[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 10th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
344/23:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
4
354/01:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 214
1
358/04:25:00
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
6
Coasting Arc #1 (Orbit 2593)
---------------------------------------
Vector Time (GMT): 2018/344/14:03:13
160
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -355463
43 A = 6779402
16 meter
Y = 4703817
93 meter E =
0014932
Z = -4882126
40 I = 51
38123
XDOT = -6676
185000 Wp = 89
21244
YDOT = -2928
835161 meter/sec RA = 218
55527 deg
ZDOT = -2341
800698 TA = 157
77669
MA = 157
71190
Ha = 222
597 n
mi
Hp = 213
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1166218
59 X = -384321
59
Y = 15432473
54 feet Y = 4699682
13 meter
Z = -16017475
06 Z = -4883922
64
XDOT = -21903
494095 XDOT = -6631
562512
YDOT = -9609
039243 feet/sec YDOT = -3003
243118 meter/sec
ZDOT = -7683
073156 ZDOT = -2374
123309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14923111
98 X = -4548564
53
Y = 4067815
15 feet Y = 1239870
06 meter
Z = -16026054
45 Z = -4884741
40
XDOT = 2195
840421 XDOT = 669
292160
YDOT = -22707
553717 feet/sec YDOT = -6921
262373 meter/sec
ZDOT = -7828
212161 ZDOT = -2386
039067
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 18344
60586513
00016717 00000-0 10270-3 0 9001
2 25544 51
6371 219
5539 0004789 132
3433 227
8126 15
54072319 25941
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
60586513 = yrday
fracday
Element set: 900
Inclination: 51
6371 deg
RA of node: 219
5539 deg
Eccentricity:
0004789
Arg of perigee: 132
3433 deg
Mean anomaly: 227
8126 deg
Mean motion: 15
54072319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 316
Coasting Arc #2 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2018/344/23:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -680088
52 A = 6778815
54 meter
Y = 4503560
54 meter E =
0016035
Z = -5034469
08 I = 51
39031
XDOT = -6730
993987 Wp = 92
11859
YDOT = -3122
200815 meter/sec RA = 216
61778 deg
ZDOT = -1889
489779 TA = 159
50404
MA = 159
43963
Ha = 222
682 n
mi
Hp = 213
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2231261
53 X = -705943
25
Y = 14775461
10 feet Y = 4495811
35 meter
Z = -16517287
01 Z = -5037834
98
XDOT = -22083
313606 XDOT = -6686
402257
YDOT = -10243
440994 feet/sec YDOT = -3197
221918 meter/sec
ZDOT = -6199
113448 ZDOT = -1922
078685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13001072
44 X = 3962726
88
Y = 7331348
43 feet Y = 2234595
00 meter
Z = -16532906
40 Z = -5039229
87
XDOT = -17001
139423 XDOT = -5181
947296
YDOT = 15882
356620 feet/sec YDOT = 4840
942298 meter/sec
ZDOT = -6345
440581 ZDOT = -1934
090289
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 18344
99169217
00016717 00000-0 10270-3 0 9012
2 25544 51
6382 217
6299 0005094 136
6468 223
5086 15
54052103 26005
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
99169217 = yrday
fracday
Element set: 901
Inclination: 51
6382 deg
RA of node: 217
6299 deg
Eccentricity:
0005094
Arg of perigee: 136
6468 deg
Mean anomaly: 223
5086 deg
Mean motion: 15
54052103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 311
Coasting Arc #3 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2018/345/23:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2205183
47 A = 6777429
47 meter
Y = -3603400
56 meter E =
0006881
Z = 5294738
83 I = 51
41412
XDOT = 6538
110998 Wp = 124
63350
YDOT = 4016
540894 meter/sec RA = 211
60306 deg
ZDOT = 6
631448 TA = 325
28071
MA = 325
32560
Ha = 222
489 n
mi
Hp = 213
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7234853
89 X = 2219594
81
Y = -11822180
33 feet Y = -3578660
65 meter
Z = 17371190
38 Z = 5305485
45
XDOT = 21450
495399 XDOT = 6492
678776
YDOT = 13177
627605 feet/sec YDOT = 4089
400567 meter/sec
ZDOT = 21
756719 ZDOT = 38
281346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8623790
45 X = -2628531
33
Y = -10772259
83 feet Y = -3283384
80 meter
Z = 17419930
25 Z = 5309594
74
XDOT = 19005
384785 XDOT = 5792
841283
YDOT = -14929
650087 feet/sec YDOT = -4550
557346 meter/sec
ZDOT = 163
791488 ZDOT = 49
923645
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 18346
02055802
00016717 00000-0 10270-3 0 9023
2 25544 51
6387 212
5014 0004996 139
0979 221
0549 15
54099173 26165
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
02055802 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 212
5014 deg
Eccentricity:
0004996
Arg of perigee: 139
0979 deg
Mean anomaly: 221
0549 deg
Mean motion: 15
54099173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 312
Coasting Arc #4 (Orbit 2630)
---------------------------------------
Vector Time (GMT): 2018/346/23:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3712664
17 A = 6778679
50 meter
Y = 2632808
57 meter E =
0017370
Z = -5039235
76 I = 51
44607
XDOT = -5823
262898 Wp = 114
15640
YDOT = -4596
536232 meter/sec RA = 206
58992 deg
ZDOT = 1886
977005 TA = 174
22720
MA = 174
20715
Ha = 222
591 n
mi
Hp = 213
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12180656
72 X = -3717351
15
Y = 8637823
39 feet Y = 2591265
23 meter
Z = -16532925
72 Z = -5057281
69
XDOT = -19105
193235 XDOT = -5780
596261
YDOT = -15080
499448 feet/sec YDOT = -4661
417614 meter/sec
ZDOT = 6190
869440 ZDOT = 1858
792895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4167417
92 X = 1270228
98
Y = 14244702
22 feet Y = 4341785
24 meter
Z = -16614424
77 Z = -5064076
67
XDOT = -19516
754589 XDOT = -5948
706799
YDOT = 12790
021673 feet/sec YDOT = 3898
398606 meter/sec
ZDOT = 6064
468314 ZDOT = 1848
449942
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 18346
98512045
00016717 00000-0 10270-3 0 9036
2 25544 51
6379 207
6935 0005007 140
4439 219
7079 15
54064985 26316
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
98512045 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 207
6935 deg
Eccentricity:
0005007
Arg of perigee: 140
4439 deg
Mean anomaly: 219
7079 deg
Mean motion: 15
54064985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 326
Coasting Arc #5 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2018/347/23:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5019972
68 A = 6781611
16 meter
Y = -1643980
46 meter E =
0012333
Z = 4241478
37 I = 51
48651
XDOT = 4659
519771 Wp = 95
94315
YDOT = 4923
352123 meter/sec RA = 201
58512 deg
ZDOT = -3598
712810 TA = 30
91068
MA = 30
83813
Ha = 222
306 n
mi
Hp = 213
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16469726
64 X = 5017380
22
Y = -5393636
69 feet Y = -1587858
46 meter
Z = 13915611
46 Z = 4265857
18
XDOT = 15287
138357 XDOT = 4621
599773
YDOT = 16152
730062 feet/sec YDOT = 4975
246366 meter/sec
ZDOT = -11806
800559 ZDOT = -3576
170249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19854
75 X = 6051
73
Y = -17241566
16 feet Y = -5255229
37 meter
Z = 14025528
75 Z = 4274981
16
XDOT = 18901
041893 XDOT = 5761
037569
YDOT = -9521
121057 feet/sec YDOT = -2902
037698 meter/sec
ZDOT = -11705
806872 ZDOT = -3567
929934
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 18348
01398264
00016717 00000-0 10270-3 0 9048
2 25544 51
6379 202
5650 0004948 145
4369 214
7106 15
54111856 26477
Satellite: ISS
Catalog Number: 25544
Epoch time: 18348
01398264 = yrday
fracday
Element set: 904
Inclination: 51
6379 deg
RA of node: 202
5650 deg
Eccentricity:
0004948
Arg of perigee: 145
4369 deg
Mean anomaly: 214
7106 deg
Mean motion: 15
54111856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 319
Coasting Arc #6 (Orbit 2661)
---------------------------------------
Vector Time (GMT): 2018/348/23:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6030316
85 A = 6785345
51 meter
Y = 720294
27 meter E =
0007740
Z = -3036024
49 I = 51
53133
XDOT = -3072
530721 Wp = 112
61614
YDOT = -4997
949118 meter/sec RA = 196
59166 deg
ZDOT = 4924
207734 TA = 212
55644
MA = 212
60420
Ha = 222
448 n
mi
Hp = 213
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19784504
11 X = -6023175
81
Y = 2363170
19 feet Y = 652899
20 meter
Z = -9960710
27 Z = -3065300
27
XDOT = -10080
481367 XDOT = -3040
333083
YDOT = -16397
470860 feet/sec YDOT = -5032
128583 meter/sec
ZDOT = 16155
537184 ZDOT = 4909
360335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3610169
94 X = -1100379
80
Y = 19527751
74 feet Y = 5952058
73 meter
Z = -10092596
80 Z = -3076223
50
XDOT = -17260
724544 XDOT = -5261
068841
YDOT = 5112
423807 feet/sec YDOT = 1558
266777 meter/sec
ZDOT = 16089
179966 ZDOT = 4903
982054
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 18348
97854032
00016717 00000-0 10270-3 0 9054
2 25544 51
6388 197
7567 0005093 146
0150 214
1330 15
54119183 26627
Satellite: ISS
Catalog Number: 25544
Epoch time: 18348
97854032 = yrday
fracday
Element set: 905
Inclination: 51
6388 deg
RA of node: 197
7567 deg
Eccentricity:
0005093
Arg of perigee: 146
0150 deg
Mean anomaly: 214
1330 deg
Mean motion: 15
54119183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2662
Checksum: 315
Coasting Arc #7 (Orbit 2677)
---------------------------------------
Vector Time (GMT): 2018/349/23:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6612827
54 A = 6788413
91 meter
Y = 159101
74 meter E =
0018283
Z = 1481129
29 I = 51
57336
XDOT = 1183
052324 Wp = 126
48186
YDOT = 4917
405264 meter/sec RA = 191
61064 deg
ZDOT = -5771
346172 TA = 37
32272
MA = 37
19583
Ha = 222
332 n
mi
Hp = 213
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21695628
42 X = 6603362
39
Y = 521987
34 feet Y = 232997
97 meter
Z = 4859348
05 Z = 1513229
19
XDOT = 3881
405262 XDOT = 1156
010797
YDOT = 16133
219371 feet/sec YDOT = 4930
484106 meter/sec
ZDOT = -18934
862768 ZDOT = -5765
664705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6588865
23 X = 2008286
12
Y = -20643014
71 feet Y = -6291990
88 meter
Z = 5003881
07 Z = 1525182
95
XDOT = 15102
632932 XDOT = 4603
282518
YDOT = 206
716296 feet/sec YDOT = 63
007127 meter/sec
ZDOT = -18909
760235 ZDOT = -5763
694919
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 18350
00739781
00016717 00000-0 10270-3 0 9065
2 25544 51
6387 192
6282 0004936 149
5814 210
5626 15
54105993 26783
Satellite: ISS
Catalog Number: 25544
Epoch time: 18350
00739781 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 192
6282 deg
Eccentricity:
0004936
Arg of perigee: 149
5814 deg
Mean anomaly: 210
5626 deg
Mean motion: 15
54105993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2678
Checksum: 332
Coasting Arc #8 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2018/350/23:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6719665
89 A = 6789472
73 meter
Y = -931066
23 meter E =
0012040
Z = 186972
87 I = 51
60903
XDOT = 826
027019 Wp = 70
29340
YDOT = -4693
359966 meter/sec RA = 186
63727 deg
ZDOT = 6004
262811 TA = 291
72101
MA = 291
84914
Ha = 222
349 n
mi
Hp = 213
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22046147
94 X = -6709663
25
Y = -3054679
24 feet Y = -1006154
29 meter
Z = 613428
04 Z = 154355
15
XDOT = 2710
062399 XDOT = 849
282417
YDOT = -15398
162617 feet/sec YDOT = -4683
993067 meter/sec
ZDOT = 19699
024972 ZDOT = 6008
331602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8777275
98 X = -2675313
72
Y = 20456825
01 feet Y = 6235240
26 meter
Z = 466620
71 Z = 142225
99
XDOT = -12674
803808 XDOT = -3863
280201
YDOT = -5918
662482 feet/sec YDOT = -1804
008324 meter/sec
ZDOT = 19717
806910 ZDOT = 6009
987546
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 18351
03625554
00016717 00000-0 10270-3 0 9072
2 25544 51
6385 187
4998 0004865 152
4585 207
6826 15
54075669 26949
Satellite: ISS
Catalog Number: 25544
Epoch time: 18351
03625554 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 187
4998 deg
Eccentricity:
0004865
Arg of perigee: 152
4585 deg
Mean anomaly: 207
6826 deg
Mean motion: 15
54075669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2694
Checksum: 355
Coasting Arc #9 (Orbit 2708)
---------------------------------------
Vector Time (GMT): 2018/351/23:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6297828
07 A = 6787990
91 meter
Y = 1673933
34 meter E =
0012039
Z = -1882715
28 I = 51
63781
XDOT = -2836
007746 Wp = 148
17576
YDOT = 4372
238372 meter/sec RA = 181
66535 deg
ZDOT = -5625
670794 TA = 52
55567
MA = 52
44620
Ha = 222
319 n
mi
Hp = 213
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20662165
57 X = 6287786
91
Y = 5491907
28 feet Y = 1744304
01 meter
Z = -6176887
39 Z = -1852146
66
XDOT = -9304
487355 XDOT = -2857
361820
YDOT = 14344
614081 feet/sec YDOT = 4340
405135 meter/sec
ZDOT = -18456
925178 ZDOT = -5639
498816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10451081
60 X = 3185489
67
Y = -18696016
90 feet Y = -5698545
95 meter
Z = -6039363
79 Z = -1840798
08
XDOT = 10256
972926 XDOT = 3126
325348
YDOT = 11687
435792 feet/sec YDOT = 3562
330429 meter/sec
ZDOT = -18519
635617 ZDOT = -5644
784936
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 18352
00080448
00016717 00000-0 10270-3 0 9088
2 25544 51
6390 182
6916 0004920 157
3370 202
8001 15
54093592 27094
Satellite: ISS
Catalog Number: 25544
Epoch time: 18352
00080448 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 182
6916 deg
Eccentricity:
0004920
Arg of perigee: 157
3370 deg
Mean anomaly: 202
8001 deg
Mean motion: 15
54093592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2709
Checksum: 296
Coasting Arc #10 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2018/352/23:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5417513
04 A = 6784801
27 meter
Y = -2335218
15 meter E =
0014946
Z = 3343266
57 I = 51
65903
XDOT = 4607
681000 Wp = 106
18329
YDOT = -3968
656812 meter/sec RA = 176
68873 deg
ZDOT = 4672
933483 TA = 292
76481
MA = 292
92267
Ha = 222
264 n
mi
Hp = 213
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17773992
90 X = -5407237
31
Y = -7661476
87 feet Y = -2395743
37 meter
Z = 10968722
36 Z = 3316974
69
XDOT = 15117
063648 XDOT = 4629
018324
YDOT = -13020
527598 feet/sec YDOT = -3917
011609 meter/sec
ZDOT = 15331
146599 ZDOT = 4695
367700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11578251
13 X = -3529050
94
Y = 15592832
22 feet Y = 4752695
26 meter
Z = 10850511
77 Z = 3307235
99
XDOT = -8059
397849 XDOT = -2456
504464
YDOT = -16772
855837 feet/sec YDOT = -5112
366459 meter/sec
ZDOT = 15432
596882 ZDOT = 4703
855529
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 18353
02965566
00016717 00000-0 10270-3 0 9095
2 25544 51
6377 177
5628 0004779 158
5067 201
6287 15
54091844 27259
Satellite: ISS
Catalog Number: 25544
Epoch time: 18353
02965566 = yrday
fracday
Element set: 909
Inclination: 51
6377 deg
RA of node: 177
5628 deg
Eccentricity:
0004779
Arg of perigee: 158
5067 deg
Mean anomaly: 201
6287 deg
Mean motion: 15
54091844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2725
Checksum: 348
Coasting Arc #11 (Orbit 2739)
---------------------------------------
Vector Time (GMT): 2018/353/23:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4105070
55 A = 6780926
10 meter
Y = 2994383
27 meter E =
0010244
Z = -4498330
72 I = 51
67859
XDOT = -6035
378888 Wp = 97
84644
YDOT = 3450
569206 meter/sec RA = 171
70497 deg
ZDOT = -3218
465157 TA = 139
81474
MA = 139
73895
Ha = 222
125 n
mi
Hp = 214
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13468079
24 X = 4093132
15
Y = 9824092
10 feet Y = 3040222
76 meter
Z = -14758302
89 Z = -4478418
19
XDOT = -19801
111837 XDOT = -6057
881802
YDOT = 11320
765111 feet/sec YDOT = 3382
951928 meter/sec
ZDOT = -10559
268887 ZDOT = -3247
837505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12502778
94 X = 3810847
02
Y = -11145125
05 feet Y = -3397034
12 meter
Z = -14668883
88 Z = -4471075
81
XDOT = 6014
602704 XDOT = 1833
250904
YDOT = 20786
484400 feet/sec YDOT = 6335
720445 meter/sec
ZDOT = -10691
945318 ZDOT = -3258
904933
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 18353
99420109
00016717 00000-0 10270-3 0 9102
2 25544 51
6369 172
7551 0004802 163
6299 196
5009 15
54106936 27403
Satellite: ISS
Catalog Number: 25544
Epoch time: 18353
99420109 = yrday
fracday
Element set: 910
Inclination: 51
6369 deg
RA of node: 172
7551 deg
Eccentricity:
0004802
Arg of perigee: 163
6299 deg
Mean anomaly: 196
5009 deg
Mean motion: 15
54106936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2740
Checksum: 319
Coasting Arc #12 (Orbit 2741)
---------------------------------------
Vector Time (GMT): 2018/354/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2943269
57 A = 6778928
91 meter
Y = -3528911
74 meter E =
0010155
Z = 4980800
74 I = 51
67353
XDOT = 6851
046858 Wp = 141
19624
YDOT = -2738
174373 meter/sec RA = 171
20755 deg
ZDOT = 2098
380126 TA = 288
33989
MA = 288
45032
Ha = 222
076 n
mi
Hp = 214
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9656396
23 X = -2927783
87
Y = -11577794
42 feet Y = -3561739
39 meter
Z = 16341209
79 Z = 4966540
45
XDOT = 22477
187855 XDOT = 6870
963786
YDOT = -8983
511723 feet/sec YDOT = -2661
450073 meter/sec
ZDOT = 6884
449233 ZDOT = 2131
708532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6789076
52 X = -2069310
52
Y = 13538246
11 feet Y = 4126457
41 meter
Z = 16277308
79 Z = 4961323
72
XDOT = -16111
393727 XDOT = -4910
752808
YDOT = -16577
448442 feet/sec YDOT = -5052
806285 meter/sec
ZDOT = 7034
881657 ZDOT = 2144
231929
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 18354
12280769
00016717 00000-0 10270-3 0 9115
2 25544 51
6352 172
1140 0004618 165
7336 194
3947 15
54111288 27428
Satellite: ISS
Catalog Number: 25544
Epoch time: 18354
12280769 = yrday
fracday
Element set: 911
Inclination: 51
6352 deg
RA of node: 172
1140 deg
Eccentricity:
0004618
Arg of perigee: 165
7336 deg
Mean anomaly: 194
3947 deg
Mean motion: 15
54111288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 307
Coasting Arc #13 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2018/355/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1211612
44 A = 6777467
79 meter
Y = 4032214
64 meter E =
0016280
Z = -5324538
30 I = 51
70184
XDOT = -7396
002932 Wp = 104
81272
YDOT = 1972
576393 meter/sec RA = 166
21155 deg
ZDOT = -193
725236 TA = 163
36659
MA = 163
31312
Ha = 221
953 n
mi
Hp = 214
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3975106
43 X = 1192297
02
Y = 13229050
66 feet Y = 4045656
44 meter
Z = -17468957
69 Z = -5318699
04
XDOT = -24265
101482 XDOT = -7416
570125
YDOT = 6471
707327 feet/sec YDOT = 1889
754175 meter/sec
ZDOT = -635
581483 ZDOT = -229
702421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10387362
00 X = 3166067
94
Y = -9155137
61 feet Y = -2790485
94 meter
Z = -17443047
36 Z = -5316640
83
XDOT = 15181
698789 XDOT = 4627
381791
YDOT = 18716
757661 feet/sec YDOT = 5704
867735 meter/sec
ZDOT = -797
900735 ZDOT = -243
200144
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 18355
08735155
00016717 00000-0 10270-3 0 9126
2 25544 51
6358 167
3049 0004615 168
3239 191
8021 15
54097939 27573
Satellite: ISS
Catalog Number: 25544
Epoch time: 18355
08735155 = yrday
fracday
Element set: 912
Inclination: 51
6358 deg
RA of node: 167
3049 deg
Eccentricity:
0004615
Arg of perigee: 168
3239 deg
Mean anomaly: 191
8021 deg
Mean motion: 15
54097939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2757
Checksum: 333
Coasting Arc #14 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2018/356/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 539683
18 A = 6778325
46 meter
Y = -4429960
93 meter E =
0005026
Z = 5097423
36 I = 51
73735
XDOT = 7397
885804 Wp = 108
11468
YDOT = -1080
784503 meter/sec RA = 161
21811 deg
ZDOT = -1722
641091 TA = 358
50058
MA = 358
50209
Ha = 221
833 n
mi
Hp = 214
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1770614
10 X = 564419
47
Y = -14533992
57 feet Y = -4423788
27 meter
Z = 16723829
93 Z = 5100104
38
XDOT = 24271
278883 XDOT = 7417
789319
YDOT = -3545
880914 feet/sec YDOT = -997
944657 meter/sec
ZDOT = -5651
709615 ZDOT = -1686
656429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13856799
42 X = -4223552
46
Y = 4684213
00 feet Y = 1427748
12 meter
Z = 16736360
42 Z = 5101242
66
XDOT = -13213
685234 XDOT = -4027
531259
YDOT = -19476
889086 feet/sec YDOT = -5936
555793 meter/sec
ZDOT = -5489
415947 ZDOT = -1673
173981
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 18356
11619486
00016717 00000-0 10270-3 0 9130
2 25544 51
6362 162
1760 0004492 172
4025 187
7196 15
54109762 27736
Satellite: ISS
Catalog Number: 25544
Epoch time: 18356
11619486 = yrday
fracday
Element set: 913
Inclination: 51
6362 deg
RA of node: 162
1760 deg
Eccentricity:
0004492
Arg of perigee: 172
4025 deg
Mean anomaly: 187
7196 deg
Mean motion: 15
54109762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 320
Coasting Arc #15 (Orbit 2787)
---------------------------------------
Vector Time (GMT): 2018/357/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2191155
05 A = 6781311
50 meter
Y = 4718419
50 meter E =
0011401
Z = -4361855
41 I = 51
77818
XDOT = -6830
960357 Wp = 131
63216
YDOT = 29
347298 meter/sec RA = 156
23223 deg
ZDOT = 3461
703523 TA = 173
50164
MA = 173
48684
Ha = 221
734 n
mi
Hp = 214
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7188828
90 X = -2222567
36
Y = 15480378
93 feet Y = 4693741
52 meter
Z = -14310549
24 Z = -4372574
81
XDOT = -22411
287262 XDOT = -6847
595914
YDOT = 96
283787 feet/sec YDOT = -47
134799 meter/sec
ZDOT = 11357
295024 ZDOT = 3428
480781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17020819
69 X = 5187945
84
Y = -462544
18 feet Y = -140983
47 meter
Z = -14359351
04 Z = -4376730
20
XDOT = 9972
818912 XDOT = 3039
715204
YDOT = 18896
437077 feet/sec YDOT = 5759
634021 meter/sec
ZDOT = 11207
527810 ZDOT = 3416
054476
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 18357
08073375
00016717 00000-0 10270-3 0 9149
2 25544 51
6360 157
3678 0004415 176
2141 183
9046 15
54099212 27880
Satellite: ISS
Catalog Number: 25544
Epoch time: 18357
08073375 = yrday
fracday
Element set: 914
Inclination: 51
6360 deg
RA of node: 157
3678 deg
Eccentricity:
0004415
Arg of perigee: 176
2141 deg
Mean anomaly: 183
9046 deg
Mean motion: 15
54099212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2788
Checksum: 323
Coasting Arc #16 (Orbit 2803)
---------------------------------------
Vector Time (GMT): 2018/358/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3597833
65 A = 6785066
41 meter
Y = -4800412
03 meter E =
0013857
Z = 3152665
69 I = 51
82231
XDOT = 5823
174522 Wp = 112
82140
YDOT = 1164
816673 meter/sec RA = 151
25822 deg
ZDOT = -4860
095509 TA = 30
89479
MA = 30
81333
Ha = 221
566 n
mi
Hp = 214
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11803916
19 X = 3635931
97
Y = -15749383
30 feet Y = -4759966
00 meter
Z = 10343391
36 Z = 3170234
38
XDOT = 19104
903289 XDOT = 5833
323985
YDOT = 3821
577011 feet/sec YDOT = 1229
992923 meter/sec
ZDOT = -15945
195238 ZDOT = -4831
783982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19368754
46 X = -5903596
36
Y = -3251416
48 feet Y = -991031
74 meter
Z = 10423094
46 Z = 3176959
19
XDOT = -5607
701709 XDOT = -1709
227481
YDOT = -17423
984620 feet/sec YDOT = -5310
830512 meter/sec
ZDOT = -15817
665997 ZDOT = -4821
224596
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 18358
10957355
00016717 00000-0 10270-3 0 9153
2 25544 51
6374 152
2390 0004385 180
3428 179
7722 15
54121518 28048
Satellite: ISS
Catalog Number: 25544
Epoch time: 18358
10957355 = yrday
fracday
Element set: 915
Inclination: 51
6374 deg
RA of node: 152
2390 deg
Eccentricity:
0004385
Arg of perigee: 180
3428 deg
Mean anomaly: 179
7722 deg
Mean motion: 15
54121518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2804
Checksum: 315
Coasting Arc #17 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2018/358/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4920705
54 A = 6780963
42 meter
Y = -1284564
64 meter E =
0011504
Z = 4482280
88 I = 51
81324
XDOT = 4381
977102 Wp = 132
44826
YDOT = -5387
901012 meter/sec RA = 150
74389 deg
ZDOT = 3253
591148 TA = 284
82173
MA = 284
94915
Ha = 221
727 n
mi
Hp = 214
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16144047
05 X = -4927747
80
Y = -4214450
93 feet Y = -1339631
42 meter
Z = 14705645
94 Z = 4458360
74
XDOT = 14376
565294 XDOT = 4426
096374
YDOT = -17676
840591 feet/sec YDOT = -5338
652486 meter/sec
ZDOT = 10674
511639 ZDOT = 3274
983437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13484769
59 X = 4110157
77
Y = 9985459
77 feet Y = 3043568
14 meter
Z = 14597926
45 Z = 4449447
98
XDOT = -19152
394597 XDOT = -5837
649873
YDOT = 10054
784252 feet/sec YDOT = 3064
698240 meter/sec
ZDOT = 10771
516388 ZDOT = 3283
158195
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 18358
23817864
00016717 00000-0 10270-3 0 9168
2 25544 51
6390 151
5988 0004443 180
6210 179
4938 15
54117428 28061
Satellite: ISS
Catalog Number: 25544
Epoch time: 18358
23817864 = yrday
fracday
Element set: 916
Inclination: 51
6390 deg
RA of node: 151
5988 deg
Eccentricity:
0004443
Arg of perigee: 180
6210 deg
Mean anomaly: 179
4938 deg
Mean motion: 15
54117428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 333
Coasting Arc #18 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2018/359/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3648441
75 A = 6778048
23 meter
Y = 2438515
74 meter E =
0013243
Z = -5176662
64 I = 51
83381
XDOT = -5496
052119 Wp = 97
32350
YDOT = 5130
248698 meter/sec RA = 145
76135 deg
ZDOT = -1461
736855 TA = 158
65578
MA = 158
60050
Ha = 221
494 n
mi
Hp = 214
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11969953
24 X = 3646047
55
Y = 8000379
72 feet Y = 2479302
41 meter
Z = -16983801
30 Z = -5158945
53
XDOT = -18031
667057 XDOT = -5545
911280
YDOT = 16831
524599 feet/sec YDOT = 5068
509425 meter/sec
ZDOT = -4795
724591 ZDOT = -1488
554842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8415577
63 X = -2565068
06
Y = -11796734
32 feet Y = -3595644
62 meter
Z = -16904155
57 Z = -5152386
62
XDOT = 21973
908604 XDOT = 6697
647343
YDOT = -8652
583373 feet/sec YDOT = -2637
307412 meter/sec
ZDOT = -4917
188327 ZDOT = -1498
759002
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 18359
20271171
00016717 00000-0 10270-3 0 9172
2 25544 51
6406 146
7906 0004309 184
0218 176
0900 15
54145015 28214
Satellite: ISS
Catalog Number: 25544
Epoch time: 18359
20271171 = yrday
fracday
Element set: 917
Inclination: 51
6406 deg
RA of node: 146
7906 deg
Eccentricity:
0004309
Arg of perigee: 184
0218 deg
Mean anomaly: 176
0900 deg
Mean motion: 15
54145015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 290
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