[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 11th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 ET - UTC (sec) : 67 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
105/14:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 218
0
000/00:00:00
000 0
0 0
0 213
5
Coasting Arc #1 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2015/100/12:00:43
975
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 356843
11 A = 6780769
91 meter
Y = 5950324
44 meter E =
0011463
Z = 3228122
17 I = 51
97101
XDOT = -5519
740712 Wp = 113
89125
YDOT = -2287
113060 meter/sec RA = 61
50990 deg
ZDOT = 4807
985562 TA = 283
30456
MA = 283
43237
Ha = 219
087 n
mi
Hp = 213
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1170745
11 X = 274597
51
Y = 19522061
81 feet Y = 5953855
23 meter
Z = 10590952
01 Z = 3229655
53
XDOT = -18109
385537 XDOT = -5517
111014
YDOT = -7503
651772 feet/sec YDOT = -2348
823409 meter/sec
ZDOT = 15774
230846 ZDOT = 4781
178044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7002533
28 X = 2134372
14
Y = 18257327
63 feet Y = 5564833
46 meter
Z = 10596429
65 Z = 3229791
76
XDOT = -18298
076663 XDOT = -5577
253767
YDOT = -2104
791462 feet/sec YDOT = -641
540438 meter/sec
ZDOT = 15659
675687 ZDOT = 4773
069150
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 15100
55807289
00016717 00000-0 10270-3 0 9008
2 25544 51
6440 61
9006 0005844 203
3727 156
7162 15
55551283 17511
Satellite: ISS
Catalog Number: 25544
Epoch time: 15100
55807289 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 61
9006 deg
Eccentricity:
0005844
Arg of perigee: 203
3727 deg
Mean anomaly: 156
7162 deg
Mean motion: 15
55551283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 293
Coasting Arc #2 (Orbit 1765)
---------------------------------------
Vector Time (GMT): 2015/101/12:00:43
975
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1237743
47 A = 6775939
95 meter
Y = -4757287
60 meter E =
0007522
Z = -4669288
88 I = 51
93934
XDOT = 5608
856727 Wp = 101
28744
YDOT = 4327
545477 meter/sec RA = 56
53216 deg
ZDOT = -2927
713547 TA = 139
72217
MA = 139
66642
Ha = 218
946 n
mi
Hp = 213
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4060838
17 X = 1313530
37
Y = -15607898
96 feet Y = -4743022
88 meter
Z = -15319189
24 Z = -4663091
76
XDOT = 18401
760914 XDOT = 5574
270029
YDOT = 14197
983847 feet/sec YDOT = 4390
073811 meter/sec
ZDOT = -9605
359407 ZDOT = -2900
550951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1075799
83 X = -327903
79
Y = -16117702
19 feet Y = -4912675
63 meter
Z = -15291723
45 Z = -4660917
31
XDOT = 20868
726357 XDOT = 6360
787794
YDOT = 7593
548069 feet/sec YDOT = 2314
513451 meter/sec
ZDOT = -9489
663701 ZDOT = -2892
449496
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 15101
52172696
00016717 00000-0 10270-3 0 9014
2 25544 51
6443 57
0860 0005671 207
1097 152
9761 15
55563208 17667
Satellite: ISS
Catalog Number: 25544
Epoch time: 15101
52172696 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 57
0860 deg
Eccentricity:
0005671
Arg of perigee: 207
1097 deg
Mean anomaly: 152
9761 deg
Mean motion: 15
55563208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1766
Checksum: 305
Coasting Arc #3 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2015/102/12:00:43
975
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2865372
01 A = 6773101
64 meter
Y = 3081545
07 meter E =
0005941
Z = 5308240
70 I = 51
91248
XDOT = -5093
291668 Wp = 183
96993
YDOT = -5708
366045 meter/sec RA = 51
54054 deg
ZDOT = 558
744085 TA = 260
68628
MA = 260
75346
Ha = 218
737 n
mi
Hp = 213
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9400826
81 X = -2925403
13
Y = 10110055
99 feet Y = 3049167
32 meter
Z = 17415487
85 Z = 5294175
22
XDOT = -16710
274500 XDOT = -5031
794995
YDOT = -18728
235057 feet/sec YDOT = -5764
978674 meter/sec
ZDOT = 1833
149886 ZDOT = 534
151563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5541406
32 X = -1689020
65
Y = 12727893
57 feet Y = 3879461
96 meter
Z = 17354582
54 Z = 5289676
76
XDOT = -21132
110963 XDOT = -6441
067422
YDOT = -11583
307856 feet/sec YDOT = -3530
592235 meter/sec
ZDOT = 1728
741517 ZDOT = 526
920414
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 15102
54959536
00016717 00000-0 10270-3 0 9024
2 25544 51
6447 51
9516 0005734 212
0490 148
0316 15
55619565 17822
Satellite: ISS
Catalog Number: 25544
Epoch time: 15102
54959536 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 51
9516 deg
Eccentricity:
0005734
Arg of perigee: 212
0490 deg
Mean anomaly: 148
0316 deg
Mean motion: 15
55619565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1782
Checksum: 310
Coasting Arc #4 (Orbit 1796)
---------------------------------------
Vector Time (GMT): 2015/103/12:00:43
975
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4372843
87 A = 6774224
17 meter
Y = -1148546
43 meter E =
0012098
Z = -5054936
38 I = 51
89590
XDOT = 3894
041193 Wp = 130
42108
YDOT = 6310
262068 meter/sec RA = 46
54228 deg
ZDOT = 1930
214158 TA = 158
27599
MA = 158
22463
Ha = 218
533 n
mi
Hp = 213
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14346600
62 X = 4409917
22
Y = -3768196
96 feet Y = -1099439
56 meter
Z = -16584436
94 Z = -5033603
78
XDOT = 12775
725698 XDOT = 3813
812656
YDOT = 20702
959542 feet/sec YDOT = 6353
359355 meter/sec
ZDOT = 6332
723616 ZDOT = 1948
935302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12185262
56 X = 3714068
03
Y = -8635809
13 feet Y = -2632194
62 meter
Z = -16492725
16 Z = -5026982
63
XDOT = 18603
097554 XDOT = 5670
224134
YDOT = 13974
873579 feet/sec YDOT = 4259
541467 meter/sec
ZDOT = 6411
829260 ZDOT = 1954
325558
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 15103
51319693
00016717 00000-0 10270-3 0 9037
2 25544 51
6447 47
1364 0005717 215
5318 144
5455 15
55640406 17977
Satellite: ISS
Catalog Number: 25544
Epoch time: 15103
51319693 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 47
1364 deg
Eccentricity:
0005717
Arg of perigee: 215
5318 deg
Mean anomaly: 144
5455 deg
Mean motion: 15
55640406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1797
Checksum: 308
Coasting Arc #5 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2015/104/12:00:43
975
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5477476
71 A = 6778397
24 meter
Y = -754011
52 meter E =
0007974
Z = 3912542
31 I = 51
88847
XDOT = -2084
681565 Wp = 109
69050
YDOT = -6143
949439 meter/sec RA = 41
55395 deg
ZDOT = -4098
401781 TA = 23
07468
MA = 23
03889
Ha = 218
445 n
mi
Hp = 213
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17970724
11 X = -5487643
79
Y = -2473791
06 feet Y = -815320
71 meter
Z = 12836424
90 Z = 3885909
10
XDOT = -6839
506447 XDOT = -1995
914972
YDOT = -20157
314431 feet/sec YDOT = -6166
765782 meter/sec
ZDOT = -13446
200069 ZDOT = -4108
312586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17687449
89 X = -5391134
73
Y = 4374529
62 feet Y = 1333356
63 meter
Z = 12722341
71 Z = 3877769
75
XDOT = -13407
518658 XDOT = -4086
611687
YDOT = -14944
909740 feet/sec YDOT = -4555
208489 meter/sec
ZDOT = -13487
543227 ZDOT = -4111
003176
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 15104
54101064
00016717 00000-0 10270-3 0 9043
2 25544 51
6453 42
0012 0005738 219
3507 140
7230 15
55690086 18130
Satellite: ISS
Catalog Number: 25544
Epoch time: 15104
54101064 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 42
0012 deg
Eccentricity:
0005738
Arg of perigee: 219
3507 deg
Mean anomaly: 140
7230 deg
Mean motion: 15
55690086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1813
Checksum: 267
Coasting Arc #6 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2015/105/12:00:43
975
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5988556
92 A = 6782924
95 meter
Y = 2404958
44 meter E =
0000899
Z = -2086970
44 I = 51
87956
XDOT = -188
246047 Wp = 20
59410
YDOT = 5284
383393 meter/sec RA = 36
57992 deg
ZDOT = 5550
928337 TA = 316
38168
MA = 316
38879
Ha = 218
096 n
mi
Hp = 213
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19647496
46 X = 5971356
79
Y = 7890283
59 feet Y = 2471830
00 meter
Z = -6847015
87 Z = -2057921
08
XDOT = -617
605142 XDOT = -274
287760
YDOT = 17337
215857 feet/sec YDOT = 5281
797818 meter/sec
ZDOT = 18211
707142 ZDOT = 5549
804308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21210090
01 X = 6464835
44
Y = -311670
44 feet Y = -94997
15 meter
Z = -6722890
88 Z = -2049137
14
XDOT = 5985
535485 XDOT = 1824
391216
YDOT = 14734
410698 feet/sec YDOT = 4491
048381 meter/sec
ZDOT = 18205
882152 ZDOT = 5549
152880
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 15105
50455992
00016717 00000-0 10270-3 0 9053
2 25544 51
6453 37
1861 0005754 223
6236 136
4463 15
55718154 18285
Satellite: ISS
Catalog Number: 25544
Epoch time: 15105
50455992 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 37
1861 deg
Eccentricity:
0005754
Arg of perigee: 223
6236 deg
Mean anomaly: 136
4463 deg
Mean motion: 15
55718154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 312
Coasting Arc #7 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2015/105/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -114298
76 A = 6774744
44 meter
Y = -4765846
16 meter E =
0006999
Z = -4819416
98 I = 51
85208
XDOT = 6793
716689 Wp = 94
11127
YDOT = 2441
183000 meter/sec RA = 36
06032 deg
ZDOT = -2578
878817 TA = 150
58176
MA = 150
54234
Ha = 218
039 n
mi
Hp = 213
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -374995
92 X = -37586
38
Y = -15635978
22 feet Y = -4766695
93 meter
Z = -15811735
50 Z = -4819785
37
XDOT = 22289
096749 XDOT = 6778
441174
YDOT = 8009
130576 feet/sec YDOT = 2517
069088 meter/sec
ZDOT = -8460
888506 ZDOT = -2545
913451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14070137
00 X = -4288577
76
Y = -6828936
79 feet Y = -2081459
94 meter
Z = -15812409
16 Z = -4819622
31
XDOT = 16751
147133 XDOT = 5105
749646
YDOT = -15276
824834 feet/sec YDOT = -4656
376209 meter/sec
ZDOT = -8319
977180 ZDOT = -2535
929045
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 15105
63303044
00016717 00000-0 10270-3 0 9068
2 25544 51
6474 36
5447 0005755 224
3233 135
7460 15
55754376 18305
Satellite: ISS
Catalog Number: 25544
Epoch time: 15105
63303044 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 36
5447 deg
Eccentricity:
0005755
Arg of perigee: 224
3233 deg
Mean anomaly: 135
7460 deg
Mean motion: 15
55754376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 297
Coasting Arc #8 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2015/106/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2059355
36 A = 6772494
76 meter
Y = 3646980
52 meter E =
0004503
Z = 5323858
07 I = 51
81903
XDOT = -6611
099189 Wp = 205
15750
YDOT = -3887
855844 meter/sec RA = 31
05850 deg
ZDOT = 102
055332 TA = 243
84947
MA = 243
89579
Ha = 217
870 n
mi
Hp = 213
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6756415
23 X = -2125845
27
Y = 11965159
20 feet Y = 3623580
31 meter
Z = 17466725
94 Z = 5313692
11
XDOT = -21689
957969 XDOT = -6567
628659
YDOT = -12755
432559 feet/sec YDOT = -3961
542408 meter/sec
ZDOT = 334
827206 ZDOT = 70
045617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7763141
36 X = 2366205
49
Y = 11405837
42 feet Y = 3476499
25 meter
Z = 17422433
97 Z = 5310357
88
XDOT = -20119
934689 XDOT = -6132
556093
YDOT = 13371
478006 feet/sec YDOT = 4075
626496 meter/sec
ZDOT = 198
302319 ZDOT = 60
442547
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 15106
66078522
00016717 00000-0 10270-3 0 9073
2 25544 51
6478 31
4088 0005864 228
0097 132
0557 15
55796524 18469
Satellite: ISS
Catalog Number: 25544
Epoch time: 15106
66078522 = yrday
fracday
Element set: 907
Inclination: 51
6478 deg
RA of node: 31
4088 deg
Eccentricity:
0005864
Arg of perigee: 228
0097 deg
Mean anomaly: 132
0557 deg
Mean motion: 15
55796524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 326
Coasting Arc #9 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2015/107/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4130444
73 A = 6774393
20 meter
Y = -2256269
64 meter E =
0009688
Z = -4880847
44 I = 51
79796
XDOT = 5473
727517 Wp = 137
10005
YDOT = 4790
361788 meter/sec RA = 26
05346 deg
ZDOT = 2413
623627 TA = 156
54810
MA = 156
50389
Ha = 217
623 n
mi
Hp = 213
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13551327
86 X = 4179077
56
Y = -7402459
46 feet Y = -2209808
91 meter
Z = -16013279
02 Z = -4860663
89
XDOT = 17958
423611 XDOT = 5408
029084
YDOT = 15716
410065 feet/sec YDOT = 4851
205507 meter/sec
ZDOT = 7918
712688 ZDOT = 2440
054211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -960724
10 X = -292828
71
Y = -15501291
91 feet Y = -4724793
77 meter
Z = -15926297
62 Z = -4854335
52
XDOT = 20669
706279 XDOT = 6300
126474
YDOT = -9546
290139 feet/sec YDOT = -2909
709234 meter/sec
ZDOT = 8031
125999 ZDOT = 2447
887204
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 15107
62428072
00016717 00000-0 10270-3 0 9080
2 25544 51
6478 26
5935 0005903 232
5557 127
5060 15
55828936 18618
Satellite: ISS
Catalog Number: 25544
Epoch time: 15107
62428072 = yrday
fracday
Element set: 908
Inclination: 51
6478 deg
RA of node: 26
5935 deg
Eccentricity:
0005903
Arg of perigee: 232
5557 deg
Mean anomaly: 127
5060 deg
Mean motion: 15
55828936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 322
Coasting Arc #10 (Orbit 1876)
---------------------------------------
Vector Time (GMT): 2015/108/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5724819
76 A = 6779015
27 meter
Y = 779605
62 meter E =
0007844
Z = 3536921
54 I = 51
78530
XDOT = -3486
148120 Wp = 110
77276
YDOT = -5142
293683 meter/sec RA = 21
06038 deg
ZDOT = -4503
844062 TA = 27
58207
MA = 27
54048
Ha = 217
448 n
mi
Hp = 213
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18782217
05 X = -5750293
35
Y = 2557761
22 feet Y = 715444
84 meter
Z = 11604073
30 Z = 3509049
04
XDOT = -11437
493833 XDOT = -3406
508296
YDOT = -16871
042267 feet/sec YDOT = -5180
833196 meter/sec
ZDOT = -14776
391280 ZDOT = -4520
585471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5312188
59 X = -1619155
08
Y = 18271761
21 feet Y = 5569232
82 meter
Z = 11484412
54 Z = 3500448
94
XDOT = -18691
346308 XDOT = -5697
122355
YDOT = 3908
885384 feet/sec YDOT = 1191
428265 meter/sec
ZDOT = -14847
177396 ZDOT = -4525
419670
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 15108
65198210
00016717 00000-0 10270-3 0 9093
2 25544 51
6480 21
4580 0005857 237
1242 122
9348 15
55885667 18770
Satellite: ISS
Catalog Number: 25544
Epoch time: 15108
65198210 = yrday
fracday
Element set: 909
Inclination: 51
6480 deg
RA of node: 21
4580 deg
Eccentricity:
0005857
Arg of perigee: 237
1242 deg
Mean anomaly: 122
9348 deg
Mean motion: 15
55885667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1877
Checksum: 327
Coasting Arc #11 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2015/109/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6573095
80 A = 6783234
36 meter
Y = 631359
52 meter E =
0003675
Z = -1541162
40 I = 51
76904
XDOT = 873
027078 Wp = 356
67129
YDOT = 4979
285534 meter/sec RA = 16
08151 deg
ZDOT = 5766
210216 TA = 346
51027
MA = 346
52010
Ha = 217
133 n
mi
Hp = 213
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21565274
92 X = 6573033
79
Y = 2071389
49 feet Y = 704863
71 meter
Z = -5056307
07 Z = -1509231
16
XDOT = 2864
262066 XDOT = 789
272011
YDOT = 16336
238627 feet/sec YDOT = 4988
580403 meter/sec
ZDOT = 18918
012521 ZDOT = 5770
247501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10329382
43 X = 3148395
76
Y = -19079310
90 feet Y = -5815373
96 meter
Z = -4919525
61 Z = -1499471
40
XDOT = 14723
215532 XDOT = 4487
636094
YDOT = 3091
394286 feet/sec YDOT = 942
256979 meter/sec
ZDOT = 18934
350008 ZDOT = 5771
189883
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 15109
61542745
00016717 00000-0 10270-3 0 9108
2 25544 51
6474 16
6421 0005992 241
0757 118
9796 15
55896957 18921
Satellite: ISS
Catalog Number: 25544
Epoch time: 15109
61542745 = yrday
fracday
Element set: 910
Inclination: 51
6474 deg
RA of node: 16
6421 deg
Eccentricity:
0005992
Arg of perigee: 241
0757 deg
Mean anomaly: 118
9796 deg
Mean motion: 15
55896957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 343
Coasting Arc #12 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2015/110/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6464817
46 A = 6783902
14 meter
Y = -1883650
03 meter E =
0010739
Z = -763925
95 I = 51
74029
XDOT = 1985
219079 Wp = 173
95730
YDOT = -4402
403411 meter/sec RA = 11
11155 deg
ZDOT = -5962
970473 TA = 14
29667
MA = 14
26631
Ha = 217
009 n
mi
Hp = 213
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21210031
03 X = -6439562
62
Y = -6179954
17 feet Y = -1955802
67 meter
Z = -2506318
74 Z = -795269
92
XDOT = 6513
185955 XDOT = 2063
266666
YDOT = -14443
580744 feet/sec YDOT = -4379
767292 meter/sec
ZDOT = -19563
551420 ZDOT = -5953
136700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13659708
98 X = -4163479
30
Y = 17343007
07 feet Y = 5286148
56 meter
Z = -2640329
46 Z = -804772
42
XDOT = -9648
968410 XDOT = -2941
005571
YDOT = -10563
014330 feet/sec YDOT = -3219
606768 meter/sec
ZDOT = -19520
525376 ZDOT = -5949
856135
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 15110
64307674
00016717 00000-0 10270-3 0 9114
2 25544 51
6470 11
5062 0006155 243
4328 116
6196 15
55902942 19083
Satellite: ISS
Catalog Number: 25544
Epoch time: 15110
64307674 = yrday
fracday
Element set: 911
Inclination: 51
6470 deg
RA of node: 11
5062 deg
Eccentricity:
0006155
Arg of perigee: 243
4328 deg
Mean anomaly: 116
6196 deg
Mean motion: 15
55902942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 291
Coasting Arc #13 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2015/111/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5384185
05 A = 6780233
34 meter
Y = 2899811
46 meter E =
0007349
Z = 2922196
71 I = 51
69669
XDOT = -4618
197851 Wp = 93
16991
YDOT = 3497
398498 meter/sec RA = 6
13199 deg
ZDOT = 5027
181707 TA = 300
15687
MA = 300
22967
Ha = 216
635 n
mi
Hp = 213
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17664649
11 X = 5337163
34
Y = 9513817
12 feet Y = 2959758
10 meter
Z = 9587259
53 Z = 2948238
16
XDOT = -15151
567754 XDOT = -4681
383915
YDOT = 11474
404522 feet/sec YDOT = 3445
401643 meter/sec
ZDOT = 16493
378304 ZDOT = 5004
593462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15187172
97 X = 4629050
32
Y = -13029207
85 feet Y = -3971302
55 meter
Z = 9698330
26 Z = 2956051
06
XDOT = 4302
032692 XDOT = 1311
259565
YDOT = 17246
136679 feet/sec YDOT = 5256
622460 meter/sec
ZDOT = 16395
847258 ZDOT = 4997
454244
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 15111
67069712
00016717 00000-0 10270-3 0 9127
2 25544 51
6461 6
3682 0006179 249
2186 110
8306 15
55982652 19248
Satellite: ISS
Catalog Number: 25544
Epoch time: 15111
67069712 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 6
3682 deg
Eccentricity:
0006179
Arg of perigee: 249
2186 deg
Mean anomaly: 110
8306 deg
Mean motion: 15
55982652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1924
Checksum: 309
Coasting Arc #14 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2015/112/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3447957
75 A = 6775008
46 meter
Y = -3662897
60 meter E =
0003791
Z = -4542036
61 I = 51
64658
XDOT = 6599
856379 Wp = 65
16084
YDOT = -2340
859963 meter/sec RA = 1
13364 deg
ZDOT = -3122
808123 TA = 173
55223
MA = 173
54735
Ha = 216
380 n
mi
Hp = 213
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11312197
36 X = -3384678
30
Y = -12017380
56 feet Y = -3701101
17 meter
Z = -14901694
92 Z = -4558632
57
XDOT = 21653
072108 XDOT = 6640
711541
YDOT = -7679
986754 feet/sec YDOT = -2266
827675 meter/sec
ZDOT = -10245
433473 ZDOT = -3090
647613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15130089
81 X = -4611651
37
Y = 6431164
63 feet Y = 1960218
98 meter
Z = -14972116
09 Z = -4563500
98
XDOT = 677
765102 XDOT = 206
582803
YDOT = -21931
662600 feet/sec YDOT = -6684
770760 meter/sec
ZDOT = -10107
095160 ZDOT = -3080
642605
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 15112
63406777
00016717 00000-0 10270-3 0 9131
2 25544 51
6447 1
5519 0006208 252
4133 107
6343 15
56013165 19395
Satellite: ISS
Catalog Number: 25544
Epoch time: 15112
63406777 = yrday
fracday
Element set: 913
Inclination: 51
6447 deg
RA of node: 1
5519 deg
Eccentricity:
0006208
Arg of perigee: 252
4133 deg
Mean anomaly: 107
6343 deg
Mean motion: 15
56013165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 290
Coasting Arc #15 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2015/113/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 975779
43 A = 6771934
60 meter
Y = 4128697
24 meter E =
0004280
Z = 5281455
81 I = 51
60480
XDOT = -7578
666191 Wp = 231
23098
YDOT = 1002
430212 meter/sec RA = 356
11611 deg
ZDOT = 614
280727 TA = 212
89004
MA = 212
91668
Ha = 216
193 n
mi
Hp = 213
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3201376
09 X = 903883
25
Y = 13545594
63 feet Y = 4139207
13 meter
Z = 17327610
91 Z = 5286021
31
XDOT = -24864
390389 XDOT = -7592
296313
YDOT = 3288
813032 feet/sec YDOT = 917
604414 meter/sec
ZDOT = 2015
356716 ZDOT = 577
431559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13815241
20 X = 4210885
52
Y = 1490251
18 feet Y = 454228
56 meter
Z = 17346362
86 Z = 5287171
40
XDOT = -4885
272376 XDOT = -1489
031020
YDOT = 23583
779411 feet/sec YDOT = 7188
335965 meter/sec
ZDOT = 1857
187097 ZDOT = 566
070627
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 15113
66163824
00016717 00000-0 10270-3 0 9149
2 25544 51
6450 356
4142 0006164 255
8605 104
1864 15
56026328 19558
Satellite: ISS
Catalog Number: 25544
Epoch time: 15113
66163824 = yrday
fracday
Element set: 914
Inclination: 51
6450 deg
RA of node: 356
4142 deg
Eccentricity:
0006164
Arg of perigee: 255
8605 deg
Mean anomaly: 104
1864 deg
Mean motion: 15
56026328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1955
Checksum: 301
Coasting Arc #16 (Orbit 1969)
---------------------------------------
Vector Time (GMT): 2015/114/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1649048
40 A = 6773039
36 meter
Y = -4271386
64 meter E =
0007590
Z = -4997675
94 I = 51
57629
XDOT = 7377
524123 Wp = 126
18825
YDOT = 472
271623 meter/sec RA = 351
09109 deg
ZDOT = 2028
437598 TA = 163
56399
MA = 163
53937
Ha = 215
964 n
mi
Hp = 213
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5410263
77 X = 1720966
51
Y = -14013735
68 feet Y = -4252543
89 meter
Z = -16396574
60 Z = -4989490
35
XDOT = 24204
475469 XDOT = 7361
841294
YDOT = 1549
447581 feet/sec YDOT = 554
684274 meter/sec
ZDOT = 6654
978997 ZDOT = 2064
238329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11621035
03 X = -3542091
48
Y = -9580423
71 feet Y = -2920113
15 meter
Z = -16360636
51 Z = -4986722
01
XDOT = 8251
899894 XDOT = 2515
179088
YDOT = -21648
818623 feet/sec YDOT = -6598
559916 meter/sec
ZDOT = 6808
356702 ZDOT = 2075
187123
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 15114
62495950
00016717 00000-0 10270-3 0 9155
2 25544 51
6437 351
5964 0006230 259
0651 100
9801 15
56101711 19704
Satellite: ISS
Catalog Number: 25544
Epoch time: 15114
62495950 = yrday
fracday
Element set: 915
Inclination: 51
6437 deg
RA of node: 351
5964 deg
Eccentricity:
0006230
Arg of perigee: 259
0651 deg
Mean anomaly: 100
9801 deg
Mean motion: 15
56101711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 293
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