[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 21st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 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
There are no maneuvers
Coasting Arc #1 (Orbit 917)
---------------------------------------
Vector Time (GMT): 2013/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2488387
65 A = 6789610
15 meter
Y = -3789796
80 meter E =
0015047
Z = -5067600
03 I = 51
67175
XDOT = 7097
022916 Wp = 97
45015
YDOT = 2156
530347 meter/sec RA = 5
37441 deg
ZDOT = 1875
037392 TA = 190
73845
MA = 190
77061
Ha = 227
858 n
mi
Hp = 219
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8164001
47 X = 2555198
01
Y = -12433716
53 feet Y = -3761597
20 meter
Z = -16625984
36 Z = -5055348
91
XDOT = 23284
195917 XDOT = 7063
272252
YDOT = 7075
230797 feet/sec YDOT = 2235
705314 meter/sec
ZDOT = 6151
697480 ZDOT = 1909
431712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8958407
69 X = -2730522
66
Y = 11946578
85 feet Y = 3641317
23 meter
Z = -16574008
81 Z = -5051757
89
XDOT = -21936
120662 XDOT = -6686
129578
YDOT = -7728
182425 feet/sec YDOT = -2355
550003 meter/sec
ZDOT = 6295
676739 ZDOT = 1918
922270
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 13261
51279454
00016717 00000-0 10270-3 0 9007
2 25544 51
6508 5
8626 0002621 64
6244 295
5178 15
50345414 9188
Satellite: ISS
Catalog Number: 25544
Epoch time: 13261
51279454 = yrday
fracday
Element set: 900
Inclination: 51
6508 deg
RA of node: 5
8626 deg
Eccentricity:
0002621
Arg of perigee: 64
6244 deg
Mean anomaly: 295
5178 deg
Mean motion: 15
50345414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 918
Checksum: 299
Coasting Arc #2 (Orbit 933)
---------------------------------------
Vector Time (GMT): 2013/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2700597
70 A = 6790264
56 meter
Y = 3851408
16 meter E =
0009591
Z = 4891557
98 I = 51
64367
XDOT = -7035
198401 Wp = 60
61082
YDOT = -1921
319897 meter/sec RA =
41643 deg
ZDOT = -2363
223901 TA = 52
58115
MA = 52
49390
Ha = 227
937 n
mi
Hp = 219
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8860228
67 X = -2767226
19
Y = 12635853
56 feet Y = 3820836
52 meter
Z = 16048418
56 Z = 4878276
31
XDOT = -23081
359583 XDOT = -7001
710981
YDOT = -6303
542968 feet/sec YDOT = -1999
805054 meter/sec
ZDOT = -7753
359254 ZDOT = -2397
318706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9451649
68 X = 2880862
82
Y = -12273499
27 feet Y = -3740962
58 meter
Z = 15992114
29 Z = 4874396
44
XDOT = 21870
923213 XDOT = 6666
257395
YDOT = 6519
293617 feet/sec YDOT = 1987
080694 meter/sec
ZDOT = -7896
106363 ZDOT = -2406
733219
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 13262
54414849
00016717 00000-0 10270-3 0 9011
2 25544 51
6511
7509 0002685 65
5260 294
6170 15
50358652 9342
Satellite: ISS
Catalog Number: 25544
Epoch time: 13262
54414849 = yrday
fracday
Element set: 901
Inclination: 51
6511 deg
RA of node:
7509 deg
Eccentricity:
0002685
Arg of perigee: 65
5260 deg
Mean anomaly: 294
6170 deg
Mean motion: 15
50358652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 934
Checksum: 297
Coasting Arc #3 (Orbit 948)
---------------------------------------
Vector Time (GMT): 2013/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2892525
57 A = 6790939
65 meter
Y = -3967390
30 meter E =
0012774
Z = -4703484
59 I = 51
61546
XDOT = 6907
486939 Wp = 101
16176
YDOT = 1694
406626 meter/sec RA = 355
45797 deg
ZDOT = 2822
810351 TA = 196
89142
MA = 196
93400
Ha = 227
820 n
mi
Hp = 219
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9489913
30 X = 2959523
23
Y = -13016372
39 feet Y = -3934670
29 meter
Z = -15431379
90 Z = -4689269
59
XDOT = 22662
358723 XDOT = 6874
313791
YDOT = 5559
076858 feet/sec YDOT = 1771
465448 meter/sec
ZDOT = 9261
188817 ZDOT = 2856
285696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9873293
66 X = -3009379
91
Y = 12800696
21 feet Y = 3901652
20 meter
Z = -15371146
32 Z = -4685125
40
XDOT = -21541
442054 XDOT = -6565
831538
YDOT = -5342
163901 feet/sec YDOT = -1628
291557 meter/sec
ZDOT = 9401
360256 ZDOT = 2865
534606
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 13263
51102512
00016717 00000-0 10270-3 0 9021
2 25544 51
6510 355
9598 0002703 69
0683 291
0757 15
50402620 9496
Satellite: ISS
Catalog Number: 25544
Epoch time: 13263
51102512 = yrday
fracday
Element set: 902
Inclination: 51
6510 deg
RA of node: 355
9598 deg
Eccentricity:
0002703
Arg of perigee: 69
0683 deg
Mean anomaly: 291
0757 deg
Mean motion: 15
50402620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 949
Checksum: 291
Coasting Arc #4 (Orbit 964)
---------------------------------------
Vector Time (GMT): 2013/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3093317
72 A = 6791856
48 meter
Y = 4091324
85 meter E =
0012044
Z = 4444819
74 I = 51
58797
XDOT = -6754
647457 Wp = 69
27753
YDOT = -1516
851463 meter/sec RA = 350
49648 deg
ZDOT = -3293
195875 TA = 54
02381
MA = 53
91218
Ha = 227
876 n
mi
Hp = 219
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10148680
19 X = -3160429
85
Y = 13422981
80 feet Y = 4056358
74 meter
Z = 14582741
93 Z = 4429628
99
XDOT = -22160
916855 XDOT = -6721
186055
YDOT = -4976
546795 feet/sec YDOT = -1592
199558 meter/sec
ZDOT = -10804
448410 ZDOT = -3325
928184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10307185
61 X = 3141630
17
Y = -13371855
24 feet Y = -4075741
48 meter
Z = 14518399
51 Z = 4425208
17
XDOT = 21092
692780 XDOT = 6429
052759
YDOT = 4338
026934 feet/sec YDOT = 1322
230609 meter/sec
ZDOT = -10941
519633 ZDOT = -3334
975184
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 13264
54234157
00016717 00000-0 10270-3 0 9037
2 25544 51
6509 350
8478 0002754 69
3175 290
8271 15
50419289 9655
Satellite: ISS
Catalog Number: 25544
Epoch time: 13264
54234157 = yrday
fracday
Element set: 903
Inclination: 51
6509 deg
RA of node: 350
8478 deg
Eccentricity:
0002754
Arg of perigee: 69
3175 deg
Mean anomaly: 290
8271 deg
Mean motion: 15
50419289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 965
Checksum: 326
Coasting Arc #5 (Orbit 979)
---------------------------------------
Vector Time (GMT): 2013/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3255178
86 A = 6792748
59 meter
Y = -4263658
07 meter E =
0010013
Z = -4177012
34 I = 51
56046
XDOT = 6548
534730 Wp = 99
51579
YDOT = 1360
461396 meter/sec RA = 345
53445 deg
ZDOT = 3720
661040 TA = 208
82009
MA = 208
87544
Ha = 227
784 n
mi
Hp = 219
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10679720
68 X = 3322905
12
Y = -13988379
51 feet Y = -4226878
40 meter
Z = -13704108
73 Z = -4161033
80
XDOT = 21484
693997 XDOT = 6514
760873
YDOT = 4463
456022 feet/sec YDOT = 1433
502860 meter/sec
ZDOT = 12206
893175 ZDOT = 3752
391399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10594331
46 X = -3229152
23
Y = 14118834
55 feet Y = 4303420
77 meter
Z = -13636438
05 Z = -4156386
32
XDOT = -20431
417200 XDOT = -6227
495963
YDOT = -3432
094739 feet/sec YDOT = -1046
102476 meter/sec
ZDOT = 12339
777067 ZDOT = 3761
164050
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 13265
50918332
00016717 00000-0 10270-3 0 9049
2 25544 51
6503 346
0562 0002775 73
3071 286
8384 15
50455042 9807
Satellite: ISS
Catalog Number: 25544
Epoch time: 13265
50918332 = yrday
fracday
Element set: 904
Inclination: 51
6503 deg
RA of node: 346
0562 deg
Eccentricity:
0002775
Arg of perigee: 73
3071 deg
Mean anomaly: 286
8384 deg
Mean motion: 15
50455042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 980
Checksum: 300
Coasting Arc #6 (Orbit 995)
---------------------------------------
Vector Time (GMT): 2013/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3419524
99 A = 6793809
29 meter
Y = 4436451
83 meter E =
0014199
Z = 3834405
72 I = 51
53463
XDOT = -6318
599254 Wp = 80
25624
YDOT = -1268
591905 meter/sec RA = 340
56969 deg
ZDOT = -4151
663415 TA = 53
57048
MA = 53
43966
Ha = 227
794 n
mi
Hp = 219
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11218914
02 X = -3487506
94
Y = 14555288
16 feet Y = 4397832
80 meter
Z = 12580071
25 Z = 3817628
22
XDOT = -20730
312512 XDOT = -6283
776072
YDOT = -4162
046932 feet/sec YDOT = -1339
056199 meter/sec
ZDOT = -13620
942961 ZDOT = -4182
274242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10865258
01 X = 3311730
64
Y = -14881165
75 feet Y = -4535779
32 meter
Z = 12509025
22 Z = 3812750
89
XDOT = 19673
319556 XDOT = 5996
427801
YDOT = 2763
761894 feet/sec YDOT = 842
394625 meter/sec
ZDOT = -13749
138925 ZDOT = -4190
737544
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 13266
54046211
00016717 00000-0 10270-3 0 9053
2 25544 51
6502 340
9437 0002804 72
6990 287
4468 15
50482008 9964
Satellite: ISS
Catalog Number: 25544
Epoch time: 13266
54046211 = yrday
fracday
Element set: 905
Inclination: 51
6502 deg
RA of node: 340
9437 deg
Eccentricity:
0002804
Arg of perigee: 72
6990 deg
Mean anomaly: 287
4468 deg
Mean motion: 15
50482008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 996
Checksum: 311
Coasting Arc #7 (Orbit 1010)
---------------------------------------
Vector Time (GMT): 2013/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3529359
83 A = 6794822
57 meter
Y = -4646392
81 meter E =
0007765
Z = -3488206
84 I = 51
50861
XDOT = 6054
352373 Wp = 86
23083
YDOT = 1207
068154 meter/sec RA = 335
60434 deg
ZDOT = 4527
163192 TA = 232
80570
MA = 232
87660
Ha = 227
754 n
mi
Hp = 219
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11579264
52 X = 3597999
44
Y = -15244070
90 feet Y = -4606541
78 meter
Z = -11444248
18 Z = -3470894
24
XDOT = 19863
360805 XDOT = 6018
412733
YDOT = 3960
197356 feet/sec YDOT = 1274
571205 meter/sec
ZDOT = 14852
897613 ZDOT = 4556
487592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10928554
25 X = -3331023
33
Y = 15770243
44 feet Y = 4806770
20 meter
Z = -11370928
05 Z = -3465858
87
XDOT = -18783
557364 XDOT = -5725
228285
YDOT = -2240
684990 feet/sec YDOT = -682
960785 meter/sec
ZDOT = 14975
703273 ZDOT = 4564
594358
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 13267
50726919
00016717 00000-0 10270-3 0 9061
2 25544 51
6493 336
1514 0002853 77
1903 282
9567 15
50502278 10115
Satellite: ISS
Catalog Number: 25544
Epoch time: 13267
50726919 = yrday
fracday
Element set: 906
Inclination: 51
6493 deg
RA of node: 336
1514 deg
Eccentricity:
0002853
Arg of perigee: 77
1903 deg
Mean anomaly: 282
9567 deg
Mean motion: 15
50502278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1011
Checksum: 310
Coasting Arc #8 (Orbit 1026)
---------------------------------------
Vector Time (GMT): 2013/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3637130
91 A = 6795864
13 meter
Y = 4844951
73 meter E =
0015802
Z = 3064717
77 I = 51
48516
XDOT = -5771
483901 Wp = 92
28647
YDOT = -1222
843460 meter/sec RA = 330
63693 deg
ZDOT = -4895
021021 TA = 52
47987
MA = 52
33636
Ha = 227
717 n
mi
Hp = 219
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11932844
19 X = -3705925
60
Y = 15895510
94 feet Y = 4803894
61 meter
Z = 10054848
31 Z = 3046881
29
XDOT = -18935
314636 XDOT = -5733
601957
YDOT = -4011
953610 feet/sec YDOT = -1287
172430 meter/sec
ZDOT = -16059
780253 ZDOT = -4922
966491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10958434
15 X = 3340130
73
Y = -16627875
11 feet Y = -5068176
33 meter
Z = 9979303
76 Z = 3041691
79
XDOT = 17839
990557 XDOT = 5437
629122
YDOT = 2006
493979 feet/sec YDOT = 611
579365 meter/sec
ZDOT = -16176
797701 ZDOT = -4930
687939
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 13268
53851040
00016717 00000-0 10270-3 0 9070
2 25544 51
6496 331
0386 0002886 76
2585 283
8887 15
50544098 10279
Satellite: ISS
Catalog Number: 25544
Epoch time: 13268
53851040 = yrday
fracday
Element set: 907
Inclination: 51
6496 deg
RA of node: 331
0386 deg
Eccentricity:
0002886
Arg of perigee: 76
2585 deg
Mean anomaly: 283
8887 deg
Mean motion: 15
50544098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1027
Checksum: 333
Coasting Arc #9 (Orbit 1041)
---------------------------------------
Vector Time (GMT): 2013/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3679932
61 A = 6796855
88 meter
Y = -5065372
54 meter E =
0007790
Z = -2645892
10 I = 51
46142
XDOT = 5477
729630 Wp = 62
90520
YDOT = 1272
503856 meter/sec RA = 325
66880 deg
ZDOT = 5197
668261 TA = 267
24921
MA = 267
33837
Ha = 227
733 n
mi
Hp = 219
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12073269
71 X = 3749154
32
Y = -16618676
33 feet Y = -5023834
36 meter
Z = -8680748
35 Z = -2627846
68
XDOT = 17971
553903 XDOT = 5437
844070
YDOT = 4174
881417 feet/sec YDOT = 1333
536694 meter/sec
ZDOT = 17052
717393 ZDOT = 5224
181761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10743797
06 X = -3274709
34
Y = 17545270
41 feet Y = 5347798
42 meter
Z = -8604298
18 Z = -2622590
09
XDOT = -16864
970129 XDOT = -5140
442895
YDOT = -1934
879382 feet/sec YDOT = -589
751236 meter/sec
ZDOT = 17163
720431 ZDOT = 5231
501987
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 13269
50528285
00016717 00000-0 10270-3 0 9081
2 25544 51
6489 326
2458 0002960 80
7536 279
3949 15
50546021 10420
Satellite: ISS
Catalog Number: 25544
Epoch time: 13269
50528285 = yrday
fracday
Element set: 908
Inclination: 51
6489 deg
RA of node: 326
2458 deg
Eccentricity:
0002960
Arg of perigee: 80
7536 deg
Mean anomaly: 279
3949 deg
Mean motion: 15
50546021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1042
Checksum: 325
Coasting Arc #10 (Orbit 1057)
---------------------------------------
Vector Time (GMT): 2013/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3719553
99 A = 6797699
41 meter
Y = 5258980
25 meter E =
0016594
Z = 2149745
29 I = 51
44038
XDOT = -5174
179823 Wp = 104
51645
YDOT = -1407
556924 meter/sec RA = 320
69930 deg
ZDOT = -5477
720293 TA = 51
60212
MA = 51
45321
Ha = 227
671 n
mi
Hp = 219
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12203261
12 X = -3788527
54
Y = 17253872
21 feet Y = 5217000
35 meter
Z = 7052970
11 Z = 2131508
00
XDOT = -16975
655587 XDOT = -5131
446256
YDOT = -4617
968912 feet/sec YDOT = -1465
179397 meter/sec
ZDOT = -17971
523271 ZDOT = -5502
752185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10497487
70 X = 3199634
25
Y = -18371242
57 feet Y = -5599554
73 meter
Z = 6975691
66 Z = 2126190
82
XDOT = 15895
456679 XDOT = 4844
935196
YDOT = 2179
483877 feet/sec YDOT = 664
306686 meter/sec
ZDOT = -18076
291843 ZDOT = -5509
653754
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 13270
53648665
00016717 00000-0 10270-3 0 9092
2 25544 51
6494 321
1327 0003032 80
8929 279
2565 15
50600463 10584
Satellite: ISS
Catalog Number: 25544
Epoch time: 13270
53648665 = yrday
fracday
Element set: 909
Inclination: 51
6494 deg
RA of node: 321
1327 deg
Eccentricity:
0003032
Arg of perigee: 80
8929 deg
Mean anomaly: 279
2565 deg
Mean motion: 15
50600463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1058
Checksum: 310
Coasting Arc #11 (Orbit 1072)
---------------------------------------
Vector Time (GMT): 2013/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3690498
50 A = 6798482
68 meter
Y = -5457091
62 meter E =
0010219
Z = -1668925
03 I = 51
41936
XDOT = 4884
765539 Wp = 50
36795
YDOT = 1573
395304 meter/sec RA = 315
72897 deg
ZDOT = 5686
652260 TA = 291
32289
MA = 291
43195
Ha = 227
716 n
mi
Hp = 219
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12107934
70 X = 3759353
82
Y = -17903843
91 feet Y = -5415437
28 meter
Z = -5475475
81 Z = -1650829
13
XDOT = 16026
133657 XDOT = 4839
184137
YDOT = 5162
058085 feet/sec YDOT = 1627
765503 meter/sec
ZDOT = 18656
995604 ZDOT = 5710
271223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10000716
92 X = -3048218
52
Y = 19182531
37 feet Y = 5846835
56 meter
Z = -5398768
03 Z = -1645544
49
XDOT = -14999
590387 XDOT = -4571
875150
YDOT = -2569
087366 feet/sec YDOT = -783
057829 meter/sec
ZDOT = 18755
813989 ZDOT = 5716
772104
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 13271
50322401
00016717 00000-0 10270-3 0 9109
2 25544 51
6490 316
3397 0003102 84
4797 275
6708 15
50591207 10735
Satellite: ISS
Catalog Number: 25544
Epoch time: 13271
50322401 = yrday
fracday
Element set: 910
Inclination: 51
6490 deg
RA of node: 316
3397 deg
Eccentricity:
0003102
Arg of perigee: 84
4797 deg
Mean anomaly: 275
6708 deg
Mean motion: 15
50591207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1073
Checksum: 288
Coasting Arc #12 (Orbit 1088)
---------------------------------------
Vector Time (GMT): 2013/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3661792
41 A = 6798966
94 meter
Y = 5610928
93 meter E =
0016296
Z = 1114155
76 I = 51
40040
XDOT = -4596
924239 Wp = 116
12777
YDOT = -1825
554502 meter/sec RA = 310
75745 deg
ZDOT = -5854
986958 TA = 51
75611
MA = 51
60957
Ha = 227
647 n
mi
Hp = 218
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12013754
63 X = -3729675
18
Y = 18408559
50 feet Y = 5569601
00 meter
Z = 3655366
67 Z = 1096201
62
XDOT = -15081
772439 XDOT = -4547
726820
YDOT = -5989
352040 feet/sec YDOT = -1876
685741 meter/sec
ZDOT = -19209
274798 ZDOT = -5877
198770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9498033
48 X = 2895000
61
Y = -19837930
16 feet Y = -6046601
11 meter
Z = 3579239
52 Z = 1090952
21
XDOT = 14175
969700 XDOT = 4320
835565
YDOT = 3268
504862 feet/sec YDOT = 996
240282 meter/sec
ZDOT = -19302
155149 ZDOT = -5883
296889
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 13272
53439034
00016717 00000-0 10270-3 0 9115
2 25544 51
6493 311
2265 0003204 86
9782 273
1736 15
50647699 10898
Satellite: ISS
Catalog Number: 25544
Epoch time: 13272
53439034 = yrday
fracday
Element set: 911
Inclination: 51
6493 deg
RA of node: 311
2265 deg
Eccentricity:
0003204
Arg of perigee: 86
9782 deg
Mean anomaly: 273
1736 deg
Mean motion: 15
50647699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1089
Checksum: 317
Coasting Arc #13 (Orbit 1103)
---------------------------------------
Vector Time (GMT): 2013/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3568262
97 A = 6799336
44 meter
Y = -5752242
84 meter E =
0013248
Z = -587099
89 I = 51
38206
XDOT = 4346
462926 Wp = 51
38197
YDOT = 2099
013228 meter/sec RA = 305
78513 deg
ZDOT = 5950
546225 TA = 302
26862
MA = 302
39691
Ha = 227
678 n
mi
Hp = 218
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11706899
51 X = 3635172
59
Y = -18872187
80 feet Y = -5711966
21 meter
Z = -1926180
75 Z = -569602
36
XDOT = 14260
048971 XDOT = 4293
762032
YDOT = 6886
526340 feet/sec YDOT = 2147
324159 meter/sec
ZDOT = 19522
789453 ZDOT = 5971
532755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8772207
24 X = -2673768
77
Y = 20409306
01 feet Y = 6220756
47 meter
Z = -1851958
13 Z = -564476
84
XDOT = -13519
527537 XDOT = -4120
751993
YDOT = -4062
145283 feet/sec YDOT = -1238
141882 meter/sec
ZDOT = 19610
492194 ZDOT = 5977
278021
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 13273
50109180
00016717 00000-0 10270-3 0 9120
2 25544 51
6490 306
4335 0003245 89
2034 270
9489 15
50645007 11049
Satellite: ISS
Catalog Number: 25544
Epoch time: 13273
50109180 = yrday
fracday
Element set: 912
Inclination: 51
6490 deg
RA of node: 306
4335 deg
Eccentricity:
0003245
Arg of perigee: 89
2034 deg
Mean anomaly: 270
9489 deg
Mean motion: 15
50645007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1104
Checksum: 283
Coasting Arc #14 (Orbit 1119)
---------------------------------------
Vector Time (GMT): 2013/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3483879
67 A = 6799343
02 meter
Y = 5832148
32 meter E =
0014704
Z = -6098
50 I = 51
36501
XDOT = -4109
437812 Wp = 125
88057
YDOT = -2450
429717 meter/sec RA = 300
81120 deg
ZDOT = -5986
022029 TA = 54
18527
MA = 54
04872
Ha = 227
609 n
mi
Hp = 218
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11430051
40 X = -3548807
47
Y = 19134344
89 feet Y = 5792826
33 meter
Z = -20008
21 Z = -23181
42
XDOT = -13482
407520 XDOT = -4052
652540
YDOT = -8039
467575 feet/sec YDOT = -2496
067344 meter/sec
ZDOT = -19639
179886 ZDOT = -6005
847140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8091387
01 X = 2466254
76
Y = -20767535
50 feet Y = -6329944
82 meter
Z = -92492
50 Z = -28191
72
XDOT = 12996
108784 XDOT = 3961
213957
YDOT = 5119
195246 feet/sec YDOT = 1560
330711 meter/sec
ZDOT = -19721
962312 ZDOT = -6011
254113
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 13274
53222007
00016717 00000-0 10270-3 0 9139
2 25544 51
6488 301
3198 0003324 93
8534 266
2997 15
50689806 11206
Satellite: ISS
Catalog Number: 25544
Epoch time: 13274
53222007 = yrday
fracday
Element set: 913
Inclination: 51
6488 deg
RA of node: 301
3198 deg
Eccentricity:
0003324
Arg of perigee: 93
8534 deg
Mean anomaly: 266
2997 deg
Mean motion: 15
50689806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1120
Checksum: 309
Coasting Arc #15 (Orbit 1135)
---------------------------------------
Vector Time (GMT): 2013/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3345785
22 A = 6799140
95 meter
Y = -5885277
93 meter E =
0015599
Z = 558328
38 I = 51
34924
XDOT = 3927
968317 Wp = 59
57993
YDOT = 2808
718281 meter/sec RA = 295
83647 deg
ZDOT = 5951
158652 TA = 306
46141
MA = 306
60507
Ha = 227
585 n
mi
Hp = 218
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10976985
64 X = 3408634
80
Y = -19308654
64 feet Y = -5847511
74 meter
Z = 1831786
03 Z = 574735
52
XDOT = 12887
035162 XDOT = 3867
359349
YDOT = 9214
954991 feet/sec YDOT = 2852
305293 meter/sec
ZDOT = 19524
798726 ZDOT = 5970
092877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7244604
29 X = -2208155
39
Y = 20989856
11 feet Y = 6397708
14 meter
Z = 1901432
90 Z = 579556
75
XDOT = -12706
589425 XDOT = -3872
968457
YDOT = -6194
984985 feet/sec YDOT = -1888
231424 meter/sec
ZDOT = 19603
795247 ZDOT = 5975
236791
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 13275
56332870
00016717 00000-0 10270-3 0 9144
2 25544 51
6484 296
2069 0003323 95
5790 264
5740 15
50711525 11361
Satellite: ISS
Catalog Number: 25544
Epoch time: 13275
56332870 = yrday
fracday
Element set: 914
Inclination: 51
6484 deg
RA of node: 296
2069 deg
Eccentricity:
0003323
Arg of perigee: 95
5790 deg
Mean anomaly: 264
5740 deg
Mean motion: 15
50711525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1136
Checksum: 309
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