[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 1st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
033/17:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 216
5
039/16:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 215
6
040/11:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 215
6
044/15:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
7
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 3385)
---------------------------------------
Vector Time (GMT): 2019/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1446999
13 A = 6780366
61 meter
Y = 4070424
65 meter E =
0006541
Z = 5226595
89 I = 51
40657
XDOT = -6669
755812 Wp = 3
68154
YDOT = 3649
127598 meter/sec RA = 325
35767 deg
ZDOT = -988
891490 TA = 95
85454
MA = 95
77997
Ha = 222
396 n
mi
Hp = 216
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4747372
46 X = 1375987
44
Y = 13354411
57 feet Y = 4086208
77 meter
Z = 17147624
30 Z = 5233452
43
XDOT = -21882
400957 XDOT = -6705
262267
YDOT = 11972
203407 feet/sec YDOT = 3574
343245 meter/sec
ZDOT = -3244
394652 ZDOT = -1021
376276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7557500
63 X = -2303526
19
Y = 11946497
69 feet Y = 3641292
49 meter
Z = 17178016
47 Z = 5235859
42
XDOT = -22115
259471 XDOT = -6740
731087
YDOT = -9083
334216 feet/sec YDOT = -2768
600269 meter/sec
ZDOT = -3391
421398 ZDOT = -1033
705242
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 19030
54650550
00016717 00000-0 10270-3 0 9000
2 25544 51
6405 325
7678 0005254 330
0187 30
0664 15
53214819 33867
Satellite: ISS
Catalog Number: 25544
Epoch time: 19030
54650550 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 325
7678 deg
Eccentricity:
0005254
Arg of perigee: 330
0187 deg
Mean anomaly: 30
0664 deg
Mean motion: 15
53214819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3386
Checksum: 291
Coasting Arc #2 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2019/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -273174
25 A = 6782161
50 meter
Y = -4771971
04 meter E =
0008804
Z = -4818663
73 I = 51
38587
XDOT = 6633
610380 Wp = 81
95413
YDOT = -2901
422116 meter/sec RA = 320
35227 deg
ZDOT = 2502
382419 TA = 212
73055
MA = 212
78513
Ha = 222
554 n
mi
Hp = 216
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -896240
97 X = -196386
46
Y = -15656072
95 feet Y = -4774596
32 meter
Z = -15809264
21 Z = -4819804
38
XDOT = 21763
813584 XDOT = 6653
406922
YDOT = -9519
101432 feet/sec YDOT = -2827
129873 meter/sec
ZDOT = 8209
916072 ZDOT = 2534
653381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11571693
29 X = 3527052
12
Y = -10576806
19 feet Y = -3223810
53 meter
Z = -15813784
75 Z = -4820041
59
XDOT = 20388
723023 XDOT = 6214
482777
YDOT = 9838
573934 feet/sec YDOT = 2998
797335 meter/sec
ZDOT = 8355
872368 ZDOT = 2546
869898
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 19031
51160876
00016717 00000-0 10270-3 0 9016
2 25544 51
6406 320
9629 0005234 334
9985 25
0913 15
53213132 34014
Satellite: ISS
Catalog Number: 25544
Epoch time: 19031
51160876 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 320
9629 deg
Eccentricity:
0005234
Arg of perigee: 334
9985 deg
Mean anomaly: 25
0913 deg
Mean motion: 15
53213132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 284
Coasting Arc #3 (Orbit 3416)
---------------------------------------
Vector Time (GMT): 2019/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -837553
18 A = 6785081
35 meter
Y = 5377012
66 meter E =
0011108
Z = 4050429
34 I = 51
37056
XDOT = -6338
303962 Wp = 49
99693
YDOT = 1928
617613 meter/sec RA = 315
35206 deg
ZDOT = -3856
866162 TA = 80
15784
MA = 80
03245
Ha = 222
699 n
mi
Hp = 216
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2747877
88 X = -917292
51
Y = 17641117
67 feet Y = 5367200
55 meter
Z = 13288810
18 Z = 4046167
46
XDOT = -20794
960504 XDOT = -6340
665132
YDOT = 6327
485607 feet/sec YDOT = 1857
725230 meter/sec
ZDOT = -12653
760375 ZDOT = -3887
660254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15253616
84 X = -4649302
41
Y = 9306775
62 feet Y = 2836705
21 meter
Z = 13268890
01 Z = 4044357
67
XDOT = -17586
825714 XDOT = -5360
464478
YDOT = -10519
466603 feet/sec YDOT = -3206
333420 meter/sec
ZDOT = -12792
922005 ZDOT = -3899
282627
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19032
54105099
00016717 00000-0 10270-3 0 9027
2 25544 51
6406 315
8393 0005238 338
2900 21
8030 15
53207688 34173
Satellite: ISS
Catalog Number: 25544
Epoch time: 19032
54105099 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 315
8393 deg
Eccentricity:
0005238
Arg of perigee: 338
2900 deg
Mean anomaly: 21
8030 deg
Mean motion: 15
53207688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3417
Checksum: 294
Coasting Arc #4 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2019/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1771663
62 A = 6788140
63 meter
Y = -5812689
42 meter E =
0007024
Z = -3019291
93 I = 51
35865
XDOT = 5824
760120 Wp = 20
88894
YDOT = -776
625373 meter/sec RA = 310
35591 deg
ZDOT = 4922
988450 TA = 304
38261
MA = 304
44902
Ha = 222
761 n
mi
Hp = 216
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5812544
68 X = 1851196
76
Y = -19070503
34 feet Y = -5792432
65 meter
Z = -9905813
43 Z = -3010493
09
XDOT = 19110
105380 XDOT = 5809
099114
YDOT = -2547
983506 feet/sec YDOT = -711
576567 meter/sec
ZDOT = 16151
536911 ZDOT = 4951
244185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18177522
72 X = 5540508
92
Y = -8236916
32 feet Y = -2510612
10 meter
Z = -9865383
44 Z = -3006968
87
XDOT = 13899
655243 XDOT = 4236
614918
YDOT = 11216
116245 feet/sec YDOT = 3418
672231 meter/sec
ZDOT = 16279
096579 ZDOT = 4961
868637
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19033
50615104
00016717 00000-0 10270-3 0 9038
2 25544 51
6412 311
0348 0005270 341
1115 18
9841 15
53218902 34320
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
50615104 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 311
0348 deg
Eccentricity:
0005270
Arg of perigee: 341
1115 deg
Mean anomaly: 18
9841 deg
Mean motion: 15
53218902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3432
Checksum: 262
Coasting Arc #5 (Orbit 3435)
---------------------------------------
Vector Time (GMT): 2019/033/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1926874
39 A = 6788615
43 meter
Y = 5880978
39 meter E =
0011583
Z = 2784454
37 I = 51
35442
XDOT = -5704
390693 Wp = 76
45718
YDOT = 550
984550 meter/sec RA = 309
22678 deg
ZDOT = -5090
669377 TA = 71
85077
MA = 71
72467
Ha = 222
704 n
mi
Hp = 216
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6321766
36 X = -2006018
92
Y = 19294548
52 feet Y = 5858988
13 meter
Z = 9135348
99 Z = 2774902
53
XDOT = -18715
192561 XDOT = -5685
400988
YDOT = 1807
692093 feet/sec YDOT = 487
300403 meter/sec
ZDOT = -16701
671186 ZDOT = -5118
332324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5149501
59 X = 1569568
09
Y = 19660261
70 feet Y = 5992447
76 meter
Z = 9091516
76 Z = 2771094
31
XDOT = -13188
176566 XDOT = -4019
756217
YDOT = 11266
751199 feet/sec YDOT = 3434
105766 meter/sec
ZDOT = -16826
527673 ZDOT = -5128
725635
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19033
76350724
00016717 00000-0 10270-3 0 9041
2 25544 51
6399 309
7515 0005469 339
4346 20
6586 15
53256676 34360
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
76350724 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 309
7515 deg
Eccentricity:
0005469
Arg of perigee: 339
4346 deg
Mean anomaly: 20
6586 deg
Mean motion: 15
53256676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3436
Checksum: 335
Coasting Arc #6 (Orbit 3450)
---------------------------------------
Vector Time (GMT): 2019/034/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2659809
73 A = 6791040
18 meter
Y = -6055616
89 meter E =
0012180
Z = -1509959
75 I = 51
34045
XDOT = 5024
112274 Wp = 17
40783
YDOT = 781
005406 meter/sec RA = 304
23587 deg
ZDOT = 5741
267876 TA = 326
03161
MA = 326
10953
Ha = 222
850 n
mi
Hp = 216
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8726409
88 X = 2734662
01
Y = -19867509
47 feet Y = -6025454
49 meter
Z = -4953936
19 Z = -1496858
04
XDOT = 16483
307985 XDOT = 4987
118338
YDOT = 2562
353694 feet/sec YDOT = 836
981602 meter/sec
ZDOT = 18836
180694 ZDOT = 5765
582614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3835782
58 X = -1169146
53
Y = -21371578
23 feet Y = -6514057
04 meter
Z = -4894084
34 Z = -1491716
91
XDOT = 13439
807487 XDOT = 4096
453322
YDOT = -6732
943836 feet/sec YDOT = -2052
201281 meter/sec
ZDOT = 18945
766331 ZDOT = 5774
669578
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19034
72860604
00016717 00000-0 10270-3 0 9052
2 25544 51
6384 304
9465 0005210 344
7247 15
3747 15
53215534 34513
Satellite: ISS
Catalog Number: 25544
Epoch time: 19034
72860604 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 304
9465 deg
Eccentricity:
0005210
Arg of perigee: 344
7247 deg
Mean anomaly: 15
3747 deg
Mean motion: 15
53215534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3451
Checksum: 299
Coasting Arc #7 (Orbit 3466)
---------------------------------------
Vector Time (GMT): 2019/035/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3249383
75 A = 6791818
50 meter
Y = 5960794
15 meter E =
0008402
Z = 96631
53 I = 51
32532
XDOT = -4248
656625 Wp = 111
60324
YDOT = -2212
315962 meter/sec RA = 299
24873 deg
ZDOT = -5981
721007 TA = 67
35220
MA = 67
26337
Ha = 222
940 n
mi
Hp = 216
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10660707
84 X = -3316266
90
Y = 19556411
25 feet Y = 5924083
31 meter
Z = 317032
57 Z = 80685
24
XDOT = -13939
162155 XDOT = -4194
547081
YDOT = -7258
254470 feet/sec YDOT = -2259
524873 meter/sec
ZDOT = -19625
068921 ZDOT = -6002
227368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2464455
97 X = 751166
18
Y = 22137550
87 feet Y = 6747525
51 meter
Z = 244377
95 Z = 74486
40
XDOT = -13861
866373 XDOT = -4225
096871
YDOT = 1780
439657 feet/sec YDOT = 542
678008 meter/sec
ZDOT = -19717
303231 ZDOT = -6009
834025
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19035
75804073
00016717 00000-0 10270-3 0 9065
2 25544 51
6378 299
8220 0005441 349
0368 11
0665 15
53270352 34673
Satellite: ISS
Catalog Number: 25544
Epoch time: 19035
75804073 = yrday
fracday
Element set: 906
Inclination: 51
6378 deg
RA of node: 299
8220 deg
Eccentricity:
0005441
Arg of perigee: 349
0368 deg
Mean anomaly: 11
0665 deg
Mean motion: 15
53270352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3467
Checksum: 312
Coasting Arc #8 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2019/036/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3645608
43 A = 6791252
64 meter
Y = -5570230
65 meter E =
0016460
Z = 1292249
91 I = 51
30687
XDOT = 3467
556403 Wp = 42
72834
YDOT = 3623
710760 meter/sec RA = 294
25955 deg
ZDOT = 5805
857820 TA = 331
40301
MA = 331
49320
Ha = 222
979 n
mi
Hp = 216
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11960657
59 X = 3701348
53
Y = -18275034
93 feet Y = -5529151
22 meter
Z = 4239665
06 Z = 1310093
89
XDOT = 11376
497384 XDOT = 3398
576511
YDOT = 11888
814829 feet/sec YDOT = 3662
101821 meter/sec
ZDOT = 19048
089960 ZDOT = 5822
533817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1064826
50 X = -324559
12
Y = -21799213
06 feet Y = -6644400
14 meter
Z = 4320815
42 Z = 1316984
54
XDOT = 14496
527255 XDOT = 4418
541507
YDOT = 3102
440614 feet/sec YDOT = 945
623899 meter/sec
ZDOT = 19122
884737 ZDOT = 5828
655268
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19036
78747706
00016717 00000-0 10270-3 0 9079
2 25544 51
6371 294
6968 0005111 352
6557 7
4519 15
53216642 34839
Satellite: ISS
Catalog Number: 25544
Epoch time: 19036
78747706 = yrday
fracday
Element set: 907
Inclination: 51
6371 deg
RA of node: 294
6968 deg
Eccentricity:
0005111
Arg of perigee: 352
6557 deg
Mean anomaly: 7
4519 deg
Mean motion: 15
53216642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3483
Checksum: 332
Coasting Arc #9 (Orbit 3497)
---------------------------------------
Vector Time (GMT): 2019/037/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3929685
68 A = 6788915
71 meter
Y = 4881042
72 meter E =
0004495
Z = -2618881
57 I = 51
28761
XDOT = -2683
287250 Wp = 58
81971
YDOT = -4946
088534 meter/sec RA = 289
26639 deg
ZDOT = -5196
496131 TA = 150
79606
MA = 150
77091
Ha = 223
161 n
mi
Hp = 215
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12892669
55 X = -3971254
09
Y = 16013919
70 feet Y = 4836865
72 meter
Z = -8592131
14 Z = -2638071
13
XDOT = -8803
435858 XDOT = -2602
538263
YDOT = -16227
324585 feet/sec YDOT = -4975
643619 meter/sec
ZDOT = -17048
871820 ZDOT = -5209
333878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -640709
34 X = -195288
21
Y = 20512223
44 feet Y = 6252125
71 meter
Z = -8679254
05 Z = -2645436
63
XDOT = -15200
030613 XDOT = -4632
969331
YDOT = -7706
872429 feet/sec YDOT = -2349
054716 meter/sec
ZDOT = -17106
210503 ZDOT = -5213
972961
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19037
75256925
00016717 00000-0 10270-3 0 9086
2 25544 51
6379 289
8922 0005260 358
1148 1
9984 15
53251309 34985
Satellite: ISS
Catalog Number: 25544
Epoch time: 19037
75256925 = yrday
fracday
Element set: 908
Inclination: 51
6379 deg
RA of node: 289
8922 deg
Eccentricity:
0005260
Arg of perigee: 358
1148 deg
Mean anomaly: 1
9984 deg
Mean motion: 15
53251309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3498
Checksum: 345
Coasting Arc #10 (Orbit 3513)
---------------------------------------
Vector Time (GMT): 2019/038/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4084712
82 A = 6785902
20 meter
Y = -3915746
60 meter E =
0012164
Z = 3732406
72 I = 51
26616
XDOT = 1958
576234 Wp = 72
04531
YDOT = 6089
160215 meter/sec RA = 284
26568 deg
ZDOT = 4237
093176 TA = 332
85437
MA = 332
91791
Ha = 223
052 n
mi
Hp = 215
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13401288
79 X = 4110066
71
Y = -12846937
66 feet Y = -3869926
54 meter
Z = 12245428
88 Z = 3752310
01
XDOT = 6425
775045 XDOT = 1869
759026
YDOT = 19977
559760 feet/sec YDOT = 6110
565986 meter/sec
ZDOT = 13901
224330 ZDOT = 4246
390948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2615780
18 X = 797289
80
Y = -18318798
39 feet Y = -5583569
75 meter
Z = 12335647
39 Z = 3759905
32
XDOT = 15935
641764 XDOT = 4857
183610
YDOT = 11681
115651 feet/sec YDOT = 3560
404051 meter/sec
ZDOT = 13942
480460 ZDOT = 4249
668044
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19038
78199970
00016717 00000-0 10270-3 0 9097
2 25544 51
6365 284
7667 0005019 1
0794 359
0368 15
53244917 35142
Satellite: ISS
Catalog Number: 25544
Epoch time: 19038
78199970 = yrday
fracday
Element set: 909
Inclination: 51
6365 deg
RA of node: 284
7667 deg
Eccentricity:
0005019
Arg of perigee: 1
0794 deg
Mean anomaly: 359
0368 deg
Mean motion: 15
53244917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3514
Checksum: 343
Coasting Arc #11 (Orbit 3527)
---------------------------------------
Vector Time (GMT): 2019/039/16:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2566036
98 A = 6784675
20 meter
Y = -4739373
22 meter E =
0008028
Z = -4126110
79 I = 51
25469
XDOT = 3947
904726 Wp = 70
83430
YDOT = -5392
112790 meter/sec RA = 279
47213 deg
ZDOT = 3746
910960 TA = 237
95873
MA = 238
03674
Ha = 223
266 n
mi
Hp = 215
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8418756
51 X = -2492807
34
Y = -15549124
73 feet Y = -4767659
22 meter
Z = -13537108
89 Z = -4138397
23
XDOT = 12952
443327 XDOT = 3989
707420
YDOT = -17690
658760 feet/sec YDOT = -5347
730610 meter/sec
ZDOT = 12293
014960 ZDOT = 3766
189830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13163451
16 X = -4012219
91
Y = -11742439
35 feet Y = -3579095
51 meter
Z = -13592009
78 Z = -4142844
58
XDOT = 5152
929188 XDOT = 1570
612817
YDOT = -20074
707528 feet/sec YDOT = -6118
770854 meter/sec
ZDOT = 12380
567390 ZDOT = 3773
596941
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19039
68275119
00016717 00000-0 10270-3 0 9109
2 25544 51
6361 280
2833 0005155 4
5488 355
5710 15
53230243 35287
Satellite: ISS
Catalog Number: 25544
Epoch time: 19039
68275119 = yrday
fracday
Element set: 910
Inclination: 51
6361 deg
RA of node: 280
2833 deg
Eccentricity:
0005155
Arg of perigee: 4
5488 deg
Mean anomaly: 355
5710 deg
Mean motion: 15
53230243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3528
Checksum: 300
Coasting Arc #12 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2019/040/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3842927
36 A = 6780882
67 meter
Y = 2387062
96 meter E =
0009838
Z = 5049255
39 I = 51
24356
XDOT = -2111
617338 Wp = 29
45601
YDOT = 7157
346772 meter/sec RA = 275
48187 deg
ZDOT = -1766
650186 TA = 77
78191
MA = 77
67174
Ha = 223
246 n
mi
Hp = 215
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12608029
40 X = 3791422
92
Y = 7831571
40 feet Y = 2429749
59 meter
Z = 16565798
52 Z = 5067797
30
XDOT = -6927
878406 XDOT = -2182
914626
YDOT = 23482
108832 feet/sec YDOT = 7133
334436 meter/sec
ZDOT = -5796
096412 ZDOT = -1777
081043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1779330
87 X = 542340
05
Y = 14641053
04 feet Y = 4462592
97 meter
Z = 16649178
47 Z = 5074669
60
XDOT = -21515
221009 XDOT = -6557
839364
YDOT = 9296
944531 feet/sec YDOT = 2833
708693 meter/sec
ZDOT = -5843
916515 ZDOT = -1781
225754
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19040
51916036
00016717 00000-0 10270-3 0 9114
2 25544 51
6409 276
1240 0005523 4
5515 355
5686 15
53277724 35418
Satellite: ISS
Catalog Number: 25544
Epoch time: 19040
51916036 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 276
1240 deg
Eccentricity:
0005523
Arg of perigee: 4
5515 deg
Mean anomaly: 355
5686 deg
Mean motion: 15
53277724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 296
Coasting Arc #13 (Orbit 3555)
---------------------------------------
Vector Time (GMT): 2019/041/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3556192
49 A = 6783365
15 meter
Y = -3670067
76 meter E =
0009992
Z = -4467980
46 I = 51
24920
XDOT = 2627
300730 Wp = 77
18392
YDOT = -6440
966974 meter/sec RA = 270
46776 deg
ZDOT = 3207
830459 TA = 225
25257
MA = 225
33393
Ha = 223
459 n
mi
Hp = 215
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11667298
19 X = -3493185
82
Y = -12040904
73 feet Y = -3709483
56 meter
Z = -14658728
55 Z = -4485101
60
XDOT = 8619
753050 XDOT = 2683
548554
YDOT = -21131
781411 feet/sec YDOT = -6411
271974 meter/sec
ZDOT = 10524
378146 ZDOT = 3220
729696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1790245
66 X = 545666
88
Y = -16602575
92 feet Y = -5060465
14 meter
Z = -14735570
90 Z = -4491402
01
XDOT = 20472
816656 XDOT = 6240
114517
YDOT = -7161
614447 feet/sec YDOT = -2182
860084 meter/sec
ZDOT = 10583
240011 ZDOT = 3225
771555
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19041
48424858
00016717 00000-0 10270-3 0 9128
2 25544 51
6407 271
3190 0005601 8
6670 351
4578 15
53244189 35561
Satellite: ISS
Catalog Number: 25544
Epoch time: 19041
48424858 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 271
3190 deg
Eccentricity:
0005601
Arg of perigee: 8
6670 deg
Mean anomaly: 351
4578 deg
Mean motion: 15
53244189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 313
Coasting Arc #14 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2019/042/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3226827
04 A = 6786472
13 meter
Y = 4806873
79 meter E =
0014689
Z = 3535168
64 I = 51
26006
XDOT = -3148
158920 Wp = 65
34543
YDOT = 5396
829483 meter/sec RA = 265
46044 deg
ZDOT = -4444
028661 TA = 72
73120
MA = 72
57052
Ha = 223
573 n
mi
Hp = 215
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10586702
89 X = 3155663
73
Y = 15770583
30 feet Y = 4842560
70 meter
Z = 11598322
30 Z = 3550670
08
XDOT = -10328
605379 XDOT = -3186
687463
YDOT = 17706
133473 feet/sec YDOT = 5361
408926 meter/sec
ZDOT = -14580
146527 ZDOT = -4459
414887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5015167
23 X = -1528622
97
Y = 18276278
21 feet Y = 5570609
60 meter
Z = 11667750
78 Z = 3556330
44
XDOT = -18743
014413 XDOT = -5712
870793
YDOT = 4252
472687 feet/sec YDOT = 1296
153675 meter/sec
ZDOT = -14650
106163 ZDOT = -4465
352358
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19042
51367353
00016717 00000-0 10270-3 0 9130
2 25544 51
6401 266
1940 0005733 12
8694 347
2603 15
53269805 35721
Satellite: ISS
Catalog Number: 25544
Epoch time: 19042
51367353 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 266
1940 deg
Eccentricity:
0005733
Arg of perigee: 12
8694 deg
Mean anomaly: 347
2603 deg
Mean motion: 15
53269805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 305
Coasting Arc #15 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2019/043/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2890079
00 A = 6789499
19 meter
Y = -5657129
93 meter E =
0010789
Z = -2384982
93 I = 51
27319
XDOT = 3653
236767 Wp = 30
73783
YDOT = -4110
121106 meter/sec RA = 260
46043 deg
ZDOT = 5342
034877 TA = 302
48417
MA = 302
58841
Ha = 223
638 n
mi
Hp = 215
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9481886
49 X = -2815019
79
Y = -18560137
56 feet Y = -5689029
21 meter
Z = -7824747
15 Z = -2398839
19
XDOT = 11985
684932 XDOT = 3672
977441
YDOT = -13484
649298 feet/sec YDOT = -4069
157498 meter/sec
ZDOT = 17526
361145 ZDOT = 5359
828820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7495929
25 X = 2284759
24
Y = -19422225
94 feet Y = -5919894
47 meter
Z = -7886680
53 Z = -2403860
23
XDOT = 16545
368643 XDOT = 5043
028362
YDOT = -737
758559 feet/sec YDOT = -224
868809 meter/sec
ZDOT = 17607
043701 ZDOT = 5366
626920
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19043
47875941
00016717 00000-0 10270-3 0 9144
2 25544 51
6398 261
3894 0005659 14
7846 345
3471 15
53226794 35876
Satellite: ISS
Catalog Number: 25544
Epoch time: 19043
47875941 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 261
3894 deg
Eccentricity:
0005659
Arg of perigee: 14
7846 deg
Mean anomaly: 345
3471 deg
Mean motion: 15
53226794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 354
Coasting Arc #16 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2019/044/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2463161
75 A = 6791489
84 meter
Y = 6242777
14 meter E =
0013366
Z = 1020221
25 I = 51
28704
XDOT = -4179
404926 Wp = 99
76079
YDOT = 2618
286385 meter/sec RA = 255
46639 deg
ZDOT = -5867
234136 TA = 69
13401
MA = 68
99094
Ha = 223
782 n
mi
Hp = 215
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8081239
33 X = 2388214
58
Y = 20481552
29 feet Y = 6269902
89 meter
Z = 3347182
58 Z = 1032004
08
XDOT = -13711
958420 XDOT = -4179
873289
YDOT = 8590
178430 feet/sec YDOT = 2571
546637 meter/sec
ZDOT = -19249
455828 ZDOT = -5887
537068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9500807
44 X = -2895846
11
Y = 19853982
37 feet Y = 6051493
83 meter
Z = 3399718
58 Z = 1036234
22
XDOT = -14093
671220 XDOT = -4295
750988
YDOT = -3397
158816 feet/sec YDOT = -1035
454007 meter/sec
ZDOT = -19341
305976 ZDOT = -5895
230062
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19044
50818230
00016717 00000-0 10270-3 0 9158
2 25544 51
6404 256
2640 0005631 19
7309 340
4060 15
53229111 36030
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
50818230 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 256
2640 deg
Eccentricity:
0005631
Arg of perigee: 19
7309 deg
Mean anomaly: 340
4060 deg
Mean motion: 15
53229111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 272
Coasting Arc #17 (Orbit 3605)
---------------------------------------
Vector Time (GMT): 2019/044/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4441284
09 A = 6783083
78 meter
Y = 2344494
89 meter E =
0012949
Z = 4554917
11 I = 51
25724
XDOT = -581
377782 Wp = 50
74437
YDOT = 7020
104191 meter/sec RA = 254
52567 deg
ZDOT = -3032
629429 TA = 69
78840
MA = 69
64920
Ha = 223
683 n
mi
Hp = 215
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14571142
04 X = 4392612
21
Y = 7691912
35 feet Y = 2393888
35 meter
Z = 14943953
77 Z = 4576372
70
XDOT = -1907
407420 XDOT = -645
104704
YDOT = 23031
837897 feet/sec YDOT = 7013
246453 meter/sec
ZDOT = -9949
571618 ZDOT = -3035
608397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16209105
27 X = 4940535
29
Y = 2419357
59 feet Y = 737420
19 meter
Z = 15040514
13 Z = 4584348
71
XDOT = 6131
688329 XDOT = 1868
938603
YDOT = 21141
927628 feet/sec YDOT = 6444
059541 meter/sec
ZDOT = -9963
703879 ZDOT = -3036
936942
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19044
70120045
00016717 00000-0 10270-3 0 9161
2 25544 51
6373 255
2977 0005242 24
9591 335
1814 15
53212411 36062
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
70120045 = yrday
fracday
Element set: 916
Inclination: 51
6373 deg
RA of node: 255
2977 deg
Eccentricity:
0005242
Arg of perigee: 24
9591 deg
Mean anomaly: 335
1814 deg
Mean motion: 15
53212411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3606
Checksum: 287
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