[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 1st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
311/10:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 221
1
314/23:26:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
0
000/00:00:00
000 0
0 0
0 221
0
Coasting Arc #1 (Orbit 1571)
---------------------------------------
Vector Time (GMT): 2013/303/14:54:52
989
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6301842
46 A = 6799860
09 meter
Y = 666672
93 meter E =
0014883
Z = 2447965
05 I = 51
79507
XDOT = 1529
412640 Wp = 77
64936
YDOT = -5271
243040 meter/sec RA = 156
26075 deg
ZDOT = 5348
404238 TA = 309
64542
MA = 309
77665
Ha = 228
554 n
mi
Hp = 221
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20675336
14 X = -6320720
76
Y = 2187247
14 feet Y = 596096
38 meter
Z = 8031381
39 Z = 2417304
74
XDOT = 5017
758004 XDOT = 1562
261545
YDOT = -17294
104463 feet/sec YDOT = -5253
956022 meter/sec
ZDOT = 17547
258000 ZDOT = 5355
914403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 722104
94 X = 220097
59
Y = -20827531
69 feet Y = -6348231
66 meter
Z = 7902477
47 Z = 2408675
13
XDOT = 14921
007381 XDOT = 4547
923050
YDOT = 7218
216625 feet/sec YDOT = 2200
112427 meter/sec
ZDOT = 17579
488259 ZDOT = 5358
228021
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 13303
68112224
00016717 00000-0 10270-3 0 9003
2 25544 51
6448 157
0216 0001403 111
0791 249
0510 15
49676047 15725
Satellite: ISS
Catalog Number: 25544
Epoch time: 13303
68112224 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 157
0216 deg
Eccentricity:
0001403
Arg of perigee: 111
0791 deg
Mean anomaly: 249
0510 deg
Mean motion: 15
49676047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1572
Checksum: 272
Coasting Arc #2 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2013/304/14:54:52
989
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6173471
79 A = 6799252
03 meter
Y = -979302
08 meter E =
0006395
Z = -2675154
50 I = 51
82162
XDOT = -1391
564626 Wp = 122
50870
YDOT = 5433
136312 meter/sec RA = 151
32093 deg
ZDOT = -5212
681829 TA = 87
52617
MA = 87
45296
Ha = 228
501 n
mi
Hp = 221
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20254172
55 X = 6196959
22
Y = -3212933
34 feet Y = -910135
30 meter
Z = -8776753
61 Z = -2645106
48
XDOT = -4565
500740 XDOT = -1426
893327
YDOT = 17825
250369 feet/sec YDOT = 5417
376957 meter/sec
ZDOT = -17101
974505 ZDOT = -5219
528378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 705256
97 X = 214962
33
Y = 20548954
48 feet Y = 6263321
33 meter
Z = -8650371
82 Z = -2636633
33
XDOT = -15646
130948 XDOT = -4768
940713
YDOT = -6657
311515 feet/sec YDOT = -2029
148550 meter/sec
ZDOT = -17131
445107 ZDOT = -5221
664469
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 13304
64842116
00016717 00000-0 10270-3 0 9011
2 25544 51
6451 152
2319 0001444 107
1901 252
9407 15
49716048 15874
Satellite: ISS
Catalog Number: 25544
Epoch time: 13304
64842116 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 152
2319 deg
Eccentricity:
0001444
Arg of perigee: 107
1901 deg
Mean anomaly: 252
9407 deg
Mean motion: 15
49716048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 289
Coasting Arc #3 (Orbit 1602)
---------------------------------------
Vector Time (GMT): 2013/305/14:54:52
989
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6020146
53 A = 6798790
13 meter
Y = 1299395
72 meter E =
0014517
Z = 2865288
12 I = 51
84615
XDOT = 1218
968236 Wp = 84
23993
YDOT = -5605
151066 meter/sec RA = 146
38181 deg
ZDOT = 5082
330689 TA = 308
20065
MA = 308
33129
Ha = 228
486 n
mi
Hp = 221
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19751136
92 X = -6048148
40
Y = 4263109
30 feet Y = 1231918
25 meter
Z = 9400551
57 Z = 2835973
88
XDOT = 3999
239621 XDOT = 1256
866410
YDOT = -18389
603235 feet/sec YDOT = -5591
307504 meter/sec
ZDOT = 16674
313283 ZDOT = 5088
344965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2155545
40 X = -657010
24
Y = -20147929
23 feet Y = -6141088
83 meter
Z = 9277200
66 Z = 2827690
76
XDOT = 16407
027125 XDOT = 5000
861868
YDOT = 5966
111643 feet/sec YDOT = 1818
470829 meter/sec
ZDOT = 16700
319063 ZDOT = 5090
257250
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 13305
68019245
00016717 00000-0 10270-3 0 9026
2 25544 51
6446 147
1220 0001458 118
9601 241
1696 15
49725184 16034
Satellite: ISS
Catalog Number: 25544
Epoch time: 13305
68019245 = yrday
fracday
Element set: 902
Inclination: 51
6446 deg
RA of node: 147
1220 deg
Eccentricity:
0001458
Arg of perigee: 118
9601 deg
Mean anomaly: 241
1696 deg
Mean motion: 15
49725184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1603
Checksum: 294
Coasting Arc #4 (Orbit 1617)
---------------------------------------
Vector Time (GMT): 2013/306/14:54:52
989
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5851041
61 A = 6798142
76 meter
Y = -1559286
31 meter E =
0005959
Z = -3092409
14 I = 51
86973
XDOT = -1054
069991 Wp = 110
23248
YDOT = 5774
212251 meter/sec RA = 141
44477 deg
ZDOT = -4915
588710 TA = 105
09179
MA = 105
02585
Ha = 228
424 n
mi
Hp = 221
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19196330
73 X = 5883065
56
Y = -5115768
74 feet Y = -1493677
35 meter
Z = -10145699
27 Z = -3063906
58
XDOT = -3458
234880 XDOT = -1094
680846
YDOT = 18944
265915 feet/sec YDOT = 5762
197637 meter/sec
ZDOT = -16127
259548 ZDOT = -4920
808396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3399678
94 X = 1036222
14
Y = 19634986
14 feet Y = 5984743
78 meter
Z = -10025712
91 Z = -3055837
29
XDOT = -17141
621868 XDOT = -5224
766345
YDOT = -5261
854358 feet/sec YDOT = -1603
813208 meter/sec
ZDOT = -16149
960736 ZDOT = -4922
508032
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 13306
64746435
00016717 00000-0 10270-3 0 9032
2 25544 51
6449 142
3320 0001455 115
8986 244
2315 15
49751927 16186
Satellite: ISS
Catalog Number: 25544
Epoch time: 13306
64746435 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 142
3320 deg
Eccentricity:
0001455
Arg of perigee: 115
8986 deg
Mean anomaly: 244
2315 deg
Mean motion: 15
49751927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1618
Checksum: 312
Coasting Arc #5 (Orbit 1633)
---------------------------------------
Vector Time (GMT): 2013/307/14:54:52
989
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5660351
83 A = 6797559
35 meter
Y = 1821295
56 meter E =
0013878
Z = 3282281
93 I = 51
89152
XDOT = 852
974886 Wp = 91
18633
YDOT = -5949
824432 meter/sec RA = 136
50840 deg
ZDOT = 4754
820373 TA = 306
70600
MA = 306
83342
Ha = 228
385 n
mi
Hp = 221
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18570708
11 X = -5696242
20
Y = 5975379
15 feet Y = 1757797
33 meter
Z = 10768641
50 Z = 3254696
37
XDOT = 2798
474036 XDOT = 896
345392
YDOT = -19520
421365 feet/sec YDOT = -5940
043292 meter/sec
ZDOT = 15599
804372 ZDOT = 4759
069692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4638541
98 X = -1413827
59
Y = -19014442
47 feet Y = -5795602
07 meter
Z = 10652459
86 Z = 3246869
77
XDOT = 17891
698610 XDOT = 5453
389736
YDOT = 4418
038485 feet/sec YDOT = 1346
618130 meter/sec
ZDOT = 15618
464970 ZDOT = 4760
508123
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 13307
67920596
00016717 00000-0 10270-3 0 9049
2 25544 51
6449 137
2220 0001451 126
2135 233
9150 15
49778259 16343
Satellite: ISS
Catalog Number: 25544
Epoch time: 13307
67920596 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 137
2220 deg
Eccentricity:
0001451
Arg of perigee: 126
2135 deg
Mean anomaly: 233
9150 deg
Mean motion: 15
49778259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1634
Checksum: 306
Coasting Arc #6 (Orbit 1648)
---------------------------------------
Vector Time (GMT): 2013/308/14:54:52
989
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5464608
37 A = 6796907
77 meter
Y = -2020690
25 meter E =
0006171
Z = -3505074
27 I = 51
91153
XDOT = -654
530610 Wp = 95
87241
YDOT = 6117
797173 meter/sec RA = 131
57373 deg
ZDOT = -4554
891664 TA = 125
04535
MA = 124
98744
Ha = 228
322 n
mi
Hp = 221
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17928505
17 X = 5503825
24
Y = -6629561
18 feet Y = -1959362
26 meter
Z = -11499587
49 Z = -3478431
63
XDOT = -2147
410138 XDOT = -700
765432
YDOT = 20071
513036 feet/sec YDOT = 6110
219262 meter/sec
ZDOT = -14943
870290 ZDOT = -4558
183742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5652529
78 X = 1722891
08
Y = 18330319
23 feet Y = 5587081
30 meter
Z = -11387326
08 Z = -3470856
99
XDOT = -18594
058677 XDOT = -5667
469085
YDOT = -3543
374997 feet/sec YDOT = -1080
020699 meter/sec
ZDOT = -14958
545182 ZDOT = -4559
364571
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 13308
64645086
00016717 00000-0 10270-3 0 9056
2 25544 51
6453 132
4318 0001409 124
3938 235
7346 15
49784632 16491
Satellite: ISS
Catalog Number: 25544
Epoch time: 13308
64645086 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 132
4318 deg
Eccentricity:
0001409
Arg of perigee: 124
3938 deg
Mean anomaly: 235
7346 deg
Mean motion: 15
49784632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1649
Checksum: 321
Coasting Arc #7 (Orbit 1664)
---------------------------------------
Vector Time (GMT): 2013/309/14:54:52
989
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5251781
92 A = 6796207
21 meter
Y = 2217520
01 meter E =
0012962
Z = 3690610
34 I = 51
93019
XDOT = 419
952438 Wp = 98
38348
YDOT = -6288
340562 meter/sec RA = 126
63980 deg
ZDOT = 4361
061977 TA = 305
27053
MA = 305
39173
Ha = 228
265 n
mi
Hp = 221
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17230255
63 X = -5294116
85
Y = 7275328
11 feet Y = 2158554
49 meter
Z = 12108301
63 Z = 3664994
17
XDOT = 1377
796711 XDOT = 469
053419
YDOT = -20631
038590 feet/sec YDOT = -6283
369905 meter/sec
ZDOT = 14307
946120 ZDOT = 4363
221307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6637811
48 X = -2023204
94
Y = -17560041
93 feet Y = -5352300
78 meter
Z = 12000310
94 Z = 3657694
77
XDOT = 19288
370842 XDOT = 5879
095433
YDOT = 2527
276881 feet/sec YDOT = 770
313993 meter/sec
ZDOT = 14317
897345 ZDOT = 4364
095111
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 13309
67816261
00016717 00000-0 10270-3 0 9066
2 25544 51
6462 127
3219 0001384 132
2734 227
8534 15
49830686 16658
Satellite: ISS
Catalog Number: 25544
Epoch time: 13309
67816261 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 127
3219 deg
Eccentricity:
0001384
Arg of perigee: 132
2734 deg
Mean anomaly: 227
8534 deg
Mean motion: 15
49830686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1665
Checksum: 318
Coasting Arc #8 (Orbit 1679)
---------------------------------------
Vector Time (GMT): 2013/310/14:54:52
989
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5045492
89 A = 6795564
42 meter
Y = -2352141
63 meter E =
0007130
Z = -3904168
14 I = 51
94606
XDOT = -184
304191 Wp = 84
09097
YDOT = 6444
247362 meter/sec RA = 121
70718 deg
ZDOT = -4126
403689 TA = 142
72807
MA = 142
67857
Ha = 228
201 n
mi
Hp = 221
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16553454
36 X = 5090385
87
Y = -7717000
08 feet Y = -2295468
62 meter
Z = -12808950
58 Z = -3879548
06
XDOT = -604
672544 XDOT = -236
306099
YDOT = 21142
543839 feet/sec YDOT = 6441
895686 meter/sec
ZDOT = -13538
069847 ZDOT = -4127
425215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7393590
30 X = 2253566
32
Y = 16779544
45 feet Y = 5114405
15 meter
Z = -12705111
85 Z = -3872518
09
XDOT = -19903
776932 XDOT = -6066
671209
YDOT = -1470
026859 feet/sec YDOT = -448
064187 meter/sec
ZDOT = -13543
272253 ZDOT = -4127
989383
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 13310
64538033
00016717 00000-0 10270-3 0 9074
2 25544 51
6466 122
5319 0001321 131
7333 228
3930 15
49819998 16806
Satellite: ISS
Catalog Number: 25544
Epoch time: 13310
64538033 = yrday
fracday
Element set: 907
Inclination: 51
6466 deg
RA of node: 122
5319 deg
Eccentricity:
0001321
Arg of perigee: 131
7333 deg
Mean anomaly: 228
3930 deg
Mean motion: 15
49819998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1680
Checksum: 304
Coasting Arc #9 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2013/311/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2360038
80 A = 6791329
78 meter
Y = -3935313
66 meter E =
0006606
Z = 5002374
48 I = 51
94375
XDOT = 4800
710670 Wp = 64
09777
YDOT = -5584
758485 meter/sec RA = 117
63612 deg
ZDOT = -2123
587527 TA = 46
53143
MA = 46
47651
Ha = 228
143 n
mi
Hp = 221
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7742909
44 X = -2340158
47
Y = -12911134
05 feet Y = -3961594
06 meter
Z = 16411989
75 Z = 4990957
62
XDOT = 15750
363091 XDOT = 4873
119869
YDOT = -18322
698443 feet/sec YDOT = -5530
668977 meter/sec
ZDOT = -6967
150678 ZDOT = -2100
089922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12413357
73 X = 3783591
44
Y = 8608926
43 feet Y = 2624000
78 meter
Z = 16364546
20 Z = 4987913
68
XDOT = -6358
696153 XDOT = -1938
130587
YDOT = 22254
300344 feet/sec YDOT = 6783
110745 meter/sec
ZDOT = -6867
559162 ZDOT = -2093
232032
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 13311
48362246
00016717 00000-0 10270-3 0 9089
2 25544 51
6454 118
3826 0000903 118
8089 241
3152 15
49834420 16930
Satellite: ISS
Catalog Number: 25544
Epoch time: 13311
48362246 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 118
3826 deg
Eccentricity:
0000903
Arg of perigee: 118
8089 deg
Mean anomaly: 241
3152 deg
Mean motion: 15
49834420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 303
Coasting Arc #10 (Orbit 1707)
---------------------------------------
Vector Time (GMT): 2013/312/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2485503
14 A = 6791680
71 meter
Y = 4001941
72 meter E =
0012884
Z = -4904293
08 I = 51
95815
XDOT = -4452
090161 Wp = 108
42068
YDOT = 5731
658754 meter/sec RA = 112
70171 deg
ZDOT = 2422
010220 TA = 185
27247
MA = 185
28605
Ha = 228
045 n
mi
Hp = 221
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8154537
86 X = 2464391
88
Y = 13129730
04 feet Y = 4029618
21 meter
Z = -16090200
38 Z = -4892269
78
XDOT = -14606
595017 XDOT = -4527
617580
YDOT = 18804
654706 feet/sec YDOT = 5681
450322 meter/sec
ZDOT = 7946
227755 ZDOT = 2400
198675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13023227
79 X = -3969479
83
Y = -8419491
11 feet Y = -2566260
89 meter
Z = -16040216
78 Z = -4889058
07
XDOT = 4738
290067 XDOT = 1444
230812
YDOT = -22283
566419 feet/sec YDOT = -6792
031045 meter/sec
ZDOT = 7853
687351 ZDOT = 2393
803905
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
45081452
00016717 00000-0 10270-3 0 9095
2 25544 51
6449 113
5909 0001041 119
7802 240
3452 15
49870094 17086
Satellite: ISS
Catalog Number: 25544
Epoch time: 13312
45081452 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 113
5909 deg
Eccentricity:
0001041
Arg of perigee: 119
7802 deg
Mean anomaly: 240
3452 deg
Mean motion: 15
49870094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1708
Checksum: 295
Coasting Arc #11 (Orbit 1723)
---------------------------------------
Vector Time (GMT): 2013/313/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2608456
37 A = 6792201
22 meter
Y = -4071411
44 meter E =
0008188
Z = 4764824
83 I = 51
97107
XDOT = 4123
489466 Wp = 68
41849
YDOT = -5852
748021 meter/sec RA = 107
76959 deg
ZDOT = -2736
947825 TA = 48
57367
MA = 48
50335
Ha = 228
088 n
mi
Hp = 221
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8557927
71 X = -2585881
58
Y = -13357649
08 feet Y = -4100454
62 meter
Z = 15632627
38 Z = 4752207
87
XDOT = 13528
508747 XDOT = 4201
925228
YDOT = -19201
929203 feet/sec YDOT = -5806
197987 meter/sec
ZDOT = -8979
487616 ZDOT = -2716
725508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13626031
55 X = 4153214
42
Y = 8223983
09 feet Y = 2506670
05 meter
Z = 15580157
92 Z = 4748832
13
XDOT = -3214
632923 XDOT = -979
820115
YDOT = 22216
729229 feet/sec YDOT = 6771
659069 meter/sec
ZDOT = -8893
598421 ZDOT = -2710
768799
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
48247100
00016717 00000-0 10270-3 0 9105
2 25544 51
6450 108
4812 0000955 124
0905 236
0337 15
49873070 17249
Satellite: ISS
Catalog Number: 25544
Epoch time: 13313
48247100 = yrday
fracday
Element set: 910
Inclination: 51
6450 deg
RA of node: 108
4812 deg
Eccentricity:
0000955
Arg of perigee: 124
0905 deg
Mean anomaly: 236
0337 deg
Mean motion: 15
49873070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1724
Checksum: 278
Coasting Arc #12 (Orbit 1738)
---------------------------------------
Vector Time (GMT): 2013/314/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2769762
85 A = 6792652
30 meter
Y = 4138852
36 meter E =
0011237
Z = -4630442
75 I = 51
98154
XDOT = -3780
972031 Wp = 111
49724
YDOT = 5920
991784 meter/sec RA = 102
83706 deg
ZDOT = 3032
661640 TA = 188
69678
MA = 188
71627
Ha = 227
988 n
mi
Hp = 221
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9087148
46 X = 2745769
14
Y = 13578911
94 feet Y = 4169691
36 meter
Z = -15191741
29 Z = -4617045
69
XDOT = -12404
763882 XDOT = -3861
632880
YDOT = 19425
826064 feet/sec YDOT = 5878
259608 meter/sec
ZDOT = 9949
677296 ZDOT = 3014
097761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14335087
59 X = -4369334
70
Y = -7947251
74 feet Y = -2422322
33 meter
Z = -15136002
57 Z = -4613453
58
XDOT = 1737
072150 XDOT = 529
459591
YDOT = -21920
705375 feet/sec YDOT = -6681
430998 meter/sec
ZDOT = 9870
740628 ZDOT = 3008
601743
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
44963502
00016717 00000-0 10270-3 0 9114
2 25544 51
6450 103
6897 0001112 124
3672 235
7584 15
49913462 17395
Satellite: ISS
Catalog Number: 25544
Epoch time: 13314
44963502 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 103
6897 deg
Eccentricity:
0001112
Arg of perigee: 124
3672 deg
Mean anomaly: 235
7584 deg
Mean motion: 15
49913462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1739
Checksum: 303
Coasting Arc #13 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2013/314/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4187004
00 A = 6792351
98 meter
Y = 2565211
74 meter E =
0009034
Z = 4687875
58 I = 51
98448
XDOT = -1039
327291 Wp = 115
62595
YDOT = -7016
884901 meter/sec RA = 100
23431 deg
ZDOT = 2903
218335 TA = 305
59523
MA = 305
67937
Ha = 228
006 n
mi
Hp = 220
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13736889
77 X = -4238150
29
Y = 8416049
02 feet Y = 2518104
15 meter
Z = 15380169
24 Z = 4667410
94
XDOT = -3409
866441 XDOT = -974
888914
YDOT = -23021
275921 feet/sec YDOT = -7028
146944 meter/sec
ZDOT = 9524
994538 ZDOT = 2898
326028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4928228
21 X = -1502123
96
Y = 15423883
43 feet Y = 4701199
67 meter
Z = 15293724
66 Z = 4661527
28
XDOT = -16585
374456 XDOT = -5055
222134
YDOT = -14751
240409 feet/sec YDOT = -4496
178077 meter/sec
ZDOT = 9505
447903 ZDOT = 2897
260521
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
02992615
00016717 00000-0 10270-3 0 9127
2 25544 51
6452 100
8188 0000865 115
7511 244
3729 15
49940764 17481
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
02992615 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 100
8188 deg
Eccentricity:
0000865
Arg of perigee: 115
7511 deg
Mean anomaly: 244
3729 deg
Mean motion: 15
49940764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1748
Checksum: 312
Coasting Arc #14 (Orbit 1762)
---------------------------------------
Vector Time (GMT): 2013/315/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4039362
67 A = 6791762
20 meter
Y = -2538218
42 meter E =
0012188
Z = -4845600
81 I = 51
98720
XDOT = 1362
927617 Wp = 74
68484
YDOT = 7076
132441 meter/sec RA = 95
30187 deg
ZDOT = -2572
718004 TA = 170
06537
MA = 170
04125
Ha = 227
937 n
mi
Hp = 221
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13252502
21 X = 4090984
35
Y = -8327488
25 feet Y = -2492759
24 meter
Z = -15897640
47 Z = -4825852
18
XDOT = 4471
547299 XDOT = 1296
197201
YDOT = 23215
657616 feet/sec YDOT = 7091
000359 meter/sec
ZDOT = -8440
675865 ZDOT = -2566
259274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4363473
82 X = 1329986
82
Y = -15118924
20 feet Y = -4608248
09 meter
Z = -15814204
86 Z = -4820169
64
XDOT = 17779
538600 XDOT = 5419
203365
YDOT = 13925
079299 feet/sec YDOT = 4244
364170 meter/sec
ZDOT = -8414
559752 ZDOT = -2564
757812
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
99706854
00016717 00000-0 10270-3 0 9132
2 25544 51
6454 96
0272 0000952 110
5682 249
5571 15
49937667 17639
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
99706854 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 96
0272 deg
Eccentricity:
0000952
Arg of perigee: 110
5682 deg
Mean anomaly: 249
5571 deg
Mean motion: 15
49937667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1763
Checksum: 335
Coasting Arc #15 (Orbit 1778)
---------------------------------------
Vector Time (GMT): 2013/316/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3896639
80 A = 6791068
34 meter
Y = 2499775
26 meter E =
0007221
Z = 4964454
80 I = 51
98766
XDOT = -1707
089847 Wp = 121
15078
YDOT = -7127
469243 meter/sec RA = 90
37084 deg
ZDOT = 2242
979149 TA = 307
01234
MA = 307
07840
Ha = 227
892 n
mi
Hp = 220
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12784251
32 X = -3948419
66
Y = 8201362
41 feet Y = 2455911
23 meter
Z = 16287581
35 Z = 4945399
05
XDOT = -5600
688476 XDOT = -1638
158025
YDOT = -23384
085442 feet/sec YDOT = -7146
173503 meter/sec
ZDOT = 7358
855477 ZDOT = 2234
853814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3847582
99 X = -1172743
30
Y = 14782153
15 feet Y = 4505600
28 meter
Z = 16207059
78 Z = 4939911
82
XDOT = -18982
879168 XDOT = -5785
981571
YDOT = -12994
714372 feet/sec YDOT = -3960
788941 meter/sec
ZDOT = 7325
749617 ZDOT = 2232
888483
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
02866961
00016717 00000-0 10270-3 0 9145
2 25544 51
6457 90
9175 0000750 113
6677 246
4552 15
49992762 17790
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
02866961 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 90
9175 deg
Eccentricity:
0000750
Arg of perigee: 113
6677 deg
Mean anomaly: 246
4552 deg
Mean motion: 15
49992762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1779
Checksum: 339
Coasting Arc #16 (Orbit 1793)
---------------------------------------
Vector Time (GMT): 2013/317/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3797803
71 A = 6790594
82 meter
Y = -2429716
47 meter E =
0013725
Z = -5090316
56 I = 51
98570
XDOT = 2043
220040 Wp = 77
77058
YDOT = 7129
474520 meter/sec RA = 85
43767 deg
ZDOT = -1880
088858 TA = 174
06408
MA = 174
04779
Ha = 227
807 n
mi
Hp = 221
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12459985
94 X = 3849419
01
Y = -7971510
73 feet Y = -2386958
57 meter
Z = -16700513
64 Z = -5071741
31
XDOT = 6703
477822 XDOT = 1972
477988
YDOT = 23390
664435 feet/sec YDOT = 7151
927507 meter/sec
ZDOT = -6168
270530 ZDOT = -1870
334916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3520409
32 X = 1073020
76
Y = -14457476
87 feet Y = -4406638
95 meter
Z = -16622017
61 Z = -5066390
97
XDOT = 20025
624251 XDOT = 6103
810272
YDOT = 11916
602377 feet/sec YDOT = 3632
180405 meter/sec
ZDOT = -6128
329558 ZDOT = -1867
914849
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
99578272
00016717 00000-0 10270-3 0 9157
2 25544 51
6461 86
1256 0000806 107
5488 252
5751 15
49987549 17949
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
99578272 = yrday
fracday
Element set: 915
Inclination: 51
6461 deg
RA of node: 86
1256 deg
Eccentricity:
0000806
Arg of perigee: 107
5488 deg
Mean anomaly: 252
5751 deg
Mean motion: 15
49987549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1794
Checksum: 350
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