[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 14th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
176/10:51:33
202 1
4 3
4 3
4
N/A 3
0 -0
0 227
1
000/00:01:06
403 0
6 -0
0 220
9
Coasting Arc #1 (Orbit 1075)
---------------------------------------
Vector Time (GMT): 2014/164/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4755132
09 A = 6790186
97 meter
Y = -1268034
07 meter E =
0014289
Z = -4691963
51 I = 51
95359
XDOT = -994
085607 Wp = 76
64234
YDOT = 7007
865393 meter/sec RA = 116
81306 deg
ZDOT = -2905
617838 TA = 164
54856
MA = 164
50489
Ha = 227
904 n
mi
Hp = 218
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15600827
08 X = 4791750
28
Y = -4160216
76 feet Y = -1214653
65 meter
Z = -15393581
06 Z = -4668774
89
XDOT = -3261
435717 XDOT = -1058
260650
YDOT = 22991
684360 feet/sec YDOT = 6996
390518 meter/sec
ZDOT = -9532
866921 ZDOT = -2910
601775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3976984
19 X = -1212184
78
Y = -15744891
80 feet Y = -4799043
02 meter
Z = -15295016
37 Z = -4661920
99
XDOT = 21803
525589 XDOT = 6645
714600
YDOT = 3761
280988 feet/sec YDOT = 1146
438445 meter/sec
ZDOT = -9555
185137 ZDOT = -2912
420430
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 14164
54470287
00016717 00000-0 10270-3 0 9000
2 25544 51
6456 117
6428 0004050 92
4786 267
6829 15
50692040 10769
Satellite: ISS
Catalog Number: 25544
Epoch time: 14164
54470287 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 117
6428 deg
Eccentricity:
0004050
Arg of perigee: 92
4786 deg
Mean anomaly: 267
6829 deg
Mean motion: 15
50692040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1076
Checksum: 313
Coasting Arc #2 (Orbit 1091)
---------------------------------------
Vector Time (GMT): 2014/165/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4555189
02 A = 6789052
87 meter
Y = 1002049
00 meter E =
0010441
Z = 4926458
23 I = 51
96425
XDOT = 939
945984 Wp = 112
79030
YDOT = -7243
250666 meter/sec RA = 111
87370 deg
ZDOT = 2334
530079 TA = 314
42748
MA = 314
51287
Ha = 227
901 n
mi
Hp = 218
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14944845
85 X = -4589986
73
Y = 3287562
32 feet Y = 950914
63 meter
Z = 16162920
70 Z = 4904245
41
XDOT = 3083
812282 XDOT = 1009
531416
YDOT = -23763
945753 feet/sec YDOT = -7232
350866 meter/sec
ZDOT = 7659
219419 ZDOT = 2339
264119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3371100
48 X = 1027511
43
Y = 15027794
88 feet Y = 4580471
88 meter
Z = 16068526
75 Z = 4897686
95
XDOT = -22683
642450 XDOT = -6913
974219
YDOT = -3151
703945 feet/sec YDOT = -960
639362 meter/sec
ZDOT = 7680
530056 ZDOT = 2341
025561
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 14165
57581440
00016717 00000-0 10270-3 0 9019
2 25544 51
6464 112
5303 0003896 97
8590 262
3003 15
50737883 10922
Satellite: ISS
Catalog Number: 25544
Epoch time: 14165
57581440 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 112
5303 deg
Eccentricity:
0003896
Arg of perigee: 97
8590 deg
Mean anomaly: 262
3003 deg
Mean motion: 15
50737883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1092
Checksum: 305
Coasting Arc #3 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2014/166/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4404023
66 A = 6788246
75 meter
Y = -671700
27 meter E =
0017091
Z = -5137069
47 I = 51
97261
XDOT = -859
069797 Wp = 82
31550
YDOT = 7407
233182 meter/sec RA = 106
93246 deg
ZDOT = -1707
660508 TA = 171
23718
MA = 171
20731
Ha = 227
810 n
mi
Hp = 218
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14448896
53 X = 4436161
55
Y = -2203741
05 feet Y = -622271
24 meter
Z = -16853902
46 Z = -5115597
48
XDOT = -2818
470463 XDOT = -933
540094
YDOT = 24301
946134 feet/sec YDOT = 7397
210361 meter/sec
ZDOT = -5602
560723 ZDOT = -1712
013583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2534476
92 X = -772508
57
Y = -14500673
82 feet Y = -4419805
38 meter
Z = -16762696
65 Z = -5109269
94
XDOT = 23300
872490 XDOT = 7102
105935
YDOT = 2416
663672 feet/sec YDOT = 736
599087 meter/sec
ZDOT = -5622
293644 ZDOT = -1713
675103
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 14166
54247259
00016717 00000-0 10270-3 0 9025
2 25544 51
6468 107
7359 0003997 99
4029 260
7574 15
50728581 11077
Satellite: ISS
Catalog Number: 25544
Epoch time: 14166
54247259 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 107
7359 deg
Eccentricity:
0003997
Arg of perigee: 99
4029 deg
Mean anomaly: 260
7574 deg
Mean motion: 15
50728581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 336
Coasting Arc #4 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2014/167/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4272431
50 A = 6787504
42 meter
Y = 325188
64 meter E =
0007500
Z = 5258651
76 I = 51
97899
XDOT = 748
650688 Wp = 113
62492
YDOT = -7555
830600 meter/sec RA = 101
99253 deg
ZDOT = 1071
359188 TA = 326
13542
MA = 326
18329
Ha = 227
808 n
mi
Hp = 218
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14017163
71 X = -4301294
95
Y = 1066891
88 feet Y = 277249
56 meter
Z = 17252794
48 Z = 5237826
97
XDOT = 2456
203045 XDOT = 827
881784
YDOT = -24789
470472 feet/sec YDOT = -7547
015828 meter/sec
ZDOT = 3514
957966 ZDOT = 1075
187545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1630513
94 X = 496980
65
Y = 14071366
04 feet Y = 4288952
37 meter
Z = 17164385
69 Z = 5231704
76
XDOT = -23840
372019 XDOT = -7266
545391
YDOT = -1563
100312 feet/sec YDOT = -476
432975 meter/sec
ZDOT = 3532
499159 ZDOT = 1076
705744
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 14167
57355945
00016717 00000-0 10270-3 0 9032
2 25544 51
6470 102
6230 0003836 104
4239 255
7338 15
50776418 11236
Satellite: ISS
Catalog Number: 25544
Epoch time: 14167
57355945 = yrday
fracday
Element set: 903
Inclination: 51
6470 deg
RA of node: 102
6230 deg
Eccentricity:
0003836
Arg of perigee: 104
4239 deg
Mean anomaly: 255
7338 deg
Mean motion: 15
50776418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 302
Coasting Arc #5 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2014/168/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4202594
15 A = 6787226
21 meter
Y = 62958
17 meter E =
0018529
Z = -5345179
43 I = 51
98384
XDOT = -624
383133 Wp = 90
98284
YDOT = 7613
115705 meter/sec RA = 97
05086 deg
ZDOT = -402
757375 TA = 175
19401
MA = 175
17620
Ha = 227
709 n
mi
Hp = 218
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13788038
55 X = 4227542
77
Y = 206555
66 feet Y = 110094
30 meter
Z = -17536677
92 Z = -5324703
35
XDOT = -2048
501093 XDOT = -707
511869
YDOT = 24977
413731 feet/sec YDOT = 7605
668692 meter/sec
ZDOT = -1321
382465 ZDOT = -405
991675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -588000
88 X = -179222
67
Y = -13886904
84 feet Y = -4232728
60 meter
Z = -17449810
13 Z = -5318702
13
XDOT = 24040
349742 XDOT = 7327
498601
YDOT = 655
112539 feet/sec YDOT = 199
678302 meter/sec
ZDOT = -1336
421707 ZDOT = -407
341336
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 14168
54019445
00016717 00000-0 10270-3 0 9043
2 25544 51
6473 97
8284 0003945 106
4254 253
7331 15
50764518 11388
Satellite: ISS
Catalog Number: 25544
Epoch time: 14168
54019445 = yrday
fracday
Element set: 904
Inclination: 51
6473 deg
RA of node: 97
8284 deg
Eccentricity:
0003945
Arg of perigee: 106
4254 deg
Mean anomaly: 253
7331 deg
Mean motion: 15
50764518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 315
Coasting Arc #6 (Orbit 1153)
---------------------------------------
Vector Time (GMT): 2014/169/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4159038
76 A = 6787032
58 meter
Y = -457642
48 meter E =
0006038
Z = 5338668
01 I = 51
98638
XDOT = 493
956547 Wp = 97
65179
YDOT = -7647
408181 meter/sec RA = 92
11016 deg
ZDOT = -271
261389 TA = 354
91859
MA = 354
92472
Ha = 227
703 n
mi
Hp = 218
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13645140
29 X = -4179545
60
Y = -1501451
70 feet Y = -504266
63 meter
Z = 17515315
00 Z = 5318414
23
XDOT = 1620
592347 XDOT = 580
752590
YDOT = -25089
921854 feet/sec YDOT = -7641
399114 meter/sec
ZDOT = -889
965187 ZDOT = -268
651653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -475155
47 X = -144827
39
Y = 13828187
40 feet Y = 4214831
52 meter
Z = 17429455
84 Z = 5312498
14
XDOT = -24133
128303 XDOT = -7355
777507
YDOT = 274
691584 feet/sec YDOT = 83
725995 meter/sec
ZDOT = -877
560346 ZDOT = -267
480393
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 14169
57125658
00016717 00000-0 10270-3 0 9052
2 25544 51
6470 92
7149 0003776 110
9096 249
2459 15
50813887 11548
Satellite: ISS
Catalog Number: 25544
Epoch time: 14169
57125658 = yrday
fracday
Element set: 905
Inclination: 51
6470 deg
RA of node: 92
7149 deg
Eccentricity:
0003776
Arg of perigee: 110
9096 deg
Mean anomaly: 249
2459 deg
Mean motion: 15
50813887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1154
Checksum: 334
Coasting Arc #7 (Orbit 1168)
---------------------------------------
Vector Time (GMT): 2014/170/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4182953
23 A = 6787363
13 meter
Y = 865975
56 meter E =
0018119
Z = -5290398
55 I = 51
98820
XDOT = -368
057664 Wp = 100
67123
YDOT = 7581
395781 meter/sec RA = 87
16847 deg
ZDOT = 949
473321 TA = 178
39577
MA = 178
38995
Ha = 227
585 n
mi
Hp = 218
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13723599
85 X = 4198657
83
Y = 2841127
18 feet Y = 912840
26 meter
Z = -17356950
63 Z = -5270040
17
XDOT = -1207
538267 XDOT = -457
419433
YDOT = 24873
345738 feet/sec YDOT = 7576
780199 meter/sec
ZDOT = 3115
069951 ZDOT = 947
468889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1564235
02 X = 476778
83
Y = -14033830
59 feet Y = -4277511
56 meter
Z = -17270717
98 Z = -5264114
84
XDOT = 23858
355318 XDOT = 7272
026701
YDOT = -1164
185888 feet/sec YDOT = -354
843859 meter/sec
ZDOT = 3105
233450 ZDOT = 946
475156
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 14170
53786817
00016717 00000-0 10270-3 0 9061
2 25544 51
6477 87
9201 0003856 113
4827 246
6729 15
50800487 11698
Satellite: ISS
Catalog Number: 25544
Epoch time: 14170
53786817 = yrday
fracday
Element set: 906
Inclination: 51
6477 deg
RA of node: 87
9201 deg
Eccentricity:
0003856
Arg of perigee: 113
4827 deg
Mean anomaly: 246
6729 deg
Mean motion: 15
50800487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1169
Checksum: 333
Coasting Arc #8 (Orbit 1184)
---------------------------------------
Vector Time (GMT): 2014/171/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4232958
68 A = 6787779
15 meter
Y = -1268720
68 meter E =
0007472
Z = 5146244
22 I = 51
98752
XDOT = 261
890354 Wp = 80
91786
YDOT = -7488
992306 meter/sec RA = 82
22761 deg
ZDOT = -1627
715374 TA = 24
72944
MA = 24
69364
Ha = 227
580 n
mi
Hp = 218
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13887659
70 X = -4243455
80
Y = -4162469
42 feet Y = -1316115
46 meter
Z = 16884003
35 Z = 5125655
46
XDOT = 859
220320 XDOT = 353
521441
YDOT = -24570
184730 feet/sec YDOT = -7485
551208 meter/sec
ZDOT = -5340
273536 ZDOT = -1626
221188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2618719
20 X = -798185
61
Y = 14362118
74 feet Y = 4377573
79 meter
Z = 16796864
82 Z = 5119684
40
XDOT = -23475
231674 XDOT = -7155
250614
YDOT = 1968
434444 feet/sec YDOT = 599
978819 meter/sec
ZDOT = -5332
604804 ZDOT = -1625
377944
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 14171
56890593
00016717 00000-0 10270-3 0 9073
2 25544 51
6475 82
8062 0003702 117
3513 242
8015 15
50850116 11858
Satellite: ISS
Catalog Number: 25544
Epoch time: 14171
56890593 = yrday
fracday
Element set: 907
Inclination: 51
6475 deg
RA of node: 82
8062 deg
Eccentricity:
0003702
Arg of perigee: 117
3513 deg
Mean anomaly: 242
8015 deg
Mean motion: 15
50850116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1185
Checksum: 295
Coasting Arc #9 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2014/172/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4347280
41 A = 6788676
56 meter
Y = 1655444
36 meter E =
0015788
Z = -4959061
26 I = 51
98611
XDOT = -179
987543 Wp = 109
77757
YDOT = 7300
655922 meter/sec RA = 77
28664 deg
ZDOT = 2280
044953 TA = 182
44514
MA = 182
45286
Ha = 227
435 n
mi
Hp = 218
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14262731
00 X = 4352535
39
Y = 5431247
89 feet Y = 1704088
28 meter
Z = -16269886
03 Z = -4937929
77
XDOT = -590
510313 XDOT = -272
687540
YDOT = 23952
283209 feet/sec YDOT = 7298
124658 meter/sec
ZDOT = 7480
462443 ZDOT = 2278
946109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3583472
83 X = 1092242
52
Y = -14932608
24 feet Y = -4551458
99 meter
Z = -16180515
27 Z = -4931821
05
XDOT = 22754
556192 XDOT = 6935
588727
YDOT = -2636
042363 feet/sec YDOT = -803
465712 meter/sec
ZDOT = 7474
489740 ZDOT = 2278
224473
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 14172
53549430
00016717 00000-0 10270-3 0 9083
2 25544 51
6484 78
0115 0003721 120
7366 239
4152 15
50837087 12003
Satellite: ISS
Catalog Number: 25544
Epoch time: 14172
53549430 = yrday
fracday
Element set: 908
Inclination: 51
6484 deg
RA of node: 78
0115 deg
Eccentricity:
0003721
Arg of perigee: 120
7366 deg
Mean anomaly: 239
4152 deg
Mean motion: 15
50837087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 290
Coasting Arc #10 (Orbit 1215)
---------------------------------------
Vector Time (GMT): 2014/173/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4479734
40 A = 6789636
37 meter
Y = -2024344
62 meter E =
0010546
Z = 4675026
60 I = 51
98220
XDOT = 143
573478 Wp = 81
63208
YDOT = -7087
563637 meter/sec RA = 72
34649 deg
ZDOT = -2924
312639 TA = 37
35458
MA = 37
28130
Ha = 227
437 n
mi
Hp = 218
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14697291
35 X = -4479474
68
Y = -6641550
58 feet Y = -2074438
94 meter
Z = 15338013
78 Z = 4653264
97
XDOT = 471
041595 XDOT = 237
023010
YDOT = -23253
161540 feet/sec YDOT = -7085
435283 meter/sec
ZDOT = -9594
201570 ZDOT = -2923
388960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4462967
39 X = -1360312
46
Y = 15588953
72 feet Y = 4751513
09 meter
Z = 15246038
11 Z = 4646992
42
XDOT = -21955
384772 XDOT = -6692
001278
YDOT = 3115
413304 feet/sec YDOT = 949
577975 meter/sec
ZDOT = -9588
994992 ZDOT = -2922
725673
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 14173
56650827
00016717 00000-0 10270-3 0 9091
2 25544 51
6485 72
8975 0003606 123
9488 236
2007 15
50884458 12167
Satellite: ISS
Catalog Number: 25544
Epoch time: 14173
56650827 = yrday
fracday
Element set: 909
Inclination: 51
6485 deg
RA of node: 72
8975 deg
Eccentricity:
0003606
Arg of perigee: 123
9488 deg
Mean anomaly: 236
2007 deg
Mean motion: 15
50884458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1216
Checksum: 332
Coasting Arc #11 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2014/174/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4664392
55 A = 6790935
16 meter
Y = 2350199
69 meter E =
0011941
Z = -4352617
41 I = 51
97663
XDOT = -147
837710 Wp = 115
48998
YDOT = 6796
306259 meter/sec RA = 67
40656 deg
ZDOT = 3513
763265 TA = 190
15187
MA = 190
17601
Ha = 227
265 n
mi
Hp = 218
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15303125
16 X = 4658909
13
Y = 7710628
91 feet Y = 2402329
81 meter
Z = -14280240
85 Z = -4329971
36
XDOT = -485
031857 XDOT = -240
893385
YDOT = 22297
592714 feet/sec YDOT = 6794
132301 meter/sec
ZDOT = 11528
094701 ZDOT = 3512
819906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5153995
18 X = 1570937
73
Y = -16425556
35 feet Y = -5006509
58 meter
Z = -14184574
32 Z = -4323458
25
XDOT = 20903
992032 XDOT = 6371
536771
YDOT = -3384
332011 feet/sec YDOT = -1031
544397 meter/sec
ZDOT = 11522
842758 ZDOT = 3512
162473
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 14174
53307381
00016717 00000-0 10270-3 0 9105
2 25544 51
6491 68
1030 0003556 128
4287 231
7183 15
50872713 12318
Satellite: ISS
Catalog Number: 25544
Epoch time: 14174
53307381 = yrday
fracday
Element set: 910
Inclination: 51
6491 deg
RA of node: 68
1030 deg
Eccentricity:
0003556
Arg of perigee: 128
4287 deg
Mean anomaly: 231
7183 deg
Mean motion: 15
50872713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 287
Coasting Arc #12 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2014/175/12:33:37
988
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4851672
32 A = 6792236
09 meter
Y = -2648559
74 meter E =
0013670
Z = 3935121
82 I = 51
96876
XDOT = 219
981047 Wp = 91
91662
YDOT = -6487
277228 meter/sec RA = 62
46747 deg
ZDOT = -4083
320158 TA = 40
66700
MA = 40
56500
Ha = 227
269 n
mi
Hp = 218
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15917560
11 X = -4840810
55
Y = -8689500
46 feet Y = -2702754
07 meter
Z = 12910504
65 Z = 3911579
02
XDOT = 721
722594 XDOT = 312
342424
YDOT = -21283
717939 feet/sec YDOT = -6484
300275 meter/sec
ZDOT = -13396
719678 ZDOT = -4082
028070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5727343
68 X = -1745694
35
Y = 17280936
58 feet Y = 5267229
47 meter
Z = 12811090
27 Z = 3904820
31
XDOT = -19832
673048 XDOT = -6044
998745
YDOT = 3382
384341 feet/sec YDOT = 1030
950747 meter/sec
ZDOT = -13390
031437 ZDOT = -4081
281582
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 14175
56406443
00016717 00000-0 10270-3 0 9119
2 25544 51
6492 62
9890 0003490 130
9769 229
1684 15
50915597 12477
Satellite: ISS
Catalog Number: 25544
Epoch time: 14175
56406443 = yrday
fracday
Element set: 911
Inclination: 51
6492 deg
RA of node: 62
9890 deg
Eccentricity:
0003490
Arg of perigee: 130
9769 deg
Mean anomaly: 229
1684 deg
Mean motion: 15
50915597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1247
Checksum: 330
Coasting Arc #13 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2014/176/10:52:06
403
Vector Time (MET): N/A
Weight (LBS) : 887988
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4386157
86 A = 6789453
08 meter
Y = -609990
23 meter E =
0013891
Z = -5158875
59 I = 51
93913
XDOT = 2853
714431 Wp = 109
80394
YDOT = 6915
085840 meter/sec RA = 57
88834 deg
ZDOT = 1607
570063 TA = 175
67830
MA = 175
66629
Ha = 227
138 n
mi
Hp = 220
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14390281
70 X = 4417713
09
Y = -2001280
27 feet Y = -560764
21 meter
Z = -16925444
85 Z = -5137491
68
XDOT = 9362
580153 XDOT = 2768
367210
YDOT = 22687
289500 feet/sec YDOT = 6946
520471 meter/sec
ZDOT = 5274
179997 ZDOT = 1621
226716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1638946
45 X = 499550
88
Y = -14541893
83 feet Y = -4432369
24 meter
Z = -16834583
21 Z = -5131180
96
XDOT = 23228
501372 XDOT = 7080
047218
YDOT = -3557
368874 feet/sec YDOT = -1084
286033 meter/sec
ZDOT = 5330
838966 ZDOT = 1624
839717
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 14176
46617285
00016717 00000-0 10270-3 0 9128
2 25544 51
6491 58
5138 0001899 183
5339 176
5799 15
50282138 12616
Satellite: ISS
Catalog Number: 25544
Epoch time: 14176
46617285 = yrday
fracday
Element set: 912
Inclination: 51
6491 deg
RA of node: 58
5138 deg
Eccentricity:
0001899
Arg of perigee: 183
5339 deg
Mean anomaly: 176
5799 deg
Mean motion: 15
50282138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 338
Coasting Arc #14 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2014/177/10:52:06
403
Vector Time (MET): N/A
Weight (LBS) : 887988
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4546368
00 A = 6789882
09 meter
Y = 498416
72 meter E =
0005026
Z = 5014812
99 I = 51
92357
XDOT = -3034
828404 Wp = 71
67647
YDOT = -6724
257948 meter/sec RA = 52
94956 deg
ZDOT = -2079
776804 TA = 38
50434
MA = 38
46850
Ha = 227
106 n
mi
Hp = 220
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14915905
50 X = -4575963
79
Y = 1635225
47 feet Y = 447410
09 meter
Z = 16452798
52 Z = 4992655
62
XDOT = -9956
786104 XDOT = -2949
307807
YDOT = -22061
213739 feet/sec YDOT = -6757
716868 meter/sec
ZDOT = -6823
414710 ZDOT = -2094
312807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1865157
97 X = -568500
15
Y = 14992258
39 feet Y = 4569640
36 meter
Z = 16358672
09 Z = 4986123
25
XDOT = -22658
373320 XDOT = -6906
272188
YDOT = 4704
032581 feet/sec YDOT = 1433
789131 meter/sec
ZDOT = -6883
832769 ZDOT = -2098
192228
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 14177
49755836
00016717 00000-0 10270-3 0 9138
2 25544 51
6489 53
4025 0001826 191
8204 168
2904 15
50330979 12775
Satellite: ISS
Catalog Number: 25544
Epoch time: 14177
49755836 = yrday
fracday
Element set: 913
Inclination: 51
6489 deg
RA of node: 53
4025 deg
Eccentricity:
0001826
Arg of perigee: 191
8204 deg
Mean anomaly: 168
2904 deg
Mean motion: 15
50330979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1277
Checksum: 327
Coasting Arc #15 (Orbit 1291)
---------------------------------------
Vector Time (GMT): 2014/178/10:52:06
403
Vector Time (MET): N/A
Weight (LBS) : 887988
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4742189
45 A = 6790635
89 meter
Y = -418679
63 meter E =
0011678
Z = -4853532
99 I = 51
90663
XDOT = 3167
422989 Wp = 116
83234
YDOT = 6488
836928 meter/sec RA = 48
00930 deg
ZDOT = 2534
589680 TA = 178
05789
MA = 178
05336
Ha = 226
933 n
mi
Hp = 220
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15558364
33 X = 4770095
53
Y = -1373620
84 feet Y = -365492
69 meter
Z = -15923664
66 Z = -4830428
51
XDOT = 10391
807706 XDOT = 3082
315779
YDOT = 21288
835065 feet/sec YDOT = 6523
780858 meter/sec
ZDOT = 8315
582940 ZDOT = 2549
770708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1999046
43 X = 609309
35
Y = -15590670
41 feet Y = -4752036
34 meter
Z = -15825531
28 Z = -4823621
93
XDOT = 21869
057295 XDOT = 6665
688664
YDOT = -5702
353848 feet/sec YDOT = -1738
077453 meter/sec
ZDOT = 8378
776631 ZDOT = 2553
851117
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 14178
46447347
00016717 00000-0 10270-3 0 9142
2 25544 51
6490 48
6101 0001834 195
8883 164
2211 15
50316886 12929
Satellite: ISS
Catalog Number: 25544
Epoch time: 14178
46447347 = yrday
fracday
Element set: 914
Inclination: 51
6490 deg
RA of node: 48
6101 deg
Eccentricity:
0001834
Arg of perigee: 195
8883 deg
Mean anomaly: 164
2211 deg
Mean motion: 15
50316886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1292
Checksum: 315
Coasting Arc #16 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2014/179/10:52:06
403
Vector Time (MET): N/A
Weight (LBS) : 887988
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4944224
58 A = 6791320
62 meter
Y = 357517
02 meter E =
0007255
Z = 4636973
21 I = 51
88783
XDOT = -3261
776624 Wp = 74
75616
YDOT = -6259
092023 meter/sec RA = 43
06832 deg
ZDOT = -2989
569300 TA = 44
98977
MA = 44
93102
Ha = 226
908 n
mi
Hp = 220
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16221209
27 X = -4970379
68
Y = 1172956
10 feet Y = 302080
65 meter
Z = 15213166
71 Z = 4612891
59
XDOT = -10701
366875 XDOT = -3177
021369
YDOT = -20535
078816 feet/sec YDOT = -6295
093004 meter/sec
ZDOT = -9808
298227 ZDOT = -3005
209408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2056834
48 X = -626923
15
Y = 16228805
84 feet Y = 4946540
02 meter
Z = 15110896
41 Z = 4605801
23
XDOT = -21043
649073 XDOT = -6414
104237
YDOT = 6543
975587 feet/sec YDOT = 1994
603759 meter/sec
ZDOT = -9873
479299 ZDOT = -3009
436490
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 14179
49583662
00016717 00000-0 10270-3 0 9158
2 25544 51
6489 43
4983 0001750 203
6040 156
5030 15
50367015 13089
Satellite: ISS
Catalog Number: 25544
Epoch time: 14179
49583662 = yrday
fracday
Element set: 915
Inclination: 51
6489 deg
RA of node: 43
4983 deg
Eccentricity:
0001750
Arg of perigee: 203
6040 deg
Mean anomaly: 156
5030 deg
Mean motion: 15
50367015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 301
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