[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 25th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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
297/11:05:09
667 -0
8 2
1 2
1
N/A 1
4 -0
4 228
9
000/00:04:19
333 -1
3 -0
2 221
5
301/09:00:02
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 221
3
Coasting Arc #1 (Orbit 1461)
---------------------------------------
Vector Time (GMT): 2013/296/13:52:05
014
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4704845
63 A = 6794074
79 meter
Y = 2496568
25 meter E =
0009549
Z = -4226864
92 I = 51
57065
XDOT = -5401
496894 Wp = 96
21794
YDOT = -4008
624904 meter/sec RA = 191
07297 deg
ZDOT = 3650
747082 TA = 211
26532
MA = 211
32214
Ha = 228
427 n
mi
Hp = 220
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15435845
24 X = -4711879
75
Y = 8190840
71 feet Y = 2443916
19 meter
Z = -13867667
06 Z = -4249738
27
XDOT = -17721
446503 XDOT = -5374
004810
YDOT = -13151
656508 feet/sec YDOT = -4068
874029 meter/sec
ZDOT = 11977
516673 ZDOT = 3624
573493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 780599
87 X = 237926
84
Y = -17379998
17 feet Y = -5297423
44 meter
Z = -13964014
71 Z = -4256231
68
XDOT = 19118
824841 XDOT = 5827
417812
YDOT = -8660
813243 feet/sec YDOT = -2639
815876 meter/sec
ZDOT = 11868
141450 ZDOT = 3617
409514
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 13296
58733203
00016717 00000-0 10270-3 0 9009
2 25544 51
6499 192
1442 0002606 45
2698 314
8664 15
49881053 14626
Satellite: ISS
Catalog Number: 25544
Epoch time: 13296
58733203 = yrday
fracday
Element set: 900
Inclination: 51
6499 deg
RA of node: 192
1442 deg
Eccentricity:
0002606
Arg of perigee: 45
2698 deg
Mean anomaly: 314
8664 deg
Mean motion: 15
49881053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1462
Checksum: 319
Coasting Arc #2 (Orbit 1475)
---------------------------------------
Vector Time (GMT): 2013/297/11:07:19
333
Vector Time (MET): N/A
Weight (LBS) : 936367
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5458326
94 A = 6799492
57 meter
Y = 2903340
71 meter E =
0006011
Z = -2831906
98 I = 51
61101
XDOT = -4507
895833 Wp = 112
40894
YDOT = 3525
142542 meter/sec RA = 186
73013 deg
ZDOT = -5085
523329 TA = 99
68493
MA = 99
61703
Ha = 228
851 n
mi
Hp = 221
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17907896
77 X = 5439212
35
Y = 9525396
04 feet Y = 2964272
22 meter
Z = -9291033
40 Z = -2805436
98
XDOT = -14789
684490 XDOT = -4522
275174
YDOT = 11565
428287 feet/sec YDOT = 3474
651802 meter/sec
ZDOT = -16684
787824 ZDOT = -5107
457725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20089035
01 X = -6123137
87
Y = -3146859
01 feet Y = -959162
63 meter
Z = -9180260
83 Z = -2798143
50
XDOT = 9883
394033 XDOT = 3012
458501
YDOT = -14255
358387 feet/sec YDOT = -4345
033236 meter/sec
ZDOT = -16777
334688 ZDOT = -5113
731613
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 13297
49003567
00016717 00000-0 10270-3 0 9014
2 25544 51
6492 187
6728 0001492 85
2275 274
9046 15
49507591 14769
Satellite: ISS
Catalog Number: 25544
Epoch time: 13297
49003567 = yrday
fracday
Element set: 901
Inclination: 51
6492 deg
RA of node: 187
6728 deg
Eccentricity:
0001492
Arg of perigee: 85
2275 deg
Mean anomaly: 274
9046 deg
Mean motion: 15
49507591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1476
Checksum: 337
Coasting Arc #3 (Orbit 1491)
---------------------------------------
Vector Time (GMT): 2013/298/11:07:19
333
Vector Time (MET): N/A
Weight (LBS) : 936367
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5563442
07 A = 6799106
84 meter
Y = -2523851
78 meter E =
0014773
Z = 2969230
49 I = 51
64025
XDOT = 4400
055128 Wp = 82
80797
YDOT = -3811
035350 meter/sec RA = 181
77832 deg
ZDOT = 4985
481516 TA = 311
07348
MA = 311
20100
Ha = 228
882 n
mi
Hp = 221
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18252762
70 X = -5549230
26
Y = -8280353
62 feet Y = -2585986
15 meter
Z = 9741569
86 Z = 2942237
98
XDOT = 14435
876403 XDOT = 4418
125433
YDOT = -12503
396817 feet/sec YDOT = -3761
729897 meter/sec
ZDOT = 16356
566655 ZDOT = 5006
900973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20040732
51 X = 6108415
27
Y = 1511960
87 feet Y = 460845
67 meter
Z = 9628540
91 Z = 2934779
27
XDOT = -9079
156421 XDOT = -2767
326877
YDOT = 15191
465252 feet/sec YDOT = 4630
358609 meter/sec
ZDOT = 16446
998875 ZDOT = 5013
045257
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 13298
52192756
00016717 00000-0 10270-3 0 9029
2 25544 51
6489 182
5644 0001567 85
8432 274
2898 15
49527699 14927
Satellite: ISS
Catalog Number: 25544
Epoch time: 13298
52192756 = yrday
fracday
Element set: 902
Inclination: 51
6489 deg
RA of node: 182
5644 deg
Eccentricity:
0001567
Arg of perigee: 85
8432 deg
Mean anomaly: 274
2898 deg
Mean motion: 15
49527699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1492
Checksum: 360
Coasting Arc #4 (Orbit 1506)
---------------------------------------
Vector Time (GMT): 2013/299/11:07:19
333
Vector Time (MET): N/A
Weight (LBS) : 936367
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5620974
35 A = 6798592
37 meter
Y = 2179537
67 meter E =
0005836
Z = -3145925
66 I = 51
67007
XDOT = -4292
172278 Wp = 102
36311
YDOT = 4079
393775 meter/sec RA = 176
82858 deg
ZDOT = -4851
611163 TA = 113
77547
MA = 113
71425
Ha = 228
737 n
mi
Hp = 221
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18441516
90 X = 5611466
79
Y = 7150714
13 feet Y = 2242341
67 meter
Z = -10321278
40 Z = -3118642
27
XDOT = -14081
930046 XDOT = -4313
901790
YDOT = 13383
837844 feet/sec YDOT = 4031
274244 meter/sec
ZDOT = -15917
359460 ZDOT = -4872
515432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19838521
00 X = -6046781
20
Y = -43421
60 feet Y = -13234
90 meter
Z = -10206970
41 Z = -3111084
58
XDOT = 8255
017744 XDOT = 2516
129408
YDOT = -16057
952773 feet/sec YDOT = -4894
464005 meter/sec
ZDOT = -16005
672613 ZDOT = -4878
529013
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 13299
48930972
00016717 00000-0 10270-3 0 9036
2 25544 51
6494 177
7754 0001352 91
0959 269
0347 15
49549429 15079
Satellite: ISS
Catalog Number: 25544
Epoch time: 13299
48930972 = yrday
fracday
Element set: 903
Inclination: 51
6494 deg
RA of node: 177
7754 deg
Eccentricity:
0001352
Arg of perigee: 91
0959 deg
Mean anomaly: 269
0347 deg
Mean motion: 15
49549429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1507
Checksum: 349
Coasting Arc #5 (Orbit 1522)
---------------------------------------
Vector Time (GMT): 2013/300/11:07:19
333
Vector Time (MET): N/A
Weight (LBS) : 936367
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5657772
13 A = 6798139
15 meter
Y = -1816806
25 meter E =
0014180
Z = 3289186
40 I = 51
69938
XDOT = 4161
176766 Wp = 87
83968
YDOT = -4366
218799 meter/sec RA = 171
88036 deg
ZDOT = 4728
872655 TA = 310
26493
MA = 310
38883
Ha = 228
795 n
mi
Hp = 221
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18562244
51 X = -5653013
91
Y = -5960650
44 feet Y = -1880048
26 meter
Z = 10791293
97 Z = 3261712
73
XDOT = 13652
154745 XDOT = 4186
719602
YDOT = -14324
864825 feet/sec YDOT = -4319
542778 meter/sec
ZDOT = 15514
674065 ZDOT = 4749
149864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19505455
99 X = 5945262
98
Y = -1447681
19 feet Y = -441253
23 meter
Z = 10676127
88 Z = 3254083
78
XDOT = -7312
928279 XDOT = -2228
980539
YDOT = 16934
373195 feet/sec YDOT = 5161
596950 meter/sec
ZDOT = 15600
399518 ZDOT = 4755
001773
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 13300
52116936
00016717 00000-0 10270-3 0 9041
2 25544 51
6494 172
6667 0001477 89
1405 270
9915 15
49573115 15237
Satellite: ISS
Catalog Number: 25544
Epoch time: 13300
52116936 = yrday
fracday
Element set: 904
Inclination: 51
6494 deg
RA of node: 172
6667 deg
Eccentricity:
0001477
Arg of perigee: 89
1405 deg
Mean anomaly: 270
9915 deg
Mean motion: 15
49573115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1523
Checksum: 312
Coasting Arc #6 (Orbit 1536)
---------------------------------------
Vector Time (GMT): 2013/301/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 903298
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1268637
28 A = 6790478
51 meter
Y = -4020841
58 meter E =
0003893
Z = 5319727
44 I = 51
70131
XDOT = 7413
423904 Wp = 103
07274
YDOT = -1919
690682 meter/sec RA = 167
34917 deg
ZDOT = 315
911436 TA = 343
91048
MA = 343
92284
Ha = 228
586 n
mi
Hp = 221
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4162195
81 X = -1249423
24
Y = -13191737
45 feet Y = -4034920
48 meter
Z = 17453174
00 Z = 5313611
37
XDOT = 24322
256903 XDOT = 7432
804686
YDOT = -6298
197777 feet/sec YDOT = -1836
680672 meter/sec
ZDOT = 1036
454841 ZDOT = 351
972924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2169345
58 X = 661216
53
Y = 13693722
90 feet Y = 4173846
74 meter
Z = 17427994
34 Z = 5312052
67
XDOT = -24000
048630 XDOT = -7315
214823
YDOT = 2285
454379 feet/sec YDOT = 696
606495 meter/sec
ZDOT = 1188
181640 ZDOT = 362
157764
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 13301
42403109
00016717 00000-0 10270-3 0 9053
2 25544 51
6483 168
1968 0001310 95
7188 264
4112 15
49642782 15375
Satellite: ISS
Catalog Number: 25544
Epoch time: 13301
42403109 = yrday
fracday
Element set: 905
Inclination: 51
6483 deg
RA of node: 168
1968 deg
Eccentricity:
0001310
Arg of perigee: 95
7188 deg
Mean anomaly: 264
4112 deg
Mean motion: 15
49642782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1537
Checksum: 302
Coasting Arc #7 (Orbit 1551)
---------------------------------------
Vector Time (GMT): 2013/302/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 903298
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1351881
51 A = 6790449
00 meter
Y = 3990158
87 meter E =
0016247
Z = -5339586
53 I = 51
73176
XDOT = -7273
309250 Wp = 90
08341
YDOT = 2367
162035 meter/sec RA = 162
40195 deg
ZDOT = -72
748454 TA = 179
22377
MA = 179
22125
Ha = 228
579 n
mi
Hp = 221
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4435306
80 X = 1333100
90
Y = 13091072
42 feet Y = 4005171
03 meter
Z = -17518328
50 Z = -5333065
04
XDOT = -23862
563156 XDOT = -7298
885406
YDOT = 7766
279644 feet/sec YDOT = 2285
684252 meter/sec
ZDOT = -238
676030 ZDOT = -108
144435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2689385
90 X = -819724
82
Y = -13592522
49 feet Y = -4143000
86 meter
Z = -17491440
56 Z = -5331391
08
XDOT = 23714
475773 XDOT = 7228
172216
YDOT = -4194
119937 feet/sec YDOT = -1278
367757 meter/sec
ZDOT = -387
678360 ZDOT = -118
164364
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 13302
39137137
00016717 00000-0 10270-3 0 9066
2 25544 51
6491 163
4072 0001421 95
6493 264
4820 15
49644507 15529
Satellite: ISS
Catalog Number: 25544
Epoch time: 13302
39137137 = yrday
fracday
Element set: 906
Inclination: 51
6491 deg
RA of node: 163
4072 deg
Eccentricity:
0001421
Arg of perigee: 95
6493 deg
Mean anomaly: 264
4820 deg
Mean motion: 15
49644507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1552
Checksum: 299
Coasting Arc #8 (Orbit 1567)
---------------------------------------
Vector Time (GMT): 2013/303/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 903298
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1423853
18 A = 6790294
20 meter
Y = -3955853
30 meter E =
0003646
Z = 5329012
64 I = 51
76053
XDOT = 7129
707700 Wp = 89
45205
YDOT = -2807
074342 meter/sec RA = 157
45698 deg
ZDOT = -178
639701 TA = 2
24926
MA = 2
24762
Ha = 228
487 n
mi
Hp = 221
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4671434
32 X = -1405399
54
Y = -12978521
34 feet Y = -3971672
08 meter
Z = 17483637
27 Z = 5322140
73
XDOT = 23391
429462 XDOT = 7161
434923
YDOT = -9209
561491 feet/sec YDOT = -2727
168031 meter/sec
ZDOT = -586
088258 ZDOT = -143
926241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3170616
56 X = 966403
93
Y = 13461148
97 feet Y = 4102958
20 meter
Z = 17455272
73 Z = 5320367
13
XDOT = -23357
409289 XDOT = -7119
338351
YDOT = 6072
563933 feet/sec YDOT = 1850
917487 meter/sec
ZDOT = -439
883682 ZDOT = -134
076546
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 13303
42318198
00016717 00000-0 10270-3 0 9070
2 25544 51
6488 158
2987 0001242 99
7809 260
3482 15
49692868 15688
Satellite: ISS
Catalog Number: 25544
Epoch time: 13303
42318198 = yrday
fracday
Element set: 907
Inclination: 51
6488 deg
RA of node: 158
2987 deg
Eccentricity:
0001242
Arg of perigee: 99
7809 deg
Mean anomaly: 260
3482 deg
Mean motion: 15
49692868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1568
Checksum: 352
Coasting Arc #9 (Orbit 1582)
---------------------------------------
Vector Time (GMT): 2013/304/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 903298
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1496605
64 A = 6790341
78 meter
Y = 3951008
63 meter E =
0016044
Z = -5329776
24 I = 51
78913
XDOT = -6927
080081 Wp = 93
97842
YDOT = 3215
049172 meter/sec RA = 152
51328 deg
ZDOT = 438
269048 TA = 180
20287
MA = 180
20353
Ha = 228
445 n
mi
Hp = 221
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4910123
48 X = 1478204
56
Y = 12962626
74 feet Y = 3967641
26 meter
Z = -17486142
53 Z = -5322550
75
XDOT = -22726
640686 XDOT = -6964
645669
YDOT = 10548
061587 feet/sec YDOT = 3137
376150 meter/sec
ZDOT = 1437
890578 ZDOT = 404
525616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3640755
26 X = -1109702
20
Y = -13413683
76 feet Y = -4088490
81 meter
Z = -17456293
26 Z = -5320678
19
XDOT = 22732
440362 XDOT = 6928
847822
YDOT = -7856
015562 feet/sec YDOT = -2394
513543 meter/sec
ZDOT = 1295
695628 ZDOT = 394
928028
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 13304
39049098
00016717 00000-0 10270-3 0 9088
2 25544 51
6491 153
5090 0001291 99
4547 260
6749 15
49697162 15833
Satellite: ISS
Catalog Number: 25544
Epoch time: 13304
39049098 = yrday
fracday
Element set: 908
Inclination: 51
6491 deg
RA of node: 153
5090 deg
Eccentricity:
0001291
Arg of perigee: 99
4547 deg
Mean anomaly: 260
6749 deg
Mean motion: 15
49697162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1583
Checksum: 335
Coasting Arc #10 (Orbit 1598)
---------------------------------------
Vector Time (GMT): 2013/305/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 903298
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1559398
21 A = 6790289
66 meter
Y = -3946031
04 meter E =
0003958
Z = 5298235
90 I = 51
81595
XDOT = 6723
366813 Wp = 74
81618
YDOT = -3610
862937 meter/sec RA = 147
57136 deg
ZDOT = -709
005263 TA = 21
95089
MA = 21
93395
Ha = 228
375 n
mi
Hp = 221
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5116135
86 X = -1540895
00
Y = -12946296
06 feet Y = -3963365
34 meter
Z = 17382663
72 Z = 5290705
54
XDOT = 22058
290068 XDOT = 6766
688824
YDOT = -11846
663180 feet/sec YDOT = -3535
435799 meter/sec
ZDOT = -2326
132751 ZDOT = -676
237372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4076957
40 X = 1242656
61
Y = 13350694
66 feet Y = 4069291
73 meter
Z = 17351535
85 Z = 5288748
13
XDOT = -22046
626729 XDOT = -6719
811827
YDOT = 9582
319998 feet/sec YDOT = 2920
691135 meter/sec
ZDOT = -2187
970804 ZDOT = -666
893501
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 13305
42226853
00016717 00000-0 10270-3 0 9090
2 25544 51
6488 148
4001 0001141 102
8616 257
2662 15
49742857 15999
Satellite: ISS
Catalog Number: 25544
Epoch time: 13305
42226853 = yrday
fracday
Element set: 909
Inclination: 51
6488 deg
RA of node: 148
4001 deg
Eccentricity:
0001141
Arg of perigee: 102
8616 deg
Mean anomaly: 257
2662 deg
Mean motion: 15
49742857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1599
Checksum: 313
Coasting Arc #11 (Orbit 1613)
---------------------------------------
Vector Time (GMT): 2013/306/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 903298
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1633024
94 A = 6790434
29 meter
Y = 3968919
96 meter E =
0015502
Z = -5275787
19 I = 51
84171
XDOT = -6466
596779 Wp = 98
00872
YDOT = 3966
812318 meter/sec RA = 142
63050 deg
ZDOT = 982
945674 TA = 181
39425
MA = 181
39858
Ha = 228
301 n
mi
Hp = 221
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5357693
37 X = 1614151
33
Y = 13021390
94 feet Y = 3987075
64 meter
Z = -17309013
09 Z = -5267899
95
XDOT = -21215
868699 XDOT = -6515
248957
YDOT = 13014
476110 feet/sec YDOT = 3894
226746 meter/sec
ZDOT = 3224
887383 ZDOT = 951
412191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4541258
19 X = -1384175
50
Y = -13370364
84 feet Y = -4075287
20 meter
Z = -17276392
93 Z = -5265844
56
XDOT = 21118
757107 XDOT = 6436
997166
YDOT = -11166
529304 feet/sec YDOT = -3403
558132 meter/sec
ZDOT = 3091
848973 ZDOT = 942
395567
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 13306
38954606
00016717 00000-0 10270-3 0 9102
2 25544 51
6486 143
6099 0001126 102
5876 257
5400 15
49748324 16145
Satellite: ISS
Catalog Number: 25544
Epoch time: 13306
38954606 = yrday
fracday
Element set: 910
Inclination: 51
6486 deg
RA of node: 143
6099 deg
Eccentricity:
0001126
Arg of perigee: 102
5876 deg
Mean anomaly: 257
5400 deg
Mean motion: 15
49748324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1614
Checksum: 311
Coasting Arc #12 (Orbit 1629)
---------------------------------------
Vector Time (GMT): 2013/307/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 903298
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1698405
38 A = 6790502
93 meter
Y = -3994251
30 meter E =
0004818
Z = 5218882
77 I = 51
86616
XDOT = 6212
291487 Wp = 65
35790
YDOT = -4305
561144 meter/sec RA = 137
69141 deg
ZDOT = -1270
671364 TA = 36
82616
MA = 36
79307
Ha = 228
256 n
mi
Hp = 221
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5572196
12 X = -1678967
25
Y = -13104499
02 feet Y = -4013135
09 meter
Z = 17122318
79 Z = 5210679
17
XDOT = 20381
533750 XDOT = 6266
148273
YDOT = -14125
856772 feet/sec YDOT = -4235
790261 meter/sec
ZDOT = -4168
869304 ZDOT = -1240
360710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4979231
84 X = 1517669
86
Y = 13384530
76 feet Y = 4079604
97 meter
Z = 17088377
68 Z = 5208537
52
XDOT = -20148
036512 XDOT = -6141
121529
YDOT = 12666
557008 feet/sec YDOT = 3860
766576 meter/sec
ZDOT = -4040
905137 ZDOT = -1231
667886
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 13307
42129030
00016717 00000-0 10270-3 0 9114
2 25544 51
6484 138
5005 0001016 105
3127 254
8136 15
49791707 16308
Satellite: ISS
Catalog Number: 25544
Epoch time: 13307
42129030 = yrday
fracday
Element set: 911
Inclination: 51
6484 deg
RA of node: 138
5005 deg
Eccentricity:
0001016
Arg of perigee: 105
3127 deg
Mean anomaly: 254
8136 deg
Mean motion: 15
49791707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1630
Checksum: 276
Coasting Arc #13 (Orbit 1644)
---------------------------------------
Vector Time (GMT): 2013/308/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 903298
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1784339
62 A = 6790758
48 meter
Y = 4042975
81 meter E =
0014610
Z = -5169095
55 I = 51
88863
XDOT = -5912
996471 Wp = 102
09554
YDOT = 4598
042373 meter/sec RA = 132
75294 deg
ZDOT = 1555
940639 TA = 182
88079
MA = 182
88921
Ha = 228
162 n
mi
Hp = 221
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5854132
61 X = 1764108
38
Y = 13264356
32 feet Y = 4062816
26 meter
Z = -16958974
90 Z = -5160476
31
XDOT = -19399
594721 XDOT = -5971
531889
YDOT = 15085
440857 feet/sec YDOT = 4531
592210 meter/sec
ZDOT = 5104
792124 ZDOT = 1527
072737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5483780
33 X = -1671456
24
Y = -13466661
06 feet Y = -4104638
29 meter
Z = -16923298
73 Z = -5158221
45
XDOT = 18973
462898 XDOT = 5783
111491
YDOT = -13984
984556 feet/sec YDOT = -4262
623293 meter/sec
ZDOT = 4982
830152 ZDOT = 1518
766630
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 13308
38853622
00016717 00000-0 10270-3 0 9122
2 25544 51
6479 133
7096 0000968 105
5092 254
6165 15
49797899 16451
Satellite: ISS
Catalog Number: 25544
Epoch time: 13308
38853622 = yrday
fracday
Element set: 912
Inclination: 51
6479 deg
RA of node: 133
7096 deg
Eccentricity:
0000968
Arg of perigee: 105
5092 deg
Mean anomaly: 254
6165 deg
Mean motion: 15
49797899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1645
Checksum: 347
Coasting Arc #14 (Orbit 1660)
---------------------------------------
Vector Time (GMT): 2013/309/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 903298
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1863893
81 A = 6790963
87 meter
Y = -4095595
93 meter E =
0006036
Z = 5082342
80 I = 51
91029
XDOT = 5621
101676 Wp = 62
37609
YDOT = -4868
219736 meter/sec RA = 127
81664 deg
ZDOT = -1857
156181 TA = 45
57927
MA = 45
52989
Ha = 228
131 n
mi
Hp = 221
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6115137
16 X = -1842646
74
Y = -13436994
53 feet Y = -4116320
43 meter
Z = 16674353
01 Z = 5073339
49
XDOT = 18441
934632 XDOT = 5684
143214
YDOT = -15971
849528 feet/sec YDOT = -4805
008498 meter/sec
ZDOT = -6093
032091 ZDOT = -1829
695545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5970630
33 X = 1819848
13
Y = 13547734
35 feet Y = 4129349
43 meter
Z = 16637074
27 Z = 5070980
24
XDOT = -17782
127846 XDOT = -5419
992568
YDOT = 15194
450885 feet/sec YDOT = 4631
268630 meter/sec
ZDOT = -5976
925007 ZDOT = -1821
766742
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 13309
42024693
00016717 00000-0 10270-3 0 9137
2 25544 51
6482 128
6001 0000872 107
9643 252
1602 15
49838673 16619
Satellite: ISS
Catalog Number: 25544
Epoch time: 13309
42024693 = yrday
fracday
Element set: 913
Inclination: 51
6482 deg
RA of node: 128
6001 deg
Eccentricity:
0000872
Arg of perigee: 107
9643 deg
Mean anomaly: 252
1602 deg
Mean motion: 15
49838673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1661
Checksum: 300
Coasting Arc #15 (Orbit 1675)
---------------------------------------
Vector Time (GMT): 2013/310/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 903298
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1972482
02 A = 6791335
90 meter
Y = 4164459
75 meter E =
0013359
Z = -5001169
63 I = 51
92897
XDOT = -5294
164292 Wp = 106
03829
YDOT = 5087
889512 meter/sec RA = 122
88045 deg
ZDOT = 2149
811428 TA = 184
86663
MA = 184
87963
Ha = 228
038 n
mi
Hp = 221
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6471397
71 X = 1950062
40
Y = 13662925
67 feet Y = 4186392
04 meter
Z = -16408036
83 Z = -4991641
64
XDOT = -17369
305419 XDOT = -5361
108159
YDOT = 16692
550893 feet/sec YDOT = 5028
312451 meter/sec
ZDOT = 7053
187101 ZDOT = 2123
929759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6557121
94 X = -1998610
77
Y = -13669397
11 feet Y = -4166432
24 meter
Z = -16368565
41 Z = -4989138
74
XDOT = 16435
847453 XDOT = 5009
646304
YDOT = -16194
285901 feet/sec YDOT = -4936
018343 meter/sec
ZDOT = 6943
664333 ZDOT = 2116
428889
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 13310
38746120
00016717 00000-0 10270-3 0 9141
2 25544 51
6474 123
8088 0000844 108
9344 251
1898 15
49846135 16764
Satellite: ISS
Catalog Number: 25544
Epoch time: 13310
38746120 = yrday
fracday
Element set: 914
Inclination: 51
6474 deg
RA of node: 123
8088 deg
Eccentricity:
0000844
Arg of perigee: 108
9344 deg
Mean anomaly: 251
1898 deg
Mean motion: 15
49846135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1676
Checksum: 319
Coasting Arc #16 (Orbit 1691)
---------------------------------------
Vector Time (GMT): 2013/311/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 903298
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2076295
76 A = 6791687
83 meter
Y = -4237449
34 meter E =
0007447
Z = 4880133
75 I = 51
94704
XDOT = 4981
081121 Wp = 64
25939
YDOT = -5280
537694 meter/sec RA = 117
94671 deg
ZDOT = -2459
814498 TA = 49
82506
MA = 49
75989
Ha = 228
010 n
mi
Hp = 221
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6811993
97 X = -2052464
16
Y = -13902392
85 feet Y = -4260534
66 meter
Z = 16010937
48 Z = 4870104
90
XDOT = 16342
129661 XDOT = 5051
708382
YDOT = -17324
598733 feet/sec YDOT = -5224
441123 meter/sec
ZDOT = -8070
257540 ZDOT = -2435
444971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7133202
54 X = 2174200
14
Y = 13788635
27 feet Y = 4202776
03 meter
Z = 15969372
77 Z = 4867464
82
XDOT = -15106
966571 XDOT = -4604
603411
YDOT = 17065
376657 feet/sec YDOT = 5201
526805 meter/sec
ZDOT = -7967
044417 ZDOT = -2428
355138
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 13311
41913808
00016717 00000-0 10270-3 0 9156
2 25544 51
6480 118
6994 0000734 111
5752 248
5477 15
49883749 16923
Satellite: ISS
Catalog Number: 25544
Epoch time: 13311
41913808 = yrday
fracday
Element set: 915
Inclination: 51
6480 deg
RA of node: 118
6994 deg
Eccentricity:
0000734
Arg of perigee: 111
5752 deg
Mean anomaly: 248
5477 deg
Mean motion: 15
49883749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1692
Checksum: 333
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