[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 19th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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
294/15:33:44
000 0
0 0
0 0
0
N/A 0
0 0
0 225
5
000/00:00:00
000 0
0 0
0 221
1
300/05:39:30
000 0
0 0
0 0
0
N/A 0
0 0
0 225
6
000/00:00:00
000 0
0 0
0 220
6
Coasting Arc #1 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2014/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1775640
28 A = 6792508
64 meter
Y = -5053474
03 meter E =
0007673
Z = 4172276
22 I = 51
44233
XDOT = 6670
894050 Wp = 107
63546
YDOT = 720
041880 meter/sec RA = 212
25977 deg
ZDOT = 3703
206560 TA = 304
16294
MA = 304
23566
Ha = 225
715 n
mi
Hp = 221
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5825591
46 X = -1739266
97
Y = -16579639
19 feet Y = -5073126
61 meter
Z = 13688570
27 Z = 4163739
15
XDOT = 21886
135335 XDOT = 6644
357404
YDOT = 2362
342125 feet/sec YDOT = 794
492119 meter/sec
ZDOT = 12149
627823 ZDOT = 3735
548624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12382392
39 X = 3774153
20
Y = 12508819
85 feet Y = 3812688
29 meter
Z = 13653010
38 Z = 4161437
56
XDOT = -19842
146953 XDOT = -6047
886391
YDOT = 6202
130279 feet/sec YDOT = 1890
409309 meter/sec
ZDOT = 12287
142936 ZDOT = 3745
121167
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 14290
55525313
00016717 00000-0 10270-3 0 9002
2 25544 51
6444 213
0312 0002699 276
1957 83
8886 15
50525691 30318
Satellite: ISS
Catalog Number: 25544
Epoch time: 14290
55525313 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 213
0312 deg
Eccentricity:
0002699
Arg of perigee: 276
1957 deg
Mean anomaly: 83
8886 deg
Mean motion: 15
50525691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3031
Checksum: 304
Coasting Arc #2 (Orbit 3045)
---------------------------------------
Vector Time (GMT): 2014/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1605112
54 A = 6791240
37 meter
Y = 4847176
26 meter E =
0007230
Z = -4485102
49 I = 51
46628
XDOT = -6913
865135 Wp = 58
58046
YDOT = -685
372962 meter/sec RA = 207
28707 deg
ZDOT = -3215
165338 TA = 178
94841
MA = 178
94689
Ha = 225
649 n
mi
Hp = 221
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5266117
27 X = 1572578
44
Y = 15902809
25 feet Y = 4864943
28 meter
Z = -14714903
17 Z = -4477384
53
XDOT = -22683
284563 XDOT = -6890
068858
YDOT = -2248
598956 feet/sec YDOT = -762
555570 meter/sec
ZDOT = -10548
442710 ZDOT = -3248
694428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11801523
37 X = -3597104
32
Y = -11928933
16 feet Y = -3635938
83 meter
Z = -14682789
54 Z = -4475314
25
XDOT = 20434
204667 XDOT = 6228
345583
YDOT = -7057
468785 feet/sec YDOT = -2151
116486 meter/sec
ZDOT = -10691
027505 ZDOT = -3258
625183
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 14291
52201747
00016717 00000-0 10270-3 0 9013
2 25544 51
6452 208
2376 0002685 281
5567 78
5283 15
50573511 30467
Satellite: ISS
Catalog Number: 25544
Epoch time: 14291
52201747 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 208
2376 deg
Eccentricity:
0002685
Arg of perigee: 281
5567 deg
Mean anomaly: 78
5283 deg
Mean motion: 15
50573511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3046
Checksum: 304
Coasting Arc #3 (Orbit 3061)
---------------------------------------
Vector Time (GMT): 2014/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1392897
57 A = 6790132
94 meter
Y = -4651873
20 meter E =
0005158
Z = 4743778
24 I = 51
49095
XDOT = 7147
313331 Wp = 125
20381
YDOT = 614
502333 meter/sec RA = 202
31537 deg
ZDOT = 2696
244123 TA = 298
05157
MA = 298
10373
Ha = 225
621 n
mi
Hp = 221
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4569873
93 X = -1363819
79
Y = -15262051
19 feet Y = -4667286
36 meter
Z = 15563576
89 Z = 4737082
81
XDOT = 23449
190717 XDOT = 7126
812948
YDOT = 2016
083769 feet/sec YDOT = 694
313908 meter/sec
ZDOT = 8845
945285 ZDOT = 2730
915366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11098218
70 X = 3382737
06
Y = 11467693
24 feet Y = 3495352
90 meter
Z = 15535779
14 Z = 4735305
48
XDOT = -20914
303668 XDOT = -6374
679758
YDOT = 8034
479896 feet/sec YDOT = 2448
909472 meter/sec
ZDOT = 8993
414148 ZDOT = 2741
192632
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 14292
55320924
00016717 00000-0 10270-3 0 9027
2 25544 51
6451 203
1244 0002738 283
3102 76
7744 15
50599598 30621
Satellite: ISS
Catalog Number: 25544
Epoch time: 14292
55320924 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 203
1244 deg
Eccentricity:
0002738
Arg of perigee: 283
3102 deg
Mean anomaly: 76
7744 deg
Mean motion: 15
50599598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3062
Checksum: 302
Coasting Arc #4 (Orbit 3076)
---------------------------------------
Vector Time (GMT): 2014/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1124814
99 A = 6789073
61 meter
Y = 4493000
89 meter E =
0010250
Z = -4973290
59 I = 51
51804
XDOT = -7334
660443 Wp = 65
74227
YDOT = -519
168152 meter/sec RA = 197
34445 deg
ZDOT = -2127
271223 TA = 183
45964
MA = 183
46673
Ha = 225
569 n
mi
Hp = 221
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3690337
89 X = 1098648
66
Y = 14740816
58 feet Y = 4505432
40 meter
Z = -16316570
18 Z = -4967890
41
XDOT = -24063
846598 XDOT = -7317
976080
YDOT = -1703
307586 feet/sec YDOT = -601
096047 meter/sec
ZDOT = -6979
236297 ZDOT = -2162
861966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10276689
24 X = -3132334
88
Y = -11226200
59 feet Y = -3421745
94 meter
Z = -16294256
91 Z = -4966489
51
XDOT = 21182
345810 XDOT = 6456
379003
YDOT = -9037
888571 feet/sec YDOT = -2754
748437 meter/sec
ZDOT = -7130
645187 ZDOT = -2173
420653
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 14293
51992993
00016717 00000-0 10270-3 0 9036
2 25544 51
6460 198
3307 0002750 288
7248 71
3604 15
50647467 30771
Satellite: ISS
Catalog Number: 25544
Epoch time: 14293
51992993 = yrday
fracday
Element set: 903
Inclination: 51
6460 deg
RA of node: 198
3307 deg
Eccentricity:
0002750
Arg of perigee: 288
7248 deg
Mean anomaly: 71
3604 deg
Mean motion: 15
50647467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3077
Checksum: 331
Coasting Arc #5 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2014/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -818042
34 A = 6788242
71 meter
Y = -4357871
92 meter E =
0002268
Z = 5139301
28 I = 51
54555
XDOT = 7498
319982 Wp = 143
95743
YDOT = 400
429824 meter/sec RA = 192
37460 deg
ZDOT = 1530
941498 TA = 291
25083
MA = 291
27505
Ha = 225
528 n
mi
Hp = 221
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2683865
94 X = -794216
38
Y = -14297480
05 feet Y = -4366885
96 meter
Z = 16861224
67 Z = 5135385
66
XDOT = 24600
787343 XDOT = 7485
848015
YDOT = 1313
746141 feet/sec YDOT = 484
211347 meter/sec
ZDOT = 5022
773943 ZDOT = 1567
337657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9376101
64 X = 2857835
78
Y = 11146733
13 feet Y = 3397524
26 meter
Z = 16845207
87 Z = 5134419
36
XDOT = -21307
712080 XDOT = -6494
590642
YDOT = 10087
841843 feet/sec YDOT = 3074
774194 meter/sec
ZDOT = 5177
640984 ZDOT = 1578
144972
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 14294
55107516
00016717 00000-0 10270-3 0 9041
2 25544 51
6459 193
2172 0002824 290
5062 69
5786 15
50676071 30931
Satellite: ISS
Catalog Number: 25544
Epoch time: 14294
55107516 = yrday
fracday
Element set: 904
Inclination: 51
6459 deg
RA of node: 193
2172 deg
Eccentricity:
0002824
Arg of perigee: 290
5062 deg
Mean anomaly: 69
5786 deg
Mean motion: 15
50676071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3093
Checksum: 316
Coasting Arc #6 (Orbit 3094)
---------------------------------------
Vector Time (GMT): 2014/294/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6569966
71 A = 6799385
66 meter
Y = 1683731
71 meter E =
0008768
Z = -409751
65 I = 51
58563
XDOT = -1530
360786 Wp = 146
92741
YDOT = 4531
290592 meter/sec RA = 191
62820 deg
ZDOT = -5985
825027 TA = 37
48673
MA = 37
42561
Ha = 225
517 n
mi
Hp = 221
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21555008
90 X = 6552641
02
Y = 5524054
15 feet Y = 1757104
41 meter
Z = -1344329
55 Z = -377877
31
XDOT = -5020
868722 XDOT = -1551
839177
YDOT = 14866
438949 feet/sec YDOT = 4514
056298 meter/sec
ZDOT = -19638
533554 ZDOT = -5993
312167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8253299
57 X = -2515605
71
Y = 20672745
60 feet Y = 6301052
86 meter
Z = -1208900
47 Z = -368472
86
XDOT = -12603
354037 XDOT = -3841
502310
YDOT = -6167
580886 feet/sec YDOT = -1879
878654 meter/sec
ZDOT = -19671
080815 ZDOT = -5995
745432
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 14294
67996570
00016717 00000-0 10270-3 0 9051
2 25544 51
6444 192
5776 0002989 290
1512 69
9317 15
50655157 30953
Satellite: ISS
Catalog Number: 25544
Epoch time: 14294
67996570 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 192
5776 deg
Eccentricity:
0002989
Arg of perigee: 290
1512 deg
Mean anomaly: 69
9317 deg
Mean motion: 15
50655157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3095
Checksum: 348
Coasting Arc #7 (Orbit 3110)
---------------------------------------
Vector Time (GMT): 2014/295/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6545304
65 A = 6798933
38 meter
Y = -1535481
82 meter E =
0012115
Z = 965693
66 I = 51
61432
XDOT = 1929
225057 Wp = 43
17997
YDOT = -4486
168564 meter/sec RA = 186
66864 deg
ZDOT = 5907
536845 TA = 327
27067
MA = 327
34567
Ha = 225
449 n
mi
Hp = 221
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21474096
64 X = -6532339
21
Y = -5037670
03 feet Y = -1608603
06 meter
Z = 3168286
28 Z = 933928
40
XDOT = 6329
478532 XDOT = 1950
549450
YDOT = -14718
400801 feet/sec YDOT = -4464
474834 meter/sec
ZDOT = 19381
682561 ZDOT = 5916
961262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7405229
75 X = 2257114
03
Y = -20796988
14 feet Y = -6338921
99 meter
Z = 3033288
65 Z = 924546
38
XDOT = 12415
299003 XDOT = 3784
183136
YDOT = 7271
186495 feet/sec YDOT = 2216
257644 meter/sec
ZDOT = 19422
473869 ZDOT = 5919
970035
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 14295
71108378
00016717 00000-0 10270-3 0 9069
2 25544 51
6434 187
4626 0003035 293
2172 66
8659 15
50707737 31114
Satellite: ISS
Catalog Number: 25544
Epoch time: 14295
71108378 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 187
4626 deg
Eccentricity:
0003035
Arg of perigee: 293
2172 deg
Mean anomaly: 66
8659 deg
Mean motion: 15
50707737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3111
Checksum: 317
Coasting Arc #8 (Orbit 3125)
---------------------------------------
Vector Time (GMT): 2014/296/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6463726
58 A = 6798241
87 meter
Y = 1416972
75 meter E =
0005648
Z = -1545668
99 I = 51
64292
XDOT = -2354
318804 Wp = 155
89809
YDOT = 4481
567446 meter/sec RA = 181
71231 deg
ZDOT = -5749
407661 TA = 40
96400
MA = 40
92158
Ha = 225
478 n
mi
Hp = 221
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21206452
02 X = 6454909
82
Y = 4648860
74 feet Y = 1489204
89 meter
Z = -5071092
49 Z = -1514289
85
XDOT = -7724
143057 XDOT = -2376
328239
YDOT = 14703
305270 feet/sec YDOT = 4455
116319 meter/sec
ZDOT = -18862
886027 ZDOT = -5760
898797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6635001
25 X = -2022348
38
Y = 20703557
02 feet Y = 6310444
18 meter
Z = -4937709
76 Z = -1505013
93
XDOT = -12407
298195 XDOT = -3781
744490
YDOT = -8476
775060 feet/sec YDOT = -2583
721038 meter/sec
ZDOT = -18912
481781 ZDOT = -5764
524447
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 14296
67773604
00016717 00000-0 10270-3 0 9076
2 25544 51
6429 182
6687 0003044 297
4626 62
6215 15
50738579 31268
Satellite: ISS
Catalog Number: 25544
Epoch time: 14296
67773604 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 182
6687 deg
Eccentricity:
0003044
Arg of perigee: 297
4626 deg
Mean anomaly: 62
6215 deg
Mean motion: 15
50738579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3126
Checksum: 338
Coasting Arc #9 (Orbit 3141)
---------------------------------------
Vector Time (GMT): 2014/297/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6327270
54 A = 6797296
94 meter
Y = -1299987
16 meter E =
0012153
Z = 2094643
32 I = 51
67037
XDOT = 2766
979876 Wp = 58
67986
YDOT = -4533
514492 meter/sec RA = 176
75549 deg
ZDOT = 5527
050935 TA = 324
47513
MA = 324
55599
Ha = 225
464 n
mi
Hp = 220
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20758761
62 X = -6322438
91
Y = -4265049
73 feet Y = -1370715
62 meter
Z = 6872189
39 Z = 2063917
32
XDOT = 9078
017967 XDOT = 2790
619651
YDOT = -14873
735211 feet/sec YDOT = -4502
439732 meter/sec
ZDOT = 18133
369209 ZDOT = 5540
550672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5861309
80 X = 1786527
23
Y = -20409318
09 feet Y = -6220760
15 meter
Z = 6741557
90 Z = 2054826
85
XDOT = 12645
690318 XDOT = 3854
406409
YDOT = 9660
040100 feet/sec YDOT = 2944
380223 meter/sec
ZDOT = 18191
533939 ZDOT = 5544
779545
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 14297
70880802
00016717 00000-0 10270-3 0 9081
2 25544 51
6418 177
5533 0003008 298
4827 61
6021 15
50781176 31426
Satellite: ISS
Catalog Number: 25544
Epoch time: 14297
70880802 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 177
5533 deg
Eccentricity:
0003008
Arg of perigee: 298
4827 deg
Mean anomaly: 61
6021 deg
Mean motion: 15
50781176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3142
Checksum: 311
Coasting Arc #10 (Orbit 3156)
---------------------------------------
Vector Time (GMT): 2014/298/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6135630
07 A = 6796084
01 meter
Y = 1230621
20 meter E =
0002082
Z = -2650018
82 I = 51
69743
XDOT = -3177
911842 Wp = 131
10109
YDOT = 4620
367489 meter/sec RA = 171
80103 deg
ZDOT = -5216
262062 TA = 78
69467
MA = 78
67128
Ha = 225
481 n
mi
Hp = 220
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20130019
91 X = 6134286
26
Y = 4037471
13 feet Y = 1299226
13 meter
Z = -8694287
46 Z = -2620215
29
XDOT = -10426
219954 XDOT = -3204
002038
YDOT = 15158
685987 feet/sec YDOT = 4584
683845 meter/sec
ZDOT = -17113
720675 ZDOT = -5231
763975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5244879
09 X = -1598639
15
Y = 19904714
54 feet Y = 6066956
99 meter
Z = -8567560
41 Z = -2611392
41
XDOT = -13056
857894 XDOT = -3979
730286
YDOT = -10829
681240 feet/sec YDOT = -3300
886842 meter/sec
ZDOT = -17180
435791 ZDOT = -5236
596829
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 14298
67541714
00016717 00000-0 10270-3 0 9095
2 25544 51
6414 172
7588 0002990 304
9928 55
0942 15
50819621 31575
Satellite: ISS
Catalog Number: 25544
Epoch time: 14298
67541714 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 172
7588 deg
Eccentricity:
0002990
Arg of perigee: 304
9928 deg
Mean anomaly: 55
0942 deg
Mean motion: 15
50819621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3157
Checksum: 334
Coasting Arc #11 (Orbit 3172)
---------------------------------------
Vector Time (GMT): 2014/299/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5891721
64 A = 6794747
01 meter
Y = -1183008
05 meter E =
0010818
Z = 3159000
48 I = 51
72331
XDOT = 3558
613935 Wp = 75
55717
YDOT = -4757
210686 meter/sec RA = 166
84600 deg
ZDOT = 4844
249784 TA = 320
79367
MA = 320
87198
Ha = 225
504 n
mi
Hp = 220
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19329795
40 X = -5893400
89
Y = -3881260
02 feet Y = -1248902
37 meter
Z = 10364174
82 Z = 3130374
54
XDOT = 11675
242570 XDOT = 3588
013248
YDOT = -15607
646607 feet/sec YDOT = -4717
251385 meter/sec
ZDOT = 15893
207953 ZDOT = 4861
609088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4711512
95 X = 1436069
15
Y = -19209771
77 feet Y = -5855138
44 meter
Z = 10242441
29 Z = 3121896
10
XDOT = 13692
810277 XDOT = 4173
568572
YDOT = 11892
204326 feet/sec YDOT = 3624
743878 meter/sec
ZDOT = 15967
867792 ZDOT = 4867
006103
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 14299
70644319
00016717 00000-0 10270-3 0 9107
2 25544 51
6406 167
6430 0002944 304
4533 55
6339 15
50854524 31736
Satellite: ISS
Catalog Number: 25544
Epoch time: 14299
70644319 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 167
6430 deg
Eccentricity:
0002944
Arg of perigee: 304
4533 deg
Mean anomaly: 55
6339 deg
Mean motion: 15
50854524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3173
Checksum: 307
Coasting Arc #12 (Orbit 3181)
---------------------------------------
Vector Time (GMT): 2014/300/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2525019
65 A = 6787423
96 meter
Y = -3547866
97 meter E =
0001260
Z = 5205387
10 I = 51
71810
XDOT = 6916
345863 Wp = 108
36807
YDOT = -3043
978092 meter/sec RA = 163
92558 deg
ZDOT = 1279
624276 TA = 329
34771
MA = 329
35507
Ha = 225
554 n
mi
Hp = 220
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8284185
20 X = -2510445
64
Y = -11639983
50 feet Y = -3576021
72 meter
Z = 17078041
65 Z = 5193156
11
XDOT = 22691
423436 XDOT = 6943
654129
YDOT = -9986
804763 feet/sec YDOT = -2966
482302 meter/sec
ZDOT = 4198
242375 ZDOT = 1313
290180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5985116
74 X = -1824263
58
Y = 13040451
11 feet Y = 3974729
50 meter
Z = 17026492
86 Z = 5189675
03
XDOT = -18915
246372 XDOT = -5765
367094
YDOT = -14353
541899 feet/sec YDOT = -4374
959571 meter/sec
ZDOT = 4342
100928 ZDOT = 1323
472363
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 14300
28638634
00016717 00000-0 10270-3 0 9117
2 25544 51
6418 164
7692 0003113 311
5184 48
5699 15
50872465 31821
Satellite: ISS
Catalog Number: 25544
Epoch time: 14300
28638634 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 164
7692 deg
Eccentricity:
0003113
Arg of perigee: 311
5184 deg
Mean anomaly: 48
5699 deg
Mean motion: 15
50872465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3182
Checksum: 312
Coasting Arc #13 (Orbit 3196)
---------------------------------------
Vector Time (GMT): 2014/301/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2106720
98 A = 6786938
83 meter
Y = 3677195
44 meter E =
0012889
Z = -5312214
63 I = 51
74658
XDOT = -6950
144511 Wp = 74
87273
YDOT = 3154
601195 meter/sec RA = 158
96572 deg
ZDOT = -570
507283 TA = 189
66815
MA = 189
69298
Ha = 225
560 n
mi
Hp = 220
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6911814
25 X = 2091250
74
Y = 12064289
49 feet Y = 3700667
53 meter
Z = -17428525
70 Z = -5302017
92
XDOT = -22802
311389 XDOT = -6982
132038
YDOT = 10349
741455 feet/sec YDOT = 3076
701312 meter/sec
ZDOT = -1871
743053 ZDOT = -604
348606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6821539
12 X = 2079205
12
Y = -12176995
99 feet Y = -3711548
38 meter
Z = -17385658
97 Z = -5299148
85
XDOT = 19606
241669 XDOT = 5975
982461
YDOT = 13872
249806 feet/sec YDOT = 4228
261741 meter/sec
ZDOT = -2016
388560 ZDOT = -614
595233
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 14301
25294005
00016717 00000-0 10270-3 0 9126
2 25544 51
6419 159
9735 0003128 315
7813 44
3087 15
50886289 31977
Satellite: ISS
Catalog Number: 25544
Epoch time: 14301
25294005 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 159
9735 deg
Eccentricity:
0003128
Arg of perigee: 315
7813 deg
Mean anomaly: 44
3087 deg
Mean motion: 15
50886289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3197
Checksum: 317
Coasting Arc #14 (Orbit 3212)
---------------------------------------
Vector Time (GMT): 2014/302/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1673650
57 A = 6786663
48 meter
Y = -3853857
29 meter E =
0002705
Z = 5329450
13 I = 51
77565
XDOT = 6942
258953 Wp = 7
16405
YDOT = -3242
655219 meter/sec RA = 154
00859 deg
ZDOT = -162
083478 TA = 84
39401
MA = 84
36316
Ha = 225
585 n
mi
Hp = 220
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5490979
55 X = -1656320
67
Y = -12643888
74 feet Y = -3872476
12 meter
Z = 17485072
60 Z = 5321361
80
XDOT = 22776
440134 XDOT = 6978
790471
YDOT = -10638
632609 feet/sec YDOT = -3164
818127 meter/sec
ZDOT = -531
769940 ZDOT = -128
269558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7847829
15 X = -2392018
32
Y = 11384782
90 feet Y = 3470081
83 meter
Z = 17451213
10 Z = 5319129
75
XDOT = -20148
987537 XDOT = -6141
411401
YDOT = -13282
460324 feet/sec YDOT = -4048
493907 meter/sec
ZDOT = -387
205203 ZDOT = -118
020146
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 14302
28390726
00016717 00000-0 10270-3 0 9138
2 25544 51
6425 154
8592 0003226 319
5067 40
5844 15
50935859 32137
Satellite: ISS
Catalog Number: 25544
Epoch time: 14302
28390726 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 154
8592 deg
Eccentricity:
0003226
Arg of perigee: 319
5067 deg
Mean anomaly: 40
5844 deg
Mean motion: 15
50935859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3213
Checksum: 309
Coasting Arc #15 (Orbit 3227)
---------------------------------------
Vector Time (GMT): 2014/303/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1267053
76 A = 6786843
30 meter
Y = 4084593
64 meter E =
0012430
Z = -5280501
47 I = 51
80445
XDOT = -6854
708900 Wp = 85
92622
YDOT = 3285
348214 meter/sec RA = 149
05192 deg
ZDOT = 899
196416 TA = 192
65481
MA = 192
68604
Ha = 225
599 n
mi
Hp = 220
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4157000
53 X = 1246936
06
Y = 13400897
77 feet Y = 4098650
02 meter
Z = -17324479
88 Z = -5274395
19
XDOT = -22489
202429 XDOT = -6895
305036
YDOT = 10778
701490 feet/sec YDOT = 3208
467459 meter/sec
ZDOT = 2950
119476 ZDOT = 865
798026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9006707
34 X = 2745244
40
Y = -10799197
91 feet Y = -3291595
52 meter
Z = -17299100
11 Z = -5272765
71
XDOT = 20399
025022 XDOT = 6217
622827
YDOT = 12530
278548 feet/sec YDOT = 3819
228901 meter/sec
ZDOT = 2807
297797 ZDOT = 855
664369
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 14303
25041759
00016717 00000-0 10270-3 0 9146
2 25544 51
6428 150
0634 0003295 323
0379 37
0544 15
50958232 32281
Satellite: ISS
Catalog Number: 25544
Epoch time: 14303
25041759 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 150
0634 deg
Eccentricity:
0003295
Arg of perigee: 323
0379 deg
Mean anomaly: 37
0544 deg
Mean motion: 15
50958232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3228
Checksum: 291
Coasting Arc #16 (Orbit 3243)
---------------------------------------
Vector Time (GMT): 2014/304/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -860532
88 A = 6787328
63 meter
Y = -4356845
27 meter E =
0006063
Z = 5132173
25 I = 51
83347
XDOT = 6730
414649 Wp = 22
02887
YDOT = -3275
287566 meter/sec RA = 144
09847 deg
ZDOT = -1645
857841 TA = 83
85747
MA = 83
78840
Ha = 225
629 n
mi
Hp = 220
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2823270
62 X = -836680
43
Y = -14294111
77 feet Y = -4366334
71 meter
Z = 16837838
75 Z = 5128050
98
XDOT = 22081
412889 XDOT = 6774
534600
YDOT = -10745
694115 feet/sec YDOT = -3199
777092 meter/sec
ZDOT = -5399
796066 ZDOT = -1613
054719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10302259
00 X = -3140128
54
Y = 10330740
56 feet Y = 3148809
72 meter
Z = 16820956
01 Z = 5127027
39
XDOT = -20413
018487 XDOT = -6221
888035
YDOT = -11760
340762 feet/sec YDOT = -3584
551864 meter/sec
ZDOT = -5259
494232 ZDOT = -1603
093842
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 14304
28133925
00016717 00000-0 10270-3 0 9158
2 25544 51
6434 144
9490 0003334 327
2046 32
8898 15
50999242 32440
Satellite: ISS
Catalog Number: 25544
Epoch time: 14304
28133925 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 144
9490 deg
Eccentricity:
0003334
Arg of perigee: 327
2046 deg
Mean anomaly: 32
8898 deg
Mean motion: 15
50999242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3244
Checksum: 312
Coasting Arc #17 (Orbit 3258)
---------------------------------------
Vector Time (GMT): 2014/305/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 507526
19 A = 6788165
82 meter
Y = 4663470
59 meter E =
0009871
Z = -4915208
35 I = 51
86154
XDOT = -6540
047878 Wp = 93
29675
YDOT = 3200
789324 meter/sec RA = 139
14613 deg
ZDOT = 2365
100351 TA = 199
81168
MA = 199
85005
Ha = 225
656 n
mi
Hp = 220
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1665112
17 X = 479217
26
Y = 15300100
37 feet Y = 4668987
49 meter
Z = -16126011
66 Z = -4912811
88
XDOT = -21456
849993 XDOT = -6586
842817
YDOT = 10501
277310 feet/sec YDOT = 3127
392769 meter/sec
ZDOT = 7759
515586 ZDOT = 2333
215461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11610538
36 X = 3538892
09
Y = -10117641
13 feet Y = -3083857
02 meter
Z = -16116533
71 Z = -4912319
48
XDOT = 20094
178472 XDOT = 6124
705598
YDOT = 10934
704450 feet/sec YDOT = 3332
897916 meter/sec
ZDOT = 7623
122979 ZDOT = 2323
527884
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 14305
24780631
00016717 00000-0 10270-3 0 9168
2 25544 51
6436 140
1530 0003421 330
6801 29
4158 15
51033039 32590
Satellite: ISS
Catalog Number: 25544
Epoch time: 14305
24780631 = yrday
fracday
Element set: 916
Inclination: 51
6436 deg
RA of node: 140
1530 deg
Eccentricity:
0003421
Arg of perigee: 330
6801 deg
Mean anomaly: 29
4158 deg
Mean motion: 15
51033039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3259
Checksum: 272
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