[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 5th 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
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
3
000/00:00:00
000 0
0 0
0 213
6
227/00:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2018/215/14:00:13
667
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 63776
50 A = 6780508
47 meter
Y = 4786454
95 meter E =
0012637
Z = -4812323
12 I = 51
86187
XDOT = -6671
484291 Wp = 82
58384
YDOT = 2707
518077 meter/sec RA = 141
36131 deg
ZDOT = 2612
006085 TA = 213
07251
MA = 213
15160
Ha = 222
825 n
mi
Hp = 214
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 209240
47 X = 33623
83
Y = 15703592
34 feet Y = 4786999
63 meter
Z = -15788461
66 Z = -4812086
46
XDOT = -21888
071821 XDOT = -6713
952312
YDOT = 8882
933324 feet/sec YDOT = 2632
675427 meter/sec
ZDOT = 8569
573770 ZDOT = 2579
495498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4741906
37 X = 1445333
06
Y = -14972568
08 feet Y = -4563638
75 meter
Z = -15787927
19 Z = -4812160
21
XDOT = 22542
858335 XDOT = 6871
063220
YDOT = -1716
870273 feet/sec YDOT = -523
302059 meter/sec
ZDOT = 8423
422068 ZDOT = 2567
459046
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
59506196
00016717 00000-0 10270-3 0 9005
2 25544 51
6410 142
4389 0005534 17
2005 342
9334 15
53792478 5882
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
59506196 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 142
4389 deg
Eccentricity:
0005534
Arg of perigee: 17
2005 deg
Mean anomaly: 342
9334 deg
Mean motion: 15
53792478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 311
Coasting Arc #2 (Orbit 589)
---------------------------------------
Vector Time (GMT): 2018/215/16:37:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5484042
65 A = 6790299
50 meter
Y = -3971569
18 meter E =
0009521
Z = -488497
56 I = 51
89625
XDOT = 2435
833319 Wp = 109
33754
YDOT = 4090
044702 meter/sec RA = 140
84447 deg
ZDOT = -6005
585088 TA = 75
90918
MA = 75
80338
Ha = 222
832 n
mi
Hp = 214
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17992265
92 X = 5530419
10
Y = -13030082
61 feet Y = -3909983
51 meter
Z = -1602682
28 Z = -461745
63
XDOT = 7991
579132 XDOT = 2419
088007
YDOT = 13418
781831 feet/sec YDOT = 4117
190360 meter/sec
ZDOT = -19703
363151 ZDOT = -5993
793343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12272891
23 X = -3740777
25
Y = 18527072
80 feet Y = 5647051
79 meter
Z = -1482224
87 Z = -451782
14
XDOT = -10969
428237 XDOT = -3343
481727
YDOT = -8810
709570 feet/sec YDOT = -2685
504277 meter/sec
ZDOT = -19650
911835 ZDOT = -5989
597927
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
72369342
00016717 00000-0 10270-3 0 9011
2 25544 51
6403 141
7976 0005433 16
8473 343
2851 15
53763233 5908
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
72369342 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 141
7976 deg
Eccentricity:
0005433
Arg of perigee: 16
8473 deg
Mean anomaly: 343
2851 deg
Mean motion: 15
53763233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 590
Checksum: 303
Coasting Arc #3 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2018/216/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3681154
03 A = 6788604
11 meter
Y = 5329268
22 meter E =
0011715
Z = -2017164
60 I = 51
90083
XDOT = -5062
301077 Wp = 31
35875
YDOT = -1390
436043 meter/sec RA = 138
76833 deg
ZDOT = 5589
080054 TA = 306
44066
MA = 306
54860
Ha = 222
794 n
mi
Hp = 214
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12077277
00 X = -3730675
53
Y = 17484475
79 feet Y = 5287826
17 meter
Z = -6617994
11 Z = -2035166
40
XDOT = -16608
599334 XDOT = -5073
525210
YDOT = -4561
798041 feet/sec YDOT = -1447
109085 meter/sec
ZDOT = 18336
876817 ZDOT = 5564
462029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14955204
59 X = -4558346
36
Y = 15060740
63 feet Y = 4590513
74 meter
Z = -6699351
23 Z = -2041962
25
XDOT = -14551
719160 XDOT = -4435
364000
YDOT = -6377
176906 feet/sec YDOT = -1943
763521 meter/sec
ZDOT = 18226
580638 ZDOT = 5555
461778
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
10958975
00016717 00000-0 10270-3 0 9021
2 25544 51
6398 139
8731 0005310 19
0456 341
0894 15
53768559 5963
Satellite: ISS
Catalog Number: 25544
Epoch time: 18216
10958975 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 139
8731 deg
Eccentricity:
0005310
Arg of perigee: 19
0456 deg
Mean anomaly: 341
0894 deg
Mean motion: 15
53768559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 338
Coasting Arc #4 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2018/217/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4441341
76 A = 6790167
49 meter
Y = -5114265
47 meter E =
0012583
Z = 429351
82 I = 51
93001
XDOT = 3831
732441 Wp = 105
91675
YDOT = 2810
662191 meter/sec RA = 133
81755 deg
ZDOT = -6014
367213 TA = 69
47433
MA = 69
33934
Ha = 222
896 n
mi
Hp = 214
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14571331
22 X = 4496115
24
Y = -16779086
18 feet Y = -5064293
07 meter
Z = 1408634
58 Z = 451059
03
XDOT = 12571
300659 XDOT = 3829
232514
YDOT = 9221
332648 feet/sec YDOT = 2853
497530 meter/sec
ZDOT = -19732
175895 ZDOT = -5995
760054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17075804
12 X = 5204705
10
Y = -14212414
15 feet Y = -4331943
83 meter
Z = 1506610
67 Z = 459214
93
XDOT = 10013
405642 XDOT = 3052
086040
YDOT = 9901
479869 feet/sec YDOT = 3017
971064 meter/sec
ZDOT = -19649
001656 ZDOT = -5989
015705
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
13864598
00016717 00000-0 10270-3 0 9033
2 25544 51
6393 134
7459 0005402 24
7112 335
4298 15
53808711 6122
Satellite: ISS
Catalog Number: 25544
Epoch time: 18217
13864598 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 134
7459 deg
Eccentricity:
0005402
Arg of perigee: 24
7112 deg
Mean anomaly: 335
4298 deg
Mean motion: 15
53808711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 309
Coasting Arc #5 (Orbit 627)
---------------------------------------
Vector Time (GMT): 2018/218/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4857568
38 A = 6789870
00 meter
Y = 4586419
21 meter E =
0018643
Z = 1154761
44 I = 51
95021
XDOT = -2547
425266 Wp = 49
29529
YDOT = -4195
694276 meter/sec RA = 128
86929 deg
ZDOT = 5898
104748 TA = 323
19612
MA = 323
32396
Ha = 223
087 n
mi
Hp = 214
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15936904
15 X = -4914103
15
Y = 15047307
13 feet Y = 4531782
36 meter
Z = 3788587
41 Z = 1131028
15
XDOT = -8357
694443 XDOT = -2528
968229
YDOT = -13765
401169 feet/sec YDOT = -4224
078480 meter/sec
ZDOT = 19350
737362 ZDOT = 5885
774907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17964575
01 X = -5475602
46
Y = 12588880
96 feet Y = 3837090
92 meter
Z = 3681559
62 Z = 1122139
37
XDOT = -5494
715069 XDOT = -1674
789153
YDOT = -13533
662357 feet/sec YDOT = -4125
060286 meter/sec
ZDOT = 19295
887257 ZDOT = 5881
386436
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
16770100
00016717 00000-0 10270-3 0 9043
2 25544 51
6389 129
6187 0005491 28
2864 331
8586 15
53761443 6286
Satellite: ISS
Catalog Number: 25544
Epoch time: 18218
16770100 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 129
6187 deg
Eccentricity:
0005491
Arg of perigee: 28
2864 deg
Mean anomaly: 331
8586 deg
Mean motion: 15
53761443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 628
Checksum: 323
Coasting Arc #6 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2018/219/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5018713
27 A = 6787278
46 meter
Y = -3708183
95 meter E =
0007200
Z = -2678553
81 I = 51
96321
XDOT = 1252
341330 Wp = 76
59787
YDOT = 5460
593480 meter/sec RA = 123
91838 deg
ZDOT = -5223
319297 TA = 133
45594
MA = 133
39603
Ha = 223
061 n
mi
Hp = 213
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16465594
72 X = 5072817
10
Y = -12165957
85 feet Y = -3651758
53 meter
Z = -8787906
19 Z = -2654043
70
XDOT = 4108
731397 XDOT = 1216
558304
YDOT = 17915
332941 feet/sec YDOT = 5474
398324 meter/sec
ZDOT = -17136
874335 ZDOT = -5217
322429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17936382
19 X = 5467009
29
Y = -9967010
11 feet Y = -3037944
68 meter
Z = -8677473
06 Z = -2644893
79
XDOT = 1183
669733 XDOT = 360
782535
YDOT = 16997
546582 feet/sec YDOT = 5180
852198 meter/sec
ZDOT = -17110
595371 ZDOT = -5215
309469
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
13243387
00016717 00000-0 10270-3 0 9054
2 25544 51
6401 124
8114 0005508 32
6082 327
5410 15
53813608 6434
Satellite: ISS
Catalog Number: 25544
Epoch time: 18219
13243387 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 124
8114 deg
Eccentricity:
0005508
Arg of perigee: 32
6082 deg
Mean anomaly: 327
5410 deg
Mean motion: 15
53813608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 282
Coasting Arc #7 (Orbit 658)
---------------------------------------
Vector Time (GMT): 2018/220/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4909012
10 A = 6783827
84 meter
Y = 2535570
52 meter E =
0014616
Z = 3921593
63 I = 51
96884
XDOT = -70
891054 Wp = 79
42323
YDOT = -6489
517257 meter/sec RA = 118
96172 deg
ZDOT = 4096
867613 TA = 327
86841
MA = 327
95741
Ha = 223
264 n
mi
Hp = 213
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16105682
75 X = -4956049
50
Y = 8318800
93 feet Y = 2480411
25 meter
Z = 12866120
85 Z = 3897633
61
XDOT = -232
582199 XDOT = -18
218385
YDOT = -21291
067117 feet/sec YDOT = -6490
015823 meter/sec
ZDOT = 13441
166709 ZDOT = 4096
650671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17008082
40 X = -5184063
52
Y = 6487224
03 feet Y = 1977305
88 meter
Z = 12758275
31 Z = 3888722
31
XDOT = 2496
453957 XDOT = 760
919166
YDOT = -19955
860943 feet/sec YDOT = -6082
546415 meter/sec
ZDOT = 13440
959093 ZDOT = 4096
804332
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
16148016
00016717 00000-0 10270-3 0 9063
2 25544 51
6397 119
6845 0005560 36
4034 323
7496 15
53811978 6595
Satellite: ISS
Catalog Number: 25544
Epoch time: 18220
16148016 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 119
6845 deg
Eccentricity:
0005560
Arg of perigee: 36
4034 deg
Mean anomaly: 323
7496 deg
Mean motion: 15
53811978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 659
Checksum: 322
Coasting Arc #8 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2018/221/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4635114
91 A = 6780510
87 meter
Y = -1107401
69 meter E =
0016321
Z = -4838871
29 I = 51
97365
XDOT = -978
763651 Wp = 61
65657
YDOT = 7143
183625 meter/sec RA = 113
99686 deg
ZDOT = -2571
356789 TA = 183
09663
MA = 183
10674
Ha = 223
166 n
mi
Hp = 213
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15207069
90 X = 4670657
96
Y = -3633207
65 feet Y = -1055369
54 meter
Z = -15875561
98 Z = -4816269
66
XDOT = -3211
166834 XDOT = -1046
077883
YDOT = 23435
641813 feet/sec YDOT = 7131
862229 meter/sec
ZDOT = -8436
209939 ZDOT = -2576
274156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15583668
46 X = 4749902
15
Y = -2195412
68 feet Y = -669161
79 meter
Z = -15773968
47 Z = -4807905
59
XDOT = -5479
808183 XDOT = -1670
245534
YDOT = 21903
893024 feet/sec YDOT = 6676
306594 meter/sec
ZDOT = -8459
138287 ZDOT = -2578
345350
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
12621007
00016717 00000-0 10270-3 0 9077
2 25544 51
6406 114
8780 0005486 39
7131 320
4423 15
53803339 6745
Satellite: ISS
Catalog Number: 25544
Epoch time: 18221
12621007 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 114
8780 deg
Eccentricity:
0005486
Arg of perigee: 39
7131 deg
Mean anomaly: 320
4423 deg
Mean motion: 15
53803339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 286
Coasting Arc #9 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2018/222/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4208137
61 A = 6778456
10 meter
Y = -476026
87 meter E =
0007181
Z = 5286588
57 I = 51
97913
XDOT = 1869
498278 Wp = 69
77463
YDOT = -7396
840296 meter/sec RA = 109
02576 deg
ZDOT = 823
597859 TA = 12
40399
MA = 12
38632
Ha = 223
397 n
mi
Hp = 213
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13806225
74 X = -4228180
67
Y = -1561767
94 feet Y = -523197
55 meter
Z = 17344450
69 Z = 5266098
65
XDOT = 6133
524533 XDOT = 1948
072330
YDOT = -24267
848739 feet/sec YDOT = -7375
494987 meter/sec
ZDOT = 2702
092714 ZDOT = 832
869438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13762727
39 X = -4194879
31
Y = -2611314
18 feet Y = -795928
56 meter
Z = 17252516
66 Z = 5258567
08
XDOT = 7747
152260 XDOT = 2361
332009
YDOT = -22730
600142 feet/sec YDOT = -6928
286923 meter/sec
ZDOT = 2744
610814 ZDOT = 836
557376
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
15525084
00016717 00000-0 10270-3 0 9080
2 25544 51
6402 109
7509 0005662 43
3371 316
8226 15
53825102 6906
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
15525084 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 109
7509 deg
Eccentricity:
0005662
Arg of perigee: 43
3371 deg
Mean anomaly: 316
8226 deg
Mean motion: 15
53825102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 290
Coasting Arc #10 (Orbit 700)
---------------------------------------
Vector Time (GMT): 2018/222/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4287377
75 A = 6778583
93 meter
Y = 123641
85 meter E =
0007179
Z = 5242745
27 I = 51
98715
XDOT = 1165
720111 Wp = 77
66659
YDOT = -7500
051156 meter/sec RA = 105
51952 deg
ZDOT = 1130
365272 TA = 1
55903
MA = 1
55679
Ha = 223
263 n
mi
Hp = 213
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14066199
96 X = -4313907
56
Y = 405649
10 feet Y = 75548
88 meter
Z = 17200607
85 Z = 5221854
76
XDOT = 3824
541046 XDOT = 1244
010533
YDOT = -24606
467046 feet/sec YDOT = -7486
577564 meter/sec
ZDOT = 3708
547481 ZDOT = 1136
217645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4267473
75 X = 1300726
00
Y = -13528843
65 feet Y = -4123591
54 meter
Z = 17106796
90 Z = 5214151
70
XDOT = 21011
307333 XDOT = 6404
246475
YDOT = 11350
616761 feet/sec YDOT = 3459
667989 meter/sec
ZDOT = 3735
733686 ZDOT = 1138
651628
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
86271443
00016717 00000-0 10270-3 0 9096
2 25544 51
6404 106
2221 0005284 45
6831 314
4754 15
53849147 7015
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
86271443 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 106
2221 deg
Eccentricity:
0005284
Arg of perigee: 45
6831 deg
Mean anomaly: 314
4754 deg
Mean motion: 15
53849147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 701
Checksum: 295
Coasting Arc #11 (Orbit 715)
---------------------------------------
Vector Time (GMT): 2018/223/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3940847
27 A = 6778354
26 meter
Y = 1526996
83 meter E =
0018850
Z = -5315366
81 I = 51
99351
XDOT = -1925
884485 Wp = 83
76676
YDOT = 7375
436078 meter/sec RA = 100
54830 deg
ZDOT = 695
049569 TA = 192
82685
MA = 192
87487
Ha = 223
221 n
mi
Hp = 213
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12929288
93 X = 3949297
66
Y = 5009832
13 feet Y = 1571113
41 meter
Z = -17438867
50 Z = -5296203
50
XDOT = -6318
518652 XDOT = -2011
591612
YDOT = 24197
624928 feet/sec YDOT = 7353
420280 meter/sec
ZDOT = 2280
346356 ZDOT = 685
486442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8825752
07 X = -2690089
23
Y = 10833202
43 feet Y = 3301960
10 meter
Z = -17353007
10 Z = -5289196
56
XDOT = -20227
281286 XDOT = -6165
275336
YDOT = -12918
197547 feet/sec YDOT = -3937
466612 meter/sec
ZDOT = 2236
505346 ZDOT = 681
686829
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
82743706
00016717 00000-0 10270-3 0 9101
2 25544 51
6398 101
4166 0005390 50
6650 309
4979 15
53839681 7166
Satellite: ISS
Catalog Number: 25544
Epoch time: 18223
82743706 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 101
4166 deg
Eccentricity:
0005390
Arg of perigee: 50
6650 deg
Mean anomaly: 309
4979 deg
Mean motion: 15
53839681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 716
Checksum: 321
Coasting Arc #12 (Orbit 731)
---------------------------------------
Vector Time (GMT): 2018/224/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3516966
67 A = 6780293
86 meter
Y = -3133012
19 meter E =
0012435
Z = 4870782
87 I = 52
00488
XDOT = 2602
281590 Wp = 57
60369
YDOT = -6781
352048 meter/sec RA = 95
57718 deg
ZDOT = -2471
881337 TA = 56
58599
MA = 56
46711
Ha = 223
423 n
mi
Hp = 213
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11538604
56 X = -3505330
21
Y = -10278911
38 feet Y = -3172276
19 meter
Z = 15980258
77 Z = 4853727
39
XDOT = 8537
669260 XDOT = 2689
925949
YDOT = -22248
530341 feet/sec YDOT = -6751
761528 meter/sec
ZDOT = -8109
846906 ZDOT = -2459
027667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13258580
35 X = 4041215
29
Y = -8089192
83 feet Y = -2465585
98 meter
Z = 15904058
95 Z = 4847557
17
XDOT = 18128
944445 XDOT = 5525
702267
YDOT = 13812
919899 feet/sec YDOT = 4210
177985 meter/sec
ZDOT = -8051
294580 ZDOT = -2454
034588
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
85647241
00016717 00000-0 10270-3 0 9113
2 25544 51
6400 96
2884 0005401 54
7657 305
4000 15
53803477 7326
Satellite: ISS
Catalog Number: 25544
Epoch time: 18224
85647241 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 96
2884 deg
Eccentricity:
0005401
Arg of perigee: 54
7657 deg
Mean anomaly: 305
4000 deg
Mean motion: 15
53803477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 732
Checksum: 293
Coasting Arc #13 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2018/225/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3083909
72 A = 6783456
09 meter
Y = 4525574
52 meter E =
0011066
Z = -4011806
19 I = 52
01868
XDOT = -3183
425241 Wp = 85
37330
YDOT = 5704
944345 meter/sec RA = 90
61440 deg
ZDOT = 3998
752051 TA = 226
05848
MA = 226
14983
Ha = 223
307 n
mi
Hp = 213
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10117814
03 X = 3052561
15
Y = 14847685
43 feet Y = 4559885
51 meter
Z = -13162093
80 Z = -3996902
22
XDOT = -10444
308535 XDOT = -3266
406356
YDOT = 18717
009007 feet/sec YDOT = 5668
881249 meter/sec
ZDOT = 13119
265258 ZDOT = 3983
086631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17103717
22 X = -5213213
01
Y = 5659445
76 feet Y = 1724999
07 meter
Z = -13095730
90 Z = -3991578
78
XDOT = -14625
532514 XDOT = -4457
862310
YDOT = -14086
435416 feet/sec YDOT = -4293
545515 meter/sec
ZDOT = 13048
211345 ZDOT = 3977
094818
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
82118820
00016717 00000-0 10270-3 0 9128
2 25544 51
6408 91
4818 0005355 56
5661 303
6003 15
53828240 7475
Satellite: ISS
Catalog Number: 25544
Epoch time: 18225
82118820 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 91
4818 deg
Eccentricity:
0005355
Arg of perigee: 56
5661 deg
Mean anomaly: 303
6003 deg
Mean motion: 15
53828240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 297
Coasting Arc #14 (Orbit 762)
---------------------------------------
Vector Time (GMT): 2018/226/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2572297
46 A = 6787089
77 meter
Y = -5644417
82 meter E =
0018034
Z = 2739129
68 I = 52
02935
XDOT = 3739
154775 Wp = 90
10923
YDOT = -4235
870139 meter/sec RA = 85
66003 deg
ZDOT = -5187
932261 TA = 59
06554
MA = 58
88840
Ha = 223
406 n
mi
Hp = 213
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8439296
11 X = -2522293
89
Y = -18518431
17 feet Y = -5672903
33 meter
Z = 8986645
92 Z = 2726756
23
XDOT = 12267
568159 XDOT = 3811
443405
YDOT = -13897
211741 feet/sec YDOT = -4193
652351 meter/sec
ZDOT = -17020
775133 ZDOT = -5169
593265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20098732
74 X = 6126093
74
Y = -3343323
34 feet Y = -1019044
95 meter
Z = 8931794
23 Z = 2722410
88
XDOT = 9920
157974 XDOT = 3023
664150
YDOT = 14127
142491 feet/sec YDOT = 4305
953031 meter/sec
ZDOT = -16937
891261 ZDOT = -5162
669256
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 18226
85021749
00016717 00000-0 10270-3 0 9136
2 25544 51
6401 86
3540 0005459 61
7205 298
4498 15
53819421 7638
Satellite: ISS
Catalog Number: 25544
Epoch time: 18226
85021749 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 86
3540 deg
Eccentricity:
0005459
Arg of perigee: 61
7205 deg
Mean anomaly: 298
4498 deg
Mean motion: 15
53819421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 763
Checksum: 318
Coasting Arc #15 (Orbit 765)
---------------------------------------
Vector Time (GMT): 2018/227/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3411248
23 A = 6783962
12 meter
Y = -4433590
47 meter E =
0016787
Z = 3827599
22 I = 52
01809
XDOT = 2768
178085 Wp = 74
61217
YDOT = -5783
508599 meter/sec RA = 84
71661 deg
ZDOT = -4212
435611 TA = 59
62735
MA = 59
46149
Ha = 223
424 n
mi
Hp = 213
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11191759
29 X = -3380009
26
Y = -14545900
51 feet Y = -4471562
58 meter
Z = 12557740
22 Z = 3811104
86
XDOT = 9081
949098 XDOT = 2853
106641
YDOT = -18974
765744 feet/sec YDOT = -5752
078229 meter/sec
ZDOT = -13820
326809 ZDOT = -4198
782437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -404995
10 X = -123442
51
Y = -18398789
22 feet Y = -5607950
95 meter
Z = 12484232
91 Z = 3805194
19
XDOT = 17323
365216 XDOT = 5280
161718
YDOT = -9760
834532 feet/sec YDOT = -2975
102365 meter/sec
ZDOT = -13758
287579 ZDOT = -4193
526054
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 18227
04315851
00016717 00000-0 10270-3 0 9149
2 25544 51
6394 85
3954 0005677 58
3581 301
8125 15
53862167 7662
Satellite: ISS
Catalog Number: 25544
Epoch time: 18227
04315851 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 85
3954 deg
Eccentricity:
0005677
Arg of perigee: 58
3581 deg
Mean anomaly: 301
8125 deg
Mean motion: 15
53862167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 766
Checksum: 325
Coasting Arc #16 (Orbit 780)
---------------------------------------
Vector Time (GMT): 2018/228/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3024408
99 A = 6787341
68 meter
Y = 5510757
98 meter E =
0010908
Z = -2558351
00 I = 52
02606
XDOT = -3428
023664 Wp = 57
30377
YDOT = 4335
801073 meter/sec RA = 79
76338 deg
ZDOT = 5309
040264 TA = 274
12840
MA = 274
25306
Ha = 223
446 n
mi
Hp = 213
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9922601
67 X = 2974988
38
Y = 18079914
65 feet Y = 5544302
60 meter
Z = -8393540
04 Z = -2543779
86
XDOT = -11246
796799 XDOT = -3502
041263
YDOT = 14225
069136 feet/sec YDOT = 4297
052875 meter/sec
ZDOT = 17418
111104 ZDOT = 5292
208358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2388016
44 X = -727867
41
Y = 20511485
75 feet Y = 6251900
86 meter
Z = -8328816
34 Z = -2538623
22
XDOT = -16018
806392 XDOT = -4882
532188
YDOT = 5147
158484 feet/sec YDOT = 1568
853906 meter/sec
ZDOT = 17341
972369 ZDOT = 5285
833178
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 18228
00787244
00016717 00000-0 10270-3 0 9156
2 25544 51
6400 80
5882 0005751 63
6864 296
4879 15
53870687 7811
Satellite: ISS
Catalog Number: 25544
Epoch time: 18228
00787244 = yrday
fracday
Element set: 915
Inclination: 51
6400 deg
RA of node: 80
5882 deg
Eccentricity:
0005751
Arg of perigee: 63
6864 deg
Mean anomaly: 296
4879 deg
Mean motion: 15
53870687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 781
Checksum: 341
Coasting Arc #17 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2018/229/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2497659
68 A = 6789746
29 meter
Y = -6228092
50 meter E =
0017305
Z = 998545
27 I = 52
02716
XDOT = 4094
196726 Wp = 107
66096
YDOT = -2606
466786 meter/sec RA = 74
81756 deg
ZDOT = -5936
935658 TA = 61
57788
MA = 61
40360
Ha = 223
499 n
mi
Hp = 213
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8194421
51 X = -2432680
16
Y = -20433374
35 feet Y = -6255659
71 meter
Z = 3276067
16 Z = 986570
58
XDOT = 13432
403958 XDOT = 4151
876944
YDOT = -8551
400216 feet/sec YDOT = -2560
360282 meter/sec
ZDOT = -19478
135360 ZDOT = -5916
907471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4821100
30 X = 1469471
37
Y = -21488892
69 feet Y = -6549814
49 meter
Z = 3223108
79 Z = 982403
56
XDOT = 14453
194964 XDOT = 4405
333825
YDOT = 295
018300 feet/sec YDOT = 89
921578 meter/sec
ZDOT = -19387
860508 ZDOT = -5909
419883
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 18229
03689659
00016717 00000-0 10270-3 0 9162
2 25544 51
6403 75
4603 0005806 66
1972 293
9789 15
53845130 7971
Satellite: ISS
Catalog Number: 25544
Epoch time: 18229
03689659 = yrday
fracday
Element set: 916
Inclination: 51
6403 deg
RA of node: 75
4603 deg
Eccentricity:
0005806
Arg of perigee: 66
1972 deg
Mean anomaly: 293
9789 deg
Mean motion: 15
53845130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 347
Coasting Arc #18 (Orbit 812)
---------------------------------------
Vector Time (GMT): 2018/230/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1880418
77 A = 6790010
48 meter
Y = 6488404
91 meter E =
0018808
Z = 597932
77 I = 52
01868
XDOT = -4703
084911 Wp = 56
53141
YDOT = 797
836309 meter/sec RA = 69
87509 deg
ZDOT = 6007
533777 TA = 309
89099
MA = 310
05620
Ha = 223
547 n
mi
Hp = 213
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6169352
93 X = 1804819
46
Y = 21287417
68 feet Y = 6509010
36 meter
Z = 1961721
69 Z = 606883
44
XDOT = -15430
068606 XDOT = -4740
838222
YDOT = 2617
573193 feet/sec YDOT = 745
032138 meter/sec
ZDOT = 19709
756485 ZDOT = 5984
596277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6639512
18 X = -2023723
31
Y = 21141808
99 feet Y = 6444023
38 meter
Z = 2001052
13 Z = 609920
69
XDOT = -12872
466318 XDOT = -3923
527734
YDOT = -5936
480574 feet/sec YDOT = -1809
439279 meter/sec
ZDOT = 19606
652210 ZDOT = 5976
107594
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 18230
06591865
00016717 00000-0 10270-3 0 9179
2 25544 51
6406 70
3334 0005871 68
4744 291
7034 15
53841788 8136
Satellite: ISS
Catalog Number: 25544
Epoch time: 18230
06591865 = yrday
fracday
Element set: 917
Inclination: 51
6406 deg
RA of node: 70
3334 deg
Eccentricity:
0005871
Arg of perigee: 68
4744 deg
Mean anomaly: 291
7034 deg
Mean motion: 15
53841788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 813
Checksum: 319
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