 0007898 30
0327 330
1276 15
51197383 14219
Satellite: ISS
Catalog Number: 25544
Epoch time: 19161
53340149 = yrday
fracday
Element set: 917
Inclination: 51
6427 deg
RA of node: 34
3291 deg
Eccentricity:
0007898
Arg of perigee: 30
0327 deg
Mean anomaly: 330
1276 deg
Mean motion: 15
51197383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1421
Checksum: 295
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