[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 2nd 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 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 309)
---------------------------------------
Vector Time (GMT): 2017/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4462177
57 A = 6779520
73 meter
Y = 1991628
74 meter E =
0015411
Z = -4713694
97 I = 51
98939
XDOT = -160
063515 Wp = 99
98551
YDOT = 7102
635523 meter/sec RA = 72
98648 deg
ZDOT = 2854
805357 TA = 198
23107
MA = 198
28638
Ha = 222
617 n
mi
Hp = 212
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14639690
20 X = 4462472
36
Y = 6534215
04 feet Y = 2041529
16 meter
Z = -15464878
50 Z = -4692018
02
XDOT = -525
142767 XDOT = -253
342755
YDOT = 23302
609982 feet/sec YDOT = 7100
324238 meter/sec
ZDOT = 9366
159307 ZDOT = 2853
800709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15483783
27 X = -4719457
14
Y = 4497337
43 feet Y = 1370788
45 meter
Z = -15368974
40 Z = -4684463
40
XDOT = -14233
069088 XDOT = -4338
239458
YDOT = -17074
440095 feet/sec YDOT = -5204
289341 meter/sec
ZDOT = 9360
573662 ZDOT = 2853
102852
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
51102814
00016717 00000-0 10270-3 0 9005
2 25544 51
6392 73
7387 0005196 80
6867 279
4874 15
54310157 3106
Satellite: ISS
Catalog Number: 25544
Epoch time: 17305
51102814 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 73
7387 deg
Eccentricity:
0005196
Arg of perigee: 80
6867 deg
Mean anomaly: 279
4874 deg
Mean motion: 15
54310157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 310
Checksum: 305
Coasting Arc #2 (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 = 3905052
83 A = 6777512
22 meter
Y = -1499469
53 meter E =
0018949
Z = -5348907
41 I = 51
97637
XDOT = 2677
151886 Wp = 86
31016
YDOT = 7170
772087 meter/sec RA = 69
84734 deg
ZDOT = -54
681796 TA = 183
16424
MA = 183
17624
Ha = 222
583 n
mi
Hp = 213
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12811853
11 X = 3947513
11
Y = -4919519
47 feet Y = -1455563
52 meter
Z = -17548908
84 Z = -5329834
15
XDOT = 8783
306711 XDOT = 2597
033047
YDOT = 23526
155141 feet/sec YDOT = 7200
261853 meter/sec
ZDOT = -179
402217 ZDOT = -41
871780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4996888
46 X = -1523051
60
Y = -12897635
30 feet Y = -3931199
24 meter
Z = -17464007
64 Z = -5323029
53
XDOT = 22533
581270 XDOT = 6868
235571
YDOT = -8558
084820 feet/sec YDOT = -2608
504253 meter/sec
ZDOT = -123
688997 ZDOT = -37
700406
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
15397344
00016717 00000-0 10270-3 0 9011
2 25544 51
6416 70
5368 0004184 74
9672 285
1943 15
54076549 3209
Satellite: ISS
Catalog Number: 25544
Epoch time: 17306
15397344 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 70
5368 deg
Eccentricity:
0004184
Arg of perigee: 74
9672 deg
Mean anomaly: 285
1943 deg
Mean motion: 15
54076549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 320
Checksum: 314
Coasting Arc #3 (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 = -4478185
95 A = 6778540
19 meter
Y = -192911
83 meter E =
0009528
Z = 5078735
78 I = 51
96855
XDOT = -1793
103947 Wp = 64
49397
YDOT = -7228
489532 meter/sec RA = 64
87136 deg
ZDOT = -1848
951188 TA = 43
35572
MA = 43
28080
Ha = 222
670 n
mi
Hp = 213
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14692211
13 X = -4500366
68
Y = -632912
83 feet Y = -243113
72 meter
Z = 16662518
95 Z = 5056927
62
XDOT = -5882
886965 XDOT = -1703
158210
YDOT = -23715
516836 feet/sec YDOT = -7248
038425 meter/sec
ZDOT = -6066
112821 ZDOT = -1857
442941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -289757
07 X = -88317
95
Y = 14811923
77 feet Y = 4514674
37 meter
Z = 16565752
01 Z = 5049241
21
XDOT = -22494
752944 XDOT = -6856
400697
YDOT = 6409
862828 feet/sec YDOT = 1953
726190 meter/sec
ZDOT = -6102
630342 ZDOT = -1860
081728
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
18284852
00016717 00000-0 10270-3 0 9025
2 25544 51
6421 65
4083 0004132 77
1119 283
0496 15
54111955 3364
Satellite: ISS
Catalog Number: 25544
Epoch time: 17307
18284852 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 65
4083 deg
Eccentricity:
0004132
Arg of perigee: 77
1119 deg
Mean anomaly: 283
0496 deg
Mean motion: 15
54111955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 293
Coasting Arc #4 (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 = 4779273
85 A = 6782033
45 meter
Y = 2319054
75 meter E =
0011560
Z = -4227219
71 I = 51
97663
XDOT = 10
792992 Wp = 98
61824
YDOT = 6706
480197 meter/sec RA = 64
36375 deg
ZDOT = 3698
314533 TA = 209
15609
MA = 209
22067
Ha = 222
591 n
mi
Hp = 213
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15680032
33 X = 4773520
74
Y = 7608447
34 feet Y = 2372467
47 meter
Z = -13868831
05 Z = -4204016
87
XDOT = 35
410079 XDOT = -82
166606
YDOT = 22002
887786 feet/sec YDOT = 6706
081309 meter/sec
ZDOT = 12133
577864 ZDOT = 3698
140834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3546255
47 X = -1080898
67
Y = -17146767
14 feet Y = -5226334
62 meter
Z = -13766219
84 Z = -4195943
81
XDOT = 16248
309695 XDOT = 4952
484795
YDOT = -13081
942690 feet/sec YDOT = -3987
376132 meter/sec
ZDOT = 12131
715679 ZDOT = 3697
746939
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
24715326
00016717 00000-0 10270-3 0 9038
2 25544 51
6403 65
0863 0004107 77
5144 282
6468 15
54074866 3374
Satellite: ISS
Catalog Number: 25544
Epoch time: 17307
24715326 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 65
0863 deg
Eccentricity:
0004107
Arg of perigee: 77
5144 deg
Mean anomaly: 282
6468 deg
Mean motion: 15
54074866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 337
Checksum: 306
Coasting Arc #5 (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 = -4864443
16 A = 6785748
14 meter
Y = -3676766
71 meter E =
0017158
Z = 2961348
12 I = 51
97438
XDOT = 1212
112105 Wp = 93
39065
YDOT = -5669
872329 meter/sec RA = 59
40394 deg
ZDOT = -5024
544087 TA = 52
92779
MA = 52
77104
Ha = 222
579 n
mi
Hp = 213
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15959459
19 X = -4837352
28
Y = -12062882
91 feet Y = -3731012
68 meter
Z = 9715709
05 Z = 2937783
30
XDOT = 3976
745752 XDOT = 1299
831609
YDOT = -18601
943337 feet/sec YDOT = -5655
827327 meter/sec
ZDOT = -16484
724696 ZDOT = -5018
442617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 507251
19 X = 154610
16
Y = 20049188
06 feet Y = 6110992
52 meter
Z = 9611724
02 Z = 2929653
48
XDOT = -15651
429065 XDOT = -4770
555579
YDOT = 8323
632881 feet/sec YDOT = 2537
043302 meter/sec
ZDOT = -16456
705459 ZDOT = -5016
003824
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
27602535
00016717 00000-0 10270-3 0 9040
2 25544 51
6404 59
9584 0004084 79
3337 280
8276 15
54109011 3531
Satellite: ISS
Catalog Number: 25544
Epoch time: 17308
27602535 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 59
9584 deg
Eccentricity:
0004084
Arg of perigee: 79
3337 deg
Mean anomaly: 280
8276 deg
Mean motion: 15
54109011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 353
Checksum: 305
Coasting Arc #6 (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 = 4715001
96 A = 6788639
14 meter
Y = 4663129
72 meter E =
0011642
Z = -1438273
95 I = 51
96570
XDOT = -2507
526608 Wp = 52
00118
YDOT = 4317
614664 meter/sec RA = 54
45114 deg
ZDOT = 5817
093937 TA = 292
38776
MA = 292
51107
Ha = 222
574 n
mi
Hp = 213
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15469166
53 X = 4669493
82
Y = 15298982
04 feet Y = 4715601
64 meter
Z = -4718746
57 Z = -1415479
74
XDOT = -8226
793334 XDOT = -2583
878459
YDOT = 14165
402440 feet/sec YDOT = 4289
146884 meter/sec
ZDOT = 19084
953860 ZDOT = 5804
727303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1980721
66 X = 603723
96
Y = -21687969
92 feet Y = -6610493
23 meter
Z = -4618358
61 Z = -1407675
70
XDOT = 14666
695548 XDOT = 4470
408803
YDOT = -2684
954451 feet/sec YDOT = -818
374117 meter/sec
ZDOT = 19029
339116 ZDOT = 5800
142563
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
24059147
00016717 00000-0 10270-3 0 9054
2 25544 51
6398 55
1502 0003992 85
1392 275
0216 15
54075040 3684
Satellite: ISS
Catalog Number: 25544
Epoch time: 17309
24059147 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 55
1502 deg
Eccentricity:
0003992
Arg of perigee: 85
1392 deg
Mean anomaly: 275
0216 deg
Mean motion: 15
54075040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 368
Checksum: 302
Coasting Arc #7 (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 = -4231034
25 A = 6789401
94 meter
Y = -5295745
81 meter E =
0014472
Z = -283236
41 I = 51
94876
XDOT = 3847
052767 Wp = 124
21491
YDOT = -2763
242841 meter/sec RA = 49
50263 deg
ZDOT = -6030
101709 TA = 58
82416
MA = 58
68236
Ha = 222
557 n
mi
Hp = 213
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13881345
95 X = -4170125
47
Y = -17374494
13 feet Y = -5342719
56 meter
Z = -929253
32 Z = -303642
23
XDOT = 12621
564196 XDOT = 3906
958291
YDOT = -9065
757352 feet/sec YDOT = -2719
887390 meter/sec
ZDOT = -19783
798257 ZDOT = -6011
267928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4241432
81 X = -1292788
72
Y = 21826597
79 feet Y = 6652747
01 meter
Z = -1018921
00 Z = -310567
12
XDOT = -13577
400519 XDOT = -4138
391678
YDOT = -3526
307486 feet/sec YDOT = -1074
818522 meter/sec
ZDOT = -19699
733506 ZDOT = -6004
478773
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
26945622
00016717 00000-0 10270-3 0 9061
2 25544 51
6400 50
0214 0004113 87
4467 272
7156 15
54088988 3846
Satellite: ISS
Catalog Number: 25544
Epoch time: 17310
26945622 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 50
0214 deg
Eccentricity:
0004113
Arg of perigee: 87
4467 deg
Mean anomaly: 272
7156 deg
Mean motion: 15
54088988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 301
Coasting Arc #8 (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 = 5026215
93 A = 6780722
06 meter
Y = 221429
13 meter E =
0013804
Z = -4559385
95 I = 51
91409
XDOT = 2563
462542 Wp = 104
80589
YDOT = 6493
210525 meter/sec RA = 47
77572 deg
ZDOT = 3145
790916 TA = 196
63633
MA = 196
68166
Ha = 222
591 n
mi
Hp = 213
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16490209
74 X = 5045514
16
Y = 726473
53 feet Y = 277743
74 meter
Z = -14958615
31 Z = -4534922
59
XDOT = 8410
310177 XDOT = 2475
382073
YDOT = 21303
184137 feet/sec YDOT = 6521
384340 meter/sec
ZDOT = 10320
836340 ZDOT = 3158
030002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5240336
27 X = -1597254
50
Y = 15755290
00 feet Y = 4802212
39 meter
Z = -14850072
93 Z = -4526302
23
XDOT = -21625
341679 XDOT = -6591
404144
YDOT = 2571
190302 feet/sec YDOT = 783
698804 meter/sec
ZDOT = 10374
046927 ZDOT = 3162
009503
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
59097591
00016717 00000-0 10270-3 0 9071
2 25544 51
6415 48
4190 0004236 93
0514 267
1124 15
54108717 3899
Satellite: ISS
Catalog Number: 25544
Epoch time: 17310
59097591 = yrday
fracday
Element set: 907
Inclination: 51
6415 deg
RA of node: 48
4190 deg
Eccentricity:
0004236
Arg of perigee: 93
0514 deg
Mean anomaly: 267
1124 deg
Mean motion: 15
54108717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 389
Checksum: 304
Coasting Arc #9 (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 = -5635628
97 A = 6784466
50 meter
Y = -1558740
37 meter E =
0016561
Z = 3426162
99 I = 51
90389
XDOT = -1158
774643 Wp = 91
17729
YDOT = -6013
704131 meter/sec RA = 42
80766 deg
ZDOT = -4623
086171 TA = 48
85181
MA = 48
70902
Ha = 222
608 n
mi
Hp = 213
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18489596
37 X = -5634422
86
Y = -5113977
60 feet Y = -1621755
20 meter
Z = 11240692
21 Z = 3398789
10
XDOT = -3801
754078 XDOT = -1068
984484
YDOT = -19730
000431 feet/sec YDOT = -6026
160125 meter/sec
ZDOT = -15167
605548 ZDOT = -4628
497393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9716767
08 X = 2961670
61
Y = -16622667
93 feet Y = -5066589
18 meter
Z = 11119462
70 Z = 3389212
23
XDOT = 18807
392719 XDOT = 5732
493301
YDOT = 790
406122 feet/sec YDOT = 240
915786 meter/sec
ZDOT = -15190
581368 ZDOT = -4630
089201
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
61983461
00016717 00000-0 10270-3 0 9086
2 25544 51
6414 43
2907 0004113 95
2434 264
9186 15
54124831 4053
Satellite: ISS
Catalog Number: 25544
Epoch time: 17311
61983461 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 43
2907 deg
Eccentricity:
0004113
Arg of perigee: 95
2434 deg
Mean anomaly: 264
9186 deg
Mean motion: 15
54124831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 293
Coasting Arc #10 (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 = 5930392
28 A = 6787853
31 meter
Y = 2639135
58 meter E =
0009693
Z = -1982050
02 I = 51
88949
XDOT = -455
141920 Wp = 60
64972
YDOT = 5210
772413 meter/sec RA = 37
84782 deg
ZDOT = 5601
645036 TA = 277
56308
MA = 277
67318
Ha = 222
604 n
mi
Hp = 213
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19456667
60 X = 5910068
00
Y = 8658581
30 feet Y = 2705339
70 meter
Z = -6502788
78 Z = -1953290
78
XDOT = -1493
247770 XDOT = -540
586862
YDOT = 17095
710017 feet/sec YDOT = 5205
204762 meter/sec
ZDOT = 18378
100513 ZDOT = 5599
226702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13095452
10 X = -3991493
80
Y = 16842804
18 feet Y = 5133686
72 meter
Z = -6375600
97 Z = -1943283
18
XDOT = -14978
412403 XDOT = -4565
420100
YDOT = -4725
449566 feet/sec YDOT = -1440
317028 meter/sec
ZDOT = 18366
456291 ZDOT = 5598
095877
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
58438680
00016717 00000-0 10270-3 0 9092
2 25544 51
6407 38
4831 0004123 98
9139 261
2481 15
54083385 4203
Satellite: ISS
Catalog Number: 25544
Epoch time: 17312
58438680 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 38
4831 deg
Eccentricity:
0004123
Arg of perigee: 98
9139 deg
Mean anomaly: 261
2481 deg
Mean motion: 15
54083385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 420
Checksum: 309
Coasting Arc #11 (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 = -5808282
51 A = 6789310
57 meter
Y = -3491072
10 meter E =
0016359
Z = 283924
32 I = 51
86908
XDOT = 2216
874610 Wp = 123
72261
YDOT = -4197
769373 meter/sec RA = 32
89269 deg
ZDOT = -6024
079614 TA = 53
22685
MA = 53
07681
Ha = 222
556 n
mi
Hp = 213
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19056044
97 X = -5770191
90
Y = -11453648
61 feet Y = -3555811
31 meter
Z = 931510
23 Z = 255801
53
XDOT = 7273
210662 XDOT = 2292
912852
YDOT = -13772
209230 feet/sec YDOT = -4172
553477 meter/sec
ZDOT = -19764
040728 ZDOT = -6013
125982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15430486
15 X = 4703212
18
Y = -16013587
67 feet Y = -4880941
52 meter
Z = 807300
79 Z = 246065
28
XDOT = 10599
105330 XDOT = 3230
607304
YDOT = 9173
500653 feet/sec YDOT = 2796
082999 meter/sec
ZDOT = -19714
685731 ZDOT = -6009
036211
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
61323585
00016717 00000-0 10270-3 0 9106
2 25544 51
6414 33
3539 0004296 100
1946 259
9691 15
54126659 4369
Satellite: ISS
Catalog Number: 25544
Epoch time: 17313
61323585 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 33
3539 deg
Eccentricity:
0004296
Arg of perigee: 100
1946 deg
Mean anomaly: 259
9691 deg
Mean motion: 15
54126659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 436
Checksum: 309
Coasting Arc #12 (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 = 5270596
68 A = 6788612
67 meter
Y = 4034053
94 meter E =
0017383
Z = 1392885
72 I = 51
83748
XDOT = -3921
954407 Wp = 70
00607
YDOT = 3096
543708 meter/sec RA = 27
93738 deg
ZDOT = 5819
243698 TA = 305
13628
MA = 305
29906
Ha = 222
648 n
mi
Hp = 213
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17291983
86 X = 5218329
05
Y = 13235085
11 feet Y = 4092701
10 meter
Z = 4569835
04 Z = 1418362
02
XDOT = -12867
304485 XDOT = -3984
556666
YDOT = 10159
264133 feet/sec YDOT = 3052
335672 meter/sec
ZDOT = 19092
006882 ZDOT = 5800
039796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16523229
30 X = -5036280
29
Y = 14146501
33 feet Y = 4311853
61 meter
Z = 4682197
05 Z = 1427133
66
XDOT = -6218
450437 XDOT = -1895
383693
YDOT = -13610
075912 feet/sec YDOT = -4148
351138 meter/sec
ZDOT = 19006
227108 ZDOT = 5793
098023
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
64208201
00016717 00000-0 10270-3 0 9118
2 25544 51
6405 28
2258 0004369 102
2999 257
8642 15
54079650 4521
Satellite: ISS
Catalog Number: 25544
Epoch time: 17314
64208201 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 28
2258 deg
Eccentricity:
0004369
Arg of perigee: 102
2999 deg
Mean anomaly: 257
8642 deg
Mean motion: 15
54079650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 452
Checksum: 303
Coasting Arc #13 (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 = 1450151
91 A = 6777466
41 meter
Y = -3947369
90 meter E =
0018784
Z = -5331183
72 I = 51
77265
XDOT = 7092
373765 Wp = 92
84221
YDOT = 2872
525450 meter/sec RA = 23
22370 deg
ZDOT = -199
199661 TA = 175
26828
MA = 175
25050
Ha = 222
517 n
mi
Hp = 213
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4757716
25 X = 1520081
27
Y = -12950688
64 feet Y = -3930762
36 meter
Z = -17490760
22 Z = -5323969
35
XDOT = 23268
942799 XDOT = 7060
692922
YDOT = 9424
296096 feet/sec YDOT = 2951
660078 meter/sec
ZDOT = -653
542196 ZDOT = -164
823671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8653416
19 X = 2637561
26
Y = 10798979
99 feet Y = 3291529
10 meter
Z = -17458044
36 Z = -5321211
92
XDOT = -19191
957598 XDOT = -5849
708676
YDOT = 14576
185122 feet/sec YDOT = 4442
821225 meter/sec
ZDOT = -501
483313 ZDOT = -152
852114
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
54231602
00016717 00000-0 10270-3 0 9120
2 25544 51
6406 23
7380 0004132 109
6098 250
5501 15
54094777 4663
Satellite: ISS
Catalog Number: 25544
Epoch time: 17315
54231602 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 23
7380 deg
Eccentricity:
0004132
Arg of perigee: 109
6098 deg
Mean anomaly: 250
5501 deg
Mean motion: 15
54094777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 287
Coasting Arc #14 (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 = -3102475
85 A = 6778307
50 meter
Y = 3207740
46 meter E =
0008315
Z = 5095369
01 I = 51
74636
XDOT = -6557
351449 Wp = 79
08486
YDOT = -3593
358544 meter/sec RA = 18
23283 deg
ZDOT = -1726
560427 TA = 27
58593
MA = 27
54183
Ha = 222
500 n
mi
Hp = 213
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10178726
55 X = -3162866
23
Y = 10524082
86 feet Y = 3172708
90 meter
Z = 16717089
93 Z = 5080151
18
XDOT = -21513
620239 XDOT = -6508
295293
YDOT = -11789
234067 feet/sec YDOT = -3666
413077 meter/sec
ZDOT = -5664
568329 ZDOT = -1758
295218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4047142
14 X = -1233568
93
Y = -14151175
27 feet Y = -4313278
22 meter
Z = 16648987
02 Z = 5074611
24
XDOT = 19847
808298 XDOT = 6049
611969
YDOT = -12520
916519 feet/sec YDOT = -3816
375355 meter/sec
ZDOT = -5804
767549 ZDOT = -1769
293149
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
57115016
00016717 00000-0 10270-3 0 9135
2 25544 51
6415 18
6094 0004089 112
1618 247
9969 15
54153431 4825
Satellite: ISS
Catalog Number: 25544
Epoch time: 17316
57115016 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 18
6094 deg
Eccentricity:
0004089
Arg of perigee: 112
1618 deg
Mean anomaly: 247
9969 deg
Mean motion: 15
54153431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 482
Checksum: 304
Coasting Arc #15 (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 = -5282274
40 A = 6786418
15 meter
Y = -3385762
66 meter E =
0009227
Z = -2585685
89 I = 51
74489
XDOT = 4590
046027 Wp = 121
59613
YDOT = -3154
337901 meter/sec RA = 13
69639 deg
ZDOT = -5265
134690 TA = 87
43078
MA = 87
32515
Ha = 222
421 n
mi
Hp = 213
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17330296
58 X = -5231461
10
Y = -11108145
22 feet Y = -3444548
62 meter
Z = -8483221
44 Z = -2611222
46
XDOT = 15059
206126 XDOT = 4650
553407
YDOT = -10348
877629 feet/sec YDOT = -3102
670705 meter/sec
ZDOT = -17274
063942 ZDOT = -5242
690238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20535501
64 X = 6259220
90
Y = 313176
70 feet Y = 95456
26 meter
Z = -8595941
39 Z = -2620042
94
XDOT = -7397
070704 XDOT = -2254
627151
YDOT = 15303
545331 feet/sec YDOT = 4664
520617 meter/sec
ZDOT = -17173
904954 ZDOT = -5234
606230
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
47137840
00016717 00000-0 10270-3 0 9145
2 25544 51
6417 14
1213 0004222 116
3763 243
7823 15
54127335 4969
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
47137840 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 14
1213 deg
Eccentricity:
0004222
Arg of perigee: 116
3763 deg
Mean anomaly: 243
7823 deg
Mean motion: 15
54127335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 288
Coasting Arc #16 (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 = 5008028
11 A = 6782583
24 meter
Y = -2224161
41 meter E =
0010983
Z = -4008660
67 I = 51
71753
XDOT = 5032
179716 Wp = 108
38453
YDOT = 4197
439723 meter/sec RA = 11
31933 deg
ZDOT = 3963
344020 TA = 202
83707
MA = 202
88595
Ha = 222
457 n
mi
Hp = 213
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16430538
43 X = 5051999
54
Y = -7297117
48 feet Y = -2167912
48 meter
Z = -13151773
84 Z = -3984225
90
XDOT = 16509
775972 XDOT = 4965
616482
YDOT = 13771
127699 feet/sec YDOT = 4253
340935 meter/sec
ZDOT = 13003
097179 ZDOT = 3987
627439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12813520
23 X = 3905560
97
Y = -12723002
45 feet Y = -3877971
15 meter
Z = -13042951
34 Z = -3975491
57
XDOT = 19335
717597 XDOT = 5893
526724
YDOT = 6052
261718 feet/sec YDOT = 1844
729372 meter/sec
ZDOT = 13110
107131 ZDOT = 3995
960654
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
92149183
00016717 00000-0 10270-3 0 9159
2 25544 51
6422 11
8796 0004190 111
6519 248
5080 15
54147877 5036
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
92149183 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 11
8796 deg
Eccentricity:
0004190
Arg of perigee: 111
6519 deg
Mean anomaly: 248
5080 deg
Mean motion: 15
54147877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 309
Coasting Arc #17 (Orbit 518)
---------------------------------------
Vector Time (GMT): 2017/318/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934611
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6066903
07 A = 6786439
79 meter
Y = 1437812
11 meter E =
0017691
Z = 2657934
10 I = 51
69755
XDOT = -3364
440363 Wp = 105
63969
YDOT = -4516
176492 meter/sec RA = 6
34311 deg
ZDOT = -5212
337048 TA = 44
37926
MA = 44
23761
Ha = 222
518 n
mi
Hp = 213
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19904537
63 X = -6095441
38
Y = 4717231
33 feet Y = 1369808
35 meter
Z = 8720256
25 Z = 2628392
97
XDOT = -11038
190168 XDOT = -3288
369687
YDOT = -14816
852008 feet/sec YDOT = -4553
374761 meter/sec
ZDOT = -17100
843332 ZDOT = -5228
495926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16752237
99 X = -5106082
14
Y = 11835483
28 feet Y = 3607455
30 meter
Z = 8588924
05 Z = 2617904
05
XDOT = -14808
466625 XDOT = -4513
620627
YDOT = -8440
415884 feet/sec YDOT = -2572
638761 meter/sec
ZDOT = -17171
736304 ZDOT = -5233
945225
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 17318
95031862
00016717 00000-0 10270-3 0 9168
2 25544 51
6418 6
7519 0004185 116
8758 243
2823 15
54123495 5197
Satellite: ISS
Catalog Number: 25544
Epoch time: 17318
95031862 = yrday
fracday
Element set: 916
Inclination: 51
6418 deg
RA of node: 6
7519 deg
Eccentricity:
0004185
Arg of perigee: 116
8758 deg
Mean anomaly: 243
2823 deg
Mean motion: 15
54123495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 519
Checksum: 319
Coasting Arc #18 (Orbit 533)
---------------------------------------
Vector Time (GMT): 2017/319/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934611
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6666108
43 A = 6788782
60 meter
Y = -686605
67 meter E =
0011047
Z = -1070248
14 I = 51
67424
XDOT = 1421
181530 Wp = 59
12719
YDOT = 4692
849444 meter/sec RA = 1
37194 deg
ZDOT = 5891
941383 TA = 289
27564
MA = 289
39510
Ha = 222
341 n
mi
Hp = 213
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21870434
49 X = 6678489
67
Y = -2252643
29 feet Y = -611991
48 meter
Z = -3511312
81 Z = -1037835
38
XDOT = 4662
669062 XDOT = 1339
978344
YDOT = 15396
487676 feet/sec YDOT = 4708
288121 meter/sec
ZDOT = 19330
516350 ZDOT = 5898
647906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19285535
70 X = 5878231
28
Y = -10604172
06 feet Y = -3232151
64 meter
Z = -3367383
54 Z = -1026378
50
XDOT = 9402
875306 XDOT = 2865
996393
YDOT = 11008
171209 feet/sec YDOT = 3355
290584 meter/sec
ZDOT = 19359
431766 ZDOT = 5900
754802
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 17319
91483791
00016717 00000-0 10270-3 0 9178
2 25544 51
6428 1
9434 0004021 119
4495 240
7059 15
54160896 5343
Satellite: ISS
Catalog Number: 25544
Epoch time: 17319
91483791 = yrday
fracday
Element set: 917
Inclination: 51
6428 deg
RA of node: 1
9434 deg
Eccentricity:
0004021
Arg of perigee: 119
4495 deg
Mean anomaly: 240
7059 deg
Mean motion: 15
54160896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 534
Checksum: 315
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