[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 21st 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
300/09:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 215
5
303/21:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 1783)
---------------------------------------
Vector Time (GMT): 2018/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3461356
61 A = 6778229
90 meter
Y = 2375305
22 meter E =
0011755
Z = -5331701
28 I = 51
95056
XDOT = -3893
279100 Wp = 81
84282
YDOT = 6583
833456 meter/sec RA = 118
20475 deg
ZDOT = 407
998775 TA = 192
02162
MA = 192
04970
Ha = 220
690 n
mi
Hp = 216
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11356156
85 X = 3460436
91
Y = 7792996
14 feet Y = 2414007
02 meter
Z = -17492458
28 Z = -5314889
42
XDOT = -12773
225393 XDOT = -3968
593867
YDOT = 21600
503463 feet/sec YDOT = 6539
875021 meter/sec
ZDOT = 1338
578657 ZDOT = 388
902999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13760275
53 X = -4194131
98
Y = -1726044
18 feet Y = -526098
27 meter
Z = -17417082
79 Z = -5308726
83
XDOT = 1441
567668 XDOT = 439
389825
YDOT = -24046
624036 feet/sec YDOT = -7329
411006 meter/sec
ZDOT = 1252
007000 ZDOT = 381
611734
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 18292
51543861
00016717 00000-0 10270-3 0 9002
2 25544 51
6366 119
1576 0004006 308
2586 51
8206 15
53844899 17849
Satellite: ISS
Catalog Number: 25544
Epoch time: 18292
51543861 = yrday
fracday
Element set: 900
Inclination: 51
6366 deg
RA of node: 119
1576 deg
Eccentricity:
0004006
Arg of perigee: 308
2586 deg
Mean anomaly: 51
8206 deg
Mean motion: 15
53844899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1784
Checksum: 325
Coasting Arc #2 (Orbit 1799)
---------------------------------------
Vector Time (GMT): 2018/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2594105
70 A = 6779827
31 meter
Y = -3812157
27 meter E =
0006504
Z = 4970350
28 I = 51
97003
XDOT = 4400
654566 Wp = 21
17703
YDOT = -5878
947735 meter/sec RA = 113
23116 deg
ZDOT = -2205
457822 TA = 90
27780
MA = 90
20326
Ha = 220
852 n
mi
Hp = 216
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8510845
46 X = -2575427
94
Y = -12507077
65 feet Y = -3841061
53 meter
Z = 16306923
50 Z = 4957794
53
XDOT = 14437
843064 XDOT = 4476
780619
YDOT = -19287
886269 feet/sec YDOT = -5829
311090 meter/sec
ZDOT = -7235
754008 ZDOT = -2183
895323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13483801
75 X = 4109862
77
Y = 6991025
54 feet Y = 2130864
58 meter
Z = 16250842
69 Z = 4953256
85
XDOT = -3216
823630 XDOT = -980
487843
YDOT = 22849
270071 feet/sec YDOT = 6964
457517 meter/sec
ZDOT = -7138
144623 ZDOT = -2175
706481
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 18293
54446346
00016717 00000-0 10270-3 0 9017
2 25544 51
6363 114
0299 0004031 311
5402 48
5404 15
53817924 18005
Satellite: ISS
Catalog Number: 25544
Epoch time: 18293
54446346 = yrday
fracday
Element set: 901
Inclination: 51
6363 deg
RA of node: 114
0299 deg
Eccentricity:
0004031
Arg of perigee: 311
5402 deg
Mean anomaly: 48
5404 deg
Mean motion: 15
53817924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1800
Checksum: 286
Coasting Arc #3 (Orbit 1814)
---------------------------------------
Vector Time (GMT): 2018/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1756588
85 A = 6782846
35 meter
Y = 5061020
34 meter E =
0004493
Z = -4163968
81 I = 51
99193
XDOT = -4681
653332 Wp = 87
76288
YDOT = 4738
806310 meter/sec RA = 108
26393 deg
ZDOT = 3788
408069 TA = 221
08003
MA = 221
11387
Ha = 220
886 n
mi
Hp = 216
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5763086
79 X = 1720091
25
Y = 16604397
45 feet Y = 5080459
29 meter
Z = -13661315
00 Z = -4155524
88
XDOT = -15359
755025 XDOT = -4752
698412
YDOT = 15547
264795 feet/sec YDOT = 4686
055914 meter/sec
ZDOT = 12429
160332 ZDOT = 3765
492880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13170428
63 X = -4014346
65
Y = -11682496
90 feet Y = -3560825
05 meter
Z = -13623868
30 Z = -4152555
06
XDOT = 5114
297065 XDOT = 1558
837745
YDOT = -20125
333729 feet/sec YDOT = -6134
201721 meter/sec
ZDOT = 12325
572476 ZDOT = 3756
834491
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 18294
50917240
00016717 00000-0 10270-3 0 9021
2 25544 51
6357 109
2219 0003872 314
9576 45
1262 15
53845320 18159
Satellite: ISS
Catalog Number: 25544
Epoch time: 18294
50917240 = yrday
fracday
Element set: 902
Inclination: 51
6357 deg
RA of node: 109
2219 deg
Eccentricity:
0003872
Arg of perigee: 314
9576 deg
Mean anomaly: 45
1262 deg
Mean motion: 15
53845320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1815
Checksum: 304
Coasting Arc #4 (Orbit 1830)
---------------------------------------
Vector Time (GMT): 2018/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -939921
52 A = 6786442
47 meter
Y = -6035340
35 meter E =
0010407
Z = 2950211
19 I = 52
01382
XDOT = 4802
747069 Wp = 83
29343
YDOT = -3218
006476 meter/sec RA = 103
30680 deg
ZDOT = -5036
677425 TA = 63
21429
MA = 63
10787
Ha = 220
911 n
mi
Hp = 216
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3083732
02 X = -886693
66
Y = -19800985
41 feet Y = -6045553
32 meter
Z = 9679170
59 Z = 2945775
13
XDOT = 15757
044190 XDOT = 4862
840766
YDOT = -10557
764030 feet/sec YDOT = -3163
963278 meter/sec
ZDOT = -16524
532234 ZDOT = -5013
200638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12623922
03 X = 3847771
44
Y = 15575567
40 feet Y = 4747432
94 meter
Z = 9659868
66 Z = 2944327
97
XDOT = -7328
413731 XDOT = -2233
700505
YDOT = 16155
714256 feet/sec YDOT = 4924
261705 meter/sec
ZDOT = -16418
569961 ZDOT = -5004
380124
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 18295
53819121
00016717 00000-0 10270-3 0 9035
2 25544 51
6361 104
0938 0004109 317
8380 42
2456 15
53858268 18310
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
53819121 = yrday
fracday
Element set: 903
Inclination: 51
6361 deg
RA of node: 104
0938 deg
Eccentricity:
0004109
Arg of perigee: 317
8380 deg
Mean anomaly: 42
2456 deg
Mean motion: 15
53858268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1831
Checksum: 309
Coasting Arc #5 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2018/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 198961
67 A = 6789195
73 meter
Y = 6615986
01 meter E =
0010099
Z = -1484507
15 I = 52
03022
XDOT = -4794
217727 Wp = 16
32782
YDOT = 1443
334208 meter/sec RA = 98
35826 deg
ZDOT = 5808
914021 TA = 327
55501
MA = 327
61706
Ha = 221
092 n
mi
Hp = 215
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 652761
39 X = 132176
21
Y = 21705990
84 feet Y = 6617837
39 meter
Z = -4870430
27 Z = -1483703
40
XDOT = -15729
060783 XDOT = -4838
218484
YDOT = 4735
348451 feet/sec YDOT = 1389
476396 meter/sec
ZDOT = 19058
116867 ZDOT = 5785
517833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11758978
43 X = -3584136
63
Y = -18257344
69 feet Y = -5564838
66 meter
Z = -4867547
41 Z = -1483628
45
XDOT = 9824
938691 XDOT = 2994
641313
YDOT = -11364
265055 feet/sec YDOT = -3463
827989 meter/sec
ZDOT = 18952
703918 ZDOT = 5776
784154
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 18296
50289564
00016717 00000-0 10270-3 0 9046
2 25544 51
6368 99
2859 0003832 323
8502 36
2391 15
53852748 18463
Satellite: ISS
Catalog Number: 25544
Epoch time: 18296
50289564 = yrday
fracday
Element set: 904
Inclination: 51
6368 deg
RA of node: 99
2859 deg
Eccentricity:
0003832
Arg of perigee: 323
8502 deg
Mean anomaly: 36
2391 deg
Mean motion: 15
53852748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 343
Coasting Arc #6 (Orbit 1861)
---------------------------------------
Vector Time (GMT): 2018/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 519087
19 A = 6790010
32 meter
Y = -6765215
51 meter E =
0007929
Z = -147473
85 I = 52
03622
XDOT = 4693
197001 Wp = 129
43958
YDOT = 486
986233 meter/sec RA = 93
41591 deg
ZDOT = -6041
352427 TA = 52
13980
MA = 52
06809
Ha = 221
131 n
mi
Hp = 215
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1703041
95 X = 595415
50
Y = -22195588
96 feet Y = -6758983
95 meter
Z = -483838
09 Z = -144766
39
XDOT = 15397
627957 XDOT = 4716
749081
YDOT = 1597
723863 feet/sec YDOT = 539
600101 meter/sec
ZDOT = -19820
710063 ZDOT = -6018
496712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10301823
29 X = 3139995
74
Y = 19733963
61 feet Y = 6014912
11 meter
Z = -470890
07 Z = -143527
29
XDOT = -12580
923561 XDOT = -3834
665501
YDOT = 6114
933087 feet/sec YDOT = 1863
831605 meter/sec
ZDOT = -19717
941953 ZDOT = -6010
028707
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 18297
53190922
00016717 00000-0 10270-3 0 9050
2 25544 51
6359 94
1581 0004034 328
2213 31
8696 15
53890226 18622
Satellite: ISS
Catalog Number: 25544
Epoch time: 18297
53190922 = yrday
fracday
Element set: 905
Inclination: 51
6359 deg
RA of node: 94
1581 deg
Eccentricity:
0004034
Arg of perigee: 328
2213 deg
Mean anomaly: 31
8696 deg
Mean motion: 15
53890226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1862
Checksum: 316
Coasting Arc #7 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2018/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1186570
93 A = 6788782
09 meter
Y = 6445037
49 meter E =
0014134
Z = 1740238
50 I = 52
03495
XDOT = -4526
551834 Wp = 49
11424
YDOT = -2382
895012 meter/sec RA = 88
47284 deg
ZDOT = 5717
564999 TA = 329
88428
MA = 329
96548
Ha = 221
213 n
mi
Hp = 215
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3892949
24 X = -1267006
36
Y = 21145136
11 feet Y = 6431318
77 meter
Z = 5709443
90 Z = 1734278
70
XDOT = -14850
891843 XDOT = -4527
342953
YDOT = -7817
897020 feet/sec YDOT = -2433
518210 meter/sec
ZDOT = 18758
415350 ZDOT = 5695
574121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8201806
81 X = -2499910
71
Y = -19882559
57 feet Y = -6060204
16 meter
Z = 5681881
26 Z = 1731837
41
XDOT = 15368
196010 XDOT = 4684
226144
YDOT = -987
188580 feet/sec YDOT = -300
895079 meter/sec
ZDOT = 18659
758222 ZDOT = 5687
494306
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 18298
56092159
00016717 00000-0 10270-3 0 9068
2 25544 51
6380 89
0301 0003822 329
9922 30
1011 15
53880859 18789
Satellite: ISS
Catalog Number: 25544
Epoch time: 18298
56092159 = yrday
fracday
Element set: 906
Inclination: 51
6380 deg
RA of node: 89
0301 deg
Eccentricity:
0003822
Arg of perigee: 329
9922 deg
Mean anomaly: 30
1011 deg
Mean motion: 15
53880859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 321
Coasting Arc #8 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2018/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1865084
06 A = 6785779
53 meter
Y = -5691072
85 meter E =
0003942
Z = -3196205
66 I = 52
02352
XDOT = 4273
036338 Wp = 46
52494
YDOT = 4120
048136 meter/sec RA = 83
52427 deg
ZDOT = -4843
690190 TA = 170
15207
MA = 170
14434
Ha = 221
348 n
mi
Hp = 215
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6119042
19 X = 1944110
55
Y = -18671498
86 feet Y = -5669774
40 meter
Z = -10486239
06 Z = -3186953
37
XDOT = 14019
148091 XDOT = 4250
176034
YDOT = 13517
218294 feet/sec YDOT = 4167
704254 meter/sec
ZDOT = -15891
372014 ZDOT = -4822
988262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5288651
12 X = 1611980
86
Y = 18946851
54 feet Y = 5775000
35 meter
Z = -10443933
29 Z = -3183310
87
XDOT = -17882
394382 XDOT = -5450
553808
YDOT = -3715
094228 feet/sec YDOT = -1132
360721 meter/sec
ZDOT = -15798
726189 ZDOT = -4815
451743
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 18299
52561777
00016717 00000-0 10270-3 0 9073
2 25544 51
6385 84
2229 0003935 336
1397 23
9573 15
53872986 18933
Satellite: ISS
Catalog Number: 25544
Epoch time: 18299
52561777 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 84
2229 deg
Eccentricity:
0003935
Arg of perigee: 336
1397 deg
Mean anomaly: 23
9573 deg
Mean motion: 15
53872986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1893
Checksum: 360
Coasting Arc #9 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2018/300/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3388325
34 A = 6779559
43 meter
Y = -3084289
80 meter E =
0013018
Z = -5008529
34 I = 51
99698
XDOT = 2988
817820 Wp = 56
17468
YDOT = 6725
535764 meter/sec RA = 79
02561 deg
ZDOT = -2116
560554 TA = 193
27494
MA = 193
30923
Ha = 221
507 n
mi
Hp = 215
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11116552
94 X = 3446892
40
Y = -10119061
01 feet Y = -3046071
75 meter
Z = -16432182
88 Z = -4991927
29
XDOT = 9805
832742 XDOT = 2923
670302
YDOT = 22065
406051 feet/sec YDOT = 6758
594527 meter/sec
ZDOT = -6944
096306 ZDOT = -2102
199764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11033552
83 X = -3363026
90
Y = 10329346
31 feet Y = 3148384
75 meter
Z = -16357111
48 Z = -4985647
58
XDOT = -9511
349407 XDOT = -2899
059299
YDOT = -21071
361854 feet/sec YDOT = -6422
551093 meter/sec
ZDOT = -6880
306892 ZDOT = -2097
117541
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 18300
42599820
00016717 00000-0 10270-3 0 9086
2 25544 51
6371 79
7379 0004086 341
5543 18
5461 15
53873826 19070
Satellite: ISS
Catalog Number: 25544
Epoch time: 18300
42599820 = yrday
fracday
Element set: 908
Inclination: 51
6371 deg
RA of node: 79
7379 deg
Eccentricity:
0004086
Arg of perigee: 341
5543 deg
Mean anomaly: 18
5461 deg
Mean motion: 15
53873826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 330
Coasting Arc #10 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2018/301/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3914445
77 A = 6778247
21 meter
Y = 1473354
66 meter E =
0003657
Z = 5332622
30 I = 51
98465
XDOT = -2334
637257 Wp = 21
93326
YDOT = -7299
289995 meter/sec RA = 74
05331 deg
ZDOT = 306
206417 TA = 65
18104
MA = 65
14300
Ha = 221
804 n
mi
Hp = 215
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12842669
84 X = -3956534
03
Y = 4833840
75 feet Y = 1429345
21 meter
Z = 17495480
00 Z = 5313504
58
XDOT = -7659
571054 XDOT = -2254
328474
YDOT = -23947
801822 feet/sec YDOT = -7324
948499 meter/sec
ZDOT = 1004
614228 ZDOT = 295
060233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12776443
25 X = 3894259
90
Y = -5298252
23 feet Y = -1614907
28 meter
Z = 17409279
89 Z = 5306348
51
XDOT = 8136
425488 XDOT = 2479
982489
YDOT = 22724
720797 feet/sec YDOT = 6926
494899 meter/sec
ZDOT = 955
376342 ZDOT = 291
198709
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 18301
45500401
00016717 00000-0 10270-3 0 9098
2 25544 51
6369 74
6098 0004118 344
8439 15
2589 15
53828865 19231
Satellite: ISS
Catalog Number: 25544
Epoch time: 18301
45500401 = yrday
fracday
Element set: 909
Inclination: 51
6369 deg
RA of node: 74
6098 deg
Eccentricity:
0004118
Arg of perigee: 344
8439 deg
Mean anomaly: 15
2589 deg
Mean motion: 15
53828865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 323
Coasting Arc #11 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2018/302/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4390391
72 A = 6778849
91 meter
Y = 157405
57 meter E =
0012640
Z = -5173142
86 I = 51
97887
XDOT = 1530
547661 Wp = 84
22087
YDOT = 7347
605974 meter/sec RA = 69
08008 deg
ZDOT = 1526
963689 TA = 200
41325
MA = 200
46381
Ha = 221
702 n
mi
Hp = 215
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14404172
30 X = 4413434
19
Y = 516422
47 feet Y = 206630
93 meter
Z = -16972253
48 Z = -5151759
43
XDOT = 5021
481826 XDOT = 1440
853587
YDOT = 24106
318812 feet/sec YDOT = 7364
220074 meter/sec
ZDOT = 5009
723389 ZDOT = 1534
181030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14523657
86 X = -4426810
92
Y = 257338
17 feet Y = 78436
68 meter
Z = -16876059
94 Z = -5143823
07
XDOT = -6243
859742 XDOT = -1903
128449
YDOT = -22748
320838 feet/sec YDOT = -6933
688192 meter/sec
ZDOT = 5041
261568 ZDOT = 1536
576526
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 18302
41969161
00016717 00000-0 10270-3 0 9109
2 25544 51
6388 69
8028 0004066 348
8496 11
2566 15
53882859 19380
Satellite: ISS
Catalog Number: 25544
Epoch time: 18302
41969161 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 69
8028 deg
Eccentricity:
0004066
Arg of perigee: 348
8496 deg
Mean anomaly: 11
2566 deg
Mean motion: 15
53882859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 343
Coasting Arc #12 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2018/303/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4758951
47 A = 6781637
69 meter
Y = -1732431
20 meter E =
0010786
Z = 4507363
49 I = 51
97393
XDOT = -552
107310 Wp = 47
18278
YDOT = -6931
056498 meter/sec RA = 64
10976 deg
ZDOT = -3234
887684 TA = 75
25485
MA = 75
13535
Ha = 221
897 n
mi
Hp = 215
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15613357
83 X = -4761120
00
Y = -5683829
39 feet Y = -1785661
32 meter
Z = 14787937
95 Z = 4484240
47
XDOT = -1811
375688 XDOT = -458
847633
YDOT = -22739
686674 feet/sec YDOT = -6936
709028 meter/sec
ZDOT = -10613
148568 ZDOT = -3237
343308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16072212
57 X = 4898810
39
Y = 4563619
49 feet Y = 1390991
22 meter
Z = 14684118
24 Z = 4475719
24
XDOT = 3668
622483 XDOT = 1118
196133
YDOT = 21389
711360 feet/sec YDOT = 6519
584023 meter/sec
ZDOT = -10623
301157 ZDOT = -3237
982193
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 18303
44869050
00016717 00000-0 10270-3 0 9110
2 25544 51
6377 64
6745 0004031 353
0650 7
0446 15
53852056 19543
Satellite: ISS
Catalog Number: 25544
Epoch time: 18303
44869050 = yrday
fracday
Element set: 911
Inclination: 51
6377 deg
RA of node: 64
6745 deg
Eccentricity:
0004031
Arg of perigee: 353
0650 deg
Mean anomaly: 7
0446 deg
Mean motion: 15
53852056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 297
Coasting Arc #13 (Orbit 1960)
---------------------------------------
Vector Time (GMT): 2018/303/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4836130
18 A = 6785070
90 meter
Y = 3250556
38 meter E =
0006327
Z = -3475516
63 I = 51
97845
XDOT = -799
204061 Wp = 45
83506
YDOT = 6086
499693 meter/sec RA = 61
70472 deg
ZDOT = 4589
905478 TA = 273
60475
MA = 273
67711
Ha = 222
023 n
mi
Hp = 215
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15866568
82 X = 4816304
59
Y = 10664555
06 feet Y = 3304526
55 meter
Z = -11402613
62 Z = -3452072
15
XDOT = -2622
060566 XDOT = -889
501261
YDOT = 19968
831014 feet/sec YDOT = 6077
057479 meter/sec
ZDOT = 15058
745008 ZDOT = 4585
803947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15803365
63 X = 4816865
85
Y = 10868276
68 feet Y = 3312650
73 meter
Z = -11297545
52 Z = -3443491
87
XDOT = -2186
808934 XDOT = -666
539363
YDOT = 18780
796133 feet/sec YDOT = 5724
386661 meter/sec
ZDOT = 15039
497262 ZDOT = 4584
038765
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 18303
89887529
00016717 00000-0 10270-3 0 9121
2 25544 51
6377 62
4358 0004525 355
1985 4
9123 15
53863423 19617
Satellite: ISS
Catalog Number: 25544
Epoch time: 18303
89887529 = yrday
fracday
Element set: 912
Inclination: 51
6377 deg
RA of node: 62
4358 deg
Eccentricity:
0004525
Arg of perigee: 355
1985 deg
Mean anomaly: 4
9123 deg
Mean motion: 15
53863423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1961
Checksum: 332
Coasting Arc #14 (Orbit 1976)
---------------------------------------
Vector Time (GMT): 2018/304/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4780295
34 A = 6788252
81 meter
Y = -4350913
58 meter E =
0012779
Z = 2061486
36 I = 51
97301
XDOT = 2016
443949 Wp = 91
82586
YDOT = -4868
102663 meter/sec RA = 56
75051 deg
ZDOT = -5569
306189 TA = 65
48520
MA = 65
35202
Ha = 221
974 n
mi
Hp = 214
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15683383
67 X = -4741300
66
Y = -14274650
84 feet Y = -4404152
12 meter
Z = 6763406
71 Z = 2038359
79
XDOT = 6615
629755 XDOT = 2097
783633
YDOT = -15971
465430 feet/sec YDOT = -4845
098592 meter/sec
ZDOT = -18272
001933 ZDOT = -5559
313324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15789504
91 X = -4812641
10
Y = -14206156
30 feet Y = -4330036
44 meter
Z = 6659918
03 Z = 2029943
02
XDOT = 5632
173211 XDOT = 1716
686395
YDOT = -14850
335573 feet/sec YDOT = -4526
382283 meter/sec
ZDOT = -18226
396886 ZDOT = -5555
405771
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 18304
92787006
00016717 00000-0 10270-3 0 9136
2 25544 51
6380 57
3074 0004602 357
5035 2
6094 15
53898740 19776
Satellite: ISS
Catalog Number: 25544
Epoch time: 18304
92787006 = yrday
fracday
Element set: 913
Inclination: 51
6380 deg
RA of node: 57
3074 deg
Eccentricity:
0004602
Arg of perigee: 357
5035 deg
Mean anomaly: 2
6094 deg
Mean motion: 15
53898740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1977
Checksum: 316
Coasting Arc #15 (Orbit 1991)
---------------------------------------
Vector Time (GMT): 2018/305/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4475159
75 A = 6789873
09 meter
Y = 5072228
43 meter E =
0014868
Z = -486198
46 I = 51
96023
XDOT = -3272
050236 Wp = 30
40260
YDOT = 3454
783836 meter/sec RA = 51
80235 deg
ZDOT = 6017
098531 TA = 324
37457
MA = 324
47372
Ha = 222
056 n
mi
Hp = 214
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14682282
65 X = 4420469
80
Y = 16641169
38 feet Y = 5121966
97 meter
Z = -1595139
31 Z = -464592
39
XDOT = -10735
072954 XDOT = -3339
667627
YDOT = 11334
592638 feet/sec YDOT = 3417
815557 meter/sec
ZDOT = 19741
136912 ZDOT = 6001
039560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15047222
75 X = 4586393
50
Y = 16321081
82 feet Y = 4974665
74 meter
Z = -1498595
04 Z = -456771
77
XDOT = -9429
657129 XDOT = -2874
159493
YDOT = 10469
942269 feet/sec YDOT = 3191
238404 meter/sec
ZDOT = 19668
419700 ZDOT = 5994
934324
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 18305
89254925
00016717 00000-0 10270-3 0 9143
2 25544 51
6387 52
5005 0004492 2
0805 358
0366 15
53911375 19925
Satellite: ISS
Catalog Number: 25544
Epoch time: 18305
89254925 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 52
5005 deg
Eccentricity:
0004492
Arg of perigee: 2
0805 deg
Mean anomaly: 358
0366 deg
Mean motion: 15
53911375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1992
Checksum: 312
Coasting Arc #16 (Orbit 2007)
---------------------------------------
Vector Time (GMT): 2018/306/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3859797
38 A = 6789371
39 meter
Y = -5460180
91 meter E =
0006557
Z = -1172145
59 I = 51
93768
XDOT = 4509
491128 Wp = 112
17955
YDOT = -1930
055545 meter/sec RA = 46
85402 deg
ZDOT = -5887
414926 TA = 80
48831
MA = 80
41422
Ha = 222
150 n
mi
Hp = 214
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12663377
24 X = -3792759
51
Y = -17913979
36 feet Y = -5502969
06 meter
Z = -3845622
02 Z = -1190732
35
XDOT = 14794
918399 XDOT = 4559
336723
YDOT = -6332
203232 feet/sec YDOT = -1879
348815 meter/sec
ZDOT = -19315
665768 ZDOT = -5865
387952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13321492
38 X = -4060390
88
Y = -17411638
71 feet Y = -5307067
48 meter
Z = -3928519
61 Z = -1197412
78
XDOT = 13397
121040 XDOT = 4083
442493
YDOT = -5935
116917 feet/sec YDOT = -1809
023636 meter/sec
ZDOT = -19216
299401 ZDOT = -5857
128058
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 18306
92153707
00016717 00000-0 10270-3 0 9155
2 25544 51
6391 47
3722 0004750 5
0359 355
0841 15
53903050 20087
Satellite: ISS
Catalog Number: 25544
Epoch time: 18306
92153707 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 47
3722 deg
Eccentricity:
0004750
Arg of perigee: 5
0359 deg
Mean anomaly: 355
0841 deg
Mean motion: 15
53903050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2008
Checksum: 286
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