[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 20th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21814 1409 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
325/21:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
2
331/13:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
9
337/11:31:54
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
0
337/17:35:42
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
1
337/18:00:00
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
1
Coasting Arc #1 (Orbit 2265)
---------------------------------------
Vector Time (GMT): 2018/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1062665
06 A = 6778604
64 meter
Y = -4301519
11 meter E =
0018021
Z = -5145693
24 I = 51
40043
XDOT = 6698
252212 Wp = 90
43436
YDOT = -3403
197040 meter/sec RA = 324
10561 deg
ZDOT = 1465
921449 TA = 193
72503
MA = 193
77409
Ha = 223
060 n
mi
Hp = 213
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3486433
93 X = -989489
70
Y = -14112595
50 feet Y = -4312993
42 meter
Z = -16882195
68 Z = -5150677
68
XDOT = 21975
893085 XDOT = 6728
689057
YDOT = -11165
344620 feet/sec YDOT = -3328
122346 meter/sec
ZDOT = 4809
453573 ZDOT = 1498
533852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13723550
73 X = 4182938
26
Y = 4716786
62 feet Y = 1437676
56 meter
Z = -16903999
05 Z = -5152338
91
XDOT = -1992
183554 XDOT = -607
217547
YDOT = 23508
667487 feet/sec YDOT = 7165
441850 meter/sec
ZDOT = 4956
530074 ZDOT = 1510
750367
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 18323
51349617
00016717 00000-0 10270-3 0 9000
2 25544 51
6389 324
6857 0005219 61
9526 298
2153 15
53959795 22669
Satellite: ISS
Catalog Number: 25544
Epoch time: 18323
51349617 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 324
6857 deg
Eccentricity:
0005219
Arg of perigee: 61
9526 deg
Mean anomaly: 298
2153 deg
Mean motion: 15
53959795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2266
Checksum: 343
Coasting Arc #2 (Orbit 2281)
---------------------------------------
Vector Time (GMT): 2018/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -407633
30 A = 6781226
76 meter
Y = 5076631
23 meter E =
0014222
Z = 4469073
55 I = 51
38193
XDOT = -6577
058263 Wp = 66
85619
YDOT = 2307
894207 meter/sec RA = 319
09412 deg
ZDOT = -3207
918351 TA = 55
56103
MA = 55
42671
Ha = 222
998 n
mi
Hp = 213
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1337379
60 X = -486080
25
Y = 16655614
28 feet Y = 5071634
11 meter
Z = 14662314
80 Z = 4466902
89
XDOT = -21578
275141 XDOT = -6586
794200
YDOT = 7571
831387 feet/sec YDOT = 2234
290579 meter/sec
ZDOT = -10524
666505 ZDOT = -3239
891817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13465101
20 X = -4104162
84
Y = -9909382
36 feet Y = -3020379
74 meter
Z = 14651851
00 Z = 4465884
18
XDOT = 4031
170992 XDOT = 1228
700918
YDOT = -21318
412435 feet/sec YDOT = -6497
852110 meter/sec
ZDOT = -10668
706663 ZDOT = -3251
821791
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 18324
54242388
00016717 00000-0 10270-3 0 9012
2 25544 51
6375 319
5570 0005141 64
6272 295
5412 15
54002170 22824
Satellite: ISS
Catalog Number: 25544
Epoch time: 18324
54242388 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 319
5570 deg
Eccentricity:
0005141
Arg of perigee: 64
6272 deg
Mean anomaly: 295
5412 deg
Mean motion: 15
54002170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2282
Checksum: 290
Coasting Arc #3 (Orbit 2296)
---------------------------------------
Vector Time (GMT): 2018/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1688411
88 A = 6784928
39 meter
Y = -5634391
03 meter E =
0009996
Z = -3388260
13 I = 51
37025
XDOT = 6046
845598 Wp = 77
58858
YDOT = -950
368546 meter/sec RA = 314
09058 deg
ZDOT = 4607
239462 TA = 242
69724
MA = 242
79906
Ha = 223
133 n
mi
Hp = 213
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5539409
04 X = 1767750
55
Y = -18485534
88 feet Y = -5615066
31 meter
Z = -11116339
01 Z = -3379865
68
XDOT = 19838
732277 XDOT = 6034
643327
YDOT = -3118
007041 feet/sec YDOT = -882
816908 meter/sec
ZDOT = 15115
615033 ZDOT = 4636
584060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13094062
69 X = 3991070
31
Y = 14205643
00 feet Y = 4329879
99 meter
Z = -11077828
06 Z = -3376521
99
XDOT = -6276
940985 XDOT = -1913
211612
YDOT = 17641
158750 feet/sec YDOT = 5377
025187 meter/sec
ZDOT = 15247
642734 ZDOT = 4647
481505
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 18325
50704181
00016717 00000-0 10270-3 0 9024
2 25544 51
6381 314
7498 0005348 68
6628 291
5095 15
53979840 22970
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
50704181 = yrday
fracday
Element set: 902
Inclination: 51
6381 deg
RA of node: 314
7498 deg
Eccentricity:
0005348
Arg of perigee: 68
6628 deg
Mean anomaly: 291
5095 deg
Mean motion: 15
53979840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2297
Checksum: 338
Coasting Arc #4 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2018/325/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4231153
40 A = 6778621
61 meter
Y = 1402071
02 meter E =
0008735
Z = 5099617
98 I = 51
34113
XDOT = -4018
700661 Wp = 95
16331
YDOT = 6342
648949 meter/sec RA = 312
09497 deg
ZDOT = 1587
369357 TA = 339
45963
MA = 339
49473
Ha = 222
921 n
mi
Hp = 213
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13881736
87 X = 4190388
65
Y = 4599970
55 feet Y = 1449158
56 meter
Z = 16731030
13 Z = 5120073
07
XDOT = -13184
713455 XDOT = -4097
038067
YDOT = 20809
215712 feet/sec YDOT = 6297
270963 meter/sec
ZDOT = 5207
904716 ZDOT = 1567
657382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14386383
82 X = 4384969
79
Y = -1953433
81 feet Y = -595406
62 meter
Z = 16822775
45 Z = 5127581
96
XDOT = -2811
783312 XDOT = -857
031553
YDOT = 23459
268152 feet/sec YDOT = 7150
384933 meter/sec
ZDOT = 5118
429415 ZDOT = 1560
097286
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 18325
95719547
00016717 00000-0 10270-3 0 9036
2 25544 51
6393 312
5049 0005122 67
8290 292
3405 15
53966146 23045
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
95719547 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 312
5049 deg
Eccentricity:
0005122
Arg of perigee: 67
8290 deg
Mean anomaly: 292
3405 deg
Mean motion: 15
53966146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 315
Coasting Arc #5 (Orbit 2318)
---------------------------------------
Vector Time (GMT): 2018/326/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3185810
47 A = 6777759
86 meter
Y = -2816490
36 meter E =
0019704
Z = -5294933
60 I = 51
31522
XDOT = 4792
964073 Wp = 87
01462
YDOT = -5960
217729 meter/sec RA = 307
07391 deg
ZDOT = 288
518745 TA = 185
74206
MA = 185
76468
Ha = 223
024 n
mi
Hp = 212
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10452134
08 X = -3128358
21
Y = -9240453
94 feet Y = -2851794
70 meter
Z = -17371829
40 Z = -5310270
24
XDOT = 15724
947747 XDOT = 4857
855157
YDOT = -19554
520109 feet/sec YDOT = -5906
256667 meter/sec
ZDOT = 946
583808 ZDOT = 311
959134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13417267
14 X = -4089583
02
Y = -3496259
79 feet Y = -1065659
98 meter
Z = -17440374
50 Z = -5315826
15
XDOT = 4788
962028 XDOT = 1459
675626
YDOT = -23598
006821 feet/sec YDOT = -7192
672479 meter/sec
ZDOT = 1052
757894 ZDOT = 320
880606
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 18326
92180727
00016717 00000-0 10270-3 0 9047
2 25544 51
6375 307
6960 0005124 72
2546 287
9165 15
54003589 23191
Satellite: ISS
Catalog Number: 25544
Epoch time: 18326
92180727 = yrday
fracday
Element set: 904
Inclination: 51
6375 deg
RA of node: 307
6960 deg
Eccentricity:
0005124
Arg of perigee: 72
2546 deg
Mean anomaly: 287
9165 deg
Mean motion: 15
54003589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2319
Checksum: 322
Coasting Arc #6 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2018/327/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2062091
96 A = 6779315
22 meter
Y = 4156630
54 meter E =
0011161
Z = 4935343
17 I = 51
30177
XDOT = -5257
899635 Wp = 65
32747
YDOT = 5162
531748 meter/sec RA = 302
05361 deg
ZDOT = -2142
705786 TA = 45
68148
MA = 45
59004
Ha = 222
932 n
mi
Hp = 213
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6765393
58 X = 1991484
21
Y = 13637239
31 feet Y = 4179295
04 meter
Z = 16192070
78 Z = 4945189
24
XDOT = -17250
326887 XDOT = -5304
829335
YDOT = 16937
440117 feet/sec YDOT = 5103
472059 meter/sec
ZDOT = -7029
874626 ZDOT = -2168
360987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12309051
38 X = 3751798
86
Y = 8877804
92 feet Y = 2705954
94 meter
Z = 16235757
96 Z = 4948659
03
XDOT = -6517
998326 XDOT = -1986
685890
YDOT = 22155
899988 feet/sec YDOT = 6753
118316 meter/sec
ZDOT = -7145
889711 ZDOT = -2178
067184
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 18327
95072502
00016717 00000-0 10270-3 0 9053
2 25544 51
6381 302
5677 0004957 76
1237 284
0467 15
53992818 23352
Satellite: ISS
Catalog Number: 25544
Epoch time: 18327
95072502 = yrday
fracday
Element set: 905
Inclination: 51
6381 deg
RA of node: 302
5677 deg
Eccentricity:
0004957
Arg of perigee: 76
1237 deg
Mean anomaly: 284
0467 deg
Mean motion: 15
53992818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 329
Coasting Arc #7 (Orbit 2349)
---------------------------------------
Vector Time (GMT): 2018/328/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -995892
53 A = 6782473
41 meter
Y = -5306066
44 meter E =
0012219
Z = -4117227
25 I = 51
29561
XDOT = 5390
482212 Wp = 97
40474
YDOT = -3926
556730 meter/sec RA = 297
03737 deg
ZDOT = 3764
561816 TA = 211
60258
MA = 211
67600
Ha = 223
022 n
mi
Hp = 212
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3267363
94 X = -916484
87
Y = -17408354
45 feet Y = -5316758
76 meter
Z = -13507963
43 Z = -4121872
75
XDOT = 17685
309094 XDOT = 5415
702806
YDOT = -12882
403970 feet/sec YDOT = -3866
136002 meter/sec
ZDOT = 12350
924592 ZDOT = 3790
808281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11258847
51 X = -3431696
72
Y = -13653559
85 feet Y = -4161605
04 meter
Z = -13528126
40 Z = -4123372
93
XDOT = 8097
403231 XDOT = 2468
088505
YDOT = -19005
789626 feet/sec YDOT = -5792
964678 meter/sec
ZDOT = 12469
426833 ZDOT = 3800
681299
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 18328
91533230
00016717 00000-0 10270-3 0 9061
2 25544 51
6379 297
7587 0005087 80
5860 279
5867 15
54011662 23500
Satellite: ISS
Catalog Number: 25544
Epoch time: 18328
91533230 = yrday
fracday
Element set: 906
Inclination: 51
6379 deg
RA of node: 297
7587 deg
Eccentricity:
0005087
Arg of perigee: 80
5860 deg
Mean anomaly: 279
5867 deg
Mean motion: 15
54011662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2350
Checksum: 335
Coasting Arc #8 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2018/329/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -28769
12 A = 6786178
97 meter
Y = 6152003
16 meter E =
0018162
Z = 2846539
77 I = 51
29403
XDOT = -5297
365324 Wp = 94
72716
YDOT = 2320
324990 meter/sec RA = 292
03097 deg
ZDOT = -5041
901000 TA = 52
71761
MA = 52
55215
Ha = 222
947 n
mi
Hp = 213
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -94386
86 X = -111387
59
Y = 20183737
39 feet Y = 6151219
17 meter
Z = 9339041
24 Z = 2846200
05
XDOT = -17379
807492 XDOT = -5298
426878
YDOT = 7612
614796 feet/sec YDOT = 2261
080809 meter/sec
ZDOT = -16541
669948 ZDOT = -5067
636463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10003124
74 X = 3048952
42
Y = 17532071
08 feet Y = 5343775
27 meter
Z = 9336692
89 Z = 2845823
99
XDOT = -9831
023459 XDOT = -2996
495950
YDOT = 14526
321870 feet/sec YDOT = 4427
622906 meter/sec
ZDOT = -16657
659190 ZDOT = -5077
254521
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 18329
94424146
00016717 00000-0 10270-3 0 9071
2 25544 51
6379 292
6302 0004961 82
9969 277
1748 15
54031704 23663
Satellite: ISS
Catalog Number: 25544
Epoch time: 18329
94424146 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 292
6302 deg
Eccentricity:
0004961
Arg of perigee: 82
9969 deg
Mean anomaly: 277
1748 deg
Mean motion: 15
54031704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 338
Coasting Arc #9 (Orbit 2380)
---------------------------------------
Vector Time (GMT): 2018/330/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 897323
50 A = 6788904
19 meter
Y = -6591900
07 meter E =
0012692
Z = -1338789
92 I = 51
29086
XDOT = 5001
158444 Wp = 56
19413
YDOT = -485
532430 meter/sec RA = 287
03275 deg
ZDOT = 5789
242413 TA = 289
16127
MA = 289
29862
Ha = 223
074 n
mi
Hp = 212
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2943974
74 X = 977472
47
Y = -21626968
73 feet Y = -6581417
29 meter
Z = -4392355
38 Z = -1334237
03
XDOT = 16408
000145 XDOT = 4978
094758
YDOT = -1592
954167 feet/sec YDOT = -429
735585 meter/sec
ZDOT = 18993
577471 ZDOT = 5813
480468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8638530
68 X = -2633024
15
Y = -20048827
63 feet Y = -6110882
66 meter
Z = -4371023
64 Z = -1332288
01
XDOT = 11650
494135 XDOT = 3551
070612
YDOT = -9151
159156 feet/sec YDOT = -2789
273311 meter/sec
ZDOT = 19102
595325 ZDOT = 5822
471055
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 18330
90884432
00016717 00000-0 10270-3 0 9088
2 25544 51
6372 287
8227 0005189 89
1503 271
0244 15
54013890 23811
Satellite: ISS
Catalog Number: 25544
Epoch time: 18330
90884432 = yrday
fracday
Element set: 908
Inclination: 51
6372 deg
RA of node: 287
8227 deg
Eccentricity:
0005189
Arg of perigee: 89
1503 deg
Mean anomaly: 271
0244 deg
Mean motion: 15
54013890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2381
Checksum: 313
Coasting Arc #10 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2018/331/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1681518
02 A = 6789633
59 meter
Y = -6571379
96 meter E =
0016493
Z = 79561
94 I = 51
28950
XDOT = 4626
602849 Wp = 58
17611
YDOT = 1267
300513 meter/sec RA = 283
81454 deg
ZDOT = 5983
362656 TA = 302
68511
MA = 302
84407
Ha = 223
037 n
mi
Hp = 212
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5516791
40 X = 1754489
58
Y = -21559645
53 feet Y = -6552168
05 meter
Z = 261029
99 Z = 87906
81
XDOT = 15179
143206 XDOT = 4583
023471
YDOT = 4157
810081 feet/sec YDOT = 1318
794141 meter/sec
ZDOT = 19630
454909 ZDOT = 6005
731518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20901830
25 X = 6370877
86
Y = 7638409
14 feet Y = 2328187
11 meter
Z = 299395
24 Z = 91255
67
XDOT = -5082
866817 XDOT = -1549
257806
YDOT = 13033
772985 feet/sec YDOT = 3972
694006 meter/sec
ZDOT = 19730
845428 ZDOT = 6013
961687
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 18331
61621708
00016717 00000-0 10270-3 0 9093
2 25544 51
6393 284
3007 0005139 88
0431 272
1310 15
54023252 23926
Satellite: ISS
Catalog Number: 25544
Epoch time: 18331
61621708 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 284
3007 deg
Eccentricity:
0005139
Arg of perigee: 88
0431 deg
Mean anomaly: 272
1310 deg
Mean motion: 15
54023252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 283
Coasting Arc #11 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2018/332/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2375294
54 A = 6788280
66 meter
Y = 6109231
20 meter E =
0011392
Z = -1759352
15 I = 51
27913
XDOT = -4081
079731 Wp = 120
71698
YDOT = -3202
138151 meter/sec RA = 278
81923 deg
ZDOT = -5642
378084 TA = 78
68926
MA = 78
56128
Ha = 223
025 n
mi
Hp = 212
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7792961
10 X = -2434887
10
Y = 20043409
44 feet Y = 6082335
94 meter
Z = -5772152
71 Z = -1771034
81
XDOT = -13389
369195 XDOT = -4017
561405
YDOT = -10505
702595 feet/sec YDOT = -3247
420025 meter/sec
ZDOT = -18511
739121 ZDOT = -5662
048612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19333605
23 X = -5892882
87
Y = -9384141
65 feet Y = -2860286
37 meter
Z = -5825448
12 Z = -1775596
59
XDOT = 10883
120587 XDOT = 3317
175155
YDOT = -10942
218879 feet/sec YDOT = -3335
188314 meter/sec
ZDOT = -18599
761399 ZDOT = -5669
207274
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 18332
58081217
00016717 00000-0 10270-3 0 9107
2 25544 51
6402 279
4926 0005164 90
1575 270
0169 15
54027607 24077
Satellite: ISS
Catalog Number: 25544
Epoch time: 18332
58081217 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 279
4926 deg
Eccentricity:
0005164
Arg of perigee: 90
1575 deg
Mean anomaly: 270
0169 deg
Mean motion: 15
54027607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 298
Coasting Arc #12 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2018/333/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2928068
67 A = 6785196
80 meter
Y = -5201596
40 meter E =
0017945
Z = 3210239
32 I = 51
26391
XDOT = 3491
467644 Wp = 88
85100
YDOT = 4911
234463 meter/sec RA = 273
81801 deg
ZDOT = 4750
451821 TA = 308
53783
MA = 308
69854
Ha = 223
002 n
mi
Hp = 212
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9606524
51 X = 2970423
04
Y = -17065604
97 feet Y = -5168616
06 meter
Z = 10532281
25 Z = 3224565
50
XDOT = 11454
946337 XDOT = 3413
214072
YDOT = 16112
973960 feet/sec YDOT = 4949
840671 meter/sec
ZDOT = 15585
471853 ZDOT = 4767
222439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16403717
24 X = 4999853
01
Y = 10633142
88 feet Y = 3240981
95 meter
Z = 10597333
06 Z = 3230067
12
XDOT = -16047
477383 XDOT = -4891
271106
YDOT = 9075
065629 feet/sec YDOT = 2766
080004 meter/sec
ZDOT = 15660
256982 ZDOT = 4773
246328
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 18333
60971042
00016717 00000-0 10270-3 0 9116
2 25544 51
6393 274
3650 0005204 93
9665 266
2082 15
54028352 24237
Satellite: ISS
Catalog Number: 25544
Epoch time: 18333
60971042 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 274
3650 deg
Eccentricity:
0005204
Arg of perigee: 93
9665 deg
Mean anomaly: 266
2082 deg
Mean motion: 15
54028352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 297
Coasting Arc #13 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/334/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3438600
59 A = 6781332
64 meter
Y = 3880282
75 meter E =
0013813
Z = -4384339
00 I = 51
25084
XDOT = -2821
363369 Wp = 79
41897
YDOT = -6279
866006 meter/sec RA = 268
80618 deg
ZDOT = -3351
661720 TA = 156
46977
MA = 156
40651
Ha = 222
987 n
mi
Hp = 212
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11281498
01 X = -3460438
50
Y = 12730586
46 feet Y = 3841708
00 meter
Z = -14384314
32 Z = -4401095
52
XDOT = -9256
441498 XDOT = -2734
649758
YDOT = -20603
234927 feet/sec YDOT = -6310
931476 meter/sec
ZDOT = -10996
265485 ZDOT = -3365
156639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12174275
28 X = -3710719
10
Y = -11787301
74 feet Y = -3592769
57 meter
Z = -14460119
87 Z = -4407444
54
XDOT = 20164
089278 XDOT = 6146
014412
YDOT = -7289
080526 feet/sec YDOT = -2221
711744 meter/sec
ZDOT = -11056
172790 ZDOT = -3369
921466
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 18334
57429968
00016717 00000-0 10270-3 0 9129
2 25544 51
6400 269
5571 0005174 97
0787 263
0954 15
54052984 24387
Satellite: ISS
Catalog Number: 25544
Epoch time: 18334
57429968 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 269
5571 deg
Eccentricity:
0005174
Arg of perigee: 97
0787 deg
Mean anomaly: 263
0954 deg
Mean motion: 15
54052984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 340
Coasting Arc #14 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2018/335/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3851318
82 A = 6778423
48 meter
Y = -2292197
54 meter E =
0009896
Z = 5078383
05 I = 51
24317
XDOT = 2108
839881 Wp = 113
50018
YDOT = 7193
956750 meter/sec RA = 263
78522 deg
ZDOT = 1641
367487 TA = 320
54523
MA = 320
61725
Ha = 222
784 n
mi
Hp = 212
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12635560
42 X = 3851996
23
Y = -7520333
14 feet Y = -2249125
79 meter
Z = 16661361
70 Z = 5097093
17
XDOT = 6918
766014 XDOT = 2020
265338
YDOT = 23602
220307 feet/sec YDOT = 7217
043961 meter/sec
ZDOT = 5385
063935 ZDOT = 1651
396686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7125664
98 X = 2171902
68
Y = 12752191
48 feet Y = 3886867
96 meter
Z = 16745754
16 Z = 5104105
87
XDOT = -22875
491191 XDOT = -6972
449715
YDOT = 5625
215830 feet/sec YDOT = 1714
565785 meter/sec
ZDOT = 5429
297514 ZDOT = 1654
849882
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 18335
60318994
00016717 00000-0 10270-3 0 9131
2 25544 51
6401 264
4289 0005036 102
0042 258
1675 15
54069866 24546
Satellite: ISS
Catalog Number: 25544
Epoch time: 18335
60318994 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 264
4289 deg
Eccentricity:
0005036
Arg of perigee: 102
0042 deg
Mean anomaly: 258
1675 deg
Mean motion: 15
54069866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 311
Coasting Arc #15 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2018/336/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4222005
34 A = 6777582
30 meter
Y = 544983
11 meter E =
0019908
Z = -5291141
82 I = 51
24569
XDOT = -1291
459068 Wp = 95
00345
YDOT = -7539
645928 meter/sec RA = 258
75856 deg
ZDOT = 253
049566 TA = 177
43157
MA = 177
42133
Ha = 222
964 n
mi
Hp = 212
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13851723
55 X = -4202083
79
Y = 1788002
34 feet Y = 497881
28 meter
Z = -17359389
18 Z = -5311602
73
XDOT = -4237
070433 XDOT = -1208
281851
YDOT = -24736
371155 feet/sec YDOT = -7553
622857 meter/sec
ZDOT = 830
215113 ZDOT = 246
977797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1595268
07 X = -486237
71
Y = -13759277
28 feet Y = -4193827
71 meter
Z = -17451446
90 Z = -5319201
01
XDOT = 23789
645967 XDOT = 7251
084091
YDOT = -3781
326828 feet/sec YDOT = -1152
548417 meter/sec
ZDOT = 803
798683 ZDOT = 244
997839
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 18336
56777294
00016717 00000-0 10270-3 0 9140
2 25544 51
6409 259
6208 0005145 103
6802 256
4924 15
54059529 24692
Satellite: ISS
Catalog Number: 25544
Epoch time: 18336
56777294 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 259
6208 deg
Eccentricity:
0005145
Arg of perigee: 103
6802 deg
Mean anomaly: 256
4924 deg
Mean motion: 15
54059529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2469
Checksum: 336
Coasting Arc #16 (Orbit 2483)
---------------------------------------
Vector Time (GMT): 2018/337/11:31:54
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3190085
44 A = 6778914
24 meter
Y = -3332653
81 meter E =
0011002
Z = 4959977
40 I = 51
25571
XDOT = 3558
689882 Wp = 116
79105
YDOT = 6480
238940 meter/sec RA = 254
12601 deg
ZDOT = 2056
887635 TA = 313
06286
MA = 313
15492
Ha = 222
744 n
mi
Hp = 212
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10466159
57 X = 3203021
67
Y = -10933903
59 feet Y = -3296907
95 meter
Z = 16272891
72 Z = 4975505
25
XDOT = 11675
491738 XDOT = 3475
970113
YDOT = 21260
626445 feet/sec YDOT = 6519
572079 meter/sec
ZDOT = 6748
319011 ZDOT = 2073
974160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5369943
05 X = 1636758
64
Y = 14069994
13 feet Y = 4288534
21 meter
Z = 16343094
13 Z = 4981375
09
XDOT = -23174
552769 XDOT = -7063
603684
YDOT = 885
918209 feet/sec YDOT = 270
027870 meter/sec
ZDOT = 6824
396167 ZDOT = 2080
075952
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 18337
53235185
00016717 00000-0 10270-3 0 9157
2 25544 51
6394 254
8131 0004985 108
8743 251
2950 15
54083031 24843
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
53235185 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 254
8131 deg
Eccentricity:
0004985
Arg of perigee: 108
8743 deg
Mean anomaly: 251
2950 deg
Mean motion: 15
54083031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2484
Checksum: 314
Coasting Arc #17 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/337/17:35:42
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1390821
12 A = 6783737
77 meter
Y = -5516292
08 meter E =
0016459
Z = 3683672
80 I = 51
27222
XDOT = 4863
140854 Wp = 99
72840
YDOT = 4102
438154 meter/sec RA = 252
86744 deg
ZDOT = 4288
101866 TA = 304
43521
MA = 304
59066
Ha = 222
780 n
mi
Hp = 213
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4563061
42 X = 1434508
84
Y = -18098071
11 feet Y = -5500494
85 meter
Z = 12085540
69 Z = 3690534
89
XDOT = 15955
186530 XDOT = 4796
075125
YDOT = 13459
442762 feet/sec YDOT = 4156
445983 meter/sec
ZDOT = 14068
575676 ZDOT = 4311
563009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11573090
63 X = 3527478
03
Y = -14617221
32 feet Y = -4455329
06 meter
Z = 12117029
98 Z = 3693270
74
XDOT = 7798
617244 XDOT = 2377
018536
YDOT = 17975
718928 feet/sec YDOT = 5478
999129 meter/sec
ZDOT = 14173
592510 ZDOT = 4320
110997
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 18337
78957184
00016717 00000-0 10270-3 0 9165
2 25544 51
6377 253
5291 0004823 110
6389 249
5281 15
54061394 24884
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
78957184 = yrday
fracday
Element set: 916
Inclination: 51
6377 deg
RA of node: 253
5291 deg
Eccentricity:
0004823
Arg of perigee: 110
6389 deg
Mean anomaly: 249
5281 deg
Mean motion: 15
54061394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 343
Coasting Arc #18 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/337/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4177392
08 A = 6784289
90 meter
Y = 4047290
67 meter E =
0016769
Z = 3476315
23 I = 51
27461
XDOT = -1950
189978 Wp = 94
64727
YDOT = 5898
154539 meter/sec RA = 252
73070 deg
ZDOT = -4505
942770 TA = 44
23613
MA = 44
10220
Ha = 222
706 n
mi
Hp = 213
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13705354
58 X = 4114937
28
Y = 13278512
71 feet Y = 4093655
80 meter
Z = 11405233
68 Z = 3496456
38
XDOT = -6398
261082 XDOT = -1994
111996
YDOT = 19350
900720 feet/sec YDOT = 5876
100792 meter/sec
ZDOT = -14783
276805 ZDOT = -4515
522671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8750336
05 X = 2667102
43
Y = 16897456
03 feet Y = 5150344
60 meter
Z = 11495329
40 Z = 3503776
40
XDOT = -10843
714448 XDOT = -3305
164164
YDOT = 15740
935025 feet/sec YDOT = 4797
836996 meter/sec
ZDOT = -14827
030032 ZDOT = -4519
278754
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 18337
78957138
00016717 00000-0 10270-3 0 9175
2 25544 51
6379 253
5280 0004814 110
5576 249
6093 15
54069672 24880
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
78957138 = yrday
fracday
Element set: 917
Inclination: 51
6379 deg
RA of node: 253
5280 deg
Eccentricity:
0004814
Arg of perigee: 110
5576 deg
Mean anomaly: 249
6093 deg
Mean motion: 15
54069672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 349
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