[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 24th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 185 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 19)
---------------------------------------
Vector Time (GMT): 2013/203/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2928788
77 A = 6801373
55 meter
Y = -6115522
16 meter E =
0008679
Z = 480480
76 I = 51
34311
XDOT = 4141
549637 Wp = 56
33638
YDOT = 2457
169011 meter/sec RA = 292
34085 deg
ZDOT = 5956
484037 TA = 308
85686
MA = 308
93427
Ha = 227
187 n
mi
Hp = 222
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9608887
04 X = 2994622
20
Y = -20064049
08 feet Y = -6082402
54 meter
Z = 1576380
46 Z = 494867
54
XDOT = 13587
761277 XDOT = 4084
830887
YDOT = 8061
578119 feet/sec YDOT = 2503
164716 meter/sec
ZDOT = 19542
270462 ZDOT = 5976
465348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19794000
59 X = -6033211
38
Y = 10143859
99 feet Y = 3091848
53 meter
Z = 1637496
94 Z = 499109
07
XDOT = -5086
544379 XDOT = -1550
378727
YDOT = -13130
932649 feet/sec YDOT = -4002
308271 meter/sec
ZDOT = 19625
500664 ZDOT = 5981
852602
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 13203
62754766
00016717 00000-0 10270-3 0 9009
2 25544 51
6506 292
7253 0004384 218
5435 141
5403 15
49957954 200
Satellite: ISS
Catalog Number: 25544
Epoch time: 13203
62754766 = yrday
fracday
Element set: 900
Inclination: 51
6506 deg
RA of node: 292
7253 deg
Eccentricity:
0004384
Arg of perigee: 218
5435 deg
Mean anomaly: 141
5403 deg
Mean motion: 15
49957954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 20
Checksum: 303
Coasting Arc #2 (Orbit 34)
---------------------------------------
Vector Time (GMT): 2013/204/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2639867
28 A = 6801027
48 meter
Y = 6204294
91 meter E =
0011656
Z = -834093
95 I = 51
33119
XDOT = -4155
051919 Wp = 162
09455
YDOT = -2557
978352 meter/sec RA = 287
36790 deg
ZDOT = -5909
578596 TA = 26
95229
MA = 26
89180
Ha = 226
965 n
mi
Hp = 222
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8660981
88 X = -2704997
14
Y = 20355298
25 feet Y = 6174410
14 meter
Z = -2736528
69 Z = -847075
62
XDOT = -13632
060103 XDOT = -4097
432791
YDOT = -8392
317429 feet/sec YDOT = -2604
120175 meter/sec
ZDOT = -19388
381220 ZDOT = -5929
623219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19019413
30 X = 5797117
17
Y = -11283054
37 feet Y = -3439074
97 meter
Z = -2791767
33 Z = -850930
68
XDOT = 5093
913092 XDOT = 1552
624710
YDOT = 13378
328328 feet/sec YDOT = 4077
714474 meter/sec
ZDOT = -19471
869912 ZDOT = -5935
025949
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 13204
59465032
00016717 00000-0 10270-3 0 9012
2 25544 51
6501 287
9349 0004360 221
3535 138
7286 15
50008344 359
Satellite: ISS
Catalog Number: 25544
Epoch time: 13204
59465032 = yrday
fracday
Element set: 901
Inclination: 51
6501 deg
RA of node: 287
9349 deg
Eccentricity:
0004360
Arg of perigee: 221
3535 deg
Mean anomaly: 138
7286 deg
Mean motion: 15
50008344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 35
Checksum: 285
Coasting Arc #3 (Orbit 50)
---------------------------------------
Vector Time (GMT): 2013/205/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2333374
22 A = 6800820
04 meter
Y = -6276493
08 meter E =
0009622
Z = 1164098
01 I = 51
32130
XDOT = 4199
286855 Wp = 62
85521
YDOT = 2649
221182 meter/sec RA = 282
39351 deg
ZDOT = 5833
577370 TA = 309
81847
MA = 309
90312
Ha = 226
904 n
mi
Hp = 222
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7655427
22 X = 2397731
16
Y = -20592168
89 feet Y = -6250040
03 meter
Z = 3819219
18 Z = 1175589
09
XDOT = 13777
187843 XDOT = 4141
013293
YDOT = 8691
670545 feet/sec YDOT = 2695
854163 meter/sec
ZDOT = 19139
033365 ZDOT = 5853
835250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18133586
50 X = -5527117
17
Y = 12387063
76 feet Y = 3775577
03 meter
Z = 3868218
28 Z = 1179032
93
XDOT = -5213
085060 XDOT = -1588
948326
YDOT = -13667
984507 feet/sec YDOT = -4166
001678 meter/sec
ZDOT = 19223
408692 ZDOT = 5859
294969
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 13205
62621936
00016717 00000-0 10270-3 0 9025
2 25544 51
6494 282
8247 0004165 226
4444 133
6361 15
49983284 518
Satellite: ISS
Catalog Number: 25544
Epoch time: 13205
62621936 = yrday
fracday
Element set: 902
Inclination: 51
6494 deg
RA of node: 282
8247 deg
Eccentricity:
0004165
Arg of perigee: 226
4444 deg
Mean anomaly: 133
6361 deg
Mean motion: 15
49983284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 51
Checksum: 307
Coasting Arc #4 (Orbit 65)
---------------------------------------
Vector Time (GMT): 2013/206/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2045590
73 A = 6800248
82 meter
Y = 6299173
34 meter E =
0009355
Z = -1517554
87 I = 51
31455
XDOT = -4268
645530 Wp = 168
62888
YDOT = -2763
458682 meter/sec RA = 277
41839 deg
ZDOT = -5731
884451 TA = 27
99723
MA = 27
94694
Ha = 226
669 n
mi
Hp = 222
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6711255
68 X = -2108505
70
Y = 20666579
21 feet Y = 6275946
52 meter
Z = -4978854
55 Z = -1527644
60
XDOT = -14004
742553 XDOT = -4209
583281
YDOT = -9066
465492 feet/sec YDOT = -2810
862977 meter/sec
ZDOT = -18805
395180 ZDOT = -5752
477364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17174246
40 X = 5234710
30
Y = -13295202
65 feet Y = -4052377
77 meter
Z = -5021980
57 Z = -1530699
68
XDOT = 5381
983608 XDOT = 1640
428604
YDOT = 14069
485099 feet/sec YDOT = 4288
379058 meter/sec
ZDOT = -18891
162478 ZDOT = -5758
026323
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 13206
59330451
00016717 00000-0 10270-3 0 9032
2 25544 51
6497 278
0337 0004171 229
6462 130
4325 15
50040510 669
Satellite: ISS
Catalog Number: 25544
Epoch time: 13206
59330451 = yrday
fracday
Element set: 903
Inclination: 51
6497 deg
RA of node: 278
0337 deg
Eccentricity:
0004171
Arg of perigee: 229
6462 deg
Mean anomaly: 130
4325 deg
Mean motion: 15
50040510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 66
Checksum: 275
Coasting Arc #5 (Orbit 81)
---------------------------------------
Vector Time (GMT): 2013/207/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1747921
35 A = 6799867
29 meter
Y = -6302333
19 meter E =
0010085
Z = 1845138
58 I = 51
30893
XDOT = 4370
859684 Wp = 71
12296
YDOT = 2859
566738 meter/sec RA = 272
44237 deg
ZDOT = 5604
663367 TA = 309
23416
MA = 309
32363
Ha = 226
643 n
mi
Hp = 222
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5734650
09 X = 1809302
46
Y = -20676946
16 feet Y = -6282443
66 meter
Z = 6053604
26 Z = 1853778
66
XDOT = 14340
090828 XDOT = 4311
333024
YDOT = 9381
780636 feet/sec YDOT = 2908
111515 meter/sec
ZDOT = 18388
003173 ZDOT = 5625
751749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16127388
42 X = -4915627
99
Y = 14137882
35 feet Y = 4309226
54 meter
Z = 6090653
86 Z = 1856431
30
XDOT = -5692
054413 XDOT = -1734
938185
YDOT = -14483
453994 feet/sec YDOT = -4414
556777 meter/sec
ZDOT = 18475
835796 ZDOT = 5631
434751
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 13207
62485566
00016717 00000-0 10270-3 0 9046
2 25544 51
6486 272
9231 0003959 234
3105 125
7677 15
50012943 827
Satellite: ISS
Catalog Number: 25544
Epoch time: 13207
62485566 = yrday
fracday
Element set: 904
Inclination: 51
6486 deg
RA of node: 272
9231 deg
Eccentricity:
0003959
Arg of perigee: 234
3105 deg
Mean anomaly: 125
7677 deg
Mean motion: 15
50012943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 82
Checksum: 307
Coasting Arc #6 (Orbit 96)
---------------------------------------
Vector Time (GMT): 2013/208/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1479635
51 A = 6799118
97 meter
Y = 6259745
43 meter E =
0006703
Z = -2191132
10 I = 51
30752
XDOT = -4497
709374 Wp = 173
60178
YDOT = -2966
685580 meter/sec RA = 267
46591 deg
ZDOT = -5446
308912 TA = 30
79980
MA = 30
76049
Ha = 226
416 n
mi
Hp = 222
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4854447
20 X = -1538879
57
Y = 20537222
54 feet Y = 6242868
00 meter
Z = -7188753
60 Z = -2198463
72
XDOT = -14756
264350 XDOT = -4437
744596
YDOT = -9733
220406 feet/sec YDOT = -3016
646422 meter/sec
ZDOT = -17868
467559 ZDOT = -5468
012525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15057606
28 X = 4589558
39
Y = -14770135
97 feet Y = -4501937
44 meter
Z = -7220313
17 Z = -2200751
45
XDOT = 6080
393571 XDOT = 1853
303960
YDOT = 14964
831723 feet/sec YDOT = 4561
280709 meter/sec
ZDOT = -17958
865066 ZDOT = -5473
862072
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 13208
59192394
00016717 00000-0 10270-3 0 9058
2 25544 51
6495 268
1318 0004043 237
8350 122
2409 15
50065908 975
Satellite: ISS
Catalog Number: 25544
Epoch time: 13208
59192394 = yrday
fracday
Element set: 905
Inclination: 51
6495 deg
RA of node: 268
1318 deg
Eccentricity:
0004043
Arg of perigee: 237
8350 deg
Mean anomaly: 122
2409 deg
Mean motion: 15
50065908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 97
Checksum: 307
Coasting Arc #7 (Orbit 112)
---------------------------------------
Vector Time (GMT): 2013/209/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1209872
08 A = 6798547
88 meter
Y = -6197215
50 meter E =
0009964
Z = 2508942
44 I = 51
30661
XDOT = 4656
302915 Wp = 80
67506
YDOT = 3047
667284 meter/sec RA = 262
48903 deg
ZDOT = 5266
134407 TA = 307
56147
MA = 307
65194
Ha = 226
392 n
mi
Hp = 222
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3969396
58 X = 1266893
12
Y = -20332071
86 feet Y = -6183367
19 meter
Z = 8231438
44 Z = 2514958
16
XDOT = 15276
584368 XDOT = 4596
295956
YDOT = 9998
908411 feet/sec YDOT = 3099
401346 meter/sec
ZDOT = 17277
343854 ZDOT = 5288
608425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13933369
50 X = -4246891
02
Y = 15316041
96 feet Y = 4668329
59 meter
Z = 8257475
84 Z = 2516878
64
XDOT = -6624
792619 XDOT = -2019
236790
YDOT = -15420
973401 feet/sec YDOT = -4700
312693 meter/sec
ZDOT = 17370
959948 ZDOT = 5294
668592
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 13209
62345740
00016717 00000-0 10270-3 0 9069
2 25544 51
6484 263
0210 0003837 242
5444 117
5317 15
50047621 1131
Satellite: ISS
Catalog Number: 25544
Epoch time: 13209
62345740 = yrday
fracday
Element set: 906
Inclination: 51
6484 deg
RA of node: 263
0210 deg
Eccentricity:
0003837
Arg of perigee: 242
5444 deg
Mean anomaly: 117
5317 deg
Mean motion: 15
50047621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 113
Checksum: 274
Coasting Arc #8 (Orbit 127)
---------------------------------------
Vector Time (GMT): 2013/210/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -979023
22 A = 6797686
02 meter
Y = 6095935
46 meter E =
0003827
Z = -2839424
44 I = 51
30994
XDOT = -4835
591277 Wp = 172
84930
YDOT = -3127
133843 meter/sec RA = 257
51217 deg
ZDOT = -5050
785078 TA = 39
51543
MA = 39
48753
Ha = 226
194 n
mi
Hp = 222
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3212018
44 X = -1033323
49
Y = 19999788
24 feet Y = 6084683
90 meter
Z = -9315696
99 Z = -2844312
06
XDOT = -15864
800778 XDOT = -4775
728447
YDOT = -10259
625469 feet/sec YDOT = -3180
873573 meter/sec
ZDOT = -16570
817185 ZDOT = -5074
130476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12840624
48 X = 3913822
34
Y = -15653424
94 feet Y = -4771163
92 meter
Z = -9336993
79 Z = -2845915
71
XDOT = 7260
993108 XDOT = 2213
150699
YDOT = 15889
749460 feet/sec YDOT = 4843
195636 meter/sec
ZDOT = -16668
075993 ZDOT = -5080
429563
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 13210
59050959
00016717 00000-0 10270-3 0 9073
2 25544 51
6493 258
2298 0003973 246
2202 113
8532 15
50086405 1284
Satellite: ISS
Catalog Number: 25544
Epoch time: 13210
59050959 = yrday
fracday
Element set: 907
Inclination: 51
6493 deg
RA of node: 258
2298 deg
Eccentricity:
0003973
Arg of perigee: 246
2202 deg
Mean anomaly: 113
8532 deg
Mean motion: 15
50086405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 128
Checksum: 301
Coasting Arc #9 (Orbit 143)
---------------------------------------
Vector Time (GMT): 2013/211/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 755201
16 A = 6796939
40 meter
Y = -5976736
07 meter E =
0009238
Z = 3139707
61 I = 51
31387
XDOT = 5042
418241 Wp = 91
37049
YDOT = 3174
258071 meter/sec RA = 252
53511 deg
ZDOT = 4817
093171 TA = 304
93495
MA = 305
02170
Ha = 226
145 n
mi
Hp = 222
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2477694
09 X = 806726
47
Y = -19608714
13 feet Y = -5968003
00 meter
Z = 10300877
99 Z = 3143501
12
XDOT = 16543
366934 XDOT = 4983
148293
YDOT = 10414
232515 feet/sec YDOT = 3230
313934 meter/sec
ZDOT = 15804
111452 ZDOT = 4841
444786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11732387
01 X = -3576031
56
Y = 15894888
44 feet Y = 4844762
00 meter
Z = 10317574
40 Z = 3144796
68
XDOT = -8050
893366 XDOT = -2453
912298
YDOT = -16293
748967 feet/sec YDOT = -4966
334685 meter/sec
ZDOT = 15905
583694 ZDOT = 4848
021910
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 13211
62202544
00016717 00000-0 10270-3 0 9088
2 25544 51
6482 253
1190 0003827 251
2906 108
7829 15
50084568 1440
Satellite: ISS
Catalog Number: 25544
Epoch time: 13211
62202544 = yrday
fracday
Element set: 908
Inclination: 51
6482 deg
RA of node: 253
1190 deg
Eccentricity:
0003827
Arg of perigee: 251
2906 deg
Mean anomaly: 108
7829 deg
Mean motion: 15
50084568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 144
Checksum: 292
Coasting Arc #10 (Orbit 158)
---------------------------------------
Vector Time (GMT): 2013/212/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -577503
94 A = 6796026
55 meter
Y = 5828890
01 meter E =
0001455
Z = -3446300
42 I = 51
32131
XDOT = -5262
470255 Wp = 128
45859
YDOT = -3207
938703 meter/sec RA = 247
55834 deg
ZDOT = -4546
090727 TA = 92
05131
MA = 92
03465
Ha = 226
008 n
mi
Hp = 222
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1894697
96 X = -625899
90
Y = 19123654
87 feet Y = 5822161
61 meter
Z = -11306759
90 Z = -3449223
04
XDOT = -17265
322358 XDOT = -5204
123804
YDOT = -10524
733278 feet/sec YDOT = -3266
460461 meter/sec
ZDOT = -14914
995823 ZDOT = -4571
513567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10708110
14 X = 3263831
97
Y = -15948219
31 feet Y = -4861017
24 meter
Z = -11319785
93 Z = -3450270
75
XDOT = 8927
789138 XDOT = 2721
190129
YDOT = 16650
905653 feet/sec YDOT = 5075
196043 meter/sec
ZDOT = -15020
957775 ZDOT = -4578
387930
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 13212
58906209
00016717 00000-0 10270-3 0 9094
2 25544 51
6483 248
3279 0003931 254
9654 105
1062 15
50105707 1596
Satellite: ISS
Catalog Number: 25544
Epoch time: 13212
58906209 = yrday
fracday
Element set: 909
Inclination: 51
6483 deg
RA of node: 248
3279 deg
Eccentricity:
0003931
Arg of perigee: 254
9654 deg
Mean anomaly: 105
1062 deg
Mean motion: 15
50105707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 159
Checksum: 304
Coasting Arc #11 (Orbit 174)
---------------------------------------
Vector Time (GMT): 2013/213/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 414775
80 A = 6795155
77 meter
Y = -5667271
88 meter E =
0007985
Z = 3720997
94 I = 51
33010
XDOT = 5503
342096 Wp = 103
29504
YDOT = 3205
803474 meter/sec RA = 242
58164 deg
ZDOT = 4259
609653 TA = 301
26486
MA = 301
34305
Ha = 225
924 n
mi
Hp = 222
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1360812
98 X = 460042
25
Y = -18593411
69 feet Y = -5662380
75 meter
Z = 12207998
48 Z = 3723122
43
XDOT = 18055
584303 XDOT = 5446
393301
YDOT = 10517
727933 feet/sec YDOT = 3267
026623 meter/sec
ZDOT = 13975
097287 ZDOT = 4286
205966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9709031
14 X = -2959312
69
Y = 15908035
44 feet Y = 4848769
20 meter
Z = 12217656
07 Z = 3723941
57
XDOT = -9938
827894 XDOT = -3029
354742
YDOT = -16908
203898 feet/sec YDOT = -5153
620548 meter/sec
ZDOT = 14085
984309 ZDOT = 4293
408017
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 13213
62056026
00016717 00000-0 10270-3 0 9105
2 25544 51
6473 243
2171 0003899 260
3031 99
7680 15
50120022 1752
Satellite: ISS
Catalog Number: 25544
Epoch time: 13213
62056026 = yrday
fracday
Element set: 910
Inclination: 51
6473 deg
RA of node: 243
2171 deg
Eccentricity:
0003899
Arg of perigee: 260
3031 deg
Mean anomaly: 99
7680 deg
Mean motion: 15
50120022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 175
Checksum: 271
Coasting Arc #12 (Orbit 189)
---------------------------------------
Vector Time (GMT): 2013/214/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -302014
65 A = 6794249
61 meter
Y = 5489668
16 meter E =
0003146
Z = -3995344
84 I = 51
34165
XDOT = -5746
760244 Wp = 58
68768
YDOT = -3180
225708 meter/sec RA = 237
60514 deg
ZDOT = -3935
975749 TA = 170
14759
MA = 170
14142
Ha = 225
882 n
mi
Hp = 222
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -990861
72 X = -343970
85
Y = 18010722
31 feet Y = 5486056
52 meter
Z = -13108086
75 Z = -3996913
52
XDOT = -18854
200275 XDOT = -5691
651532
YDOT = -10433
811377 feet/sec YDOT = -3244
181223 meter/sec
ZDOT = -12913
306264 ZDOT = -3963
758946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8838118
50 X = 2693858
52
Y = -15718274
18 feet Y = -4790929
97 meter
Z = -13115387
21 Z = -3997570
02
XDOT = 11012
322069 XDOT = 3356
555767
YDOT = 17061
719462 feet/sec YDOT = 5200
412092 meter/sec
ZDOT = -13029
180084 ZDOT = -3971
294090
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 13214
58758140
00016717 00000-0 10270-3 0 9118
2 25544 51
6468 238
4256 0003902 264
0524 96
0182 15
50126637 1901
Satellite: ISS
Catalog Number: 25544
Epoch time: 13214
58758140 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 238
4256 deg
Eccentricity:
0003902
Arg of perigee: 264
0524 deg
Mean anomaly: 96
0182 deg
Mean motion: 15
50126637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 190
Checksum: 293
Coasting Arc #13 (Orbit 205)
---------------------------------------
Vector Time (GMT): 2013/215/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 210944
42 A = 6793332
69 meter
Y = -5304138
36 meter E =
0006340
Z = 4236158
07 I = 51
35531
XDOT = 6002
587531 Wp = 116
69975
YDOT = 3118
543886 meter/sec RA = 232
62928 deg
ZDOT = 3598
876066 TA = 296
29904
MA = 296
36416
Ha = 225
775 n
mi
Hp = 222
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 692074
88 X = 249663
02
Y = -17402028
74 feet Y = -5301563
22 meter
Z = 13898156
41 Z = 4237276
52
XDOT = 19693
528645 XDOT = 5949
787106
YDOT = 10231
443194 feet/sec YDOT = 3185
373171 meter/sec
ZDOT = 11807
336173 ZDOT = 3627
907541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8030465
44 X = -2447685
87
Y = 15448997
59 feet Y = 4708854
46 meter
Z = 13903539
90 Z = 4237798
96
XDOT = -12185
716810 XDOT = -3714
206484
YDOT = -17089
980904 feet/sec YDOT = -5209
026179 meter/sec
ZDOT = 11928
460679 ZDOT = 3635
794815
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 13215
61906175
00016717 00000-0 10270-3 0 9127
2 25544 51
6460 233
3147 0003994 269
3043 90
7650 15
50152368 2060
Satellite: ISS
Catalog Number: 25544
Epoch time: 13215
61906175 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 233
3147 deg
Eccentricity:
0003994
Arg of perigee: 269
3043 deg
Mean anomaly: 90
7650 deg
Mean motion: 15
50152368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 206
Checksum: 291
Coasting Arc #14 (Orbit 220)
---------------------------------------
Vector Time (GMT): 2013/216/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -169562
30 A = 6792491
47 meter
Y = 5116864
65 meter E =
0005982
Z = -4470126
92 I = 51
37139
XDOT = -6247
920190 Wp = 54
59219
YDOT = -3026
682349 meter/sec RA = 227
65340 deg
ZDOT = -3227
250207 TA = 182
74987
MA = 182
75316
Ha = 225
836 n
mi
Hp = 222
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -556306
76 X = -205053
35
Y = 16787613
67 feet Y = 5114770
28 meter
Z = -14665770
75 Z = -4471036
57
XDOT = -20498
425820 XDOT = -6197
934008
YDOT = -9930
060199 feet/sec YDOT = -3096
270890 meter/sec
ZDOT = -10588
091230 ZDOT = -3257
480198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7380960
72 X = 2249716
83
Y = -15083883
55 feet Y = -4597567
71 meter
Z = -14670247
35 Z = -4471491
39
XDOT = 13378
741135 XDOT = 4077
840298
YDOT = 16968
106448 feet/sec YDOT = 5171
878845 meter/sec
ZDOT = -10714
263536 ZDOT = -3265
707526
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 13216
58606694
00016717 00000-0 10270-3 0 9138
2 25544 51
6455 228
5226 0003900 273
3351 86
7353 15
50150554 2219
Satellite: ISS
Catalog Number: 25544
Epoch time: 13216
58606694 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 228
5226 deg
Eccentricity:
0003900
Arg of perigee: 273
3351 deg
Mean anomaly: 86
7353 deg
Mean motion: 15
50150554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 221
Checksum: 291
Coasting Arc #15 (Orbit 236)
---------------------------------------
Vector Time (GMT): 2013/217/13:32:12
395
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 154752
49 A = 6791617
26 meter
Y = -4928701
33 meter E =
0004433
Z = 4668668
30 I = 51
38984
XDOT = 6496
386133 Wp = 132
28598
YDOT = 2901
697972 meter/sec RA = 222
67901 deg
ZDOT = 2843
318540 TA = 289
33734
MA = 289
38527
Ha = 225
736 n
mi
Hp = 222
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 507718
14 X = 187176
15
Y = -16170279
95 feet Y = -4926789
67 meter
Z = 15317153
21 Z = 4669498
63
XDOT = 21313
602798 XDOT = 6449
644107
YDOT = 9520
006469 feet/sec YDOT = 2974
083218 meter/sec
ZDOT = 9328
472901 ZDOT = 2874
763318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6825954
85 X = -2080551
04
Y = 14663427
01 feet Y = 4469412
55 meter
Z = 15321265
04 Z = 4669921
58
XDOT = -14626
654303 XDOT = -4458
204232
YDOT = -16708
964702 feet/sec YDOT = -5092
892441 meter/sec
ZDOT = 9459
766130 ZDOT = 2883
336716
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 13217
61752931
00016717 00000-0 10270-3 0 9140
2 25544 51
6452 223
4116 0004071 278
1798 81
8890 15
50182684 2374
Satellite: ISS
Catalog Number: 25544
Epoch time: 13217
61752931 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 223
4116 deg
Eccentricity:
0004071
Arg of perigee: 278
1798 deg
Mean anomaly: 81
8890 deg
Mean motion: 15
50182684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 237
Checksum: 308
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