[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 31st 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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 1803)
---------------------------------------
Vector Time (GMT): 2014/211/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3710299
68 A = 6788086
41 meter
Y = 2079311
46 meter E =
0010741
Z = -5298891
54 I = 51
29837
XDOT = -3491
211188 Wp = 63
18634
YDOT = -6809
389175 meter/sec RA = 244
19391 deg
ZDOT = -223
080051 TA = 204
64809
MA = 204
69946
Ha = 226
266 n
mi
Hp = 222
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12172899
22 X = -3707535
38
Y = 6821887
99 feet Y = 2037835
98 meter
Z = -17384814
76 Z = -5316908
63
XDOT = -11454
104946 XDOT = -3413
723930
YDOT = -22340
515667 feet/sec YDOT = -6847
996892 meter/sec
ZDOT = -731
889931 ZDOT = -239
851416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10518833
07 X = 3206140
32
Y = 9021938
59 feet Y = 2749886
88 meter
Z = -17461620
50 Z = -5322301
93
XDOT = -16452
380187 XDOT = -5014
685481
YDOT = 17602
122586 feet/sec YDOT = 5365
126964 meter/sec
ZDOT = -801
959500 ZDOT = -244
437256
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 14211
46855137
00016717 00000-0 10270-3 0 9005
2 25544 51
6451 245
0583 0006830 309
9810 50
0740 15
50456387 18041
Satellite: ISS
Catalog Number: 25544
Epoch time: 14211
46855137 = yrday
fracday
Element set: 900
Inclination: 51
6451 deg
RA of node: 245
0583 deg
Eccentricity:
0006830
Arg of perigee: 309
9810 deg
Mean anomaly: 50
0740 deg
Mean motion: 15
50456387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1804
Checksum: 290
Coasting Arc #2 (Orbit 1819)
---------------------------------------
Vector Time (GMT): 2014/212/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3845960
27 A = 6787969
57 meter
Y = -1822103
81 meter E =
0005923
Z = 5290535
79 I = 51
31275
XDOT = 3672
575427 Wp = 336
46300
YDOT = 6714
036134 meter/sec RA = 239
20919 deg
ZDOT = -352
220501 TA = 116
94397
MA = 116
88345
Ha = 226
329 n
mi
Hp = 221
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12617979
90 X = 3840350
24
Y = -5978030
86 feet Y = -1779127
16 meter
Z = 17357400
87 Z = 5309205
04
XDOT = 12049
131977 XDOT = 3598
935533
YDOT = 22027
677606 feet/sec YDOT = 6754
693496 meter/sec
ZDOT = -1155
579072 ZDOT = -334
558767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10042758
99 X = -3061032
94
Y = -9556462
92 feet Y = -2912809
90 meter
Z = 17436933
30 Z = 5314777
27
XDOT = 15586
122809 XDOT = 4750
650232
YDOT = -18383
884846 feet/sec YDOT = -5603
408101 meter/sec
ZDOT = -1081
699356 ZDOT = -329
701964
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 14212
49980598
00016717 00000-0 10270-3 0 9010
2 25544 51
6450 239
9455 0006809 314
4989 45
5605 15
50500473 18207
Satellite: ISS
Catalog Number: 25544
Epoch time: 14212
49980598 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 239
9455 deg
Eccentricity:
0006809
Arg of perigee: 314
4989 deg
Mean anomaly: 45
5605 deg
Mean motion: 15
50500473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1820
Checksum: 321
Coasting Arc #3 (Orbit 1834)
---------------------------------------
Vector Time (GMT): 2014/213/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4010671
29 A = 6788257
58 meter
Y = 1610623
33 meter E =
0010384
Z = -5242668
73 I = 51
33100
XDOT = -3828
029645 Wp = 71
05468
YDOT = -6566
471698 meter/sec RA = 234
22523 deg
ZDOT = 915
948539 TA = 207
73206
MA = 207
78747
Ha = 226
579 n
mi
Hp = 221
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13158370
36 X = -4002916
63
Y = 5284197
28 feet Y = 1565816
75 meter
Z = -17200356
73 Z = -5262132
98
XDOT = -12559
152377 XDOT = -3758
766682
YDOT = -21543
542315 feet/sec YDOT = -6608
891918 meter/sec
ZDOT = 3005
080509 ZDOT = 897
520965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9763414
34 X = 2975888
69
Y = 10143144
25 feet Y = 3091630
37 meter
Z = -17283231
41 Z = -5267928
94
XDOT = -14568
359589 XDOT = -4440
436003
YDOT = 18985
228504 feet/sec YDOT = 5786
697648 meter/sec
ZDOT = 2927
912337 ZDOT = 892
427680
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 14213
46660189
00016717 00000-0 10270-3 0 9020
2 25544 51
6457 235
1519 0006852 318
6831 41
3801 15
50480093 18356
Satellite: ISS
Catalog Number: 25544
Epoch time: 14213
46660189 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 235
1519 deg
Eccentricity:
0006852
Arg of perigee: 318
6831 deg
Mean anomaly: 41
3801 deg
Mean motion: 15
50480093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1835
Checksum: 300
Coasting Arc #4 (Orbit 1850)
---------------------------------------
Vector Time (GMT): 2014/214/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4218006
86 A = 6788576
85 meter
Y = -1395707
17 meter E =
0008112
Z = 5134781
53 I = 51
35078
XDOT = 3941
009664 Wp = 358
28527
YDOT = 6398
218317 meter/sec RA = 229
24304 deg
ZDOT = -1490
351617 TA = 106
18334
MA = 106
09404
Ha = 226
651 n
mi
Hp = 221
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13838605
20 X = 4208357
56
Y = -4579091
77 feet Y = -1348592
65 meter
Z = 16846396
10 Z = 5155248
42
XDOT = 12929
821732 XDOT = 3876
410010
YDOT = 20991
529913 feet/sec YDOT = 6441
928031 meter/sec
ZDOT = -4889
605044 ZDOT = -1471
363800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9551777
55 X = -2911381
80
Y = -10876414
39 feet Y = -3315131
11 meter
Z = 16933496
17 Z = 5161329
63
XDOT = 13516
413095 XDOT = 4119
802711
YDOT = -19399
090211 feet/sec YDOT = -5912
842696 meter/sec
ZDOT = -4810
019082 ZDOT = -1466
093816
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 14214
49784188
00016717 00000-0 10270-3 0 9031
2 25544 51
6450 230
0391 0006809 323
3786 36
6898 15
50525462 18516
Satellite: ISS
Catalog Number: 25544
Epoch time: 14214
49784188 = yrday
fracday
Element set: 903
Inclination: 51
6450 deg
RA of node: 230
0391 deg
Eccentricity:
0006809
Arg of perigee: 323
3786 deg
Mean anomaly: 36
6898 deg
Mean motion: 15
50525462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1851
Checksum: 321
Coasting Arc #5 (Orbit 1865)
---------------------------------------
Vector Time (GMT): 2014/215/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4439035
70 A = 6789262
26 meter
Y = 1242417
15 meter E =
0008918
Z = -4991196
28 I = 51
37507
XDOT = -4018
438899 Wp = 73
99405
YDOT = -6190
545582 meter/sec RA = 224
26272 deg
ZDOT = 2038
384402 TA = 215
89934
MA = 215
95929
Ha = 226
861 n
mi
Hp = 221
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14563765
43 X = -4428353
29
Y = 4076171
74 feet Y = 1192836
76 meter
Z = -16375315
88 Z = -5012734
41
XDOT = -13183
854656 XDOT = -3958
817900
YDOT = -20310
188918 feet/sec YDOT = -6235
149017 meter/sec
ZDOT = 6687
612866 ZDOT = 2019
008256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9571768
51 X = 2917475
04
Y = 11579740
34 feet Y = 3529504
86 meter
Z = -16466944
79 Z = -5019124
77
XDOT = -12386
741256 XDOT = -3775
478735
YDOT = 19608
049507 feet/sec YDOT = 5976
533490 meter/sec
ZDOT = 6606
333358 ZDOT = 2013
610407
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 14215
46462356
00016717 00000-0 10270-3 0 9040
2 25544 51
6462 225
2458 0006902 327
0006 33
0713 15
50504012 18660
Satellite: ISS
Catalog Number: 25544
Epoch time: 14215
46462356 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 225
2458 deg
Eccentricity:
0006902
Arg of perigee: 327
0006 deg
Mean anomaly: 33
0713 deg
Mean motion: 15
50504012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1866
Checksum: 274
Coasting Arc #6 (Orbit 1881)
---------------------------------------
Vector Time (GMT): 2014/216/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4695511
45 A = 6789971
98 meter
Y = -1091858
25 meter E =
0010092
Z = 4782833
23 I = 51
39950
XDOT = 4037
612613 Wp = 18
36833
YDOT = 5973
469690 meter/sec RA = 219
28410 deg
ZDOT = -2589
341728 TA = 97
31449
MA = 97
19977
Ha = 226
943 n
mi
Hp = 221
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15405221
28 X = 4684138
53
Y = -3582212
10 feet Y = -1039413
71 meter
Z = 15691710
06 Z = 4805615
59
XDOT = 13246
760542 XDOT = 3983
093945
YDOT = 19597
997672 feet/sec YDOT = 6018
316107 meter/sec
ZDOT = -8495
215642 ZDOT = -2569
859957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9676367
60 X = -2949356
84
Y = -12388329
09 feet Y = -3775962
71 meter
Z = 15788605
49 Z = 4812366
95
XDOT = 11298
823307 XDOT = 3443
881344
YDOT = -19593
336890 feet/sec YDOT = -5972
049084 meter/sec
ZDOT = -8413
441297 ZDOT = -2564
416907
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 14216
49584854
00016717 00000-0 10270-3 0 9053
2 25544 51
6448 220
1326 0006873 331
6215 28
4560 15
50551708 18822
Satellite: ISS
Catalog Number: 25544
Epoch time: 14216
49584854 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 220
1326 deg
Eccentricity:
0006873
Arg of perigee: 331
6215 deg
Mean anomaly: 28
4560 deg
Mean motion: 15
50551708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1882
Checksum: 309
Coasting Arc #7 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2014/217/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4946537
80 A = 6790980
29 meter
Y = 1012983
98 meter E =
0007020
Z = -4545341
38 I = 51
42808
XDOT = -4017
666483 Wp = 66
12763
YDOT = -5735
181946 meter/sec RA = 214
30856 deg
ZDOT = 3100
720263 TA = 235
02916
MA = 235
09509
Ha = 227
120 n
mi
Hp = 220
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16228798
55 X = -4935417
91
Y = 3323438
27 feet Y = 957730
96 meter
Z = -14912537
32 Z = -4569343
76
XDOT = -13181
320483 XDOT = -3968
297967
YDOT = -18816
213732 feet/sec YDOT = -5779
834165 meter/sec
ZDOT = 10172
966741 ZDOT = 3081
322822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10015851
09 X = 3052831
41
Y = 13078497
82 feet Y = 3986326
14 meter
Z = -15014610
73 Z = -4576453
35
XDOT = -10217
497033 XDOT = -3114
293096
YDOT = 19385
605439 feet/sec YDOT = 5908
732538 meter/sec
ZDOT = 10091
500119 ZDOT = 3075
889236
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 14217
46261565
00016717 00000-0 10270-3 0 9063
2 25544 51
6455 215
3397 0006976 334
9611 25
1201 15
50527237 18976
Satellite: ISS
Catalog Number: 25544
Epoch time: 14217
46261565 = yrday
fracday
Element set: 906
Inclination: 51
6455 deg
RA of node: 215
3397 deg
Eccentricity:
0006976
Arg of perigee: 334
9611 deg
Mean anomaly: 25
1201 deg
Mean motion: 15
50527237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 313
Coasting Arc #8 (Orbit 1912)
---------------------------------------
Vector Time (GMT): 2014/218/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5222363
56 A = 6791968
23 meter
Y = -939635
00 meter E =
0011700
Z = 4239637
23 I = 51
45653
XDOT = 3927
853279 Wp = 37
15117
YDOT = 5501
440609 meter/sec RA = 209
33437 deg
ZDOT = -3604
660549 TA = 89
90062
MA = 89
76655
Ha = 227
212 n
mi
Hp = 220
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17133738
72 X = 5211888
03
Y = -3082791
98 feet Y = -881293
94 meter
Z = 13909570
97 Z = 4264981
01
XDOT = 12886
657739 XDOT = 3883
553102
YDOT = 18049
345829 feet/sec YDOT = 5545
116878 meter/sec
ZDOT = -11826
314136 ZDOT = -3585
687094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10435416
98 X = -3180715
10
Y = -13826097
70 feet Y = -4214194
58 meter
Z = 14017341
69 Z = 4272485
75
XDOT = 9258
812211 XDOT = 2822
085962
YDOT = -18944
674801 feet/sec YDOT = -5774
336879 meter/sec
ZDOT = -11746
597180 ZDOT = -3580
362820
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 14218
49382498
00016717 00000-0 10270-3 0 9077
2 25544 51
6439 210
2260 0006995 339
1242 20
9622 15
50577965 19131
Satellite: ISS
Catalog Number: 25544
Epoch time: 14218
49382498 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 210
2260 deg
Eccentricity:
0006995
Arg of perigee: 339
1242 deg
Mean anomaly: 20
9622 deg
Mean motion: 15
50577965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1913
Checksum: 322
Coasting Arc #9 (Orbit 1927)
---------------------------------------
Vector Time (GMT): 2014/219/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5471980
11 A = 6793164
99 meter
Y = 941002
57 meter E =
0006465
Z = -3913871
89 I = 51
48800
XDOT = -3802
574994 Wp = 41
99880
YDOT = -5267
480230 meter/sec RA = 204
36407 deg
ZDOT = 4058
523851 TA = 270
58249
MA = 270
65658
Ha = 227
363 n
mi
Hp = 220
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17952690
65 X = -5463083
85
Y = 3087278
77 feet Y = 879861
31 meter
Z = -12840787
04 Z = -3940431
99
XDOT = -12475
639745 XDOT = -3763
104949
YDOT = -17281
759284 feet/sec YDOT = -5309
782599 meter/sec
ZDOT = 13315
366965 ZDOT = 4040
147311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11060602
47 X = 3371271
63
Y = 14372889
16 feet Y = 4380856
62 meter
Z = -12953738
21 Z = -3948299
41
XDOT = -8386
449895 XDOT = -2556
189928
YDOT = 18359
593340 feet/sec YDOT = 5596
004050 meter/sec
ZDOT = 13238
133102 ZDOT = 4034
982969
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 14219
46057717
00016717 00000-0 10270-3 0 9089
2 25544 51
6440 205
4329 0007059 342
7633 17
3277 15
50551109 19285
Satellite: ISS
Catalog Number: 25544
Epoch time: 14219
46057717 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 205
4329 deg
Eccentricity:
0007059
Arg of perigee: 342
7633 deg
Mean anomaly: 17
3277 deg
Mean motion: 15
50551109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1928
Checksum: 308
Coasting Arc #10 (Orbit 1943)
---------------------------------------
Vector Time (GMT): 2014/220/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5733703
21 A = 6794267
43 meter
Y = -946255
04 meter E =
0012763
Z = 3518319
99 I = 51
51986
XDOT = 3601
718119 Wp = 54
71474
YDOT = 5053
208663 meter/sec RA = 199
39511 deg
ZDOT = -4491
782109 TA = 83
86405
MA = 83
71864
Ha = 227
466 n
mi
Hp = 220
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18811362
25 X = 5726767
75
Y = -3104511
27 feet Y = -882176
01 meter
Z = 11543044
60 Z = 3546156
13
XDOT = 11816
660497 XDOT = 3566
763537
YDOT = 16578
768579 feet/sec YDOT = 5093
290156 meter/sec
ZDOT = -14736
817942 ZDOT = -4474
370455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11738571
78 X = -3577916
68
Y = -14931984
01 feet Y = -4551268
73 meter
Z = 11661432
35 Z = 3554404
58
XDOT = 7711
100231 XDOT = 2350
343351
YDOT = -17561
432335 feet/sec YDOT = -5352
724576 meter/sec
ZDOT = -14663
632861 ZDOT = -4469
475296
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 14220
49177024
00016717 00000-0 10270-3 0 9099
2 25544 51
6429 200
3186 0007145 346
2035 13
8919 15
50603457 19444
Satellite: ISS
Catalog Number: 25544
Epoch time: 14220
49177024 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 200
3186 deg
Eccentricity:
0007145
Arg of perigee: 346
2035 deg
Mean anomaly: 13
8919 deg
Mean motion: 15
50603457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1944
Checksum: 297
Coasting Arc #11 (Orbit 1958)
---------------------------------------
Vector Time (GMT): 2014/221/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5949376
64 A = 6795469
52 meter
Y = 1021860
61 meter E =
0008677
Z = -3113964
26 I = 51
55336
XDOT = -3376
185296 Wp = 22
30301
YDOT = -4859
467588 meter/sec RA = 194
43038 deg
ZDOT = 4868
018178 TA = 301
86813
MA = 301
95255
Ha = 227
588 n
mi
Hp = 220
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19518952
24 X = -5945234
85
Y = 3352561
05 feet Y = 955354
08 meter
Z = -10216418
17 Z = -3142854
78
XDOT = -11076
723411 XDOT = -3345
241441
YDOT = -15943
135131 feet/sec YDOT = -4897
049377 meter/sec
ZDOT = 15971
188248 ZDOT = 4851
692537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12564425
91 X = 3829637
02
Y = 15226233
41 feet Y = 4640955
94 meter
Z = -10339312
36 Z = -3151422
41
XDOT = -7182
956121 XDOT = -2189
365026
YDOT = 16698
727916 feet/sec YDOT = 5089
772269 meter/sec
ZDOT = 15902
570665 ZDOT = 4847
103539
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 14221
45850722
00016717 00000-0 10270-3 0 9101
2 25544 51
6429 195
5253 0007138 350
4534 9
6480 15
50578830 19595
Satellite: ISS
Catalog Number: 25544
Epoch time: 14221
45850722 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 195
5253 deg
Eccentricity:
0007138
Arg of perigee: 350
4534 deg
Mean anomaly: 9
6480 deg
Mean motion: 15
50578830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1959
Checksum: 310
Coasting Arc #12 (Orbit 1974)
---------------------------------------
Vector Time (GMT): 2014/222/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6164277
04 A = 6796501
48 meter
Y = -1094869
65 meter E =
0013113
Z = 2640668
28 I = 51
58756
XDOT = 3076
635631 Wp = 70
77766
YDOT = 4699
721307 meter/sec RA = 189
46745 deg
ZDOT = -5207
985270 TA = 79
48814
MA = 79
34043
Ha = 227
707 n
mi
Hp = 219
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20224006
03 X = 6163234
77
Y = -3592092
03 feet Y = -1025942
55 meter
Z = 8663609
83 Z = 2670610
23
XDOT = 10093
948922 XDOT = 3049
151728
YDOT = 15419
033159 feet/sec YDOT = 4733
972556 meter/sec
ZDOT = -17086
565847 ZDOT = -5193
106519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13395834
53 X = -4083050
36
Y = -15499731
34 feet Y = -4724318
11 meter
Z = 8790996
87 Z = 2679495
85
XDOT = 6906
966551 XDOT = 2105
243405
YDOT = -15671
572735 feet/sec YDOT = -4776
695370 meter/sec
ZDOT = -17024
056577 ZDOT = -5188
932445
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 14222
48968381
00016717 00000-0 10270-3 0 9117
2 25544 51
6428 190
4109 0007282 353
2324 6
8727 15
50626455 19754
Satellite: ISS
Catalog Number: 25544
Epoch time: 14222
48968381 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 190
4109 deg
Eccentricity:
0007282
Arg of perigee: 353
2324 deg
Mean anomaly: 6
8727 deg
Mean motion: 15
50626455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1975
Checksum: 315
Coasting Arc #13 (Orbit 1989)
---------------------------------------
Vector Time (GMT): 2014/223/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6316831
58 A = 6797501
14 meter
Y = 1226929
32 meter E =
0012298
Z = -2171426
70 I = 51
62184
XDOT = -2768
859272 Wp = 18
88259
YDOT = -4578
193235 meter/sec RA = 184
50872 deg
ZDOT = 5488
041505 TA = 317
04701
MA = 317
14297
Ha = 227
788 n
mi
Hp = 219
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20724513
06 X = -6319534
05
Y = 4025358
66 feet Y = 1156275
27 meter
Z = -7124103
34 Z = -2202118
88
XDOT = -9084
183964 XDOT = -2744
117616
YDOT = -15020
319014 feet/sec YDOT = -4609
017921 meter/sec
ZDOT = 18005
385514 ZDOT = 5474
651298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14297387
50 X = 4357843
71
Y = 15473063
11 feet Y = 4716189
64 meter
Z = -7254710
96 Z = -2211235
90
XDOT = -6810
067353 XDOT = -2075
708529
YDOT = 14677
967003 feet/sec YDOT = 4473
844342 meter/sec
ZDOT = 17949
170944 ZDOT = 5470
907304
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 14223
45640516
00016717 00000-0 10270-3 0 9123
2 25544 51
6430 185
6176 0007206 357
8406 2
2713 15
50612385 19903
Satellite: ISS
Catalog Number: 25544
Epoch time: 14223
45640516 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 185
6176 deg
Eccentricity:
0007206
Arg of perigee: 357
8406 deg
Mean anomaly: 2
2713 deg
Mean motion: 15
50612385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1990
Checksum: 290
Coasting Arc #14 (Orbit 2005)
---------------------------------------
Vector Time (GMT): 2014/224/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6457666
74 A = 6798285
96 meter
Y = -1345384
55 meter E =
0012596
Z = 1637021
73 I = 51
65648
XDOT = 2396
439506 Wp = 84
61290
YDOT = 4501
614372 meter/sec RA = 179
55210 deg
ZDOT = -5714
649364 TA = 77
50216
MA = 77
36127
Ha = 227
928 n
mi
Hp = 219
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21186570
66 X = 6464279
22
Y = -4413991
29 feet Y = -1273133
70 meter
Z = 5370806
20 Z = 1668407
68
XDOT = 7862
334337 XDOT = 2373
682708
YDOT = 14769
076025 feet/sec YDOT = 4528
285405 meter/sec
ZDOT = -18748
849618 ZDOT = -5703
063501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15144207
64 X = -4615954
49
Y = -15412796
87 feet Y = -4697820
49 meter
Z = 5504391
21 Z = 1677738
44
XDOT = 6989
161806 XDOT = 2130
296519
YDOT = -13590
517141 feet/sec YDOT = -4142
389625 meter/sec
ZDOT = -18700
282591 ZDOT = -5699
846134
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 14224
48756512
00016717 00000-0 10270-3 0 9132
2 25544 51
6436 180
5034 0007372
3465 359
7690 15
50645192 20060
Satellite: ISS
Catalog Number: 25544
Epoch time: 14224
48756512 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 180
5034 deg
Eccentricity:
0007372
Arg of perigee:
3465 deg
Mean anomaly: 359
7690 deg
Mean motion: 15
50645192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2006
Checksum: 296
Coasting Arc #15 (Orbit 2020)
---------------------------------------
Vector Time (GMT): 2014/225/10:50:54
029
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6525603
40 A = 6798895
60 meter
Y = 1505986
10 meter E =
0015851
Z = -1120303
03 I = 51
68966
XDOT = -2035
353116 Wp = 23
96178
YDOT = -4475
697573 meter/sec RA = 174
59915 deg
ZDOT = 5882
448383 TA = 323
90025
MA = 324
00717
Ha = 227
964 n
mi
Hp = 219
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21409459
97 X = -6536516
69
Y = 4940899
27 feet Y = 1432951
51 meter
Z = -3675534
87 Z = -1152029
61
XDOT = -6677
667703 XDOT = -2013
728187
YDOT = -14684
047156 feet/sec YDOT = -4498
336981 meter/sec
ZDOT = 19299
371335 ZDOT = 5872
613834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15975164
36 X = 4869230
10
Y = 15051925
16 feet Y = 4587826
79 meter
Z = -3810602
46 Z = -1161471
63
XDOT = -7346
027585 XDOT = -2239
069208
YDOT = 12637
375931 feet/sec YDOT = 3851
872184 meter/sec
ZDOT = 19258
238095 ZDOT = 5869
910971
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 14225
45427014
00016717 00000-0 10270-3 0 9143
2 25544 51
6436 175
7102 0007265 4
7069 355
4149 15
50648121 20215
Satellite: ISS
Catalog Number: 25544
Epoch time: 14225
45427014 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 175
7102 deg
Eccentricity:
0007265
Arg of perigee: 4
7069 deg
Mean anomaly: 355
4149 deg
Mean motion: 15
50648121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2021
Checksum: 282
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