[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 15th 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 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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 3862)
---------------------------------------
Vector Time (GMT): 2013/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5308981
54 A = 6799858
93 meter
Y = -3590578
50 meter E =
0004642
Z = -2277386
67 I = 51
55722
XDOT = 4422
287358 Wp = 101
89583
YDOT = 3106
044700 meter/sec RA = 342
31216 deg
ZDOT = 5420
510732 TA = 232
79579
MA = 232
83817
Ha = 228
808 n
mi
Hp = 221
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17417918
45 X = 5359800
37
Y = -11780113
18 feet Y = -3530925
81 meter
Z = -7471741
05 Z = -2251473
27
XDOT = 14508
816791 XDOT = 4360
895206
YDOT = 10190
435369 feet/sec YDOT = 3155
153887 meter/sec
ZDOT = 17783
827860 ZDOT = 5441
844604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16984741
59 X = -5176949
24
Y = -12461556
25 feet Y = -3798282
34 meter
Z = -7362746
27 Z = -2244165
06
XDOT = 3824
023891 XDOT = 1165
562482
YDOT = -15755
187431 feet/sec YDOT = -4802
181129 meter/sec
ZDOT = 17872
590305 ZDOT = 5447
565525
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 13193
50446642
00016717 00000-0 10270-3 0 9005
2 25544 51
6487 342
8544 0005368 175
7903 184
3293 15
49784299 38635
Satellite: ISS
Catalog Number: 25544
Epoch time: 13193
50446642 = yrday
fracday
Element set: 900
Inclination: 51
6487 deg
RA of node: 342
8544 deg
Eccentricity:
0005368
Arg of perigee: 175
7903 deg
Mean anomaly: 184
3293 deg
Mean motion: 15
49784299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3863
Checksum: 344
Coasting Arc #2 (Orbit 3878)
---------------------------------------
Vector Time (GMT): 2013/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5186124
31 A = 6800329
14 meter
Y = 3894960
10 meter E =
0016635
Z = 2010784
89 I = 51
52918
XDOT = -4381
204352 Wp = 128
84855
YDOT = -2954
984780 meter/sec RA = 337
35365 deg
ZDOT = -5555
089830 TA = 28
92776
MA = 28
83565
Ha = 228
705 n
mi
Hp = 221
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17014843
55 X = -5239060
90
Y = 12778740
50 feet Y = 3836669
48 meter
Z = 6597063
28 Z = 1985463
08
XDOT = -14374
030025 XDOT = -4320
850624
YDOT = -9694
831955 feet/sec YDOT = -3003
640405 meter/sec
ZDOT = -18225
360334 ZDOT = -5576
226667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17986086
67 X = 5482159
22
Y = 11432252
97 feet Y = 3484550
70 meter
Z = 6490503
24 Z = 1978305
39
XDOT = -3191
183151 XDOT = -972
672624
YDOT = 15457
131813 feet/sec YDOT = 4711
333777 meter/sec
ZDOT = -18313
321033 ZDOT = -5581
900251
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 13194
53618094
00016717 00000-0 10270-3 0 9012
2 25544 51
6481 337
7449 0005318 180
2973 179
8175 15
49787897 38791
Satellite: ISS
Catalog Number: 25544
Epoch time: 13194
53618094 = yrday
fracday
Element set: 901
Inclination: 51
6481 deg
RA of node: 337
7449 deg
Eccentricity:
0005318
Arg of perigee: 180
2973 deg
Mean anomaly: 179
8175 deg
Mean motion: 15
49787897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3879
Checksum: 367
Coasting Arc #3 (Orbit 3893)
---------------------------------------
Vector Time (GMT): 2013/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5035803
62 A = 6800628
47 meter
Y = -4216979
36 meter E =
0004441
Z = -1764478
52 I = 51
50395
XDOT = 4329
516058 Wp = 80
57645
YDOT = 2810
030200 meter/sec RA = 332
39372 deg
ZDOT = 5653
528638 TA = 260
06452
MA = 260
11465
Ha = 228
547 n
mi
Hp = 221
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16521665
43 X = 5091155
82
Y = -13835234
13 feet Y = -4160356
24 meter
Z = -5788971
54 Z = -1739881
01
XDOT = 14204
449010 XDOT = 4270
308809
YDOT = 9219
259186 feet/sec YDOT = 2858
114236 meter/sec
ZDOT = 18548
322304 ZDOT = 5674
417220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18977419
15 X = -5784317
36
Y = -10267674
06 feet Y = -3129587
05 meter
Z = -5685398
43 Z = -1732909
44
XDOT = 2608
669197 XDOT = 795
122371
YDOT = -15116
330276 feet/sec YDOT = -4607
457468 meter/sec
ZDOT = 18635
265381 ZDOT = 5680
028888
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 13195
50340373
00016717 00000-0 10270-3 0 9023
2 25544 51
6495 332
9555 0005248 183
2939 176
8178 15
49813746 38948
Satellite: ISS
Catalog Number: 25544
Epoch time: 13195
50340373 = yrday
fracday
Element set: 902
Inclination: 51
6495 deg
RA of node: 332
9555 deg
Eccentricity:
0005248
Arg of perigee: 183
2939 deg
Mean anomaly: 176
8178 deg
Mean motion: 15
49813746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3894
Checksum: 345
Coasting Arc #4 (Orbit 3909)
---------------------------------------
Vector Time (GMT): 2013/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4863785
52 A = 6801000
58 meter
Y = 4503089
26 meter E =
0016460
Z = 1478241
36 I = 51
47792
XDOT = -4270
821638 Wp = 135
67410
YDOT = -2713
051611 meter/sec RA = 327
43165 deg
ZDOT = -5760
117688 TA = 28
17175
MA = 28
08280
Ha = 228
420 n
mi
Hp = 221
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15957301
56 X = -4920959
41
Y = 14773914
89 feet Y = 4448379
57 meter
Z = 4849873
22 Z = 1454475
02
XDOT = -14011
882014 XDOT = -4212
185318
YDOT = -8901
087963 feet/sec YDOT = -2760
482446 meter/sec
ZDOT = -18898
023910 ZDOT = -5780
722602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19797298
28 X = 6034216
51
Y = 9051644
42 feet Y = 2758941
22 meter
Z = 4749738
82 Z = 1447720
39
XDOT = -2194
602894 XDOT = -668
914962
YDOT = 14809
481439 feet/sec YDOT = 4513
929943 meter/sec
ZDOT = -18983
793570 ZDOT = -5786
260280
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 13196
53509809
00016717 00000-0 10270-3 0 9039
2 25544 51
6489 327
8459 0005229 187
6760 172
4311 15
49820875 39107
Satellite: ISS
Catalog Number: 25544
Epoch time: 13196
53509809 = yrday
fracday
Element set: 903
Inclination: 51
6489 deg
RA of node: 327
8459 deg
Eccentricity:
0005229
Arg of perigee: 187
6760 deg
Mean anomaly: 172
4311 deg
Mean motion: 15
49820875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3910
Checksum: 340
Coasting Arc #5 (Orbit 3924)
---------------------------------------
Vector Time (GMT): 2013/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4662320
80 A = 6801225
74 meter
Y = -4799844
34 meter E =
0005213
Z = -1212499
46 I = 51
45459
XDOT = 4211
446558 Wp = 63
94084
YDOT = 2623
257541 meter/sec RA = 322
46802 deg
ZDOT = 5831
215124 TA = 282
88167
MA = 282
93990
Ha = 228
260 n
mi
Hp = 221
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15296328
09 X = 4721537
17
Y = -15747520
80 feet Y = -4747376
14 meter
Z = -3978016
61 Z = -1189706
88
XDOT = 13817
081884 XDOT = 4153
473312
YDOT = 8606
487995 feet/sec YDOT = 2670
028036 meter/sec
ZDOT = 19131
283214 ZDOT = 5851
533286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20574136
67 X = -6270996
86
Y = -7708587
73 feet Y = -2349577
54 meter
Z = -3881913
96 Z = -1183207
38
XDOT = 1821
545177 XDOT = 555
206970
YDOT = -14501
523328 feet/sec YDOT = -4420
064310 meter/sec
ZDOT = 19215
866052 ZDOT = 5856
995973
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 13197
50230176
00016717 00000-0 10270-3 0 9046
2 25544 51
6499 323
0562 0005084 191
1673 168
9365 15
49840483 39255
Satellite: ISS
Catalog Number: 25544
Epoch time: 13197
50230176 = yrday
fracday
Element set: 904
Inclination: 51
6499 deg
RA of node: 323
0562 deg
Eccentricity:
0005084
Arg of perigee: 191
1673 deg
Mean anomaly: 168
9365 deg
Mean motion: 15
49840483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3925
Checksum: 325
Coasting Arc #6 (Orbit 3940)
---------------------------------------
Vector Time (GMT): 2013/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4444214
35 A = 6801462
75 meter
Y = 5054922
80 meter E =
0015907
Z = 908878
48 I = 51
43149
XDOT = -4152
272556 Wp = 142
68420
YDOT = -2581
396794 meter/sec RA = 317
50273 deg
ZDOT = -5904
735205 TA = 27
46089
MA = 27
37692
Ha = 228
114 n
mi
Hp = 221
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14580755
75 X = -4504824
37
Y = 16584392
38 feet Y = 5004885
81 meter
Z = 2981884
78 Z = 887142
15
XDOT = -13622
941456 XDOT = -4094
414645
YDOT = -8469
149585 feet/sec YDOT = -2627
506099 meter/sec
ZDOT = -19372
490829 ZDOT = -5924
766243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21163069
24 X = 6450503
51
Y = 6348511
63 feet Y = 1935026
35 meter
Z = 2890163
66 Z = 880921
88
XDOT = -1601
944004 XDOT = -488
272532
YDOT = 14262
126033 feet/sec YDOT = 4347
096015 meter/sec
ZDOT = -19455
879087 ZDOT = -5930
151946
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 13198
53397606
00016717 00000-0 10270-3 0 9053
2 25544 51
6497 317
9466 0005110 195
2983 164
8013 15
49853261 39418
Satellite: ISS
Catalog Number: 25544
Epoch time: 13198
53397606 = yrday
fracday
Element set: 905
Inclination: 51
6497 deg
RA of node: 317
9466 deg
Eccentricity:
0005110
Arg of perigee: 195
2983 deg
Mean anomaly: 164
8013 deg
Mean motion: 15
49853261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3941
Checksum: 335
Coasting Arc #7 (Orbit 3955)
---------------------------------------
Vector Time (GMT): 2013/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4196597
36 A = 6801589
91 meter
Y = -5313326
58 meter E =
0006469
Z = -626304
35 I = 51
41091
XDOT = 4102
177069 Wp = 56
98165
YDOT = 2545
025946 meter/sec RA = 312
53565 deg
ZDOT = 5944
123903 TA = 296
25089
MA = 296
31736
Ha = 227
963 n
mi
Hp = 221
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13768364
05 X = 4258742
64
Y = -17432173
81 feet Y = -5266050
03 meter
Z = -2054804
31 Z = -605767
35
XDOT = 13458
586186 XDOT = 4044
538291
YDOT = 8349
822657 feet/sec YDOT = 2590
576156 meter/sec
ZDOT = 19501
718843 ZDOT = 5963
912134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21679288
30 X = -6607847
07
Y = -4879133
75 feet Y = -1487159
97 meter
Z = -1968061
45 Z = -599865
13
XDOT = 1400
829751 XDOT = 426
972908
YDOT = -14057
134791 feet/sec YDOT = -4284
614684 meter/sec
ZDOT = 19584
098992 ZDOT = 5969
233373
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 13199
50116105
00016717 00000-0 10270-3 0 9065
2 25544 51
6505 313
1565 0004909 199
1432 160
9535 15
49866147 39562
Satellite: ISS
Catalog Number: 25544
Epoch time: 13199
50116105 = yrday
fracday
Element set: 906
Inclination: 51
6505 deg
RA of node: 313
1565 deg
Eccentricity:
0004909
Arg of perigee: 199
1432 deg
Mean anomaly: 160
9535 deg
Mean motion: 15
49866147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3956
Checksum: 321
Coasting Arc #8 (Orbit 3971)
---------------------------------------
Vector Time (GMT): 2013/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3939191
53 A = 6801671
54 meter
Y = 5525116
09 meter E =
0014960
Z = 308468
30 I = 51
39118
XDOT = -4059
584538 Wp = 149
80575
YDOT = -2554
117495 meter/sec RA = 307
56774 deg
ZDOT = -5979
655584 TA = 26
86263
MA = 26
78525
Ha = 227
807 n
mi
Hp = 221
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12923856
72 X = -4002180
25
Y = 18127021
29 feet Y = 5480713
33 meter
Z = 1012035
12 Z = 289179
88
XDOT = -13318
846908 XDOT = -4001
674763
YDOT = -8379
650574 feet/sec YDOT = -2599
189800 meter/sec
ZDOT = -19618
292599 ZDOT = -5999
236216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21999661
89 X = 6705496
94
Y = 3433404
27 feet Y = 1046501
62 meter
Z = 930483
90 Z = 283611
49
XDOT = -1326
633784 XDOT = -404
357977
YDOT = 13949
482219 feet/sec YDOT = 4251
802180 meter/sec
ZDOT = -19699
807139 ZDOT = -6004
501216
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 13200
53281577
00016717 00000-0 10270-3 0 9078
2 25544 51
6504 308
0472 0004980 202
9274 157
1655 15
49881932 39725
Satellite: ISS
Catalog Number: 25544
Epoch time: 13200
53281577 = yrday
fracday
Element set: 907
Inclination: 51
6504 deg
RA of node: 308
0472 deg
Eccentricity:
0004980
Arg of perigee: 202
9274 deg
Mean anomaly: 157
1655 deg
Mean motion: 15
49881932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3972
Checksum: 317
Coasting Arc #9 (Orbit 3987)
---------------------------------------
Vector Time (GMT): 2013/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3654315
74 A = 6801664
24 meter
Y = -5733178
82 meter E =
0007738
Z = -12563
62 I = 51
37406
XDOT = 4034
689353 Wp = 56
77709
YDOT = 2564
476369 meter/sec RA = 302
59795 deg
ZDOT = 5983
119806 TA = 303
08738
MA = 303
16165
Ha = 227
663 n
mi
Hp = 221
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11989224
88 X = 3718214
83
Y = -18809641
81 feet Y = -5691956
67 meter
Z = -41219
22 Z = 5342
98
XDOT = 13237
169794 XDOT = 3976
648920
YDOT = 8413
636380 feet/sec YDOT = 2609
269521 meter/sec
ZDOT = 19629
658155 ZDOT = 6002
579093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22224245
18 X = -6773949
93
Y = -1904617
38 feet Y = -580527
38 meter
Z = 34580
54 Z = 10540
15
XDOT = 1238
348185 XDOT = 377
448527
YDOT = -13901
242242 feet/sec YDOT = -4237
098635 meter/sec
ZDOT = 19710
670023 ZDOT = 6007
812223
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 13201
56446055
00016717 00000-0 10270-3 0 9087
2 25544 51
6512 302
9377 0004757 207
3812 152
7088 15
49893829 39886
Satellite: ISS
Catalog Number: 25544
Epoch time: 13201
56446055 = yrday
fracday
Element set: 908
Inclination: 51
6512 deg
RA of node: 302
9377 deg
Eccentricity:
0004757
Arg of perigee: 207
3812 deg
Mean anomaly: 152
7088 deg
Mean motion: 15
49893829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3988
Checksum: 337
Coasting Arc #10 (Orbit 4002)
---------------------------------------
Vector Time (GMT): 2013/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3368065
33 A = 6801580
97 meter
Y = 5891154
68 meter E =
0013583
Z = -315366
10 I = 51
35764
XDOT = -4024
051283 Wp = 156
95473
YDOT = -2615
189233 meter/sec RA = 297
62795 deg
ZDOT = -5976
174623 TA = 26
45271
MA = 26
38344
Ha = 227
500 n
mi
Hp = 222
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11050083
11 X = -3432159
25
Y = 19327935
29 feet Y = 5853132
51 meter
Z = -1034665
67 Z = -331882
54
XDOT = -13202
267989 XDOT = -3965
478463
YDOT = -8580
017169 feet/sec YDOT = -2659
860499 meter/sec
ZDOT = -19606
872124 ZDOT = -5995
580812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22255940
41 X = 6783610
64
Y = 443596
01 feet Y = 135208
06 meter
Z = -1104668
11 Z = -336702
84
XDOT = -1240
406924 XDOT = -378
076030
YDOT = 13969
442860 feet/sec YDOT = 4257
886184 meter/sec
ZDOT = -19687
662412 ZDOT = -6000
799503
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 13202
53161835
00016717 00000-0 10270-3 0 9096
2 25544 51
6506 298
1482 0004844 210
6784 149
4084 15
49907653 40033
Satellite: ISS
Catalog Number: 25544
Epoch time: 13202
53161835 = yrday
fracday
Element set: 909
Inclination: 51
6506 deg
RA of node: 298
1482 deg
Eccentricity:
0004844
Arg of perigee: 210
6784 deg
Mean anomaly: 149
4084 deg
Mean motion: 15
49907653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4003
Checksum: 313
Coasting Arc #11 (Orbit 4018)
---------------------------------------
Vector Time (GMT): 2013/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3058516
56 A = 6801409
85 meter
Y = -6039183
97 meter E =
0008764
Z = 620383
06 I = 51
34427
XDOT = 4037
697124 Wp = 60
41464
YDOT = 2661
138873 meter/sec RA = 292
65593 deg
ZDOT = 5939
851363 TA = 306
29656
MA = 306
37747
Ha = 227
358 n
mi
Hp = 222
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10034503
13 X = 3122807
12
Y = -19813595
69 feet Y = -6004622
29 meter
Z = 2035377
48 Z = 635396
28
XDOT = 13247
037809 XDOT = 3978
786046
YDOT = 8730
770581 feet/sec YDOT = 2705
960968 meter/sec
ZDOT = 19487
701322 ZDOT = 5959
322883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22178065
79 X = -6759874
45
Y = 1067590
02 feet Y = 325401
44 meter
Z = 2099104
15 Z = 639806
94
XDOT = 1190
827957 XDOT = 362
964361
YDOT = -14108
699748 feet/sec YDOT = -4300
331683 meter/sec
ZDOT = 19568
767203 ZDOT = 5964
560243
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
56324415
00016717 00000-0 10270-3 0 9107
2 25544 51
6510 293
0386 0004640 215
5226 144
5617 15
49922397 40191
Satellite: ISS
Catalog Number: 25544
Epoch time: 13203
56324415 = yrday
fracday
Element set: 910
Inclination: 51
6510 deg
RA of node: 293
0386 deg
Eccentricity:
0004640
Arg of perigee: 215
5226 deg
Mean anomaly: 144
5617 deg
Mean motion: 15
49922397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4019
Checksum: 292
Coasting Arc #12 (Orbit 4033)
---------------------------------------
Vector Time (GMT): 2013/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2757123
84 A = 6801150
95 meter
Y = 6135759
45 meter E =
0011742
Z = -953477
03 I = 51
33133
XDOT = -4070
978534 Wp = 163
93623
YDOT = -2739
646130 meter/sec RA = 287
68378 deg
ZDOT = -5886
656201 TA = 26
41877
MA = 26
35895
Ha = 227
183 n
mi
Hp = 222
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9045681
89 X = -2820898
70
Y = 20130444
38 feet Y = 6104571
03 meter
Z = -3128205
49 Z = -967025
02
XDOT = -13356
228786 XDOT = -4011
445553
YDOT = -8988
340321 feet/sec YDOT = -2784
837082 meter/sec
ZDOT = -19313
176512 ZDOT = -5906
287782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21922780
22 X = 6682063
41
Y = -2467221
07 feet Y = -752008
98 meter
Z = -3185804
27 Z = -971033
14
XDOT = -1187
885847 XDOT = -362
067606
YDOT = 14370
065435 feet/sec YDOT = 4379
995945 meter/sec
ZDOT = -19394
909444 ZDOT = -5911
568398
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
53038466
00016717 00000-0 10270-3 0 9114
2 25544 51
6498 288
2490 0004685 218
7819 141
2996 15
49934438 40340
Satellite: ISS
Catalog Number: 25544
Epoch time: 13204
53038466 = yrday
fracday
Element set: 911
Inclination: 51
6498 deg
RA of node: 288
2490 deg
Eccentricity:
0004685
Arg of perigee: 218
7819 deg
Mean anomaly: 141
2996 deg
Mean motion: 15
49934438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4034
Checksum: 338
Coasting Arc #13 (Orbit 4049)
---------------------------------------
Vector Time (GMT): 2013/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2438459
04 A = 6800813
07 meter
Y = -6217515
53 meter E =
0009448
Z = 1262675
31 I = 51
32209
XDOT = 4132
605244 Wp = 66
35735
YDOT = 2806
405324 meter/sec RA = 282
70963 deg
ZDOT = 5807
217848 TA = 307
40908
MA = 307
49504
Ha = 227
048 n
mi
Hp = 222
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8000193
71 X = 2501669
83
Y = -20398673
01 feet Y = -6189893
77 meter
Z = 4142635
55 Z = 1274674
09
XDOT = 13558
416155 XDOT = 4072
707020
YDOT = 9207
366548 feet/sec YDOT = 2852
283537 meter/sec
ZDOT = 19052
551994 ZDOT = 5827
147864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21555149
07 X = -6570009
44
Y = 3880514
00 feet Y = 1182780
67 meter
Z = 4193751
13 Z = 1278255
35
XDOT = 1096
070273 XDOT = 334
082219
YDOT = -14700
121058 feet/sec YDOT = -4480
596899 meter/sec
ZDOT = 19135
531997 ZDOT = 5832
510153
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
56199185
00016717 00000-0 10270-3 0 9125
2 25544 51
6499 283
1390 0004527 223
8062 136
2730 15
49950437 40501
Satellite: ISS
Catalog Number: 25544
Epoch time: 13205
56199185 = yrday
fracday
Element set: 912
Inclination: 51
6499 deg
RA of node: 283
1390 deg
Eccentricity:
0004527
Arg of perigee: 223
8062 deg
Mean anomaly: 136
2730 deg
Mean motion: 15
49950437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4050
Checksum: 310
Coasting Arc #14 (Orbit 4064)
---------------------------------------
Vector Time (GMT): 2013/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2138011
56 A = 6800364
90 meter
Y = 6249086
35 meter E =
0009458
Z = -1595304
98 I = 51
31360
XDOT = -4216
948350 Wp = 170
30391
YDOT = -2895
548068 meter/sec RA = 277
73523 deg
ZDOT = -5704
951105 TA = 27
20102
MA = 27
15150
Ha = 226
859 n
mi
Hp = 222
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7014473
63 X = -2199981
90
Y = 20502251
81 feet Y = 6224831
31 meter
Z = -5233940
21 Z = -1605841
37
XDOT = -13835
132382 XDOT = -4156
543730
YDOT = -9499
829618 feet/sec YDOT = -2942
366742 meter/sec
ZDOT = -18717
031185 ZDOT = -5725
289625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21038571
14 X = 6412556
48
Y = -5143027
87 feet Y = -1567594
89 meter
Z = -5278928
72 Z = -1609017
47
XDOT = -1004
662416 XDOT = -306
221105
YDOT = 15141
694149 feet/sec YDOT = 4615
188377 meter/sec
ZDOT = -18801
714581 ZDOT = -5730
762604
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
52911546
00016717 00000-0 10270-3 0 9136
2 25544 51
6486 278
3488 0004494 227
2262 132
8511 15
49965263 40652
Satellite: ISS
Catalog Number: 25544
Epoch time: 13206
52911546 = yrday
fracday
Element set: 913
Inclination: 51
6486 deg
RA of node: 278
3488 deg
Eccentricity:
0004494
Arg of perigee: 227
2262 deg
Mean anomaly: 132
8511 deg
Mean motion: 15
49965263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4065
Checksum: 322
Coasting Arc #15 (Orbit 4080)
---------------------------------------
Vector Time (GMT): 2013/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1827641
81 A = 6799882
97 meter
Y = -6262790
45 meter E =
0009760
Z = 1902903
15 I = 51
30897
XDOT = 4331
069219 Wp = 73
87306
YDOT = 2965
758790 meter/sec RA = 272
75936 deg
ZDOT = 5579
792140 TA = 307
14994
MA = 307
23905
Ha = 226
747 n
mi
Hp = 222
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5996200
16 X = 1888294
22
Y = -20547212
75 feet Y = -6242013
51 meter
Z = 6243120
58 Z = 1911928
73
XDOT = 14209
544683 XDOT = 4270
478876
YDOT = 9730
179757 feet/sec YDOT = 3013
852657 meter/sec
ZDOT = 18306
404659 ZDOT = 5600
684640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20418511
28 X = -6223562
24
Y = 6382991
67 feet Y = 1945535
86 meter
Z = 6281778
21 Z = 1914686
00
XDOT = 791
925750 XDOT = 241
378969
YDOT = -15636
717270 feet/sec YDOT = -4766
071424 meter/sec
ZDOT = 18393
402169 ZDOT = 5606
308981
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
56070470
00016717 00000-0 10270-3 0 9144
2 25544 51
6487 273
2383 0004378 232
1174 127
9581 15
49975827 40816
Satellite: ISS
Catalog Number: 25544
Epoch time: 13207
56070470 = yrday
fracday
Element set: 914
Inclination: 51
6487 deg
RA of node: 273
2383 deg
Eccentricity:
0004378
Arg of perigee: 232
1174 deg
Mean anomaly: 127
9581 deg
Mean motion: 15
49975827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4081
Checksum: 324
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