[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 31st 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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
306/03:16:43
186 0
6 1
4 1
4
N/A 1
2 -0
1 222
6
000/00:03:26
372 -0
0 0
0 213
4
307/05:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 213
4
310/13:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 213
3
315/12:37:22
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
3
317/10:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
2
317/21:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 278)
---------------------------------------
Vector Time (GMT): 2017/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3940267
01 A = 6777183
45 meter
Y = -1681498
24 meter E =
0019554
Z = -5268479
57 I = 51
99392
XDOT = 1742
245835 Wp = 79
69696
YDOT = 7378
596169 meter/sec RA = 82
93881 deg
ZDOT = -1051
863934 TA = 180
25828
MA = 180
25929
Ha = 222
605 n
mi
Hp = 212
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12927385
20 X = 3984369
24
Y = -5516726
51 feet Y = -1637189
23 meter
Z = -17285037
95 Z = -5249231
43
XDOT = 5716
029641 XDOT = 1664
716437
YDOT = 24207
992680 feet/sec YDOT = 7397
645591 meter/sec
ZDOT = -3450
997160 ZDOT = -1043
589286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6851325
14 X = -2088283
90
Y = 12392184
51 feet Y = 3777137
84 meter
Z = -17199337
29 Z = -5242358
01
XDOT = -18556
590305 XDOT = -5656
048725
YDOT = -15000
174983 feet/sec YDOT = -4572
053335 meter/sec
ZDOT = -3415
408406 ZDOT = -1041
016482
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 17303
51789025
00016717 00000-0 10270-3 0 9008
2 25544 51
6388 83
6772 0005285 73
7590 286
4144 15
54313213 2792
Satellite: ISS
Catalog Number: 25544
Epoch time: 17303
51789025 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 83
6772 deg
Eccentricity:
0005285
Arg of perigee: 73
7590 deg
Mean anomaly: 286
4144 deg
Mean motion: 15
54313213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 279
Checksum: 314
Coasting Arc #2 (Orbit 294)
---------------------------------------
Vector Time (GMT): 2017/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4251385
02 A = 6777211
49 meter
Y = -194694
87 meter E =
0008784
Z = 5267656
80 I = 51
98844
XDOT = -847
340218 Wp = 69
63327
YDOT = -7567
470862 meter/sec RA = 77
96028 deg
ZDOT = -959
295489 TA = 29
51948
MA = 29
46991
Ha = 222
861 n
mi
Hp = 212
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13948113
57 X = -4274480
10
Y = -638762
71 feet Y = -242365
51 meter
Z = 17282338
58 Z = 5246948
41
XDOT = -2779
987593 XDOT = -757
995883
YDOT = -24827
660309 feet/sec YDOT = -7576
446915 meter/sec
ZDOT = -3147
294913 ZDOT = -963
194121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11312290
86 X = 3447986
25
Y = -8376021
00 feet Y = -2553011
20 meter
Z = 17190446
90 Z = 5239648
22
XDOT = 17192
797227 XDOT = 5240
364595
YDOT = 16698
554039 feet/sec YDOT = 5089
719271 meter/sec
ZDOT = -3163
415936 ZDOT = -964
209177
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 17304
54660930
00016717 00000-0 10270-3 0 9016
2 25544 51
6385 78
5467 0005362 77
4171 282
7581 15
54279564 2957
Satellite: ISS
Catalog Number: 25544
Epoch time: 17304
54660930 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 78
5467 deg
Eccentricity:
0005362
Arg of perigee: 77
4171 deg
Mean anomaly: 282
7581 deg
Mean motion: 15
54279564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 295
Checksum: 327
Coasting Arc #3 (Orbit 309)
---------------------------------------
Vector Time (GMT): 2017/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4462228
90 A = 6779521
68 meter
Y = 1991362
57 meter E =
0015436
Z = -4713793
57 I = 51
98905
XDOT = -159
848429 Wp = 100
10593
YDOT = 7102
712960 meter/sec RA = 72
98638 deg
ZDOT = 2854
553136 TA = 198
10831
MA = 198
16335
Ha = 222
623 n
mi
Hp = 212
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14639858
60 X = 4462527
14
Y = 6533341
75 feet Y = 2041263
58 meter
Z = -15465201
99 Z = -4692116
36
XDOT = -524
437104 XDOT = -253
127325
YDOT = 23302
864043 feet/sec YDOT = 7100
404083 meter/sec
ZDOT = 9365
331812 ZDOT = 2853
549534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15483351
20 X = -4719325
45
Y = 4498115
29 feet Y = 1371025
54 meter
Z = -15369296
71 Z = -4684561
64
XDOT = -14233
719897 XDOT = -4338
437825
YDOT = -17074
207883 feet/sec YDOT = -5204
218563 meter/sec
ZDOT = 9359
750797 ZDOT = 2852
852043
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 17305
51102865
00016717 00000-0 10270-3 0 9023
2 25544 51
6389 73
7386 0005209 81
1143 279
0599 15
54309724 3107
Satellite: ISS
Catalog Number: 25544
Epoch time: 17305
51102865 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 73
7386 deg
Eccentricity:
0005209
Arg of perigee: 81
1143 deg
Mean anomaly: 279
0599 deg
Mean motion: 15
54309724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 310
Checksum: 304
Coasting Arc #4 (Orbit 319)
---------------------------------------
Vector Time (GMT): 2017/306/03:18:26
372
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3904947
01 A = 6777514
31 meter
Y = -1499864
22 meter E =
0018964
Z = -5348890
92 I = 51
97603
XDOT = 2677
437595 Wp = 86
42428
YDOT = 7170
647744 meter/sec RA = 69
84722 deg
ZDOT = -55
057621 TA = 183
04676
MA = 183
05833
Ha = 222
588 n
mi
Hp = 213
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12811505
94 X = 3947411
63
Y = -4920814
38 feet Y = -1455959
37 meter
Z = -17548854
72 Z = -5329818
16
XDOT = 8784
244077 XDOT = 2597
321951
YDOT = 23525
747192 feet/sec YDOT = 7200
140723 meter/sec
ZDOT = -180
635240 ZDOT = -42
246209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4998181
30 X = -1523445
66
Y = -12897280
17 feet Y = -3931091
00 meter
Z = -17463955
69 Z = -5323013
69
XDOT = 22533
193564 XDOT = 6868
117398
YDOT = -8558
933570 feet/sec YDOT = -2608
762952 meter/sec
ZDOT = -124
915806 ZDOT = -38
074338
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 17306
15397416
00016717 00000-0 10270-3 0 9033
2 25544 51
6413 70
5366 0004191 75
5231 284
6387 15
54075871 3203
Satellite: ISS
Catalog Number: 25544
Epoch time: 17306
15397416 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 70
5366 deg
Eccentricity:
0004191
Arg of perigee: 75
5231 deg
Mean anomaly: 284
6387 deg
Mean motion: 15
54075871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 320
Checksum: 300
Coasting Arc #5 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2017/307/03:18:26
372
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4478006
26 A = 6778542
38 meter
Y = -192091
76 meter E =
0009523
Z = 5078905
15 I = 51
96821
XDOT = -1793
732123 Wp = 64
74432
YDOT = -7228
532479 meter/sec RA = 64
87121 deg
ZDOT = -1848
249950 TA = 43
09824
MA = 43
02371
Ha = 222
676 n
mi
Hp = 213
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14691621
59 X = -4500196
99
Y = -630222
32 feet Y = -242291
70 meter
Z = 16663074
64 Z = 5057097
85
XDOT = -5884
947911 XDOT = -1703
789265
YDOT = -23715
657740 feet/sec YDOT = -7248
088413 meter/sec
ZDOT = -6063
812171 ZDOT = -1856
744761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -287080
74 X = -87502
21
Y = 14811275
95 feet Y = 4514476
91 meter
Z = 16566311
33 Z = 5049411
69
XDOT = -22494
892946 XDOT = -6856
443370
YDOT = 6411
746368 feet/sec YDOT = 1954
300293 meter/sec
ZDOT = -6100
343260 ZDOT = -1859
384626
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 17307
18284978
00016717 00000-0 10270-3 0 9046
2 25544 51
6419 65
4081 0004138 77
6845 282
4771 15
54110921 3367
Satellite: ISS
Catalog Number: 25544
Epoch time: 17307
18284978 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 65
4081 deg
Eccentricity:
0004138
Arg of perigee: 77
6845 deg
Mean anomaly: 282
4771 deg
Mean motion: 15
54110921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 317
Coasting Arc #6 (Orbit 336)
---------------------------------------
Vector Time (GMT): 2017/307/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4779320
44 A = 6782035
25 meter
Y = 2318329
37 meter E =
0011581
Z = -4227609
15 I = 51
97629
XDOT = 11
449021 Wp = 98
80246
YDOT = 6706
782360 meter/sec RA = 64
36359 deg
ZDOT = 3697
702235 TA = 208
96502
MA = 209
02934
Ha = 222
596 n
mi
Hp = 213
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15680185
18 X = 4773577
33
Y = 7606067
48 feet Y = 2371742
67 meter
Z = -13870108
76 Z = -4204406
06
XDOT = 37
562405 XDOT = -81
511030
YDOT = 22003
879133 feet/sec YDOT = 6706
390805 meter/sec
ZDOT = 12131
569013 ZDOT = 3697
531722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3548243
25 X = -1081504
54
Y = -17145448
44 feet Y = -5225932
68 meter
Z = -13767496
31 Z = -4196332
88
XDOT = 16247
876544 XDOT = 4952
352771
YDOT = -13084
119704 feet/sec YDOT = -3988
039686 meter/sec
ZDOT = 12129
720919 ZDOT = 3697
138936
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 17307
24715457
00016717 00000-0 10270-3 0 9055
2 25544 51
6400 65
0860 0004112 78
0905 282
0709 15
54073793 3375
Satellite: ISS
Catalog Number: 25544
Epoch time: 17307
24715457 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 65
0860 deg
Eccentricity:
0004112
Arg of perigee: 78
0905 deg
Mean anomaly: 282
0709 deg
Mean motion: 15
54073793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 337
Checksum: 294
Coasting Arc #7 (Orbit 352)
---------------------------------------
Vector Time (GMT): 2017/308/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4864674
12 A = 6785750
28 meter
Y = -3675698
44 meter E =
0017171
Z = 2962237
70 I = 51
97405
XDOT = 1210
997787 Wp = 93
51240
YDOT = -5670
761946 meter/sec RA = 59
40374 deg
ZDOT = -5023
853651 TA = 52
79425
MA = 52
63766
Ha = 222
585 n
mi
Hp = 213
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15960216
94 X = -4837599
49
Y = -12059378
09 feet Y = -3729947
09 meter
Z = 9718627
64 Z = 2938671
72
XDOT = 3973
089851 XDOT = 1298
723967
YDOT = -18604
862028 feet/sec YDOT = -5656
729368 meter/sec
ZDOT = -16482
459484 ZDOT = -5017
757577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 510480
05 X = 155594
32
Y = 20047618
51 feet Y = 6110514
12 meter
Z = 9614637
28 Z = 2930541
44
XDOT = -15651
548902 XDOT = -4770
592105
YDOT = 8328
086953 feet/sec YDOT = 2538
400903 meter/sec
ZDOT = -16454
464055 ZDOT = -5015
320644
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 17308
27602749
00016717 00000-0 10270-3 0 9069
2 25544 51
6401 59
9582 0004088 79
9245 280
2368 15
54107503 3534
Satellite: ISS
Catalog Number: 25544
Epoch time: 17308
27602749 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 59
9582 deg
Eccentricity:
0004088
Arg of perigee: 79
9245 deg
Mean anomaly: 280
2368 deg
Mean motion: 15
54107503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 353
Checksum: 317
Coasting Arc #8 (Orbit 367)
---------------------------------------
Vector Time (GMT): 2017/309/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4715733
48 A = 6788642
73 meter
Y = 4661954
44 meter E =
0011619
Z = -1439858
40 I = 51
96537
XDOT = -2505
884335 Wp = 52
19721
YDOT = 4319
246275 meter/sec RA = 54
45091 deg
ZDOT = 5816
538254 TA = 292
17410
MA = 292
29736
Ha = 222
580 n
mi
Hp = 213
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15471566
53 X = 4670246
12
Y = 15295126
11 feet Y = 4714434
65 meter
Z = -4723944
88 Z = -1417060
58
XDOT = -8221
405297 XDOT = -2582
251853
YDOT = 14170
755495 feet/sec YDOT = 4290
796773 meter/sec
ZDOT = 19083
130753 ZDOT = 5804
179559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1976196
81 X = 602344
79
Y = -21687402
48 feet Y = -6610320
28 meter
Z = -4623540
73 Z = -1409255
21
XDOT = 14667
444839 XDOT = 4470
637187
YDOT = -2692
194915 feet/sec YDOT = -820
581010 meter/sec
ZDOT = 19027
550977 ZDOT = 5799
597538
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 17309
24059465
00016717 00000-0 10270-3 0 9079
2 25544 51
6395 55
1499 0003997 85
7496 274
4113 15
54073146 3686
Satellite: ISS
Catalog Number: 25544
Epoch time: 17309
24059465 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 55
1499 deg
Eccentricity:
0003997
Arg of perigee: 85
7496 deg
Mean anomaly: 274
4113 deg
Mean motion: 15
54073146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 368
Checksum: 339
Coasting Arc #9 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2017/310/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4232533
87 A = 6789409
33 meter
Y = -5294639
00 meter E =
0014507
Z = -280895
92 I = 51
94843
XDOT = 3844
979647 Wp = 124
33106
YDOT = -2765
922533 meter/sec RA = 49
50238 deg
ZDOT = -6030
237715 TA = 58
68290
MA = 58
54096
Ha = 222
563 n
mi
Hp = 213
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13886265
99 X = -4171648
74
Y = -17370862
85 feet Y = -5341629
65 meter
Z = -921574
54 Z = -301309
08
XDOT = 12614
762621 XDOT = 3904
915950
YDOT = -9074
548993 feet/sec YDOT = -2722
590093 meter/sec
ZDOT = -19784
244473 ZDOT = -6011
413931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4235445
76 X = -1290963
87
Y = 21828029
71 feet Y = 6653183
46 meter
Z = -1011274
99 Z = -308236
62
XDOT = -13579
586384 XDOT = -4139
057930
YDOT = -3515
868967 feet/sec YDOT = -1071
636861 meter/sec
ZDOT = -19700
223635 ZDOT = -6004
628164
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 17310
26946079
00016717 00000-0 10270-3 0 9080
2 25544 51
6397 50
0211 0004118 88
0464 272
1161 15
54086673 3846
Satellite: ISS
Catalog Number: 25544
Epoch time: 17310
26946079 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 50
0211 deg
Eccentricity:
0004118
Arg of perigee: 88
0464 deg
Mean anomaly: 272
1161 deg
Mean motion: 15
54086673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 300
Coasting Arc #10 (Orbit 388)
---------------------------------------
Vector Time (GMT): 2017/310/13:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025156
26 A = 6780724
30 meter
Y = 218606
98 meter E =
0013828
Z = -4560729
99 I = 51
91374
XDOT = 2566
227300 Wp = 104
97228
YDOT = 6493
310800 meter/sec RA = 47
77550 deg
ZDOT = 3143
257980 TA = 196
44223
MA = 196
48712
Ha = 222
597 n
mi
Hp = 213
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16486733
15 X = 5044492
66
Y = 717214
51 feet Y = 274909
95 meter
Z = -14963024
89 Z = -4536271
69
XDOT = 8419
380906 XDOT = 2478
157809
YDOT = 21303
513123 feet/sec YDOT = 6521
515594 meter/sec
ZDOT = 10312
526180 ZDOT = 3155
510522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5230486
71 X = -1594252
35
Y = 15754510
03 feet Y = 4801974
66 meter
Z = -14854504
46 Z = -4527652
96
XDOT = -21628
213311 XDOT = -6592
279417
YDOT = 2579
158395 feet/sec YDOT = 786
127479 meter/sec
ZDOT = 10365
796480 ZDOT = 3159
494767
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 17310
59098098
00016717 00000-0 10270-3 0 9096
2 25544 51
6413 48
4186 0004244 93
6282 266
5356 15
54106201 3895
Satellite: ISS
Catalog Number: 25544
Epoch time: 17310
59098098 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 48
4186 deg
Eccentricity:
0004244
Arg of perigee: 93
6282 deg
Mean anomaly: 266
5356 deg
Mean motion: 15
54106201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 389
Checksum: 315
Coasting Arc #11 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2017/311/13:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5634953
01 A = 6784467
35 meter
Y = -1555148
25 meter E =
0016559
Z = 3428864
87 I = 51
90354
XDOT = -1163
026187 Wp = 91
29443
YDOT = -6014
905693 meter/sec RA = 42
80740 deg
ZDOT = -4620
494610 TA = 48
69640
MA = 48
55398
Ha = 222
615 n
mi
Hp = 213
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18487378
65 X = -5633800
24
Y = -5102192
44 feet Y = -1618155
83 meter
Z = 11249556
66 Z = 3401494
14
XDOT = -3815
702713 XDOT = -1073
234864
YDOT = -19733
942563 feet/sec YDOT = -6027
409224 meter/sec
ZDOT = -15159
103050 ZDOT = -4625
926482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9704822
33 X = 2958029
85
Y = -16623613
40 feet Y = -5066877
36 meter
Z = 11128340
53 Z = 3391918
19
XDOT = 18814
735475 XDOT = 5734
731373
YDOT = 778
758431 feet/sec YDOT = 237
365570 meter/sec
ZDOT = -15182
170319 ZDOT = -4627
525513
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 17311
61984147
00016717 00000-0 10270-3 0 9101
2 25544 51
6411 43
2904 0004119 95
8524 264
3096 15
54121842 4052
Satellite: ISS
Catalog Number: 25544
Epoch time: 17311
61984147 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 43
2904 deg
Eccentricity:
0004119
Arg of perigee: 95
8524 deg
Mean anomaly: 264
3096 deg
Mean motion: 15
54121842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 287
Coasting Arc #12 (Orbit 419)
---------------------------------------
Vector Time (GMT): 2017/312/13:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5930790
83 A = 6787856
07 meter
Y = 2635144
62 meter E =
0009660
Z = -1986312
82 I = 51
88913
XDOT = -449
362993 Wp = 60
93535
YDOT = 5213
340019 meter/sec RA = 37
84752 deg
ZDOT = 5599
656747 TA = 277
22823
MA = 277
33804
Ha = 222
610 n
mi
Hp = 213
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19457975
15 X = 5910531
85
Y = 8645487
58 feet Y = 2701353
56 meter
Z = -6516774
35 Z = -1957551
49
XDOT = -1474
288034 XDOT = -534
827418
YDOT = 17104
133921 feet/sec YDOT = 5207
836883 meter/sec
ZDOT = 18371
577254 ZDOT = 5597
266438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13083078
64 X = -3987722
37
Y = 16847313
29 feet Y = 5135061
09 meter
Z = -6389576
55 Z = -1947542
93
XDOT = -14990
831725 XDOT = -4569
205510
YDOT = -4709
934772 feet/sec YDOT = -1435
588118 meter/sec
ZDOT = 18360
056976 ZDOT = 5596
145366
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 17312
58439565
00016717 00000-0 10270-3 0 9118
2 25544 51
6404 38
4827 0004129 99
5363 260
6257 15
54080015 4208
Satellite: ISS
Catalog Number: 25544
Epoch time: 17312
58439565 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 38
4827 deg
Eccentricity:
0004129
Arg of perigee: 99
5363 deg
Mean anomaly: 260
6257 deg
Mean motion: 15
54080015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 420
Checksum: 300
Coasting Arc #13 (Orbit 435)
---------------------------------------
Vector Time (GMT): 2017/313/13:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5810438
02 A = 6789320
92 meter
Y = -3486946
41 meter E =
0016392
Z = 289776
20 I = 51
86875
XDOT = 2209
659701 Wp = 123
82329
YDOT = -4202
161268 meter/sec RA = 32
89236 deg
ZDOT = -6023
716898 TA = 53
06321
MA = 52
91318
Ha = 222
562 n
mi
Hp = 213
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19063116
85 X = -5772421
81
Y = -11440112
89 feet Y = -3551710
14 meter
Z = 950709
31 Z = 261642
76
XDOT = 7249
539702 XDOT = 2285
745829
YDOT = -13786
618333 feet/sec YDOT = -4177
025786 meter/sec
ZDOT = -19762
850716 ZDOT = -6012
798199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15418903
94 X = 4699681
92
Y = -16023633
60 feet Y = -4884003
52 meter
Z = 826451
88 Z = 251902
53
XDOT = 10617
717238 XDOT = 3236
280214
YDOT = 9154
494007 feet/sec YDOT = 2790
289773 meter/sec
ZDOT = -19713
649994 ZDOT = -6008
720518
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 17313
61324716
00016717 00000-0 10270-3 0 9125
2 25544 51
6411 33
3536 0004300 100
7943 259
3693 15
54122695 4364
Satellite: ISS
Catalog Number: 25544
Epoch time: 17313
61324716 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 33
3536 deg
Eccentricity:
0004300
Arg of perigee: 100
7943 deg
Mean anomaly: 259
3693 deg
Mean motion: 15
54122695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 436
Checksum: 283
Coasting Arc #14 (Orbit 451)
---------------------------------------
Vector Time (GMT): 2017/314/13:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5275376
43 A = 6788634
28 meter
Y = 4030316
97 meter E =
0017354
Z = 1385868
81 I = 51
83717
XDOT = -3913
796795 Wp = 70
07096
YDOT = 3102
799145 meter/sec RA = 27
93704 deg
ZDOT = 5821
334748 TA = 304
99323
MA = 305
15602
Ha = 222
655 n
mi
Hp = 213
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17307665
47 X = 5223184
32
Y = 13222824
71 feet Y = 4089018
00 meter
Z = 4546813
69 Z = 1411368
52
XDOT = -12840
540665 XDOT = -3976
479767
YDOT = 10179
787220 feet/sec YDOT = 3058
681881 meter/sec
ZDOT = 19098
867285 ZDOT = 5802
170279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16514511
51 X = -5033623
11
Y = 14164529
97 feet Y = 4317348
74 meter
Z = 4659280
23 Z = 1420148
61
XDOT = -6242
747548 XDOT = -1902
789453
YDOT = -13588
822827 feet/sec YDOT = -4141
873198 meter/sec
ZDOT = 19013
261422 ZDOT = 5795
242081
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 17314
64209613
00016717 00000-0 10270-3 0 9138
2 25544 51
6402 28
2254 0004371 102
8945 257
2696 15
54075108 4521
Satellite: ISS
Catalog Number: 25544
Epoch time: 17314
64209613 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 28
2254 deg
Eccentricity:
0004371
Arg of perigee: 102
8945 deg
Mean anomaly: 257
2696 deg
Mean motion: 15
54075108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 452
Checksum: 293
Coasting Arc #15 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2017/315/12:37:22
000
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1439896
52 A = 6777482
04 meter
Y = -3951554
11 meter E =
0018773
Z = -5330869
91 I = 51
77232
XDOT = 7095
049161 Wp = 92
92293
YDOT = 2865
219875 meter/sec RA = 23
22351 deg
ZDOT = -209
026828 TA = 175
09419
MA = 175
07576
Ha = 222
524 n
mi
Hp = 213
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4724069
96 X = 1509871
91
Y = -12964416
36 feet Y = -3935061
00 meter
Z = -17489730
67 Z = -5323705
25
XDOT = 23277
720346 XDOT = 7063
497548
YDOT = 9400
327674 feet/sec YDOT = 2944
385143 meter/sec
ZDOT = -685
783558 ZDOT = -174
637528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8682392
59 X = 2646393
26
Y = 10777041
53 feet Y = 3284842
26 meter
Z = -17457234
67 Z = -5320965
13
XDOT = -19177
527514 XDOT = -5845
310386
YDOT = 14594
033665 feet/sec YDOT = 4448
261461 meter/sec
ZDOT = -533
664312 ZDOT = -162
660882
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 17315
54233287
00016717 00000-0 10270-3 0 9143
2 25544 51
6403 23
7376 0004138 110
2510 249
9088 15
54089788 4666
Satellite: ISS
Catalog Number: 25544
Epoch time: 17315
54233287 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 23
7376 deg
Eccentricity:
0004138
Arg of perigee: 110
2510 deg
Mean anomaly: 249
9088 deg
Mean motion: 15
54089788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 313
Coasting Arc #16 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2017/316/12:37:22
000
Vector Time (MET): N/A
Weight (LBS) : 919897
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3091005
18 A = 6778310
23 meter
Y = 3214069
81 meter E =
0008268
Z = 5098365
13 I = 51
74599
XDOT = -6564
271776 Wp = 79
43092
YDOT = -3586
158849 meter/sec RA = 18
23264 deg
ZDOT = -1715
148410 TA = 27
12630
MA = 27
08313
Ha = 222
506 n
mi
Hp = 213
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10141093
11 X = -3151481
74
Y = 10544848
46 feet Y = 3179166
05 meter
Z = 16726919
73 Z = 5083202
82
XDOT = -21536
324723 XDOT = -6515
351049
YDOT = -11765
613022 feet/sec YDOT = -3659
291528 meter/sec
ZDOT = -5627
127330 ZDOT = -1746
917148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4083791
10 X = -1244739
53
Y = -14128826
69 feet Y = -4306466
38 meter
Z = 16659062
06 Z = 5077682
12
XDOT = 19840
283967 XDOT = 6047
318553
YDOT = -12549
882693 feet/sec YDOT = -3825
204245 meter/sec
ZDOT = -5767
478474 ZDOT = -1757
927439
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 17316
57117043
00016717 00000-0 10270-3 0 9159
2 25544 51
6411 18
6090 0004094 112
8136 247
3450 15
54147940 4822
Satellite: ISS
Catalog Number: 25544
Epoch time: 17316
57117043 = yrday
fracday
Element set: 915
Inclination: 51
6411 deg
RA of node: 18
6090 deg
Eccentricity:
0004094
Arg of perigee: 112
8136 deg
Mean anomaly: 247
3450 deg
Mean motion: 15
54147940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 482
Checksum: 285
Coasting Arc #17 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2017/317/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 934611
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5291565
12 A = 6786458
62 meter
Y = -3379336
78 meter E =
0009257
Z = -2574997
96 I = 51
74464
XDOT = 4576
380022 Wp = 122
08866
YDOT = -3163
153059 meter/sec RA = 13
69607 deg
ZDOT = -5271
818473 TA = 86
80716
MA = 86
70125
Ha = 222
427 n
mi
Hp = 213
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17360777
94 X = -5240874
90
Y = -11087062
94 feet Y = -3438227
33 meter
Z = -8448156
02 Z = -2600579
95
XDOT = 15014
370150 XDOT = 4637
019458
YDOT = -10377
798750 feet/sec YDOT = -3111
637947 meter/sec
ZDOT = -17295
992367 ZDOT = -5249
440087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20550449
51 X = 6263777
01
Y = 279054
64 feet Y = 85055
86 meter
Z = -8561078
72 Z = -2609416
79
XDOT = -7346
334023 XDOT = -2239
162610
YDOT = 15303
420677 feet/sec YDOT = 4664
482623 meter/sec
ZDOT = -17196
124987 ZDOT = -5241
378896
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 17317
47140193
00016717 00000-0 10270-3 0 9162
2 25544 51
6414 14
1208 0004227 117
0062 243
1522 15
54121514 4968
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
47140193 = yrday
fracday
Element set: 916
Inclination: 51
6414 deg
RA of node: 14
1208 deg
Eccentricity:
0004227
Arg of perigee: 117
0062 deg
Mean anomaly: 243
1522 deg
Mean motion: 15
54121514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 264
Coasting Arc #18 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2017/317/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934611
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4997084
73 A = 6782572
04 meter
Y = -2233344
53 meter E =
0011021
Z = -4017262
09 I = 51
71710
XDOT = 5046
049108 Wp = 108
70781
YDOT = 4191
241057 meter/sec RA = 11
31908 deg
ZDOT = 3952
165121 TA = 202
37322
MA = 202
42133
Ha = 222
462 n
mi
Hp = 213
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16394634
94 X = 5041201
44
Y = -7327245
85 feet Y = -2177217
17 meter
Z = -13179993
75 Z = -3992880
14
XDOT = 16555
279225 XDOT = 4979
608460
YDOT = 13750
790870 feet/sec YDOT = 4247
298051 meter/sec
ZDOT = 12966
421001 ZDOT = 3976
516213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12769388
67 X = 3892109
67
Y = -12738364
63 feet Y = -3882653
54 meter
Z = -13071403
94 Z = -3984163
92
XDOT = 19370
039315 XDOT = 5903
987983
YDOT = 6020
124247 feet/sec YDOT = 1834
933870 meter/sec
ZDOT = 13073
732346 ZDOT = 3984
873619
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 17317
92151709
00016717 00000-0 10270-3 0 9178
2 25544 51
6419 11
8792 0004189 112
2905 247
8692 15
54141743 5039
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
92151709 = yrday
fracday
Element set: 917
Inclination: 51
6419 deg
RA of node: 11
8792 deg
Eccentricity:
0004189
Arg of perigee: 112
2905 deg
Mean anomaly: 247
8692 deg
Mean motion: 15
54141743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 311
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