[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 24th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15476 3504 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
207/15:56:39
616 -1
2 1
3 1
3
N/A 0
4 -0
1 221
8
000/00:03:19
233 -0
3 -0
0 215
4
209/20:18:00
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
3
212/23:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 214
9
215/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 214
7
216/02:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
6
Coasting Arc #1 (Orbit 415)
---------------------------------------
Vector Time (GMT): 2018/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6579758
58 A = 6789585
51 meter
Y = 1607696
33 meter E =
0009934
Z = 419997
33 I = 51
54169
XDOT = -766
900772 Wp = 114
25437
YDOT = 4729
981075 meter/sec RA = 196
55353 deg
ZDOT = -5983
567511 TA = 61
21257
MA = 61
11284
Ha = 221
545 n
mi
Hp = 214
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21587134
45 X = 6559251
75
Y = 5274594
26 feet Y = 1681161
03 meter
Z = 1377943
98 Z = 451909
56
XDOT = -2516
078647 XDOT = -790
671001
YDOT = 15518
310615 feet/sec YDOT = 4721
272773 meter/sec
ZDOT = -19631
127004 ZDOT = -5987
350056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6332289
37 X = -1930081
80
Y = -21291170
71 feet Y = -6489548
83 meter
Z = 1520726
43 Z = 463517
42
XDOT = 13048
224844 XDOT = 3977
098932
YDOT = -5307
014745 feet/sec YDOT = -1617
578094 meter/sec
ZDOT = -19648
603544 ZDOT = -5988
894360
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
53308212
00016717 00000-0 10270-3 0 9006
2 25544 51
6355 197
5591 0004355 349
6100 10
4961 15
54008321 4165
Satellite: ISS
Catalog Number: 25544
Epoch time: 18204
53308212 = yrday
fracday
Element set: 900
Inclination: 51
6355 deg
RA of node: 197
5591 deg
Eccentricity:
0004355
Arg of perigee: 349
6100 deg
Mean anomaly: 10
4961 deg
Mean motion: 15
54008321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 416
Checksum: 275
Coasting Arc #2 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2018/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6264008
56 A = 6788940
78 meter
Y = -2281949
20 meter E =
0015802
Z = 1232984
73 I = 51
57223
XDOT = 2681
826286 Wp = 44
77417
YDOT = -4184
541312 meter/sec RA = 191
57882 deg
ZDOT = 5845
460356 TA = 328
64934
MA = 328
74345
Ha = 221
474 n
mi
Hp = 214
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20551209
20 X = -6244014
74
Y = -7486709
99 feet Y = -2351886
02 meter
Z = 4045225
48 Z = 1202605
04
XDOT = 8798
642671 XDOT = 2700
025861
YDOT = -13728
810079 feet/sec YDOT = -4154
450156 meter/sec
ZDOT = 19178
019542 ZDOT = 5858
531322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4288239
20 X = 1307055
31
Y = 21473117
35 feet Y = 6545006
17 meter
Z = 3909361
97 Z = 1191573
53
XDOT = -14668
355677 XDOT = -4470
914810
YDOT = -594
366266 feet/sec YDOT = -181
162838 meter/sec
ZDOT = 19237
052401 ZDOT = 5863
453572
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 18205
56199622
00016717 00000-0 10270-3 0 9014
2 25544 51
6358 192
4311 0004098 351
8373 8
2712 15
54057066 4320
Satellite: ISS
Catalog Number: 25544
Epoch time: 18205
56199622 = yrday
fracday
Element set: 901
Inclination: 51
6358 deg
RA of node: 192
4311 deg
Eccentricity:
0004098
Arg of perigee: 351
8373 deg
Mean anomaly: 8
2712 deg
Mean motion: 15
54057066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 298
Coasting Arc #3 (Orbit 446)
---------------------------------------
Vector Time (GMT): 2018/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5482887
58 A = 6786452
23 meter
Y = 2865483
31 meter E =
0004304
Z = -2795801
46 I = 51
59601
XDOT = -4463
303831 Wp = 63
70587
YDOT = 3560
071724 meter/sec RA = 186
60063 deg
ZDOT = -5108
494153 TA = 147
99686
MA = 147
97071
Ha = 221
748 n
mi
Hp = 214
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17988476
31 X = 5464017
77
Y = 9401191
96 feet Y = 2926691
54 meter
Z = -9172576
95 Z = -2769213
43
XDOT = -14643
385271 XDOT = -4477
967836
YDOT = 11680
025340 feet/sec YDOT = 3510
078539 meter/sec
ZDOT = -16760
151419 ZDOT = -5130
210227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1688441
14 X = -514636
86
Y = -20280105
92 feet Y = -6181376
29 meter
Z = -9053746
65 Z = -2759581
98
XDOT = 16154
807846 XDOT = 4923
985432
YDOT = 6174
653478 feet/sec YDOT = 1882
034380 meter/sec
ZDOT = -16857
862769 ZDOT = -5138
276572
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 18206
52660471
00016717 00000-0 10270-3 0 9027
2 25544 51
6358 187
6224 0004458 357
2018 2
9109 15
54007630 4474
Satellite: ISS
Catalog Number: 25544
Epoch time: 18206
52660471 = yrday
fracday
Element set: 902
Inclination: 51
6358 deg
RA of node: 187
6224 deg
Eccentricity:
0004458
Arg of perigee: 357
2018 deg
Mean anomaly: 2
9109 deg
Mean motion: 15
54007630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 447
Checksum: 295
Coasting Arc #4 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2018/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4283977
60 A = 6782700
89 meter
Y = -3334700
77 meter E =
0010606
Z = 4055486
78 I = 51
61645
XDOT = 5945
281211 Wp = 78
73598
YDOT = -2908
459450 meter/sec RA = 181
61756 deg
ZDOT = 3882
130508 TA = 331
03612
MA = 331
09493
Ha = 221
774 n
mi
Hp = 214
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14055044
63 X = -4266068
72
Y = -10940619
32 feet Y = -3382507
44 meter
Z = 13305402
81 Z = 4034720
24
XDOT = 19505
515785 XDOT = 5958
505555
YDOT = -9542
189797 feet/sec YDOT = -2841
901660 meter/sec
ZDOT = 12736
648649 ZDOT = 3911
041913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1391971
77 X = -424273
00
Y = 17825887
66 feet Y = 5433330
56 meter
Z = 13212695
36 Z = 4027229
54
XDOT = -17328
755895 XDOT = -5281
804797
YDOT = -10906
056600 feet/sec YDOT = -3324
166052 meter/sec
ZDOT = 12866
550538 ZDOT = 3921
724604
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 18207
55551536
00016717 00000-0 10270-3 0 9033
2 25544 51
6356 182
4947 0004353 357
9428 2
1706 15
54039474 4637
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
55551536 = yrday
fracday
Element set: 903
Inclination: 51
6356 deg
RA of node: 182
4947 deg
Eccentricity:
0004353
Arg of perigee: 357
9428 deg
Mean anomaly: 2
1706 deg
Mean motion: 15
54039474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 314
Coasting Arc #5 (Orbit 464)
---------------------------------------
Vector Time (GMT): 2018/207/15:58:19
233
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1555298
35 A = 6779078
09 meter
Y = 4116751
72 meter E =
0014268
Z = -5168785
85 I = 51
61028
XDOT = -7453
939220 Wp = 61
78972
YDOT = 1025
685132 meter/sec RA = 180
77920 deg
ZDOT = -1422
391490 TA = 194
48094
MA = 194
52186
Ha = 221
826 n
mi
Hp = 215
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5102684
87 X = 1534254
86
Y = 13506403
27 feet Y = 4134026
99 meter
Z = -16957958
82 Z = -5161281
59
XDOT = -24455
181167 XDOT = -7457
945630
YDOT = 3365
108701 feet/sec YDOT = 942
307776 meter/sec
ZDOT = -4666
638748 ZDOT = -1458
609085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5914781
52 X = -1802825
41
Y = -13213627
19 feet Y = -4027513
57 meter
Z = -16924777
85 Z = -5158672
29
XDOT = 23250
546106 XDOT = 7086
766453
YDOT = -4207
083942 feet/sec YDOT = -1282
319186 meter/sec
ZDOT = -4829
083280 ZDOT = -1471
904584
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 18207
68413213
00016717 00000-0 10270-3 0 9047
2 25544 51
6384 181
8537 0004291 347
0921 13
0121 15
53785217 4651
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
68413213 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 181
8537 deg
Eccentricity:
0004291
Arg of perigee: 347
0921 deg
Mean anomaly: 13
0121 deg
Mean motion: 15
53785217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 465
Checksum: 292
Coasting Arc #6 (Orbit 480)
---------------------------------------
Vector Time (GMT): 2018/208/15:58:19
233
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 121226
40 A = 6778305
53 meter
Y = -4217758
94 meter E =
0005133
Z = 5303727
41 I = 51
64155
XDOT = 7655
518506 Wp = 18
00161
YDOT = -263
336138 meter/sec RA = 175
78269 deg
ZDOT = -379
524917 TA = 75
64507
MA = 75
58810
Ha = 221
775 n
mi
Hp = 215
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 397724
40 X = 142619
37
Y = -13837791
79 feet Y = -4216284
14 meter
Z = 17400680
47 Z = 5304367
87
XDOT = 25116
530531 XDOT = 7659
737727
YDOT = -863
963708 feet/sec YDOT = -177
703219 meter/sec
ZDOT = -1245
160488 ZDOT = -342
327622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 680181
70 X = 207319
38
Y = 13822590
57 feet Y = 4213125
61 meter
Z = 17404013
62 Z = 5304743
35
XDOT = -23995
458736 XDOT = -7313
815823
YDOT = 2558
683957 feet/sec YDOT = 779
886870 meter/sec
ZDOT = -1078
383541 ZDOT = -328
691303
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 18208
71320025
00016717 00000-0 10270-3 0 9051
2 25544 51
6389 176
7267 0004334 347
7256 12
3790 15
53811815 4811
Satellite: ISS
Catalog Number: 25544
Epoch time: 18208
71320025 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 176
7267 deg
Eccentricity:
0004334
Arg of perigee: 347
7256 deg
Mean anomaly: 12
3790 deg
Mean motion: 15
53811815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 481
Checksum: 306
Coasting Arc #7 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2018/209/15:58:19
233
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1752306
56 A = 6779807
83 meter
Y = 4268810
14 meter E =
0011686
Z = -4976905
86 I = 51
68048
XDOT = -7336
048707 Wp = 85
47761
YDOT = -523
232932 meter/sec RA = 170
78911 deg
ZDOT = 2139
373446 TA = 205
34873
MA = 205
40611
Ha = 221
985 n
mi
Hp = 215
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5749037
25 X = -1775736
69
Y = 14005282
60 feet Y = 4249083
98 meter
Z = -16328431
29 Z = -4985474
37
XDOT = -24068
401271 XDOT = -7340
044263
YDOT = -1716
643479 feet/sec YDOT = -605
292188 meter/sec
ZDOT = 7018
941752 ZDOT = 2103
728514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4405779
40 X = 1342881
56
Y = -14440125
50 feet Y = -4401350
25 meter
Z = -16367312
61 Z = -4988756
88
XDOT = 23119
462431 XDOT = 7046
812149
YDOT = -701
306147 feet/sec YDOT = -213
758114 meter/sec
ZDOT = 6859
186494 ZDOT = 2090
680043
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 18209
67795115
00016717 00000-0 10270-3 0 9064
2 25544 51
6401 171
9197 0004398 353
3580 6
7513 15
53781550 4966
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
67795115 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 171
9197 deg
Eccentricity:
0004398
Arg of perigee: 353
3580 deg
Mean anomaly: 6
7513 deg
Mean motion: 15
53781550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 324
Coasting Arc #8 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2018/209/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5573435
11 A = 6785410
34 meter
Y = 1775261
59 meter E =
0006119
Z = -3447203
83 I = 51
70130
XDOT = -4246
004892 Wp = 45
22399
YDOT = 4430
623174 meter/sec RA = 169
93139 deg
ZDOT = -4584
017833 TA = 175
08824
MA = 175
08223
Ha = 221
983 n
mi
Hp = 215
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18285548
25 X = 5569913
74
Y = 5824349
05 feet Y = 1837568
13 meter
Z = -11309723
85 Z = -3420139
05
XDOT = -13930
462243 XDOT = -4272
967529
YDOT = 14536
165268 feet/sec YDOT = 4382
990963 meter/sec
ZDOT = -15039
428586 ZDOT = -4604
708183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11733476
90 X = -3576363
76
Y = 15275325
90 feet Y = 4655919
34 meter
Z = -11188570
44 Z = -3410276
27
XDOT = -7835
880487 XDOT = -2388
376373
YDOT = -17101
160388 feet/sec YDOT = -5212
433686 meter/sec
ZDOT = -15132
676835 ZDOT = -4612
439899
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 18209
87089944
00016717 00000-0 10270-3 0 9073
2 25544 51
6365 170
9564 0004396 352
8983 7
2110 15
53782997 4999
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
87089944 = yrday
fracday
Element set: 907
Inclination: 51
6365 deg
RA of node: 170
9564 deg
Eccentricity:
0004396
Arg of perigee: 352
8983 deg
Mean anomaly: 7
2110 deg
Mean motion: 15
53782997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 356
Coasting Arc #9 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2018/210/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4429414
32 A = 6781945
00 meter
Y = -2478539
60 meter E =
0008209
Z = 4490401
50 I = 51
72176
XDOT = 5593
792875 Wp = 82
96929
YDOT = -4141
476498 meter/sec RA = 164
95217 deg
ZDOT = 3227
800606 TA = 334
60284
MA = 334
64316
Ha = 222
180 n
mi
Hp = 215
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14532199
20 X = -4423180
93
Y = -8131691
62 feet Y = -2528037
74 meter
Z = 14732288
38 Z = 4468900
43
XDOT = 18352
338828 XDOT = 5624
009659
YDOT = -13587
521319 feet/sec YDOT = -4078
754047 meter/sec
ZDOT = 10589
897002 ZDOT = 3255
045905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12439894
87 X = 3791679
96
Y = -11197405
15 feet Y = -3412969
09 meter
Z = 14636142
81 Z = 4461096
33
XDOT = 6098
678887 XDOT = 1858
877325
YDOT = 20795
331269 feet/sec YDOT = 6338
416971 meter/sec
ZDOT = 10712
517178 ZDOT = 3265
175236
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 18210
89996503
00016717 00000-0 10270-3 0 9086
2 25544 51
6364 165
8288 0004368 355
3963 4
7148 15
53761907 5159
Satellite: ISS
Catalog Number: 25544
Epoch time: 18210
89996503 = yrday
fracday
Element set: 908
Inclination: 51
6364 deg
RA of node: 165
8288 deg
Eccentricity:
0004368
Arg of perigee: 355
3963 deg
Mean anomaly: 4
7148 deg
Mean motion: 15
53761907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 339
Coasting Arc #10 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2018/211/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3053688
77 A = 6779216
06 meter
Y = 3206045
82 meter E =
0015026
Z = -5146737
98 I = 51
74457
XDOT = -6522
052998 Wp = 62
30997
YDOT = 3692
584140 meter/sec RA = 159
96663 deg
ZDOT = -1566
176369 TA = 192
57231
MA = 192
60983
Ha = 222
118 n
mi
Hp = 215
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10018663
96 X = 3042610
56
Y = 10518523
02 feet Y = 3240132
50 meter
Z = -16885623
30 Z = -5131931
32
XDOT = -21397
811674 XDOT = -6555
252259
YDOT = 12114
777362 feet/sec YDOT = 3619
464457 meter/sec
ZDOT = -5138
373914 ZDOT = -1597
938115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13128502
52 X = -4001567
57
Y = 6393890
42 feet Y = 1948857
80 meter
Z = -16819566
44 Z = -5126603
85
XDOT = -4470
455168 XDOT = -1362
594735
YDOT = -23100
393066 feet/sec YDOT = -7040
999806 meter/sec
ZDOT = -5281
213791 ZDOT = -1609
713964
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 18211
86471104
00016717 00000-0 10270-3 0 9090
2 25544 51
6364 161
0215 0004235
5529 359
5628 15
53786643 5302
Satellite: ISS
Catalog Number: 25544
Epoch time: 18211
86471104 = yrday
fracday
Element set: 909
Inclination: 51
6364 deg
RA of node: 161
0215 deg
Eccentricity:
0004235
Arg of perigee:
5529 deg
Mean anomaly: 359
5628 deg
Mean motion: 15
53786643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 296
Coasting Arc #11 (Orbit 545)
---------------------------------------
Vector Time (GMT): 2018/212/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1526392
51 A = 6778455
42 meter
Y = -3911402
36 meter E =
0005423
Z = 5319227
05 I = 51
77277
XDOT = 7024
496453 Wp = 31
50606
YDOT = -3071
623547 meter/sec RA = 154
97854 deg
ZDOT = -238
309056 TA = 60
78766
MA = 60
73343
Ha = 222
305 n
mi
Hp = 214
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5007849
44 X = -1508378
23
Y = -12832684
92 feet Y = -3928370
92 meter
Z = 17451532
32 Z = 5311856
17
XDOT = 23046
248205 XDOT = 7059
479683
YDOT = -10077
505076 feet/sec YDOT = -2992
875164 meter/sec
ZDOT = -781
853859 ZDOT = -204
102178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13768147
24 X = 4196531
28
Y = -1154360
23 feet Y = -351849
00 meter
Z = 17418895
28 Z = 5309279
28
XDOT = 2824
828659 XDOT = 861
007775
YDOT = 23984
811076 feet/sec YDOT = 7310
570416 meter/sec
ZDOT = -628
098760 ZDOT = -191
444502
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 18212
89377156
00016717 00000-0 10270-3 0 9108
2 25544 51
6367 155
8936 0004273 5
0858 355
0337 15
53751986 5460
Satellite: ISS
Catalog Number: 25544
Epoch time: 18212
89377156 = yrday
fracday
Element set: 910
Inclination: 51
6367 deg
RA of node: 155
8936 deg
Eccentricity:
0004273
Arg of perigee: 5
0858 deg
Mean anomaly: 355
0337 deg
Mean motion: 15
53751986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 546
Checksum: 332
Coasting Arc #12 (Orbit 547)
---------------------------------------
Vector Time (GMT): 2018/212/23:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1875234
44 A = 6778319
51 meter
Y = -3750114
45 meter E =
0004723
Z = 5323472
52 I = 51
77909
XDOT = 6893
013072 Wp = 36
88063
YDOT = -3364
761025 meter/sec RA = 154
34274 deg
ZDOT = 61
474996 TA = 52
55635
MA = 52
51340
Ha = 222
203 n
mi
Hp = 214
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6152343
95 X = -1859018
43
Y = -12303525
09 feet Y = -3770994
04 meter
Z = 17465461
02 Z = 5314402
75
XDOT = 22614
872283 XDOT = 6929
827851
YDOT = -11039
242209 feet/sec YDOT = -3287
472745 meter/sec
ZDOT = 201
689621 ZDOT = 95
047646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7665448
67 X = 2336428
75
Y = -11483648
01 feet Y = -3500215
91 meter
Z = 17425186
35 Z = 5311196
80
XDOT = 19850
242477 XDOT = 6050
353907
YDOT = 13767
053990 feet/sec YDOT = 4196
198056 meter/sec
ZDOT = 352
633839 ZDOT = 107
482794
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 18213
02240363
00016717 00000-0 10270-3 0 9114
2 25544 51
6392 155
2513 0004032 5
7476 354
3722 15
53795212 5481
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
02240363 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 155
2513 deg
Eccentricity:
0004032
Arg of perigee: 5
7476 deg
Mean anomaly: 354
3722 deg
Mean motion: 15
53795212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 548
Checksum: 279
Coasting Arc #13 (Orbit 562)
---------------------------------------
Vector Time (GMT): 2018/213/23:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 373898
74 A = 6779228
98 meter
Y = 4451331
85 meter E =
0013809
Z = -5111065
92 I = 51
81120
XDOT = -7004
264941 Wp = 86
50235
YDOT = 2568
174153 meter/sec RA = 149
35925 deg
ZDOT = 1729
128137 TA = 200
16535
MA = 200
21995
Ha = 222
208 n
mi
Hp = 214
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1226701
92 X = 348921
46
Y = 14604107
13 feet Y = 4455373
45 meter
Z = -16768588
96 Z = -5109310
28
XDOT = -22979
871855 XDOT = -7040
861483
YDOT = 8425
768220 feet/sec YDOT = 2489
642977 meter/sec
ZDOT = 5672
992577 ZDOT = 1695
015456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11938520
31 X = -3638860
99
Y = 8514947
52 feet Y = 2595356
00 meter
Z = -16761196
86 Z = -5108812
80
XDOT = -18256
750996 XDOT = -5564
657704
YDOT = -14763
284523 feet/sec YDOT = -4499
849123 meter/sec
ZDOT = 5519
696007 ZDOT = 1682
403343
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 18213
98714466
00016717 00000-0 10270-3 0 9120
2 25544 51
6388 150
4460 0003946 10
2509 349
8723 15
53806264 5632
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
98714466 = yrday
fracday
Element set: 912
Inclination: 51
6388 deg
RA of node: 150
4460 deg
Eccentricity:
0003946
Arg of perigee: 10
2509 deg
Mean anomaly: 349
8723 deg
Mean motion: 15
53806264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 563
Checksum: 316
Coasting Arc #14 (Orbit 578)
---------------------------------------
Vector Time (GMT): 2018/214/23:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1079717
62 A = 6782088
06 meter
Y = -5034697
91 meter E =
0011964
Z = 4409545
87 I = 51
84889
XDOT = 6708
941292 Wp = 54
69336
YDOT = -1536
561568 meter/sec RA = 144
38035 deg
ZDOT = -3383
941016 TA = 69
50075
MA = 69
37237
Ha = 222
295 n
mi
Hp = 214
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3542380
63 X = 1114517
72
Y = -16518037
75 feet Y = -5022429
24 meter
Z = 14467014
02 Z = 4414875
17
XDOT = 22010
962243 XDOT = 6742
062161
YDOT = -5041
212493 feet/sec YDOT = -1461
352313 meter/sec
ZDOT = -11102
168687 ZDOT = -3351
271212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15908525
52 X = 4848918
58
Y = -5621793
88 feet Y = -1713522
78 meter
Z = 14491472
51 Z = 4417000
82
XDOT = 15356
744163 XDOT = 4680
735621
YDOT = 15104
745842 feet/sec YDOT = 4603
926533 meter/sec
ZDOT = -10955
441147 ZDOT = -3339
218462
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 18215
01619980
00016717 00000-0 10270-3 0 9132
2 25544 51
6393 145
3179 0003908 14
4131 345
7132 15
53772981 5797
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
01619980 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 145
3179 deg
Eccentricity:
0003908
Arg of perigee: 14
4131 deg
Mean anomaly: 345
7132 deg
Mean motion: 15
53772981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 579
Checksum: 313
Coasting Arc #15 (Orbit 586)
---------------------------------------
Vector Time (GMT): 2018/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5663229
55 A = 6790048
44 meter
Y = -3656187
87 meter E =
0008478
Z = -801508
68 I = 51
88964
XDOT = 1993
151809 Wp = 115
28536
YDOT = 4382
808994 meter/sec RA = 141
80214 deg
ZDOT = -5962
431965 TA = 73
34502
MA = 73
25197
Ha = 222
447 n
mi
Hp = 214
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18580149
43 X = 5707586
42
Y = -11995367
01 feet Y = -3592609
69 meter
Z = -2629621
65 Z = -773891
24
XDOT = 6539
211973 XDOT = 1972
955998
YDOT = 14379
294601 feet/sec YDOT = 4404
984976 meter/sec
ZDOT = -19561
784663 ZDOT = -5952
798984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21269207
73 X = -6482854
52
Y = -6113090
14 feet Y = -1863269
88 meter
Z = -2505319
19 Z = -763621
29
XDOT = 5994
287169 XDOT = 1827
058729
YDOT = -12930
776057 feet/sec YDOT = -3941
300542 meter/sec
ZDOT = -19519
050340 ZDOT = -5949
406544
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 18215
53072528
00016717 00000-0 10270-3 0 9141
2 25544 51
6394 142
7580 0004520 13
4511 346
6761 15
53794365 5874
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
53072528 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 142
7580 deg
Eccentricity:
0004520
Arg of perigee: 13
4511 deg
Mean anomaly: 346
6761 deg
Mean motion: 15
53794365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 587
Checksum: 309
Coasting Arc #16 (Orbit 596)
---------------------------------------
Vector Time (GMT): 2018/216/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5459591
45 A = 6783696
85 meter
Y = 655152
14 meter E =
0012284
Z = 3960607
67 I = 51
88450
XDOT = 2198
916473 Wp = 80
06988
YDOT = -6142
849391 meter/sec RA = 138
74932 deg
ZDOT = 4038
719421 TA = 327
90487
MA = 327
97960
Ha = 222
497 n
mi
Hp = 214
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17912045
45 X = -5485750
19
Y = 2149449
27 feet Y = 593952
85 meter
Z = 12994119
64 Z = 3934023
53
XDOT = 7214
292892 XDOT = 2247
826252
YDOT = -20153
705352 feet/sec YDOT = -6117
986213 meter/sec
ZDOT = 13250
391802 ZDOT = 4049
519565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18122787
34 X = -5523825
58
Y = 336724
50 feet Y = 102633
63 meter
Z = 12874775
54 Z = 3924231
58
XDOT = 9133
637508 XDOT = 2783
932712
YDOT = -18015
939145 feet/sec YDOT = -5491
258251 meter/sec
ZDOT = 13299
528574 ZDOT = 4053
696310
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 18216
17387905
00016717 00000-0 10270-3 0 9151
2 25544 51
6395 139
5520 0004213 15
8772 344
2512 15
53817128 5979
Satellite: ISS
Catalog Number: 25544
Epoch time: 18216
17387905 = yrday
fracday
Element set: 915
Inclination: 51
6395 deg
RA of node: 139
5520 deg
Eccentricity:
0004213
Arg of perigee: 15
8772 deg
Mean anomaly: 344
2512 deg
Mean motion: 15
53817128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 597
Checksum: 314
Coasting Arc #17 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2018/217/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4706083
88 A = 6780456
29 meter
Y = 595750
27 meter E =
0014590
Z = -4858589
04 I = 51
89691
XDOT = -3397
858736 Wp = 59
14151
YDOT = 6386
629858 meter/sec RA = 133
77902 deg
ZDOT = -2506
382360 TA = 186
26561
MA = 186
28388
Ha = 222
495 n
mi
Hp = 214
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15439907
74 X = 4722672
60
Y = 1954561
26 feet Y = 648469
90 meter
Z = -15940252
75 Z = -4835688
33
XDOT = -11147
830499 XDOT = -3456
848645
YDOT = 20953
510033 feet/sec YDOT = 6348
302919 meter/sec
ZDOT = -8223
039238 ZDOT = -2523
030908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15329470
39 X = 4672422
58
Y = 3237533
08 feet Y = 986800
08 meter
Z = -15837564
05 Z = -4827289
52
XDOT = -12558
587788 XDOT = -3827
857558
YDOT = 18841
465799 feet/sec YDOT = 5742
878776 meter/sec
ZDOT = -8298
460475 ZDOT = -2529
370753
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 18217
13861231
00016717 00000-0 10270-3 0 9168
2 25544 51
6388 134
7456 0004266 20
7221 339
4103 15
53793532 6120
Satellite: ISS
Catalog Number: 25544
Epoch time: 18217
13861231 = yrday
fracday
Element set: 916
Inclination: 51
6388 deg
RA of node: 134
7456 deg
Eccentricity:
0004266
Arg of perigee: 20
7221 deg
Mean anomaly: 339
4103 deg
Mean motion: 15
53793532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 292
Coasting Arc #18 (Orbit 627)
---------------------------------------
Vector Time (GMT): 2018/218/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3761166
52 A = 6778437
71 meter
Y = -1939912
54 meter E =
0005107
Z = 5290903
29 I = 51
91250
XDOT = 4309
276648 Wp = 62
26159
YDOT = -6302
510108 meter/sec RA = 128
80289 deg
ZDOT = 754
296816 TA = 20
57279
MA = 20
55224
Ha = 222
630 n
mi
Hp = 214
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12339785
17 X = -3764894
60
Y = -6364542
47 feet Y = -1981993
65 meter
Z = 17358606
58 Z = 5272623
79
XDOT = 14138
046744 XDOT = 4375
768828
YDOT = -20677
526602 feet/sec YDOT = -6253
949060 meter/sec
ZDOT = 2474
727088 ZDOT = 775
390798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12008413
31 X = -3660164
38
Y = -7170016
24 feet Y = -2185420
95 meter
Z = 17276799
42 Z = 5265968
46
XDOT = 14930
176931 XDOT = 4550
717929
YDOT = -18826
296542 feet/sec YDOT = -5738
255186 meter/sec
ZDOT = 2570
107636 ZDOT = 783
368808
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 18218
16765566
00016717 00000-0 10270-3 0 9177
2 25544 51
6386 129
6183 0004285 23
5917 336
5431 15
53822415 6284
Satellite: ISS
Catalog Number: 25544
Epoch time: 18218
16765566 = yrday
fracday
Element set: 917
Inclination: 51
6386 deg
RA of node: 129
6183 deg
Eccentricity:
0004285
Arg of perigee: 23
5917 deg
Mean anomaly: 336
5431 deg
Mean motion: 15
53822415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 628
Checksum: 325
Coasting Arc #19 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2018/219/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2755942
95 A = 6778672
42 meter
Y = 3288977
21 meter E =
0016320
Z = -5261309
93 I = 51
93421
XDOT = -4888
646641 Wp = 83
24191
YDOT = 5795
032328 meter/sec RA = 123
82553 deg
ZDOT = 1066
583985 TA = 196
92261
MA = 196
97710
Ha = 222
663 n
mi
Hp = 214
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9041807
57 X = 2744516
32
Y = 10790607
65 feet Y = 3319732
56 meter
Z = -17261515
52 Z = -5247950
15
XDOT = -16038
866933 XDOT = -4958
265817
YDOT = 19012
573254 feet/sec YDOT = 5739
974761 meter/sec
ZDOT = 3499
291290 ZDOT = 1042
668159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8619727
99 X = 2627293
09
Y = 11222521
71 feet Y = 3420624
62 meter
Z = -17201939
18 Z = -5243151
06
XDOT = -16150
523248 XDOT = -4922
679486
YDOT = 17579
252860 feet/sec YDOT = 5358
156272 meter/sec
ZDOT = 3391
282216 ZDOT = 1033
662819
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 18219
13238128
00016717 00000-0 10270-3 0 9185
2 25544 51
6399 124
8111 0004457 26
9228 333
2155 15
53798014 6430
Satellite: ISS
Catalog Number: 25544
Epoch time: 18219
13238128 = yrday
fracday
Element set: 918
Inclination: 51
6399 deg
RA of node: 124
8111 deg
Eccentricity:
0004457
Arg of perigee: 26
9228 deg
Mean anomaly: 333
2155 deg
Mean motion: 15
53798014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 309
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