[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 10th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25336 0914 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
013/12:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
7
000/00:00:00
000 0
0 0
0 212
3
015/23:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
8
000/00:00:00
000 0
0 0
0 212
1
Coasting Arc #1 (Orbit 3706)
---------------------------------------
Vector Time (GMT): 2017/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2334872
66 A = 6789586
77 meter
Y = -6366609
97 meter E =
0015552
Z = -258960
92 I = 52
01434
XDOT = 4357
369612 Wp = 111
43965
YDOT = 1831
463151 meter/sec RA = 108
43104 deg
ZDOT = -6035
349035 TA = 71
33548
MA = 71
16670
Ha = 223
671 n
mi
Hp = 212
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7660343
39 X = 2407150
11
Y = -20887827
98 feet Y = -6340095
70 meter
Z = -849609
33 Z = -247443
80
XDOT = 14295
832059 XDOT = 4365
882643
YDOT = 6008
737372 feet/sec YDOT = 1880
238279 meter/sec
ZDOT = -19801
013894 ZDOT = -6014
161449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22239184
76 X = 6778503
52
Y = 697199
57 feet Y = 212506
43 meter
Z = -797889
88 Z = -243196
84
XDOT = -1107
661362 XDOT = -337
615183
YDOT = 13960
291376 feet/sec YDOT = 4255
096811 meter/sec
ZDOT = -19708
249322 ZDOT = -6007
074393
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 17009
53174972
00016717 00000-0 10270-3 0 9002
2 25544 51
6428 109
2258 0007065 66
9496 293
2401 15
54030195 37074
Satellite: ISS
Catalog Number: 25544
Epoch time: 17009
53174972 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 109
2258 deg
Eccentricity:
0007065
Arg of perigee: 66
9496 deg
Mean anomaly: 293
2401 deg
Mean motion: 15
54030195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3707
Checksum: 310
Coasting Arc #2 (Orbit 3722)
---------------------------------------
Vector Time (GMT): 2017/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2910134
21 A = 6788104
10 meter
Y = 5824392
13 meter E =
0021150
Z = 1884848
08 I = 52
01964
XDOT = -3660
589581 Wp = 67
56547
YDOT = -3673
329309 meter/sec RA = 103
48631 deg
ZDOT = 5656
626099 TA = 313
09220
MA = 313
26899
Ha = 223
737 n
mi
Hp = 212
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9547684
42 X = -2984203
40
Y = 19108898
06 feet Y = 5791434
73 meter
Z = 6183884
76 Z = 1870532
24
XDOT = -12009
808336 XDOT = -3646
718396
YDOT = -12051
605344 feet/sec YDOT = -3714
187442 meter/sec
ZDOT = 18558
484576 ZDOT = 5638
877521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21206423
42 X = -6463717
86
Y = -2717085
62 feet Y = -828167
70 meter
Z = 6119946
48 Z = 1865359
69
XDOT = 7153
873896 XDOT = 2180
500764
YDOT = -13890
217097 feet/sec YDOT = -4233
738171 meter/sec
ZDOT = 18481
152095 ZDOT = 5633
055159
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 17010
56064190
00016717 00000-0 10270-3 0 9018
2 25544 51
6436 104
0983 0007200 69
4885 290
7040 15
54044827 37238
Satellite: ISS
Catalog Number: 25544
Epoch time: 17010
56064190 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 104
0983 deg
Eccentricity:
0007200
Arg of perigee: 69
4885 deg
Mean anomaly: 290
7040 deg
Mean motion: 15
54044827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3723
Checksum: 290
Coasting Arc #3 (Orbit 3737)
---------------------------------------
Vector Time (GMT): 2017/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3391867
61 A = 6784813
57 meter
Y = -4814810
84 meter E =
0011716
Z = -3380324
61 I = 52
01435
XDOT = 2898
903907 Wp = 81
22279
YDOT = 5321
254080 meter/sec RA = 98
53592 deg
ZDOT = -4682
681338 TA = 137
94374
MA = 137
85375
Ha = 223
716 n
mi
Hp = 212
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11128174
59 X = 3461875
78
Y = -15796623
49 feet Y = -4776488
95 meter
Z = -11090303
84 Z = -3363678
53
XDOT = 9510
839589 XDOT = 2861
930763
YDOT = 17458
182676 feet/sec YDOT = 5353
465272 meter/sec
ZDOT = -15363
127750 ZDOT = -4668
688814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18704597
66 X = 5701161
37
Y = 5014358
27 feet Y = 1528376
40 meter
Z = -11016290
67 Z = -3357765
40
XDOT = -12665
185590 XDOT = -3860
348568
YDOT = 13712
436380 feet/sec YDOT = 4179
550609 meter/sec
ZDOT = -15302
594740 ZDOT = -4664
230877
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 17011
52522496
00016717 00000-0 10270-3 0 9024
2 25544 51
6427 99
2915 0007115 73
5955 286
5980 15
54039102 37389
Satellite: ISS
Catalog Number: 25544
Epoch time: 17011
52522496 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 99
2915 deg
Eccentricity:
0007115
Arg of perigee: 73
5955 deg
Mean anomaly: 286
5980 deg
Mean motion: 15
54039102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3738
Checksum: 317
Coasting Arc #4 (Orbit 3753)
---------------------------------------
Vector Time (GMT): 2017/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3727466
21 A = 6780995
41 meter
Y = 3440027
41 meter E =
0015443
Z = 4488149
82 I = 52
00665
XDOT = -2145
934634 Wp = 96
08687
YDOT = -6605
311157 meter/sec RA = 93
57533 deg
ZDOT = 3269
330086 TA = 321
14453
MA = 321
25545
Ha = 223
757 n
mi
Hp = 212
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12229219
86 X = -3787457
36
Y = 11286179
18 feet Y = 3398008
59 meter
Z = 14724900
98 Z = 4469897
78
XDOT = -7040
467960 XDOT = -2087
793418
YDOT = -21670
968363 feet/sec YDOT = -6628
983619 meter/sec
ZDOT = 10726
148576 ZDOT = 3259
046635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14995236
74 X = -4570548
16
Y = -7378928
61 feet Y = -2249097
44 meter
Z = 14644065
53 Z = 4463511
17
XDOT = 17065
395982 XDOT = 5201
532695
YDOT = -13406
827661 feet/sec YDOT = -4086
401071 meter/sec
ZDOT = 10682
149892 ZDOT = 3255
919287
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 17012
55410618
00016717 00000-0 10270-3 0 9031
2 25544 51
6435 94
1634 0007078 76
6081 283
5860 15
54081685 37547
Satellite: ISS
Catalog Number: 25544
Epoch time: 17012
55410618 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 94
1634 deg
Eccentricity:
0007078
Arg of perigee: 76
6081 deg
Mean anomaly: 283
5860 deg
Mean motion: 15
54081685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3754
Checksum: 312
Coasting Arc #5 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2017/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4009293
64 A = 6778344
26 meter
Y = -1782306
10 meter E =
0020853
Z = -5185212
59 I = 51
99772
XDOT = 1348
794324 Wp = 78
80041
YDOT = 7382
665666 meter/sec RA = 88
60607 deg
ZDOT = -1495
876896 TA = 176
84285
MA = 176
82967
Ha = 223
725 n
mi
Hp = 212
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13153850
52 X = 4054112
63
Y = -5847460
97 feet Y = -1737220
57 meter
Z = -17011852
32 Z = -5165628
28
XDOT = 4425
178229 XDOT = 1273
405314
YDOT = 24221
344048 feet/sec YDOT = 7397
327357 meter/sec
ZDOT = -4907
732600 ZDOT = -1489
507646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10444651
40 X = 3183529
75
Y = 10052759
74 feet Y = 3064081
17 meter
Z = -16925453
66 Z = -5158878
27
XDOT = -19985
219880 XDOT = -6091
495020
YDOT = 12552
623654 feet/sec YDOT = 3826
039690 meter/sec
ZDOT = -4881
082531 ZDOT = -1487
753956
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 17013
51867920
00016717 00000-0 10270-3 0 9041
2 25544 51
6428 89
3564 0007131 79
1012 281
0943 15
54042778 37690
Satellite: ISS
Catalog Number: 25544
Epoch time: 17013
51867920 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 89
3564 deg
Eccentricity:
0007131
Arg of perigee: 79
1012 deg
Mean anomaly: 281
0943 deg
Mean motion: 15
54042778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3769
Checksum: 315
Coasting Arc #6 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2017/013/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4179627
97 A = 6777680
91 meter
Y = 491356
81 meter E =
0021723
Z = -5331501
36 I = 51
99558
XDOT = -224
006815 Wp = 88
96294
YDOT = 7630
615721 meter/sec RA = 88
57234 deg
ZDOT = 529
878154 TA = 186
06542
MA = 186
09177
Ha = 223
728 n
mi
Hp = 212
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13712690
19 X = 4199720
21
Y = 1612063
04 feet Y = 538208
89 meter
Z = -17491802
38 Z = -5311149
56
XDOT = -734
930495 XDOT = -311
891520
YDOT = 25034
828482 feet/sec YDOT = 7627
619301 meter/sec
ZDOT = 1738
445388 ZDOT = 528
577027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4048567
23 X = 1234003
29
Y = 13317800
49 feet Y = 4059265
59 meter
Z = -17402444
18 Z = -5304264
99
XDOT = -22276
380859 XDOT = -6789
840886
YDOT = 9024
632127 feet/sec YDOT = 2750
707872 meter/sec
ZDOT = 1731
338420 ZDOT = 527
711950
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 17013
51867900
00016717 00000-0 10270-3 0 9050
2 25544 51
6428 89
3565 0007173 78
4663 281
7295 15
54050517 37698
Satellite: ISS
Catalog Number: 25544
Epoch time: 17013
51867900 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 89
3565 deg
Eccentricity:
0007173
Arg of perigee: 78
4663 deg
Mean anomaly: 281
7295 deg
Mean motion: 15
54050517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3769
Checksum: 332
Coasting Arc #7 (Orbit 3784)
---------------------------------------
Vector Time (GMT): 2017/014/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4101424
12 A = 6779304
24 meter
Y = -2254269
61 meter E =
0013762
Z = 4895155
61 I = 51
99971
XDOT = 1081
265773 Wp = 70
77662
YDOT = -7208
875918 meter/sec RA = 83
59940 deg
ZDOT = -2403
919172 TA = 42
69514
MA = 42
58828
Ha = 223
769 n
mi
Hp = 212
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13456115
87 X = -4099689
28
Y = -7395897
68 feet Y = -2300124
98 meter
Z = 16060221
83 Z = 4875236
68
XDOT = 3547
459884 XDOT = 1173
473758
YDOT = -23651
167711 feet/sec YDOT = -7196
268824 meter/sec
ZDOT = -7886
873924 ZDOT = -2398
443122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1094936
20 X = 333736
55
Y = -15406451
76 feet Y = -4695886
50 meter
Z = 15973084
89 Z = 4868596
28
XDOT = 21886
774283 XDOT = 6671
088801
YDOT = -6628
989701 feet/sec YDOT = -2020
516061 meter/sec
ZDOT = -7861
486482 ZDOT = -2396
181080
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 17014
54754988
00016717 00000-0 10270-3 0 9066
2 25544 51
6426 84
2283 0007142 82
1498 278
0465 15
54109525 37851
Satellite: ISS
Catalog Number: 25544
Epoch time: 17014
54754988 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 84
2283 deg
Eccentricity:
0007142
Arg of perigee: 82
1498 deg
Mean anomaly: 278
0465 deg
Mean motion: 15
54109525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3785
Checksum: 331
Coasting Arc #8 (Orbit 3799)
---------------------------------------
Vector Time (GMT): 2017/015/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3952567
82 A = 6782703
50 meter
Y = 3805382
03 meter E =
0013939
Z = -4000728
00 I = 52
00553
XDOT = -1944
514064 Wp = 96
17269
YDOT = 6225
918383 meter/sec RA = 78
63383 deg
ZDOT = 4011
332348 TA = 215
44301
MA = 215
53571
Ha = 223
750 n
mi
Hp = 212
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12967742
18 X = 3929154
52
Y = 12484849
16 feet Y = 3849451
44 meter
Z = -13125748
04 Z = -3981584
82
XDOT = -6379
639319 XDOT = -2033
474104
YDOT = 20426
241413 feet/sec YDOT = 6203
676063 meter/sec
ZDOT = 13160
539200 ZDOT = 4001
670681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5640943
92 X = -1719359
71
Y = 17158002
75 feet Y = 5229759
24 meter
Z = -13042306
20 Z = -3975294
93
XDOT = -19968
349394 XDOT = -6086
352895
YDOT = 3379
283022 feet/sec YDOT = 1030
005465 meter/sec
ZDOT = 13116
927355 ZDOT = 3998
039458
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 17015
51211420
00016717 00000-0 10270-3 0 9074
2 25544 51
6417 79
4210 0007375 86
2694 273
9301 15
54106947 38004
Satellite: ISS
Catalog Number: 25544
Epoch time: 17015
51211420 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 79
4210 deg
Eccentricity:
0007375
Arg of perigee: 86
2694 deg
Mean anomaly: 273
9301 deg
Mean motion: 15
54106947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3800
Checksum: 292
Coasting Arc #9 (Orbit 3807)
---------------------------------------
Vector Time (GMT): 2017/015/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3701974
10 A = 6785243
55 meter
Y = -4709204
57 meter E =
0020241
Z = 3169432
35 I = 52
01256
XDOT = 2602
320244 Wp = 90
86120
YDOT = -5336
087348 meter/sec RA = 76
23468 deg
ZDOT = -4862
487574 TA = 52
74056
MA = 52
55612
Ha = 223
826 n
mi
Hp = 212
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12145584
33 X = -3664434
71
Y = -15450146
23 feet Y = -4750392
65 meter
Z = 10398400
11 Z = 3151540
78
XDOT = 8537
796077 XDOT = 2685
415519
YDOT = -17506
848256 feet/sec YDOT = -5306
521823 meter/sec
ZDOT = -15953
043222 ZDOT = -4849
644717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10230045
95 X = -3118118
01
Y = 16827945
84 feet Y = 5129157
89 meter
Z = 10320627
92 Z = 3145727
39
XDOT = -18194
404304 XDOT = -5545
654432
YDOT = -1258
395145 feet/sec YDOT = -383
558840 meter/sec
ZDOT = -15895
609374 ZDOT = -4844
981737
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 17016
02654638
00016717 00000-0 10270-3 0 9084
2 25544 51
6436 76
8589 0007396 84
9276 275
2721 15
54090600 38086
Satellite: ISS
Catalog Number: 25544
Epoch time: 17016
02654638 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 76
8589 deg
Eccentricity:
0007396
Arg of perigee: 84
9276 deg
Mean anomaly: 275
2721 deg
Mean motion: 15
54090600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3808
Checksum: 334
Coasting Arc #10 (Orbit 3822)
---------------------------------------
Vector Time (GMT): 2017/016/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3311276
81 A = 6788212
82 meter
Y = 5680222
31 meter E =
0013695
Z = -1681948
78 I = 52
01401
XDOT = -3472
908438 Wp = 61
98637
YDOT = 3710
961447 meter/sec RA = 71
28308 deg
ZDOT = 5737
114281 TA = 279
68639
MA = 279
84106
Ha = 223
735 n
mi
Hp = 212
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10863769
06 X = 3255682
96
Y = 18635899
97 feet Y = 5716940
38 meter
Z = -5518204
67 Z = -1665998
94
XDOT = -11394
056555 XDOT = -3542
014944
YDOT = 12175
070365 feet/sec YDOT = 3671
738703 meter/sec
ZDOT = 18822
553414 ZDOT = 5720
076327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13384827
35 X = 4079695
37
Y = -16938770
69 feet Y = -5162937
31 meter
Z = -5449153
41 Z = -1660901
96
XDOT = 14299
906152 XDOT = 4358
611395
YDOT = 5313
392419 feet/sec YDOT = 1619
522009 meter/sec
ZDOT = 18746
975760 ZDOT = 5714
078212
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 17016
99110030
00016717 00000-0 10270-3 0 9094
2 25544 51
6435 72
0504 0007317 88
0117 272
1874 15
54107818 38234
Satellite: ISS
Catalog Number: 25544
Epoch time: 17016
99110030 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 72
0504 deg
Eccentricity:
0007317
Arg of perigee: 88
0117 deg
Mean anomaly: 272
1874 deg
Mean motion: 15
54107818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 292
Coasting Arc #11 (Orbit 3838)
---------------------------------------
Vector Time (GMT): 2017/017/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2692703
83 A = 6789522
26 meter
Y = -6226143
67 meter E =
0018141
Z = -41566
77 I = 52
00595
XDOT = 4342
839902 Wp = 119
08722
YDOT = -1851
149941 meter/sec RA = 66
33808 deg
ZDOT = -6043
481762 TA = 61
35828
MA = 61
17596
Ha = 223
792 n
mi
Hp = 212
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8834330
14 X = -2622679
45
Y = -20426980
54 feet Y = -6255863
77 meter
Z = -136373
92 Z = -54476
79
XDOT = 14248
162407 XDOT = 4392
573108
YDOT = -6073
326579 feet/sec YDOT = -1802
307380 meter/sec
ZDOT = -19827
696068 ZDOT = -6022
265015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15534120
53 X = -4734799
94
Y = 15936742
90 feet Y = 4857519
24 meter
Z = -191952
91 Z = -58507
25
XDOT = -9923
162426 XDOT = -3024
579907
YDOT = -9854
264778 feet/sec YDOT = -3003
579904 meter/sec
ZDOT = -19734
094941 ZDOT = -6014
952138
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 17018
01995538
00016717 00000-0 10270-3 0 9105
2 25544 51
6428 66
9221 0007342 93
2086 266
9907 15
54061653 38396
Satellite: ISS
Catalog Number: 25544
Epoch time: 17018
01995538 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 66
9221 deg
Eccentricity:
0007342
Arg of perigee: 93
2086 deg
Mean anomaly: 266
9907 deg
Mean motion: 15
54061653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3839
Checksum: 325
Coasting Arc #12 (Orbit 3854)
---------------------------------------
Vector Time (GMT): 2017/018/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1913091
26 A = 6788106
86 meter
Y = 6279332
04 meter E =
0020425
Z = 1698011
09 I = 51
98813
XDOT = -5103
774341 Wp = 74
61940
YDOT = -7
919090 meter/sec RA = 61
39113 deg
ZDOT = 5727
668887 TA = 303
91374
MA = 304
10780
Ha = 223
626 n
mi
Hp = 212
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6276546
14 X = 1834483
94
Y = 20601483
06 feet Y = 6300286
01 meter
Z = 5570902
51 Z = 1707113
23
XDOT = -16744
666474 XDOT = -5131
128426
YDOT = -25
981265 feet/sec YDOT = -65
145833 meter/sec
ZDOT = 18791
564591 ZDOT = 5702
810116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16445435
41 X = 5012568
71
Y = -13889915
15 feet Y = -4233646
14 meter
Z = 5609723
90 Z = 1709843
84
XDOT = 5645
336827 XDOT = 1720
698665
YDOT = 14297
463034 feet/sec YDOT = 4357
866733 meter/sec
ZDOT = 18682
305607 ZDOT = 5694
366749
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 17019
04880249
00016717 00000-0 10270-3 0 9112
2 25544 51
6430 61
7934 0007161 95
5839 264
6131 15
54124750 38553
Satellite: ISS
Catalog Number: 25544
Epoch time: 17019
04880249 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 61
7934 deg
Eccentricity:
0007161
Arg of perigee: 95
5839 deg
Mean anomaly: 264
6131 deg
Mean motion: 15
54124750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3855
Checksum: 309
Coasting Arc #13 (Orbit 3869)
---------------------------------------
Vector Time (GMT): 2017/019/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -869819
35 A = 6784928
86 meter
Y = -5900363
81 meter E =
0011724
Z = -3242968
53 I = 51
96072
XDOT = 5694
933556 Wp = 98
20915
YDOT = 1789
905361 meter/sec RA = 56
43666 deg
ZDOT = -4800
523143 TA = 119
12971
MA = 119
01231
Ha = 223
630 n
mi
Hp = 212
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2853738
03 X = -788022
68
Y = -19358149
00 feet Y = -5909633
37 meter
Z = -10639660
53 Z = -3246995
15
XDOT = 18684
165209 XDOT = 5697
813533
YDOT = 5872
392917 feet/sec YDOT = 1853
606050 meter/sec
ZDOT = -15749
747845 ZDOT = -4772
852125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16494600
62 X = -5027554
27
Y = 10509849
61 feet Y = 3203402
16 meter
Z = -10656234
86 Z = -3248020
38
XDOT = -1620
063579 XDOT = -493
795379
YDOT = -18334
168321 feet/sec YDOT = -5588
254504 meter/sec
ZDOT = -15628
470365 ZDOT = -4763
557767
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 17020
01334319
00016717 00000-0 10270-3 0 9124
2 25544 51
6426 56
9846 0007118 98
9052 261
2906 15
54103701 38705
Satellite: ISS
Catalog Number: 25544
Epoch time: 17020
01334319 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 56
9846 deg
Eccentricity:
0007118
Arg of perigee: 98
9052 deg
Mean anomaly: 261
2906 deg
Mean motion: 15
54103701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3870
Checksum: 293
Coasting Arc #14 (Orbit 3885)
---------------------------------------
Vector Time (GMT): 2017/020/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -311009
78 A = 6781207
19 meter
Y = 5141569
42 meter E =
0016645
Z = 4399354
49 I = 51
92877
XDOT = -6036
031355 Wp = 105
83327
YDOT = -3294
527776 meter/sec RA = 51
47205 deg
ZDOT = 3408
526810 TA = 309
75164
MA = 309
89817
Ha = 223
725 n
mi
Hp = 212
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1020373
28 X = -389850
78
Y = 16868666
06 feet Y = 5137650
62 meter
Z = 14433577
74 Z = 4397652
28
XDOT = -19803
252478 XDOT = -6015
299329
YDOT = -10808
818163 feet/sec YDOT = -3361
910860 meter/sec
ZDOT = 11182
830740 ZDOT = 3379
256153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15727502
62 X = 4793742
80
Y = -6203476
32 feet Y = -1890819
58 meter
Z = 14425108
86 Z = 4396773
18
XDOT = -1727
706905 XDOT = -526
605065
YDOT = 21441
172916 feet/sec YDOT = 6535
269505 meter/sec
ZDOT = 11054
817497 ZDOT = 3369
508373
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 17021
04218280
00016717 00000-0 10270-3 0 9137
2 25544 51
6419 51
8563 0007295 101
7475 258
4496 15
54096887 38860
Satellite: ISS
Catalog Number: 25544
Epoch time: 17021
04218280 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 51
8563 deg
Eccentricity:
0007295
Arg of perigee: 101
7475 deg
Mean anomaly: 258
4496 deg
Mean motion: 15
54096887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3886
Checksum: 331
Coasting Arc #15 (Orbit 3900)
---------------------------------------
Vector Time (GMT): 2017/021/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1662227
79 A = 6778178
89 meter
Y = -4109552
00 meter E =
0020123
Z = -5145154
28 I = 51
89728
XDOT = 5999
617672 Wp = 87
31294
YDOT = 4463
204595 meter/sec RA = 46
49552 deg
ZDOT = -1631
169298 TA = 166
99870
MA = 166
94674
Ha = 223
562 n
mi
Hp = 212
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5453503
26 X = 1733050
79
Y = -13482782
14 feet Y = -4090567
74 meter
Z = -16880427
44 Z = -5136907
82
XDOT = 19683
785013 XDOT = 5957
186430
YDOT = 14643
059695 feet/sec YDOT = 4530
059147 meter/sec
ZDOT = -5351
605307 ZDOT = -1602
128182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14553537
55 X = -4435918
25
Y = 984759
64 feet Y = 300154
74 meter
Z = -16843388
49 Z = -5133864
81
XDOT = 4466
231315 XDOT = 1361
307305
YDOT = -23102
770943 feet/sec YDOT = -7041
724583 meter/sec
ZDOT = -5224
835177 ZDOT = -1592
529762
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 17022
00671321
00016717 00000-0 10270-3 0 9144
2 25544 51
6412 47
0476 0007133 106
3567 253
8370 15
54135175 39019
Satellite: ISS
Catalog Number: 25544
Epoch time: 17022
00671321 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 47
0476 deg
Eccentricity:
0007133
Arg of perigee: 106
3567 deg
Mean anomaly: 253
8370 deg
Mean motion: 15
54135175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3901
Checksum: 277
Coasting Arc #16 (Orbit 3916)
---------------------------------------
Vector Time (GMT): 2017/022/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3015449
74 A = 6777391
35 meter
Y = 2907277
47 meter E =
0009410
Z = 5319983
86 I = 51
87205
XDOT = -5587
047915 Wp = 100
61084
YDOT = -5255
502589 meter/sec RA = 41
51267 deg
ZDOT = -296
034022 TA = 352
19195
MA = 352
20659
Ha = 223
695 n
mi
Hp = 212
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9893207
80 X = -3073577
21
Y = 9538311
91 feet Y = 2873231
51 meter
Z = 17454015
29 Z = 5305194
77
XDOT = -18330
209694 XDOT = -5526
426313
YDOT = -17242
462563 feet/sec YDOT = -5317
641757 meter/sec
ZDOT = -971
240231 ZDOT = -323
026864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13064882
84 X = 3982176
29
Y = 4521968
51 feet Y = 1378296
00 meter
Z = 17388451
39 Z = 5299999
98
XDOT = -6598
393405 XDOT = -2011
190310
YDOT = 23235
259614 feet/sec YDOT = 7082
107130 meter/sec
ZDOT = -1088
845087 ZDOT = -331
879982
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 17023
03554204
00016717 00000-0 10270-3 0 9159
2 25544 51
6417 41
9188 0007195 110
1085 250
0847 15
54122997 39176
Satellite: ISS
Catalog Number: 25544
Epoch time: 17023
03554204 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 41
9188 deg
Eccentricity:
0007195
Arg of perigee: 110
1085 deg
Mean anomaly: 250
0847 deg
Mean motion: 15
54122997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3917
Checksum: 299
Coasting Arc #17 (Orbit 3931)
---------------------------------------
Vector Time (GMT): 2017/023/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4316168
07 A = 6778942
94 meter
Y = -1664422
32 meter E =
0019545
Z = -4973335
49 I = 51
85051
XDOT = 4699
155389 Wp = 108
66334
YDOT = 5627
310142 meter/sec RA = 36
52825 deg
ZDOT = 2195
905186 TA = 182
73043
MA = 182
74111
Ha = 223
549 n
mi
Hp = 212
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14160656
40 X = 4358617
06
Y = -5460703
14 feet Y = -1615918
49 meter
Z = -16316717
49 Z = -4952266
06
XDOT = 15417
176474 XDOT = 4625
213588
YDOT = 18462
303616 feet/sec YDOT = 5679
445748 meter/sec
ZDOT = 7204
413339 ZDOT = 2218
552603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11566182
36 X = -3525372
38
Y = -9979512
50 feet Y = -3041755
41 meter
Z = -16223794
06 Z = -4945012
43
XDOT = 8256
734823 XDOT = 2516
652774
YDOT = -21436
565083 feet/sec YDOT = -6533
865037 meter/sec
ZDOT = 7302
839639 ZDOT = 2225
905522
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 17024
00006343
00016717 00000-0 10270-3 0 9164
2 25544 51
6397 37
1096 0007291 113
7566 246
4352 15
54149157 39322
Satellite: ISS
Catalog Number: 25544
Epoch time: 17024
00006343 = yrday
fracday
Element set: 916
Inclination: 51
6397 deg
RA of node: 37
1096 deg
Eccentricity:
0007291
Arg of perigee: 113
7566 deg
Mean anomaly: 246
4352 deg
Mean motion: 15
54149157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3932
Checksum: 300
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