[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 3rd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
153/12:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
9
154/09:16:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
0
156/19:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
1
157/11:12:41
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
2
159/13:07:21
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 214
3
164/10:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
7
Coasting Arc #1 (Orbit 3606)
---------------------------------------
Vector Time (GMT): 2018/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3183834
19 A = 6780632
67 meter
Y = 3880142
26 meter E =
0012859
Z = -4571961
21 I = 52
00692
XDOT = -3117
872559 Wp = 118
23844
YDOT = 6251
681973 meter/sec RA = 95
98603 deg
ZDOT = 3135
240652 TA = 183
05923
MA = 183
06710
Ha = 221
978 n
mi
Hp = 213
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10445650
24 X = 3162417
05
Y = 12730125
54 feet Y = 3915627
00 meter
Z = -14999872
72 Z = -4556546
62
XDOT = -10229
240679 XDOT = -3202
778280
YDOT = 20510
767627 feet/sec YDOT = 6216
340588 meter/sec
ZDOT = 10286
222612 ZDOT = 3119
889696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15657907
01 X = 4772530
06
Y = -5295853
03 feet Y = -1614176
00 meter
Z = -14931435
82 Z = -4551101
64
XDOT = 15087
145939 XDOT = 4598
562082
YDOT = 15809
073506 feet/sec YDOT = 4818
605605 meter/sec
ZDOT = 10216
636469 ZDOT = 3114
030796
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 18152
51051540
00016717 00000-0 10270-3 0 9005
2 25544 51
6394 96
8676 0003386 141
7912 218
3481 15
54106849 36073
Satellite: ISS
Catalog Number: 25544
Epoch time: 18152
51051540 = yrday
fracday
Element set: 900
Inclination: 51
6394 deg
RA of node: 96
8676 deg
Eccentricity:
0003386
Arg of perigee: 141
7912 deg
Mean anomaly: 218
3481 deg
Mean motion: 15
54106849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3607
Checksum: 312
Coasting Arc #2 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2018/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2592120
98 A = 6784357
76 meter
Y = -5231904
67 meter E =
0014619
Z = 3439761
55 I = 52
02243
XDOT = 3697
765400 Wp = 100
26117
YDOT = -4881
498871 meter/sec RA = 91
02467 deg
ZDOT = -4624
164857 TA = 39
65273
MA = 39
54592
Ha = 221
986 n
mi
Hp = 213
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8504333
91 X = -2550132
33
Y = -17165041
58 feet Y = -5260657
26 meter
Z = 11285306
93 Z = 3427271
15
XDOT = 12131
776247 XDOT = 3774
538645
YDOT = -16015
416243 feet/sec YDOT = -4839
718008 meter/sec
ZDOT = -15171
144545 ZDOT = -4606
016547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19061854
38 X = -5810053
22
Y = 2202235
06 feet Y = 671241
25 meter
Z = 11230154
42 Z = 3422951
07
XDOT = -10716
559890 XDOT = -3266
407454
YDOT = -15575
844711 feet/sec YDOT = -4747
517468 meter/sec
ZDOT = -15089
217787 ZDOT = -4599
193582
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 18153
53935357
00016717 00000-0 10270-3 0 9016
2 25544 51
6399 91
7391 0003322 143
1796 216
9586 15
54128076 36236
Satellite: ISS
Catalog Number: 25544
Epoch time: 18153
53935357 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 91
7391 deg
Eccentricity:
0003322
Arg of perigee: 143
1796 deg
Mean anomaly: 216
9586 deg
Mean motion: 15
54128076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3623
Checksum: 326
Coasting Arc #3 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2018/153/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3570849
37 A = 6780864
26 meter
Y = -3624996
98 meter E =
0010861
Z = -4491700
59 I = 52
01109
XDOT = 2451
422463 Wp = 86
74909
YDOT = 6472
768643 meter/sec RA = 90
98662 deg
ZDOT = -3281
175822 TA = 150
35817
MA = 150
29657
Ha = 221
958 n
mi
Hp = 213
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11715385
09 X = 3632938
06
Y = -11893034
71 feet Y = -3584717
50 meter
Z = -14736550
48 Z = -4474204
28
XDOT = 8042
724616 XDOT = 2394
798261
YDOT = 21236
117596 feet/sec YDOT = 6499
865985 meter/sec
ZDOT = -10765
012539 ZDOT = -3269
404265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8758346
67 X = -2669544
07
Y = -14293459
63 feet Y = -4356646
50 meter
Z = -14657722
12 Z = -4467673
70
XDOT = 21510
409646 XDOT = 6556
372860
YDOT = -2215
319961 feet/sec YDOT = -675
229524 meter/sec
ZDOT = -10713
255453 ZDOT = -3265
400262
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 18153
53935371
00016717 00000-0 10270-3 0 9023
2 25544 51
6401 91
7390 0003374 142
3116 217
8273 15
54133805 36232
Satellite: ISS
Catalog Number: 25544
Epoch time: 18153
53935371 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 91
7390 deg
Eccentricity:
0003374
Arg of perigee: 142
3116 deg
Mean anomaly: 217
8273 deg
Mean motion: 15
54133805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3623
Checksum: 289
Coasting Arc #4 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2018/154/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3515933
79 A = 6779831
84 meter
Y = 3329642
75 meter E =
0010855
Z = 4740689
24 I = 52
00527
XDOT = -2561
691049 Wp = 126
68075
YDOT = -6675
862684 meter/sec RA = 86
67505 deg
ZDOT = 2778
238628 TA = 295
90475
MA = 296
01660
Ha = 221
929 n
mi
Hp = 213
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11535215
84 X = -3575933
24
Y = 10924024
75 feet Y = 3289989
06 meter
Z = 15553442
38 Z = 4723464
74
XDOT = -8404
498192 XDOT = -2500
344564
YDOT = -21902
436627 feet/sec YDOT = -6704
166629 meter/sec
ZDOT = 9114
956128 ZDOT = 2765
942940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4607433
81 X = -1404345
82
Y = 15283137
12 feet Y = 4658300
19 meter
Z = 15475863
94 Z = 4717043
33
XDOT = -17175
340350 XDOT = -5235
043739
YDOT = -14388
764320 feet/sec YDOT = -4385
695365 meter/sec
ZDOT = 9060
889951 ZDOT = 2761
759257
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 18154
43958439
00016717 00000-0 10270-3 0 9034
2 25544 51
6379 87
2520 0003393 149
5773 210
5577 15
54145778 36374
Satellite: ISS
Catalog Number: 25544
Epoch time: 18154
43958439 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 87
2520 deg
Eccentricity:
0003393
Arg of perigee: 149
5773 deg
Mean anomaly: 210
5577 deg
Mean motion: 15
54145778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 342
Coasting Arc #5 (Orbit 3651)
---------------------------------------
Vector Time (GMT): 2018/155/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3938837
81 A = 6777662
59 meter
Y = -1617797
23 meter E =
0016021
Z = -5286631
41 I = 51
99517
XDOT = 1803
335058 Wp = 94
33389
YDOT = 7384
425134 meter/sec RA = 81
70187 deg
ZDOT = -919
741771 TA = 166
91832
MA = 166
87672
Ha = 221
865 n
mi
Hp = 214
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12922696
22 X = 3982315
38
Y = -5307733
71 feet Y = -1573506
71 meter
Z = -17344591
25 Z = -5267392
50
XDOT = 5916
453601 XDOT = 1725
093986
YDOT = 24227
116582 feet/sec YDOT = 7404
153905 meter/sec
ZDOT = -3017
525497 ZDOT = -911
170957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8437129
27 X = 2571637
00
Y = -11268141
48 feet Y = -3434529
52 meter
Z = -17258238
55 Z = -5260311
11
XDOT = 16750
070049 XDOT = 5105
421351
YDOT = 17088
274112 feet/sec YDOT = 5208
505949 meter/sec
ZDOT = -2980
245027 ZDOT = -908
378684
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 18155
40411758
00016717 00000-0 10270-3 0 9041
2 25544 51
6383 82
4431 0003407 151
3898 208
7442 15
54117553 36529
Satellite: ISS
Catalog Number: 25544
Epoch time: 18155
40411758 = yrday
fracday
Element set: 904
Inclination: 51
6383 deg
RA of node: 82
4431 deg
Eccentricity:
0003407
Arg of perigee: 151
3898 deg
Mean anomaly: 208
7442 deg
Mean motion: 15
54117553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3652
Checksum: 304
Coasting Arc #6 (Orbit 3667)
---------------------------------------
Vector Time (GMT): 2018/156/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4264879
91 A = 6777702
56 meter
Y = -171187
60 meter E =
0004621
Z = 5260832
24 I = 51
99034
XDOT = -958
316188 Wp = 102
63272
YDOT = -7543
265046 meter/sec RA = 76
72657 deg
ZDOT = -1022
581440 TA = 357
10486
MA = 357
10754
Ha = 221
925 n
mi
Hp = 214
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13992388
17 X = -4288203
02
Y = -561639
09 feet Y = -219011
38 meter
Z = 17259948
30 Z = 5240058
27
XDOT = -3144
081981 XDOT = -868
926948
YDOT = -24748
244903 feet/sec YDOT = -7553
481685 meter/sec
ZDOT = -3354
925985 ZDOT = -1027
020289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12259296
91 X = -3736633
70
Y = 7000888
67 feet Y = 2133870
87 meter
Z = 17166985
10 Z = 5232497
06
XDOT = -15252
891270 XDOT = -4649
081259
YDOT = -18438
647780 feet/sec YDOT = -5620
099843 meter/sec
ZDOT = -3373
676491 ZDOT = -1028
296595
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 18156
43294854
00016717 00000-0 10270-3 0 9052
2 25544 51
6390 77
3147 0003306 154
7890 205
3425 15
54125428 36682
Satellite: ISS
Catalog Number: 25544
Epoch time: 18156
43294854 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 77
3147 deg
Eccentricity:
0003306
Arg of perigee: 154
7890 deg
Mean anomaly: 205
3425 deg
Mean motion: 15
54125428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 318
Coasting Arc #7 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2018/156/19:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4062030
01 A = 6783776
01 meter
Y = 4043187
57 meter E =
0007962
Z = -3639049
83 I = 52
00660
XDOT = -1949
751942 Wp = 121
29702
YDOT = 5939
531467 meter/sec RA = 74
59966 deg
ZDOT = 4425
881485 TA = 195
84663
MA = 195
87156
Ha = 221
833 n
mi
Hp = 214
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13326870
11 X = 4034192
67
Y = 13265051
10 feet Y = 4088456
71 meter
Z = -11939139
85 Z = -3619385
09
XDOT = -6396
823956 XDOT = -2037
523104
YDOT = 19486
651794 feet/sec YDOT = 5917
236798 meter/sec
ZDOT = 14520
608548 ZDOT = 4416
197672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14572940
84 X = -4441832
37
Y = -11969806
76 feet Y = -3648397
10 meter
Z = -11851718
40 Z = -3612403
77
XDOT = 3793
062176 XDOT = 1156
125351
YDOT = -18941
343720 feet/sec YDOT = -5773
321566 meter/sec
ZDOT = 14476
376670 ZDOT = 4412
399609
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 18156
81875918
00016717 00000-0 10270-3 0 9061
2 25544 51
6382 75
3876 0003706 156
8528 203
2792 15
54137797 36748
Satellite: ISS
Catalog Number: 25544
Epoch time: 18156
81875918 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 75
3876 deg
Eccentricity:
0003706
Arg of perigee: 156
8528 deg
Mean anomaly: 203
2792 deg
Mean motion: 15
54137797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 353
Coasting Arc #8 (Orbit 3684)
---------------------------------------
Vector Time (GMT): 2018/157/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -95822
82 A = 6786314
02 meter
Y = 6235838
66 meter E =
0014463
Z = 2663369
76 I = 52
01057
XDOT = -5097
961332 Wp = 90
42261
YDOT = -2325
455175 meter/sec RA = 71
39742 deg
ZDOT = 5236
680876 TA = 299
46662
MA = 299
61084
Ha = 221
698 n
mi
Hp = 214
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -314379
32 X = -178483
81
Y = 20458788
25 feet Y = 6234304
67 meter
Z = 8738089
77 Z = 2662704
09
XDOT = -16725
594922 XDOT = -5097
015634
YDOT = -7629
446113 feet/sec YDOT = -2382
459286 meter/sec
ZDOT = 17180
711535 ZDOT = 5211
918791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17909755
19 X = 5458893
38
Y = 9897975
95 feet Y = 3016903
07 meter
Z = 8734174
55 Z = 2662176
40
XDOT = -13896
218305 XDOT = -4235
567339
YDOT = 10010
041443 feet/sec YDOT = 3051
060632 meter/sec
ZDOT = 17070
219514 ZDOT = 5203
002908
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 18157
52607853
00016717 00000-0 10270-3 0 9072
2 25544 51
6397 71
8660 0003246 158
3443 201
7848 15
54133284 36852
Satellite: ISS
Catalog Number: 25544
Epoch time: 18157
52607853 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 71
8660 deg
Eccentricity:
0003246
Arg of perigee: 158
3443 deg
Mean anomaly: 201
7848 deg
Mean motion: 15
54133284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3685
Checksum: 328
Coasting Arc #9 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2018/158/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1085673
03 A = 6782442
38 meter
Y = -5361802
71 meter E =
0007663
Z = -4015104
61 I = 51
98752
XDOT = 5156
800726 Wp = 96
67525
YDOT = 4025
633132 meter/sec RA = 66
43978 deg
ZDOT = -3988
855977 TA = 132
00035
MA = 131
93507
Ha = 221
598 n
mi
Hp = 214
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3561919
38 X = 1165052
82
Y = -17591216
23 feet Y = -5349217
78 meter
Z = -13172915
40 Z = -4009638
43
XDOT = 16918
637552 XDOT = 5130
777563
YDOT = 13207
457782 feet/sec YDOT = 4083
154866 meter/sec
ZDOT = -13086
797825 ZDOT = -3963
868790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14037841
12 X = -4278733
97
Y = -11213500
22 feet Y = -3417874
87 meter
Z = -13147634
30 Z = -4007398
94
XDOT = 18653
313816 XDOT = 5685
530051
YDOT = -8166
333073 feet/sec YDOT = -2489
098321 meter/sec
ZDOT = -12975
561367 ZDOT = -3954
951105
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 18158
49060212
00016717 00000-0 10270-3 0 9082
2 25544 51
6408 67
0578 0003184 162
2036 197
9229 15
54156739 37000
Satellite: ISS
Catalog Number: 25544
Epoch time: 18158
49060212 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 67
0578 deg
Eccentricity:
0003184
Arg of perigee: 162
2036 deg
Mean anomaly: 197
9229 deg
Mean motion: 15
54156739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 316
Coasting Arc #10 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2018/159/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2120519
11 A = 6779010
38 meter
Y = 4153482
43 meter E =
0009227
Z = 4916928
73 I = 51
96227
XDOT = -4988
334045 Wp = 135
87266
YDOT = -5334
187238 meter/sec RA = 61
47125 deg
ZDOT = 2345
550002 TA = 291
23280
MA = 291
33133
Ha = 221
551 n
mi
Hp = 214
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6957083
71 X = -2190690
90
Y = 13626910
86 feet Y = 4129376
55 meter
Z = 16131655
93 Z = 4906457
83
XDOT = -16365
925344 XDOT = -4939
708482
YDOT = -17500
614298 feet/sec YDOT = -5389
698544 meter/sec
ZDOT = 7695
374022 ZDOT = 2321
435884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9170872
80 X = 2795282
03
Y = 12309315
99 feet Y = 3751879
52 meter
Z = 16084149
60 Z = 4902448
80
XDOT = -22017
172922 XDOT = -6710
834307
YDOT = 6449
177834 feet/sec YDOT = 1965
709404 meter/sec
ZDOT = 7588
256452 ZDOT = 2312
900567
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 18159
51942264
00016717 00000-0 10270-3 0 9093
2 25544 51
6411 61
9292 0003232 167
8824 192
2407 15
54167892 37165
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
51942264 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 61
9292 deg
Eccentricity:
0003232
Arg of perigee: 167
8824 deg
Mean anomaly: 192
2407 deg
Mean motion: 15
54167892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 322
Coasting Arc #11 (Orbit 3716)
---------------------------------------
Vector Time (GMT): 2018/159/13:07:21
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4579710
45 A = 6786902
40 meter
Y = -4374009
08 meter E =
0015639
Z = 2416788
83 I = 51
98814
XDOT = 2000
622424 Wp = 116
36092
YDOT = -5083
199085 meter/sec RA = 61
03853 deg
ZDOT = -5388
596306 TA = 36
73276
MA = 36
62568
Ha = 221
633 n
mi
Hp = 214
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15025296
77 X = -4542198
28
Y = -14350423
48 feet Y = -4425013
02 meter
Z = 7929097
22 Z = 2394632
76
XDOT = 6563
721865 XDOT = 2083
490606
YDOT = -16677
162354 feet/sec YDOT = -5060
362943 meter/sec
ZDOT = -17679
121740 ZDOT = -5378
677064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13587591
70 X = -4141497
95
Y = 15767811
32 feet Y = 4806028
89 meter
Z = 7830597
53 Z = 2386766
13
XDOT = -15838
376071 XDOT = -4827
537026
YDOT = -4857
877351 feet/sec YDOT = -1480
681017 meter/sec
ZDOT = -17633
941079 ZDOT = -5374
825241
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 18159
58372487
00016717 00000-0 10270-3 0 9106
2 25544 51
6423 61
6097 0003226 166
5998 193
5240 15
54133122 37178
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
58372487 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 61
6097 deg
Eccentricity:
0003226
Arg of perigee: 166
5998 deg
Mean anomaly: 193
5240 deg
Mean motion: 15
54133122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3717
Checksum: 318
Coasting Arc #12 (Orbit 3731)
---------------------------------------
Vector Time (GMT): 2018/160/13:07:21
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4255721
44 A = 6788954
14 meter
Y = 5227207
06 meter E =
0008603
Z = -787191
77 I = 51
97847
XDOT = -3249
697930 Wp = 55
08378
YDOT = 3537
652896 meter/sec RA = 56
08845 deg
ZDOT = 5973
497409 TA = 296
44893
MA = 296
53717
Ha = 221
392 n
mi
Hp = 214
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13962340
68 X = 4200776
88
Y = 17149629
45 feet Y = 5274490
33 meter
Z = -2582650
16 Z = -766651
69
XDOT = -10661
738616 XDOT = -3318
031807
YDOT = 11606
472757 feet/sec YDOT = 3500
929892 meter/sec
ZDOT = 19598
088612 ZDOT = 5957
545700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16180887
99 X = 4931934
66
Y = -15089664
67 feet Y = -4599329
79 meter
Z = -2491528
32 Z = -759417
83
XDOT = 11200
248460 XDOT = 3413
835731
YDOT = 8814
719723 feet/sec YDOT = 2686
726572 meter/sec
ZDOT = 19526
138670 ZDOT = 5951
567067
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 18160
54824044
00016717 00000-0 10270-3 0 9116
2 25544 51
6422 56
8011 0003112 172
2837 187
8364 15
54171599 37329
Satellite: ISS
Catalog Number: 25544
Epoch time: 18160
54824044 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 56
8011 deg
Eccentricity:
0003112
Arg of perigee: 172
2837 deg
Mean anomaly: 187
8364 deg
Mean motion: 15
54171599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3732
Checksum: 299
Coasting Arc #13 (Orbit 3747)
---------------------------------------
Vector Time (GMT): 2018/161/13:07:21
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3600489
11 A = 6788951
50 meter
Y = -5667022
85 meter E =
0012561
Z = -960805
63 I = 51
95866
XDOT = 4482
591341 Wp = 149
84834
YDOT = -1847
889446 meter/sec RA = 51
14160 deg
ZDOT = -5942
822301 TA = 40
51390
MA = 40
42046
Ha = 221
397 n
mi
Hp = 214
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11812628
31 X = -3532184
16
Y = -18592594
64 feet Y = -5706903
97 meter
Z = -3152249
45 Z = -978130
51
XDOT = 14706
664504 XDOT = 4531
789251
YDOT = -6062
629415 feet/sec YDOT = -1797
486276 meter/sec
ZDOT = -19497
448493 ZDOT = -5920
927858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17540432
22 X = -5346323
74
Y = 13306648
77 feet Y = 4055866
54 meter
Z = -3228897
00 Z = -984167
81
XDOT = -6314
547328 XDOT = -1924
674026
YDOT = -12996
609056 feet/sec YDOT = -3961
366440 meter/sec
ZDOT = -19399
161235 ZDOT = -5912
864344
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 18161
57705683
00016717 00000-0 10270-3 0 9128
2 25544 51
6421 51
6731 0003259 177
7925 182
3242 15
54117031 37483
Satellite: ISS
Catalog Number: 25544
Epoch time: 18161
57705683 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 51
6731 deg
Eccentricity:
0003259
Arg of perigee: 177
7925 deg
Mean anomaly: 182
3242 deg
Mean motion: 15
54117031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3748
Checksum: 305
Coasting Arc #14 (Orbit 3763)
---------------------------------------
Vector Time (GMT): 2018/162/13:07:21
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2660077
63 A = 6786391
44 meter
Y = 5683375
34 meter E =
0013136
Z = 2572530
95 I = 51
92926
XDOT = -5551
749311 Wp = 88
89811
YDOT = 194
936767 meter/sec RA = 46
18814 deg
ZDOT = 5287
012610 TA = 299
90690
MA = 300
03731
Ha = 221
183 n
mi
Hp = 214
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8727288
83 X = 2583830
70
Y = 18646244
57 feet Y = 5712695
50 meter
Z = 8440062
18 Z = 2585268
43
XDOT = -18214
400628 XDOT = -5579
198393
YDOT = 639
556321 feet/sec YDOT = 132
699096 meter/sec
ZDOT = 17345
841897 ZDOT = 5259
977123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17677412
04 X = 5388075
19
Y = -10507474
25 feet Y = -3202678
15 meter
Z = 8496160
59 Z = 2589629
75
XDOT = 1719
848686 XDOT = 524
209879
YDOT = 16881
719569 feet/sec YDOT = 5145
548125 meter/sec
ZDOT = 17224
807708 ZDOT = 5250
121389
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 18162
60586792
00016717 00000-0 10270-3 0 9132
2 25544 51
6423 46
5437 0002962 182
7054 177
4083 15
54162111 37645
Satellite: ISS
Catalog Number: 25544
Epoch time: 18162
60586792 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 46
5437 deg
Eccentricity:
0002962
Arg of perigee: 182
7054 deg
Mean anomaly: 177
4083 deg
Mean motion: 15
54162111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3764
Checksum: 311
Coasting Arc #15 (Orbit 3778)
---------------------------------------
Vector Time (GMT): 2018/163/13:07:21
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1396267
24 A = 6782604
40 meter
Y = -5339455
25 meter E =
0006156
Z = -3947117
51 I = 51
89198
XDOT = 6358
998024 Wp = 99
02515
YDOT = 1335
466862 meter/sec RA = 41
22448 deg
ZDOT = -4062
340358 TA = 128
64737
MA = 128
59226
Ha = 221
118 n
mi
Hp = 214
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4580929
26 X = -1317282
97
Y = -17517897
79 feet Y = -5354627
02 meter
Z = -12949860
61 Z = -3953709
18
XDOT = 20862
854411 XDOT = 6363
324796
YDOT = 4381
452958 feet/sec YDOT = 1406
602389 meter/sec
ZDOT = -13327
888313 ZDOT = -4031
439452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16866496
48 X = -5140908
13
Y = 6529969
55 feet Y = 1990334
72 meter
Z = -12978495
28 Z = -3955845
36
XDOT = 2354
970418 XDOT = 717
794983
YDOT = -20091
136563 feet/sec YDOT = -6123
778424 meter/sec
ZDOT = -13189
803362 ZDOT = -4020
252065
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 18163
57037559
00016717 00000-0 10270-3 0 9142
2 25544 51
6412 41
7351 0002977 187
0698 173
0414 15
54160335 37795
Satellite: ISS
Catalog Number: 25544
Epoch time: 18163
57037559 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 41
7351 deg
Eccentricity:
0002977
Arg of perigee: 187
0698 deg
Mean anomaly: 173
0414 deg
Mean motion: 15
54160335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3779
Checksum: 321
Coasting Arc #16 (Orbit 3792)
---------------------------------------
Vector Time (GMT): 2018/164/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -73562
63 A = 6779324
65 meter
Y = -4776847
51 meter E =
0010553
Z = -4819311
83 I = 51
85923
XDOT = 6759
445570 Wp = 86
17245
YDOT = 2505
638463 meter/sec RA = 36
73212 deg
ZDOT = -2590
935861 TA = 158
37965
MA = 158
33506
Ha = 221
066 n
mi
Hp = 214
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -241347
20 X = 3268
73
Y = -15672071
88 feet Y = -4777239
70 meter
Z = -15811390
52 Z = -4819483
40
XDOT = 22176
658693 XDOT = 6743
509963
YDOT = 8220
598633 feet/sec YDOT = 2581
138591 meter/sec
ZDOT = -8500
445738 ZDOT = -2558
138798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14005814
18 X = -4268972
16
Y = -7036317
92 feet Y = -2144669
70 meter
Z = -15811374
23 Z = -4819306
87
XDOT = 16952
916684 XDOT = 5167
249005
YDOT = -15003
283938 feet/sec YDOT = -4573
000944 meter/sec
ZDOT = -8354
068632 ZDOT = -2546
320119
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 18164
47058227
00016717 00000-0 10270-3 0 9158
2 25544 51
6421 37
2485 0002967 188
0661 172
0444 15
54187671 37933
Satellite: ISS
Catalog Number: 25544
Epoch time: 18164
47058227 = yrday
fracday
Element set: 915
Inclination: 51
6421 deg
RA of node: 37
2485 deg
Eccentricity:
0002967
Arg of perigee: 188
0661 deg
Mean anomaly: 172
0444 deg
Mean motion: 15
54187671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3793
Checksum: 325
Coasting Arc #17 (Orbit 3808)
---------------------------------------
Vector Time (GMT): 2018/165/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1500795
45 A = 6777315
95 meter
Y = 3961239
98 meter E =
0004762
Z = 5289055
09 I = 51
82582
XDOT = -6772
676079 Wp = 154
37465
YDOT = -3528
404613 meter/sec RA = 31
74797 deg
ZDOT = 716
389827 TA = 288
77622
MA = 288
82788
Ha = 221
025 n
mi
Hp = 214
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4923869
60 X = -1570671
09
Y = 12996194
15 feet Y = 3944065
37 meter
Z = 17352542
94 Z = 5281595
74
XDOT = -22220
065876 XDOT = -6736
196986
YDOT = -11576
130620 feet/sec YDOT = -3603
937506 meter/sec
ZDOT = 2350
360326 ZDOT = 683
578364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9439714
88 X = 2877225
10
Y = 10257563
03 feet Y = 3126505
21 meter
Z = 17318501
22 Z = 5278679
17
XDOT = -19452
505852 XDOT = -5929
123784
YDOT = 14155
638476 feet/sec YDOT = 4314
638608 meter/sec
ZDOT = 2204
090811 ZDOT = 671
806879
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 18165
49938589
00016717 00000-0 10270-3 0 9160
2 25544 51
6425 32
1196 0003054 192
9111 167
1964 15
54190387 38090
Satellite: ISS
Catalog Number: 25544
Epoch time: 18165
49938589 = yrday
fracday
Element set: 916
Inclination: 51
6425 deg
RA of node: 32
1196 deg
Eccentricity:
0003054
Arg of perigee: 192
9111 deg
Mean anomaly: 167
1964 deg
Mean motion: 15
54190387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3809
Checksum: 334
Coasting Arc #18 (Orbit 3823)
---------------------------------------
Vector Time (GMT): 2018/166/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3103064
08 A = 6777709
54 meter
Y = -3034289
98 meter E =
0013930
Z = -5218023
82 I = 51
79812
XDOT = 6249
590723 Wp = 111
33145
YDOT = 4247
800721 meter/sec RA = 26
75880 deg
ZDOT = 1244
148290 TA = 170
61253
MA = 170
58647
Ha = 220
873 n
mi
Hp = 214
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10180656
44 X = 3162110
04
Y = -9955019
62 feet Y = -2999258
28 meter
Z = -17119500
71 Z = -5202807
40
XDOT = 20503
906570 XDOT = 6195
582774
YDOT = 13936
354070 feet/sec YDOT = 4317
385744 meter/sec
ZDOT = 4081
851346 ZDOT = 1274
376142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4625322
04 X = -1409798
16
Y = -13553559
96 feet Y = -4131125
08 meter
Z = -17050891
31 Z = -5197111
67
XDOT = 20340
954064 XDOT = 6199
922799
YDOT = -12255
432229 feet/sec YDOT = -3735
455743 meter/sec
ZDOT = 4216
435242 ZDOT = 1285
169462
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 18166
46388663
00016717 00000-0 10270-3 0 9171
2 25544 51
6422 27
3107 0002905 197
5494 162
5559 15
54195580 38240
Satellite: ISS
Catalog Number: 25544
Epoch time: 18166
46388663 = yrday
fracday
Element set: 917
Inclination: 51
6422 deg
RA of node: 27
3107 deg
Eccentricity:
0002905
Arg of perigee: 197
5494 deg
Mean anomaly: 162
5559 deg
Mean motion: 15
54195580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3824
Checksum: 335
Coasting Arc #19 (Orbit 3839)
---------------------------------------
Vector Time (GMT): 2018/167/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4550021
10 A = 6780258
92 meter
Y = 2064911
42 meter E =
0006943
Z = 4577656
46 I = 51
77630
XDOT = -5229
328093 Wp = 82
86806
YDOT = -4696
195872 meter/sec RA = 21
77274 deg
ZDOT = -3074
542728 TA = 37
82987
MA = 37
78110
Ha = 220
835 n
mi
Hp = 214
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14927890
76 X = -4595009
00
Y = 6774643
76 feet Y = 2013777
64 meter
Z = 15018557
95 Z = 4555445
29
XDOT = -17156
588231 XDOT = -5161
490905
YDOT = -15407
466771 feet/sec YDOT = -4754
294006 meter/sec
ZDOT = -10087
082440 ZDOT = -3099
780814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15585
20 X = 4750
37
Y = 16484048
75 feet Y = 5024338
06 meter
Z = 14918803
48 Z = 4547251
30
XDOT = -19860
253341 XDOT = -6053
405218
YDOT = 9264
009053 feet/sec YDOT = 2823
669959 meter/sec
ZDOT = -10199
256725 ZDOT = -3108
733450
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 18167
49268432
00016717 00000-0 10270-3 0 9187
2 25544 51
6415 22
1819 0002842 203
4128 156
6895 15
54227665 38401
Satellite: ISS
Catalog Number: 25544
Epoch time: 18167
49268432 = yrday
fracday
Element set: 918
Inclination: 51
6415 deg
RA of node: 22
1819 deg
Eccentricity:
0002842
Arg of perigee: 203
4128 deg
Mean anomaly: 156
6895 deg
Mean motion: 15
54227665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3840
Checksum: 322
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