[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 31st 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24007 8258 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
307/06:05:00
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
8
311/16:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
2
319/09:49:38
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2018/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4941503
97 A = 6782093
01 meter
Y = -1519697
03 meter E =
0011228
Z = 4386270
96 I = 51
96142
XDOT = -977
809765 Wp = 51
29152
YDOT = -6784
182828 meter/sec RA = 58
68355 deg
ZDOT = -3439
322470 TA = 73
48088
MA = 73
35755
Ha = 221
935 n
mi
Hp = 215
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16212283
38 X = -4945449
49
Y = -4985882
65 feet Y = -1574978
45 meter
Z = 14390652
77 Z = 4362256
96
XDOT = -3208
037287 XDOT = -885
167844
YDOT = -22257
817678 feet/sec YDOT = -6794
599359 meter/sec
ZDOT = -11283
866370 ZDOT = -3443
847423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15825951
55 X = 4823750
03
Y = -6350511
62 feet Y = -1935635
94 meter
Z = 14282797
52 Z = 4353396
69
XDOT = 15942
257447 XDOT = 4859
200070
YDOT = 14212
372428 feet/sec YDOT = 4331
931116 meter/sec
ZDOT = -11303
337706 ZDOT = -3445
257333
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 18304
54201707
00016717 00000-0 10270-3 0 9009
2 25544 51
6405 59
2264 0003934 355
8516 4
2603 15
53853173 19717
Satellite: ISS
Catalog Number: 25544
Epoch time: 18304
54201707 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 59
2264 deg
Eccentricity:
0003934
Arg of perigee: 355
8516 deg
Mean anomaly: 4
2603 deg
Mean motion: 15
53853173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 290
Coasting Arc #2 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2018/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5238046
04 A = 6785649
95 meter
Y = 2807320
82 meter E =
0006483
Z = -3273525
89 I = 51
95652
XDOT = -234
912392 Wp = 41
73912
YDOT = 5992
793646 meter/sec RA = 53
72182 deg
ZDOT = 4773
557233 TA = 280
48067
MA = 280
55371
Ha = 221
981 n
mi
Hp = 215
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17185190
42 X = 5222165
73
Y = 9210370
14 feet Y = 2865807
45 meter
Z = -10739914
33 Z = -3248119
60
XDOT = -770
709947 XDOT = -325
095704
YDOT = 19661
396476 feet/sec YDOT = 5989
662511 meter/sec
ZDOT = 15661
277012 ZDOT = 4772
196975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19149623
40 X = -5836805
21
Y = 3985998
35 feet Y = 1214932
30 meter
Z = -10625967
66 Z = -3238794
94
XDOT = -11636
127538 XDOT = -3546
691673
YDOT = -14260
300663 feet/sec YDOT = -4346
539642 meter/sec
ZDOT = 15654
363175 ZDOT = 4771
449896
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 18305
50670199
00016717 00000-0 10270-3 0 9012
2 25544 51
6417 54
4197 0004156 357
1015 3
0113 15
53863502 19864
Satellite: ISS
Catalog Number: 25544
Epoch time: 18305
50670199 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 54
4197 deg
Eccentricity:
0004156
Arg of perigee: 357
1015 deg
Mean anomaly: 3
0113 deg
Mean motion: 15
53863502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 290
Coasting Arc #3 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2018/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5275540
30 A = 6788725
31 meter
Y = -3858960
21 meter E =
0013039
Z = 1819019
37 I = 51
94607
XDOT = 1614
277891 Wp = 97
30151
YDOT = -4897
182423 meter/sec RA = 48
76761 deg
ZDOT = -5674
241368 TA = 62
79215
MA = 62
65932
Ha = 222
017 n
mi
Hp = 214
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17308203
08 X = -5240832
18
Y = -12660630
61 feet Y = -3917760
84 meter
Z = 5967911
33 Z = 1793476
75
XDOT = 5296
187308 XDOT = 1696
482381
YDOT = -16066
871468 feet/sec YDOT = -4878
671004 meter/sec
ZDOT = -18616
277455 ZDOT = -5666
199844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21403446
20 X = 6523770
40
Y = -1763653
72 feet Y = -537561
66 meter
Z = 5853498
38 Z = 1784146
31
XDOT = 6276
698734 XDOT = 1913
137774
YDOT = 14140
706171 feet/sec YDOT = 4310
087241 meter/sec
ZDOT = -18579
441093 ZDOT = -5663
013645
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 18306
53569833
00016717 00000-0 10270-3 0 9029
2 25544 51
6414 49
2919 0004081 3
4853 356
6327 15
53872835 20026
Satellite: ISS
Catalog Number: 25544
Epoch time: 18306
53569833 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 49
2919 deg
Eccentricity:
0004081
Arg of perigee: 3
4853 deg
Mean anomaly: 356
6327 deg
Mean motion: 15
53872835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2002
Checksum: 309
Coasting Arc #4 (Orbit 2013)
---------------------------------------
Vector Time (GMT): 2018/307/06:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 60804
30 A = 6781469
86 meter
Y = 5061646
01 meter E =
0008640
Z = 4504621
15 I = 51
90180
XDOT = -6371
354902 Wp = 81
31481
YDOT = -2801
192340 meter/sec RA = 45
06771 deg
ZDOT = 3229
579122 TA = 336
33046
MA = 336
37019
Ha = 222
186 n
mi
Hp = 214
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 199489
18 X = -17682
34
Y = 16606450
15 feet Y = 5061887
32 meter
Z = 14778940
78 Z = 4504725
66
XDOT = -20903
395347 XDOT = -6355
245469
YDOT = -9190
263583 feet/sec YDOT = -2872
351038 meter/sec
ZDOT = 10595
732027 ZDOT = 3198
668106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12111764
06 X = 3691665
69
Y = -11363333
89 feet Y = -3463544
17 meter
Z = 14778730
92 Z = 4504557
18
XDOT = 6688
465686 XDOT = 2038
644341
YDOT = 20746
087501 feet/sec YDOT = 6323
407470 meter/sec
ZDOT = 10457
030611 ZDOT = 3187
302930
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 18307
30744393
00016717 00000-0 10270-3 0 9032
2 25544 51
6381 45
4473 0004619 3
7866 356
3320 15
53867449 20144
Satellite: ISS
Catalog Number: 25544
Epoch time: 18307
30744393 = yrday
fracday
Element set: 903
Inclination: 51
6381 deg
RA of node: 45
4473 deg
Eccentricity:
0004619
Arg of perigee: 3
7866 deg
Mean anomaly: 356
3320 deg
Mean motion: 15
53867449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2014
Checksum: 310
Coasting Arc #5 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2018/308/06:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1294469
34 A = 6778785
30 meter
Y = -4210979
66 meter E =
0015860
Z = -5165889
10 I = 51
86875
XDOT = 6437
319966 Wp = 62
95391
YDOT = 3854
091786 meter/sec RA = 40
09138 deg
ZDOT = -1525
181654 TA = 192
35674
MA = 192
39568
Ha = 222
194 n
mi
Hp = 214
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4246946
65 X = 1366555
10
Y = -13815550
06 feet Y = -4196101
21 meter
Z = -16948455
05 Z = -5159425
60
XDOT = 21119
816163 XDOT = 6401
152662
YDOT = 12644
658089 feet/sec YDOT = 3925
876067 meter/sec
ZDOT = -5003
876817 ZDOT = -1493
998869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12988718
84 X = -3958961
50
Y = 6418983
36 feet Y = 1956506
13 meter
Z = -16918804
43 Z = -5156851
59
XDOT = -5050
914965 XDOT = -1539
518881
YDOT = -23070
631644 feet/sec YDOT = -7031
928525 meter/sec
ZDOT = -4864
108067 ZDOT = -1482
580139
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 18308
27212550
00016717 00000-0 10270-3 0 9045
2 25544 51
6380 40
6397 0004493 9
1946 350
9288 15
53889782 20297
Satellite: ISS
Catalog Number: 25544
Epoch time: 18308
27212550 = yrday
fracday
Element set: 904
Inclination: 51
6380 deg
RA of node: 40
6397 deg
Eccentricity:
0004493
Arg of perigee: 9
1946 deg
Mean anomaly: 350
9288 deg
Mean motion: 15
53889782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2029
Checksum: 326
Coasting Arc #6 (Orbit 2044)
---------------------------------------
Vector Time (GMT): 2018/309/06:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2703221
15 A = 6778184
59 meter
Y = 3209712
29 meter E =
0006244
Z = 5320216
72 I = 51
84094
XDOT = -6120
870407 Wp = 33
91650
YDOT = -4612
516805 meter/sec RA = 35
10856 deg
ZDOT = -322
045447 TA = 59
17482
MA = 59
11339
Ha = 222
450 n
mi
Hp = 214
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8868835
79 X = -2764755
52
Y = 10530552
12 feet Y = 3179139
19 meter
Z = 17454779
28 Z = 5306935
50
XDOT = -20081
595824 XDOT = -6067
272677
YDOT = -15132
929151 feet/sec YDOT = -4680
664963 meter/sec
ZDOT = -1056
579551 ZDOT = -351
648766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13804153
16 X = 4207505
88
Y = -1044823
32 feet Y = -318462
15 meter
Z = 17394590
99 Z = 5301871
33
XDOT = 3329
170957 XDOT = 1014
731308
YDOT = 23900
852040 feet/sec YDOT = 7284
979702 meter/sec
ZDOT = -1189
122778 ZDOT = -362
444623
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 18309
30111767
00016717 00000-0 10270-3 0 9059
2 25544 51
6387 35
5114 0004546 13
2181 346
9089 15
53855505 20458
Satellite: ISS
Catalog Number: 25544
Epoch time: 18309
30111767 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 35
5114 deg
Eccentricity:
0004546
Arg of perigee: 13
2181 deg
Mean anomaly: 346
9089 deg
Mean motion: 15
53855505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2045
Checksum: 301
Coasting Arc #7 (Orbit 2059)
---------------------------------------
Vector Time (GMT): 2018/310/06:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4041640
46 A = 6779578
61 meter
Y = -2194113
35 meter E =
0013455
Z = -4992609
17 I = 51
81815
XDOT = 5357
367738 Wp = 86
00638
YDOT = 5042
444103 meter/sec RA = 30
12558 deg
ZDOT = 2126
757166 TA = 204
65001
MA = 204
71438
Ha = 222
398 n
mi
Hp = 214
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13259975
27 X = 4090127
36
Y = -7198534
61 feet Y = -2148645
99 meter
Z = -16379951
36 Z = -4972857
93
XDOT = 17576
665806 XDOT = 5290
252615
YDOT = 16543
451782 feet/sec YDOT = 5101
978726 meter/sec
ZDOT = 6977
549757 ZDOT = 2152
618872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14602256
35 X = -4450767
74
Y = -4163249
25 feet Y = -1268958
37 meter
Z = -16290798
52 Z = -4965435
39
XDOT = -1329
433616 XDOT = -405
211366
YDOT = -23017
245383 feet/sec YDOT = -7015
656393 meter/sec
ZDOT = 7093
184640 ZDOT = 2162
002678
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 18310
26579475
00016717 00000-0 10270-3 0 9061
2 25544 51
6387 30
7041 0004483 18
9670 341
1648 15
53895123 20604
Satellite: ISS
Catalog Number: 25544
Epoch time: 18310
26579475 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 30
7041 deg
Eccentricity:
0004483
Arg of perigee: 18
9670 deg
Mean anomaly: 341
1648 deg
Mean motion: 15
53895123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2060
Checksum: 309
Coasting Arc #8 (Orbit 2075)
---------------------------------------
Vector Time (GMT): 2018/311/06:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5219336
92 A = 6782831
96 meter
Y = 1170844
18 meter E =
0013457
Z = 4165177
86 I = 51
79890
XDOT = -4178
577350 Wp = 60
19085
YDOT = -5223
536007 meter/sec RA = 25
14717 deg
ZDOT = -3752
166279 TA = 68
38249
MA = 68
23919
Ha = 222
519 n
mi
Hp = 214
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17123808
79 X = -5252274
52
Y = 3841352
29 feet Y = 1112293
84 meter
Z = 13665281
70 Z = 4139743
40
XDOT = -13709
243275 XDOT = -4101
629192
YDOT = -17137
585325 feet/sec YDOT = -5269
833586 meter/sec
ZDOT = -12310
256821 ZDOT = -3772
277936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15173926
33 X = 4625012
75
Y = 8991713
94 feet Y = 2740674
41 meter
Z = 13550711
37 Z = 4130256
83
XDOT = -1155
132918 XDOT = -352
084513
YDOT = 20714
221652 feet/sec YDOT = 6313
694760 meter/sec
ZDOT = -12399
985404 ZDOT = -3779
515551
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18311
29478304
00016717 00000-0 10270-3 0 9075
2 25544 51
6380 25
5766 0004407 21
3165 338
8170 15
53874966 20768
Satellite: ISS
Catalog Number: 25544
Epoch time: 18311
29478304 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 25
5766 deg
Eccentricity:
0004407
Arg of perigee: 21
3165 deg
Mean anomaly: 338
8170 deg
Mean motion: 15
53874966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2076
Checksum: 317
Coasting Arc #9 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2018/311/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4194165
15 A = 6780336
72 meter
Y = 2322334
91 meter E =
0011582
Z = 4790777
42 I = 51
77897
XDOT = -5554
287790 Wp = 46
24065
YDOT = -4593
344608 meter/sec RA = 22
92842 deg
ZDOT = -2624
185773 TA = 69
63671
MA = 69
51232
Ha = 222
576 n
mi
Hp = 214
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13760384
35 X = -4243094
16
Y = 7619209
01 feet Y = 2275159
30 meter
Z = 15717773
67 Z = 4770284
17
XDOT = -18222
728971 XDOT = -5489
763645
YDOT = -15070
028241 feet/sec YDOT = -4655
095757 meter/sec
ZDOT = -8609
533375 ZDOT = -2651
010588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13306445
81 X = -4055804
68
Y = -8557945
71 feet Y = -2608461
85 meter
Z = 15625267
93 Z = 4762581
66
XDOT = 3969
276157 XDOT = 1209
835373
YDOT = -22181
225175 feet/sec YDOT = -6760
837433 meter/sec
ZDOT = -8729
539924 ZDOT = -2660
763769
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18311
74496305
00016717 00000-0 10270-3 0 9087
2 25544 51
6395 23
3369 0004707 21
9486 338
1867 15
53910403 20835
Satellite: ISS
Catalog Number: 25544
Epoch time: 18311
74496305 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 23
3369 deg
Eccentricity:
0004707
Arg of perigee: 21
9486 deg
Mean anomaly: 338
1867 deg
Mean motion: 15
53910403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 316
Coasting Arc #10 (Orbit 2097)
---------------------------------------
Vector Time (GMT): 2018/312/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5376491
69 A = 6783802
26 meter
Y = -1466484
93 meter E =
0008683
Z = -3872882
58 I = 51
75964
XDOT = 4287
388652 Wp = 70
60229
YDOT = 4817
040771 meter/sec RA = 17
95011 deg
ZDOT = 4138
304136 TA = 242
79683
MA = 242
88536
Ha = 222
708 n
mi
Hp = 214
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17639408
42 X = 5411303
69
Y = -4811302
27 feet Y = -1406166
57 meter
Z = -12706307
68 Z = -3846680
18
XDOT = 14066
235734 XDOT = 4213
102240
YDOT = 15803
939538 feet/sec YDOT = 4864
569907 meter/sec
ZDOT = 13577
113308 ZDOT = 4158
951010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12903244
35 X = 3932908
88
Y = 13068662
03 feet Y = 3983328
19 meter
Z = -12588247
38 Z = -3836897
80
XDOT = -5940
333296 XDOT = -1810
613589
YDOT = 18998
847033 feet/sec YDOT = 5790
848576 meter/sec
ZDOT = 13669
287379 ZDOT = 4166
398793
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18312
70963686
00016717 00000-0 10270-3 0 9096
2 25544 51
6398 18
5306 0004891 26
7636 333
3768 15
53883649 20983
Satellite: ISS
Catalog Number: 25544
Epoch time: 18312
70963686 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 18
5306 deg
Eccentricity:
0004891
Arg of perigee: 26
7636 deg
Mean anomaly: 333
3768 deg
Mean motion: 15
53883649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2098
Checksum: 353
Coasting Arc #11 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2018/313/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6254792
13 A = 6787255
09 meter
Y = 621599
94 meter E =
0015611
Z = 2549093
77 I = 51
73838
XDOT = -2650
263313 Wp = 86
04809
YDOT = -4886
187432 meter/sec RA = 12
97779 deg
ZDOT = -5282
597330 TA = 65
35595
MA = 65
19343
Ha = 222
668 n
mi
Hp = 214
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20520971
56 X = -6273660
64
Y = 2039369
88 feet Y = 551548
92 meter
Z = 8363168
55 Z = 2518663
56
XDOT = -8695
089609 XDOT = -2569
766881
YDOT = -16030
798661 feet/sec YDOT = -4915
374249 meter/sec
ZDOT = -17331
356068 ZDOT = -5295
276382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12180574
00 X = -3712638
96
Y = -16708525
74 feet Y = -5092758
64 meter
Z = 8226218
83 Z = 2507351
50
XDOT = 8259
773492 XDOT = 2517
578960
YDOT = -14629
507453 feet/sec YDOT = -4459
073872 meter/sec
ZDOT = -17387
674214 ZDOT = -5299
763100
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18313
73861917
00016717 00000-0 10270-3 0 9106
2 25544 51
6384 13
4022 0004963 28
0643 332
0776 15
53926506 21144
Satellite: ISS
Catalog Number: 25544
Epoch time: 18313
73861917 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 13
4022 deg
Eccentricity:
0004963
Arg of perigee: 28
0643 deg
Mean anomaly: 332
0776 deg
Mean motion: 15
53926506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 294
Coasting Arc #12 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2018/314/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6703618
88 A = 6789507
85 meter
Y = 125663
40 meter E =
0014617
Z = -1026064
44 I = 51
71311
XDOT = 805
521287 Wp = 36
84403
YDOT = 4823
376258 meter/sec RA = 8
01233 deg
ZDOT = 5908
442254 TA = 312
04412
MA = 312
16841
Ha = 222
729 n
mi
Hp = 213
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21993500
28 X = 6706699
65
Y = 412281
48 feet Y = 200645
19 meter
Z = -3366353
15 Z = -993492
34
XDOT = 2642
786374 XDOT = 722
824318
YDOT = 15824
725255 feet/sec YDOT = 4831
921482 meter/sec
ZDOT = 19384
653064 ZDOT = 5912
154660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11123803
53 X = 3390535
32
Y = 19002886
81 feet Y = 5792079
90 meter
Z = -3219883
84 Z = -981420
60
XDOT = -10810
198837 XDOT = -3294
948606
YDOT = 9583
340525 feet/sec YDOT = 2921
002192 meter/sec
ZDOT = 19400
647417 ZDOT = 5913
317333
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18314
70329055
00016717 00000-0 10270-3 0 9117
2 25544 51
6381 8
5959 0004829 34
4889 325
6576 15
53926010 21291
Satellite: ISS
Catalog Number: 25544
Epoch time: 18314
70329055 = yrday
fracday
Element set: 911
Inclination: 51
6381 deg
RA of node: 8
5959 deg
Eccentricity:
0004829
Arg of perigee: 34
4889 deg
Mean anomaly: 325
6576 deg
Mean motion: 15
53926010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2129
Checksum: 322
Coasting Arc #13 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2018/315/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6701972
95 A = 6789739
58 meter
Y = -864488
96 meter E =
0010555
Z = -641656
72 I = 51
68196
XDOT = 1165
088707 Wp = 111
78488
YDOT = -4662
568448 meter/sec RA = 3
04653 deg
ZDOT = -5970
030857 TA = 75
13516
MA = 75
01829
Ha = 222
759 n
mi
Hp = 213
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21988100
24 X = -6688691
00
Y = -2836249
86 feet Y = -939360
77 meter
Z = -2105172
98 Z = -674181
01
XDOT = 3822
469510 XDOT = 1246
140088
YDOT = -15297
140579 feet/sec YDOT = -4649
086109 meter/sec
ZDOT = -19586
715410 ZDOT = -5964
174536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9379685
88 X = -2858928
25
Y = -20072510
96 feet Y = -6118101
34 meter
Z = -2251314
21 Z = -686200
57
XDOT = 13571
205420 XDOT = 4136
503412
YDOT = -4176
344078 feet/sec YDOT = -1272
949675 meter/sec
ZDOT = -19559
697793 ZDOT = -5961
795887
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18315
73226989
00016717 00000-0 10270-3 0 9124
2 25544 51
6391 3
4669 0005010 35
8689 324
2800 15
53916906 21456
Satellite: ISS
Catalog Number: 25544
Epoch time: 18315
73226989 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 3
4669 deg
Eccentricity:
0005010
Arg of perigee: 35
8689 deg
Mean anomaly: 324
2800 deg
Mean motion: 15
53916906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2145
Checksum: 314
Coasting Arc #14 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2018/316/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6223867
70 A = 6787718
63 meter
Y = 1534949
00 meter E =
0018118
Z = 2202262
64 I = 51
64205
XDOT = -3040
463488 Wp = 63
04388
YDOT = 4436
507654 meter/sec RA = 358
07768 deg
ZDOT = 5473
897499 TA = 321
43424
MA = 321
56354
Ha = 222
649 n
mi
Hp = 213
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20419513
46 X = 6195543
29
Y = 5035921
90 feet Y = 1604390
12 meter
Z = 7225271
14 Z = 2232427
82
XDOT = -9975
273911 XDOT = -3116
437526
YDOT = 14555
471305 feet/sec YDOT = 4402
081995 meter/sec
ZDOT = 17958
981295 ZDOT = 5458
943438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7004667
95 X = 2135022
79
Y = 19780705
36 feet Y = 6029158
99 meter
Z = 7360700
01 Z = 2243541
36
XDOT = -16267
085654 XDOT = -4958
207707
YDOT = -929
030929 feet/sec YDOT = -283
168627 meter/sec
ZDOT = 17891
084596 ZDOT = 5453
202585
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18316
76124559
00016717 00000-0 10270-3 0 9139
2 25544 51
6388 358
3399 0004816 39
6739 320
4765 15
53950011 21616
Satellite: ISS
Catalog Number: 25544
Epoch time: 18316
76124559 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 358
3399 deg
Eccentricity:
0004816
Arg of perigee: 39
6739 deg
Mean anomaly: 320
4765 deg
Mean motion: 15
53950011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2161
Checksum: 329
Coasting Arc #15 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2018/317/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5316412
97 A = 6784378
02 meter
Y = -2224333
82 meter E =
0009833
Z = -3591822
42 I = 51
59751
XDOT = 4707
483341 Wp = 62
03700
YDOT = -4106
521118 meter/sec RA = 353
09798 deg
ZDOT = -4429
453291 TA = 160
41324
MA = 160
37544
Ha = 222
854 n
mi
Hp = 213
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17442299
78 X = -5273697
30
Y = -7297683
15 feet Y = -2283546
64 meter
Z = -11784194
30 Z = -3617544
43
XDOT = 15444
499150 XDOT = 4774
569987
YDOT = -13472
838315 feet/sec YDOT = -4053
503461 meter/sec
ZDOT = -14532
327070 ZDOT = -4406
422891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3778830
90 X = -1151787
66
Y = -18452064
47 feet Y = -5624189
25 meter
Z = -11899537
38 Z = -3626978
99
XDOT = 18549
579744 XDOT = 5653
911906
YDOT = 5495
757621 feet/sec YDOT = 1675
106923 meter/sec
ZDOT = -14428
164774 ZDOT = -4397
704623
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18317
72591272
00016717 00000-0 10270-3 0 9147
2 25544 51
6387 353
5319 0005024 41
9426 318
2110 15
53916560 21761
Satellite: ISS
Catalog Number: 25544
Epoch time: 18317
72591272 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 353
5319 deg
Eccentricity:
0005024
Arg of perigee: 41
9426 deg
Mean anomaly: 318
2110 deg
Mean motion: 15
53916560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2176
Checksum: 302
Coasting Arc #16 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2018/318/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4051172
27 A = 6780723
60 meter
Y = 2880744
13 meter E =
0010879
Z = 4602256
24 I = 51
55389
XDOT = -6027
330622 Wp = 89
99376
YDOT = 3693
271971 meter/sec RA = 348
10791 deg
ZDOT = 2987
724775 TA = 330
16793
MA = 330
22990
Ha = 222
651 n
mi
Hp = 213
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13291247
61 X = 3996302
28
Y = 9451260
26 feet Y = 2925740
18 meter
Z = 15099265
89 Z = 4621802
52
XDOT = -19774
706765 XDOT = -6082
694831
YDOT = 12117
034026 feet/sec YDOT = 3625
560504 meter/sec
ZDOT = 9802
246638 ZDOT = 2958
311383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -75760
44 X = -23091
78
Y = 16227403
09 feet Y = 4946112
46 meter
Z = 15186739
72 Z = 4628918
27
XDOT = -20180
199364 XDOT = -6150
924766
YDOT = -9162
207709 feet/sec YDOT = -2792
640910 meter/sec
ZDOT = 9669
450189 ZDOT = 2947
248418
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18318
75488557
00016717 00000-0 10270-3 0 9153
2 25544 51
6397 348
4048 0004797 44
6474 315
5064 15
53956354 21924
Satellite: ISS
Catalog Number: 25544
Epoch time: 18318
75488557 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 348
4048 deg
Eccentricity:
0004797
Arg of perigee: 44
6474 deg
Mean anomaly: 315
5064 deg
Mean motion: 15
53956354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 351
Coasting Arc #17 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2018/319/09:49:38
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3881667
04 A = 6780154
56 meter
Y = 2853947
80 meter E =
0010056
Z = 4761997
16 I = 51
53038
XDOT = -6084
960053 Wp = 92
01003
YDOT = 3857
742873 meter/sec RA = 344
57187 deg
ZDOT = 2642
875084 TA = 331
86785
MA = 331
92215
Ha = 222
713 n
mi
Hp = 213
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12735128
10 X = 3826333
35
Y = 9363345
80 feet Y = 2897045
77 meter
Z = 15623350
25 Z = 4780718
87
XDOT = -19963
779703 XDOT = -6140
484016
YDOT = 12656
636722 feet/sec YDOT = 3789
386094 meter/sec
ZDOT = 8670
850014 ZDOT = 2613
181341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15145197
50 X = -4616256
20
Y = -4225425
37 feet Y = -1287909
65 meter
Z = 15707118
71 Z = 4787529
78
XDOT = 13858
964200 XDOT = 4224
212288
YDOT = -17878
315364 feet/sec YDOT = -5449
310523 meter/sec
ZDOT = 8536
776621 ZDOT = 2602
009514
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18319
46230389
00016717 00000-0 10270-3 0 9161
2 25544 51
6412 344
8781 0004740 48
7122 311
4438 15
53933453 22037
Satellite: ISS
Catalog Number: 25544
Epoch time: 18319
46230389 = yrday
fracday
Element set: 916
Inclination: 51
6412 deg
RA of node: 344
8781 deg
Eccentricity:
0004740
Arg of perigee: 48
7122 deg
Mean anomaly: 311
4438 deg
Mean motion: 15
53933453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 302
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