[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 10th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12055 58 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
254/21:27:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
1
000/00:00:00
000 0
0 0
0 213
3
257/01:13:13
330 7
0 7
1 7
2
N/A -1
4 -0
7 219
3
000/00:02:26
659 -0
6 -0
2 217
2
Coasting Arc #1 (Orbit 116)
---------------------------------------
Vector Time (GMT): 2015/252/13:36:25
568
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6455141
23 A = 6785436
76 meter
Y = 1153003
95 meter E =
0007630
Z = -1731677
08 I = 51
80287
XDOT = 615
054625 Wp = 31
04064
YDOT = 5091
814334 meter/sec RA = 22
12024 deg
ZDOT = 5700
558766 TA = 310
00021
MA = 310
06716
Ha = 219
325 n
mi
Hp = 213
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21178284
86 X = 6450180
04
Y = 3782821
36 feet Y = 1225161
69 meter
Z = -5681355
24 Z = -1700331
79
XDOT = 2017
895750 XDOT = 530
380161
YDOT = 16705
427605 feet/sec YDOT = 5098
219355 meter/sec
ZDOT = 18702
620625 ZDOT = 5703
340420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21541841
61 X = -6565953
32
Y = 542143
23 feet Y = 165245
26 meter
Z = -5546388
49 Z = -1690539
21
XDOT = -5165
876443 XDOT = -1574
559140
YDOT = -14417
741636 feet/sec YDOT = -4394
527651 meter/sec
ZDOT = 18713
623035 ZDOT = 5703
912301
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 15252
57027502
00016717 00000-0 10270-3 0 9000
2 25544 51
6452 22
6947 0000879 300
0160 60
0906 15
55049286 1174
Satellite: ISS
Catalog Number: 25544
Epoch time: 15252
57027502 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 22
6947 deg
Eccentricity:
0000879
Arg of perigee: 300
0160 deg
Mean anomaly: 60
0906 deg
Mean motion: 15
55049286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 117
Checksum: 278
Coasting Arc #2 (Orbit 132)
---------------------------------------
Vector Time (GMT): 2015/253/13:36:25
568
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6400239
74 A = 6786491
65 meter
Y = -2221505
18 meter E =
0010647
Z = -298107
08 I = 51
77689
XDOT = 1802
184217 Wp = 138
26906
YDOT = -4402
441831 meter/sec RA = 17
15576 deg
ZDOT = -6016
121721 TA = 44
93868
MA = 44
85255
Ha = 219
216 n
mi
Hp = 213
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20998161
86 X = -6373474
57
Y = -7288402
81 feet Y = -2292927
25 meter
Z = -978041
59 Z = -329132
59
XDOT = 5912
677876 XDOT = 1880
503178
YDOT = -14443
706795 feet/sec YDOT = -4381
851355 meter/sec
ZDOT = -19737
932156 ZDOT = -6007
176466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22073061
89 X = 6727869
26
Y = 2558296
73 feet Y = 779768
84 meter
Z = -1111413
14 Z = -338758
72
XDOT = -2572
483634 XDOT = -784
093012
YDOT = 13802
202920 feet/sec YDOT = 4206
911450 meter/sec
ZDOT = -19698
493518 ZDOT = -6004
100824
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 15253
59847700
00016717 00000-0 10270-3 0 9014
2 25544 51
6451 17
5619 0000812 298
2392 61
8679 15
55088073 1335
Satellite: ISS
Catalog Number: 25544
Epoch time: 15253
59847700 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 17
5619 deg
Eccentricity:
0000812
Arg of perigee: 298
2392 deg
Mean anomaly: 61
8679 deg
Mean motion: 15
55088073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 133
Checksum: 313
Coasting Arc #3 (Orbit 148)
---------------------------------------
Vector Time (GMT): 2015/254/13:36:25
568
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5622720
90 A = 6784210
52 meter
Y = 3036487
53 meter E =
0013441
Z = 2258489
42 I = 51
73965
XDOT = -4096
805171 Wp = 68
81000
YDOT = 3514
574363 meter/sec RA = 12
18674 deg
ZDOT = 5452
754260 TA = 316
30163
MA = 316
40796
Ha = 219
181 n
mi
Hp = 213
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18447247
05 X = 5577377
48
Y = 9962229
43 feet Y = 3099111
24 meter
Z = 7409742
19 Z = 2285692
73
XDOT = -13440
961847 XDOT = -4162
288689
YDOT = 11530
755784 feet/sec YDOT = 3468
395711 meter/sec
ZDOT = 17889
613713 ZDOT = 5432
693497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20219057
92 X = -6162768
85
Y = -5384540
03 feet Y = -1641207
80 meter
Z = 7526462
90 Z = 2294065
89
XDOT = 10090
005688 XDOT = 3075
433734
YDOT = -12907
676139 feet/sec YDOT = -3934
259687 meter/sec
ZDOT = 17802
416447 ZDOT = 5426
176533
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 15254
62666336
00016717 00000-0 10270-3 0 9024
2 25544 51
6457 12
4286 0000849 312
5983 47
5098 15
55122432 1492
Satellite: ISS
Catalog Number: 25544
Epoch time: 15254
62666336 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 12
4286 deg
Eccentricity:
0000849
Arg of perigee: 312
5983 deg
Mean anomaly: 47
5098 deg
Mean motion: 15
55122432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 149
Checksum: 310
Coasting Arc #4 (Orbit 153)
---------------------------------------
Vector Time (GMT): 2015/254/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 927453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3101098
82 A = 6778076
28 meter
Y = 4112555
07 meter E =
0008382
Z = 4400223
56 I = 51
70571
XDOT = -6733
973640 Wp = 104
97401
YDOT = 1456
631609 meter/sec RA = 10
56308 deg
ZDOT = 3376
946206 TA = 310
88018
MA = 310
95277
Ha = 219
141 n
mi
Hp = 213
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10174208
72 X = 3033506
30
Y = 13492634
73 feet Y = 4146856
22 meter
Z = 14436429
02 Z = 4415123
27
XDOT = -22093
089371 XDOT = -6766
165357
YDOT = 4778
975095 feet/sec YDOT = 1381
148310 meter/sec
ZDOT = 11079
219837 ZDOT = 3344
155800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3429483
49 X = -1045306
57
Y = 16491462
41 feet Y = 5026597
74 meter
Z = 14499879
60 Z = 4419563
30
XDOT = -17060
386265 XDOT = -5200
005733
YDOT = -13185
948341 feet/sec YDOT = -4019
077054 meter/sec
ZDOT = 10937
531647 ZDOT = 3333
759646
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 15254
94796840
00016717 00000-0 10270-3 0 9034
2 25544 51
6422 10
8266 0001176 326
7712 33
3368 15
55143911 1549
Satellite: ISS
Catalog Number: 25544
Epoch time: 15254
94796840 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 10
8266 deg
Eccentricity:
0001176
Arg of perigee: 326
7712 deg
Mean anomaly: 33
3368 deg
Mean motion: 15
55143911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 154
Checksum: 297
Coasting Arc #5 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2015/255/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 927453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -993591
15 A = 6774906
03 meter
Y = -4233895
87 meter E =
0013955
Z = -5207140
74 I = 51
66373
XDOT = 7554
789986 Wp = 75
46186
YDOT = -248
712839 meter/sec RA = 5
56013 deg
ZDOT = -1238
685088 TA = 182
63660
MA = 182
64396
Ha = 219
310 n
mi
Hp = 213
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3259813
50 X = -920878
67
Y = -13890734
47 feet Y = -4244601
00 meter
Z = -17083795
08 Z = -5211790
20
XDOT = 24786
056385 XDOT = 7563
026697
YDOT = -815
987003 feet/sec YDOT = -164
184315 meter/sec
ZDOT = -4063
927455 ZDOT = -1201
965577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8119340
05 X = 2474774
85
Y = -11704615
32 feet Y = -3567566
75 meter
Z = -17103018
45 Z = -5213000
02
XDOT = 16502
467602 XDOT = 5029
952125
YDOT = 17157
479355 feet/sec YDOT = 5229
599707 meter/sec
ZDOT = -3905
544005 ZDOT = -1190
409813
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 15255
91187672
00016717 00000-0 10270-3 0 9040
2 25544 51
6426 6
0135 0001227 339
4107 20
6996 15
55131875 1699
Satellite: ISS
Catalog Number: 25544
Epoch time: 15255
91187672 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 6
0135 deg
Eccentricity:
0001227
Arg of perigee: 339
4107 deg
Mean anomaly: 20
6996 deg
Mean motion: 15
55131875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 169
Checksum: 303
Coasting Arc #6 (Orbit 184)
---------------------------------------
Vector Time (GMT): 2015/256/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 927453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1263302
48 A = 6774776
83 meter
Y = 4123164
29 meter E =
0004451
Z = 5223188
30 I = 51
63195
XDOT = -7537
804855 Wp = 38
87952
YDOT = -930
918156 meter/sec RA =
55031 deg
ZDOT = -1084
370779 TA = 61
52844
MA = 61
48362
Ha = 219
340 n
mi
Hp = 213
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4144693
18 X = -1334687
04
Y = 13527441
91 feet Y = 4108638
82 meter
Z = 17136444
55 Z = 5216877
47
XDOT = -24730
330889 XDOT = -7521
567422
YDOT = -3054
193425 feet/sec YDOT = -1015
120220 meter/sec
ZDOT = -3557
646913 ZDOT = -1120
948299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12746296
19 X = -3885071
08
Y = 6217829
22 feet Y = 1895194
35 meter
Z = 17108431
59 Z = 5214649
95
XDOT = -14323
788375 XDOT = -4365
890697
YDOT = -19105
646115 feet/sec YDOT = -5823
400936 meter/sec
ZDOT = -3715
174799 ZDOT = -1132
385279
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 15256
94002985
00016717 00000-0 10270-3 0 9058
2 25544 51
6429
8807 0001358 342
4494 17
6612 15
55157401 1850
Satellite: ISS
Catalog Number: 25544
Epoch time: 15256
94002985 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node:
8807 deg
Eccentricity:
0001358
Arg of perigee: 342
4494 deg
Mean anomaly: 17
6612 deg
Mean motion: 15
55157401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 185
Checksum: 302
Coasting Arc #7 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2015/257/01:14:26
659
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -580025
95 A = 6778182
15 meter
Y = -4194529
77 meter E =
0008899
Z = -5300456
72 I = 51
62858
XDOT = 7633
681548 Wp = 81
17002
YDOT = -424
855206 meter/sec RA = 359
77382 deg
ZDOT = -498
519898 TA = 184
06578
MA = 184
07302
Ha = 219
260 n
mi
Hp = 217
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1902972
27 X = -507331
01
Y = -13761580
59 feet Y = -4200610
29 meter
Z = -17389949
88 Z = -5303097
21
XDOT = 25044
886968 XDOT = 7640
286648
YDOT = -1393
881908 feet/sec YDOT = -339
453489 meter/sec
ZDOT = -1635
563970 ZDOT = -461
420934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4264424
04 X = -1299796
45
Y = -13207930
52 feet Y = -4025777
22 meter
Z = -17400517
80 Z = -5303677
82
XDOT = 23420
620921 XDOT = 7138
605257
YDOT = -5615
203034 feet/sec YDOT = -1711
513885 meter/sec
ZDOT = -1475
525954 ZDOT = -449
740311
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 15257
06855116
00016717 00000-0 10270-3 0 9065
2 25544 51
6456
2380 0005956 273
8604 86
1867 15
53866209 1874
Satellite: ISS
Catalog Number: 25544
Epoch time: 15257
06855116 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node:
2380 deg
Eccentricity:
0005956
Arg of perigee: 273
8604 deg
Mean anomaly: 86
1867 deg
Mean motion: 15
53866209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 323
Coasting Arc #8 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2015/258/01:14:26
659
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1130202
76 A = 6778628
95 meter
Y = 4226669
55 meter E =
0004192
Z = 5180411
37 I = 51
59836
XDOT = -7539
161507 Wp = 324
16309
YDOT = -374
401875 meter/sec RA = 354
77508 deg
ZDOT = -1336
558510 TA = 138
70748
MA = 138
67577
Ha = 219
331 n
mi
Hp = 217
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3708014
32 X = -1202546
95
Y = 13867026
09 feet Y = 4213627
12 meter
Z = 16996100
31 Z = 5174744
74
XDOT = -24734
781846 XDOT = -7527
922014
YDOT = -1228
352609 feet/sec YDOT = -458
647092 meter/sec
ZDOT = -4385
034480 ZDOT = -1373
154991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -984592
15 X = -300103
69
Y = 14350335
06 feet Y = 4373982
13 meter
Z = 16970847
66 Z = 5172714
37
XDOT = -23411
343709 XDOT = -7135
777563
YDOT = 3776
797534 feet/sec YDOT = 1151
167888 meter/sec
ZDOT = -4542
736769 ZDOT = -1384
626167
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 15258
09756064
00016717 00000-0 10270-3 0 9072
2 25544 51
6454 355
1106 0006129 278
3976 81
6481 15
53907266 2035
Satellite: ISS
Catalog Number: 25544
Epoch time: 15258
09756064 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 355
1106 deg
Eccentricity:
0006129
Arg of perigee: 278
3976 deg
Mean anomaly: 81
6481 deg
Mean motion: 15
53907266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 203
Checksum: 321
Coasting Arc #9 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2015/259/01:14:26
659
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2745985
66 A = 6781192
88 meter
Y = -4185668
42 meter E =
0003975
Z = -4578304
97 I = 51
57558
XDOT = 6926
414540 Wp = 121
54499
YDOT = 1208
791968 meter/sec RA = 349
77761 deg
ZDOT = 3049
133522 TA = 178
97600
MA = 178
97518
Ha = 219
538 n
mi
Hp = 217
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9009139
29 X = 2814826
53
Y = -13732507
93 feet Y = -4154576
72 meter
Z = -15020685
60 Z = -4564797
66
XDOT = 22724
457153 XDOT = 6897
571126
YDOT = 3965
852913 feet/sec YDOT = 1286
086846 meter/sec
ZDOT = 10003
718905 ZDOT = 3082
710630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5930743
45 X = 1807690
60
Y = -15373447
18 feet Y = -4685826
70 meter
Z = -14961643
12 Z = -4560308
82
XDOT = 21861
458313 XDOT = 6663
372494
YDOT = -1442
972932 feet/sec YDOT = -439
818150 meter/sec
ZDOT = 10148
229765 ZDOT = 3093
180432
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 15259
06224585
00016717 00000-0 10270-3 0 9089
2 25544 51
6458 350
3033 0006091 282
6035 77
4437 15
53896311 2185
Satellite: ISS
Catalog Number: 25544
Epoch time: 15259
06224585 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 350
3033 deg
Eccentricity:
0006091
Arg of perigee: 282
6035 deg
Mean anomaly: 77
4437 deg
Mean motion: 15
53896311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 218
Checksum: 308
Coasting Arc #10 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2015/260/01:14:26
659
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4155913
64 A = 6784743
45 meter
Y = 4034263
21 meter E =
0006791
Z = 3530073
62 I = 51
55615
XDOT = -5853
687920 Wp = 71
32120
YDOT = -2097
722045 meter/sec RA = 344
78654 deg
ZDOT = -4484
934622 TA = 67
03622
MA = 66
96458
Ha = 219
730 n
mi
Hp = 217
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13634887
26 X = -4217864
77
Y = 13235771
69 feet Y = 3987443
11 meter
Z = 11581606
36 Z = 3509733
86
XDOT = -19205
012861 XDOT = -5808
009329
YDOT = -6882
290174 feet/sec YDOT = -2162
927015 meter/sec
ZDOT = -14714
352436 ZDOT = -4513
259684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10258648
42 X = -3126836
04
Y = 16059175
83 feet Y = 4894836
79 meter
Z = 11493146
36 Z = 3503111
01
XDOT = -19015
905912 XDOT = -5796
048122
YDOT = -1507
847143 feet/sec YDOT = -459
591809 meter/sec
ZDOT = -14836
040488 ZDOT = -4522
025141
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 15260
09122894
00016717 00000-0 10270-3 0 9095
2 25544 51
6454 345
1758 0006033 287
2747 72
7745 15
53916952 2346
Satellite: ISS
Catalog Number: 25544
Epoch time: 15260
09122894 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 345
1758 deg
Eccentricity:
0006033
Arg of perigee: 287
2747 deg
Mean anomaly: 72
7745 deg
Mean motion: 15
53916952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 234
Checksum: 325
Coasting Arc #11 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2015/261/01:14:26
659
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5231853
58 A = 6787971
51 meter
Y = -3744196
73 meter E =
0007180
Z = -2149501
17 I = 51
53697
XDOT = 4417
747258 Wp = 347
24563
YDOT = 3022
576728 meter/sec RA = 339
80161 deg
ZDOT = 5491
079326 TA = 348
88184
MA = 348
89770
Ha = 219
923 n
mi
Hp = 217
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17164873
95 X = 5283774
82
Y = -12284110
01 feet Y = -3685400
64 meter
Z = -7052169
21 Z = -2123959
08
XDOT = 14493
921449 XDOT = 4356
945892
YDOT = 9916
590316 feet/sec YDOT = 3071
639570 meter/sec
ZDOT = 18015
352120 ZDOT = 5512
392033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13608686
79 X = 4147927
73
Y = -16182913
11 feet Y = -4932551
92 meter
Z = -6941348
15 Z = -2115722
92
XDOT = 15215
267633 XDOT = 4637
613575
YDOT = 5033
263637 feet/sec YDOT = 1534
138757 meter/sec
ZDOT = 18106
627694 ZDOT = 5518
900121
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 15261
05588649
00016717 00000-0 10270-3 0 9108
2 25544 51
6456 340
3677 0006178 291
1653 68
8839 15
53942014 2499
Satellite: ISS
Catalog Number: 25544
Epoch time: 15261
05588649 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 340
3677 deg
Eccentricity:
0006178
Arg of perigee: 291
1653 deg
Mean anomaly: 68
8839 deg
Mean motion: 15
53942014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 331
Coasting Arc #12 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2015/262/01:14:26
659
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5924878
24 A = 6789829
23 meter
Y = 3262680
82 meter E =
0007293
Z = 543524
23 I = 51
51323
XDOT = -2731
719440 Wp = 142
24623
YDOT = -3960
109924 meter/sec RA = 334
82260 deg
ZDOT = -5969
384905 TA = 31
88038
MA = 31
83626
Ha = 220
026 n
mi
Hp = 217
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19438576
90 X = -5963562
24
Y = 10704333
40 feet Y = 3196208
69 meter
Z = 1783215
97 Z = 514647
77
XDOT = -8962
334122 XDOT = -2658
236207
YDOT = -12992
486626 feet/sec YDOT = -3990
247558 meter/sec
ZDOT = -19584
596145 ZDOT = -5982
476288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15907602
92 X = -4848637
37
Y = 15486112
48 feet Y = 4720167
08 meter
Z = 1658123
67 Z = 505396
09
XDOT = -10841
915990 XDOT = -3304
615994
YDOT = -9020
170885 feet/sec YDOT = -2749
348086 meter/sec
ZDOT = -19640
251421 ZDOT = -5986
348633
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 15262
08484252
00016717 00000-0 10270-3 0 9118
2 25544 51
6453 335
2399 0006086 293
8940 66
1574 15
53918813 2651
Satellite: ISS
Catalog Number: 25544
Epoch time: 15262
08484252 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 335
2399 deg
Eccentricity:
0006086
Arg of perigee: 293
8940 deg
Mean anomaly: 66
1574 deg
Mean motion: 15
53918813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 323
Coasting Arc #13 (Orbit 280)
---------------------------------------
Vector Time (GMT): 2015/263/01:14:26
659
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6177405
52 A = 6789171
27 meter
Y = -2568558
46 meter E =
0012014
Z = 1108846
83 I = 51
48305
XDOT = 958
298772 Wp = 29
73830
YDOT = 4845
773223 meter/sec RA = 329
84204 deg
ZDOT = 5869
068162 TA = 342
32444
MA = 342
36620
Ha = 220
115 n
mi
Hp = 216
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20267078
49 X = 6200282
24
Y = -8427029
05 feet Y = -2499350
63 meter
Z = 3637948
92 Z = 1138911
49
XDOT = 3144
024844 XDOT = 875
530983
YDOT = 15898
206111 feet/sec YDOT = 4856
027303 meter/sec
ZDOT = 19255
472971 ZDOT = 5873
521948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17043190
27 X = 5194764
39
Y = -13796218
32 feet Y = -4205087
34 meter
Z = 3768021
60 Z = 1148492
98
XDOT = 6378
594333 XDOT = 1944
195553
YDOT = 13158
638150 feet/sec YDOT = 4010
752908 meter/sec
ZDOT = 19273
729280 ZDOT = 5874
632685
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 15263
11378136
00016717 00000-0 10270-3 0 9127
2 25544 51
6449 330
1107 0006295 299
2167 60
8356 15
53991769 2818
Satellite: ISS
Catalog Number: 25544
Epoch time: 15263
11378136 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 330
1107 deg
Eccentricity:
0006295
Arg of perigee: 299
2167 deg
Mean anomaly: 60
8356 deg
Mean motion: 15
53991769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 281
Checksum: 319
Coasting Arc #14 (Orbit 295)
---------------------------------------
Vector Time (GMT): 2015/264/01:14:26
659
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6021187
90 A = 6786662
33 meter
Y = 1637999
88 meter E =
0001488
Z = -2668355
18 I = 51
44708
XDOT = 775
109917 Wp = 296
34797
YDOT = -5594
404832 meter/sec RA = 324
85657 deg
ZDOT = -5180
342870 TA = 273
83526
MA = 273
85228
Ha = 220
358 n
mi
Hp = 216
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19754553
47 X = -6026094
96
Y = 5374015
36 feet Y = 1570639
34 meter
Z = -8754446
11 Z = -2697617
14
XDOT = 2543
011539 XDOT = 862
774602
YDOT = -18354
346561 feet/sec YDOT = -5585
247309 meter/sec
ZDOT = -16995
875559 ZDOT = -5176
364124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17194884
93 X = -5241000
93
Y = 11010392
85 feet Y = 3355967
74 meter
Z = -8880874
51 Z = -2706890
55
XDOT = -2148
099650 XDOT = -654
740773
YDOT = -17056
231603 feet/sec YDOT = -5198
739392 meter/sec
ZDOT = -16977
648190 ZDOT = -5174
787168
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 15264
07840108
00016717 00000-0 10270-3 0 9137
2 25544 51
6444 325
3032 0006351 302
2115 57
8421 15
53977424 2964
Satellite: ISS
Catalog Number: 25544
Epoch time: 15264
07840108 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 325
3032 deg
Eccentricity:
0006351
Arg of perigee: 302
2115 deg
Mean anomaly: 57
8421 deg
Mean motion: 15
53977424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 296
Checksum: 285
Coasting Arc #15 (Orbit 311)
---------------------------------------
Vector Time (GMT): 2015/265/01:14:26
659
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5481498
92 A = 6782953
90 meter
Y = -490045
92 meter E =
0005978
Z = 3958657
45 I = 51
40908
XDOT = -2331
820296 Wp = 71
62299
YDOT = 6125
355649 meter/sec RA = 319
85918 deg
ZDOT = 3984
001045 TA = 336
71585
MA = 336
74292
Ha = 220
451 n
mi
Hp = 216
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17983920
34 X = 5467341
61
Y = -1607762
19 feet Y = -428827
02 meter
Z = 12987721
30 Z = 3985251
23
XDOT = -7650
329055 XDOT = -2419
495037
YDOT = 20096
311185 feet/sec YDOT = 6098
789803 meter/sec
ZDOT = 13070
869569 ZDOT = 3972
460038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16483299
96 X = 5024109
83
Y = -7163409
92 feet Y = -2183407
34 meter
Z = 13102426
32 Z = 3993619
54
XDOT = -1531
695932 XDOT = -466
860920
YDOT = 20308
455630 feet/sec YDOT = 6190
017276 meter/sec
ZDOT = 13019
955654 ZDOT = 3968
482483
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 15265
10731525
00016717 00000-0 10270-3 0 9145
2 25544 51
6441 320
1737 0006368 308
3188 51
7391 15
53993557 3124
Satellite: ISS
Catalog Number: 25544
Epoch time: 15265
10731525 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 320
1737 deg
Eccentricity:
0006368
Arg of perigee: 308
3188 deg
Mean anomaly: 51
7391 deg
Mean motion: 15
53993557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 312
Checksum: 303
Coasting Arc #16 (Orbit 326)
---------------------------------------
Vector Time (GMT): 2015/266/01:14:26
659
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4659446
63 A = 6779457
16 meter
Y = -826314
48 meter E =
0010146
Z = -4863277
58 I = 51
37293
XDOT = 3609
840709 Wp = 40
30532
YDOT = -6324
318313 meter/sec RA = 314
85074 deg
ZDOT = -2379
185677 TA = 206
24478
MA = 206
29623
Ha = 220
607 n
mi
Hp = 216
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15286898
39 X = -4626236
30
Y = -2711005
51 feet Y = -878234
22 meter
Z = -15955635
09 Z = -4885831
52
XDOT = 11843
309413 XDOT = 3691
849672
YDOT = -20749
075831 feet/sec YDOT = -6283
492365 meter/sec
ZDOT = -7805
727287 ZDOT = -2361
450033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15225857
93 X = -4640841
50
Y = 2471015
44 feet Y = 753165
50 meter
Z = -16052676
96 Z = -4892855
94
XDOT = 4527
701152 XDOT = 1380
043311
YDOT = -22407
648485 feet/sec YDOT = -6829
851258 meter/sec
ZDOT = -7728
088442 ZDOT = -2355
521357
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 15266
07190741
00016717 00000-0 10270-3 0 9152
2 25544 51
6430 315
3655 0006409 310
8615 49
1982 15
54038797 3276
Satellite: ISS
Catalog Number: 25544
Epoch time: 15266
07190741 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 315
3655 deg
Eccentricity:
0006409
Arg of perigee: 310
8615 deg
Mean anomaly: 49
1982 deg
Mean motion: 15
54038797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 327
Checksum: 312
Coasting Arc #17 (Orbit 342)
---------------------------------------
Vector Time (GMT): 2015/267/01:14:26
659
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3621121
42 A = 6777697
28 meter
Y = 2243444
72 meter E =
0003963
Z = 5273178
79 I = 51
34543
XDOT = -4567
189464 Wp = 330
94935
YDOT = 6136
148347 meter/sec RA = 309
83334 deg
ZDOT = 529
293450 TA = 114
00010
MA = 113
95861
Ha = 220
710 n
mi
Hp = 216
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11880319
62 X = 3570150
47
Y = 7360382
93 feet Y = 2283654
02 meter
Z = 17300455
33 Z = 5290645
42
XDOT = -14984
217400 XDOT = -4638
037025
YDOT = 20131
720299 feet/sec YDOT = 6084
678947 meter/sec
ZDOT = 1736
527068 ZDOT = 506
934272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13594262
11 X = 4143531
09
Y = 2813853
66 feet Y = 857662
59 meter
Z = 17375305
79 Z = 5295993
20
XDOT = -6860
652773 XDOT = -2091
126965
YDOT = 23096
363473 feet/sec YDOT = 7039
771587 meter/sec
ZDOT = 1639
010733 ZDOT = 499
570471
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 15267
10079429
00016717 00000-0 10270-3 0 9167
2 25544 51
6432 310
2367 0006323 315
1430 44
9211 15
54036410 3436
Satellite: ISS
Catalog Number: 25544
Epoch time: 15267
10079429 = yrday
fracday
Element set: 916
Inclination: 51
6432 deg
RA of node: 310
2367 deg
Eccentricity:
0006323
Arg of perigee: 315
1430 deg
Mean anomaly: 44
9211 deg
Mean motion: 15
54036410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 343
Checksum: 267
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