[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 1st 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
037/00:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
7
040/08:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
5
042/12:24:39
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
6
043/19:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 1726)
---------------------------------------
Vector Time (GMT): 2018/031/14:37:35
785
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -539493
40 A = 6777934
88 meter
Y = -4268978
22 meter E =
0016819
Z = -5251448
91 I = 51
49171
XDOT = 7323
165394 Wp = 89
21638
YDOT = -2039
562629 meter/sec RA = 338
98102 deg
ZDOT = 908
413248 TA = 189
48919
MA = 189
52100
Ha = 222
163 n
mi
Hp = 213
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1769991
45 X = -466208
40
Y = -14005834
06 feet Y = -4274601
39 meter
Z = -17229163
09 Z = -5253891
56
XDOT = 24026
133182 XDOT = 7341
015603
YDOT = -6691
478441 feet/sec YDOT = -1957
570176 meter/sec
ZDOT = 2980
358426 ZDOT = 944
028948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 974093
36 X = 296903
66
Y = -14071166
54 feet Y = -4288891
56 meter
Z = -17239307
77 Z = -5254541
01
XDOT = 23804
960715 XDOT = 7255
752026
YDOT = -2187
091870 feet/sec YDOT = -666
625602 meter/sec
ZDOT = 3139
255010 ZDOT = 956
844927
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 18031
62390151
00016717 00000-0 10270-3 0 9007
2 25544 51
6427 339
5082 0003196 52
5921 307
5522 15
54034170 17271
Satellite: ISS
Catalog Number: 25544
Epoch time: 18031
62390151 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 339
5082 deg
Eccentricity:
0003196
Arg of perigee: 52
5921 deg
Mean anomaly: 307
5522 deg
Mean motion: 15
54034170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1727
Checksum: 282
Coasting Arc #2 (Orbit 1742)
---------------------------------------
Vector Time (GMT): 2018/032/14:37:35
785
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1120345
15 A = 6780109
82 meter
Y = 4730351
10 meter E =
0010974
Z = 4720523
31 I = 51
46832
XDOT = -7094
618604 Wp = 60
15445
YDOT = 1049
183574 meter/sec RA = 333
97495 deg
ZDOT = -2725
050823 TA = 56
90245
MA = 56
79715
Ha = 222
161 n
mi
Hp = 213
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3675673
06 X = -1196087
09
Y = 15519524
60 feet Y = 4717399
22 meter
Z = 15487281
20 Z = 4714897
17
XDOT = -23276
307757 XDOT = -7092
587105
YDOT = 3442
203328 feet/sec YDOT = 969
857989 meter/sec
ZDOT = -8940
455457 ZDOT = -2759
508098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6343483
53 X = -1933493
78
Y = 14660362
61 feet Y = 4468478
52 meter
Z = 15461438
49 Z = 4712646
45
XDOT = -22395
562902 XDOT = -6826
167573
YDOT = -64
472316 feet/sec YDOT = -19
651162 meter/sec
ZDOT = -9094
017221 ZDOT = -2771
856449
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 18032
65280135
00016717 00000-0 10270-3 0 9012
2 25544 51
6422 334
3810 0003141 54
7139 305
4307 15
54055380 17435
Satellite: ISS
Catalog Number: 25544
Epoch time: 18032
65280135 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 334
3810 deg
Eccentricity:
0003141
Arg of perigee: 54
7139 deg
Mean anomaly: 305
4307 deg
Mean motion: 15
54055380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1743
Checksum: 271
Coasting Arc #3 (Orbit 1757)
---------------------------------------
Vector Time (GMT): 2018/033/14:37:35
785
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2584026
27 A = 6783689
69 meter
Y = -5036483
34 meter E =
0008263
Z = -3745006
90 I = 51
45201
XDOT = 6373
901878 Wp = 86
24797
YDOT = 117
132496 meter/sec RA = 328
97380 deg
ZDOT = 4249
065667 TA = 228
88219
MA = 228
95355
Ha = 222
157 n
mi
Hp = 213
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8477776
48 X = 2658344
32
Y = -16523895
46 feet Y = -5007171
62 meter
Z = -12286768
04 Z = -3732274
20
XDOT = 20911
751567 XDOT = 6351
479189
YDOT = 384
292967 feet/sec YDOT = 188
284662 meter/sec
ZDOT = 13940
504158 ZDOT = 4279
972571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10968290
62 X = 3343134
98
Y = -15033910
24 feet Y = -4582335
84 meter
Z = -12229252
95 Z = -3727476
30
XDOT = 19423
214205 XDOT = 5920
195690
YDOT = 2742
063592 feet/sec YDOT = 835
780983 meter/sec
ZDOT = 14078
057185 ZDOT = 4290
991830
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 18033
61739178
00016717 00000-0 10270-3 0 9026
2 25544 51
6431 329
5733 0003063 57
5245 302
6203 15
54043343 17583
Satellite: ISS
Catalog Number: 25544
Epoch time: 18033
61739178 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 329
5733 deg
Eccentricity:
0003063
Arg of perigee: 57
5245 deg
Mean anomaly: 302
6203 deg
Mean motion: 15
54043343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1758
Checksum: 293
Coasting Arc #4 (Orbit 1773)
---------------------------------------
Vector Time (GMT): 2018/034/14:37:35
785
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3810323
88 A = 6787336
27 meter
Y = 5091071
86 meter E =
0016273
Z = 2354478
07 I = 51
43592
XDOT = -5280
223985 Wp = 98
94825
YDOT = -1454
685416 meter/sec RA = 323
98140 deg
ZDOT = -5370
384076 TA = 54
68817
MA = 54
53611
Ha = 222
276 n
mi
Hp = 213
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12501062
60 X = -3878406
98
Y = 16702991
67 feet Y = 5048081
67 meter
Z = 7724665
57 Z = 2335803
59
XDOT = -17323
569505 XDOT = -5237
478976
YDOT = -4772
589946 feet/sec YDOT = -1513
493836 meter/sec
ZDOT = -17619
370328 ZDOT = -5395
929067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14688827
84 X = -4477154
73
Y = 14859167
58 feet Y = 4529074
28 meter
Z = 7640708
76 Z = 2328888
03
XDOT = -15322
866462 XDOT = -4670
409698
YDOT = -5978
855267 feet/sec YDOT = -1822
355085 meter/sec
ZDOT = -17732
828990 ZDOT = -5404
966276
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 18034
64628473
00016717 00000-0 10270-3 0 9036
2 25544 51
6427 324
4456 0003188 63
5564 296
5915 15
54024262 17741
Satellite: ISS
Catalog Number: 25544
Epoch time: 18034
64628473 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 324
4456 deg
Eccentricity:
0003188
Arg of perigee: 63
5564 deg
Mean anomaly: 296
5915 deg
Mean motion: 15
54024262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1774
Checksum: 321
Coasting Arc #5 (Orbit 1788)
---------------------------------------
Vector Time (GMT): 2018/035/14:37:35
785
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4663442
57 A = 6789292
24 meter
Y = -4866600
62 meter E =
0013301
Z = -767970
14 I = 51
41641
XDOT = 3937
248708 Wp = 45
05729
YDOT = 2848
183965 meter/sec RA = 318
99425 deg
ZDOT = 5932
071558 TA = 306
61591
MA = 306
73818
Ha = 222
171 n
mi
Hp = 213
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15300008
43 X = 4721245
94
Y = -15966537
46 feet Y = -4814127
65 meter
Z = -2519587
07 Z = -745176
47
XDOT = 12917
482637 XDOT = 3876
292600
YDOT = 9344
435580 feet/sec YDOT = 2891
872551 meter/sec
ZDOT = 19462
177028 ZDOT = 5951
048738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17089634
76 X = 5208920
67
Y = -14052391
49 feet Y = -4283168
93 meter
Z = -2417348
26 Z = -736807
75
XDOT = 10574
832502 XDOT = 3223
208946
YDOT = 9540
543663 feet/sec YDOT = 2907
957709 meter/sec
ZDOT = 19546
173048 ZDOT = 5957
673545
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 18035
61086700
00016717 00000-0 10270-3 0 9046
2 25544 51
6421 319
6379 0003064 64
2534 295
8935 15
54061142 17891
Satellite: ISS
Catalog Number: 25544
Epoch time: 18035
61086700 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 319
6379 deg
Eccentricity:
0003064
Arg of perigee: 64
2534 deg
Mean anomaly: 295
8935 deg
Mean motion: 15
54061142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1789
Checksum: 311
Coasting Arc #6 (Orbit 1804)
---------------------------------------
Vector Time (GMT): 2018/036/14:37:35
785
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5181013
09 A = 6789248
64 meter
Y = 4279816
71 meter E =
0011096
Z = -942821
03 I = 51
39189
XDOT = -2444
495912 Wp = 126
45066
YDOT = -4246
016480 meter/sec RA = 314
00889 deg
ZDOT = -5896
103749 TA = 63
79093
MA = 63
67689
Ha = 222
179 n
mi
Hp = 213
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16998074
46 X = -5223906
45
Y = 14041393
40 feet Y = 4221639
18 meter
Z = -3093244
85 Z = -968092
63
XDOT = -8019
999711 XDOT = -2368
194422
YDOT = -13930
500264 feet/sec YDOT = -4272
926241 meter/sec
ZDOT = -19344
172404 ZDOT = -5907
792494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18304183
59 X = -5579115
16
Y = 12261291
51 feet Y = 3737241
65 meter
Z = -3206403
16 Z = -977311
68
XDOT = -5556
001194 XDOT = -1693
469164
YDOT = -13320
839767 feet/sec YDOT = -4060
191961 meter/sec
ZDOT = -19395
506426 ZDOT = -5911
750359
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 18036
63975336
00016717 00000-0 10270-3 0 9052
2 25544 51
6422 314
5100 0002926 70
0525 290
0943 15
54015645 18051
Satellite: ISS
Catalog Number: 25544
Epoch time: 18036
63975336 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 314
5100 deg
Eccentricity:
0002926
Arg of perigee: 70
0525 deg
Mean anomaly: 290
0943 deg
Mean motion: 15
54015645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1805
Checksum: 287
Coasting Arc #7 (Orbit 1810)
---------------------------------------
Vector Time (GMT): 2018/037/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4188555
95 A = 6778332
87 meter
Y = -1484768
88 meter E =
0016521
Z = -5133130
61 I = 51
34612
XDOT = 4071
045879 Wp = 78
16740
YDOT = -6308
237428 meter/sec RA = 312
01937 deg
ZDOT = -1498
021750 TA = 177
32632
MA = 177
31748
Ha = 222
133 n
mi
Hp = 213
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13741981
46 X = -4146707
89
Y = -4871288
96 feet Y = -1531374
49 meter
Z = -16840979
70 Z = -5153375
13
XDOT = 13356
449734 XDOT = 4148
560220
YDOT = -20696
317021 feet/sec YDOT = -6262
278875 meter/sec
ZDOT = -4914
769522 ZDOT = -1478
057697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6806019
32 X = 2074474
69
Y = 12775564
21 feet Y = 3893991
97 meter
Z = -16930834
83 Z = -5160518
46
XDOT = -22898
290075 XDOT = -6979
398815
YDOT = 5807
934540 feet/sec YDOT = 1770
258448 meter/sec
ZDOT = -4824
909973 ZDOT = -1470
632560
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 18037
02558326
00016717 00000-0 10270-3 0 9063
2 25544 51
6418 312
5830 0002773 76
9702 283
1760 15
54039890 18111
Satellite: ISS
Catalog Number: 25544
Epoch time: 18037
02558326 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 312
5830 deg
Eccentricity:
0002773
Arg of perigee: 76
9702 deg
Mean anomaly: 283
1760 deg
Mean motion: 15
54039890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1811
Checksum: 308
Coasting Arc #8 (Orbit 1826)
---------------------------------------
Vector Time (GMT): 2018/038/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3099896
91 A = 6777498
46 meter
Y = 2904637
26 meter E =
0005506
Z = 5276404
82 I = 51
32291
XDOT = -4863
337270 Wp = 74
63196
YDOT = 5921
234056 meter/sec RA = 306
99895 deg
ZDOT = -400
609809 TA = 19
21315
MA = 19
19239
Ha = 221
967 n
mi
Hp = 213
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10170265
44 X = 3041556
43
Y = 9529649
80 feet Y = 2938976
46 meter
Z = 17311039
44 Z = 5291321
02
XDOT = -15955
830938 XDOT = -4927
242734
YDOT = 19426
620920 feet/sec YDOT = 5866
491547 meter/sec
ZDOT = -1314
336644 ZDOT = -424
389368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1264692
38 X = -385478
24
Y = -13797194
59 feet Y = -4205384
91 meter
Z = 17376955
60 Z = 5296496
07
XDOT = 23795
520037 XDOT = 7252
874507
YDOT = -3978
326807 feet/sec YDOT = -1212
594011 meter/sec
ZDOT = -1421
101135 ZDOT = -433
151626
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 18038
05446199
00016717 00000-0 10270-3 0 9072
2 25544 51
6420 307
4544 0002847 78
7035 281
4437 15
54096346 18278
Satellite: ISS
Catalog Number: 25544
Epoch time: 18038
05446199 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 307
4544 deg
Eccentricity:
0002847
Arg of perigee: 78
7035 deg
Mean anomaly: 281
4437 deg
Mean motion: 15
54096346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1827
Checksum: 324
Coasting Arc #9 (Orbit 1841)
---------------------------------------
Vector Time (GMT): 2018/039/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1978933
22 A = 6779237
31 meter
Y = -4252885
24 meter E =
0014934
Z = -4908144
51 I = 51
30824
XDOT = 5287
090502 Wp = 101
58398
YDOT = -5058
575013 meter/sec RA = 301
97961 deg
ZDOT = 2254
414359 TA = 190
56264
MA = 190
59404
Ha = 222
163 n
mi
Hp = 213
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6492563
05 X = -1907388
37
Y = -13953035
56 feet Y = -4274615
15 meter
Z = -16102836
30 Z = -4917583
45
XDOT = 17346
097446 XDOT = 5332
313300
YDOT = -16596
374716 feet/sec YDOT = -4999
198214 meter/sec
ZDOT = 7396
372569 ZDOT = 2280
206862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4158042
47 X = -1267371
34
Y = 14772217
32 feet Y = 4502571
84 meter
Z = -16144168
97 Z = -4920742
70
XDOT = -22848
903311 XDOT = -6964
345729
YDOT = 1767
780158 feet/sec YDOT = 538
819392 meter/sec
ZDOT = 7511
947171 ZDOT = 2289
641498
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 18039
01903639
00016717 00000-0 10270-3 0 9087
2 25544 51
6407 302
6475 0003004 82
1056 278
0438 15
54078523 18428
Satellite: ISS
Catalog Number: 25544
Epoch time: 18039
01903639 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 302
6475 deg
Eccentricity:
0003004
Arg of perigee: 82
1056 deg
Mean anomaly: 278
0438 deg
Mean motion: 15
54078523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1842
Checksum: 299
Coasting Arc #10 (Orbit 1857)
---------------------------------------
Vector Time (GMT): 2018/040/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 861085
89 A = 6782573
92 meter
Y = 5393749
03 meter E =
0013682
Z = 4011299
70 I = 51
30365
XDOT = -5424
133959 Wp = 79
38006
YDOT = 3775
240425 meter/sec RA = 296
96488 deg
ZDOT = -3898
134451 TA = 51
29535
MA = 51
17308
Ha = 222
067 n
mi
Hp = 213
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2825084
96 X = 781223
04
Y = 17696027
01 feet Y = 5402931
83 meter
Z = 13160432
09 Z = 4015288
41
XDOT = -17795
715089 XDOT = -5447
011779
YDOT = 12385
959400 feet/sec YDOT = 3714
456037 meter/sec
ZDOT = -12789
155022 ZDOT = -3924
538278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9097149
11 X = 2772811
05
Y = -15424883
64 feet Y = -4701504
53 meter
Z = 13177340
12 Z = 4016453
27
XDOT = 20424
285221 XDOT = 6225
322135
YDOT = 980
403501 feet/sec YDOT = 298
826987 meter/sec
ZDOT = -12907
240595 ZDOT = -3934
126933
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 18040
04791095
00016717 00000-0 10270-3 0 9094
2 25544 51
6414 297
5188 0002874 83
8829 276
2651 15
54096562 18586
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
04791095 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 297
5188 deg
Eccentricity:
0002874
Arg of perigee: 83
8829 deg
Mean anomaly: 276
2651 deg
Mean motion: 15
54096562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1858
Checksum: 344
Coasting Arc #11 (Orbit 1862)
---------------------------------------
Vector Time (GMT): 2018/040/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4458340
94 A = 6778310
04 meter
Y = -167613
20 meter E =
0016737
Z = -5118030
88 I = 51
28253
XDOT = 2040
689437 Wp = 78
48267
YDOT = -7215
666274 meter/sec RA = 295
28234 deg
ZDOT = -1542
366377 TA = 176
55908
MA = 176
54756
Ha = 222
207 n
mi
Hp = 213
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14627102
83 X = -4431274
97
Y = -549912
07 feet Y = -217318
19 meter
Z = -16791439
89 Z = -5139621
89
XDOT = 6695
175317 XDOT = 2128
717191
YDOT = -23673
445780 feet/sec YDOT = -7192
353720 meter/sec
ZDOT = -5060
257142 ZDOT = -1532
239627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1874087
67 X = 571221
92
Y = -14405115
41 feet Y = -4390679
18 meter
Z = -16887493
59 Z = -5147308
05
XDOT = 21910
364758 XDOT = 6678
279178
YDOT = 8724
730371 feet/sec YDOT = 2659
297817 meter/sec
ZDOT = -5014
071643 ZDOT = -1528
289037
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 18040
36943557
00016717 00000-0 10270-3 0 9103
2 25544 51
6398 295
9170 0003080 80
0608 280
0892 15
54067631 18635
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
36943557 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 295
9170 deg
Eccentricity:
0003080
Arg of perigee: 80
0608 deg
Mean anomaly: 280
0892 deg
Mean motion: 15
54067631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1863
Checksum: 312
Coasting Arc #12 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2018/041/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3828101
48 A = 6777520
35 meter
Y = 1846551
27 meter E =
0005685
Z = 5274515
98 I = 51
26698
XDOT = -2921
900662 Wp = 77
27412
YDOT = 7085
929207 meter/sec RA = 290
25882 deg
ZDOT = -358
511667 TA = 16
16879
MA = 16
15066
Ha = 222
052 n
mi
Hp = 213
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12559388
07 X = 3781547
96
Y = 6058239
08 feet Y = 1889099
51 meter
Z = 17304842
46 Z = 5292998
16
XDOT = -9586
288262 XDOT = -2999
178848
YDOT = 23247
799235 feet/sec YDOT = 7052
822415 meter/sec
ZDOT = -1176
219380 ZDOT = -372
892798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6965675
63 X = -2123137
93
Y = 11961455
43 feet Y = 3645851
61 meter
Z = 17386805
60 Z = 5299498
35
XDOT = -21601
307874 XDOT = -6584
078640
YDOT = -10767
659357 feet/sec YDOT = -3281
982572 meter/sec
ZDOT = -1241
303683 ZDOT = -378
349363
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 18041
39830619
00016717 00000-0 10270-3 0 9112
2 25544 51
6398 290
7894 0003088 81
2699 278
8803 15
54083926 18791
Satellite: ISS
Catalog Number: 25544
Epoch time: 18041
39830619 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 290
7894 deg
Eccentricity:
0003088
Arg of perigee: 81
2699 deg
Mean anomaly: 278
8803 deg
Mean motion: 15
54083926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 357
Coasting Arc #13 (Orbit 1893)
---------------------------------------
Vector Time (GMT): 2018/042/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3143485
41 A = 6779183
63 meter
Y = -3469401
53 meter E =
0015208
Z = -4917005
80 I = 51
26154
XDOT = 3585
780059 Wp = 102
06131
YDOT = -6390
483996 meter/sec RA = 285
23479 deg
ZDOT = 2219
379364 TA = 189
73963
MA = 189
76914
Ha = 222
214 n
mi
Hp = 213
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10313272
34 X = -3080572
24
Y = -11382550
94 feet Y = -3504202
44 meter
Z = -16131908
78 Z = -4932122
60
XDOT = 11764
370271 XDOT = 3646
193316
YDOT = -20966
154844 feet/sec YDOT = -6350
047520 meter/sec
ZDOT = 7281
428358 ZDOT = 2236
944321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11946921
76 X = 3641421
75
Y = -9541443
04 feet Y = -2908231
84 meter
Z = -16198656
07 Z = -4937350
37
XDOT = 19568
170319 XDOT = 5964
378313
YDOT = 12020
441311 feet/sec YDOT = 3663
830512 meter/sec
ZDOT = 7360
561902 ZDOT = 2243
499268
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 18042
36287167
00016717 00000-0 10270-3 0 9125
2 25544 51
6394 285
9815 0003113 85
5851 274
5658 15
54073477 18940
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
36287167 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 285
9815 deg
Eccentricity:
0003113
Arg of perigee: 85
5851 deg
Mean anomaly: 274
5658 deg
Mean motion: 15
54073477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1894
Checksum: 339
Coasting Arc #14 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2018/042/12:24:39
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1074524
00 A = 6785250
23 meter
Y = 5914370
84 meter E =
0015980
Z = 3132547
57 I = 51
28246
XDOT = -4873
391875 Wp = 92
52339
YDOT = 3448
591114 meter/sec RA = 284
39590 deg
ZDOT = -4818
764360 TA = 51
15635
MA = 51
01384
Ha = 222
153 n
mi
Hp = 213
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3525341
20 X = 993092
08
Y = 19404103
79 feet Y = 5925931
63 meter
Z = 10277387
03 Z = 3137569
26
XDOT = -15988
818488 XDOT = -4888
186209
YDOT = 11314
275308 feet/sec YDOT = 3394
010709 meter/sec
ZDOT = -15809
594356 ZDOT = -4842
473116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7729113
52 X = -2355833
80
Y = 18131922
58 feet Y = 5526610
00 meter
Z = 10298841
99 Z = 3139087
04
XDOT = -18163
566763 XDOT = -5536
255149
YDOT = 1335
778188 feet/sec YDOT = 407
145192 meter/sec
ZDOT = -15915
622792 ZDOT = -4851
081827
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 18042
55578354
00016717 00000-0 10270-3 0 9138
2 25544 51
6413 285
0215 0003095 84
5062 275
6443 15
54094387 18979
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
55578354 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 285
0215 deg
Eccentricity:
0003095
Arg of perigee: 84
5062 deg
Mean anomaly: 275
6443 deg
Mean motion: 15
54094387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 321
Coasting Arc #15 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2018/043/12:24:39
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -249776
49 A = 6788308
10 meter
Y = -6578191
70 meter E =
0009975
Z = -1647061
75 I = 51
28540
XDOT = 4884
898655 Wp = 50
67463
YDOT = -1601
856306 meter/sec RA = 279
39487 deg
ZDOT = 5686
211786 TA = 291
20157
MA = 291
30811
Ha = 222
128 n
mi
Hp = 213
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -819476
69 X = -168198
43
Y = -21581993
78 feet Y = -6580528
78 meter
Z = -5403745
88 Z = -1648076
77
XDOT = 16026
570392 XDOT = 4874
827998
YDOT = -5255
434076 feet/sec YDOT = -1547
286204 meter/sec
ZDOT = 18655
550480 ZDOT = 5709
915969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10838877
06 X = 3303689
73
Y = -18679787
45 feet Y = -5693599
21 meter
Z = -5407286
93 Z = -1648141
06
XDOT = 14894
395000 XDOT = 4539
811596
YDOT = 3239
405426 feet/sec YDOT = 987
370774 meter/sec
ZDOT = 18761
279379 ZDOT = 5718
437955
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 18043
52034547
00016717 00000-0 10270-3 0 9148
2 25544 51
6413 280
2135 0002916 87
4675 272
6811 15
54081742 19125
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
52034547 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 280
2135 deg
Eccentricity:
0002916
Arg of perigee: 87
4675 deg
Mean anomaly: 272
6811 deg
Mean motion: 15
54081742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1912
Checksum: 297
Coasting Arc #16 (Orbit 1916)
---------------------------------------
Vector Time (GMT): 2018/043/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3616303
32 A = 6778989
77 meter
Y = 2867972
64 meter E =
0008721
Z = 4958779
15 I = 51
25152
XDOT = -2639
490203 Wp = 71
18496
YDOT = 6903
614758 meter/sec RA = 277
98455 deg
ZDOT = -2062
134511 TA = 39
00294
MA = 38
94007
Ha = 222
149 n
mi
Hp = 213
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11864512
22 X = 3559877
53
Y = 9409359
05 feet Y = 2908097
25 meter
Z = 16268960
47 Z = 4976208
38
XDOT = -8659
744761 XDOT = -2706
475590
YDOT = 22649
654718 feet/sec YDOT = 6873
723579 meter/sec
ZDOT = -6765
533171 ZDOT = -2075
118800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13010951
02 X = 3965737
87
Y = -7582995
06 feet Y = -2311296
90 meter
Z = 16346103
57 Z = 4982292
37
XDOT = 17478
899113 XDOT = 5327
568450
YDOT = 15239
213628 feet/sec YDOT = 4644
912314 meter/sec
ZDOT = -6824
337300 ZDOT = -2080
058009
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 18043
84186768
00016717 00000-0 10270-3 0 9157
2 25544 51
6403 278
6054 0003198 99
8326 260
3188 15
54056196 19179
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
84186768 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 278
6054 deg
Eccentricity:
0003198
Arg of perigee: 99
8326 deg
Mean anomaly: 260
3188 deg
Mean motion: 15
54056196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1917
Checksum: 340
Coasting Arc #17 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2018/044/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3100275
65 A = 6782136
81 meter
Y = -4395349
55 meter E =
0010773
Z = -4142350
84 I = 51
25847
XDOT = 3292
971639 Wp = 107
43847
YDOT = -5826
713058 meter/sec RA = 272
96639 deg
ZDOT = 3722
885450 TA = 201
09171
MA = 201
13617
Ha = 222
175 n
mi
Hp = 213
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10171508
05 X = -3030774
40
Y = -14420438
14 feet Y = -4429630
50 meter
Z = -13590389
89 Z = -4157241
56
XDOT = 10803
712728 XDOT = 3339
799421
YDOT = -19116
512657 feet/sec YDOT = -5789
626821 meter/sec
ZDOT = 12214
191110 ZDOT = 3738
995112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17008233
92 X = -5184109
70
Y = 4510018
80 feet Y = 1374653
73 meter
Z = -13656025
00 Z = -4162356
42
XDOT = -13935
911000 XDOT = -4247
665673
YDOT = -15400
046836 feet/sec YDOT = -4693
934276 meter/sec
ZDOT = 12286
731715 ZDOT = 3744
995827
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 18044
80642533
00016717 00000-0 10270-3 0 9162
2 25544 51
6400 273
7984 0003085 102
4731 257
6767 15
54080375 19325
Satellite: ISS
Catalog Number: 25544
Epoch time: 18044
80642533 = yrday
fracday
Element set: 916
Inclination: 51
6400 deg
RA of node: 273
7984 deg
Eccentricity:
0003085
Arg of perigee: 102
4731 deg
Mean anomaly: 257
6767 deg
Mean motion: 15
54080375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1932
Checksum: 311
Coasting Arc #18 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2018/045/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2500197
04 A = 6785975
50 meter
Y = 5610731
00 meter E =
0016455
Z = 2866011
53 I = 51
26975
XDOT = -3880
029299 Wp = 100
55611
YDOT = 4307
490310 meter/sec RA = 267
95706 deg
ZDOT = -5026
217863 TA = 46
62334
MA = 46
48640
Ha = 222
169 n
mi
Hp = 213
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8202746
21 X = 2423349
30
Y = 18407910
09 feet Y = 5638260
39 meter
Z = 9402924
96 Z = 2877969
36
XDOT = -12729
754918 XDOT = -3903
494368
YDOT = 14132
186056 feet/sec YDOT = 4263
969691 meter/sec
ZDOT = -16490
216087 ZDOT = -5045
122430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20059548
06 X = 6114150
25
Y = -1661954
30 feet Y = -506563
67 meter
Z = 9455349
63 Z = 2881990
57
XDOT = 9096
417428 XDOT = 2772
588032
YDOT = 15090
142429 feet/sec YDOT = 4599
475412 meter/sec
ZDOT = -16574
965983 ZDOT = -5052
049631
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 18045
83528664
00016717 00000-0 10270-3 0 9175
2 25544 51
6393 268
6698 0003183 108
0226 252
1274 15
54071020 19488
Satellite: ISS
Catalog Number: 25544
Epoch time: 18045
83528664 = yrday
fracday
Element set: 917
Inclination: 51
6393 deg
RA of node: 268
6698 deg
Eccentricity:
0003183
Arg of perigee: 108
0226 deg
Mean anomaly: 252
1274 deg
Mean motion: 15
54071020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1948
Checksum: 317
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