[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 10th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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
190/12:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 216
2
191/01:39:14
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 216
1
191/20:25:30
000 -0
0 0
2 0
2
N/A -0
2 0
0 220
1
000/00:01:00
000 0
0 -0
0 216
0
193/18:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
9
196/12:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
8
196/17:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
8
197/12:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 215
7
199/12:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
5
203/19:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 215
2
Coasting Arc #1 (Orbit 197)
---------------------------------------
Vector Time (GMT): 2018/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4230120
74 A = 6778198
39 meter
Y = -1177482
90 meter E =
0010297
Z = -5172798
78 I = 51
24227
XDOT = 562
341212 Wp = 96
83754
YDOT = -7535
966000 meter/sec RA = 266
59657 deg
ZDOT = 1256
505096 TA = 185
29907
MA = 185
30998
Ha = 219
920 n
mi
Hp = 216
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13878348
87 X = -4191512
69
Y = -3863132
86 feet Y = -1224570
45 meter
Z = -16971124
60 Z = -5193253
63
XDOT = 1844
951483 XDOT = 640
465223
YDOT = -24724
297899 feet/sec YDOT = -7529
240865 meter/sec
ZDOT = 4122
392048 ZDOT = 1259
425482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 204626
47 X = 62370
15
Y = 14296222
47 feet Y = 4357488
61 meter
Z = -17062461
26 Z = -5200638
19
XDOT = -23179
420990 XDOT = -7065
087518
YDOT = 5264
938650 feet/sec YDOT = 1604
753301 meter/sec
ZDOT = 4136
500114 ZDOT = 1260
805235
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 18190
51392241
00016717 00000-0 10270-3 0 9003
2 25544 51
6402 267
4299 0003800 287
3606 72
7131 15
54019161 1984
Satellite: ISS
Catalog Number: 25544
Epoch time: 18190
51392241 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 267
4299 deg
Eccentricity:
0003800
Arg of perigee: 287
3606 deg
Mean anomaly: 72
7131 deg
Mean motion: 15
54019161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 198
Checksum: 291
Coasting Arc #2 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2018/190/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4254963
88 A = 6777777
55 meter
Y = 577875
86 meter E =
0002741
Z = 5245094
75 I = 51
24133
XDOT = -121
144394 Wp = 340
17433
YDOT = 7631
053616 meter/sec RA = 266
44462 deg
ZDOT = -740
050500 TA = 116
94935
MA = 116
92135
Ha = 219
726 n
mi
Hp = 216
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13959855
27 X = 4222707
78
Y = 1895918
17 feet Y = 625276
73 meter
Z = 17208316
09 Z = 5265685
62
XDOT = -397
455360 XDOT = -202
873155
YDOT = 25036
265145 feet/sec YDOT = 7629
242023 meter/sec
ZDOT = -2427
987204 ZDOT = -740
836442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4774950
48 X = -1455404
91
Y = -13133778
36 feet Y = -4003175
65 meter
Z = 17300344
54 Z = 5273145
02
XDOT = 21370
074359 XDOT = 6513
598665
YDOT = -10984
036043 feet/sec YDOT = -3347
934186 meter/sec
ZDOT = -2432
560155 ZDOT = -741
444335
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 18190
57822814
00016717 00000-0 10270-3 0 9014
2 25544 51
6403 267
1097 0003864 287
0411 73
0319 15
54043835 1997
Satellite: ISS
Catalog Number: 25544
Epoch time: 18190
57822814 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 267
1097 deg
Eccentricity:
0003864
Arg of perigee: 287
0411 deg
Mean anomaly: 73
0319 deg
Mean motion: 15
54043835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 199
Checksum: 305
Coasting Arc #3 (Orbit 206)
---------------------------------------
Vector Time (GMT): 2018/191/01:39:14
000
Vector Time (MET): N/A
Weight (LBS) : 959630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2590456
89 A = 6783247
05 meter
Y = 4931696
06 meter E =
0004206
Z = -3875370
46 I = 51
26048
XDOT = -3854
055905 Wp = 37
24704
YDOT = -5223
945033 meter/sec RA = 263
78484 deg
ZDOT = -4070
684775 TA = 189
82012
MA = 189
82834
Ha = 220
038 n
mi
Hp = 216
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8498874
32 X = -2626587
47
Y = 16180105
19 feet Y = 4902526
34 meter
Z = -12714470
01 Z = -3888041
02
XDOT = -12644
540370 XDOT = -3775
580661
YDOT = -17138
927273 feet/sec YDOT = -5266
604364 meter/sec
ZDOT = -13355
265011 ZDOT = -4089
216589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17664019
62 X = -5383993
18
Y = 4532900
96 feet Y = 1381628
21 meter
Z = -12771829
80 Z = -3892853
72
XDOT = 4713
638483 XDOT = 1436
717010
YDOT = -19501
672655 feet/sec YDOT = -5944
109825 meter/sec
ZDOT = -13437
446787 ZDOT = -4095
733781
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 18191
09268178
00016717 00000-0 10270-3 0 9020
2 25544 51
6402 264
5479 0004000 293
8282 66
2451 15
54012688 2078
Satellite: ISS
Catalog Number: 25544
Epoch time: 18191
09268178 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 264
5479 deg
Eccentricity:
0004000
Arg of perigee: 293
8282 deg
Mean anomaly: 66
2451 deg
Mean motion: 15
54012688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 207
Checksum: 302
Coasting Arc #4 (Orbit 218)
---------------------------------------
Vector Time (GMT): 2018/191/20:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 959612
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4347368
46 A = 6778845
54 meter
Y = -1292927
79 meter E =
0009340
Z = -5046399
47 I = 51
24760
XDOT = 129
413419 Wp = 97
89683
YDOT = -7446
035233 meter/sec RA = 259
82269 deg
ZDOT = 1797
853765 TA = 189
60695
MA = 189
62483
Ha = 220
112 n
mi
Hp = 216
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14263019
88 X = -4308074
83
Y = -4241889
06 feet Y = -1341322
55 meter
Z = -16556428
72 Z = -5067422
17
XDOT = 424
584708 XDOT = 203
934423
YDOT = -24429
249451 feet/sec YDOT = -7444
171657 meter/sec
ZDOT = 5898
470358 ZDOT = 1798
662217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11699404
70 X = 3565978
55
Y = -9024081
10 feet Y = -2750539
92 meter
Z = -16650302
72 Z = -5075012
27
XDOT = 18963
711451 XDOT = 5780
139250
YDOT = 13703
667255 feet/sec YDOT = 4176
877779 meter/sec
ZDOT = 5903
101586 ZDOT = 1799
265363
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 18191
86436125
00016717 00000-0 10270-3 0 9035
2 25544 51
6389 260
7003 0004006 296
8308 63
2434 15
53983968 2199
Satellite: ISS
Catalog Number: 25544
Epoch time: 18191
86436125 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 260
7003 deg
Eccentricity:
0004006
Arg of perigee: 296
8308 deg
Mean anomaly: 63
2434 deg
Mean motion: 15
53983968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 219
Checksum: 318
Coasting Arc #5 (Orbit 234)
---------------------------------------
Vector Time (GMT): 2018/192/20:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 959612
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4362015
81 A = 6781799
61 meter
Y = 2916448
86 meter E =
0007746
Z = 4294656
59 I = 51
26467
XDOT = -1066
917112 Wp = 48
54192
YDOT = 6744
905690 meter/sec RA = 254
80381 deg
ZDOT = -3487
589628 TA = 77
16941
MA = 77
08287
Ha = 220
187 n
mi
Hp = 216
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14311075
50 X = 4308218
11
Y = 9568401
76 feet Y = 2964926
40 meter
Z = 14090080
67 Z = 4315715
38
XDOT = -3500
384225 XDOT = -1125
320493
YDOT = 22128
955677 feet/sec YDOT = 6732
648719 meter/sec
ZDOT = -11442
223188 ZDOT = -3492
913014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15959095
87 X = -4864332
42
Y = 6246238
87 feet Y = 1903853
61 meter
Z = 14183910
84 Z = 4323256
02
XDOT = -15792
603979 XDOT = -4813
585693
YDOT = -14243
277095 feet/sec YDOT = -4341
350859 meter/sec
ZDOT = -11466
946168 ZDOT = -3495
125192
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 18192
89328745
00016717 00000-0 10270-3 0 9048
2 25544 51
6391 255
5727 0004062 302
0798 57
9959 15
53992355 2352
Satellite: ISS
Catalog Number: 25544
Epoch time: 18192
89328745 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 255
5727 deg
Eccentricity:
0004062
Arg of perigee: 302
0798 deg
Mean anomaly: 57
9959 deg
Mean motion: 15
53992355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 235
Checksum: 344
Coasting Arc #6 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2018/193/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 959612
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3327748
25 A = 6778488
76 meter
Y = 2928021
98 meter E =
0011387
Z = -5138397
71 I = 51
26032
XDOT = -3598
845067 Wp = 64
20268
YDOT = -6608
258689 meter/sec RA = 250
21292 deg
ZDOT = -1432
517796 TA = 191
91109
MA = 191
93804
Ha = 220
377 n
mi
Hp = 215
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10917809
22 X = -3335283
62
Y = 9606371
33 feet Y = 2890767
51 meter
Z = -16858260
22 Z = -5154580
35
XDOT = -11807
234473 XDOT = -3517
723918
YDOT = -21680
638743 feet/sec YDOT = -6648
049646 meter/sec
ZDOT = -4699
861534 ZDOT = -1449
803534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4858714
08 X = 1480936
05
Y = -13616681
15 feet Y = -4150364
41 meter
Z = -16931058
97 Z = -5160586
77
XDOT = 19754
726064 XDOT = 6021
240504
YDOT = 12997
489394 feet/sec YDOT = 3961
634767 meter/sec
ZDOT = -4776
337916 ZDOT = -1455
827797
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 18193
79359689
00016717 00000-0 10270-3 0 9050
2 25544 51
6372 251
0850 0004023 305
6072 54
4705 15
53981222 2497
Satellite: ISS
Catalog Number: 25544
Epoch time: 18193
79359689 = yrday
fracday
Element set: 905
Inclination: 51
6372 deg
RA of node: 251
0850 deg
Eccentricity:
0004023
Arg of perigee: 305
6072 deg
Mean anomaly: 54
4705 deg
Mean motion: 15
53981222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 311
Coasting Arc #7 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2018/194/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 959612
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4051176
01 A = 6777819
21 meter
Y = -1314935
12 meter E =
0003491
Z = 5273117
28 I = 51
27048
XDOT = 2884
906777 Wp = 349
79569
YDOT = 7090
749025 meter/sec RA = 245
18948 deg
ZDOT = -444
864295 TA = 104
48859
MA = 104
44986
Ha = 220
329 n
mi
Hp = 216
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13291259
86 X = 4039965
38
Y = -4314091
61 feet Y = -1269695
53 meter
Z = 17300253
54 Z = 5292768
67
XDOT = 9464
917247 XDOT = 2807
562533
YDOT = 23263
612287 feet/sec YDOT = 7122
577649 meter/sec
ZDOT = -1459
528528 ZDOT = -431
037519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9305838
15 X = -2836419
47
Y = 10276856
89 feet Y = 3132385
98 meter
Z = 17388367
85 Z = 5299974
52
XDOT = -19010
495450 XDOT = -5794
399013
YDOT = -14829
504564 feet/sec YDOT = -4520
032991 meter/sec
ZDOT = -1398
566629 ZDOT = -426
283109
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 18194
82252153
00016717 00000-0 10270-3 0 9064
2 25544 51
6373 245
9576 0004078 309
4123 50
6668 15
53987875 2658
Satellite: ISS
Catalog Number: 25544
Epoch time: 18194
82252153 = yrday
fracday
Element set: 906
Inclination: 51
6373 deg
RA of node: 245
9576 deg
Eccentricity:
0004078
Arg of perigee: 309
4123 deg
Mean anomaly: 50
6668 deg
Mean motion: 15
53987875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 336
Coasting Arc #8 (Orbit 279)
---------------------------------------
Vector Time (GMT): 2018/195/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 959612
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4687422
41 A = 6779451
04 meter
Y = -284286
41 meter E =
0008700
Z = -4897384
64 I = 51
29094
XDOT = -1944
544751 Wp = 94
53466
YDOT = -7053
250381 meter/sec RA = 240
16700 deg
ZDOT = 2273
434406 TA = 197
80045
MA = 197
83095
Ha = 220
505 n
mi
Hp = 215
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15378682
45 X = -4660106
70
Y = -932698
19 feet Y = -336551
09 meter
Z = -16067534
92 Z = -4920087
69
XDOT = -6379
739997 XDOT = -1876
571735
YDOT = -23140
585239 feet/sec YDOT = -7074
615830 meter/sec
ZDOT = 7458
774299 ZDOT = 2264
152954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13608237
02 X = 4147790
64
Y = -6993939
97 feet Y = -2131752
90 meter
Z = -16169111
51 Z = -4928345
19
XDOT = 16832
163415 XDOT = 5130
443409
YDOT = 15622
173896 feet/sec YDOT = 4761
638603 meter/sec
ZDOT = 7418
123255 ZDOT = 2261
043968
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 18195
78713554
00016717 00000-0 10270-3 0 9078
2 25544 51
6375 241
1493 0004143 312
7623 47
3181 15
53988749 2802
Satellite: ISS
Catalog Number: 25544
Epoch time: 18195
78713554 = yrday
fracday
Element set: 907
Inclination: 51
6375 deg
RA of node: 241
1493 deg
Eccentricity:
0004143
Arg of perigee: 312
7623 deg
Mean anomaly: 47
3181 deg
Mean motion: 15
53988749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 280
Checksum: 324
Coasting Arc #9 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2018/196/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5056577
15 A = 6786181
13 meter
Y = 3528843
42 meter E =
0010440
Z = 2825733
24 I = 51
32713
XDOT = -1108
395630 Wp = 86
13353
YDOT = 5653
605117 meter/sec RA = 236
42741 deg
ZDOT = -5060
014299 TA = 61
61687
MA = 61
51165
Ha = 220
580 n
mi
Hp = 215
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16589820
04 X = 5003015
24
Y = 11577570
27 feet Y = 3585089
80 meter
Z = 9270778
35 Z = 2850166
03
XDOT = -3636
468601 XDOT = -1146
955109
YDOT = 18548
573218 feet/sec YDOT = 5640
995161 meter/sec
ZDOT = -16601
096781 ZDOT = -5065
491483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1785711
04 X = 544284
73
Y = -20100795
92 feet Y = -6126722
60 meter
Z = 9379703
27 Z = 2858933
56
XDOT = 16366
740268 XDOT = 4988
582434
YDOT = -6329
977347 feet/sec YDOT = -1929
377095 meter/sec
ZDOT = -16626
313818 ZDOT = -5067
700452
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 18196
55882456
00016717 00000-0 10270-3 0 9083
2 25544 51
6381 237
3029 0003984 316
4506 43
6332 15
54020144 2921
Satellite: ISS
Catalog Number: 25544
Epoch time: 18196
55882456 = yrday
fracday
Element set: 908
Inclination: 51
6381 deg
RA of node: 237
3029 deg
Eccentricity:
0003984
Arg of perigee: 316
4506 deg
Mean anomaly: 43
6332 deg
Mean motion: 15
54020144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 292
Checksum: 308
Coasting Arc #10 (Orbit 294)
---------------------------------------
Vector Time (GMT): 2018/196/17:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4867780
71 A = 6780208
23 meter
Y = 437599
26 meter E =
0007781
Z = 4698799
98 I = 51
30838
XDOT = 2044
821345 Wp = 31
92590
YDOT = 6860
013970 meter/sec RA = 235
49108 deg
ZDOT = -2748
650432 TA = 85
45799
MA = 85
36912
Ha = 220
570 n
mi
Hp = 215
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15970409
15 X = 4839701
80
Y = 1435693
10 feet Y = 491876
71 meter
Z = 15416010
43 Z = 4722377
27
XDOT = 6708
731447 XDOT = 1981
309994
YDOT = 22506
607513 feet/sec YDOT = 6882
525711 meter/sec
ZDOT = -9017
881995 ZDOT = -2738
871253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15918211
47 X = -4851870
85
Y = 680003
75 feet Y = 207265
14 meter
Z = 15521491
53 Z = 4730950
62
XDOT = -9643
543748 XDOT = -2939
352134
YDOT = -20248
804037 feet/sec YDOT = -6171
835470 meter/sec
ZDOT = -8974
955880 ZDOT = -2735
566552
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 18196
75174797
00016717 00000-0 10270-3 0 9098
2 25544 51
6361 236
3413 0004153 317
4737 42
6094 15
54000674 2954
Satellite: ISS
Catalog Number: 25544
Epoch time: 18196
75174797 = yrday
fracday
Element set: 909
Inclination: 51
6361 deg
RA of node: 236
3413 deg
Eccentricity:
0004153
Arg of perigee: 317
4737 deg
Mean anomaly: 42
6094 deg
Mean motion: 15
54000674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 295
Checksum: 316
Coasting Arc #11 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2018/197/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -733778
01 A = 6784016
77 meter
Y = -5643750
09 meter E =
0009632
Z = 3682237
58 I = 51
33787
XDOT = 6019
892588 Wp = 77
88672
YDOT = 2028
291233 meter/sec RA = 231
41793 deg
ZDOT = 4300
805905 TA = 326
19461
MA = 326
25599
Ha = 220
816 n
mi
Hp = 215
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2407408
17 X = -688499
50
Y = -18516240
47 feet Y = -5651702
80 meter
Z = 12080831
96 Z = 3678782
78
XDOT = 19750
303767 XDOT = 5975
873666
YDOT = 6654
498796 feet/sec YDOT = 2095
363395 meter/sec
ZDOT = 14110
255594 ZDOT = 4329
941074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13810220
24 X = -4209355
13
Y = 12580998
15 feet Y = 3834688
24 meter
Z = 12066050
65 Z = 3677732
24
XDOT = -4794
180033 XDOT = -1461
266074
YDOT = -18943
979724 feet/sec YDOT = -5774
125020 meter/sec
ZDOT = 14240
432167 ZDOT = 4340
483725
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 18197
58774573
00016717 00000-0 10270-3 0 9100
2 25544 51
6373 232
1740 0003866 322
8137 37
2747 15
53981772 3084
Satellite: ISS
Catalog Number: 25544
Epoch time: 18197
58774573 = yrday
fracday
Element set: 910
Inclination: 51
6373 deg
RA of node: 232
1740 deg
Eccentricity:
0003866
Arg of perigee: 322
8137 deg
Mean anomaly: 37
2747 deg
Mean motion: 15
53981772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 328
Coasting Arc #12 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2018/198/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -539139
49 A = 6780366
92 meter
Y = 4875134
82 meter E =
0010269
Z = -4691254
06 I = 51
34860
XDOT = -6287
005203 Wp = 49
41990
YDOT = -3375
960057 meter/sec RA = 226
40985 deg
ZDOT = -2783
224459 TA = 192
83886
MA = 192
86503
Ha = 220
828 n
mi
Hp = 215
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1768830
36 X = -570827
29
Y = 15994536
81 feet Y = 4868928
88 meter
Z = -15391253
48 Z = -4693949
65
XDOT = -20626
657490 XDOT = -6235
267831
YDOT = -11075
984439 feet/sec YDOT = -3445
976252 meter/sec
ZDOT = -9131
313842 ZDOT = -2813
638545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13965081
19 X = 4256556
75
Y = -7971261
57 feet Y = -2429640
53 meter
Z = -15403900
44 Z = -4695108
85
XDOT = 2411
115117 XDOT = 734
907888
YDOT = 22148
098261 feet/sec YDOT = 6750
740350 meter/sec
ZDOT = -9267
071660 ZDOT = -2824
603442
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 18198
55235561
00016717 00000-0 10270-3 0 9118
2 25544 51
6386 227
3668 0003950 323
3857 36
7025 15
54003064 3232
Satellite: ISS
Catalog Number: 25544
Epoch time: 18198
55235561 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 227
3668 deg
Eccentricity:
0003950
Arg of perigee: 323
3857 deg
Mean anomaly: 36
7025 deg
Mean motion: 15
54003064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 304
Coasting Arc #13 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2018/199/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3658567
87 A = 6788058
07 meter
Y = -5350275
55 meter E =
0013941
Z = 1988770
93 I = 51
39751
XDOT = 5098
518819 Wp = 51
39797
YDOT = -1414
579595 meter/sec RA = 221
45553 deg
ZDOT = 5555
886070 TA = 330
64828
MA = 330
72652
Ha = 220
998 n
mi
Hp = 215
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12003175
41 X = -3608127
97
Y = -17553397
48 feet Y = -5390906
26 meter
Z = 6524839
01 Z = 1971121
35
XDOT = 16727
423948 XDOT = 5086
970918
YDOT = -4641
009169 feet/sec YDOT = -1357
629294 meter/sec
ZDOT = 18227
972672 ZDOT = 5580
624444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8197154
59 X = -2498492
72
Y = 19647430
61 feet Y = 5988536
85 meter
Z = 6446443
55 Z = 1964876
00
XDOT = -11481
296302 XDOT = -3499
499113
YDOT = -10826
696238 feet/sec YDOT = -3299
977013 meter/sec
ZDOT = 18338
897006 ZDOT = 5589
695807
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 18199
58127174
00016717 00000-0 10270-3 0 9123
2 25544 51
6385 222
2381 0004071 329
6042 30
4874 15
54004005 3393
Satellite: ISS
Catalog Number: 25544
Epoch time: 18199
58127174 = yrday
fracday
Element set: 912
Inclination: 51
6385 deg
RA of node: 222
2381 deg
Eccentricity:
0004071
Arg of perigee: 329
6042 deg
Mean anomaly: 30
4874 deg
Mean motion: 15
54004005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 290
Coasting Arc #14 (Orbit 353)
---------------------------------------
Vector Time (GMT): 2018/200/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2537043
98 A = 6784772
90 meter
Y = 5279005
11 meter E =
0004669
Z = -3430984
62 I = 51
41073
XDOT = -6150
608571 Wp = 40
07854
YDOT = -12
804208 meter/sec RA = 216
46245 deg
ZDOT = -4567
746552 TA = 180
21165
MA = 180
21184
Ha = 221
079 n
mi
Hp = 215
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8323635
10 X = 2494489
87
Y = 17319570
58 feet Y = 5307138
35 meter
Z = -11256511
23 Z = -3418763
73
XDOT = -20179
161979 XDOT = -6127
820796
YDOT = -42
008555 feet/sec YDOT = -81
456888 meter/sec
ZDOT = -14986
045118 ZDOT = -4597
568420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9697077
24 X = 2955669
14
Y = -16626256
25 feet Y = -5067682
91 meter
Z = -11202400
08 Z = -3414491
54
XDOT = 9944
495414 XDOT = 3031
082202
YDOT = 15987
305224 feet/sec YDOT = 4872
930632 meter/sec
ZDOT = -15119
574927 ZDOT = -4608
446438
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 18200
54587958
00016717 00000-0 10270-3 0 9133
2 25544 51
6373 217
4307 0004056 332
3702 27
7234 15
53997227 3543
Satellite: ISS
Catalog Number: 25544
Epoch time: 18200
54587958 = yrday
fracday
Element set: 913
Inclination: 51
6373 deg
RA of node: 217
4307 deg
Eccentricity:
0004056
Arg of perigee: 332
3702 deg
Mean anomaly: 27
7234 deg
Mean motion: 15
53997227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 354
Checksum: 310
Coasting Arc #15 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2018/201/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1149281
64 A = 6781098
76 meter
Y = -4923302
40 meter E =
0006584
Z = 4513326
22 I = 51
42483
XDOT = 6882
221546 Wp = 86
45773
YDOT = 1275
088609 meter/sec RA = 211
46076 deg
ZDOT = 3139
851415 TA = 331
95476
MA = 331
99021
Ha = 221
196 n
mi
Hp = 215
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3770609
07 X = -1116065
68
Y = -16152566
93 feet Y = -4935969
04 meter
Z = 14807500
73 Z = 4507823
80
XDOT = 22579
467016 XDOT = 6852
200038
YDOT = 4183
361577 feet/sec YDOT = 1351
882293 meter/sec
ZDOT = 10301
349788 ZDOT = 3173
209762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11040980
15 X = -3365290
75
Y = 12406939
07 feet Y = 3781635
03 meter
Z = 14783423
46 Z = 4505987
47
XDOT = -8529
758699 XDOT = -2599
870452
YDOT = -20056
958469 feet/sec YDOT = -6113
360941 meter/sec
ZDOT = 10450
586034 ZDOT = 3185
338623
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 18201
57479432
00016717 00000-0 10270-3 0 9145
2 25544 51
6365 212
3020 0004168 336
3106 23
7855 15
53994197 3702
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
57479432 = yrday
fracday
Element set: 914
Inclination: 51
6365 deg
RA of node: 212
3020 deg
Eccentricity:
0004168
Arg of perigee: 336
3106 deg
Mean anomaly: 23
7855 deg
Mean motion: 15
53994197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 301
Coasting Arc #16 (Orbit 384)
---------------------------------------
Vector Time (GMT): 2018/202/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -421310
80 A = 6778415
52 meter
Y = 4386237
00 meter E =
0013841
Z = -5162718
13 I = 51
44517
XDOT = -7162
522107 Wp = 62
26202
YDOT = -2327
106517 meter/sec RA = 206
45276 deg
ZDOT = -1389
150273 TA = 194
30586
MA = 194
34510
Ha = 221
308 n
mi
Hp = 215
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1382253
27 X = -445250
01
Y = 14390541
35 feet Y = 4381392
18 meter
Z = -16938051
60 Z = -5164822
49
XDOT = -23499
088279 XDOT = -7129
219720
YDOT = -7634
863901 feet/sec YDOT = -2407
016470 meter/sec
ZDOT = -4557
579637 ZDOT = -1423
862373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12407020
84 X = 3781659
95
Y = -7397830
32 feet Y = -2254858
68 meter
Z = -16947974
42 Z = -5165742
60
XDOT = 7016
085843 XDOT = 2138
502965
YDOT = 22589
377820 feet/sec YDOT = 6885
242359 meter/sec
ZDOT = -4712
778345 ZDOT = -1436
454840
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 18202
53939933
00016717 00000-0 10270-3 0 9150
2 25544 51
6370 207
4946 0004139 341
1353 18
9645 15
54000943 3853
Satellite: ISS
Catalog Number: 25544
Epoch time: 18202
53939933 = yrday
fracday
Element set: 915
Inclination: 51
6370 deg
RA of node: 207
4946 deg
Eccentricity:
0004139
Arg of perigee: 341
1353 deg
Mean anomaly: 18
9645 deg
Mean motion: 15
54000943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 385
Checksum: 307
Coasting Arc #17 (Orbit 400)
---------------------------------------
Vector Time (GMT): 2018/203/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2068355
88 A = 6777769
15 meter
Y = -3706973
07 meter E =
0005194
Z = 5282976
75 I = 51
47185
XDOT = 6967
664560 Wp = 15
13768
YDOT = 3165
588906 meter/sec RA = 201
44164 deg
ZDOT = -501
667721 TA = 79
68789
MA = 79
62933
Ha = 221
295 n
mi
Hp = 215
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6785944
48 X = 2083992
84
Y = -12161985
14 feet Y = -3683756
35 meter
Z = 17332600
88 Z = 5293061
66
XDOT = 22859
791865 XDOT = 6934
185042
YDOT = 10385
790375 feet/sec YDOT = 3243
318994 meter/sec
ZDOT = -1645
891473 ZDOT = -467
902510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13732175
61 X = -4185567
13
Y = 1951350
04 feet Y = 594771
49 meter
Z = 17378192
20 Z = 5296872
98
XDOT = -5256
317742 XDOT = -1602
125648
YDOT = -23529
504786 feet/sec YDOT = -7171
793059 meter/sec
ZDOT = -1495
006366 ZDOT = -455
677940
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 18203
56830984
00016717 00000-0 10270-3 0 9161
2 25544 51
6356 202
3660 0004292 343
5312 16
5701 15
54007883 4011
Satellite: ISS
Catalog Number: 25544
Epoch time: 18203
56830984 = yrday
fracday
Element set: 916
Inclination: 51
6356 deg
RA of node: 202
3660 deg
Eccentricity:
0004292
Arg of perigee: 343
5312 deg
Mean anomaly: 16
5701 deg
Mean motion: 15
54007883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 401
Checksum: 286
Coasting Arc #18 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2018/203/19:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3062842
48 A = 6782872
49 meter
Y = 4527574
61 meter E =
0008283
Z = -4025260
80 I = 51
50127
XDOT = -6519
280070 Wp = 40
24373
YDOT = 930
921932 meter/sec RA = 200
06836 deg
ZDOT = -3911
785277 TA = 189
01443
MA = 189
02931
Ha = 221
390 n
mi
Hp = 215
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10048695
79 X = 3031538
68
Y = 14854247
40 feet Y = 4561650
78 meter
Z = -13206236
23 Z = -4010458
29
XDOT = -21388
714140 XDOT = -6510
204143
YDOT = 3054
205813 feet/sec YDOT = 858
069964 meter/sec
ZDOT = -12833
941196 ZDOT = -3943
431281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17835313
46 X = -5436203
54
Y = -2293481
66 feet Y = -699053
21 meter
Z = -13140440
02 Z = -4005206
12
XDOT = 11705
139138 XDOT = 3567
726409
YDOT = -16649
091761 feet/sec YDOT = -5074
643169 meter/sec
ZDOT = -12975
801804 ZDOT = -3955
024390
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 18203
82553790
00016717 00000-0 10270-3 0 9178
2 25544 51
6394 201
0858 0004461 342
9708 17
1294 15
54014282 4057
Satellite: ISS
Catalog Number: 25544
Epoch time: 18203
82553790 = yrday
fracday
Element set: 917
Inclination: 51
6394 deg
RA of node: 201
0858 deg
Eccentricity:
0004461
Arg of perigee: 342
9708 deg
Mean anomaly: 17
1294 deg
Mean motion: 15
54014282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 299
Coasting Arc #19 (Orbit 420)
---------------------------------------
Vector Time (GMT): 2018/204/19:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1499303
87 A = 6779536
22 meter
Y = -4435703
98 meter E =
0004923
Z = 4898444
86 I = 51
52153
XDOT = 7316
770871 Wp = 81
07972
YDOT = 73
085956 meter/sec RA = 195
06876 deg
ZDOT = 2304
448439 TA = 346
34924
MA = 346
36255
Ha = 221
531 n
mi
Hp = 215
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4918975
95 X = -1473384
98
Y = -14552834
57 feet Y = -4452325
83 meter
Z = 16071013
32 Z = 4891224
32
XDOT = 24005
153776 XDOT = 7304
216135
YDOT = 239
783320 feet/sec YDOT = 154
836698 meter/sec
ZDOT = 7560
526374 ZDOT = 2339
959914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14313896
77 X = 4362875
74
Y = 5667135
45 feet Y = 1727342
89 meter
Z = 16039162
16 Z = 4888736
63
XDOT = -15374
652849 XDOT = -4686
194188
YDOT = 16973
318240 feet/sec YDOT = 5173
467400 meter/sec
ZDOT = 7719
612662 ZDOT = 2352
937939
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 18204
85444811
00016717 00000-0 10270-3 0 9186
2 25544 51
6395 195
9572 0004414 347
8076 12
2969 15
54005416 4214
Satellite: ISS
Catalog Number: 25544
Epoch time: 18204
85444811 = yrday
fracday
Element set: 918
Inclination: 51
6395 deg
RA of node: 195
9572 deg
Eccentricity:
0004414
Arg of perigee: 347
8076 deg
Mean anomaly: 12
2969 deg
Mean motion: 15
54005416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 421
Checksum: 314
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