[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 7th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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
101/03:32:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 214
7
105/08:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 214
6
108/10:36:13
344 0
3 1
0 1
0
N/A -0
8 -0
0 220
9
000/00:02:26
689 -0
4 -0
0 214
9
Coasting Arc #1 (Orbit 2704)
---------------------------------------
Vector Time (GMT): 2018/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4337579
67 A = 6779596
74 meter
Y = -2100239
68 meter E =
0009288
Z = -4777111
90 I = 51
79486
XDOT = 5292
458849 Wp = 104
11749
YDOT = 4849
629482 meter/sec RA = 25
44084 deg
ZDOT = 2675
536987 TA = 192
25951
MA = 192
28213
Ha = 220
445 n
mi
Hp = 215
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14230904
41 X = 4383947
66
Y = -6890550
13 feet Y = -2051474
97 meter
Z = -15672939
29 Z = -4755928
46
XDOT = 17363
710136 XDOT = 5224
839150
YDOT = 15910
857879 feet/sec YDOT = 4908
435508 meter/sec
ZDOT = 8778
008488 ZDOT = 2701
081574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12607878
49 X = 3842881
36
Y = -9695585
61 feet Y = -2955214
50 meter
Z = -15578073
28 Z = -4748196
74
XDOT = 19503
826664 XDOT = 5944
766367
YDOT = 11087
897175 feet/sec YDOT = 3379
591059 meter/sec
ZDOT = 8891
258675 ZDOT = 2710
055644
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 18094
51129658
00016717 00000-0 10270-3 0 9006
2 25544 51
6409 26
0109 0001935 310
0788 50
0194 15
54192740 27051
Satellite: ISS
Catalog Number: 25544
Epoch time: 18094
51129658 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 26
0109 deg
Eccentricity:
0001935
Arg of perigee: 310
0788 deg
Mean anomaly: 50
0194 deg
Mean motion: 15
54192740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2705
Checksum: 291
Coasting Arc #2 (Orbit 2720)
---------------------------------------
Vector Time (GMT): 2018/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5545691
41 A = 6783292
55 meter
Y = 1080648
39 meter E =
0010458
Z = 3747179
37 I = 51
77726
XDOT = -3882
224288 Wp = 75
99811
YDOT = -5044
830101 meter/sec RA = 20
46185 deg
ZDOT = -4278
204997 TA = 59
29021
MA = 59
18722
Ha = 220
518 n
mi
Hp = 215
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18194525
63 X = -5575565
32
Y = 3545434
37 feet Y = 1018465
84 meter
Z = 12293895
59 Z = 3720167
49
XDOT = -12736
956325 XDOT = -3804
741654
YDOT = -16551
279859 feet/sec YDOT = -5087
810820 meter/sec
ZDOT = -14036
105633 ZDOT = -4296
875163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17026521
73 X = -5189683
82
Y = 7527414
49 feet Y = 2294355
94 meter
Z = 12173180
59 Z = 3710385
44
XDOT = -15463
890935 XDOT = -4713
393957
YDOT = -12079
127903 feet/sec YDOT = -3681
718185 meter/sec
ZDOT = -14118
634531 ZDOT = -4303
359805
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 18095
54008712
00016717 00000-0 10270-3 0 9018
2 25544 51
6411 20
8829 0002004 311
8741 48
2241 15
54196375 27219
Satellite: ISS
Catalog Number: 25544
Epoch time: 18095
54008712 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 20
8829 deg
Eccentricity:
0002004
Arg of perigee: 311
8741 deg
Mean anomaly: 48
2241 deg
Mean motion: 15
54196375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2721
Checksum: 281
Coasting Arc #3 (Orbit 2735)
---------------------------------------
Vector Time (GMT): 2018/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6366172
05 A = 6786876
83 meter
Y = -149256
68 meter E =
0006235
Z = -2339876
31 I = 51
75852
XDOT = 2102
289700 Wp = 24
83295
YDOT = 5007
794890 meter/sec RA = 15
48996 deg
ZDOT = 5411
072326 TA = 309
11835
MA = 309
17376
Ha = 220
513 n
mi
Hp = 215
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20886391
23 X = 6378733
88
Y = -489687
27 feet Y = -77995
64 meter
Z = -7676759
55 Z = -2308920
95
XDOT = 6897
275919 XDOT = 2019
850631
YDOT = 16429
773260 feet/sec YDOT = 5030
843467 meter/sec
ZDOT = 17752
861962 ZDOT = 5421
084098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20210190
31 X = 6160066
01
Y = -5489217
89 feet Y = -1673113
61 meter
Z = -7538598
27 Z = -2297764
75
XDOT = 10116
741336 XDOT = 3083
582759
YDOT = 12856
006428 feet/sec YDOT = 3918
510759 meter/sec
ZDOT = 17796
749798 ZDOT = 5424
449339
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 18096
50457439
00016717 00000-0 10270-3 0 9020
2 25544 51
6415 16
0743 0002049 315
3867 44
7121 15
54200679 27369
Satellite: ISS
Catalog Number: 25544
Epoch time: 18096
50457439 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 16
0743 deg
Eccentricity:
0002049
Arg of perigee: 315
3867 deg
Mean anomaly: 44
7121 deg
Mean motion: 15
54200679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2736
Checksum: 303
Coasting Arc #4 (Orbit 2751)
---------------------------------------
Vector Time (GMT): 2018/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6713455
93 A = 6788983
07 meter
Y = -723292
28 meter E =
0011167
Z = 653113
22 I = 51
73416
XDOT = -69
752488 Wp = 125
84660
YDOT = -4806
327013 meter/sec RA = 10
52482 deg
ZDOT = -5974
663928 TA = 47
11002
MA = 47
01632
Ha = 220
533 n
mi
Hp = 215
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22025774
06 X = -6708041
42
Y = -2373006
16 feet Y = -798336
45 meter
Z = 2142759
91 Z = 620514
64
XDOT = -228
846747 XDOT = 13
020232
YDOT = -15768
789412 feet/sec YDOT = -4806
644512 meter/sec
ZDOT = -19601
915775 ZDOT = -5974
801489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21912083
53 X = -6678803
06
Y = 3350857
68 feet Y = 1021341
42 meter
Z = 1997410
62 Z = 608810
76
XDOT = -3890
669715 XDOT = -1185
876129
YDOT = -13621
031041 feet/sec YDOT = -4151
690261 meter/sec
ZDOT = -19601
768917 ZDOT = -5974
619166
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 18097
53335701
00016717 00000-0 10270-3 0 9032
2 25544 51
6421 10
9453 0001992 320
7607 39
3402 15
54193612 27523
Satellite: ISS
Catalog Number: 25544
Epoch time: 18097
53335701 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 10
9453 deg
Eccentricity:
0001992
Arg of perigee: 320
7607 deg
Mean anomaly: 39
3402 deg
Mean motion: 15
54193612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2752
Checksum: 289
Coasting Arc #5 (Orbit 2767)
---------------------------------------
Vector Time (GMT): 2018/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6528095
50 A = 6788600
22 meter
Y = 1487694
36 meter E =
0013758
Z = 1074036
19 I = 51
70018
XDOT = -1998
099123 Wp = 47
88724
YDOT = 4483
291483 meter/sec RA = 5
55986 deg
ZDOT = 5895
285840 TA = 323
75644
MA = 323
84957
Ha = 220
566 n
mi
Hp = 214
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21417636
16 X = 6505757
41
Y = 4880887
00 feet Y = 1560571
17 meter
Z = 3523740
77 Z = 1105693
14
XDOT = -6555
443317 XDOT = -2076
720251
YDOT = 14708
961558 feet/sec YDOT = 4460
508067 meter/sec
ZDOT = 19341
488978 ZDOT = 5885
388564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21914138
80 X = 6679429
51
Y = -1137981
14 feet Y = -346856
65 meter
Z = 3664759
91 Z = 1117018
82
XDOT = -2501
179028 XDOT = -762
359368
YDOT = 14377
399027 feet/sec YDOT = 4382
231223 meter/sec
ZDOT = 19296
616315 ZDOT = 5881
608653
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 18098
56213700
00016717 00000-0 10270-3 0 9041
2 25544 51
6418 5
8165 0002109 325
8101 34
2915 15
54198757 27683
Satellite: ISS
Catalog Number: 25544
Epoch time: 18098
56213700 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 5
8165 deg
Eccentricity:
0002109
Arg of perigee: 325
8101 deg
Mean anomaly: 34
2915 deg
Mean motion: 15
54198757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2768
Checksum: 308
Coasting Arc #6 (Orbit 2782)
---------------------------------------
Vector Time (GMT): 2018/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5815181
65 A = 6785893
65 meter
Y = -2206809
81 meter E =
0002898
Z = -2714545
75 I = 51
65958
XDOT = 3948
280832 Wp = 105
98831
YDOT = -4049
628507 meter/sec RA =
58884 deg
ZDOT = -5171
321728 TA = 104
67429
MA = 104
64217
Ha = 220
517 n
mi
Hp = 214
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19078679
94 X = -5776886
46
Y = -7240189
67 feet Y = -2271625
21 meter
Z = -8905989
99 Z = -2742700
75
XDOT = 12953
677270 XDOT = 4018
391003
YDOT = -13286
182766 feet/sec YDOT = -4005
084404 meter/sec
ZDOT = -16966
278636 ZDOT = -5151
971822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20300789
19 X = -6187680
54
Y = -1430833
62 feet Y = -436118
09 meter
Z = -9031262
69 Z = -2752728
87
XDOT = 8559
899504 XDOT = 2609
057369
YDOT = -15017
981450 feet/sec YDOT = -4577
480746 meter/sec
ZDOT = -16879
302025 ZDOT = -5144
811257
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 18099
52661389
00016717 00000-0 10270-3 0 9059
2 25544 51
6429 1
0086 0002144 323
1455 36
9550 15
54204628 27833
Satellite: ISS
Catalog Number: 25544
Epoch time: 18099
52661389 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 1
0086 deg
Eccentricity:
0002144
Arg of perigee: 323
1455 deg
Mean anomaly: 36
9550 deg
Mean motion: 15
54204628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2783
Checksum: 306
Coasting Arc #7 (Orbit 2798)
---------------------------------------
Vector Time (GMT): 2018/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4636320
39 A = 6782056
53 meter
Y = 2851805
63 meter E =
0009421
Z = 4037809
59 I = 51
61414
XDOT = -5580
010790 Wp = 91
76533
YDOT = 3531
360193 meter/sec RA = 355
60505 deg
ZDOT = 3904
845963 TA = 317
70545
MA = 317
77806
Ha = 220
560 n
mi
Hp = 214
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15211024
92 X = 4584472
60
Y = 9356317
69 feet Y = 2903362
54 meter
Z = 13247406
81 Z = 4060205
10
XDOT = -18307
122015 XDOT = -5638
052385
YDOT = 11585
827406 feet/sec YDOT = 3468
636410 meter/sec
ZDOT = 12811
174420 ZDOT = 3877
598998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17259448
49 X = 5260679
90
Y = 4287437
54 feet Y = 1306810
96 meter
Z = 13346874
69 Z = 4068127
41
XDOT = -13657
338122 XDOT = -4162
756659
YDOT = 15394
822723 feet/sec YDOT = 4692
341966 meter/sec
ZDOT = 12689
054095 ZDOT = 3867
623688
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 18100
55538623
00016717 00000-0 10270-3 0 9060
2 25544 51
6432 355
8791 0002179 333
4546 26
6495 15
54213452 27999
Satellite: ISS
Catalog Number: 25544
Epoch time: 18100
55538623 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 355
8791 deg
Eccentricity:
0002179
Arg of perigee: 333
4546 deg
Mean anomaly: 26
6495 deg
Mean motion: 15
54213452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2799
Checksum: 323
Coasting Arc #8 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2018/101/03:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2255144
46 A = 6777778
42 meter
Y = 3805568
41 meter E =
0003228
Z = 5132703
37 I = 51
57645
XDOT = -7189
757956 Wp = 105
50963
YDOT = 2191
049176 meter/sec RA = 352
36122 deg
ZDOT = 1532
777611 TA = 329
70439
MA = 329
72305
Ha = 220
641 n
mi
Hp = 214
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7398767
91 X = 2187489
98
Y = 12485460
65 feet Y = 3830409
10 meter
Z = 16839577
98 Z = 5143493
46
XDOT = -23588
444737 XDOT = -7221
169934
YDOT = 7188
481548 feet/sec YDOT = 2110
472836 meter/sec
ZDOT = 5028
797935 ZDOT = 1497
775801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14150743
34 X = -4313146
57
Y = 2963380
11 feet Y = 903238
26 meter
Z = 16887117
04 Z = 5147193
27
XDOT = 868
164232 XDOT = 264
616458
YDOT = -23650
358314 feet/sec YDOT = -7208
629214 meter/sec
ZDOT = 4872
298864 ZDOT = 1485
076694
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 18101
19836579
00016717 00000-0 10270-3 0 9073
2 25544 51
6409 352
6724 0001932 338
5131 21
5940 15
54230718 28091
Satellite: ISS
Catalog Number: 25544
Epoch time: 18101
19836579 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 352
6724 deg
Eccentricity:
0001932
Arg of perigee: 338
5131 deg
Mean anomaly: 21
5940 deg
Mean motion: 15
54230718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2809
Checksum: 308
Coasting Arc #9 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2018/102/03:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -444219
24 A = 6777188
04 meter
Y = -4214854
10 meter E =
0013947
Z = -5300457
07 I = 51
54172
XDOT = 7528
604901 Wp = 85
92515
YDOT = -1336
088144 meter/sec RA = 347
35608 deg
ZDOT = 433
439845 TA = 188
20810
MA = 188
23094
Ha = 220
698 n
mi
Hp = 214
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1457412
20 X = -371307
72
Y = -13828261
49 feet Y = -4219414
47 meter
Z = -17389951
03 Z = -5302437
47
XDOT = 24700
147314 XDOT = 7540
880437
YDOT = -4383
491285 feet/sec YDOT = -1251
829425 meter/sec
ZDOT = 1422
046737 ZDOT = 470
041177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13595498
58 X = 4143907
97
Y = 2867561
66 feet Y = 874032
79 meter
Z = -17398125
52 Z = -5302948
66
XDOT = -3015
280554 XDOT = -919
057513
YDOT = 23876
730908 feet/sec YDOT = 7277
627581 meter/sec
ZDOT = 1585
533521 ZDOT = 483
270617
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 18102
16283572
00016717 00000-0 10270-3 0 9081
2 25544 51
6409 347
8650 0002008 336
4009 23
7051 15
54212771 28244
Satellite: ISS
Catalog Number: 25544
Epoch time: 18102
16283572 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 347
8650 deg
Eccentricity:
0002008
Arg of perigee: 336
4009 deg
Mean anomaly: 23
7051 deg
Mean motion: 15
54212771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 289
Coasting Arc #10 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2018/103/03:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1367122
53 A = 6778925
54 meter
Y = 4503363
61 meter E =
0007665
Z = 4876478
52 I = 51
51525
XDOT = -7289
656630 Wp = 43
48327
YDOT = 350
753156 meter/sec RA = 342
34886 deg
ZDOT = -2359
912829 TA = 69
70275
MA = 69
62039
Ha = 220
766 n
mi
Hp = 214
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4485310
15 X = -1441066
23
Y = 14774814
99 feet Y = 4487662
54 meter
Z = 15998945
27 Z = 4869657
45
XDOT = -23916
196294 XDOT = -7281
573806
YDOT = 1150
764947 feet/sec YDOT = 269
280159 meter/sec
ZDOT = -7742
496159 ZDOT = -2395
303995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12868304
20 X = -3922259
12
Y = -8591562
93 feet Y = -2618708
38 meter
Z = 15967817
90 Z = 4866990
90
XDOT = 5036
119593 XDOT = 1535
009252
YDOT = -22273
113425 feet/sec YDOT = -6788
844972 meter/sec
ZDOT = -7900
416484 ZDOT = -2408
046944
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 18103
19159983
00016717 00000-0 10270-3 0 9094
2 25544 51
6403 342
7355 0002090 342
2036 17
9043 15
54247853 28403
Satellite: ISS
Catalog Number: 25544
Epoch time: 18103
19159983 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 342
7355 deg
Eccentricity:
0002090
Arg of perigee: 342
2036 deg
Mean anomaly: 17
9043 deg
Mean motion: 15
54247853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 301
Coasting Arc #11 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2018/104/03:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2984002
62 A = 6782537
69 meter
Y = -4645411
71 meter E =
0005909
Z = -3944211
65 I = 51
49543
XDOT = 6481
636509 Wp = 86
54696
YDOT = 757
801432 meter/sec RA = 337
34863 deg
ZDOT = 4016
731084 TA = 225
48263
MA = 225
53093
Ha = 220
892 n
mi
Hp = 214
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9790034
85 X = 3054886
16
Y = -15240852
07 feet Y = -4611646
60 meter
Z = -12940326
94 Z = -3929543
66
XDOT = 21265
211644 XDOT = 6453
169522
YDOT = 2486
225170 feet/sec YDOT = 830
124785 meter/sec
ZDOT = 13178
251589 ZDOT = 4048
147652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12052341
49 X = 3673553
69
Y = 13585905
88 feet Y = 4140984
11 meter
Z = -12874185
08 Z = -3924051
61
XDOT = -7059
932984 XDOT = -2151
867574
YDOT = 18866
208745 feet/sec YDOT = 5750
420425 meter/sec
ZDOT = 13318
258439 ZDOT = 4059
405172
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 18104
15606448
00016717 00000-0 10270-3 0 9106
2 25544 51
6397 337
9279 0002195 349
0583 11
0521 15
54219667 28558
Satellite: ISS
Catalog Number: 25544
Epoch time: 18104
15606448 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 337
9279 deg
Eccentricity:
0002195
Arg of perigee: 349
0583 deg
Mean anomaly: 11
0521 deg
Mean motion: 15
54219667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 318
Coasting Arc #12 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2018/105/03:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4319785
05 A = 6786225
90 meter
Y = 4559912
66 meter E =
0012874
Z = 2556301
06 I = 51
47674
XDOT = -5220
795034 Wp = 94
29521
YDOT = -1987
791799 meter/sec RA = 332
35561 deg
ZDOT = -5254
663425 TA = 56
90040
MA = 56
77688
Ha = 220
849 n
mi
Hp = 214
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14172523
13 X = -4382871
49
Y = 14960343
36 feet Y = 4511253
35 meter
Z = 8386814
51 Z = 2535163
14
XDOT = -17128
592631 XDOT = -5172
654288
YDOT = -6521
626636 feet/sec YDOT = -2045
905641 meter/sec
ZDOT = -17239
709399 ZDOT = -5279
907428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10922751
27 X = -3329254
59
Y = -17519983
92 feet Y = -5340091
10 meter
Z = 8291840
04 Z = 2527352
84
XDOT = 9297
146582 XDOT = 2833
770278
YDOT = -14043
030699 feet/sec YDOT = -4280
315757 meter/sec
ZDOT = -17351
986424 ZDOT = -5288
885462
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 18105
18482381
00016717 00000-0 10270-3 0 9119
2 25544 51
6383 332
7982 0002344 349
5426 10
5678 15
54265064 28711
Satellite: ISS
Catalog Number: 25544
Epoch time: 18105
18482381 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 332
7982 deg
Eccentricity:
0002344
Arg of perigee: 349
5426 deg
Mean anomaly: 10
5678 deg
Mean motion: 15
54265064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 314
Coasting Arc #13 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2018/105/08:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1801114
05 A = 6781111
37 meter
Y = -4913262
34 meter E =
0007561
Z = -4319605
97 I = 51
45605
XDOT = 6800
785900 Wp = 94
63174
YDOT = -565
399037 meter/sec RA = 331
25159 deg
ZDOT = 3483
451682 TA = 210
88742
MA = 210
93192
Ha = 220
849 n
mi
Hp = 214
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5909166
84 X = 1876904
27
Y = -16119627
11 feet Y = -4892697
67 meter
Z = -14171935
59 Z = -4310672
14
XDOT = 22312
289697 XDOT = 6789
681903
YDOT = -1854
983717 feet/sec YDOT = -489
409737 meter/sec
ZDOT = 11428
647252 ZDOT = 3516
461049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12233278
32 X = 3728703
23
Y = -12093660
82 feet Y = -3686147
82 meter
Z = -14131336
06 Z = -4307231
23
XDOT = 20067
295926 XDOT = 6116
511798
YDOT = 6790
547467 feet/sec YDOT = 2069
758868 meter/sec
ZDOT = 11575
947389 ZDOT = 3528
348764
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 18105
37771793
00016717 00000-0 10270-3 0 9129
2 25544 51
6412 331
8373 0002323 349
6663 10
4442 15
54251657 28743
Satellite: ISS
Catalog Number: 25544
Epoch time: 18105
37771793 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 331
8373 deg
Eccentricity:
0002323
Arg of perigee: 349
6663 deg
Mean anomaly: 10
4442 deg
Mean motion: 15
54251657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2874
Checksum: 306
Coasting Arc #14 (Orbit 2889)
---------------------------------------
Vector Time (GMT): 2018/106/08:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3245113
69 A = 6785098
00 meter
Y = 5104984
19 meter E =
0012736
Z = 3063574
73 I = 51
44075
XDOT = -5856
373786 Wp = 85
67650
YDOT = -776
356570 meter/sec RA = 326
25314 deg
ZDOT = -4891
200016 TA = 59
02817
MA = 58
90310
Ha = 220
942 n
mi
Hp = 214
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10646698
45 X = -3316839
31
Y = 16748635
80 feet Y = 5068294
29 meter
Z = 10051098
19 Z = 3047636
23
XDOT = -19213
824758 XDOT = -5823
497826
YDOT = -2547
101607 feet/sec YDOT = -841
663124 meter/sec
ZDOT = -16047
244147 ZDOT = -4919
568812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16584005
17 X = -5054804
78
Y = 10967184
73 feet Y = 3342797
90 meter
Z = 9979238
22 Z = 3041671
81
XDOT = -15633
294228 XDOT = -4765
028081
YDOT = -8867
472127 feet/sec YDOT = -2702
805504 meter/sec
ZDOT = -16173
632630 ZDOT = -4929
723226
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 18106
40647469
00016717 00000-0 10270-3 0 9137
2 25544 51
6411 326
7084 0002313 352
7186 7
3932 15
54234963 28906
Satellite: ISS
Catalog Number: 25544
Epoch time: 18106
40647469 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 326
7084 deg
Eccentricity:
0002313
Arg of perigee: 352
7186 deg
Mean anomaly: 7
3932 deg
Mean motion: 15
54234963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2890
Checksum: 307
Coasting Arc #15 (Orbit 2904)
---------------------------------------
Vector Time (GMT): 2018/107/08:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4324235
54 A = 6788023
77 meter
Y = -5005354
98 meter E =
0010304
Z = -1502383
66 I = 51
42459
XDOT = 4560
746220 Wp = 28
24049
YDOT = 2221
520448 meter/sec RA = 321
26166 deg
ZDOT = 5750
803692 TA = 315
30146
MA = 315
38446
Ha = 220
955 n
mi
Hp = 214
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14187124
49 X = 4387183
33
Y = -16421768
29 feet Y = -4956646
52 meter
Z = -4929080
23 Z = -1481224
45
XDOT = 14963
078148 XDOT = 4507
630701
YDOT = 7288
452912 feet/sec YDOT = 2272
225187 meter/sec
ZDOT = 18867
466181 ZDOT = 5772
829501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19494698
53 X = 5941984
11
Y = -9583023
83 feet Y = -2920905
66 meter
Z = -4833962
19 Z = -1473391
68
XDOT = 10125
640630 XDOT = 3086
295264
YDOT = 11074
171810 feet/sec YDOT = 3375
407568 meter/sec
ZDOT = 18965
342011 ZDOT = 5780
636245
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 18107
37093043
00016717 00000-0 10270-3 0 9148
2 25544 51
6417 321
8991 0002423 355
9393 4
1740 15
54259797 29053
Satellite: ISS
Catalog Number: 25544
Epoch time: 18107
37093043 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 321
8991 deg
Eccentricity:
0002423
Arg of perigee: 355
9393 deg
Mean anomaly: 4
1740 deg
Mean motion: 15
54259797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2905
Checksum: 315
Coasting Arc #16 (Orbit 2920)
---------------------------------------
Vector Time (GMT): 2018/108/08:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5039473
24 A = 6789011
83 meter
Y = 4536075
79 meter E =
0009922
Z = -256962
77 I = 51
40222
XDOT = -3038
155781 Wp = 127
68022
YDOT = -3705
042396 meter/sec RA = 316
27578 deg
ZDOT = -5985
120194 TA = 55
09725
MA = 55
00404
Ha = 220
996 n
mi
Hp = 214
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16533704
86 X = -5088574
12
Y = 14882138
43 feet Y = 4479446
39 meter
Z = -843053
70 Z = -281562
66
XDOT = -9967
702693 XDOT = -2967
426065
YDOT = -12155
650906 feet/sec YDOT = -3738
621868 meter/sec
ZDOT = -19636
221110 ZDOT = -5999
706870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20892401
87 X = -6368004
09
Y = 7625659
59 feet Y = 2324301
04 meter
Z = -953435
93 Z = -290607
27
XDOT = -4024
524884 XDOT = -1226
675184
YDOT = -13429
655305 feet/sec YDOT = -4093
358937 meter/sec
ZDOT = -19700
697067 ZDOT = -6004
772466
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 18108
39968312
00016717 00000-0 10270-3 0 9152
2 25544 51
6413 316
7704 0002292 358
8166 1
2981 15
54224534 29212
Satellite: ISS
Catalog Number: 25544
Epoch time: 18108
39968312 = yrday
fracday
Element set: 915
Inclination: 51
6413 deg
RA of node: 316
7704 deg
Eccentricity:
0002292
Arg of perigee: 358
8166 deg
Mean anomaly: 1
2981 deg
Mean motion: 15
54224534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2921
Checksum: 308
Coasting Arc #17 (Orbit 2921)
---------------------------------------
Vector Time (GMT): 2018/108/10:37:26
689
Vector Time (MET): N/A
Weight (LBS) : 928411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4968138
64 A = 6780339
08 meter
Y = -321456
58 meter E =
0010610
Z = -4613539
81 I = 51
36924
XDOT = 3148
324694 Wp = 57
64542
YDOT = -6329
003244 meter/sec RA = 315
92124 deg
ZDOT = -2948
732050 TA = 182
82475
MA = 182
83074
Ha = 220
948 n
mi
Hp = 214
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16299667
46 X = -4941764
21
Y = -1054647
56 feet Y = -376866
40 meter
Z = -15136285
48 Z = -4637609
70
XDOT = 10329
149259 XDOT = 3233
187003
YDOT = -20764
446337 feet/sec YDOT = -6293
322107 meter/sec
ZDOT = -9674
317750 ZDOT = -2933
231971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16229774
88 X = -4946835
38
Y = 356051
68 feet Y = 108524
55 meter
Z = -15243563
02 Z = -4646238
01
XDOT = 8574
756719 XDOT = 2613
585848
YDOT = -20406
381763 feet/sec YDOT = -6219
865161 meter/sec
ZDOT = -9604
238021 ZDOT = -2927
371749
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 18108
46397930
00016717 00000-0 10270-3 0 9163
2 25544 51
6404 316
4494 0002252 338
8150 21
2909 15
54079102 29224
Satellite: ISS
Catalog Number: 25544
Epoch time: 18108
46397930 = yrday
fracday
Element set: 916
Inclination: 51
6404 deg
RA of node: 316
4494 deg
Eccentricity:
0002252
Arg of perigee: 338
8150 deg
Mean anomaly: 21
2909 deg
Mean motion: 15
54079102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2922
Checksum: 301
Coasting Arc #18 (Orbit 2937)
---------------------------------------
Vector Time (GMT): 2018/109/10:37:26
689
Vector Time (MET): N/A
Weight (LBS) : 928411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3994736
57 A = 6777941
70 meter
Y = 1732702
20 meter E =
0002589
Z = 5192006
17 I = 51
33897
XDOT = -4230
664624 Wp = 89
33284
YDOT = 6293
445817 meter/sec RA = 310
90526 deg
ZDOT = 1154
329145 TA = 349
55287
MA = 349
55824
Ha = 220
902 n
mi
Hp = 214
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13106091
11 X = 3949843
67
Y = 5684718
49 feet Y = 1777123
12 meter
Z = 17034140
98 Z = 5211302
49
XDOT = -13880
133282 XDOT = -4306
332436
YDOT = 20647
788114 feet/sec YDOT = 6245
712539 meter/sec
ZDOT = 3787
169111 ZDOT = 1133
593853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13514296
83 X = 4119157
68
Y = 4303463
01 feet Y = 1311695
53 meter
Z = 17119918
07 Z = 5218151
03
XDOT = -11367
479232 XDOT = -3464
807670
YDOT = 20997
139185 feet/sec YDOT = 6399
928024 meter/sec
ZDOT = 3693
757208 ZDOT = 1125
857197
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 18109
49284631
00016717 00000-0 10270-3 0 9171
2 25544 51
6412 311
3206 0002242 343
7020 16
4061 15
54067716 29388
Satellite: ISS
Catalog Number: 25544
Epoch time: 18109
49284631 = yrday
fracday
Element set: 917
Inclination: 51
6412 deg
RA of node: 311
3206 deg
Eccentricity:
0002242
Arg of perigee: 343
7020 deg
Mean anomaly: 16
4061 deg
Mean motion: 15
54067716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2938
Checksum: 283
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