[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 29th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
146/20:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
6
148/06:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
6
153/12:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
9
154/09:16:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
0
156/19:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
1
157/11:12:41
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
2
159/13:07:21
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 214
3
Coasting Arc #1 (Orbit 3497)
---------------------------------------
Vector Time (GMT): 2018/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3947370
48 A = 6789095
84 meter
Y = 5470175
50 meter E =
0011783
Z = -738636
40 I = 51
93927
XDOT = -4233
412892 Wp = 59
54314
YDOT = -2257
945615 meter/sec RA = 130
73318 deg
ZDOT = 5978
705553 TA = 292
51067
MA = 292
63536
Ha = 222
354 n
mi
Hp = 213
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12950690
56 X = -4004658
16
Y = 17946770
00 feet Y = 5425713
00 meter
Z = -2423347
78 Z = -757950
47
XDOT = -13889
149908 XDOT = -4236
891040
YDOT = -7407
958053 feet/sec YDOT = -2305
306299 meter/sec
ZDOT = 19615
175699 ZDOT = 5958
132290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9825093
64 X = 2994688
54
Y = 19820315
50 feet Y = 6041232
17 meter
Z = -2510414
74 Z = -765174
41
XDOT = -11652
319189 XDOT = -3551
626889
YDOT = 8218
225920 feet/sec YDOT = 2504
915260 meter/sec
ZDOT = 19523
440415 ZDOT = 5950
744639
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 18145
50148080
00016717 00000-0 10270-3 0 9002
2 25544 51
6362 131
8073 0003982 119
1445 241
0107 15
54121639 34981
Satellite: ISS
Catalog Number: 25544
Epoch time: 18145
50148080 = yrday
fracday
Element set: 900
Inclination: 51
6362 deg
RA of node: 131
8073 deg
Eccentricity:
0003982
Arg of perigee: 119
1445 deg
Mean anomaly: 241
0107 deg
Mean motion: 15
54121639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3498
Checksum: 287
Coasting Arc #2 (Orbit 3513)
---------------------------------------
Vector Time (GMT): 2018/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4529063
09 A = 6789021
72 meter
Y = -4951444
85 meter E =
0013421
Z = -995510
73 I = 51
96025
XDOT = 2936
334509 Wp = 135
46283
YDOT = 3867
506977 meter/sec RA = 125
78352 deg
ZDOT = -5934
883284 TA = 55
27566
MA = 55
14933
Ha = 222
367 n
mi
Hp = 213
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14859130
86 X = 4588930
62
Y = -16244897
81 feet Y = -4900462
95 meter
Z = -3266111
31 Z = -973364
69
XDOT = 9633
643401 XDOT = 2921
697710
YDOT = 12688
671186 feet/sec YDOT = 3900
261633 meter/sec
ZDOT = -19471
401849 ZDOT = -5920
654680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7767379
03 X = -2367497
13
Y = -20615516
98 feet Y = -6283609
58 meter
Z = -3166423
90 Z = -965126
00
XDOT = 14226
035339 XDOT = 4336
095571
YDOT = -2408
934794 feet/sec YDOT = -734
243325 meter/sec
ZDOT = -19408
247721 ZDOT = -5915
633905
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 18146
53033623
00016717 00000-0 10270-3 0 9013
2 25544 51
6370 126
6772 0003778 119
3990 240
7540 15
54097749 35148
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
53033623 = yrday
fracday
Element set: 901
Inclination: 51
6370 deg
RA of node: 126
6772 deg
Eccentricity:
0003778
Arg of perigee: 119
3990 deg
Mean anomaly: 240
7540 deg
Mean motion: 15
54097749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3514
Checksum: 315
Coasting Arc #3 (Orbit 3519)
---------------------------------------
Vector Time (GMT): 2018/146/20:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -738853
73 A = 6781099
56 meter
Y = -5090495
70 meter E =
0011746
Z = 4409339
90 I = 51
94266
XDOT = 5746
587505 Wp = 83
60902
YDOT = -3784
465899 meter/sec RA = 123
89412 deg
ZDOT = -3397
147398 TA = 40
64511
MA = 40
55749
Ha = 222
175 n
mi
Hp = 213
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2424060
78 X = -703294
07
Y = -16701101
38 feet Y = -5098559
56 meter
Z = 14466338
24 Z = 4405836
76
XDOT = 18853
633546 XDOT = 5804
981143
YDOT = -12416
226704 feet/sec YDOT = -3719
876860 meter/sec
ZDOT = -11145
496713 ZDOT = -3369
090473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7590710
63 X = 2313648
60
Y = 15087024
48 feet Y = 4598525
06 meter
Z = 14451318
44 Z = 4404761
86
XDOT = -13023
850634 XDOT = -3969
669673
YDOT = 17136
216621 feet/sec YDOT = 5223
118826 meter/sec
ZDOT = -11019
510568 ZDOT = -3358
746821
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 18146
91615415
00016717 00000-0 10270-3 0 9021
2 25544 51
6383 124
7535 0003390 122
5009 237
6471 15
54123869 35203
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
91615415 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 124
7535 deg
Eccentricity:
0003390
Arg of perigee: 122
5009 deg
Mean anomaly: 237
6471 deg
Mean motion: 15
54123869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 298
Coasting Arc #4 (Orbit 3534)
---------------------------------------
Vector Time (GMT): 2018/147/20:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -380481
29 A = 6784919
51 meter
Y = 5946860
32 meter E =
0007546
Z = -3252414
12 I = 51
97108
XDOT = -5532
101823 Wp = 102
23571
YDOT = 2262
306655 meter/sec RA = 118
92971 deg
ZDOT = 4791
481532 TA = 220
30440
MA = 220
36036
Ha = 222
180 n
mi
Hp = 213
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1248298
19 X = -431153
66
Y = 19510696
58 feet Y = 5942322
48 meter
Z = -10670650
00 Z = -3254384
93
XDOT = -18149
940364 XDOT = -5580
263263
YDOT = 7422
265928 feet/sec YDOT = 2200
173159 meter/sec
ZDOT = 15720
083766 ZDOT = 4764
491289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5275629
51 X = -1608011
88
Y = -18819896
01 feet Y = -5736304
30 meter
Z = -10680241
02 Z = -3255337
46
XDOT = 13444
106333 XDOT = 4097
763610
YDOT = -12606
568821 feet/sec YDOT = -3842
482177 meter/sec
ZDOT = 15599
047384 ZDOT = 4754
589643
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 18147
88070465
00016717 00000-0 10270-3 0 9039
2 25544 51
6366 119
9449 0003554 127
8246 232
3229 15
54100484 35354
Satellite: ISS
Catalog Number: 25544
Epoch time: 18147
88070465 = yrday
fracday
Element set: 903
Inclination: 51
6366 deg
RA of node: 119
9449 deg
Eccentricity:
0003554
Arg of perigee: 127
8246 deg
Mean anomaly: 232
3229 deg
Mean motion: 15
54100484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3535
Checksum: 317
Coasting Arc #5 (Orbit 3541)
---------------------------------------
Vector Time (GMT): 2018/148/06:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4705465
07 A = 6779854
62 meter
Y = 1023899
06 meter E =
0011419
Z = 4766746
48 I = 51
96215
XDOT = 1218
840805 Wp = 121
86576
YDOT = -7072
680605 meter/sec RA = 116
97171 deg
ZDOT = 2711
764455 TA = 301
41347
MA = 301
52509
Ha = 222
349 n
mi
Hp = 213
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15437877
51 X = -4739719
58
Y = 3359248
90 feet Y = 971087
31 meter
Z = 15638932
04 Z = 4743805
50
XDOT = 3998
821539 XDOT = 1284
666335
YDOT = -23204
332695 feet/sec YDOT = -7058
682905 meter/sec
ZDOT = 8896
865010 ZDOT = 2717
844435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15879669
58 X = -4840123
29
Y = -807729
22 feet Y = -246195
87 meter
Z = 15536166
77 Z = 4735423
63
XDOT = 9794
542567 XDOT = 2985
376574
YDOT = -20215
851667 feet/sec YDOT = -6161
791588 meter/sec
ZDOT = 8924
993454 ZDOT = 2720
338005
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 18148
33082752
00016717 00000-0 10270-3 0 9043
2 25544 51
6383 117
7018 0003752 130
2982 229
8499 15
54111642 35422
Satellite: ISS
Catalog Number: 25544
Epoch time: 18148
33082752 = yrday
fracday
Element set: 904
Inclination: 51
6383 deg
RA of node: 117
7018 deg
Eccentricity:
0003752
Arg of perigee: 130
2982 deg
Mean anomaly: 229
8499 deg
Mean motion: 15
54111642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3542
Checksum: 309
Coasting Arc #6 (Orbit 3556)
---------------------------------------
Vector Time (GMT): 2018/149/06:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4198952
75 A = 6777728
99 meter
Y = 659977
49 meter E =
0017156
Z = -5293922
74 I = 51
97028
XDOT = -2218
204893 Wp = 92
97992
YDOT = 7277
399963 meter/sec RA = 111
99660 deg
ZDOT = -855
403032 TA = 168
88434
MA = 168
84639
Ha = 222
229 n
mi
Hp = 213
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13776091
71 X = 4216976
10
Y = 2165280
47 feet Y = 707034
47 meter
Z = -17368512
93 Z = -5273481
52
XDOT = -7277
575107 XDOT = -2295
262750
YDOT = 23875
984132 feet/sec YDOT = 7252
163714 meter/sec
ZDOT = -2806
440394 ZDOT = -866
364762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12942416
17 X = 3944848
45
Y = 5488943
25 feet Y = 1673029
90 meter
Z = -17277145
29 Z = -5266073
88
XDOT = -12466
721155 XDOT = -3799
856608
YDOT = 20438
068356 feet/sec YDOT = 6229
523235 meter/sec
ZDOT = -2856
458718 ZDOT = -870
648617
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 18149
29537441
00016717 00000-0 10270-3 0 9050
2 25544 51
6397 112
8933 0003739 132
6415 227
5053 15
54087375 35573
Satellite: ISS
Catalog Number: 25544
Epoch time: 18149
29537441 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 112
8933 deg
Eccentricity:
0003739
Arg of perigee: 132
6415 deg
Mean anomaly: 227
5053 deg
Mean motion: 15
54087375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3557
Checksum: 327
Coasting Arc #7 (Orbit 3572)
---------------------------------------
Vector Time (GMT): 2018/150/06:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3571363
55 A = 6777714
55 meter
Y = -2357638
41 meter E =
0005802
Z = 5250828
01 I = 51
98198
XDOT = 3016
382638 Wp = 95
72318
YDOT = -6972
554317 meter/sec RA = 107
02071 deg
ZDOT = -1078
642781 TA = 4
55792
MA = 4
55264
Ha = 222
269 n
mi
Hp = 213
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11717072
01 X = -3570240
43
Y = -7735034
16 feet Y = -2397570
28 meter
Z = 17227126
02 Z = 5233481
75
XDOT = 9896
268498 XDOT = 3099
367008
YDOT = -22875
834374 feet/sec YDOT = -6938
358911 meter/sec
ZDOT = -3538
854268 ZDOT = -1063
789430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9762586
93 X = -2975636
50
Y = -10221035
67 feet Y = -3115371
67 meter
Z = 17149831
69 Z = 5227268
70
XDOT = 14115
609421 XDOT = 4302
437751
YDOT = -19309
714300 feet/sec YDOT = -5885
600919 meter/sec
ZDOT = -3471
441256 ZDOT = -1058
095295
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 18150
32421985
00016717 00000-0 10270-3 0 9062
2 25544 51
6396 107
7653 0003697 134
4885 225
6571 15
54128113 35736
Satellite: ISS
Catalog Number: 25544
Epoch time: 18150
32421985 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 107
7653 deg
Eccentricity:
0003697
Arg of perigee: 134
4885 deg
Mean anomaly: 225
6571 deg
Mean motion: 15
54128113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3573
Checksum: 322
Coasting Arc #8 (Orbit 3587)
---------------------------------------
Vector Time (GMT): 2018/151/06:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2903761
10 A = 6780177
85 meter
Y = 3956572
70 meter E =
0013939
Z = -4691767
44 I = 51
99946
XDOT = -3617
488521 Wp = 116
66828
YDOT = 6093
306158 meter/sec RA = 102
04838 deg
ZDOT = 2900
163481 TA = 182
05824
MA = 182
06398
Ha = 222
130 n
mi
Hp = 213
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9526775
26 X = 2882092
15
Y = 12980881
56 feet Y = 3988924
07 meter
Z = -15392937
79 Z = -4677713
90
XDOT = -11868
400658 XDOT = -3699
444276
YDOT = 19991
161936 feet/sec YDOT = 6052
394255 meter/sec
ZDOT = 9514
972052 ZDOT = 2882
392615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6679250
24 X = 2035835
47
Y = 14716168
79 feet Y = 4485488
25 meter
Z = -15330598
78 Z = -4672766
51
XDOT = -14800
395233 XDOT = -4511
160467
YDOT = 16544
088450 feet/sec YDOT = 5042
638160 meter/sec
ZDOT = 9434
602663 ZDOT = 2875
666892
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 18151
28876287
00016717 00000-0 10270-3 0 9078
2 25544 51
6404 102
9573 0003671 137
1553 222
9887 15
54100813 35881
Satellite: ISS
Catalog Number: 25544
Epoch time: 18151
28876287 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 102
9573 deg
Eccentricity:
0003671
Arg of perigee: 137
1553 deg
Mean anomaly: 222
9887 deg
Mean motion: 15
54100813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3588
Checksum: 323
Coasting Arc #9 (Orbit 3603)
---------------------------------------
Vector Time (GMT): 2018/152/06:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2191323
72 A = 6783775
80 meter
Y = -5291716
58 meter E =
0014470
Z = 3621046
08 I = 52
01713
XDOT = 4084
616956 Wp = 98
28325
YDOT = -4740
321058 meter/sec RA = 97
08555 deg
ZDOT = -4442
469345 TA = 39
03064
MA = 38
92631
Ha = 222
116 n
mi
Hp = 213
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7189382
27 X = -2149576
67
Y = -17361274
87 feet Y = -5315988
57 meter
Z = 11880072
42 Z = 3610501
95
XDOT = 13400
974264 XDOT = 4158
900252
YDOT = -15552
234443 feet/sec YDOT = -4694
228076 meter/sec
ZDOT = -14575
030660 ZDOT = -4422
447824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3766846
10 X = -1148134
69
Y = -18439448
34 feet Y = -5620343
85 meter
Z = 11833630
83 Z = 3606890
68
XDOT = 14910
047901 XDOT = 4544
582600
YDOT = -12369
167447 feet/sec YDOT = -3770
122238 meter/sec
ZDOT = -14484
759608 ZDOT = -4414
954729
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 18152
31760486
00016717 00000-0 10270-3 0 9087
2 25544 51
6398 97
8291 0003682 139
9900 220
1524 15
54138885 36047
Satellite: ISS
Catalog Number: 25544
Epoch time: 18152
31760486 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 97
8291 deg
Eccentricity:
0003682
Arg of perigee: 139
9900 deg
Mean anomaly: 220
1524 deg
Mean motion: 15
54138885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3604
Checksum: 328
Coasting Arc #10 (Orbit 3618)
---------------------------------------
Vector Time (GMT): 2018/153/06:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1491148
59 A = 6787183
12 meter
Y = 6243533
54 meter E =
0006600
Z = -2207339
06 I = 52
03348
XDOT = -4410
020882 Wp = 76
79553
YDOT = 2993
973477 meter/sec RA = 92
13291 deg
ZDOT = 5504
664078 TA = 258
84429
MA = 258
91850
Ha = 222
004 n
mi
Hp = 213
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4892219
78 X = 1431942
99
Y = 20484033
91 feet Y = 6259877
86 meter
Z = -7241926
06 Z = -2200238
48
XDOT = -14468
572447 XDOT = -4469
911392
YDOT = 9822
747627 feet/sec YDOT = 2944
321949 meter/sec
ZDOT = 18059
921517 ZDOT = 5483
096605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1240080
31 X = 377976
48
Y = 21034211
65 feet Y = 6411227
71 meter
Z = -7211039
74 Z = -2197924
91
XDOT = -14561
295235 XDOT = -4438
282787
YDOT = 6999
372063 feet/sec YDOT = 2133
408605 meter/sec
ZDOT = 17962
965089 ZDOT = 5475
111759
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 18153
28214207
00016717 00000-0 10270-3 0 9090
2 25544 51
6415 93
0214 0003763 143
1432 216
9980 15
54160438 36191
Satellite: ISS
Catalog Number: 25544
Epoch time: 18153
28214207 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 93
0214 deg
Eccentricity:
0003763
Arg of perigee: 143
1432 deg
Mean anomaly: 216
9980 deg
Mean motion: 15
54160438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3619
Checksum: 295
Coasting Arc #11 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2018/153/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3571086
74 A = 6780866
02 meter
Y = -3624381
51 meter E =
0010862
Z = -4491994
72 I = 52
01109
XDOT = 2450
990330 Wp = 86
93626
YDOT = 6473
200973 meter/sec RA = 90
98690 deg
ZDOT = -3280
672156 TA = 150
17692
MA = 150
11497
Ha = 221
966 n
mi
Hp = 213
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11716163
83 X = 3633169
95
Y = -11891015
45 feet Y = -3584099
41 meter
Z = -14737515
48 Z = -4474497
28
XDOT = 8041
306856 XDOT = 2394
358879
YDOT = 21237
536001 feet/sec YDOT = 6500
293441 meter/sec
ZDOT = -10763
360092 ZDOT = -3268
902716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8756199
00 X = -2668889
46
Y = -14293744
23 feet Y = -4356733
24 meter
Z = -14658682
11 Z = -4467966
31
XDOT = 21511
428736 XDOT = 6556
683479
YDOT = -2213
752604 feet/sec YDOT = -674
751794 meter/sec
ZDOT = -10711
612541 ZDOT = -3264
899502
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 18153
53935274
00016717 00000-0 10270-3 0 9104
2 25544 51
6402 91
7390 0003404 142
6629 217
4760 15
54132804 36234
Satellite: ISS
Catalog Number: 25544
Epoch time: 18153
53935274 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 91
7390 deg
Eccentricity:
0003404
Arg of perigee: 142
6629 deg
Mean anomaly: 217
4760 deg
Mean motion: 15
54132804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3623
Checksum: 292
Coasting Arc #12 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2018/154/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3516053
61 A = 6779833
74 meter
Y = 3329381
96 meter E =
0010876
Z = 4740803
10 I = 52
00527
XDOT = -2561
471388 Wp = 126
83792
YDOT = -6676
034263 meter/sec RA = 86
67533 deg
ZDOT = 2777
989031 TA = 295
75000
MA = 295
86221
Ha = 221
935 n
mi
Hp = 213
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11535608
95 X = -3576050
69
Y = 10923169
18 feet Y = 3289726
95 meter
Z = 15553815
95 Z = 4723578
02
XDOT = -8403
777520 XDOT = -2500
121788
YDOT = -21902
999551 feet/sec YDOT = -6704
335735 meter/sec
ZDOT = 9114
137242 ZDOT = 2765
694418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4608204
47 X = -1404580
72
Y = 15282594
42 feet Y = 4658134
78 meter
Z = 15476234
97 Z = 4717156
42
XDOT = -17175
033100 XDOT = -5234
950089
YDOT = -14389
558921 feet/sec YDOT = -4385
937559 meter/sec
ZDOT = 9060
075899 ZDOT = 2761
511134
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 18154
43958393
00016717 00000-0 10270-3 0 9112
2 25544 51
6380 87
2521 0003423 149
8953 210
2397 15
54144983 36378
Satellite: ISS
Catalog Number: 25544
Epoch time: 18154
43958393 = yrday
fracday
Element set: 911
Inclination: 51
6380 deg
RA of node: 87
2521 deg
Eccentricity:
0003423
Arg of perigee: 149
8953 deg
Mean anomaly: 210
2397 deg
Mean motion: 15
54144983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 324
Coasting Arc #13 (Orbit 3651)
---------------------------------------
Vector Time (GMT): 2018/155/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3938865
30 A = 6777664
13 meter
Y = -1617686
15 meter E =
0016021
Z = -5286639
39 I = 51
99517
XDOT = 1803
253372 Wp = 94
46465
YDOT = 7384
458520 meter/sec RA = 81
70216 deg
ZDOT = -919
681693 TA = 166
78834
MA = 166
74633
Ha = 221
871 n
mi
Hp = 214
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12922786
40 X = 3982341
66
Y = -5307369
26 feet Y = -1573395
33 meter
Z = -17344617
41 Z = -5267400
34
XDOT = 5916
185604 XDOT = 1725
011641
YDOT = 24227
226115 feet/sec YDOT = 7404
186373 meter/sec
ZDOT = -3017
328389 ZDOT = -911
111277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8437394
50 X = 2571717
85
Y = -11267875
71 feet Y = -3434448
51 meter
Z = -17258264
14 Z = -5260318
91
XDOT = 16749
915093 XDOT = 5105
374120
YDOT = 17088
487426 feet/sec YDOT = 5208
570967 meter/sec
ZDOT = -2980
049706 ZDOT = -908
319150
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 18155
40411752
00016717 00000-0 10270-3 0 9124
2 25544 51
6384 82
4432 0003437 151
7291 208
4049 15
54116995 36524
Satellite: ISS
Catalog Number: 25544
Epoch time: 18155
40411752 = yrday
fracday
Element set: 912
Inclination: 51
6384 deg
RA of node: 82
4432 deg
Eccentricity:
0003437
Arg of perigee: 151
7291 deg
Mean anomaly: 208
4049 deg
Mean motion: 15
54116995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3652
Checksum: 302
Coasting Arc #14 (Orbit 3667)
---------------------------------------
Vector Time (GMT): 2018/156/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4264855
67 A = 6777703
35 meter
Y = -171024
56 meter E =
0004623
Z = 5260858
00 I = 51
99034
XDOT = -958
393294 Wp = 103
09104
YDOT = -7543
274460 meter/sec RA = 76
72687 deg
ZDOT = -1022
437777 TA = 356
64495
MA = 356
64804
Ha = 221
929 n
mi
Hp = 214
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13992308
64 X = -4288180
73
Y = -561104
22 feet Y = -218848
09 meter
Z = 17260032
81 Z = 5240084
14
XDOT = -3144
334954 XDOT = -869
004641
YDOT = -24748
275787 feet/sec YDOT = -7553
491964 meter/sec
ZDOT = -3354
454649 ZDOT = -1026
877002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12258946
47 X = -3736526
88
Y = 7001300
41 feet Y = 2133996
37 meter
Z = 17167070
09 Z = 5232522
96
XDOT = -15253
094759 XDOT = -4649
143283
YDOT = -18438
563772 feet/sec YDOT = -5620
074238 meter/sec
ZDOT = -3373
206838 ZDOT = -1028
153444
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 18156
43294876
00016717 00000-0 10270-3 0 9135
2 25544 51
6391 77
3148 0003337 155
1462 204
9852 15
54125104 36688
Satellite: ISS
Catalog Number: 25544
Epoch time: 18156
43294876 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 77
3148 deg
Eccentricity:
0003337
Arg of perigee: 155
1462 deg
Mean anomaly: 204
9852 deg
Mean motion: 15
54125104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 317
Coasting Arc #15 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2018/156/19:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4062055
20 A = 6783776
37 meter
Y = 4043105
07 meter E =
0007975
Z = -3639142
27 I = 52
00660
XDOT = -1949
666365 Wp = 121
54594
YDOT = 5939
619336 meter/sec RA = 74
59996 deg
ZDOT = 4425
771350 TA = 195
59648
MA = 195
62107
Ha = 221
837 n
mi
Hp = 214
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13326952
75 X = 4034219
23
Y = 13264780
42 feet Y = 4088374
49 meter
Z = -11939443
13 Z = -3619477
41
XDOT = -6396
543192 XDOT = -2037
437981
YDOT = 19486
940079 feet/sec YDOT = 5917
325622 meter/sec
ZDOT = 14520
247210 ZDOT = 4416
087951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14573000
13 X = -4441850
44
Y = -11969529
40 feet Y = -3648312
56 meter
Z = -11852021
11 Z = -3612496
03
XDOT = 3792
773848 XDOT = 1156
037469
YDOT = -18941
600280 feet/sec YDOT = -5773
399765 meter/sec
ZDOT = 14476
017176 ZDOT = 4412
290035
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 18156
81875946
00016717 00000-0 10270-3 0 9141
2 25544 51
6383 75
3877 0003737 157
1691 202
9628 15
54137579 36741
Satellite: ISS
Catalog Number: 25544
Epoch time: 18156
81875946 = yrday
fracday
Element set: 914
Inclination: 51
6383 deg
RA of node: 75
3877 deg
Eccentricity:
0003737
Arg of perigee: 157
1691 deg
Mean anomaly: 202
9628 deg
Mean motion: 15
54137579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 356
Coasting Arc #16 (Orbit 3684)
---------------------------------------
Vector Time (GMT): 2018/157/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -95700
63 A = 6786314
40 meter
Y = 6235930
94 meter E =
0014455
Z = 2663220
37 I = 52
01057
XDOT = -5097
934506 Wp = 90
56363
YDOT = -2325
238804 meter/sec RA = 71
39772 deg
ZDOT = 5236
762896 TA = 299
32364
MA = 299
46798
Ha = 221
701 n
mi
Hp = 214
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -313978
43 X = -178361
94
Y = 20459091
02 feet Y = 6234398
32 meter
Z = 8737599
64 Z = 2662555
29
XDOT = -16725
506908 XDOT = -5096
991627
YDOT = -7628
736232 feet/sec YDOT = -2382
242630 meter/sec
ZDOT = 17180
980631 ZDOT = 5212
000935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17910211
78 X = 5459032
55
Y = 9897760
34 feet Y = 3016837
35 meter
Z = 8733687
06 Z = 2662027
82
XDOT = -13895
566224 XDOT = -4235
368585
YDOT = 10010
263954 feet/sec YDOT = 3051
128453 meter/sec
ZDOT = 17070
489130 ZDOT = 5203
085087
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 18157
52607886
00016717 00000-0 10270-3 0 9157
2 25544 51
6398 71
8661 0003276 158
7211 201
4078 15
54133273 36854
Satellite: ISS
Catalog Number: 25544
Epoch time: 18157
52607886 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 71
8661 deg
Eccentricity:
0003276
Arg of perigee: 158
7211 deg
Mean anomaly: 201
4078 deg
Mean motion: 15
54133273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3685
Checksum: 325
Coasting Arc #17 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2018/158/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1085603
18 A = 6782441
85 meter
Y = -5361852
48 meter E =
0007655
Z = -4015018
84 I = 51
98752
XDOT = 5156
824060 Wp = 96
95220
YDOT = 4025
536997 meter/sec RA = 66
44008 deg
ZDOT = -3988
971276 TA = 131
72222
MA = 131
65672
Ha = 221
600 n
mi
Hp = 214
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3561690
23 X = 1164983
12
Y = -17591379
53 feet Y = -5349268
34 meter
Z = -13172633
99 Z = -4009552
99
XDOT = 16918
714109 XDOT = 5130
802531
YDOT = 13207
142378 feet/sec YDOT = 4083
059001 meter/sec
ZDOT = -13087
176104 ZDOT = -3963
983972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14038091
24 X = -4278810
21
Y = -11213368
09 feet Y = -3417834
59 meter
Z = -13147354
41 Z = -4007313
62
XDOT = 18653
077916 XDOT = 5685
458149
YDOT = -8166
528051 feet/sec YDOT = -2489
157750 meter/sec
ZDOT = -12975
939105 ZDOT = -3955
066239
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 18158
49060235
00016717 00000-0 10270-3 0 9166
2 25544 51
6409 67
0579 0003214 162
5922 197
5342 15
54157005 37002
Satellite: ISS
Catalog Number: 25544
Epoch time: 18158
49060235 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 67
0579 deg
Eccentricity:
0003214
Arg of perigee: 162
5922 deg
Mean anomaly: 197
5342 deg
Mean motion: 15
54157005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 302
Coasting Arc #18 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2018/159/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2120527
54 A = 6779008
83 meter
Y = 4153500
49 meter E =
0009243
Z = 4916932
32 I = 51
96228
XDOT = -4988
297105 Wp = 136
08554
YDOT = -5334
193217 meter/sec RA = 61
47155 deg
ZDOT = 2345
551747 TA = 291
01968
MA = 291
11852
Ha = 221
552 n
mi
Hp = 214
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6957111
34 X = -2190699
54
Y = 13626970
12 feet Y = 4129394
52 meter
Z = 16131667
72 Z = 4906461
38
XDOT = -16365
804150 XDOT = -4939
671487
YDOT = -17500
633914 feet/sec YDOT = -5389
704109 meter/sec
ZDOT = 7695
379749 ZDOT = 2321
437809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9170913
99 X = 2795294
58
Y = 12309366
82 feet Y = 3751895
01 meter
Z = 16084161
19 Z = 4902452
33
XDOT = -22017
133912 XDOT = -6710
822416
YDOT = 6449
057286 feet/sec YDOT = 1965
672661 meter/sec
ZDOT = 7588
262983 ZDOT = 2312
902557
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 18159
51942260
00016717 00000-0 10270-3 0 9178
2 25544 51
6412 61
9293 0003264 168
2532 191
8698 15
54168441 37161
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
51942260 = yrday
fracday
Element set: 917
Inclination: 51
6412 deg
RA of node: 61
9293 deg
Eccentricity:
0003264
Arg of perigee: 168
2532 deg
Mean anomaly: 191
8698 deg
Mean motion: 15
54168441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 323
Coasting Arc #19 (Orbit 3716)
---------------------------------------
Vector Time (GMT): 2018/159/13:07:21
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4579677
96 A = 6786900
74 meter
Y = -4374013
96 meter E =
0015642
Z = 2416789
54 I = 51
98814
XDOT = 2000
660482 Wp = 116
49891
YDOT = -5083
195381 meter/sec RA = 61
03882 deg
ZDOT = -5388
614206 TA = 36
59468
MA = 36
48793
Ha = 221
634 n
mi
Hp = 214
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15025190
17 X = -4542165
74
Y = -14350439
49 feet Y = -4425017
53 meter
Z = 7929099
54 Z = 2394633
63
XDOT = 6563
846725 XDOT = 2083
528706
YDOT = -16677
150200 feet/sec YDOT = -5060
358812 meter/sec
ZDOT = -17679
180465 ZDOT = -5378
694779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13587612
95 X = -4141504
43
Y = 15767705
66 feet Y = 4805996
69 meter
Z = 7830600
55 Z = 2386767
05
XDOT = -15838
377827 XDOT = -4827
537562
YDOT = -4858
001495 feet/sec YDOT = -1480
718856 meter/sec
ZDOT = -17633
998977 ZDOT = -5374
842888
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 18159
58372480
00016717 00000-0 10270-3 0 9187
2 25544 51
6424 61
6098 0003257 166
9867 193
1371 15
54133682 37175
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
58372480 = yrday
fracday
Element set: 918
Inclination: 51
6424 deg
RA of node: 61
6098 deg
Eccentricity:
0003257
Arg of perigee: 166
9867 deg
Mean anomaly: 193
1371 deg
Mean motion: 15
54133682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3717
Checksum: 336
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