[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 22nd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 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
174/08:16:46
599 0
3 1
3 1
4
N/A -1
0 -0
1 220
7
000/00:03:33
198 -0
9 -0
0 215
8
179/14:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
1
180/09:42:42
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
0
183/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 216
2
Coasting Arc #1 (Orbit 3933)
---------------------------------------
Vector Time (GMT): 2018/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5739603
94 A = 6786729
42 meter
Y = 2732783
24 meter E =
0012638
Z = 2356643
41 I = 51
59885
XDOT = -3993
099910 Wp = 118
16147
YDOT = -3727
667185 meter/sec RA = 351
62754 deg
ZDOT = -5386
375686 TA = 35
50801
MA = 35
42396
Ha = 220
298 n
mi
Hp = 215
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18830721
59 X = -5781183
45
Y = 8965824
29 feet Y = 2668366
31 meter
Z = 7731769
72 Z = 2328661
64
XDOT = -13100
721489 XDOT = -3924
955117
YDOT = -12229
879217 feet/sec YDOT = -3771
939217 meter/sec
ZDOT = -17671
836240 ZDOT = -5405
607684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8882647
30 X = 2707430
90
Y = 18921093
59 feet Y = 5767149
33 meter
Z = 7606125
04 Z = 2318346
91
XDOT = -10908
985084 XDOT = -3325
058654
YDOT = 12281
275399 feet/sec YDOT = 3743
332741 meter/sec
ZDOT = -17757
264186 ZDOT = -5412
414124
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 18173
53679396
00016717 00000-0 10270-3 0 9005
2 25544 51
6382 352
0434 0002875 227
3320 132
7590 15
54239345 39346
Satellite: ISS
Catalog Number: 25544
Epoch time: 18173
53679396 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 352
0434 deg
Eccentricity:
0002875
Arg of perigee: 227
3320 deg
Mean anomaly: 132
7590 deg
Mean motion: 15
54239345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3934
Checksum: 315
Coasting Arc #2 (Orbit 3946)
---------------------------------------
Vector Time (GMT): 2018/174/08:18:33
198
Vector Time (MET): N/A
Weight (LBS) : 922891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6123217
40 A = 6786513
28 meter
Y = -896626
59 meter E =
0005240
Z = -2779699
30 I = 51
57058
XDOT = 3029
084911 Wp = 163
53297
YDOT = -4835
899980 meter/sec RA = 347
45237 deg
ZDOT = -5119
977007 TA = 48
00335
MA = 47
95874
Ha = 220
654 n
mi
Hp = 215
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20089295
92 X = -6099233
63
Y = -2941688
29 feet Y = -964966
21 meter
Z = -9119748
34 Z = -2809385
72
XDOT = 9937
942620 XDOT = 3107
806373
YDOT = -15865
813583 feet/sec YDOT = -4801
585926 meter/sec
ZDOT = -16797
824826 ZDOT = -5105
072057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18059309
35 X = -5504477
49
Y = 9146440
50 feet Y = 2787835
06 meter
Z = -9252411
72 Z = -2820135
09
XDOT = -273
888589 XDOT = -83
481242
YDOT = -17441
135493 feet/sec YDOT = -5316
058098 meter/sec
ZDOT = -16730
341994 ZDOT = -5099
408240
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 18174
37268096
00016717 00000-0 10270-3 0 9010
2 25544 51
6408 347
8804 0003832 224
0054 136
0794 15
53936522 39477
Satellite: ISS
Catalog Number: 25544
Epoch time: 18174
37268096 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 347
8804 deg
Eccentricity:
0003832
Arg of perigee: 224
0054 deg
Mean anomaly: 136
0794 deg
Mean motion: 15
53936522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3947
Checksum: 321
Coasting Arc #3 (Orbit 3962)
---------------------------------------
Vector Time (GMT): 2018/175/08:18:33
198
Vector Time (MET): N/A
Weight (LBS) : 922891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5174544
72 A = 6782866
25 meter
Y = 1723052
40 meter E =
0008984
Z = 4029423
99 I = 51
52670
XDOT = -4618
790127 Wp = 120
95055
YDOT = 4713
709220 meter/sec RA = 342
46413 deg
ZDOT = 3904
741639 TA = 288
42654
MA = 288
52420
Ha = 220
520 n
mi
Hp = 215
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16976852
76 X = 5135319
61
Y = 5653059
05 feet Y = 1780697
88 meter
Z = 13219895
00 Z = 4054465
19
XDOT = -15153
510914 XDOT = -4690
124082
YDOT = 15464
925261 feet/sec YDOT = 4661
659363 meter/sec
ZDOT = 12810
832150 ZDOT = 3882
132429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16967646
51 X = 5171738
66
Y = -5413200
44 feet Y = -1649943
49 meter
Z = 13331633
92 Z = 4063482
02
XDOT = -3555
471105 XDOT = -1083
707593
YDOT = 20243
008106 feet/sec YDOT = 6170
068871 meter/sec
ZDOT = 12708
907716 ZDOT = 3873
675072
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 18175
40162525
00016717 00000-0 10270-3 0 9026
2 25544 51
6410 342
7519 0003646 229
2633 130
8203 15
53943741 39636
Satellite: ISS
Catalog Number: 25544
Epoch time: 18175
40162525 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 342
7519 deg
Eccentricity:
0003646
Arg of perigee: 229
2633 deg
Mean anomaly: 130
8203 deg
Mean motion: 15
53943741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3963
Checksum: 296
Coasting Arc #4 (Orbit 3977)
---------------------------------------
Vector Time (GMT): 2018/176/08:18:33
198
Vector Time (MET): N/A
Weight (LBS) : 922891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3894671
11 A = 6779486
02 meter
Y = -2610391
34 meter E =
0008824
Z = -4904856
23 I = 51
48362
XDOT = 5836
735258 Wp = 81
32084
YDOT = -4399
879187 meter/sec RA = 337
46305 deg
ZDOT = -2295
220220 TA = 166
17810
MA = 166
15393
Ha = 220
401 n
mi
Hp = 215
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12777792
36 X = -3841366
28
Y = -8564276
06 feet Y = -2653645
47 meter
Z = -16092048
00 Z = -4923646
16
XDOT = 19149
393891 XDOT = 5896
651113
YDOT = -14435
299170 feet/sec YDOT = -4334
273442 meter/sec
ZDOT = -7530
250064 ZDOT = -2266
722429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15271631
33 X = -4654793
23
Y = 835299
68 feet Y = 254599
34 meter
Z = -16175671
91 Z = -4930344
80
XDOT = 6629
645146 XDOT = 2020
715841
YDOT = -21991
425179 feet/sec YDOT = -6702
986395 meter/sec
ZDOT = -7402
040623 ZDOT = -2256
141982
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 18176
36625534
00016717 00000-0 10270-3 0 9037
2 25544 51
6402 337
9431 0003719 233
8345 126
2464 15
53974297 39782
Satellite: ISS
Catalog Number: 25544
Epoch time: 18176
36625534 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 337
9431 deg
Eccentricity:
0003719
Arg of perigee: 233
8345 deg
Mean anomaly: 126
2464 deg
Mean motion: 15
53974297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3978
Checksum: 333
Coasting Arc #5 (Orbit 3993)
---------------------------------------
Vector Time (GMT): 2018/177/08:18:33
198
Vector Time (MET): N/A
Weight (LBS) : 922891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2424334
55 A = 6777923
20 meter
Y = 3485086
00 meter E =
0002958
Z = 5284251
66 I = 51
44768
XDOT = -6602
927656 Wp = 188
85782
YDOT = 3870
035179 meter/sec RA = 332
45477 deg
ZDOT = 474
115122 TA = 256
59108
MA = 256
62405
Ha = 220
338 n
mi
Hp = 216
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7953853
52 X = 2359515
07
Y = 11434009
18 feet Y = 3511833
30 meter
Z = 17336783
66 Z = 5295871
36
XDOT = -21663
148478 XDOT = -6648
015711
YDOT = 12696
965812 feet/sec YDOT = 3795
944513 meter/sec
ZDOT = 1555
495806 ZDOT = 441
931483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13230135
46 X = 4032545
29
Y = 4144737
15 feet Y = 1263315
88 meter
Z = 17388188
21 Z = 5299919
77
XDOT = -8887
751133 XDOT = -2708
986545
YDOT = 22412
111691 feet/sec YDOT = 6831
211643 meter/sec
ZDOT = 1410
891539 ZDOT = 430
039741
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 18177
39519449
00016717 00000-0 10270-3 0 9049
2 25544 51
6398 332
8153 0003643 235
8045 124
2763 15
53952164 39943
Satellite: ISS
Catalog Number: 25544
Epoch time: 18177
39519449 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 332
8153 deg
Eccentricity:
0003643
Arg of perigee: 235
8045 deg
Mean anomaly: 124
2763 deg
Mean motion: 15
53952164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3994
Checksum: 336
Coasting Arc #6 (Orbit 4008)
---------------------------------------
Vector Time (GMT): 2018/178/08:18:33
198
Vector Time (MET): N/A
Weight (LBS) : 922891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -876831
53 A = 6778464
14 meter
Y = -4321751
97 meter E =
0011191
Z = -5157769
28 I = 51
42014
XDOT = 6878
030157 Wp = 113
34786
YDOT = -3067
516991 meter/sec RA = 327
44126 deg
ZDOT = 1399
100400 TA = 170
17504
MA = 170
15314
Ha = 220
255 n
mi
Hp = 216
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2876743
85 X = -803385
69
Y = -14178976
29 feet Y = -4331145
78 meter
Z = -16921815
23 Z = -5161850
95
XDOT = 22565
715739 XDOT = 6905
024714
YDOT = -10064
032124 feet/sec YDOT = -2990
451416 meter/sec
ZDOT = 4590
224409 ZDOT = 1432
576452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11098438
09 X = -3382803
93
Y = -9249292
66 feet Y = -2819184
40 meter
Z = -16939365
74 Z = -5163118
68
XDOT = 10443
292987 XDOT = 3183
115702
YDOT = -21224
520277 feet/sec YDOT = -6469
233780 meter/sec
ZDOT = 4740
472621 ZDOT = 1444
896055
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 18178
35982134
00016717 00000-0 10270-3 0 9052
2 25544 51
6390 328
0066 0003791 240
3242 119
7533 15
53985624 40098
Satellite: ISS
Catalog Number: 25544
Epoch time: 18178
35982134 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 328
0066 deg
Eccentricity:
0003791
Arg of perigee: 240
3242 deg
Mean anomaly: 119
7533 deg
Mean motion: 15
53985624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4009
Checksum: 314
Coasting Arc #7 (Orbit 4024)
---------------------------------------
Vector Time (GMT): 2018/179/08:18:33
198
Vector Time (MET): N/A
Weight (LBS) : 922891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -618553
66 A = 6781084
69 meter
Y = 5020557
14 meter E =
0005067
Z = 4512896
39 I = 51
40260
XDOT = -6706
391827 Wp = 68
92756
YDOT = 1998
632495 meter/sec RA = 322
43121 deg
ZDOT = -3138
022720 TA = 52
66530
MA = 52
61914
Ha = 220
087 n
mi
Hp = 216
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2029375
52 X = -696570
07
Y = 16471644
15 feet Y = 5013203
07 meter
Z = 14806090
51 Z = 4509703
04
XDOT = -22002
597859 XDOT = -6712
999890
YDOT = 6557
193224 feet/sec YDOT = 1923
600576 meter/sec
ZDOT = -10295
350131 ZDOT = -3170
615569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8994529
19 X = 2741532
50
Y = 13963480
56 feet Y = 4256068
87 meter
Z = 14790990
41 Z = 4508293
88
XDOT = -11520
839981 XDOT = -3511
552026
YDOT = 18497
508037 feet/sec YDOT = 5638
040450 meter/sec
ZDOT = -10441
468557 ZDOT = -3182
559616
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 18179
38875358
00016717 00000-0 10270-3 0 9066
2 25544 51
6399 322
8782 0003845 246
0752 113
9998 15
53997873 40251
Satellite: ISS
Catalog Number: 25544
Epoch time: 18179
38875358 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 322
8782 deg
Eccentricity:
0003845
Arg of perigee: 246
0752 deg
Mean anomaly: 113
9998 deg
Mean motion: 15
53997873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4025
Checksum: 371
Coasting Arc #8 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2018/179/14:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 922891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -117146
02 A = 6780475
24 meter
Y = 4897571
28 meter E =
0004307
Z = 4684994
89 I = 51
39538
XDOT = -6683
343220 Wp = 68
34569
YDOT = 2517
626371 meter/sec RA = 321
14819 deg
ZDOT = -2795
342805 TA = 49
47418
MA = 49
43667
Ha = 220
309 n
mi
Hp = 216
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -384337
32 X = -194660
37
Y = 16068147
26 feet Y = 4895827
09 meter
Z = 15370718
15 Z = 4684238
39
XDOT = -21926
979068 XDOT = -6697
421087
YDOT = 8259
929039 feet/sec YDOT = 2442
810372 meter/sec
ZDOT = -9171
072195 ZDOT = -2827
841723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12128116
28 X = 3696649
84
Y = -10553211
79 feet Y = -3216618
95 meter
Z = 15366540
42 Z = 4683721
52
XDOT = 20139
818708 XDOT = 6138
616742
YDOT = 9561
744034 feet/sec YDOT = 2914
419582 meter/sec
ZDOT = -9316
853537 ZDOT = -2839
776958
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 18179
64598906
00016717 00000-0 10270-3 0 9077
2 25544 51
6417 321
5942 0003755 238
1408 121
9380 15
53971744 40293
Satellite: ISS
Catalog Number: 25544
Epoch time: 18179
64598906 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 321
5942 deg
Eccentricity:
0003755
Arg of perigee: 238
1408 deg
Mean anomaly: 121
9380 deg
Mean motion: 15
53971744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 334
Coasting Arc #9 (Orbit 4040)
---------------------------------------
Vector Time (GMT): 2018/180/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1324360
77 A = 6778807
54 meter
Y = -4305175
17 meter E =
0010784
Z = -5075604
68 I = 51
36573
XDOT = 6314
676374 Wp = 115
55071
YDOT = -3978
107894 meter/sec RA = 317
14475 deg
ZDOT = 1724
911652 TA = 171
21335
MA = 171
19446
Ha = 220
239 n
mi
Hp = 215
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4345015
64 X = -1251466
31
Y = -14124590
44 feet Y = -4319576
69 meter
Z = -16652246
33 Z = -5081861
55
XDOT = 20717
442173 XDOT = 6350
312721
YDOT = -13051
535086 feet/sec YDOT = -3907
293853 meter/sec
ZDOT = 5659
158963 ZDOT = 1755
671790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14471774
17 X = -4410996
77
Y = -2835689
73 feet Y = -864318
23 meter
Z = -16679542
56 Z = -5083924
57
XDOT = -2118
079214 XDOT = -645
590544
YDOT = -23323
344558 feet/sec YDOT = -7108
955421 meter/sec
ZDOT = 5797
393059 ZDOT = 1767
045404
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 18180
41768620
00016717 00000-0 10270-3 0 9087
2 25544 51
6377 317
7478 0003605 242
4264 117
6522 15
53985496 40414
Satellite: ISS
Catalog Number: 25544
Epoch time: 18180
41768620 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 317
7478 deg
Eccentricity:
0003605
Arg of perigee: 242
4264 deg
Mean anomaly: 117
6522 deg
Mean motion: 15
53985496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4041
Checksum: 325
Coasting Arc #10 (Orbit 4056)
---------------------------------------
Vector Time (GMT): 2018/181/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -24828
13 A = 6781814
30 meter
Y = 5204992
82 meter E =
0005919
Z = 4343468
36 I = 51
35149
XDOT = -6252
041069 Wp = 74
48024
YDOT = 2831
081555 meter/sec RA = 312
13290 deg
ZDOT = -3422
905535 TA = 50
39821
MA = 50
34596
Ha = 220
137 n
mi
Hp = 216
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -81457
11 X = -104127
97
Y = 17076748
09 feet Y = 5204271
13 meter
Z = 14250224
26 Z = 4343155
93
XDOT = -20511
945766 XDOT = -6266
607868
YDOT = 9288
325312 feet/sec YDOT = 2761
085988 meter/sec
ZDOT = -11230
005035 ZDOT = -3453
310382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15165808
33 X = 4622538
38
Y = 7853889
30 feet Y = 2393865
46 meter
Z = 14248001
01 Z = 4342790
71
XDOT = -347
409080 XDOT = -105
890288
YDOT = 21323
601375 feet/sec YDOT = 6499
433699 meter/sec
ZDOT = -11366
459061 ZDOT = -3464
496722
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 18181
44661435
00016717 00000-0 10270-3 0 9098
2 25544 51
6372 312
6200 0003735 246
6720 113
4040 15
53960960 40578
Satellite: ISS
Catalog Number: 25544
Epoch time: 18181
44661435 = yrday
fracday
Element set: 909
Inclination: 51
6372 deg
RA of node: 312
6200 deg
Eccentricity:
0003735
Arg of perigee: 246
6720 deg
Mean anomaly: 113
4040 deg
Mean motion: 15
53960960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4057
Checksum: 290
Coasting Arc #11 (Orbit 4071)
---------------------------------------
Vector Time (GMT): 2018/182/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1230749
90 A = 6785406
08 meter
Y = -5859164
31 meter E =
0001119
Z = -3194635
63 I = 51
34445
XDOT = 5833
714349 Wp = 108
59535
YDOT = -1377
666518 meter/sec RA = 307
12804 deg
ZDOT = 4775
224295 TA = 214
33115
MA = 214
33838
Ha = 220
067 n
mi
Hp = 216
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4037893
38 X = 1311694
86
Y = -19222980
01 feet Y = -5844948
19 meter
Z = -10481088
02 Z = -3188461
35
XDOT = 19139
482772 XDOT = 5825
491012
YDOT = -4519
903274 feet/sec YDOT = -1312
476531 meter/sec
ZDOT = 15666
746375 ZDOT = 4803
541925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15519432
98 X = -4730323
17
Y = -12065325
03 feet Y = -3677511
07 meter
Z = -10452553
82 Z = -3185938
40
XDOT = 3337
500547 XDOT = 1017
270167
YDOT = -17972
539436 feet/sec YDOT = -5478
030020 meter/sec
ZDOT = 15793
629327 ZDOT = 4813
898219
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 18182
41123076
00016717 00000-0 10270-3 0 9102
2 25544 51
6392 307
8121 0003626 250
1011 109
9751 15
53997856 40720
Satellite: ISS
Catalog Number: 25544
Epoch time: 18182
41123076 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 307
8121 deg
Eccentricity:
0003626
Arg of perigee: 250
1011 deg
Mean anomaly: 109
9751 deg
Mean motion: 15
53997856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4072
Checksum: 296
Coasting Arc #12 (Orbit 4087)
---------------------------------------
Vector Time (GMT): 2018/183/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2254175
50 A = 6788484
28 meter
Y = 6163342
47 meter E =
0011412
Z = 1711116
80 I = 51
33428
XDOT = -5160
120797 Wp = 127
44348
YDOT = -308
802625 meter/sec RA = 302
13172 deg
ZDOT = -5666
270376 TA = 33
70420
MA = 33
63168
Ha = 219
964 n
mi
Hp = 216
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7395588
90 X = -2331239
74
Y = 20220939
85 feet Y = 6137703
62 meter
Z = 5613900
26 Z = 1699980
51
XDOT = -16929
530174 XDOT = -5128
760793
YDOT = -1013
131973 feet/sec YDOT = -366
330629 meter/sec
ZDOT = -18590
125906 ZDOT = -5691
259990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15234406
00 X = 4643446
95
Y = 15233561
01 feet Y = 4643189
40 meter
Z = 5563138
72 Z = 1695644
68
XDOT = -6863
843811 XDOT = -2092
099594
YDOT = 13717
204220 feet/sec YDOT = 4181
003846 meter/sec
ZDOT = -18701
858280 ZDOT = -5700
326404
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 18183
44015113
00016717 00000-0 10270-3 0 9119
2 25544 51
6378 302
6840 0003648 255
3623 104
7125 15
54000549 40885
Satellite: ISS
Catalog Number: 25544
Epoch time: 18183
44015113 = yrday
fracday
Element set: 911
Inclination: 51
6378 deg
RA of node: 302
6840 deg
Eccentricity:
0003648
Arg of perigee: 255
3623 deg
Mean anomaly: 104
7125 deg
Mean motion: 15
54000549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4088
Checksum: 288
Coasting Arc #13 (Orbit 4088)
---------------------------------------
Vector Time (GMT): 2018/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947598
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1686472
56 A = 6787624
26 meter
Y = -6173959
79 meter E =
0003519
Z = -2254552
15 I = 51
33264
XDOT = 5400
727222 Wp = 8
84996
YDOT = -501
083317 meter/sec RA = 301
65108 deg
ZDOT = 5416
635598 TA = 325
96541
MA = 325
98797
Ha = 219
986 n
mi
Hp = 216
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5533046
46 X = 1766337
41
Y = -20255773
58 feet Y = -6154653
67 meter
Z = -7396824
62 Z = -2246166
71
XDOT = 17718
921333 XDOT = 5379
618280
YDOT = -1643
974136 feet/sec YDOT = -440
807331 meter/sec
ZDOT = 17771
114167 ZDOT = 5442
818781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20903667
12 X = -6371437
74
Y = -2124877
87 feet Y = -647662
77 meter
Z = -7358367
73 Z = -2242830
48
XDOT = -4710
382974 XDOT = -1435
724731
YDOT = -15555
836045 feet/sec YDOT = -4741
418826 meter/sec
ZDOT = 17888
309797 ZDOT = 5452
356826
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 18183
50445877
00016717 00000-0 10270-3 0 9121
2 25544 51
6409 302
3643 0003687 256
0118 104
0624 15
53980419 40898
Satellite: ISS
Catalog Number: 25544
Epoch time: 18183
50445877 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 302
3643 deg
Eccentricity:
0003687
Arg of perigee: 256
0118 deg
Mean anomaly: 104
0624 deg
Mean motion: 15
53980419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4089
Checksum: 313
Coasting Arc #14 (Orbit 4104)
---------------------------------------
Vector Time (GMT): 2018/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947598
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2563351
09 A = 6789555
57 meter
Y = 6247297
38 meter E =
0011160
Z = 639724
45 I = 51
32201
XDOT = -4669
462165 Wp = 143
32072
YDOT = -1302
760719 meter/sec RA = 296
65837 deg
ZDOT = -5943
128356 TA = 29
74040
MA = 29
67700
Ha = 219
901 n
mi
Hp = 216
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8409944
51 X = -2636126
97
Y = 20496382
50 feet Y = 6218225
24 meter
Z = 2098833
51 Z = 627096
62
XDOT = -15319
757760 XDOT = -4625
679069
YDOT = -4274
149342 feet/sec YDOT = -1354
732444 meter/sec
ZDOT = -19498
452612 ZDOT = -5965
704503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21695360
44 X = 6612745
86
Y = 4514195
71 feet Y = 1375926
85 meter
Z = 2041405
58 Z = 622220
42
XDOT = -1082
673949 XDOT = -329
999020
YDOT = 14135
121291 feet/sec YDOT = 4308
384969 meter/sec
ZDOT = -19599
238706 ZDOT = -5973
847958
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 18184
53337709
00016717 00000-0 10270-3 0 9130
2 25544 51
6401 297
2366 0003756 257
2474 102
8259 15
53994735 41054
Satellite: ISS
Catalog Number: 25544
Epoch time: 18184
53337709 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 297
2366 deg
Eccentricity:
0003756
Arg of perigee: 257
2474 deg
Mean anomaly: 102
8259 deg
Mean motion: 15
53994735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4105
Checksum: 328
Coasting Arc #15 (Orbit 4120)
---------------------------------------
Vector Time (GMT): 2018/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947598
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3216920
99 A = 6789222
50 meter
Y = -5884379
06 meter E =
0010459
Z = 1020238
35 I = 51
30833
XDOT = 3823
991945 Wp = 46
95395
YDOT = 3114
168160 meter/sec RA = 291
66638 deg
ZDOT = 5872
777465 TA = 324
15602
MA = 324
22616
Ha = 219
858 n
mi
Hp = 216
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10554202
72 X = 3277526
92
Y = -19305705
58 feet Y = -5848066
46 meter
Z = 3347238
69 Z = 1036011
54
XDOT = 12545
905333 XDOT = 3760
357687
YDOT = 10217
087139 feet/sec YDOT = 3156
574334 meter/sec
ZDOT = 19267
642601 ZDOT = 5891
198640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21025840
58 X = -6408676
21
Y = -6444550
09 feet Y = -1964298
87 meter
Z = 3418665
23 Z = 1042009
16
XDOT = 7049
611053 XDOT = 2148
721449
YDOT = -12682
285506 feet/sec YDOT = -3865
560622 meter/sec
ZDOT = 19349
576601 ZDOT = 5897
750948
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 18185
56229175
00016717 00000-0 10270-3 0 9142
2 25544 51
6412 292
1085 0003663 263
6029 96
4707 15
54007660 41219
Satellite: ISS
Catalog Number: 25544
Epoch time: 18185
56229175 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 292
1085 deg
Eccentricity:
0003663
Arg of perigee: 263
6029 deg
Mean anomaly: 96
4707 deg
Mean motion: 15
54007660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4121
Checksum: 305
Coasting Arc #16 (Orbit 4135)
---------------------------------------
Vector Time (GMT): 2018/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947598
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3691255
64 A = 6786759
51 meter
Y = 5065105
38 meter E =
0003218
Z = -2599114
52 I = 51
28843
XDOT = -2922
379869 Wp = 173
60864
YDOT = -4802
133383 meter/sec RA = 286
67007 deg
ZDOT = -5211
716303 TA = 35
79256
MA = 35
77100
Ha = 219
809 n
mi
Hp = 216
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12110418
75 X = -3734995
66
Y = 16617799
79 feet Y = 5023582
87 meter
Z = -8527278
62 Z = -2617151
04
XDOT = -9587
860464 XDOT = -2843
148307
YDOT = -15755
030783 feet/sec YDOT = -4834
369987 meter/sec
ZDOT = -17098
806769 ZDOT = -5225
720093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18840507
40 X = 5742586
66
Y = 8151911
28 feet Y = 2484702
56 meter
Z = -8608694
22 Z = -2623930
00
XDOT = -12724
804546 XDOT = -3878
520426
YDOT = 11299
870291 feet/sec YDOT = 3444
200465 meter/sec
ZDOT = -17160
742119 ZDOT = -5230
594198
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 18186
52689606
00016717 00000-0 10270-3 0 9159
2 25544 51
6407 287
3013 0003687 267
2130 92
8601 15
54007831 41368
Satellite: ISS
Catalog Number: 25544
Epoch time: 18186
52689606 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 287
3013 deg
Eccentricity:
0003687
Arg of perigee: 267
2130 deg
Mean anomaly: 92
8601 deg
Mean motion: 15
54007831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4136
Checksum: 311
Coasting Arc #17 (Orbit 4151)
---------------------------------------
Vector Time (GMT): 2018/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947598
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3989664
91 A = 6783038
90 meter
Y = -3852367
08 meter E =
0007476
Z = 3900420
12 I = 51
26784
XDOT = 2027
713101 Wp = 103
82961
YDOT = 6196
567072 meter/sec RA = 281
66420 deg
ZDOT = 4037
827177 TA = 303
68446
MA = 303
75572
Ha = 219
684 n
mi
Hp = 216
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13089451
81 X = 4013500
51
Y = -12638999
60 feet Y = -3807618
97 meter
Z = 12796653
93 Z = 3919858
00
XDOT = 6652
602037 XDOT = 1938
657124
YDOT = 20329
944463 feet/sec YDOT = 6218
744056 meter/sec
ZDOT = 13247
464491 ZDOT = 4047
461320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15332130
13 X = -4673233
26
Y = -9682811
13 feet Y = -2951320
83 meter
Z = 12884151
72 Z = 3927089
44
XDOT = 17522
019690 XDOT = 5340
711601
YDOT = -10025
580742 feet/sec YDOT = -3055
797010 meter/sec
ZDOT = 13289
664497 ZDOT = 4050
689739
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 18187
55580410
00016717 00000-0 10270-3 0 9167
2 25544 51
6407 282
1732 0003692 271
1933 88
8797 15
54042423 41525
Satellite: ISS
Catalog Number: 25544
Epoch time: 18187
55580410 = yrday
fracday
Element set: 916
Inclination: 51
6407 deg
RA of node: 282
1732 deg
Eccentricity:
0003692
Arg of perigee: 271
1933 deg
Mean anomaly: 88
8797 deg
Mean motion: 15
54042423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4152
Checksum: 316
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