[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 20th 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 3902)
---------------------------------------
Vector Time (GMT): 2018/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3064906
05 A = 6779514
87 meter
Y = 3698962
39 meter E =
0005005
Z = 4780241
14 I = 51
64087
XDOT = -6840
469235 Wp = 75
70163
YDOT = -2270
194745 meter/sec RA = 1
60245 deg
ZDOT = -2625
650682 TA = 40
19927
MA = 40
16226
Ha = 220
564 n
mi
Hp = 215
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10055466
06 X = -3129260
86
Y = 12135703
37 feet Y = 3664328
23 meter
Z = 15683205
84 Z = 4765196
99
XDOT = -22442
484368 XDOT = -6801
820933
YDOT = -7448
145488 feet/sec YDOT = -2346
473252 meter/sec
ZDOT = -8614
339509 ZDOT = -2658
785498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11733347
82 X = 3576324
42
Y = 10622730
04 feet Y = 3237808
12 meter
Z = 15615274
40 Z = 4759535
64
XDOT = -7537
756390 XDOT = -2297
508148
YDOT = 21223
214776 feet/sec YDOT = 6468
835864 meter/sec
ZDOT = -8762
232692 ZDOT = -2670
728525
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 18171
54353220
00016717 00000-0 10270-3 0 9009
2 25544 51
6387 1
9825 0003009 217
8018 142
2924 15
54195506 39036
Satellite: ISS
Catalog Number: 25544
Epoch time: 18171
54353220 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 1
9825 deg
Eccentricity:
0003009
Arg of perigee: 217
8018 deg
Mean anomaly: 142
2924 deg
Mean motion: 15
54195506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3903
Checksum: 289
Coasting Arc #2 (Orbit 3917)
---------------------------------------
Vector Time (GMT): 2018/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4588540
63 A = 6783132
03 meter
Y = -3272009
03 meter E =
0005285
Z = -3781365
14 I = 51
61954
XDOT = 5633
849245 Wp = 131
91785
YDOT = 3018
463874 meter/sec RA = 356
61024 deg
ZDOT = 4224
940071 TA = 182
78503
MA = 182
78797
Ha = 220
452 n
mi
Hp = 215
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15054267
16 X = 4643155
96
Y = -10734937
76 feet Y = -3220391
08 meter
Z = -12406053
62 Z = -3758943
27
XDOT = 18483
757364 XDOT = 5579
154727
YDOT = 9903
096700 feet/sec YDOT = 3081
159256 meter/sec
ZDOT = 13861
351938 ZDOT = 4252
174766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10405965
47 X = -3171738
27
Y = -15364838
20 feet Y = -4683202
68 meter
Z = -12305187
72 Z = -3750621
22
XDOT = 9179
344959 XDOT = 2797
864343
YDOT = -17414
140132 feet/sec YDOT = -5307
829912 meter/sec
ZDOT = 13982
710658 ZDOT = 4261
930209
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 18172
50801637
00016717 00000-0 10270-3 0 9017
2 25544 51
6383 357
1727 0002953 218
3759 141
7184 15
54210305 39187
Satellite: ISS
Catalog Number: 25544
Epoch time: 18172
50801637 = yrday
fracday
Element set: 901
Inclination: 51
6383 deg
RA of node: 357
1727 deg
Eccentricity:
0002953
Arg of perigee: 218
3759 deg
Mean anomaly: 141
7184 deg
Mean motion: 15
54210305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3918
Checksum: 308
Coasting Arc #3 (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 = -5739522
93 A = 6786726
64 meter
Y = 2732811
71 meter E =
0012648
Z = 2356713
85 I = 51
59874
XDOT = -3993
192833 Wp = 118
44175
YDOT = -3727
668417 meter/sec RA = 351
62776 deg
ZDOT = -5386
356236 TA = 35
22670
MA = 35
14317
Ha = 220
301 n
mi
Hp = 215
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18830455
80 X = -5781103
10
Y = 8965917
70 feet Y = 2668395
68 meter
Z = 7732000
83 Z = 2328732
47
XDOT = -13101
026354 XDOT = -3925
048114
YDOT = -12229
883258 feet/sec YDOT = -3771
941488 meter/sec
ZDOT = -17671
772428 ZDOT = -5405
588686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8882741
90 X = 2707459
73
Y = 18920829
75 feet Y = 5767068
91 meter
Z = 7606357
90 Z = 2318417
89
XDOT = -10909
009713 XDOT = -3325
066161
YDOT = 12281
573761 feet/sec YDOT = 3743
423682 meter/sec
ZDOT = -17757
202394 ZDOT = -5412
395290
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
53679399
00016717 00000-0 10270-3 0 9020
2 25544 51
6380 352
0436 0002931 226
7620 133
3289 15
54240245 39348
Satellite: ISS
Catalog Number: 25544
Epoch time: 18173
53679399 = yrday
fracday
Element set: 902
Inclination: 51
6380 deg
RA of node: 352
0436 deg
Eccentricity:
0002931
Arg of perigee: 226
7620 deg
Mean anomaly: 133
3289 deg
Mean motion: 15
54240245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3934
Checksum: 312
Coasting Arc #4 (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 = -6123015
67 A = 6786508
21 meter
Y = -896899
54 meter E =
0005287
Z = -2779942
68 I = 51
57047
XDOT = 3029
520803 Wp = 163
96097
YDOT = -4835
871609 meter/sec RA = 347
45257 deg
ZDOT = -5119
819872 TA = 47
57873
MA = 47
53402
Ha = 220
659 n
mi
Hp = 215
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20088634
09 X = -6099027
68
Y = -2942583
79 feet Y = -965236
88 meter
Z = -9120546
86 Z = -2809628
11
XDOT = 9939
372713 XDOT = 3108
241152
YDOT = -15865
720501 feet/sec YDOT = -4801
552687 meter/sec
ZDOT = -16797
309292 ZDOT = -5104
912807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18059280
81 X = -5504468
79
Y = 9145324
14 feet Y = 2787494
80 meter
Z = -9253205
77 Z = -2820377
12
XDOT = -272
750778 XDOT = -83
134437
YDOT = -17441
884235 feet/sec YDOT = -5316
286315 meter/sec
ZDOT = -16729
817004 ZDOT = -5099
248223
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
37268031
00016717 00000-0 10270-3 0 9031
2 25544 51
6406 347
8806 0003891 223
6876 136
3969 15
53938061 39476
Satellite: ISS
Catalog Number: 25544
Epoch time: 18174
37268031 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 347
8806 deg
Eccentricity:
0003891
Arg of perigee: 223
6876 deg
Mean anomaly: 136
3969 deg
Mean motion: 15
53938061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3947
Checksum: 341
Coasting Arc #5 (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 = 5173860
05 A = 6782857
67 meter
Y = 1723805
49 meter E =
0008987
Z = 4030034
03 I = 51
52658
XDOT = -4619
802258 Wp = 121
36268
YDOT = 4713
335798 meter/sec RA = 342
46431 deg
ZDOT = 3903
915527 TA = 288
02433
MA = 288
12224
Ha = 220
523 n
mi
Hp = 215
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16974606
48 X = 5134623
61
Y = 5655529
83 feet Y = 1781443
25 meter
Z = 13221896
43 Z = 4055071
87
XDOT = -15156
831555 XDOT = -4691
127950
YDOT = 15463
700126 feet/sec YDOT = 4661
274669 meter/sec
ZDOT = 12808
121807 ZDOT = 3881
301420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16967282
78 X = 5171627
79
Y = -5409871
99 feet Y = -1648928
98 meter
Z = 13333620
23 Z = 4064087
44
XDOT = -3558
617100 XDOT = -1084
666492
YDOT = 20243
996594 feet/sec YDOT = 6170
370162 meter/sec
ZDOT = 12706
175529 ZDOT = 3872
842301
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
40162330
00016717 00000-0 10270-3 0 9042
2 25544 51
6409 342
7521 0003704 228
9226 131
1607 15
53946006 39635
Satellite: ISS
Catalog Number: 25544
Epoch time: 18175
40162330 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 342
7521 deg
Eccentricity:
0003704
Arg of perigee: 228
9226 deg
Mean anomaly: 131
1607 deg
Mean motion: 15
53946006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3963
Checksum: 291
Coasting Arc #6 (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 = -3892832
58 A = 6779474
30 meter
Y = -2611758
91 meter E =
0008788
Z = -4905529
00 I = 51
48350
XDOT = 5838
300624 Wp = 81
63435
YDOT = -4398
871665 meter/sec RA = 337
46318 deg
ZDOT = -2293
307265 TA = 165
88467
MA = 165
86009
Ha = 220
398 n
mi
Hp = 215
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12771760
42 X = -3839509
32
Y = -8568762
81 feet Y = -2654992
37 meter
Z = -16094255
24 Z = -4924309
95
XDOT = 19154
529607 XDOT = 5898
195804
YDOT = -14431
993650 feet/sec YDOT = -4333
248530 meter/sec
ZDOT = -7523
973967 ZDOT = -2264
801920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15269526
65 X = -4654151
72
Y = 828070
42 feet Y = 252395
87 meter
Z = -16177838
78 Z = -4931005
26
XDOT = 6635
174420 XDOT = 2022
401163
YDOT = -21992
024046 feet/sec YDOT = -6703
168929 meter/sec
ZDOT = -7395
730901 ZDOT = -2254
218778
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
36625172
00016717 00000-0 10270-3 0 9057
2 25544 51
6400 337
9432 0003776 233
5027 126
5778 15
53977327 39786
Satellite: ISS
Catalog Number: 25544
Epoch time: 18176
36625172 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 337
9432 deg
Eccentricity:
0003776
Arg of perigee: 233
5027 deg
Mean anomaly: 126
5778 deg
Mean motion: 15
53977327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3978
Checksum: 337
Coasting Arc #7 (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 = 2421146
41 A = 6777911
45 meter
Y = 3486978
90 meter E =
0003006
Z = 5284484
76 I = 51
44756
XDOT = -6604
421043 Wp = 189
46616
YDOT = 3867
840444 meter/sec RA = 332
45484 deg
ZDOT = 470
817910 TA = 256
01409
MA = 256
04752
Ha = 220
333 n
mi
Hp = 216
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7943393
73 X = 2356304
86
Y = 11440219
50 feet Y = 3513690
43 meter
Z = 17337548
44 Z = 5296088
93
XDOT = -21668
048041 XDOT = -6649
468428
YDOT = 12689
765236 feet/sec YDOT = 3793
733305 meter/sec
ZDOT = 1544
678181 ZDOT = 438
627115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13225747
39 X = 4031207
81
Y = 4156087
14 feet Y = 1266775
36 meter
Z = 17388883
16 Z = 5300131
59
XDOT = -8895
169698 XDOT = -2711
247724
YDOT = 22409
754335 feet/sec YDOT = 6830
493121 meter/sec
ZDOT = 1400
042265 ZDOT = 426
732882
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
39518862
00016717 00000-0 10270-3 0 9069
2 25544 51
6397 332
8154 0003702 235
5121 124
5683 15
53955908 39944
Satellite: ISS
Catalog Number: 25544
Epoch time: 18177
39518862 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 332
8154 deg
Eccentricity:
0003702
Arg of perigee: 235
5121 deg
Mean anomaly: 124
5683 deg
Mean motion: 15
53955908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3994
Checksum: 337
Coasting Arc #8 (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 = -871812
83 A = 6778455
77 meter
Y = -4323975
08 meter E =
0011166
Z = -5156715
19 I = 51
42005
XDOT = 6878
868955 Wp = 113
69326
YDOT = -3063
533008 meter/sec RA = 327
44128 deg
ZDOT = 1403
866782 TA = 169
87682
MA = 169
85431
Ha = 220
246 n
mi
Hp = 216
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2860278
33 X = -798347
63
Y = -14186269
96 feet Y = -4333312
66 meter
Z = -16918356
92 Z = -5160772
43
XDOT = 22568
467699 XDOT = 6905
795747
YDOT = -10050
961313 feet/sec YDOT = -2986
458432 meter/sec
ZDOT = 4605
862146 ZDOT = 1437
346745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11090294
93 X = -3380321
90
Y = -9265331
05 feet Y = -2824072
90 meter
Z = -16935797
80 Z = -5162031
17
XDOT = 10452
431862 XDOT = 3185
901232
YDOT = -21216
650693 feet/sec YDOT = -6466
835131 meter/sec
ZDOT = 4756
127199 ZDOT = 1449
667570
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
35981290
00016717 00000-0 10270-3 0 9076
2 25544 51
6389 328
0067 0003849 240
0457 120
0314 15
53990090 40091
Satellite: ISS
Catalog Number: 25544
Epoch time: 18178
35981290 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 328
0067 deg
Eccentricity:
0003849
Arg of perigee: 240
0457 deg
Mean anomaly: 120
0314 deg
Mean motion: 15
53990090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4009
Checksum: 311
Coasting Arc #9 (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 = -625107
90 A = 6781081
36 meter
Y = 5022510
35 meter E =
0005026
Z = 4509816
75 I = 51
40252
XDOT = -6705
614697 Wp = 69
30767
YDOT = 1992
317028 meter/sec RA = 322
43120 deg
ZDOT = -3143
693657 TA = 52
34859
MA = 52
30300
Ha = 220
073 n
mi
Hp = 216
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2050878
94 X = -703130
71
Y = 16478052
32 feet Y = 5015082
95 meter
Z = 14795986
71 Z = 4506591
55
XDOT = -22000
048219 XDOT = -6712
124650
YDOT = 6536
473189 feet/sec YDOT = 1917
294350 meter/sec
ZDOT = -10313
955567 ZDOT = -3176
282494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8982274
64 X = 2737797
31
Y = 13982199
04 feet Y = 4261774
27 meter
Z = 14780743
81 Z = 4505170
71
XDOT = -11530
791928 XDOT = -3514
585380
YDOT = 18480
838809 feet/sec YDOT = 5632
959669 meter/sec
ZDOT = -10460
055020 ZDOT = -3188
224770
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
38874192
00016717 00000-0 10270-3 0 9083
2 25544 51
6398 322
8782 0003902 245
7941 114
2804 15
54003117 40250
Satellite: ISS
Catalog Number: 25544
Epoch time: 18179
38874192 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 322
8782 deg
Eccentricity:
0003902
Arg of perigee: 245
7941 deg
Mean anomaly: 114
2804 deg
Mean motion: 15
54003117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4025
Checksum: 317
Coasting Arc #10 (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 = -124182
42 A = 6780471
88 meter
Y = 4900224
65 meter E =
0004268
Z = 4682039
73 I = 51
39531
XDOT = -6683
180664 Wp = 68
75054
YDOT = 2510
992968 meter/sec RA = 321
14816 deg
ZDOT = -2801
682342 TA = 49
13764
MA = 49
10066
Ha = 220
297 n
mi
Hp = 216
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -407422
65 X = -201711
57
Y = 16076852
52 feet Y = 4898401
68 meter
Z = 15361022
73 Z = 4681249
01
XDOT = -21926
445749 XDOT = -6697
153573
YDOT = 8238
165906 feet/sec YDOT = 2436
179374 meter/sec
ZDOT = -9191
871202 ZDOT = -2834
180217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12150136
65 X = 3703361
65
Y = -10542220
09 feet Y = -3213268
68 meter
Z = 15356691
52 Z = 4680719
58
XDOT = 20124
185011 XDOT = 6133
851591
YDOT = 9574
422563 feet/sec YDOT = 2918
283997 meter/sec
ZDOT = -9337
646802 ZDOT = -2846
114745
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
64597652
00016717 00000-0 10270-3 0 9096
2 25544 51
6416 321
5943 0003814 237
9800 122
0983 15
53976993 40294
Satellite: ISS
Catalog Number: 25544
Epoch time: 18179
64597652 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 321
5943 deg
Eccentricity:
0003814
Arg of perigee: 237
9800 deg
Mean anomaly: 122
0983 deg
Mean motion: 15
53976993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 344
Coasting Arc #11 (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 = -1315973
73 A = 6778799
99 meter
Y = -4310432
97 meter E =
0010745
Z = -5073270
45 I = 51
36564
XDOT = 6316
933219 Wp = 115
92772
YDOT = -3970
869960 meter/sec RA = 317
14464 deg
ZDOT = 1733
483190 TA = 170
92228
MA = 170
90284
Ha = 220
223 n
mi
Hp = 216
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4317499
12 X = -1243032
45
Y = -14141840
47 feet Y = -4324740
44 meter
Z = -16644588
07 Z = -5079486
46
XDOT = 20724
846518 XDOT = 6352
446825
YDOT = -13027
788582 feet/sec YDOT = -3900
031369 meter/sec
ZDOT = 5687
280808 ZDOT = 1764
253994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14474238
14 X = -4411747
78
Y = -2868028
64 feet Y = -874175
13 meter
Z = -16671700
72 Z = -5081534
38
XDOT = -2096
061257 XDOT = -638
879471
YDOT = -23318
484703 feet/sec YDOT = -7107
474138 meter/sec
ZDOT = 5825
561451 ZDOT = 1775
631130
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
41767080
00016717 00000-0 10270-3 0 9109
2 25544 51
6376 317
7478 0003664 242
2607 117
8175 15
53991571 40414
Satellite: ISS
Catalog Number: 25544
Epoch time: 18180
41767080 = yrday
fracday
Element set: 910
Inclination: 51
6376 deg
RA of node: 317
7478 deg
Eccentricity:
0003664
Arg of perigee: 242
2607 deg
Mean anomaly: 117
8175 deg
Mean motion: 15
53991571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4041
Checksum: 317
Coasting Arc #12 (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 = -35279
44 A = 6781815
13 meter
Y = 5209721
28 meter E =
0005887
Z = 4337724
52 I = 51
35145
XDOT = -6251
976726 Wp = 74
85233
YDOT = 2819
915244 meter/sec RA = 312
13276 deg
ZDOT = -3432
226911 TA = 50
13463
MA = 50
08287
Ha = 220
116 n
mi
Hp = 216
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -115746
18 X = -114603
47
Y = 17092261
40 feet Y = 5208882
58 meter
Z = 14231379
66 Z = 4337361
27
XDOT = -20511
734664 XDOT = -6266
373387
YDOT = 9251
690433 feet/sec YDOT = 2749
921349 meter/sec
ZDOT = -11260
586978 ZDOT = -3462
631034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15164258
22 X = 4622065
91
Y = 7891377
32 feet Y = 2405291
81 meter
Z = 14228928
30 Z = 4336977
35
XDOT = -377
194322 XDOT = -114
968829
YDOT = 21306
832887 feet/sec YDOT = 6494
322664 meter/sec
ZDOT = -11397
035993 ZDOT = -3473
816571
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
44659459
00016717 00000-0 10270-3 0 9114
2 25544 51
6370 312
6199 0003795 246
5300 113
5453 15
53968025 40571
Satellite: ISS
Catalog Number: 25544
Epoch time: 18181
44659459 = yrday
fracday
Element set: 911
Inclination: 51
6370 deg
RA of node: 312
6199 deg
Eccentricity:
0003795
Arg of perigee: 246
5300 deg
Mean anomaly: 113
5453 deg
Mean motion: 15
53968025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4057
Checksum: 319
Coasting Arc #13 (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 = 1243018
90 A = 6785410
47 meter
Y = -5862029
69 meter E =
0001052
Z = -3184549
04 I = 51
34443
XDOT = 5830
421332 Wp = 109
18953
YDOT = -1361
964282 meter/sec RA = 307
12790 deg
ZDOT = 4783
801192 TA = 213
87332
MA = 213
88004
Ha = 220
042 n
mi
Hp = 216
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4078146
01 X = 1323946
00
Y = -19232380
86 feet Y = -5847676
47 meter
Z = -10447995
54 Z = -3178315
21
XDOT = 19128
678910 XDOT = 5821
980992
YDOT = -4468
386751 feet/sec YDOT = -1296
812334 meter/sec
ZDOT = 15694
885802 ZDOT = 4812
102302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15510469
28 X = -4727591
04
Y = -12105456
94 feet Y = -3689743
28 meter
Z = -10419194
51 Z = -3175770
49
XDOT = 3376
172765 XDOT = 1029
057459
YDOT = -17940
874098 feet/sec YDOT = -5468
378425 meter/sec
ZDOT = 15821
692398 ZDOT = 4822
451843
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
41120637
00016717 00000-0 10270-3 0 9124
2 25544 51
6390 307
8120 0003684 249
9713 110
1043 15
54005752 40720
Satellite: ISS
Catalog Number: 25544
Epoch time: 18182
41120637 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 307
8120 deg
Eccentricity:
0003684
Arg of perigee: 249
9713 deg
Mean anomaly: 110
1043 deg
Mean motion: 15
54005752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4072
Checksum: 278
Coasting Arc #14 (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 = -2267291
30 A = 6788479
05 meter
Y = 6162509
89 meter E =
0011390
Z = 1696661
63 I = 51
33423
XDOT = -5152
759817 Wp = 127
92742
YDOT = -328
927372 meter/sec RA = 302
13158 deg
ZDOT = -5671
854546 TA = 33
38539
MA = 33
31362
Ha = 219
933 n
mi
Hp = 216
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7438619
75 X = -2344275
05
Y = 20218208
32 feet Y = 6136724
83 meter
Z = 5566475
15 Z = 1685461
82
XDOT = -16905
379976 XDOT = -5121
148195
YDOT = -1079
158043 feet/sec YDOT = -386
371652 meter/sec
ZDOT = -18608
446672 ZDOT = -5696
807794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15213994
74 X = 4637225
60
Y = 15271183
87 feet Y = 4654656
84 meter
Z = 5515429
63 Z = 1681102
95
XDOT = -6910
843423 XDOT = -2106
425075
YDOT = 13668
949867 feet/sec YDOT = 4166
295920 meter/sec
ZDOT = -18720
013285 ZDOT = -5705
860049
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
44012120
00016717 00000-0 10270-3 0 9136
2 25544 51
6376 302
6838 0003706 255
2465 104
8277 15
54009501 40884
Satellite: ISS
Catalog Number: 25544
Epoch time: 18183
44012120 = yrday
fracday
Element set: 913
Inclination: 51
6376 deg
RA of node: 302
6838 deg
Eccentricity:
0003706
Arg of perigee: 255
2465 deg
Mean anomaly: 104
8277 deg
Mean motion: 15
54009501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4088
Checksum: 294
Coasting Arc #15 (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 = 1700568
84 A = 6787625
18 meter
Y = -6175224
28 meter E =
0003537
Z = -2240362
19 I = 51
33262
XDOT = 5395
103438 Wp = 8
07485
YDOT = -480
512571 meter/sec RA = 301
65092 deg
ZDOT = 5424
149129 TA = 326
90985
MA = 326
93197
Ha = 219
956 n
mi
Hp = 216
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5579294
08 X = 1780377
85
Y = -20259922
19 feet Y = -6155760
84 meter
Z = -7350269
66 Z = -2231908
42
XDOT = 17700
470598 XDOT = 5373
728390
YDOT = -1576
484814 feet/sec YDOT = -420
300963 meter/sec
ZDOT = 17795
764858 ZDOT = 5450
304350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20915416
64 X = -6375018
99
Y = -2169480
88 feet Y = -661257
77 meter
Z = -7311506
89 Z = -2228547
30
XDOT = -4643
984889 XDOT = -1415
486594
YDOT = -15547
884229 feet/sec YDOT = -4738
995113 meter/sec
ZDOT = 17912
832253 ZDOT = 5459
831271
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
50442848
00016717 00000-0 10270-3 0 9148
2 25544 51
6407 302
3642 0003745 255
8677 104
2059 15
53989404 40894
Satellite: ISS
Catalog Number: 25544
Epoch time: 18183
50442848 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 302
3642 deg
Eccentricity:
0003745
Arg of perigee: 255
8677 deg
Mean anomaly: 104
2059 deg
Mean motion: 15
53989404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4089
Checksum: 326
Coasting Arc #16 (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 = -2577824
34 A = 6789536
54 meter
Y = 6243182
10 meter E =
0011129
Z = 621234
16 I = 51
32193
XDOT = -4659
249805 Wp = 143
86473
YDOT = -1327
638964 meter/sec RA = 296
65820 deg
ZDOT = -5945
656547 TA = 29
39786
MA = 29
33531
Ha = 219
868 n
mi
Hp = 216
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8457428
95 X = -2650463
32
Y = 20482880
89 feet Y = 6213948
87 meter
Z = 2038169
83 Z = 608536
36
XDOT = -15286
252642 XDOT = -4615
176992
YDOT = -4355
770880 feet/sec YDOT = -1379
494867 meter/sec
ZDOT = -19506
747201 ZDOT = -5968
182386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21690734
70 X = 6611335
94
Y = 4562957
09 feet Y = 1390789
32 meter
Z = 1980429
52 Z = 603634
92
XDOT = -1165
516987 XDOT = -355
249578
YDOT = 14117
467961 feet/sec YDOT = 4303
004235 meter/sec
ZDOT = -19607
304507 ZDOT = -5976
306414
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
53334065
00016717 00000-0 10270-3 0 9154
2 25544 51
6399 297
2364 0003815 257
1856 102
8870 15
54004596 41054
Satellite: ISS
Catalog Number: 25544
Epoch time: 18184
53334065 = yrday
fracday
Element set: 915
Inclination: 51
6399 deg
RA of node: 297
2364 deg
Eccentricity:
0003815
Arg of perigee: 257
1856 deg
Mean anomaly: 102
8870 deg
Mean motion: 15
54004596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4105
Checksum: 322
Coasting Arc #17 (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 = 3230981
37 A = 6789172
12 meter
Y = -5872831
83 meter E =
0010417
Z = 1041903
47 I = 51
30815
XDOT = 3808
817388 Wp = 47
13685
YDOT = 3141
867384 meter/sec RA = 291
66615 deg
ZDOT = 5867
892421 TA = 324
21223
MA = 324
28199
Ha = 219
822 n
mi
Hp = 216
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10600332
59 X = 3291351
89
Y = -19267820
98 feet Y = -5836363
32 meter
Z = 3418318
48 Z = 1057744
39
XDOT = 12496
120039 XDOT = 3744
898246
YDOT = 10307
963859 feet/sec YDOT = 3184
102273 meter/sec
ZDOT = 19251
615555 ZDOT = 5886
239195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20997880
62 X = -6400154
01
Y = -6496881
10 feet Y = -1980249
36 meter
Z = 3490046
25 Z = 1063766
10
XDOT = 7144
789330 XDOT = 2177
731788
YDOT = -12653
888105 feet/sec YDOT = -3856
905094 meter/sec
ZDOT = 19333
212649 ZDOT = 5892
763215
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
56224859
00016717 00000-0 10270-3 0 9168
2 25544 51
6411 292
1083 0003721 263
4929 96
5800 15
54018304 41210
Satellite: ISS
Catalog Number: 25544
Epoch time: 18185
56224859 = yrday
fracday
Element set: 916
Inclination: 51
6411 deg
RA of node: 292
1083 deg
Eccentricity:
0003721
Arg of perigee: 263
4929 deg
Mean anomaly: 96
5800 deg
Mean motion: 15
54018304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4121
Checksum: 302
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