[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 31st 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 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
212/23:30:00
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
7
215/16:37:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 214
4
216/02:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 214
4
222/19:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 524)
---------------------------------------
Vector Time (GMT): 2018/211/12:00:01
006
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1999043
16 A = 6781141
17 meter
Y = -4518975
39 meter E =
0011769
Z = 4641539
56 I = 51
74247
XDOT = 7081
014519 Wp = 41
34753
YDOT = 96
621812 meter/sec RA = 161
65404 deg
ZDOT = -2942
728914 TA = 77
97234
MA = 77
84046
Ha = 222
436 n
mi
Hp = 214
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6558540
54 X = 2026881
33
Y = -14826034
73 feet Y = -4496465
23 meter
Z = 15228148
17 Z = 4651317
46
XDOT = 23231
674930 XDOT = 7093
701721
YDOT = 317
000696 feet/sec YDOT = 175
877660 meter/sec
ZDOT = -9654
622422 ZDOT = -2908
301702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15712303
07 X = -4789109
98
Y = 3820599
14 feet Y = 1164518
62 meter
Z = 15272485
42 Z = 4655053
56
XDOT = -13554
904556 XDOT = -4131
534909
YDOT = -17599
970698 feet/sec YDOT = -5364
471069 meter/sec
ZDOT = -9500
243988 ZDOT = -2895
674368
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
54313482
00016717 00000-0 10270-3 0 9000
2 25544 51
6385 162
6259 0005378 3
6039 356
5151 15
53783902 5256
Satellite: ISS
Catalog Number: 25544
Epoch time: 18211
54313482 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 162
6259 deg
Eccentricity:
0005378
Arg of perigee: 3
6039 deg
Mean anomaly: 356
5151 deg
Mean motion: 15
53783902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 525
Checksum: 300
Coasting Arc #2 (Orbit 539)
---------------------------------------
Vector Time (GMT): 2018/212/12:00:01
006
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3366935
94 A = 6784569
62 meter
Y = 4603468
64 meter E =
0007598
Z = -3676059
15 I = 51
78540
XDOT = -6209
320156 Wp = 55
66940
YDOT = -1064
829392 meter/sec RA = 156
67700 deg
ZDOT = 4364
314083 TA = 260
73797
MA = 260
82391
Ha = 222
565 n
mi
Hp = 214
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11046377
76 X = -3400306
94
Y = 15103243
57 feet Y = 4565630
73 meter
Z = -12060561
52 Z = -3692495
20
XDOT = -20371
785289 XDOT = -6218
150596
YDOT = -3493
534752 feet/sec YDOT = -1134
315777 meter/sec
ZDOT = 14318
615758 ZDOT = 4334
130447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18649911
47 X = 5684493
02
Y = -718073
99 feet Y = -218868
95 meter
Z = -12134774
18 Z = -3698679
17
XDOT = 9856
181886 XDOT = 3004
164239
YDOT = 16885
308640 feet/sec YDOT = 5146
642073 meter/sec
ZDOT = 14183
357075 ZDOT = 4323
087236
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
50788243
00016717 00000-0 10270-3 0 9019
2 25544 51
6390 157
8193 0005439 6
9721 353
1506 15
53770754 5402
Satellite: ISS
Catalog Number: 25544
Epoch time: 18212
50788243 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 157
8193 deg
Eccentricity:
0005439
Arg of perigee: 6
9721 deg
Mean anomaly: 353
1506 deg
Mean motion: 15
53770754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 540
Checksum: 305
Coasting Arc #3 (Orbit 547)
---------------------------------------
Vector Time (GMT): 2018/212/23:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1327869
28 A = 6781098
44 meter
Y = -4724775
94 meter E =
0011693
Z = 4676163
66 I = 51
78884
XDOT = 7053
692572 Wp = 44
77007
YDOT = -879
745447 meter/sec RA = 154
29486 deg
ZDOT = -2879
414240 TA = 73
83753
MA = 73
70886
Ha = 222
539 n
mi
Hp = 214
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4356526
52 X = 1357890
40
Y = -15501233
41 feet Y = -4709759
02 meter
Z = 15341744
30 Z = 4682686
71
XDOT = 23142
035996 XDOT = 7076
992323
YDOT = -2886
303961 feet/sec YDOT = -800
735853 meter/sec
ZDOT = -9446
897113 ZDOT = -2845
093860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15465468
23 X = 4713874
72
Y = -4378651
15 feet Y = -1334612
87 meter
Z = 15371512
14 Z = 4685236
90
XDOT = 14156
849421 XDOT = 4315
007703
YDOT = 17235
580492 feet/sec YDOT = 5253
404934 meter/sec
ZDOT = -9292
867497 ZDOT = -2832
466013
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
02241462
00016717 00000-0 10270-3 0 9025
2 25544 51
6397 155
2515 0004913 11
7005 348
4261 15
53756782 5482
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
02241462 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 155
2515 deg
Eccentricity:
0004913
Arg of perigee: 11
7005 deg
Mean anomaly: 348
4261 deg
Mean motion: 15
53756782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 548
Checksum: 291
Coasting Arc #4 (Orbit 562)
---------------------------------------
Vector Time (GMT): 2018/213/23:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2683469
10 A = 6784432
33 meter
Y = 4997004
09 meter E =
0007748
Z = -3725337
49 I = 51
82925
XDOT = -6329
700604 Wp = 62
59939
YDOT = -189
485133 meter/sec RA = 149
32139 deg
ZDOT = 4315
652032 TA = 253
11052
MA = 253
19549
Ha = 222
578 n
mi
Hp = 214
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8804032
49 X = -2721052
06
Y = 16394370
37 feet Y = 4966785
59 meter
Z = -12222235
85 Z = -3738463
89
XDOT = -20766
734264 XDOT = -6348
074170
YDOT = -621
670385 feet/sec YDOT = -260
371004 meter/sec
ZDOT = 14158
963359 ZDOT = 4284
860333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18521479
06 X = -5645346
82
Y = 1336072
22 feet Y = 407234
81 meter
Z = -12281658
75 Z = -3743449
59
XDOT = -10475
400238 XDOT = -3192
901992
YDOT = -16642
465624 feet/sec YDOT = -5072
623522 meter/sec
ZDOT = 14020
862699 ZDOT = 4273
558951
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
98715828
00016717 00000-0 10270-3 0 9033
2 25544 51
6395 150
4458 0004972 13
2445 346
8837 15
53769829 5637
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
98715828 = yrday
fracday
Element set: 903
Inclination: 51
6395 deg
RA of node: 150
4458 deg
Eccentricity:
0004972
Arg of perigee: 13
2445 deg
Mean anomaly: 346
8837 deg
Mean motion: 15
53769829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 563
Checksum: 344
Coasting Arc #5 (Orbit 578)
---------------------------------------
Vector Time (GMT): 2018/214/23:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3827162
52 A = 6787859
85 meter
Y = -5061455
20 meter E =
0014744
Z = 2398935
72 I = 51
86885
XDOT = 5271
540915 Wp = 86
93042
YDOT = 1420
418300 meter/sec RA = 144
35763 deg
ZDOT = -5383
823674 TA = 66
35398
MA = 66
19928
Ha = 222
624 n
mi
Hp = 214
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12556307
49 X = 3871824
02
Y = -16605824
14 feet Y = -5018407
53 meter
Z = 7870524
03 Z = 2417634
97
XDOT = 17295
081742 XDOT = 5281
417127
YDOT = 4660
165027 feet/sec YDOT = 1479
423607 meter/sec
ZDOT = -17663
463499 ZDOT = -5358
192610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20739538
53 X = 6321411
35
Y = 1396240
65 feet Y = 425574
15 meter
Z = 7954964
17 Z = 2424673
08
XDOT = 5716
218060 XDOT = 1742
303265
YDOT = 15615
369233 feet/sec YDOT = 4759
564542 meter/sec
ZDOT = -17548
635716 ZDOT = -5348
824166
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
01621698
00016717 00000-0 10270-3 0 9041
2 25544 51
6397 145
3183 0004856 17
8440 342
2882 15
53778088 5797
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
01621698 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 145
3183 deg
Eccentricity:
0004856
Arg of perigee: 17
8440 deg
Mean anomaly: 342
2882 deg
Mean motion: 15
53778088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 579
Checksum: 332
Coasting Arc #6 (Orbit 589)
---------------------------------------
Vector Time (GMT): 2018/215/16:37:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5484368
28 A = 6790283
22 meter
Y = -3970939
29 meter E =
0009518
Z = -489349
31 I = 51
89639
XDOT = 2434
817713 Wp = 109
60574
YDOT = 4090
791006 meter/sec RA = 140
84471 deg
ZDOT = -6005
540373 TA = 75
65017
MA = 75
54452
Ha = 222
809 n
mi
Hp = 214
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17993334
25 X = 5530741
79
Y = -13028016
06 feet Y = -3909350
00 meter
Z = -1605476
75 Z = -462595
81
XDOT = 7988
247090 XDOT = 2418
063914
YDOT = 13421
230335 feet/sec YDOT = 4117
925259 meter/sec
ZDOT = -19703
216446 ZDOT = -5993
753581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12274635
10 X = -3741308
78
Y = 18525520
42 feet Y = 5646578
62 meter
Z = -1485012
34 Z = -452631
76
XDOT = -10967
281966 XDOT = -3342
827543
YDOT = -8814
046291 feet/sec YDOT = -2686
521310 meter/sec
ZDOT = -19650
787438 ZDOT = -5989
560011
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
72369163
00016717 00000-0 10270-3 0 9056
2 25544 51
6405 141
7977 0005388 16
8197 343
3127 15
53768728 5904
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
72369163 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 141
7977 deg
Eccentricity:
0005388
Arg of perigee: 16
8197 deg
Mean anomaly: 343
3127 deg
Mean motion: 15
53768728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 590
Checksum: 334
Coasting Arc #7 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2018/216/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3682589
06 A = 6788590
38 meter
Y = 5328866
67 meter E =
0011676
Z = -2015616
59 I = 51
90099
XDOT = -5060
981142 Wp = 31
38822
YDOT = -1392
317289 meter/sec RA = 138
76856 deg
ZDOT = 5589
791330 TA = 306
42920
MA = 306
53680
Ha = 222
771 n
mi
Hp = 214
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12081985
11 X = -3732113
49
Y = 17483158
38 feet Y = 5287408
56 meter
Z = -6612915
32 Z = -2033625
36
XDOT = -16604
268838 XDOT = -5072
187792
YDOT = -4567
970108 feet/sec YDOT = -1448
975473 meter/sec
ZDOT = 18339
210401 ZDOT = 5565
179759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14959635
85 X = -4559697
01
Y = 15058599
98 feet Y = 4589861
27 meter
Z = -6694303
70 Z = -2040423
77
XDOT = -14546
529906 XDOT = -4433
782315
YDOT = -6382
158284 feet/sec YDOT = -1945
281845 meter/sec
ZDOT = 18228
943387 ZDOT = 5556
181944
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
10958654
00016717 00000-0 10270-3 0 9069
2 25544 51
6400 139
8731 0005265 19
0231 341
1117 15
53774194 5968
Satellite: ISS
Catalog Number: 25544
Epoch time: 18216
10958654 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 139
8731 deg
Eccentricity:
0005265
Arg of perigee: 19
0231 deg
Mean anomaly: 341
1117 deg
Mean motion: 15
53774194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 301
Coasting Arc #8 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2018/217/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4443618
62 A = 6790151
14 meter
Y = -5112535
68 meter E =
0012567
Z = 425761
60 I = 51
93016
XDOT = 3828
335092 Wp = 106
14587
YDOT = 2814
589497 meter/sec RA = 133
81777 deg
ZDOT = -6014
738539 TA = 69
28382
MA = 69
14916
Ha = 222
872 n
mi
Hp = 214
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14578801
25 X = 4498390
03
Y = -16773411
02 feet Y = -5062537
83 meter
Z = 1396855
64 Z = 447479
86
XDOT = 12560
154501 XDOT = 3825
793305
YDOT = 9234
217511 feet/sec YDOT = 2857
386611 meter/sec
ZDOT = -19733
394158 ZDOT = -5996
147985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17082338
85 X = 5206696
88
Y = -14205597
43 feet Y = -4329866
10 meter
Z = 1494881
14 Z = 455639
77
XDOT = 10000
833680 XDOT = 3048
254106
YDOT = 9911
924355 feet/sec YDOT = 3021
154543 meter/sec
ZDOT = -19650
294865 ZDOT = -5989
409875
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
13863886
00016717 00000-0 10270-3 0 9076
2 25544 51
6395 134
7460 0005356 24
7045 335
4363 15
53814814 6123
Satellite: ISS
Catalog Number: 25544
Epoch time: 18217
13863886 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 134
7460 deg
Eccentricity:
0005356
Arg of perigee: 24
7045 deg
Mean anomaly: 335
4363 deg
Mean motion: 15
53814814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 313
Coasting Arc #9 (Orbit 627)
---------------------------------------
Vector Time (GMT): 2018/218/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4860029
13 A = 6789845
02 meter
Y = 4582386
82 meter E =
0018602
Z = 1160416
89 I = 51
95034
XDOT = -2541
434680 Wp = 49
39404
YDOT = -4201
300882 meter/sec RA = 128
86950 deg
ZDOT = 5896
675940 TA = 323
15952
MA = 323
28718
Ha = 223
061 n
mi
Hp = 214
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15944977
47 X = -4916546
10
Y = 15034077
49 feet Y = 4527722
54 meter
Z = 3807142
04 Z = 1136671
69
XDOT = -8338
040290 XDOT = -2522
908453
YDOT = -13783
795546 feet/sec YDOT = -4229
617708 meter/sec
ZDOT = 19346
049671 ZDOT = 5884
375367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17970778
34 X = -5477493
24
Y = 12574609
16 feet Y = 3832740
87 meter
Z = 3700061
27 Z = 1127778
67
XDOT = -5473
624366 XDOT = -1668
360707
YDOT = -13548
574218 feet/sec YDOT = -4129
605422 meter/sec
ZDOT = 19291
331546 ZDOT = 5879
997855
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
16768962
00016717 00000-0 10270-3 0 9080
2 25544 51
6391 129
6187 0005444 28
2773 331
8674 15
53768171 6289
Satellite: ISS
Catalog Number: 25544
Epoch time: 18218
16768962 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 129
6187 deg
Eccentricity:
0005444
Arg of perigee: 28
2773 deg
Mean anomaly: 331
8674 deg
Mean motion: 15
53768171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 628
Checksum: 343
Coasting Arc #10 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2018/219/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5020350
77 A = 6787242
31 meter
Y = -3700835
20 meter E =
0007173
Z = -2685520
17 I = 51
96331
XDOT = 1243
769950 Wp = 76
65661
YDOT = 5466
933668 meter/sec RA = 123
91855 deg
ZDOT = -5218
781372 TA = 133
48364
MA = 133
42398
Ha = 223
034 n
mi
Hp = 213
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16470967
08 X = 5074406
13
Y = -12141847
77 feet Y = -3644391
73 meter
Z = -8810761
73 Z = -2661002
23
XDOT = 4080
610071 XDOT = 1207
894620
YDOT = 17936
134080 feet/sec YDOT = 5480
642144 meter/sec
ZDOT = -17121
986127 ZDOT = -5212
826363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17938796
09 X = 5467745
05
Y = -9942395
09 feet Y = -3030442
02 meter
Z = -8700294
28 Z = -2651849
70
XDOT = 1154
829286 XDOT = 351
991966
YDOT = 17014
416054 feet/sec YDOT = 5185
994013 meter/sec
ZDOT = -17095
895769 ZDOT = -5210
829030
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
13241821
00016717 00000-0 10270-3 0 9099
2 25544 51
6404 124
8114 0005461 32
6011 327
5478 15
53820672 6430
Satellite: ISS
Catalog Number: 25544
Epoch time: 18219
13241821 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 124
8114 deg
Eccentricity:
0005461
Arg of perigee: 32
6011 deg
Mean anomaly: 327
5478 deg
Mean motion: 15
53820672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 283
Coasting Arc #11 (Orbit 658)
---------------------------------------
Vector Time (GMT): 2018/220/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4909132
86 A = 6783781
67 meter
Y = 2524235
83 meter E =
0014550
Z = 3928747
34 I = 51
96891
XDOT = -59
890446 Wp = 79
62306
YDOT = -6495
145761 meter/sec RA = 118
96180 deg
ZDOT = 4088
066452 TA = 327
78188
MA = 327
87069
Ha = 223
236 n
mi
Hp = 213
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16106078
95 X = -4956078
25
Y = 8281613
63 feet Y = 2469075
72 meter
Z = 12889591
02 Z = 3904786
95
XDOT = -196
490966 XDOT = -7
112905
YDOT = -21309
533335 feet/sec YDOT = -6495
520722 meter/sec
ZDOT = 13412
291510 ZDOT = 4087
903201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17004538
28 X = -5182983
27
Y = 6450203
69 feet Y = 1966022
09 meter
Z = 12781745
19 Z = 3895875
93
XDOT = 2531
848796 XDOT = 771
707513
YDOT = -19970
482257 feet/sec YDOT = -6087
002992 meter/sec
ZDOT = 13412
325553 ZDOT = 4088
076828
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 18220
16145961
00016717 00000-0 10270-3 0 9104
2 25544 51
6400 119
6846 0005512 36
3888 323
7638 15
53819697 6598
Satellite: ISS
Catalog Number: 25544
Epoch time: 18220
16145961 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 119
6846 deg
Eccentricity:
0005512
Arg of perigee: 36
3888 deg
Mean anomaly: 323
7638 deg
Mean motion: 15
53819697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 659
Checksum: 326
Coasting Arc #12 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2018/221/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4632918
12 A = 6780464
62 meter
Y = -1091777
07 meter E =
0016308
Z = -4844444
98 I = 51
97372
XDOT = -991
639338 Wp = 61
78338
YDOT = 7146
269626 meter/sec RA = 113
99682 deg
ZDOT = -2557
921189 TA = 183
11101
MA = 183
12117
Ha = 223
137 n
mi
Hp = 213
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15199862
59 X = 4668313
69
Y = -3581945
78 feet Y = -1039770
31 meter
Z = -15893848
36 Z = -4821854
38
XDOT = -3253
409901 XDOT = -1059
052384
YDOT = 23445
766491 feet/sec YDOT = 7134
803693 meter/sec
ZDOT = -8392
129886 ZDOT = -2562
901340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15571848
72 X = 4746299
49
Y = -2145032
75 feet Y = -653805
98 meter
Z = -15792306
23 Z = -4813494
94
XDOT = -5519
426480 XDOT = -1682
321191
YDOT = 21910
885494 feet/sec YDOT = 6678
437898 meter/sec
ZDOT = -8415
340448 ZDOT = -2564
995769
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 18221
12618466
00016717 00000-0 10270-3 0 9117
2 25544 51
6409 114
8781 0005438 39
6940 320
4609 15
53811369 6741
Satellite: ISS
Catalog Number: 25544
Epoch time: 18221
12618466 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 114
8781 deg
Eccentricity:
0005438
Arg of perigee: 39
6940 deg
Mean anomaly: 320
4609 deg
Mean motion: 15
53811369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 312
Coasting Arc #13 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2018/222/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4203175
54 A = 6778421
66 meter
Y = -495538
77 meter E =
0007129
Z = 5288749
11 I = 51
97925
XDOT = 1883
712991 Wp = 69
63982
YDOT = -7395
179255 meter/sec RA = 109
02561 deg
ZDOT = 805
696427 TA = 12
71016
MA = 12
69219
Ha = 223
367 n
mi
Hp = 213
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13789946
00 X = -4223011
28
Y = -1625783
36 feet Y = -542652
80 meter
Z = 17351539
06 Z = 5268283
79
XDOT = 6180
160730 XDOT = 1962
354366
YDOT = -24262
399132 feet/sec YDOT = -7373
674610 meter/sec
ZDOT = 2643
360981 ZDOT = 815
037218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13741688
83 X = -4188466
76
Y = -2673914
27 feet Y = -815009
07 meter
Z = 17259717
86 Z = 5260762
00
XDOT = 7789
064407 XDOT = 2374
106831
YDOT = -22723
139857 feet/sec YDOT = -6926
013028 meter/sec
ZDOT = 2686
189616 ZDOT = 818
750595
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 18222
15521992
00016717 00000-0 10270-3 0 9129
2 25544 51
6405 109
7509 0005613 43
3195 316
8398 15
53833567 6903
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
15521992 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 109
7509 deg
Eccentricity:
0005613
Arg of perigee: 43
3195 deg
Mean anomaly: 316
8398 deg
Mean motion: 15
53833567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 316
Coasting Arc #14 (Orbit 700)
---------------------------------------
Vector Time (GMT): 2018/222/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4283869
13 A = 6778543
98 meter
Y = 101286
06 meter E =
0007116
Z = 5246096
29 I = 51
98725
XDOT = 1182
081035 Wp = 77
54705
YDOT = -7500
459436 meter/sec RA = 105
51932 deg
ZDOT = 1110
307496 TA = 1
87219
MA = 1
86952
Ha = 223
233 n
mi
Hp = 213
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14054688
74 X = -4310165
49
Y = 332303
34 feet Y = 53233
63 meter
Z = 17211602
01 Z = 5225223
39
XDOT = 3878
218620 XDOT = 1260
472235
YDOT = -24607
806547 feet/sec YDOT = -7486
802320 meter/sec
ZDOT = 3642
741130 ZDOT = 1116
239588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4333007
25 X = 1320700
61
Y = -13493977
27 feet Y = -4112964
27 meter
Z = 17117872
84 Z = 5217527
64
XDOT = 20997
367562 XDOT = 6399
997633
YDOT = 11397
397630 feet/sec YDOT = 3473
926797 meter/sec
ZDOT = 3670
285312 ZDOT = 1118
702963
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 18222
86267955
00016717 00000-0 10270-3 0 9134
2 25544 51
6406 106
2221 0005236 45
6580 314
5000 15
53857729 7015
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
86267955 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 106
2221 deg
Eccentricity:
0005236
Arg of perigee: 45
6580 deg
Mean anomaly: 314
5000 deg
Mean motion: 15
53857729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 701
Checksum: 293
Coasting Arc #15 (Orbit 715)
---------------------------------------
Vector Time (GMT): 2018/223/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3934042
41 A = 6778338
04 meter
Y = 1552746
57 meter E =
0018782
Z = -5312867
68 I = 51
99369
XDOT = -1943
350503 Wp = 83
97591
YDOT = 7368
651821 meter/sec RA = 100
54802 deg
ZDOT = 718
663973 TA = 192
84357
MA = 192
89148
Ha = 223
189 n
mi
Hp = 213
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12906963
29 X = 3942193
23
Y = 5094312
91 feet Y = 1596785
38 meter
Z = -17430668
23 Z = -5293738
14
XDOT = -6375
821860 XDOT = -2029
095171
YDOT = 24175
366867 feet/sec YDOT = 7346
440496 meter/sec
ZDOT = 2357
821434 ZDOT = 709
015913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8899045
89 X = -2712429
19
Y = 10785600
26 feet Y = 3287450
96 meter
Z = -17344962
66 Z = -5286744
62
XDOT = -20191
584430 XDOT = -6154
394934
YDOT = -12960
850392 feet/sec YDOT = -3950
467199 meter/sec
ZDOT = 2313
599886 ZDOT = 705
185245
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 18223
82739654
00016717 00000-0 10270-3 0 9142
2 25544 51
6400 101
4166 0005339 50
6550 309
5075 15
53848896 7168
Satellite: ISS
Catalog Number: 25544
Epoch time: 18223
82739654 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 101
4166 deg
Eccentricity:
0005339
Arg of perigee: 50
6550 deg
Mean anomaly: 309
5075 deg
Mean motion: 15
53848896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 716
Checksum: 314
Coasting Arc #16 (Orbit 731)
---------------------------------------
Vector Time (GMT): 2018/224/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3506488
44 A = 6780307
35 meter
Y = -3160132
99 meter E =
0012446
Z = 4860837
75 I = 52
00516
XDOT = 2620
279669 Wp = 57
76084
YDOT = -6765
220304 meter/sec RA = 95
57689 deg
ZDOT = -2496
890884 TA = 56
68886
MA = 56
56974
Ha = 223
390 n
mi
Hp = 213
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11504227
17 X = -3494501
18
Y = -10367890
39 feet Y = -3199277
86 meter
Z = 15947630
42 Z = 4843834
02
XDOT = 8596
718074 XDOT = 2707
863781
YDOT = -22195
604673 feet/sec YDOT = -6735
428855 meter/sec
ZDOT = -8191
899226 ZDOT = -2483
949935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13333373
86 X = 4064012
35
Y = -8029860
50 feet Y = -2447501
48 meter
Z = 15871666
32 Z = 4837683
90
XDOT = 18065
110812 XDOT = 5506
245775
YDOT = 13848
768555 feet/sec YDOT = 4221
104656 meter/sec
ZDOT = -8132
956966 ZDOT = -2478
925283
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 18224
85642563
00016717 00000-0 10270-3 0 9159
2 25544 51
6402 96
2883 0005350 54
7708 305
3944 15
53812821 7326
Satellite: ISS
Catalog Number: 25544
Epoch time: 18224
85642563 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 96
2883 deg
Eccentricity:
0005350
Arg of perigee: 54
7708 deg
Mean anomaly: 305
3944 deg
Mean motion: 15
53812821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 732
Checksum: 309
Coasting Arc #17 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2018/225/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3069301
89 A = 6783489
54 meter
Y = 4551536
94 meter E =
0010954
Z = -3993480
95 I = 52
01904
XDOT = -3201
293286 Wp = 85
14782
YDOT = 5678
615149 meter/sec RA = 90
61416 deg
ZDOT = 4022
078742 TA = 226
57929
MA = 226
67052
Ha = 223
273 n
mi
Hp = 213
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10069888
10 X = 3037575
08
Y = 14932863
99 feet Y = 4585682
46 meter
Z = -13101971
62 Z = -3978648
86
XDOT = -10502
930728 XDOT = -3284
091959
YDOT = 18630
627128 feet/sec YDOT = 5642
353261 meter/sec
ZDOT = 13195
796399 ZDOT = 4006
326972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17172043
14 X = -5234038
75
Y = 5589282
08 feet Y = 1703613
18 meter
Z = -13035934
71 Z = -3973352
90
XDOT = -14531
209302 XDOT = -4429
112595
YDOT = -14114
146325 feet/sec YDOT = -4301
991800 meter/sec
ZDOT = 13124
358003 ZDOT = 4000
304319
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 18225
82113532
00016717 00000-0 10270-3 0 9167
2 25544 51
6410 91
4818 0005304 56
5116 303
6542 15
53837754 7475
Satellite: ISS
Catalog Number: 25544
Epoch time: 18225
82113532 = yrday
fracday
Element set: 916
Inclination: 51
6410 deg
RA of node: 91
4818 deg
Eccentricity:
0005304
Arg of perigee: 56
5116 deg
Mean anomaly: 303
6542 deg
Mean motion: 15
53837754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 296
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