[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 8th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25144 4947 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
311/16:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
2
319/09:49:40
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
5
320/04:47:00
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
4
320/18:14:08
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
3
322/09:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 213
1
322/19:25:00
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
325/22:20:00
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
0
Coasting Arc #1 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2018/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 665880
66 A = 6779403
20 meter
Y = 4568334
43 meter E =
0006774
Z = 4958526
46 I = 51
78521
XDOT = -7232
573757 Wp = 83
23282
YDOT = -1326
524703 meter/sec RA = 23
96502 deg
ZDOT = 2191
617458 TA = 345
43971
MA = 345
45921
Ha = 222
290 n
mi
Hp = 214
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2184647
84 X = 590660
19
Y = 14987973
85 feet Y = 4575360
25 meter
Z = 16268131
43 Z = 4961578
41
XDOT = -23728
916525 XDOT = -7227
848668
YDOT = -4352
115167 feet/sec YDOT = -1407
377919 meter/sec
ZDOT = 7190
345990 ZDOT = 2156
494618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12187244
34 X = -3714672
08
Y = -8969797
95 feet Y = -2733994
41 meter
Z = 16281214
53 Z = 4962514
19
XDOT = 19051
246118 XDOT = 5806
819817
YDOT = -13109
381123 feet/sec YDOT = -3995
739366 meter/sec
ZDOT = 7032
550947 ZDOT = 2143
521529
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 18311
55198596
00016717 00000-0 10270-3 0 9009
2 25544 51
6421 24
2967 0004389 19
8243 340
3080 15
53943315 20809
Satellite: ISS
Catalog Number: 25544
Epoch time: 18311
55198596 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 24
2967 deg
Eccentricity:
0004389
Arg of perigee: 19
8243 deg
Mean anomaly: 340
3080 deg
Mean motion: 15
53943315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2080
Checksum: 302
Coasting Arc #2 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2018/311/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4215292
05 A = 6780307
23 meter
Y = 2304765
14 meter E =
0011683
Z = 4780659
71 I = 51
77918
XDOT = -5533
850682 Wp = 46
34506
YDOT = -4604
594613 meter/sec RA = 22
92753 deg
ZDOT = -2647
608839 TA = 69
78039
MA = 69
65480
Ha = 222
555 n
mi
Hp = 214
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13829698
34 X = -4263973
88
Y = 7561565
42 feet Y = 2257354
66 meter
Z = 15684579
10 Z = 4760064
44
XDOT = -18155
678089 XDOT = -5469
088474
YDOT = -15106
937708 feet/sec YDOT = -4666
115889 meter/sec
ZDOT = -8686
380705 ZDOT = -2674
333797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13288689
95 X = -4050392
70
Y = -8646158
13 feet Y = -2635349
00 meter
Z = 15591616
93 Z = 4752324
84
XDOT = 4027
492604 XDOT = 1227
579746
YDOT = -22140
714323 feet/sec YDOT = -6748
489726 meter/sec
ZDOT = -8805
936507 ZDOT = -2684
049447
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 18311
74491825
00016717 00000-0 10270-3 0 9012
2 25544 51
6395 23
3365 0004765 21
9323 338
2033 15
53934760 20833
Satellite: ISS
Catalog Number: 25544
Epoch time: 18311
74491825 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 23
3365 deg
Eccentricity:
0004765
Arg of perigee: 21
9323 deg
Mean anomaly: 338
2033 deg
Mean motion: 15
53934760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 299
Coasting Arc #3 (Orbit 2097)
---------------------------------------
Vector Time (GMT): 2018/312/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5398848
16 A = 6783790
01 meter
Y = -1441164
55 meter E =
0008686
Z = -3851004
12 I = 51
75995
XDOT = 4251
342703 Wp = 69
69725
YDOT = 4826
776919 meter/sec RA = 17
94916 deg
ZDOT = 4164
316286 TA = 244
04223
MA = 244
13175
Ha = 222
683 n
mi
Hp = 214
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17712756
43 X = 5433269
08
Y = -4728230
16 feet Y = -1380598
37 meter
Z = -12634527
94 Z = -3824694
06
XDOT = 13947
974749 XDOT = 4176
823742
YDOT = 15835
882281 feet/sec YDOT = 4873
901663 meter/sec
ZDOT = 13662
455005 ZDOT = 4184
787491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12866718
80 X = 3921775
89
Y = 13172957
61 feet Y = 4015117
48 meter
Z = -12515987
07 Z = -3814872
86
XDOT = -6018
963066 XDOT = -1834
579943
YDOT = 18913
738243 feet/sec YDOT = 5764
907417 meter/sec
ZDOT = 13753
837577 ZDOT = 4192
169693
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 18312
70957575
00016717 00000-0 10270-3 0 9029
2 25544 51
6398 18
5301 0004953 26
7841 333
3567 15
53912270 20985
Satellite: ISS
Catalog Number: 25544
Epoch time: 18312
70957575 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 18
5301 deg
Eccentricity:
0004953
Arg of perigee: 26
7841 deg
Mean anomaly: 333
3567 deg
Mean motion: 15
53912270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2098
Checksum: 318
Coasting Arc #4 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2018/313/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6272992
71 A = 6787238
60 meter
Y = 587601
22 meter E =
0015637
Z = 2512174
60 I = 51
73871
XDOT = -2594
592697 Wp = 86
33872
YDOT = -4891
544915 meter/sec RA = 12
97685 deg
ZDOT = -5305
208402 TA = 65
51688
MA = 65
35388
Ha = 222
638 n
mi
Hp = 213
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20580684
74 X = -6291300
35
Y = 1927825
52 feet Y = 517349
81 meter
Z = 8242042
66 Z = 2481657
33
XDOT = -8512
443233 XDOT = -2513
930659
YDOT = -16048
375704 feet/sec YDOT = -4920
108257 meter/sec
ZDOT = -17405
539378 ZDOT = -5317
616617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12114222
49 X = -3692415
02
Y = -16815817
30 feet Y = -5125461
11 meter
Z = 8104706
32 Z = 2470314
49
XDOT = 8359
866480 XDOT = 2548
087303
YDOT = -14485
342638 feet/sec YDOT = -4415
132436 meter/sec
ZDOT = -17460
638654 ZDOT = -5322
002662
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 18313
73853788
00016717 00000-0 10270-3 0 9035
2 25544 51
6385 13
4016 0005029 28
1273 332
0151 15
53959042 21140
Satellite: ISS
Catalog Number: 25544
Epoch time: 18313
73853788 = yrday
fracday
Element set: 903
Inclination: 51
6385 deg
RA of node: 13
4016 deg
Eccentricity:
0005029
Arg of perigee: 28
1273 deg
Mean anomaly: 332
0151 deg
Mean motion: 15
53959042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 289
Coasting Arc #5 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2018/314/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6710295
22 A = 6789441
18 meter
Y = 168349
35 meter E =
0014823
Z = -973566
40 I = 51
71332
XDOT = 729
450365 Wp = 37
02731
YDOT = 4821
746148 meter/sec RA = 8
01140 deg
ZDOT = 5919
904533 TA = 312
43575
MA = 312
56102
Ha = 222
691 n
mi
Hp = 213
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22015404
26 X = 6712643
14
Y = 552327
25 feet Y = 243401
70 meter
Z = -3194115
48 Z = -940963
64
XDOT = 2393
209859 XDOT = 646
721599
YDOT = 15819
377126 feet/sec YDOT = 4829
440516 meter/sec
ZDOT = 19422
258967 ZDOT = 5923
247328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11015096
04 X = 3357401
27
Y = 19093605
69 feet Y = 5819731
01 meter
Z = -3047514
52 Z = -928882
43
XDOT = -10929
239940 XDOT = -3331
232334
YDOT = 9375
282084 feet/sec YDOT = 2857
585979 meter/sec
ZDOT = 19436
591287 ZDOT = 5924
273024
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 18314
70318776
00016717 00000-0 10270-3 0 9047
2 25544 51
6381 8
5951 0004893 34
5554 325
5916 15
53963654 21296
Satellite: ISS
Catalog Number: 25544
Epoch time: 18314
70318776 = yrday
fracday
Element set: 904
Inclination: 51
6381 deg
RA of node: 8
5951 deg
Eccentricity:
0004893
Arg of perigee: 34
5554 deg
Mean anomaly: 325
5916 deg
Mean motion: 15
53963654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2129
Checksum: 327
Coasting Arc #6 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2018/315/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6688534
92 A = 6789582
68 meter
Y = -915740
14 meter E =
0010399
Z = -707480
16 I = 51
68190
XDOT = 1259
269196 Wp = 111
35110
YDOT = -4650
064878 meter/sec RA = 3
04545 deg
ZDOT = -5960
528182 TA = 76
28286
MA = 76
16712
Ha = 222
720 n
mi
Hp = 213
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21944012
22 X = -6674361
12
Y = -3004396
78 feet Y = -990456
69 meter
Z = -2321129
14 Z = -739937
01
XDOT = 4131
460617 XDOT = 1340
127599
YDOT = -15256
118365 feet/sec YDOT = -4635
530426 meter/sec
ZDOT = -19555
538655 ZDOT = -5954
214824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9213309
10 X = -2808216
61
Y = -20124183
42 feet Y = -6133851
11 meter
Z = -2466959
58 Z = -751929
28
XDOT = 13698
257124 XDOT = 4175
228772
YDOT = -3905
788891 feet/sec YDOT = -1190
484454 meter/sec
ZDOT = -19526
467488 ZDOT = -5951
667290
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 18315
73214152
00016717 00000-0 10270-3 0 9055
2 25544 51
6392 3
4660 0005079 35
9810 324
1684 15
53957020 21451
Satellite: ISS
Catalog Number: 25544
Epoch time: 18315
73214152 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 3
4660 deg
Eccentricity:
0005079
Arg of perigee: 35
9810 deg
Mean anomaly: 324
1684 deg
Mean motion: 15
53957020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2145
Checksum: 290
Coasting Arc #7 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2018/316/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6182331
62 A = 6787450
16 meter
Y = 1593979
42 meter E =
0018115
Z = 2275219
65 I = 51
64166
XDOT = -3146
791442 Wp = 63
73067
YDOT = 4409
811328 meter/sec RA = 358
07619 deg
ZDOT = 5435
490750 TA = 321
61592
MA = 321
74468
Ha = 222
603 n
mi
Hp = 213
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20283240
22 X = 6152995
81
Y = 5229591
28 feet Y = 1662950
40 meter
Z = 7464631
41 Z = 2305180
61
XDOT = -10324
118904 XDOT = -3222
272489
YDOT = 14467
884936 feet/sec YDOT = 4374
199395 meter/sec
ZDOT = 17832
974902 ZDOT = 5420
021373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6767079
18 X = 2062605
73
Y = 19772177
27 feet Y = 6026559
63 meter
Z = 7599133
25 Z = 2316215
82
XDOT = -16386
068174 XDOT = -4994
473579
YDOT = -1250
477848 feet/sec YDOT = -381
145648 meter/sec
ZDOT = 17762
764722 ZDOT = 5414
090687
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 18316
76108901
00016717 00000-0 10270-3 0 9064
2 25544 51
6388 358
3388 0004889 39
7500 320
4010 15
53993860 21613
Satellite: ISS
Catalog Number: 25544
Epoch time: 18316
76108901 = yrday
fracday
Element set: 906
Inclination: 51
6388 deg
RA of node: 358
3388 deg
Eccentricity:
0004889
Arg of perigee: 39
7500 deg
Mean anomaly: 320
4010 deg
Mean motion: 15
53993860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2161
Checksum: 321
Coasting Arc #8 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2018/317/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5240363
70 A = 6784023
00 meter
Y = -2289385
76 meter E =
0010197
Z = -3661926
19 I = 51
59685
XDOT = 4814
623699 Wp = 61
22169
YDOT = -4060
800699 meter/sec RA = 353
09570 deg
ZDOT = -4355
579921 TA = 162
26094
MA = 162
22531
Ha = 222
806 n
mi
Hp = 213
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17192794
30 X = -5196585
72
Y = -7511108
14 feet Y = -2347742
20 meter
Z = -12014193
54 Z = -3687276
20
XDOT = 15796
009511 XDOT = 4880
832280
YDOT = -13322
836939 feet/sec YDOT = -4006
589837 meter/sec
ZDOT = -14289
960370 ZDOT = -4332
031193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3460933
91 X = -1054892
66
Y = -18365371
06 feet Y = -5597765
10 meter
Z = -12127854
30 Z = -3696569
99
XDOT = 18629
615896 XDOT = 5678
306925
YDOT = 5846
065351 feet/sec YDOT = 1781
880719 meter/sec
ZDOT = -14183
473919 ZDOT = -4323
122850
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 18317
72572725
00016717 00000-0 10270-3 0 9071
2 25544 51
6388 353
5306 0005097 42
1294 318
0250 15
53964619 21765
Satellite: ISS
Catalog Number: 25544
Epoch time: 18317
72572725 = yrday
fracday
Element set: 907
Inclination: 51
6388 deg
RA of node: 353
5306 deg
Eccentricity:
0005097
Arg of perigee: 42
1294 deg
Mean anomaly: 318
0250 deg
Mean motion: 15
53964619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2176
Checksum: 320
Coasting Arc #9 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2018/318/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3937153
95 A = 6780358
10 meter
Y = 2949173
74 meter E =
0010604
Z = 4657128
64 I = 51
55323
XDOT = -6123
236561 Wp = 89
96206
YDOT = 3623
529016 meter/sec RA = 348
10463 deg
ZDOT = 2876
313006 TA = 331
41840
MA = 331
47649
Ha = 222
601 n
mi
Hp = 213
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12917171
74 X = 3881260
68
Y = 9675766
86 feet Y = 2992889
04 meter
Z = 15279293
42 Z = 4676118
56
XDOT = -20089
358795 XDOT = -6177
272570
YDOT = 11888
218557 feet/sec YDOT = 3554
752492 meter/sec
ZDOT = 9436
722461 ZDOT = 2846
436954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -476029
38 X = -145093
76
Y = 16051281
66 feet Y = 4892430
65 meter
Z = 15364255
62 Z = 4683025
11
XDOT = -20187
082508 XDOT = -6153
022749
YDOT = -9520
071502 feet/sec YDOT = -2901
717794 meter/sec
ZDOT = 9301
855743 ZDOT = 2835
205631
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 18318
75466678
00016717 00000-0 10270-3 0 9085
2 25544 51
6398 348
4033 0004877 44
7840 315
3706 15
54007994 21925
Satellite: ISS
Catalog Number: 25544
Epoch time: 18318
75466678 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 348
4033 deg
Eccentricity:
0004877
Arg of perigee: 44
7840 deg
Mean anomaly: 315
3706 deg
Mean motion: 15
54007994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 344
Coasting Arc #10 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2018/319/09:49:40
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3741213
34 A = 6779758
06 meter
Y = 2940983
35 meter E =
0009727
Z = 4820679
48 I = 51
52964
XDOT = -6196
485485 Wp = 91
71822
YDOT = 3773
227742 meter/sec RA = 344
56794 deg
ZDOT = 2502
333213 TA = 333
64527
MA = 333
69472
Ha = 222
659 n
mi
Hp = 213
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12274321
97 X = 3684631
78
Y = 9648895
49 feet Y = 2982503
69 meter
Z = 15815877
56 Z = 4838715
88
XDOT = -20329
676788 XDOT = -6250
373400
YDOT = 12379
356109 feet/sec YDOT = 3703
632960 meter/sec
ZDOT = 8209
754635 ZDOT = 2472
101682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14816558
90 X = -4516087
15
Y = -4655251
27 feet Y = -1418920
59 meter
Z = 15896551
99 Z = 4845269
05
XDOT = 14262
891975 XDOT = 4347
329474
YDOT = -17775
265382 feet/sec YDOT = -5417
900888 meter/sec
ZDOT = 8073
275345 ZDOT = 2460
734325
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 18319
46206065
00016717 00000-0 10270-3 0 9097
2 25544 51
6413 344
8764 0004818 48
9436 311
2132 15
53988057 22034
Satellite: ISS
Catalog Number: 25544
Epoch time: 18319
46206065 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 344
8764 deg
Eccentricity:
0004818
Arg of perigee: 48
9436 deg
Mean anomaly: 311
2132 deg
Mean motion: 15
53988057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 315
Coasting Arc #11 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2018/320/04:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5916975
57 A = 6789195
69 meter
Y = 3094146
91 meter E =
0016130
Z = 1198574
06 I = 51
53443
XDOT = -3185
591772 Wp = 105
96364
YDOT = -3803
056750 meter/sec RA = 340
59249 deg
ZDOT = -5847
386646 TA = 60
99525
MA = 60
83370
Ha = 222
829 n
mi
Hp = 213
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19412649
50 X = -5956957
53
Y = 10151400
63 feet Y = 3027755
61 meter
Z = 3932329
58 Z = 1169734
02
XDOT = -10451
416576 XDOT = -3114
424287
YDOT = -12477
220309 feet/sec YDOT = -3838
282222 meter/sec
ZDOT = -19184
339391 ZDOT = -5862
688557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19652889
44 X = 5990200
70
Y = 9729964
93 feet Y = 2965693
31 meter
Z = 3802213
89 Z = 1158914
79
XDOT = -3294
773623 XDOT = -1004
247000
YDOT = 14259
412053 feet/sec YDOT = 4346
268794 meter/sec
ZDOT = -19252
593423 ZDOT = -5868
190475
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 18320
23376277
00016717 00000-0 10270-3 0 9109
2 25544 51
6400 341
0275 0004782 54
9044 305
2557 15
53979346 22156
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
23376277 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 341
0275 deg
Eccentricity:
0004782
Arg of perigee: 54
9044 deg
Mean anomaly: 305
2557 deg
Mean motion: 15
53979346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 299
Coasting Arc #12 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2018/320/18:14:08
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4134619
30 A = 6779833
73 meter
Y = 2427198
95 meter E =
0010283
Z = 4784984
16 I = 51
48656
XDOT = -5643
095660 Wp = 92
21095
YDOT = 4516
515124 meter/sec RA = 337
82987 deg
ZDOT = 2579
895548 TA = 332
31830
MA = 332
37300
Ha = 222
713 n
mi
Hp = 213
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13565023
95 X = 4083927
15
Y = 7963251
15 feet Y = 2473151
65 meter
Z = 15698766
94 Z = 4804945
88
XDOT = -18514
093372 XDOT = -5705
713126
YDOT = 14817
963006 feet/sec YDOT = 4453
059964 meter/sec
ZDOT = 8464
224238 ZDOT = 2552
330937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7296086
36 X = 2223847
12
Y = 13833849
17 feet Y = 4216557
23 meter
Z = 15788168
61 Z = 4812233
79
XDOT = -22571
526416 XDOT = -6879
801252
YDOT = 2367
308938 feet/sec YDOT = 721
555764 meter/sec
ZDOT = 8339
645904 ZDOT = 2541
924072
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 18320
81253603
00016717 00000-0 10270-3 0 9111
2 25544 51
6403 338
1481 0005012 52
1472 308
0134 15
54008471 22242
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
81253603 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 338
1481 deg
Eccentricity:
0005012
Arg of perigee: 52
1472 deg
Mean anomaly: 308
0134 deg
Mean motion: 15
54008471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 257
Coasting Arc #13 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2018/321/18:14:08
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2692898
86 A = 6777917
03 meter
Y = -3335218
57 meter E =
0019253
Z = -5266954
01 I = 51
45031
XDOT = 6473
352310 Wp = 76
44393
YDOT = -4011
307254 meter/sec RA = 332
82164 deg
ZDOT = -767
560945 TA = 186
17704
MA = 186
20081
Ha = 222
921 n
mi
Hp = 213
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8834970
02 X = -2629818
89
Y = -10942318
14 feet Y = -3364979
73 meter
Z = -17280032
84 Z = -5279882
17
XDOT = 21238
032513 XDOT = 6521
455218
YDOT = -13160
456871 feet/sec YDOT = -3938
648770 meter/sec
ZDOT = -2518
244570 ZDOT = -735
998319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1936124
83 X = -590130
85
Y = -13858094
75 feet Y = -4223947
28 meter
Z = -17337681
13 Z = -5284525
21
XDOT = 23983
201985 XDOT = 7310
079965
YDOT = -370
027410 feet/sec YDOT = -112
784354 meter/sec
ZDOT = -2375
777475 ZDOT = -724
136974
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 18321
77715797
00016717 00000-0 10270-3 0 9125
2 25544 51
6411 333
3403 0005145 55
1838 304
9798 15
53997468 22397
Satellite: ISS
Catalog Number: 25544
Epoch time: 18321
77715797 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 333
3403 deg
Eccentricity:
0005145
Arg of perigee: 55
1838 deg
Mean anomaly: 304
9798 deg
Mean motion: 15
53997468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2239
Checksum: 336
Coasting Arc #14 (Orbit 2248)
---------------------------------------
Vector Time (GMT): 2018/322/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 917504
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4595509
91 A = 6780238
36 meter
Y = -1664072
97 meter E =
0016011
Z = -4714937
71 I = 51
43923
XDOT = 4754
621319 Wp = 67
21354
YDOT = -5329
871673 meter/sec RA = 329
63975 deg
ZDOT = -2754
502106 TA = 175
39618
MA = 175
38144
Ha = 222
955 n
mi
Hp = 213
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15077132
25 X = -4553657
15
Y = -5459556
98 feet Y = -1715229
16 meter
Z = -15468955
73 Z = -4737159
83
XDOT = 15599
151310 XDOT = 4827
248211
YDOT = -17486
455620 feet/sec YDOT = -5276
296120 meter/sec
ZDOT = -9037
080399 ZDOT = -2731
228982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15938308
00 X = 4857996
28
Y = -60328
78 feet Y = -18388
21 meter
Z = -15568621
29 Z = -4745315
77
XDOT = -8641
795810 XDOT = -2634
019363
YDOT = 20664
316376 feet/sec YDOT = 6298
483631 meter/sec
ZDOT = -8931
702031 ZDOT = -2722
382779
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 18322
42023530
00016717 00000-0 10270-3 0 9136
2 25544 51
6410 330
1340 0005053 60
2287 299
9368 15
53982721 22497
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
42023530 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 330
1340 deg
Eccentricity:
0005053
Arg of perigee: 60
2287 deg
Mean anomaly: 299
9368 deg
Mean motion: 15
53982721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 287
Coasting Arc #15 (Orbit 2255)
---------------------------------------
Vector Time (GMT): 2018/322/19:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6126804
55 A = 6788788
53 meter
Y = -2502104
32 meter E =
0019071
Z = 1470900
46 I = 51
45715
XDOT = 656
088974 Wp = 60
42515
YDOT = 5022
454465 meter/sec RA = 327
58685 deg
ZDOT = 5763
652752 TA = 315
67965
MA = 315
83217
Ha = 222
948 n
mi
Hp = 213
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20101064
80 X = 6147183
43
Y = -8209003
67 feet Y = -2433476
18 meter
Z = 4825788
92 Z = 1500712
42
XDOT = 2152
522881 XDOT = 571
880410
YDOT = 16477
868980 feet/sec YDOT = 5029
320488 meter/sec
ZDOT = 18909
621891 ZDOT = 5766
635316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21325970
25 X = 6500155
73
Y = -3915176
40 feet Y = -1193345
77 meter
Z = 4960158
54 Z = 1511856
32
XDOT = -1684
196304 XDOT = -513
343034
YDOT = 14989
270950 feet/sec YDOT = 4568
729785 meter/sec
ZDOT = 18922
322367 ZDOT = 5767
523857
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 18322
87038965
00016717 00000-0 10270-3 0 9144
2 25544 51
6421 327
8920 0005190 58
0681 302
0976 15
53983437 22565
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
87038965 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 327
8920 deg
Eccentricity:
0005190
Arg of perigee: 58
0681 deg
Mean anomaly: 302
0976 deg
Mean motion: 15
53983437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2256
Checksum: 323
Coasting Arc #16 (Orbit 2270)
---------------------------------------
Vector Time (GMT): 2018/323/19:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5902337
54 A = 6785831
00 meter
Y = 1496285
12 meter E =
0008753
Z = -3003972
09 I = 51
41937
XDOT = 1047
468672 Wp = 83
52337
YDOT = -5760
482479 meter/sec RA = 322
59887 deg
ZDOT = -4938
875082 TA = 130
94568
MA = 130
86989
Ha = 222
937 n
mi
Hp = 213
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19364624
48 X = -5904038
71
Y = 4909071
91 feet Y = 1430271
58 meter
Z = -9855551
47 Z = -3032648
36
XDOT = 3436
577007 XDOT = 1135
797131
YDOT = -18899
220730 feet/sec YDOT = -5748
275064 meter/sec
ZDOT = -16203
658407 ZDOT = -4933
572210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19877657
21 X = -6058709
92
Y = 1185238
17 feet Y = 361260
59 meter
Z = -9984664
11 Z = -3043325
62
XDOT = 7127
628968 XDOT = 2172
501309
YDOT = -16444
913814 feet/sec YDOT = -5012
409731 meter/sec
ZDOT = -16179
015689 ZDOT = -4931
363982
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
83500178
00016717 00000-0 10270-3 0 9152
2 25544 51
6415 323
0851 0005010 62
0292 298
1367 15
53981493 22719
Satellite: ISS
Catalog Number: 25544
Epoch time: 18323
83500178 = yrday
fracday
Element set: 915
Inclination: 51
6415 deg
RA of node: 323
0851 deg
Eccentricity:
0005010
Arg of perigee: 62
0292 deg
Mean anomaly: 298
1367 deg
Mean motion: 15
53981493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2271
Checksum: 295
Coasting Arc #17 (Orbit 2286)
---------------------------------------
Vector Time (GMT): 2018/324/19:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5309934
29 A = 6782122
93 meter
Y = -310083
51 meter E =
0014361
Z = 4195695
16 I = 51
38138
XDOT = -2528
641490 Wp = 92
05923
YDOT = 6259
051713 meter/sec RA = 317
59869 deg
ZDOT = 3651
405180 TA = 320
37637
MA = 320
48123
Ha = 222
883 n
mi
Hp = 213
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17421044
27 X = 5292626
09
Y = -1017334
34 feet Y = -250800
99 meter
Z = 13765404
06 Z = 4221447
59
XDOT = -8296
067882 XDOT = -2616
181071
YDOT = 20534
946565 feet/sec YDOT = 6230
285150 meter/sec
ZDOT = 11979
675789 ZDOT = 3638
909106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17246637
26 X = 5256775
04
Y = 1969736
84 feet Y = 600375
79 meter
Z = 13881201
01 Z = 4230990
07
XDOT = -11628
819825 XDOT = -3544
464283
YDOT = 17538
137197 feet/sec YDOT = 5345
624218 meter/sec
ZDOT = 11922
637532 ZDOT = 3634
019920
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
86391924
00016717 00000-0 10270-3 0 9164
2 25544 51
6415 317
9566 0005158 65
3311 294
8379 15
53991333 22872
Satellite: ISS
Catalog Number: 25544
Epoch time: 18324
86391924 = yrday
fracday
Element set: 916
Inclination: 51
6415 deg
RA of node: 317
9566 deg
Eccentricity:
0005158
Arg of perigee: 65
3311 deg
Mean anomaly: 294
8379 deg
Mean motion: 15
53991333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2287
Checksum: 340
Coasting Arc #18 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2018/325/19:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4465385
74 A = 6778904
05 meter
Y = -1058137
73 meter E =
0017917
Z = -5005888
65 I = 51
34723
XDOT = 3726
389400 Wp = 72
85822
YDOT = -6387
916639 meter/sec RA = 312
58678 deg
ZDOT = -1974
466109 TA = 177
85824
MA = 177
85055
Ha = 222
933 n
mi
Hp = 212
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14650215
69 X = -4428904
84
Y = -3471580
47 feet Y = -1107868
58 meter
Z = -16423519
19 Z = -5027491
98
XDOT = 12225
687008 XDOT = 3807
135090
YDOT = -20957
731755 feet/sec YDOT = -6345
794002 meter/sec
ZDOT = -6477
907182 ZDOT = -1956
168258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13829509
96 X = -4215234
64
Y = -5677261
13 feet Y = -1730429
19 meter
Z = -16520473
17 Z = -5035440
22
XDOT = 14944
818526 XDOT = 4555
180687
YDOT = -17802
993558 feet/sec YDOT = -5426
352437 meter/sec
ZDOT = -6394
780949 ZDOT = -1949
129233
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
82852330
00016717 00000-0 10270-3 0 9175
2 25544 51
6416 313
1484 0005058 67
4021 292
7666 15
54030466 23026
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
82852330 = yrday
fracday
Element set: 917
Inclination: 51
6416 deg
RA of node: 313
1484 deg
Eccentricity:
0005058
Arg of perigee: 67
4021 deg
Mean anomaly: 292
7666 deg
Mean motion: 15
54030466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 295
Coasting Arc #19 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2018/325/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5516376
06 A = 6786376
44 meter
Y = 2852927
46 meter E =
0008806
Z = -2742784
68 I = 51
36584
XDOT = -397
603530 Wp = 93
51752
YDOT = -5680
892712 meter/sec RA = 311
98295 deg
ZDOT = -5124
149630 TA = 117
62587
MA = 117
53644
Ha = 222
938 n
mi
Hp = 213
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18098346
65 X = -5534544
93
Y = 9359998
24 feet Y = 2791138
05 meter
Z = -8998637
39 Z = -2769626
05
XDOT = -1304
473524 XDOT = -309
157552
YDOT = -18638
099448 feet/sec YDOT = -5684
844223 meter/sec
ZDOT = -16811
514534 ZDOT = -5125
866538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9412790
52 X = -2869018
55
Y = 18010166
60 feet Y = 5489498
78 meter
Z = -9119674
74 Z = -2779676
86
XDOT = -10350
371568 XDOT = -3154
793254
YDOT = -13901
463986 feet/sec YDOT = -4237
166223 meter/sec
ZDOT = -16818
446573 ZDOT = -5126
262515
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
95713664
00016717 00000-0 10270-3 0 9186
2 25544 51
6380 312
5047 0005056 68
6841 291
4851 15
54016824 23041
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
95713664 = yrday
fracday
Element set: 918
Inclination: 51
6380 deg
RA of node: 312
5047 deg
Eccentricity:
0005056
Arg of perigee: 68
6841 deg
Mean anomaly: 291
4851 deg
Mean motion: 15
54016824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 311
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