[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 20th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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
057/06:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 213
9
058/23:08:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 213
9
060/14:25:00
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
1
063/17:18:30
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
0
Coasting Arc #1 (Orbit 2020)
---------------------------------------
Vector Time (GMT): 2018/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1760482
69 A = 6788457
90 meter
Y = 6387814
33 meter E =
0010993
Z = -1459685
07 I = 51
31116
XDOT = -5065
768289 Wp = 134
88037
YDOT = 89
080807 meter/sec RA = 244
43041 deg
ZDOT = -5754
125273 TA = 61
11883
MA = 61
00857
Ha = 222
011 n
mi
Hp = 213
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5775861
86 X = 1696011
86
Y = 20957396
09 feet Y = 6407140
62 meter
Z = -4788993
02 Z = -1451290
64
XDOT = -16619
974701 XDOT = -5038
437819
YDOT = 292
259867 feet/sec YDOT = 32
584121 meter/sec
ZDOT = -18878
363756 ZDOT = -5778
666284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5992718
98 X = -1826580
74
Y = 20904760
61 feet Y = 6371771
03 meter
Z = -4752450
77 Z = -1448546
99
XDOT = -12694
173053 XDOT = -3869
183947
YDOT = -7929
851799 feet/sec YDOT = -2417
018828 meter/sec
ZDOT = -18987
618442 ZDOT = -5787
426101
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 18050
52937749
00016717 00000-0 10270-3 0 9007
2 25544 51
6373 245
2698 0002861 111
4643 248
6815 15
54120953 20214
Satellite: ISS
Catalog Number: 25544
Epoch time: 18050
52937749 = yrday
fracday
Element set: 900
Inclination: 51
6373 deg
RA of node: 245
2698 deg
Eccentricity:
0002861
Arg of perigee: 111
4643 deg
Mean anomaly: 248
6815 deg
Mean motion: 15
54120953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2021
Checksum: 305
Coasting Arc #2 (Orbit 2036)
---------------------------------------
Vector Time (GMT): 2018/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -789483
10 A = 6785514
52 meter
Y = -6035674
02 meter E =
0015615
Z = 2984617
73 I = 51
31582
XDOT = 5610
602081 Wp = 89
31643
YDOT = 1720
270386 meter/sec RA = 239
43163 deg
ZDOT = 4940
672070 TA = 305
01524
MA = 305
16169
Ha = 221
949 n
mi
Hp = 213
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2590167
64 X = -736429
42
Y = -19802080
13 feet Y = -6044205
63 meter
Z = 9792052
93 Z = 2980912
20
XDOT = 18407
487141 XDOT = 5566
949645
YDOT = 5643
931712 feet/sec YDOT = 1782
768405 meter/sec
ZDOT = 16209
554034 ZDOT = 4967
819931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7762121
24 X = 2365894
55
Y = -18408926
72 feet Y = -5611040
86 meter
Z = 9776325
37 Z = 2979823
97
XDOT = 11560
699253 XDOT = 3523
701132
YDOT = 13585
802397 feet/sec YDOT = 4140
952571 meter/sec
ZDOT = 16330
188587 ZDOT = 4977
441481
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 18051
55821540
00016717 00000-0 10270-3 0 9013
2 25544 51
6365 240
1401 0002908 119
1781 240
9663 15
54146361 20375
Satellite: ISS
Catalog Number: 25544
Epoch time: 18051
55821540 = yrday
fracday
Element set: 901
Inclination: 51
6365 deg
RA of node: 240
1401 deg
Eccentricity:
0002908
Arg of perigee: 119
1781 deg
Mean anomaly: 240
9663 deg
Mean motion: 15
54146361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2037
Checksum: 282
Coasting Arc #3 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2018/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -391329
24 A = 6781682
18 meter
Y = 5286661
86 meter E =
0010403
Z = -4239352
95 I = 51
32020
XDOT = -5901
254178 Wp = 83
19053
YDOT = -3310
374821 meter/sec RA = 234
42488 deg
ZDOT = -3589
843159 TA = 149
94391
MA = 149
88416
Ha = 222
014 n
mi
Hp = 213
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1283888
57 X = -429824
67
Y = 17344691
14 feet Y = 5282070
14 meter
Z = -13908638
28 Z = -4241347
83
XDOT = -19361
070137 XDOT = -5846
360661
YDOT = -10860
809781 feet/sec YDOT = -3376
060082 meter/sec
ZDOT = -11777
700653 ZDOT = -3618
375544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9581251
86 X = -2920365
57
Y = 14505883
73 feet Y = 4421393
36 meter
Z = -13918184
12 Z = -4242262
52
XDOT = -10372
332283 XDOT = -3161
486880
YDOT = -18252
901023 feet/sec YDOT = -5563
484232 meter/sec
ZDOT = -11904
309804 ZDOT = -3628
433628
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 18052
52275003
00016717 00000-0 10270-3 0 9029
2 25544 51
6361 235
3316 0003086 119
2616 240
8846 15
54138186 20523
Satellite: ISS
Catalog Number: 25544
Epoch time: 18052
52275003 = yrday
fracday
Element set: 902
Inclination: 51
6361 deg
RA of node: 235
3316 deg
Eccentricity:
0003086
Arg of perigee: 119
2616 deg
Mean anomaly: 240
8846 deg
Mean motion: 15
54138186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2052
Checksum: 286
Coasting Arc #4 (Orbit 2067)
---------------------------------------
Vector Time (GMT): 2018/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1659530
29 A = 6778637
29 meter
Y = -4236994
14 meter E =
0008684
Z = 5019467
48 I = 51
33015
XDOT = 5884
360651 Wp = 124
02173
YDOT = 4547
696598 meter/sec RA = 229
40921 deg
ZDOT = 1886
163474 TA = 307
58577
MA = 307
66460
Ha = 221
948 n
mi
Hp = 213
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5444653
17 X = 1682404
43
Y = -13900899
42 feet Y = -4218307
89 meter
Z = 16468069
14 Z = 5027584
69
XDOT = 19305
645182 XDOT = 5823
907824
YDOT = 14920
264430 feet/sec YDOT = 4613
161680 meter/sec
ZDOT = 6188
200375 ZDOT = 1914
600284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11326211
76 X = 3452229
35
Y = -9663702
24 feet Y = -2945496
44 meter
Z = 16504736
90 Z = 5030643
81
XDOT = 9094
931567 XDOT = 2772
135142
YDOT = 21483
579974 feet/sec YDOT = 6548
195176 meter/sec
ZDOT = 6314
245316 ZDOT = 1924
581972
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 18053
55158171
00016717 00000-0 10270-3 0 9030
2 25544 51
6365 230
2021 0002963 123
2363 236
9074 15
54107784 20687
Satellite: ISS
Catalog Number: 25544
Epoch time: 18053
55158171 = yrday
fracday
Element set: 903
Inclination: 51
6365 deg
RA of node: 230
2021 deg
Eccentricity:
0002963
Arg of perigee: 123
2363 deg
Mean anomaly: 236
9074 deg
Mean motion: 15
54107784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2068
Checksum: 291
Coasting Arc #5 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2018/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2994976
61 A = 6777309
84 meter
Y = 3001950
20 meter E =
0017563
Z = -5301969
10 I = 51
34873
XDOT = -5451
473933 Wp = 96
54110
YDOT = -5374
869210 meter/sec RA = 224
38905 deg
ZDOT = 34
339938 TA = 173
79888
MA = 173
77711
Ha = 222
001 n
mi
Hp = 213
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9826038
75 X = -3002568
70
Y = 9848917
98 feet Y = 2968415
59 meter
Z = -17394911
76 Z = -5316536
13
XDOT = -17885
413165 XDOT = -5391
132330
YDOT = -17634
085336 feet/sec YDOT = -5435
493943 meter/sec
ZDOT = 112
663837 ZDOT = 8
005654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13163998
20 X = -4012386
65
Y = 4241183
09 feet Y = 1292712
61 meter
Z = -17460145
91 Z = -5321852
47
XDOT = -7395
626292 XDOT = -2254
186894
YDOT = -22946
052590 feet/sec YDOT = -6993
956829 meter/sec
ZDOT = -3
936064 ZDOT = -1
199712
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 18054
51610522
00016717 00000-0 10270-3 0 9041
2 25544 51
6370 225
3938 0003210 126
3264 233
8185 15
54146022 20839
Satellite: ISS
Catalog Number: 25544
Epoch time: 18054
51610522 = yrday
fracday
Element set: 904
Inclination: 51
6370 deg
RA of node: 225
3938 deg
Eccentricity:
0003210
Arg of perigee: 126
3264 deg
Mean anomaly: 233
8185 deg
Mean motion: 15
54146022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 274
Coasting Arc #6 (Orbit 2098)
---------------------------------------
Vector Time (GMT): 2018/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4241794
40 A = 6778614
78 meter
Y = -1691024
47 meter E =
0007242
Z = 5003812
13 I = 51
37571
XDOT = 4620
374788 Wp = 81
65096
YDOT = 5807
340125 meter/sec RA = 219
37031 deg
ZDOT = -1950
720281 TA = 27
35819
MA = 27
32007
Ha = 221
887 n
mi
Hp = 213
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13916648
30 X = 4236083
05
Y = -5547980
54 feet Y = -1643621
54 meter
Z = 16416706
45 Z = 5024403
23
XDOT = 15158
709935 XDOT = 4564
567599
YDOT = 19052
953166 feet/sec YDOT = 5858
696213 meter/sec
ZDOT = -6400
000923 ZDOT = -1928
412156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14831007
01 X = 4520490
94
Y = 1211766
17 feet Y = 369346
33 meter
Z = 16508612
67 Z = 5031825
14
XDOT = 5167
354260 XDOT = 1575
009578
YDOT = 22756
672946 feet/sec YDOT = 6936
233914 meter/sec
ZDOT = -6301
362253 ZDOT = -1920
655215
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 18055
54492760
00016717 00000-0 10270-3 0 9058
2 25544 51
6356 220
2645 0003214 130
9822 229
1609 15
54112285 20997
Satellite: ISS
Catalog Number: 25544
Epoch time: 18055
54492760 = yrday
fracday
Element set: 905
Inclination: 51
6356 deg
RA of node: 220
2645 deg
Eccentricity:
0003214
Arg of perigee: 130
9822 deg
Mean anomaly: 229
1609 deg
Mean motion: 15
54112285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2099
Checksum: 299
Coasting Arc #7 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2018/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5314248
38 A = 6781648
93 meter
Y = 429082
10 meter E =
0011047
Z = -4203027
78 I = 51
41424
XDOT = -3360
063301 Wp = 117
34010
YDOT = -5830
531642 meter/sec RA = 214
35999 deg
ZDOT = 3655
626902 TA = 190
28650
MA = 190
30912
Ha = 221
893 n
mi
Hp = 213
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17435198
10 X = -5298235
77
Y = 1407749
68 feet Y = 369743
91 meter
Z = -13789461
22 Z = -4228803
25
XDOT = -11023
829728 XDOT = -3312
371809
YDOT = -19129
040821 feet/sec YDOT = -5867
839385 meter/sec
ZDOT = 11993
526582 ZDOT = 3639
421193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16252211
29 X = -4953674
00
Y = -6217132
21 feet Y = -1894981
90 meter
Z = -13904316
87 Z = -4238035
78
XDOT = -2212
491197 XDOT = -674
367317
YDOT = -20861
636640 feet/sec YDOT = -6358
626848 meter/sec
ZDOT = 11922
048729 ZDOT = 3633
840453
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 18056
50944246
00016717 00000-0 10270-3 0 9067
2 25544 51
6374 215
4561 0003164 134
9202 225
2208 15
54156151 21140
Satellite: ISS
Catalog Number: 25544
Epoch time: 18056
50944246 = yrday
fracday
Element set: 906
Inclination: 51
6374 deg
RA of node: 215
4561 deg
Eccentricity:
0003164
Arg of perigee: 134
9202 deg
Mean anomaly: 225
2208 deg
Mean motion: 15
54156151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 281
Coasting Arc #8 (Orbit 2126)
---------------------------------------
Vector Time (GMT): 2018/057/06:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1694926
81 A = 6781511
41 meter
Y = -4964820
79 meter E =
0012311
Z = 4290335
02 I = 51
43786
XDOT = 6778
775823 Wp = 112
28948
YDOT = 735
053417 meter/sec RA = 210
46118 deg
ZDOT = 3515
938372 TA = 301
76865
MA = 301
88854
Ha = 221
806 n
mi
Hp = 213
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5560783
51 X = -1660122
64
Y = -16288782
13 feet Y = -4983579
85 meter
Z = 14075902
31 Z = 4282186
56
XDOT = 22240
078160 XDOT = 6752
974212
YDOT = 2411
592574 feet/sec YDOT = 810
714222 meter/sec
ZDOT = 11535
230880 ZDOT = 3548
803963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17029830
09 X = 5190692
21
Y = -2689893
43 feet Y = -819879
52 meter
Z = 14040196
68 Z = 4279451
95
XDOT = -6482
802118 XDOT = -1975
958085
YDOT = 20147
834707 feet/sec YDOT = 6141
060019 meter/sec
ZDOT = 11681
543180 ZDOT = 3560
534361
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 18057
34535155
00016717 00000-0 10270-3 0 9076
2 25544 51
6401 211
2936 0002603 130
7675 229
3704 15
54143713 21276
Satellite: ISS
Catalog Number: 25544
Epoch time: 18057
34535155 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 211
2936 deg
Eccentricity:
0002603
Arg of perigee: 130
7675 deg
Mean anomaly: 229
3704 deg
Mean motion: 15
54143713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2127
Checksum: 286
Coasting Arc #9 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2018/058/06:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 60149
90 A = 6778284
11 meter
Y = 4507005
73 meter E =
0014667
Z = -5075438
06 I = 51
45488
XDOT = -7211
632915 Wp = 85
45586
YDOT = -1880
606517 meter/sec RA = 205
45244 deg
ZDOT = -1758
710495 TA = 167
48558
MA = 167
44912
Ha = 221
657 n
mi
Hp = 213
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 197342
20 X = 34400
10
Y = 14786764
20 feet Y = 4507534
10 meter
Z = -16651699
69 Z = -5075208
68
XDOT = -23660
212976 XDOT = -7181
524796
YDOT = -6169
968887 feet/sec YDOT = -1961
083705 meter/sec
ZDOT = -5770
047556 ZDOT = -1793
668053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14645058
83 X = -4463813
93
Y = -2055724
68 feet Y = -626584
88 meter
Z = -16651206
87 Z = -5075287
85
XDOT = 9710
309902 XDOT = 2959
702458
YDOT = -21266
600107 feet/sec YDOT = -6482
059713 meter/sec
ZDOT = -5925
567529 ZDOT = -1806
112983
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 18058
30985719
00016717 00000-0 10270-3 0 9089
2 25544 51
6387 206
4842 0002553 135
3188 224
8170 15
54180714 21421
Satellite: ISS
Catalog Number: 25544
Epoch time: 18058
30985719 = yrday
fracday
Element set: 908
Inclination: 51
6387 deg
RA of node: 206
4842 deg
Eccentricity:
0002553
Arg of perigee: 135
3188 deg
Mean anomaly: 224
8170 deg
Mean motion: 15
54180714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 314
Coasting Arc #10 (Orbit 2152)
---------------------------------------
Vector Time (GMT): 2018/058/23:08:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1305431
53 A = 6779511
36 meter
Y = -4630033
25 meter E =
0010127
Z = 4772193
25 I = 51
47704
XDOT = 7182
818758 Wp = 124
19475
YDOT = 673
889329 meter/sec RA = 202
09274 deg
ZDOT = 2609
122351 TA = 299
98824
MA = 300
08871
Ha = 221
689 n
mi
Hp = 213
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4282911
84 X = -1276740
45
Y = -15190397
80 feet Y = -4644470
72 meter
Z = 15656802
01 Z = 4765922
09
XDOT = 23565
678341 XDOT = 7162
075881
YDOT = 2210
922996 feet/sec YDOT = 754
096750 meter/sec
ZDOT = 8560
112700 ZDOT = 2643
962697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5383870
70 X = -1641003
79
Y = 14864817
94 feet Y = 4530796
51 meter
Z = 15629398
33 Z = 4763840
61
XDOT = -16630
417726 XDOT = -5068
951323
YDOT = -15219
892501 feet/sec YDOT = -4639
023234 meter/sec
ZDOT = 8715
267001 ZDOT = 2656
413382
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 18059
01716070
00016717 00000-0 10270-3 0 9091
2 25544 51
6365 202
9580 0002698 139
6292 220
5062 15
54190440 21532
Satellite: ISS
Catalog Number: 25544
Epoch time: 18059
01716070 = yrday
fracday
Element set: 909
Inclination: 51
6365 deg
RA of node: 202
9580 deg
Eccentricity:
0002698
Arg of perigee: 139
6292 deg
Mean anomaly: 220
5062 deg
Mean motion: 15
54190440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2153
Checksum: 297
Coasting Arc #11 (Orbit 2167)
---------------------------------------
Vector Time (GMT): 2018/059/23:08:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -449372
27 A = 6777432
09 meter
Y = 4250285
30 meter E =
0016233
Z = -5273891
68 I = 51
50187
XDOT = -7434
458863 Wp = 92
53167
YDOT = -1681
866161 meter/sec RA = 197
08356 deg
ZDOT = -724
600226 TA = 170
53839
MA = 170
50777
Ha = 221
681 n
mi
Hp = 213
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1474318
47 X = -471249
56
Y = 13944505
58 feet Y = 4245137
27 meter
Z = -17302794
22 Z = -5276128
07
XDOT = -24391
269234 XDOT = -7411
579602
YDOT = -5517
933600 feet/sec YDOT = -1764
875534 meter/sec
ZDOT = -2377
297330 ZDOT = -760
657614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9117381
91 X = 2778978
01
Y = -10636465
95 feet Y = -3241994
82 meter
Z = -17313245
73 Z = -5277077
30
XDOT = 16016
091510 XDOT = 4881
704692
YDOT = 17845
448066 feet/sec YDOT = 5439
292571 meter/sec
ZDOT = -2537
779906 ZDOT = -773
515315
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 18059
98166162
00016717 00000-0 10270-3 0 9100
2 25544 51
6375 198
1487 0002728 140
5071 219
6281 15
54171330 21680
Satellite: ISS
Catalog Number: 25544
Epoch time: 18059
98166162 = yrday
fracday
Element set: 910
Inclination: 51
6375 deg
RA of node: 198
1487 deg
Eccentricity:
0002728
Arg of perigee: 140
5071 deg
Mean anomaly: 219
6281 deg
Mean motion: 15
54171330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2168
Checksum: 314
Coasting Arc #12 (Orbit 2177)
---------------------------------------
Vector Time (GMT): 2018/060/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3795379
92 A = 6782960
82 meter
Y = 4096001
71 meter E =
0007532
Z = -3856039
41 I = 51
54391
XDOT = -6183
024881 Wp = 98
54693
YDOT = 1847
518203 meter/sec RA = 193
92319 deg
ZDOT = -4131
279628 TA = 127
97392
MA = 127
90586
Ha = 221
666 n
mi
Hp = 214
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12452033
87 X = 3768025
41
Y = 13438325
82 feet Y = 4138290
87 meter
Z = -12651047
92 Z = -3837670
11
XDOT = -20285
514703 XDOT = -6183
157694
YDOT = 6061
411426 feet/sec YDOT = 1778
374156 meter/sec
ZDOT = -13554
067021 ZDOT = -4161
314437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15538388
02 X = 4736100
67
Y = 9810868
03 feet Y = 2990352
58 meter
Z = -12569651
07 Z = -3831229
65
XDOT = -17277
253414 XDOT = -5266
106841
YDOT = 9860
308885 feet/sec YDOT = 3005
422148 meter/sec
ZDOT = -13688
123409 ZDOT = -4172
140015
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 18060
62465832
00016717 00000-0 10270-3 0 9110
2 25544 51
6410 194
9410 0002975 150
6464 209
4857 15
54179389 21781
Satellite: ISS
Catalog Number: 25544
Epoch time: 18060
62465832 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 194
9410 deg
Eccentricity:
0002975
Arg of perigee: 150
6464 deg
Mean anomaly: 209
4857 deg
Mean motion: 15
54179389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2178
Checksum: 325
Coasting Arc #13 (Orbit 2193)
---------------------------------------
Vector Time (GMT): 2018/061/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2219387
74 A = 6779252
87 meter
Y = -4218032
92 meter E =
0009867
Z = 4816731
80 I = 51
56458
XDOT = 7190
134779 Wp = 129
11318
YDOT = -894
820365 meter/sec RA = 188
92698 deg
ZDOT = 2519
810970 TA = 296
04301
MA = 296
14456
Ha = 221
571 n
mi
Hp = 213
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7281455
84 X = -2195452
28
Y = -13838690
67 feet Y = -4242717
16 meter
Z = 15802925
86 Z = 4806009
71
XDOT = 23589
681034 XDOT = 7187
366853
YDOT = -2935
762353 feet/sec YDOT = -814
430473 meter/sec
ZDOT = 8267
096359 ZDOT = 2554
730843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10855790
38 X = -3308844
91
Y = -11321393
08 feet Y = -3450760
61 meter
Z = 15755611
65 Z = 4802310
43
XDOT = 21035
690129 XDOT = 6411
678351
YDOT = -8405
009371 feet/sec YDOT = -2561
846856 meter/sec
ZDOT = 8422
829144 ZDOT = 2567
278323
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 18061
65344832
00016717 00000-0 10270-3 0 9121
2 25544 51
6414 189
8125 0002897 153
5615 206
5686 15
54225877 21944
Satellite: ISS
Catalog Number: 25544
Epoch time: 18061
65344832 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 189
8125 deg
Eccentricity:
0002897
Arg of perigee: 153
5615 deg
Mean anomaly: 206
5686 deg
Mean motion: 15
54225877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2194
Checksum: 329
Coasting Arc #14 (Orbit 2208)
---------------------------------------
Vector Time (GMT): 2018/062/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 407547
73 A = 6777333
32 meter
Y = 4232737
22 meter E =
0015719
Z = -5290738
79 I = 51
58986
XDOT = -7632
197082 Wp = 95
15847
YDOT = -33
048610 meter/sec RA = 183
92498 deg
ZDOT = -617
314420 TA = 168
95349
MA = 168
91894
Ha = 221
493 n
mi
Hp = 214
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1337098
86 X = 385885
05
Y = 13886933
12 feet Y = 4237172
80 meter
Z = -17358066
89 Z = -5288812
32
XDOT = -25040
016673 XDOT = -7628
261745
YDOT = -108
427198 feet/sec YDOT = -118
375171 meter/sec
ZDOT = -2025
309776 ZDOT = -654
378843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5378835
72 X = 1639469
13
Y = 12883499
36 feet Y = 3926890
60 meter
Z = -17349951
06 Z = -5288265
08
XDOT = -23063
245862 XDOT = -7029
677339
YDOT = 6692
040263 feet/sec YDOT = 2039
733872 meter/sec
ZDOT = -2190
512115 ZDOT = -667
668093
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 18062
61793673
00016717 00000-0 10270-3 0 9130
2 25544 51
6408 185
0049 0002816 157
5013 202
6263 15
54187366 22092
Satellite: ISS
Catalog Number: 25544
Epoch time: 18062
61793673 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 185
0049 deg
Eccentricity:
0002816
Arg of perigee: 157
5013 deg
Mean anomaly: 202
6263 deg
Mean motion: 15
54187366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2209
Checksum: 306
Coasting Arc #15 (Orbit 2224)
---------------------------------------
Vector Time (GMT): 2018/063/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1439102
49 A = 6777545
54 meter
Y = -4126799
83 meter E =
0004360
Z = 5176317
65 I = 51
62516
XDOT = 7496
359244 Wp = 92
38386
YDOT = 924
941287 meter/sec RA = 178
92216 deg
ZDOT = -1345
905473 TA = 10
55116
MA = 10
54202
Ha = 221
288 n
mi
Hp = 214
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4721464
86 X = 1459998
98
Y = -13539369
51 feet Y = -4110589
21 meter
Z = 16982669
45 Z = 5183359
58
XDOT = 24594
354474 XDOT = 7491
996785
YDOT = 3034
584274 feet/sec YDOT = 1008
746145 meter/sec
ZDOT = -4415
700372 ZDOT = -1309
501898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 280586
15 X = 85522
66
Y = -14298435
45 feet Y = -4358163
13 meter
Z = 17014518
32 Z = 5186025
19
XDOT = 23338
970598 XDOT = 7113
718238
YDOT = -4606
641763 feet/sec YDOT = -1404
104409 meter/sec
ZDOT = -4253
527349 ZDOT = -1296
475136
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 18063
64671548
00016717 00000-0 10270-3 0 9141
2 25544 51
6417 179
8758 0002696 161
3082 198
8170 15
54250255 22254
Satellite: ISS
Catalog Number: 25544
Epoch time: 18063
64671548 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 179
8758 deg
Eccentricity:
0002696
Arg of perigee: 161
3082 deg
Mean anomaly: 198
8170 deg
Mean motion: 15
54250255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2225
Checksum: 329
Coasting Arc #16 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2018/063/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3748675
55 A = 6780642
74 meter
Y = -3438476
21 meter E =
0011367
Z = 4478132
90 I = 51
63748
XDOT = 6392
700565 Wp = 120
29198
YDOT = -2743
503203 meter/sec RA = 178
35678 deg
ZDOT = 3233
072397 TA = 297
13592
MA = 297
25179
Ha = 221
583 n
mi
Hp = 214
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12298804
29 X = -3731699
15
Y = -11281089
93 feet Y = -3480300
92 meter
Z = 14692037
08 Z = 4459965
06
XDOT = 20973
427051 XDOT = 6407
199650
YDOT = -9000
994760 feet/sec YDOT = -2671
934099 meter/sec
ZDOT = 10607
192903 ZDOT = 3264
161191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15858952
71 X = -4833808
79
Y = 5420260
35 feet Y = 1652095
35 meter
Z = 14611431
38 Z = 4453564
29
XDOT = 2589
639363 XDOT = 789
322078
YDOT = -21495
731148 feet/sec YDOT = -6551
898854 meter/sec
ZDOT = 10746
083092 ZDOT = 3275
406126
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 18063
77531416
00016717 00000-0 10270-3 0 9155
2 25544 51
6403 179
2357 0002720 151
3417 208
7885 15
54220336 22270
Satellite: ISS
Catalog Number: 25544
Epoch time: 18063
77531416 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 179
2357 deg
Eccentricity:
0002720
Arg of perigee: 151
3417 deg
Mean anomaly: 208
7885 deg
Mean motion: 15
54220336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 299
Coasting Arc #17 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2018/064/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2050476
35 A = 6777804
06 meter
Y = 3882417
06 meter E =
0014587
Z = -5176062
51 I = 51
66174
XDOT = -7266
196116 Wp = 89
58740
YDOT = 1965
990994 meter/sec RA = 173
36180 deg
ZDOT = -1407
169624 TA = 166
88282
MA = 166
84485
Ha = 221
424 n
mi
Hp = 214
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6727284
62 X = 2032052
11
Y = 12737588
79 feet Y = 3905243
21 meter
Z = -16981832
38 Z = -5166147
33
XDOT = -23839
226102 XDOT = -7280
805087
YDOT = 6450
101685 feet/sec YDOT = 1884
653526 meter/sec
ZDOT = -4616
698242 ZDOT = -1442
501753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14456052
13 X = 4406204
69
Y = -99035
71 feet Y = -30186
09 meter
Z = -16938060
88 Z = -5162720
96
XDOT = -5423
703877 XDOT = -1653
144942
YDOT = 23010
197509 feet/sec YDOT = 7013
508201 meter/sec
ZDOT = -4774
434181 ZDOT = -1455
247538
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 18064
73978877
00016717 00000-0 10270-3 0 9169
2 25544 51
6412 174
4277 0002640 156
3134 203
8141 15
54215141 22426
Satellite: ISS
Catalog Number: 25544
Epoch time: 18064
73978877 = yrday
fracday
Element set: 916
Inclination: 51
6412 deg
RA of node: 174
4277 deg
Eccentricity:
0002640
Arg of perigee: 156
3134 deg
Mean anomaly: 203
8141 deg
Mean motion: 15
54215141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 299
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