[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 10th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 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
314/23:26:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 220
8
Coasting Arc #1 (Orbit 1708)
---------------------------------------
Vector Time (GMT): 2013/312/12:19:48
579
Vector Time (MET): N/A
Weight (LBS) : 901243
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2070550
75 A = 6801288
92 meter
Y = 6437919
56 meter E =
0010787
Z = -681743
92 I = 51
99388
XDOT = -4695
821199 Wp = 46
64729
YDOT = -883
262980 meter/sec RA = 112
34708 deg
ZDOT = 5987
509458 TA = 306
03942
MA = 306
13933
Ha = 227
953 n
mi
Hp = 220
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6793145
50 X = -2139075
32
Y = 21121783
35 feet Y = 6414382
21 meter
Z = -2236692
65 Z = -691968
98
XDOT = -15406
237530 XDOT = -4714
681457
YDOT = -2897
844423 feet/sec YDOT = -935
880162 meter/sec
ZDOT = 19644
059900 ZDOT = 5964
651441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12465313
85 X = -3799427
66
Y = -18349226
19 feet Y = -5592844
14 meter
Z = -2280614
04 Z = -695131
16
XDOT = 10507
234308 XDOT = 3202
605017
YDOT = -9540
948288 feet/sec YDOT = -2908
081038 meter/sec
ZDOT = 19548
067877 ZDOT = 5958
251089
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 13312
51510219
00016717 00000-0 10270-3 0 9001
2 25544 51
6468 113
2753 0001172 120
7080 239
4187 15
49952195 17094
Satellite: ISS
Catalog Number: 25544
Epoch time: 13312
51510219 = yrday
fracday
Element set: 900
Inclination: 51
6468 deg
RA of node: 113
2753 deg
Eccentricity:
0001172
Arg of perigee: 120
7080 deg
Mean anomaly: 239
4187 deg
Mean motion: 15
49952195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1709
Checksum: 289
Coasting Arc #2 (Orbit 1724)
---------------------------------------
Vector Time (GMT): 2013/313/12:19:48
579
Vector Time (MET): N/A
Weight (LBS) : 901243
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1781896
90 A = 6801288
57 meter
Y = -6548597
95 meter E =
0013629
Z = 333093
51 I = 52
00474
XDOT = 4636
769950 Wp = 130
21109
YDOT = 947
321046 meter/sec RA = 107
41907 deg
ZDOT = -6026
634572 TA = 46
22253
MA = 46
10985
Ha = 227
830 n
mi
Hp = 220
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5846118
45 X = 1853374
24
Y = -21484901
41 feet Y = -6528271
99 meter
Z = 1092826
49 Z = 341923
56
XDOT = 15212
499837 XDOT = 4655
108287
YDOT = 3108
008682 feet/sec YDOT = 999
274868 meter/sec
ZDOT = -19772
423135 ZDOT = -6004
064754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13635096
86 X = 4155977
52
Y = 17600498
25 feet Y = 5364631
87 meter
Z = 1130908
57 Z = 344700
93
XDOT = -10431
908168 XDOT = -3179
645610
YDOT = 9377
273417 feet/sec YDOT = 2858
192938 meter/sec
ZDOT = -19677
645616 ZDOT = -5997
746384
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 13313
54669951
00016717 00000-0 10270-3 0 9014
2 25544 51
6463 108
1648 0000975 116
2549 243
8702 15
50006577 17251
Satellite: ISS
Catalog Number: 25544
Epoch time: 13313
54669951 = yrday
fracday
Element set: 901
Inclination: 51
6463 deg
RA of node: 108
1648 deg
Eccentricity:
0000975
Arg of perigee: 116
2549 deg
Mean anomaly: 243
8702 deg
Mean motion: 15
50006577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1725
Checksum: 309
Coasting Arc #3 (Orbit 1739)
---------------------------------------
Vector Time (GMT): 2013/314/12:19:48
579
Vector Time (MET): N/A
Weight (LBS) : 901243
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1460296
33 A = 6801285
99 meter
Y = 6637231
76 meter E =
0012328
Z = -12682
85 I = 52
01461
XDOT = -4606
037419 Wp = 50
74339
YDOT = -1009
359666 meter/sec RA = 102
49178 deg
ZDOT = 6038
511655 TA = 309
12094
MA = 309
23048
Ha = 227
829 n
mi
Hp = 220
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4790998
45 X = -1534345
18
Y = 21775694
74 feet Y = 6620487
76 meter
Z = -41610
41 Z = -19956
93
XDOT = -15111
671322 XDOT = -4623
742005
YDOT = -3311
547461 feet/sec YDOT = -1060
966173 meter/sec
ZDOT = 19811
389945 ZDOT = 6016
092694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14788013
27 X = -4507386
45
Y = -16686688
95 feet Y = -5086102
79 meter
Z = -73171
78 Z = -22302
76
XDOT = 10423
794926 XDOT = 3177
172693
YDOT = -9292
098130 feet/sec YDOT = -2832
231510 meter/sec
ZDOT = 19717
251461 ZDOT = 6009
818245
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 13314
51380256
00016717 00000-0 10270-3 0 9021
2 25544 51
6476 103
3742 0001144 123
2848 236
8412 15
50023532 17403
Satellite: ISS
Catalog Number: 25544
Epoch time: 13314
51380256 = yrday
fracday
Element set: 902
Inclination: 51
6476 deg
RA of node: 103
3742 deg
Eccentricity:
0001144
Arg of perigee: 123
2848 deg
Mean anomaly: 236
8412 deg
Mean motion: 15
50023532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1740
Checksum: 268
Coasting Arc #4 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2013/314/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4215226
31 A = 6791711
77 meter
Y = 2355991
86 meter E =
0008472
Z = 4770872
52 I = 51
98451
XDOT = -881
002068 Wp = 115
92490
YDOT = -7109
620943 meter/sec RA = 100
23559 deg
ZDOT = 2725
182556 TA = 307
21015
MA = 307
28744
Ha = 227
841 n
mi
Hp = 220
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13829482
63 X = -4264434
14
Y = 7729632
09 feet Y = 2308579
51 meter
Z = 15652468
91 Z = 4750275
49
XDOT = -2890
426731 XDOT = -814
673602
YDOT = -23325
528027 feet/sec YDOT = -7119
101929 meter/sec
ZDOT = 8940
887651 ZDOT = 2721
063982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5449374
14 X = -1660969
24
Y = 14967336
83 feet Y = 4562044
27 meter
Z = 15565498
23 Z = 4744363
86
XDOT = -16423
131706 XDOT = -5005
770544
YDOT = -15285
915630 feet/sec YDOT = -4659
147084 meter/sec
ZDOT = 8924
608710 ZDOT = 2720
220735
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 13315
02958084
00016717 00000-0 10270-3 0 9039
2 25544 51
6463 100
8231 0000793 99
5403 260
5837 15
50046556 17489
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
02958084 = yrday
fracday
Element set: 903
Inclination: 51
6463 deg
RA of node: 100
8231 deg
Eccentricity:
0000793
Arg of perigee: 99
5403 deg
Mean anomaly: 260
5837 deg
Mean motion: 15
50046556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1748
Checksum: 302
Coasting Arc #5 (Orbit 1762)
---------------------------------------
Vector Time (GMT): 2013/315/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4084800
87 A = 6791054
04 meter
Y = -2282239
83 meter E =
0012831
Z = -4933720
24 I = 51
98713
XDOT = 1178
146545 Wp = 74
62070
YDOT = 7185
672565 meter/sec RA = 95
30205 deg
ZDOT = -2350
300569 TA = 172
44259
MA = 172
42323
Ha = 227
745 n
mi
Hp = 220
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13401577
67 X = 4133984
83
Y = -7487663
49 feet Y = -2236286
17 meter
Z = -16186746
18 Z = -4913756
79
XDOT = 3865
310187 XDOT = 1109
124501
YDOT = 23575
041224 feet/sec YDOT = 7198
461338 meter/sec
ZDOT = -7710
959873 ZDOT = -2344
745074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5037022
65 X = 1535284
50
Y = -14595129
57 feet Y = -4448595
49 meter
Z = -16102445
04 Z = -4908025
25
XDOT = 17603
705679 XDOT = 5365
609491
YDOT = 14551
555720 feet/sec YDOT = 4435
314183 meter/sec
ZDOT = -7688
658843 ZDOT = -2343
503215
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 13315
99665167
00016717 00000-0 10270-3 0 9043
2 25544 51
6464 96
0311 0000902 95
3878 264
7375 15
50057030 17636
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
99665167 = yrday
fracday
Element set: 904
Inclination: 51
6464 deg
RA of node: 96
0311 deg
Eccentricity:
0000902
Arg of perigee: 95
3878 deg
Mean anomaly: 264
7375 deg
Mean motion: 15
50057030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1763
Checksum: 313
Coasting Arc #6 (Orbit 1778)
---------------------------------------
Vector Time (GMT): 2013/316/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3965117
45 A = 6790312
73 meter
Y = 2190471
16 meter E =
0006425
Z = 5054651
75 I = 51
98751
XDOT = -1492
141428 Wp = 120
40813
YDOT = -7255
865386 meter/sec RA = 90
36968 deg
ZDOT = 1968
850631 TA = 310
53630
MA = 310
59224
Ha = 227
706 n
mi
Hp = 220
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13008915
52 X = -4013871
67
Y = 7186585
16 feet Y = 2145858
28 meter
Z = 16583503
12 Z = 5035270
70
XDOT = -4895
477125 XDOT = -1420
458160
YDOT = -23805
332631 feet/sec YDOT = -7272
150582 meter/sec
ZDOT = 6459
483696 ZDOT = 1961
776203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4704577
81 X = -1433955
32
Y = 14193436
48 feet Y = 4326159
44 meter
Z = 16501659
72 Z = 5029705
88
XDOT = -18792
339061 XDOT = -5727
904946
YDOT = -13724
830568 feet/sec YDOT = -4183
328357 meter/sec
ZDOT = 6430
817114 ZDOT = 1960
113056
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 13317
02816881
00016717 00000-0 10270-3 0 9051
2 25544 51
6467 90
9209 0000723 91
9121 268
2112 15
50121044 17794
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
02816881 = yrday
fracday
Element set: 905
Inclination: 51
6467 deg
RA of node: 90
9209 deg
Eccentricity:
0000723
Arg of perigee: 91
9121 deg
Mean anomaly: 268
2112 deg
Mean motion: 15
50121044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1779
Checksum: 289
Coasting Arc #7 (Orbit 1793)
---------------------------------------
Vector Time (GMT): 2013/317/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3894698
04 A = 6789808
59 meter
Y = -2065298
85 meter E =
0014407
Z = -5176874
10 I = 51
98557
XDOT = 1796
862930 Wp = 78
80619
YDOT = 7273
468399 meter/sec RA = 85
43508 deg
ZDOT = -1550
840043 TA = 176
29049
MA = 176
27980
Ha = 227
591 n
mi
Hp = 220
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12777880
70 X = 3942651
61
Y = -6775914
87 feet Y = -2021477
90 meter
Z = -16984495
08 Z = -5157837
05
XDOT = 5895
219585 XDOT = 1722
929579
YDOT = 23863
085299 feet/sec YDOT = 7293
148631 meter/sec
ZDOT = -5088
057883 ZDOT = -1542
290664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4579925
22 X = 1395961
21
Y = -13817945
21 feet Y = -4211709
70 meter
Z = -16904112
10 Z = -5152373
37
XDOT = 19812
922126 XDOT = 6038
978664
YDOT = 12744
975715 feet/sec YDOT = 3884
668598 meter/sec
ZDOT = -5053
205147 ZDOT = -1540
216929
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 13317
99519548
00016717 00000-0 10270-3 0 9068
2 25544 51
6471 86
1286 0000805 87
5897 272
5346 15
50130100 17940
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
99519548 = yrday
fracday
Element set: 906
Inclination: 51
6471 deg
RA of node: 86
1286 deg
Eccentricity:
0000805
Arg of perigee: 87
5897 deg
Mean anomaly: 272
5346 deg
Mean motion: 15
50130100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1794
Checksum: 322
Coasting Arc #8 (Orbit 1809)
---------------------------------------
Vector Time (GMT): 2013/318/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3842097
71 A = 6789230
93 meter
Y = 1924430
44 meter E =
0004391
Z = 5253249
35 I = 51
98168
XDOT = -2108
766421 Wp = 117
30923
YDOT = -7283
078321 meter/sec RA = 80
50155 deg
ZDOT = 1123
041917 TA = 321
95707
MA = 321
98807
Ha = 227
583 n
mi
Hp = 220
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12605307
44 X = -3888851
05
Y = 6313748
15 feet Y = 1881204
34 meter
Z = 17235070
04 Z = 5234470
72
XDOT = -6918
525003 XDOT = -2032
624268
YDOT = -23894
613913 feet/sec YDOT = -7306
234134 meter/sec
ZDOT = 3684
520724 ZDOT = 1112
982552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4546651
93 X = -1385819
51
Y = 13446622
31 feet Y = 4098530
48 meter
Z = 17155790
15 Z = 5229084
84
XDOT = -20802
861776 XDOT = -6340
712269
YDOT = -11693
578043 feet/sec YDOT = -3564
202588 meter/sec
ZDOT = 3643
334889 ZDOT = 1110
488474
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 13319
02666558
00016717 00000-0 10270-3 0 9079
2 25544 51
6479 81
0184 0000698 83
1384 276
9846 15
50194591 18108
Satellite: ISS
Catalog Number: 25544
Epoch time: 13319
02666558 = yrday
fracday
Element set: 907
Inclination: 51
6479 deg
RA of node: 81
0184 deg
Eccentricity:
0000698
Arg of perigee: 83
1384 deg
Mean anomaly: 276
9846 deg
Mean motion: 15
50194591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1810
Checksum: 331
Coasting Arc #9 (Orbit 1824)
---------------------------------------
Vector Time (GMT): 2013/319/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3843553
18 A = 6788951
02 meter
Y = -1766932
54 meter E =
0015389
Z = -5323236
74 I = 51
97526
XDOT = 2400
957353 Wp = 84
54587
YDOT = 7233
421841 meter/sec RA = 75
56562 deg
ZDOT = -667
644010 TA = 179
09526
MA = 179
09247
Ha = 227
455 n
mi
Hp = 220
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12610082
60 X = 3888885
26
Y = -5797022
76 feet Y = -1723698
02 meter
Z = -17464687
47 Z = -5304454
50
XDOT = 7877
156669 XDOT = 2323
136503
YDOT = 23731
698953 feet/sec YDOT = 7259
835752 meter/sec
ZDOT = -2190
433103 ZDOT = -656
169116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4689975
37 X = 1429504
49
Y = -13167633
44 feet Y = -4013494
67 meter
Z = -17385411
28 Z = -5299073
36
XDOT = 21570
747767 XDOT = 6574
763920
YDOT = 10511
748441 feet/sec YDOT = 3203
980925 meter/sec
ZDOT = -2143
302848 ZDOT = -653
278708
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 13319
99364807
00016717 00000-0 10270-3 0 9088
2 25544 51
6483 76
2261 0000768 79
2063 280
9174 15
50203209 18255
Satellite: ISS
Catalog Number: 25544
Epoch time: 13319
99364807 = yrday
fracday
Element set: 908
Inclination: 51
6483 deg
RA of node: 76
2261 deg
Eccentricity:
0000768
Arg of perigee: 79
2063 deg
Mean anomaly: 280
9174 deg
Mean motion: 15
50203209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1825
Checksum: 317
Coasting Arc #10 (Orbit 1840)
---------------------------------------
Vector Time (GMT): 2013/320/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3867907
82 A = 6788623
48 meter
Y = 1597994
74 meter E =
0003133
Z = 5342504
59 I = 51
96706
XDOT = -2688
183336 Wp = 93
23445
YDOT = -7175
402334 meter/sec RA = 70
63051 deg
ZDOT = 199
747612 TA = 354
86796
MA = 354
87117
Ha = 227
476 n
mi
Hp = 220
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12689986
29 X = -3911442
59
Y = 5242764
89 feet Y = 1554497
83 meter
Z = 17527902
21 Z = 5323608
44
XDOT = -8819
499135 XDOT = -2608
716952
YDOT = -23541
346241 feet/sec YDOT = -7205
018993 meter/sec
ZDOT = 655
339933 ZDOT = 186
881234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4922184
92 X = -1500281
96
Y = 12926067
64 feet Y = 3939865
42 meter
Z = 17448167
89 Z = 5318201
57
XDOT = -22270
558939 XDOT = -6788
066365
YDOT = -9294
833809 feet/sec YDOT = -2833
065345 meter/sec
ZDOT = 602
364388 ZDOT = 183
600665
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 13321
02507123
00016717 00000-0 10270-3 0 9096
2 25544 51
6492 71
1159 0000721 75
3848 284
7382 15
50265951 18415
Satellite: ISS
Catalog Number: 25544
Epoch time: 13321
02507123 = yrday
fracday
Element set: 909
Inclination: 51
6492 deg
RA of node: 71
1159 deg
Eccentricity:
0000721
Arg of perigee: 75
3848 deg
Mean anomaly: 284
7382 deg
Mean motion: 15
50265951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1841
Checksum: 295
Coasting Arc #11 (Orbit 1855)
---------------------------------------
Vector Time (GMT): 2013/321/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3946116
84 A = 6788627
22 meter
Y = -1431219
10 meter E =
0015562
Z = -5348713
03 I = 51
95640
XDOT = 2943
358776 Wp = 91
18722
YDOT = 7056
176762 meter/sec RA = 65
69283 deg
ZDOT = 283
813992 TA = 181
51028
MA = 181
51499
Ha = 227
348 n
mi
Hp = 220
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12946577
57 X = 3987811
00
Y = -4695600
72 feet Y = -1386857
81 meter
Z = -17548271
10 Z = -5329441
45
XDOT = 9656
688899 XDOT = 2862
857563
YDOT = 23150
186226 feet/sec YDOT = 7088
641156 meter/sec
ZDOT = 931
148268 ZDOT = 297
917603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5277071
23 X = 1608451
31
Y = -12832050
58 feet Y = -3911209
02 meter
Z = -17466978
92 Z = -5323935
17
XDOT = 22705
187564 XDOT = 6920
541170
YDOT = 7992
429187 feet/sec YDOT = 2436
092416 meter/sec
ZDOT = 989
331817 ZDOT = 301
548338
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 13321
99200977
00016717 00000-0 10270-3 0 9101
2 25544 51
6495 66
3236 0000804 73
2128 286
9111 15
50275777 18567
Satellite: ISS
Catalog Number: 25544
Epoch time: 13321
99200977 = yrday
fracday
Element set: 910
Inclination: 51
6495 deg
RA of node: 66
3236 deg
Eccentricity:
0000804
Arg of perigee: 73
2128 deg
Mean anomaly: 286
9111 deg
Mean motion: 15
50275777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1856
Checksum: 312
Coasting Arc #12 (Orbit 1871)
---------------------------------------
Vector Time (GMT): 2013/322/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4049300
43 A = 6788623
50 meter
Y = 1258526
51 meter E =
0004010
Z = 5298522
90 I = 51
94386
XDOT = -3179
452907 Wp = 62
61759
YDOT = -6930
741983 meter/sec RA = 60
75556 deg
ZDOT = -781
373428 TA = 34
83396
MA = 34
80772
Ha = 227
387 n
mi
Hp = 220
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13285106
38 X = -4088811
94
Y = 4129023
98 feet Y = 1213023
49 meter
Z = 17383605
32 Z = 5278755
42
XDOT = -10431
275942 XDOT = -3097
919728
YDOT = -22738
654799 feet/sec YDOT = -6965
840735 meter/sec
ZDOT = -2563
561116 ZDOT = -796
621534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5704271
51 X = -1738661
96
Y = 12802158
18 feet Y = 3902097
81 meter
Z = 17300250
21 Z = 5273116
26
XDOT = -23041
292267 XDOT = -7022
985883
YDOT = -6707
096620 feet/sec YDOT = -2044
323050 meter/sec
ZDOT = -2626
566071 ZDOT = -800
577338
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 13323
02338630
00016717 00000-0 10270-3 0 9116
2 25544 51
6499 61
2132 0000790 70
3289 289
7947 15
50334850 18724
Satellite: ISS
Catalog Number: 25544
Epoch time: 13323
02338630 = yrday
fracday
Element set: 911
Inclination: 51
6499 deg
RA of node: 61
2132 deg
Eccentricity:
0000790
Arg of perigee: 70
3289 deg
Mean anomaly: 289
7947 deg
Mean motion: 15
50334850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1872
Checksum: 304
Coasting Arc #13 (Orbit 1886)
---------------------------------------
Vector Time (GMT): 2013/323/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4200430
43 A = 6788945
22 meter
Y = -1107045
44 meter E =
0014745
Z = -5230320
27 I = 51
92954
XDOT = 3371
184562 Wp = 97
99839
YDOT = 6748
116643 meter/sec RA = 55
81572 deg
ZDOT = 1280
164148 TA = 184
26603
MA = 184
27861
Ha = 227
260 n
mi
Hp = 220
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13780939
72 X = 4237905
42
Y = -3632038
86 feet Y = -1059863
75 meter
Z = -17159843
41 Z = -5209823
61
XDOT = 11060
316804 XDOT = 3289
256266
YDOT = 22139
490297 feet/sec YDOT = 6785
357219 meter/sec
ZDOT = 4200
013610 ZDOT = 1296
342721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6181930
33 X = 1884252
36
Y = -12955599
64 feet Y = -3948866
77 meter
Z = -17073441
58 Z = -5203984
99
XDOT = 23090
542152 XDOT = 7037
997248
YDOT = 5399
524440 feet/sec YDOT = 1645
775049 meter/sec
ZDOT = 4266
951764 ZDOT = 1300
566898
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 13323
99028119
00016717 00000-0 10270-3 0 9121
2 25544 51
6503 56
4207 0000882 70
4900 289
6346 15
50347862 18877
Satellite: ISS
Catalog Number: 25544
Epoch time: 13323
99028119 = yrday
fracday
Element set: 912
Inclination: 51
6503 deg
RA of node: 56
4207 deg
Eccentricity:
0000882
Arg of perigee: 70
4900 deg
Mean anomaly: 289
6346 deg
Mean motion: 15
50347862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1887
Checksum: 312
Coasting Arc #14 (Orbit 1902)
---------------------------------------
Vector Time (GMT): 2013/324/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4374772
08 A = 6789306
41 meter
Y = 955418
66 meter E =
0006312
Z = 5099616
74 I = 51
91307
XDOT = -3528
734237 Wp = 56
94616
YDOT = -6564
520899 meter/sec RA = 50
87578 deg
ZDOT = -1792
343407 TA = 50
36398
MA = 50
30830
Ha = 227
310 n
mi
Hp = 220
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14352926
77 X = -4409903
58
Y = 3134575
67 feet Y = 906300
47 meter
Z = 16731026
04 Z = 5078278
87
XDOT = -11577
212064 XDOT = -3446
359193
YDOT = -21537
142057 feet/sec YDOT = -6603
520769 meter/sec
ZDOT = -5880
391756 ZDOT = -1809
286213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6703484
57 X = -2043222
10
Y = 13186968
66 feet Y = 4019388
05 meter
Z = 16641107
41 Z = 5072209
54
XDOT = -23023
941789 XDOT = -7017
697457
YDOT = -4174
161270 feet/sec YDOT = -1272
284355 meter/sec
ZDOT = -5950
566534 ZDOT = -1813
732679
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 13325
02161162
00016717 00000-0 10270-3 0 9134
2 25544 51
6502 51
3096 0000887 68
1787 291
9458 15
50402106 19030
Satellite: ISS
Catalog Number: 25544
Epoch time: 13325
02161162 = yrday
fracday
Element set: 913
Inclination: 51
6502 deg
RA of node: 51
3096 deg
Eccentricity:
0000887
Arg of perigee: 68
1787 deg
Mean anomaly: 291
9458 deg
Mean motion: 15
50402106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1903
Checksum: 288
Coasting Arc #15 (Orbit 1917)
---------------------------------------
Vector Time (GMT): 2013/325/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4585407
79 A = 6789943
73 meter
Y = -842222
21 meter E =
0012851
Z = -4948263
23 I = 51
89572
XDOT = 3632
071591 Wp = 103
87394
YDOT = 6334
130750 meter/sec RA = 45
93360 deg
ZDOT = 2289
618881 TA = 188
46420
MA = 188
48589
Ha = 227
178 n
mi
Hp = 220
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15043988
81 X = 4618522
54
Y = -2763196
23 feet Y = -790759
87 meter
Z = -16234459
41 Z = -4925907
04
XDOT = 11916
245376 XDOT = 3549
849501
YDOT = 20781
268866 feet/sec YDOT = 6374
287045 meter/sec
ZDOT = 7511
872970 ZDOT = 2307
063980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7192981
89 X = 2192420
88
Y = -13611285
72 feet Y = -4148719
89 meter
Z = -16140273
78 Z = -4919555
45
XDOT = 22679
126534 XDOT = 6912
597768
YDOT = 2999
398119 feet/sec YDOT = 914
216547 meter/sec
ZDOT = 7584
192300 ZDOT = 2311
661813
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 13325
98846327
00016717 00000-0 10270-3 0 9143
2 25544 51
6507 46
5168 0000957 69
5830 290
5424 15
50419263 19189
Satellite: ISS
Catalog Number: 25544
Epoch time: 13325
98846327 = yrday
fracday
Element set: 914
Inclination: 51
6507 deg
RA of node: 46
5168 deg
Eccentricity:
0000957
Arg of perigee: 69
5830 deg
Mean anomaly: 290
5424 deg
Mean motion: 15
50419263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1918
Checksum: 326
Coasting Arc #16 (Orbit 1933)
---------------------------------------
Vector Time (GMT): 2013/326/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886015
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4813227
41 A = 6790658
22 meter
Y = 733508
78 meter E =
0008950
Z = 4728560
92 I = 51
87614
XDOT = -3686
592300 Wp = 63
67375
YDOT = -6111
310274 meter/sec RA = 40
99089 deg
ZDOT = -2796
634261 TA = 53
99796
MA = 53
91502
Ha = 227
232 n
mi
Hp = 220
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15791428
52 X = -4844042
26
Y = 2406524
88 feet Y = 679511
73 meter
Z = 15513651
31 Z = 4705103
61
XDOT = -12095
119095 XDOT = -3604
394835
YDOT = -20050
230557 feet/sec YDOT = -6152
076392 meter/sec
ZDOT = -9175
309254 ZDOT = -2814
344183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7691206
16 X = -2344279
64
Y = 14108921
61 feet Y = 4300399
31 meter
Z = 15414851
04 Z = 4698446
60
XDOT = -22219
788721 XDOT = -6772
591602
YDOT = -1979
117778 feet/sec YDOT = -603
235099 meter/sec
ZDOT = -9248
774226 ZDOT = -2819
026384
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 13327
01974842
00016717 00000-0 10270-3 0 9154
2 25544 51
6504 41
4050 0000986 67
9336 292
1919 15
50468511 19340
Satellite: ISS
Catalog Number: 25544
Epoch time: 13327
01974842 = yrday
fracday
Element set: 915
Inclination: 51
6504 deg
RA of node: 41
4050 deg
Eccentricity:
0000986
Arg of perigee: 67
9336 deg
Mean anomaly: 292
1919 deg
Mean motion: 15
50468511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1934
Checksum: 308
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