[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 25th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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
269/02:47:15
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 219
4
272/11:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 219
1
275/19:14:34
943 1
5 6
9 6
9
N/A -6
6 0
0 228
0
000/00:05:09
887 -1
7 0
2 222
8
Coasting Arc #1 (Orbit 1026)
---------------------------------------
Vector Time (GMT): 2013/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3625494
94 A = 6795931
48 meter
Y = 4847274
35 meter E =
0015761
Z = 3074952
79 I = 51
48484
XDOT = -5781
001092 Wp = 92
29959
YDOT = -1210
453375 meter/sec RA = 330
64153 deg
ZDOT = -4886
812822 TA = 52
33168
MA = 52
18882
Ha = 227
756 n
mi
Hp = 219
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11894668
43 X = -3694366
18
Y = 15903131
07 feet Y = 4806346
92 meter
Z = 10088427
80 Z = 3057172
66
XDOT = -18966
539017 XDOT = -5743
296864
YDOT = -3971
303724 feet/sec YDOT = -1274
889765 meter/sec
ZDOT = -16032
850465 ZDOT = -4914
804959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10920059
38 X = 3328434
10
Y = -16633064
59 feet Y = -5069758
09 meter
Z = 10013119
18 Z = 3051998
73
XDOT = 17868
350722 XDOT = 5446
273300
YDOT = 1966
723859 feet/sec YDOT = 599
457432 meter/sec
ZDOT = -16150
065528 ZDOT = -4922
539973
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 13268
53853518
00016717 00000-0 10270-3 0 9005
2 25544 51
6494 331
0433 0002849 76
9259 283
2209 15
50511964 10272
Satellite: ISS
Catalog Number: 25544
Epoch time: 13268
53853518 = yrday
fracday
Element set: 900
Inclination: 51
6494 deg
RA of node: 331
0433 deg
Eccentricity:
0002849
Arg of perigee: 76
9259 deg
Mean anomaly: 283
2209 deg
Mean motion: 15
50511964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1027
Checksum: 311
Coasting Arc #2 (Orbit 1035)
---------------------------------------
Vector Time (GMT): 2013/269/02:47:15
000
Vector Time (MET): N/A
Weight (LBS) : 929266
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5008653
70 A = 6799260
37 meter
Y = -4404891
50 meter E =
0011352
Z = -1299215
38 I = 51
47713
XDOT = 4054
806543 Wp = 46
01581
YDOT = 2907
577373 meter/sec RA = 327
59033 deg
ZDOT = 5813
349569 TA = 299
83922
MA = 299
95201
Ha = 227
767 n
mi
Hp = 219
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16432590
87 X = 5063849
19
Y = -14451743
77 feet Y = -4348573
04 meter
Z = -4262517
65 Z = -1274749
22
XDOT = 13303
171074 XDOT = 3993
752133
YDOT = 9539
295842 feet/sec YDOT = 2952
579864 meter/sec
ZDOT = 19072
669189 ZDOT = 5832
899068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1010181
72 X = 307903
39
Y = -21879951
38 feet Y = -6669009
18 meter
Z = -4159237
66 Z = -1267735
64
XDOT = 14422
661690 XDOT = 4396
027283
YDOT = -2950
004337 feet/sec YDOT = -899
161322 meter/sec
ZDOT = 19154
217173 ZDOT = 5838
205394
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 13269
11861331
00016717 00000-0 10270-3 0 9013
2 25544 51
6472 328
1664 0002816 74
5601 285
5861 15
50484248 10363
Satellite: ISS
Catalog Number: 25544
Epoch time: 13269
11861331 = yrday
fracday
Element set: 901
Inclination: 51
6472 deg
RA of node: 328
1664 deg
Eccentricity:
0002816
Arg of perigee: 74
5601 deg
Mean anomaly: 285
5861 deg
Mean motion: 15
50484248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1036
Checksum: 300
Coasting Arc #3 (Orbit 1051)
---------------------------------------
Vector Time (GMT): 2013/270/02:47:15
000
Vector Time (MET): N/A
Weight (LBS) : 929266
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4967165
95 A = 6799531
83 meter
Y = 4569449
19 meter E =
0015195
Z = 772979
50 I = 51
45345
XDOT = -3760
906463 Wp = 118
06228
YDOT = -3071
413616 meter/sec RA = 322
62371 deg
ZDOT = -5928
729743 TA = 53
57236
MA = 53
43236
Ha = 227
667 n
mi
Hp = 219
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16296476
21 X = -5021648
30
Y = 14991631
22 feet Y = 4513598
62 meter
Z = 2536021
97 Z = 748716
64
XDOT = -12338
931965 XDOT = -3697
481412
YDOT = -10076
816326 feet/sec YDOT = -3113
116299 meter/sec
ZDOT = -19451
213067 ZDOT = -5946
845677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -138516
06 X = -42219
70
Y = 22154324
15 feet Y = 6752638
00 meter
Z = 2433574
69 Z = 741753
56
XDOT = -14085
801406 XDOT = -4293
352269
YDOT = 2087
769742 feet/sec YDOT = 636
352217 meter/sec
ZDOT = -19526
725111 ZDOT = -5951
745814
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 13270
14985402
00016717 00000-0 10270-3 0 9025
2 25544 51
6475 323
0538 0002885 75
2399 284
9071 15
50546231 10523
Satellite: ISS
Catalog Number: 25544
Epoch time: 13270
14985402 = yrday
fracday
Element set: 902
Inclination: 51
6475 deg
RA of node: 323
0538 deg
Eccentricity:
0002885
Arg of perigee: 75
2399 deg
Mean anomaly: 284
9071 deg
Mean motion: 15
50546231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1052
Checksum: 302
Coasting Arc #4 (Orbit 1066)
---------------------------------------
Vector Time (GMT): 2013/271/02:47:15
000
Vector Time (MET): N/A
Weight (LBS) : 929266
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4862870
39 A = 6799817
02 meter
Y = -4736477
01 meter E =
0013923
Z = -282187
90 I = 51
42917
XDOT = 3508
312940 Wp = 50
73617
YDOT = 3257
825675 meter/sec RA = 317
65405 deg
ZDOT = 5982
834032 TA = 306
21868
MA = 306
34731
Ha = 227
745 n
mi
Hp = 219
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15954299
18 X = 4916844
09
Y = -15539622
73 feet Y = -4681795
54 meter
Z = -925813
32 Z = -258432
93
XDOT = 11510
213057 XDOT = 3442
559382
YDOT = 10688
404447 feet/sec YDOT = 3296
690722 meter/sec
ZDOT = 19628
720576 ZDOT = 5999
717164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -885461
25 X = -269888
59
Y = -22257834
87 feet Y = -6784188
07 meter
Z = -825477
30 Z = -251605
48
XDOT = 13940
202560 XDOT = 4248
973740
YDOT = -1256
892066 feet/sec YDOT = -383
100702 meter/sec
ZDOT = 19699
036752 ZDOT = 6004
266402
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 13271
11663336
00016717 00000-0 10270-3 0 9033
2 25544 51
6464 318
2597 0002890 83
0082 277
1398 15
50517702 10677
Satellite: ISS
Catalog Number: 25544
Epoch time: 13271
11663336 = yrday
fracday
Element set: 903
Inclination: 51
6464 deg
RA of node: 318
2597 deg
Eccentricity:
0002890
Arg of perigee: 83
0082 deg
Mean anomaly: 277
1398 deg
Mean motion: 15
50517702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1067
Checksum: 304
Coasting Arc #5 (Orbit 1082)
---------------------------------------
Vector Time (GMT): 2013/272/02:47:15
000
Vector Time (MET): N/A
Weight (LBS) : 929266
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4756480
63 A = 6799617
21 meter
Y = 4844755
76 meter E =
0013433
Z = -265566
40 I = 51
40729
XDOT = -3255
239728 Wp = 126
28530
YDOT = -3511
767330 meter/sec RA = 312
68434 deg
ZDOT = -5981
546310 TA = 56
58105
MA = 56
45264
Ha = 227
639 n
mi
Hp = 219
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15605251
40 X = -4809012
18
Y = 15894867
99 feet Y = 4791272
03 meter
Z = -871280
83 Z = -288801
07
XDOT = -10679
920367 XDOT = -3186
671628
YDOT = -11521
546358 feet/sec YDOT = -3547
786676 meter/sec
ZDOT = -19624
495769 ZDOT = -5997
193124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1772495
88 X = 540256
74
Y = 22200186
23 feet Y = 6766616
76 meter
Z = -969443
09 Z = -295486
25
XDOT = -14004
023827 XDOT = -4268
426463
YDOT = 286
572640 feet/sec YDOT = 87
347341 meter/sec
ZDOT = -19689
592580 ZDOT = -6001
387818
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 13272
14785156
00016717 00000-0 10270-3 0 9043
2 25544 51
6466 313
1469 0002961 83
0080 277
1408 15
50582832 10834
Satellite: ISS
Catalog Number: 25544
Epoch time: 13272
14785156 = yrday
fracday
Element set: 904
Inclination: 51
6466 deg
RA of node: 313
1469 deg
Eccentricity:
0002961
Arg of perigee: 83
0080 deg
Mean anomaly: 277
1408 deg
Mean motion: 15
50582832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1083
Checksum: 301
Coasting Arc #6 (Orbit 1088)
---------------------------------------
Vector Time (GMT): 2013/272/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5459964
72 A = 6796575
28 meter
Y = -2973993
22 meter E =
0016569
Z = 2727394
24 I = 51
39118
XDOT = 511
467559 Wp = 80
73178
YDOT = 5669
918027 meter/sec RA = 310
91772 deg
ZDOT = 5134
538090 TA = 310
20464
MA = 310
34953
Ha = 227
751 n
mi
Hp = 219
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17913270
09 X = 5479565
79
Y = -9757195
61 feet Y = -2912826
56 meter
Z = 8948143
82 Z = 2753966
22
XDOT = 1678
043173 XDOT = 423
085018
YDOT = 18602
093265 feet/sec YDOT = 5675
143922 meter/sec
ZDOT = 16845
597409 ZDOT = 5136
807513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18054516
68 X = -5503016
68
Y = 9386577
05 feet Y = 2861028
68 meter
Z = 9060021
44 Z = 2761494
53
XDOT = -505
304649 XDOT = -154
016857
YDOT = -17315
290605 feet/sec YDOT = -5277
700576 meter/sec
ZDOT = 16854
274056 ZDOT = 5137
182732
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 13272
53455778
00016717 00000-0 10270-3 0 9051
2 25544 51
6485 311
2322 0003173 88
7227 271
4288 15
50536213 10894
Satellite: ISS
Catalog Number: 25544
Epoch time: 13272
53455778 = yrday
fracday
Element set: 905
Inclination: 51
6485 deg
RA of node: 311
2322 deg
Eccentricity:
0003173
Arg of perigee: 88
7227 deg
Mean anomaly: 271
4288 deg
Mean motion: 15
50536213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1089
Checksum: 309
Coasting Arc #7 (Orbit 1103)
---------------------------------------
Vector Time (GMT): 2013/273/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5253938
01 A = 6795295
21 meter
Y = 2906120
62 meter E =
0007742
Z = -3188001
86 I = 51
36863
XDOT = -400
929636 Wp = 95
96099
YDOT = -5962
476194 meter/sec RA = 305
94250 deg
ZDOT = -4785
377709 TA = 120
93226
MA = 120
85614
Ha = 227
725 n
mi
Hp = 219
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17237329
42 X = -5270557
91
Y = 9534516
47 feet Y = 2847274
45 meter
Z = -10459323
70 Z = -3213565
79
XDOT = -1315
385944 XDOT = -310
979983
YDOT = -19561
929769 feet/sec YDOT = -5966
457256 meter/sec
ZDOT = -15700
058101 ZDOT = -4787
106225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17204311
60 X = 5243874
18
Y = -9475287
10 feet Y = -2888067
51 meter
Z = -10566956
93 Z = -3220808
47
XDOT = 460
357345 XDOT = 140
316919
YDOT = 18312
599091 feet/sec YDOT = 5581
680203 meter/sec
ZDOT = -15706
432121 ZDOT = -4787
320511
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 13273
50131040
00016717 00000-0 10270-3 0 9063
2 25544 51
6492 306
4389 0003185 91
6289 268
5227 15
50576765 11049
Satellite: ISS
Catalog Number: 25544
Epoch time: 13273
50131040 = yrday
fracday
Element set: 906
Inclination: 51
6492 deg
RA of node: 306
4389 deg
Eccentricity:
0003185
Arg of perigee: 91
6289 deg
Mean anomaly: 268
5227 deg
Mean motion: 15
50576765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1104
Checksum: 306
Coasting Arc #8 (Orbit 1119)
---------------------------------------
Vector Time (GMT): 2013/274/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5030777
09 A = 6794171
00 meter
Y = -2818880
01 meter E =
0015256
Z = 3580075
65 I = 51
34626
XDOT = 357
245823 Wp = 93
33265
YDOT = 6261
010570 meter/sec RA = 300
96508 deg
ZDOT = 4410
606729 TA = 309
15244
MA = 309
28792
Ha = 227
712 n
mi
Hp = 219
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16505174
18 X = 5044533
41
Y = -9248294
00 feet Y = -2762545
28 meter
Z = 11745655
03 Z = 3604548
60
XDOT = 1172
066350 XDOT = 265
781648
YDOT = 20541
373261 feet/sec YDOT = 6264
494691 meter/sec
ZDOT = 14470
494517 ZDOT = 4412
119223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16302666
05 X = -4969052
61
Y = 9473314
15 feet Y = 2887466
15 meter
Z = 11848693
05 Z = 3611481
64
XDOT = -674
764439 XDOT = -205
668201
YDOT = -19336
776609 feet/sec YDOT = -5893
849510 meter/sec
ZDOT = 14475
928804 ZDOT = 4412
263099
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 13274
53250249
00016717 00000-0 10270-3 0 9071
2 25544 51
6480 301
3261 0003303 93
8652 266
2876 15
50574483 11207
Satellite: ISS
Catalog Number: 25544
Epoch time: 13274
53250249 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 301
3261 deg
Eccentricity:
0003303
Arg of perigee: 93
8652 deg
Mean anomaly: 266
2876 deg
Mean motion: 15
50574483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1120
Checksum: 292
Coasting Arc #9 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2013/275/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4834021
74 A = 6792805
08 meter
Y = 2651014
11 meter E =
0009955
Z = -3978050
49 I = 51
32799
XDOT = -335
782156 Wp = 80
05860
YDOT = -6542
033810 meter/sec RA = 295
98513 deg
ZDOT = -3958
458026 TA = 148
48508
MA = 148
42541
Ha = 227
695 n
mi
Hp = 218
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15859651
37 X = -4843982
25
Y = 8697552
86 feet Y = 2596900
74 meter
Z = -13051346
75 Z = -4001558
47
XDOT = -1101
647494 XDOT = -243
373485
YDOT = -21463
365520 feet/sec YDOT = -6545
272622 meter/sec
ZDOT = -12987
067014 ZDOT = -3959
863839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15501066
65 X = 4724725
11
Y = -9181502
37 feet Y = -2798521
92 meter
Z = -13150306
71 Z = -4008213
48
XDOT = 1016
316548 XDOT = 309
773284
YDOT = 20292
036032 feet/sec YDOT = 6185
012582 meter/sec
ZDOT = -12992
023231 ZDOT = -3959
968681
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 13275
49923339
00016717 00000-0 10270-3 0 9085
2 25544 51
6489 296
5327 0003239 97
2593 262
8926 15
50609857 11352
Satellite: ISS
Catalog Number: 25544
Epoch time: 13275
49923339 = yrday
fracday
Element set: 908
Inclination: 51
6489 deg
RA of node: 296
5327 deg
Eccentricity:
0003239
Arg of perigee: 97
2593 deg
Mean anomaly: 262
8926 deg
Mean motion: 15
50609857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1135
Checksum: 351
Coasting Arc #10 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2013/275/19:17:09
887
Vector Time (MET): N/A
Weight (LBS) : 938797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4298758
85 A = 6791714
06 meter
Y = -655598
74 meter E =
0012024
Z = -5227568
78 I = 51
30743
XDOT = 2352
234932 Wp = 90
25431
YDOT = -7207
737731 meter/sec RA = 294
33577 deg
ZDOT = -1032
486771 TA = 169
80270
MA = 169
77829
Ha = 227
968 n
mi
Hp = 222
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14103539
55 X = -4265713
99
Y = -2150914
51 feet Y = -703486
20 meter
Z = -17150816
21 Z = -5248371
57
XDOT = 7717
306206 XDOT = 2437
674197
YDOT = -23647
433501 feet/sec YDOT = -7180
955977 meter/sec
ZDOT = -3387
423791 ZDOT = -1020
851150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5166890
40 X = -1574868
19
Y = -13184947
51 feet Y = -4018772
00 meter
Z = -17237956
97 Z = -5254129
28
XDOT = 23374
474245 XDOT = 7124
539750
YDOT = -4805
426808 feet/sec YDOT = -1464
694091 meter/sec
ZDOT = -3337
599917 ZDOT = -1017
300455
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 13275
82148100
00016717 00000-0 10270-3 0 9098
2 25544 51
6490 294
9355 0002962 226
5264 133
5640 15
49326246 11400
Satellite: ISS
Catalog Number: 25544
Epoch time: 13275
82148100 = yrday
fracday
Element set: 909
Inclination: 51
6490 deg
RA of node: 294
9355 deg
Eccentricity:
0002962
Arg of perigee: 226
5264 deg
Mean anomaly: 133
5640 deg
Mean motion: 15
49326246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1140
Checksum: 302
Coasting Arc #11 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2013/276/19:17:09
887
Vector Time (MET): N/A
Weight (LBS) : 938797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4302200
80 A = 6791552
54 meter
Y = 418338
13 meter E =
0003692
Z = 5238451
64 I = 51
29494
XDOT = -1825
768323 Wp = 171
49883
YDOT = 7384
859496 meter/sec RA = 289
36329 deg
ZDOT = 906
039815 TA = 269
76317
MA = 269
80547
Ha = 227
704 n
mi
Hp = 223
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14114832
01 X = 4271755
81
Y = 1372500
44 feet Y = 466278
63 meter
Z = 17186521
14 Z = 5259277
58
XDOT = -5990
053552 XDOT = -1912
613098
YDOT = 24228
541654 feet/sec YDOT = 7363
957152 meter/sec
ZDOT = 2972
571570 ZDOT = 896
958246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6064989
02 X = 1848608
65
Y = 12701212
78 feet Y = 3871329
66 meter
Z = 17273790
87 Z = 5265051
46
XDOT = -22920
244238 XDOT = -6986
090444
YDOT = 6938
911252 feet/sec YDOT = 2114
980150 meter/sec
ZDOT = 2933
443519 ZDOT = 894
113585
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 13276
85350894
00016717 00000-0 10270-3 0 9109
2 25544 51
6485 289
8281 0003070 231
4811 128
6065 15
49352888 11563
Satellite: ISS
Catalog Number: 25544
Epoch time: 13276
85350894 = yrday
fracday
Element set: 910
Inclination: 51
6485 deg
RA of node: 289
8281 deg
Eccentricity:
0003070
Arg of perigee: 231
4811 deg
Mean anomaly: 128
6065 deg
Mean motion: 15
49352888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 326
Coasting Arc #12 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2013/277/19:17:09
887
Vector Time (MET): N/A
Weight (LBS) : 938797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4301448
16 A = 6791452
15 meter
Y = -206370
66 meter E =
0012040
Z = -5262014
84 I = 51
28590
XDOT = 1292
666957 Wp = 90
75888
YDOT = -7503
127077 meter/sec RA = 284
38927 deg
ZDOT = -764
109208 TA = 171
89806
MA = 171
87860
Ha = 227
751 n
mi
Hp = 222
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14112362
73 X = -4273258
92
Y = -677069
11 feet Y = -254315
33 meter
Z = -17263828
23 Z = -5282842
72
XDOT = 4241
033325 XDOT = 1380
184395
YDOT = -24616
558653 feet/sec YDOT = -7488
182424 meter/sec
ZDOT = -2506
919973 ZDOT = -757
615802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6870032
22 X = -2093985
82
Y = -12222837
93 feet Y = -3725521
00 meter
Z = -17351134
25 Z = -5288625
72
XDOT = 22221
999421 XDOT = 6773
265423
YDOT = -8979
407113 feet/sec YDOT = -2736
923288 meter/sec
ZDOT = -2478
636842 ZDOT = -755
488509
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 13277
82102620
00016717 00000-0 10270-3 0 9110
2 25544 51
6490 285
0395 0002945 235
6769 124
4103 15
49363357 11718
Satellite: ISS
Catalog Number: 25544
Epoch time: 13277
82102620 = yrday
fracday
Element set: 911
Inclination: 51
6490 deg
RA of node: 285
0395 deg
Eccentricity:
0002945
Arg of perigee: 235
6769 deg
Mean anomaly: 124
4103 deg
Mean motion: 15
49363357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1171
Checksum: 302
Coasting Arc #13 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2013/278/19:17:09
887
Vector Time (MET): N/A
Weight (LBS) : 938797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284210
75 A = 6791328
00 meter
Y = -9113
63 meter E =
0002745
Z = 5269699
30 I = 51
27891
XDOT = -753
541755 Wp = 178
86320
YDOT = 7598
278613 meter/sec RA = 279
41482 deg
ZDOT = 623
061647 TA = 265
13762
MA = 265
16896
Ha = 227
510 n
mi
Hp = 223
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14055809
56 X = 4258394
97
Y = -29900
36 feet Y = 38651
47 meter
Z = 17289039
71 Z = 5290449
31
XDOT = -2472
249852 XDOT = -841
478096
YDOT = 24928
735606 feet/sec YDOT = 7589
360429 meter/sec
ZDOT = 2044
165507 ZDOT = 619
186372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7640550
62 X = 2328839
83
Y = 11669297
21 feet Y = 3556801
79 meter
Z = 17376048
44 Z = 5296219
56
XDOT = -21389
936308 XDOT = -6519
652587
YDOT = 10974
010375 feet/sec YDOT = 3344
878362 meter/sec
ZDOT = 2026
853803 ZDOT = 617
785039
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 13278
85303210
00016717 00000-0 10270-3 0 9123
2 25544 51
6490 279
9317 0003022 239
9259 120
1591 15
49382068 11873
Satellite: ISS
Catalog Number: 25544
Epoch time: 13278
85303210 = yrday
fracday
Element set: 912
Inclination: 51
6490 deg
RA of node: 279
9317 deg
Eccentricity:
0003022
Arg of perigee: 239
9259 deg
Mean anomaly: 120
1591 deg
Mean motion: 15
49382068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 310
Coasting Arc #14 (Orbit 1201)
---------------------------------------
Vector Time (GMT): 2013/279/19:17:09
887
Vector Time (MET): N/A
Weight (LBS) : 938797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4268993
96 A = 6791227
68 meter
Y = 203122
95 meter E =
0012003
Z = -5288230
93 I = 51
27499
XDOT = 215
787795 Wp = 91
48788
YDOT = -7634
609896 meter/sec RA = 274
43943 deg
ZDOT = -468
678315 TA = 174
01646
MA = 174
00211
Ha = 227
540 n
mi
Hp = 222
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14005885
71 X = -4245258
69
Y = 666413
87 feet Y = 155516
48 meter
Z = -17349839
02 Z = -5308912
14
XDOT = 707
965208 XDOT = 303
420406
YDOT = -25047
932731 feet/sec YDOT = -7631
706889 meter/sec
ZDOT = -1537
658514 ZDOT = -467
416329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8339126
58 X = -2541765
78
Y = -11137785
55 feet Y = -3394797
04 meter
Z = -17436586
73 Z = -5314671
63
XDOT = 20335
297911 XDOT = 6198
198803
YDOT = -12834
513418 feet/sec YDOT = -3911
959690 meter/sec
ZDOT = -1531
304483 ZDOT = -466
741607
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 13279
82052769
00016717 00000-0 10270-3 0 9132
2 25544 51
6493 275
1428 0002975 245
2244 114
8597 15
49400193 12021
Satellite: ISS
Catalog Number: 25544
Epoch time: 13279
82052769 = yrday
fracday
Element set: 913
Inclination: 51
6493 deg
RA of node: 275
1428 deg
Eccentricity:
0002975
Arg of perigee: 245
2244 deg
Mean anomaly: 114
8597 deg
Mean motion: 15
49400193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1202
Checksum: 317
Coasting Arc #15 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2013/280/19:17:09
887
Vector Time (MET): N/A
Weight (LBS) : 938797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4239341
62 A = 6791146
60 meter
Y = -396268
77 meter E =
0001762
Z = 5290981
35 I = 51
27372
XDOT = 322
362566 Wp = 190
72728
YDOT = 7647
711190 meter/sec RA = 269
46425 deg
ZDOT = 312
803281 TA = 256
26279
MA = 256
28241
Ha = 227
329 n
mi
Hp = 223
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13908601
10 X = 4217754
97
Y = -1300094
38 feet Y = -348981
99 meter
Z = 17358862
69 Z = 5311523
74
XDOT = 1057
619967 XDOT = 235
300671
YDOT = 25090
915979 feet/sec YDOT = 7650
829290 meter/sec
ZDOT = 1026
257483 ZDOT = 314
157181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8992187
50 X = 2740818
75
Y = 10548937
50 feet Y = 3215316
15 meter
Z = 17445057
33 Z = 5317253
48
XDOT = -19162
783598 XDOT = -5840
816441
YDOT = 14620
978400 feet/sec YDOT = 4456
474216 meter/sec
ZDOT = 1030
875025 ZDOT = 314
210708
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 13280
85251096
00016717 00000-0 10270-3 0 9142
2 25544 51
6496 270
0351 0003012 248
7396 111
3433 15
49411813 12181
Satellite: ISS
Catalog Number: 25544
Epoch time: 13280
85251096 = yrday
fracday
Element set: 914
Inclination: 51
6496 deg
RA of node: 270
0351 deg
Eccentricity:
0003012
Arg of perigee: 248
7396 deg
Mean anomaly: 111
3433 deg
Mean motion: 15
49411813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 287
Coasting Arc #16 (Orbit 1232)
---------------------------------------
Vector Time (GMT): 2013/281/19:17:09
887
Vector Time (MET): N/A
Weight (LBS) : 938797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4216619
36 A = 6791058
11 meter
Y = 573342
18 meter E =
0011918
Z = -5302792
29 I = 51
27464
XDOT = -851
274009 Wp = 92
54008
YDOT = -7603
258402 meter/sec RA = 264
48826 deg
ZDOT = -145
966912 TA = 176
06355
MA = 176
05417
Ha = 227
358 n
mi
Hp = 222
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13834053
01 X = -4196957
14
Y = 1881043
89 feet Y = 526298
83 meter
Z = -17397612
49 Z = -5323228
95
XDOT = -2792
893729 XDOT = -765
480350
YDOT = -24945
073498 feet/sec YDOT = -7612
298200 meter/sec
ZDOT = -478
894067 ZDOT = -149
893493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9597960
68 X = -2925458
42
Y = -9990316
31 feet Y = -3045048
41 meter
Z = -17483392
12 Z = -5328937
92
XDOT = 17796
563608 XDOT = 5424
392588
YDOT = -16237
158593 feet/sec YDOT = -4949
085939 meter/sec
ZDOT = -494
311556 ZDOT = -150
666162
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 13281
81998439
00016717 00000-0 10270-3 0 9159
2 25544 51
6494 265
2461 0003033 254
3150 105
7666 15
49436102 12331
Satellite: ISS
Catalog Number: 25544
Epoch time: 13281
81998439 = yrday
fracday
Element set: 915
Inclination: 51
6494 deg
RA of node: 265
2461 deg
Eccentricity:
0003033
Arg of perigee: 254
3150 deg
Mean anomaly: 105
7666 deg
Mean motion: 15
49436102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1233
Checksum: 304
Coasting Arc #17 (Orbit 1248)
---------------------------------------
Vector Time (GMT): 2013/282/19:17:09
887
Vector Time (MET): N/A
Weight (LBS) : 938797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4182315
03 A = 6791027
86 meter
Y = -745847
53 meter E =
0000849
Z = 5298598
41 I = 51
27873
XDOT = 1374
713896 Wp = 221
19080
YDOT = 7536
457790 meter/sec RA = 259
51329 deg
ZDOT = -24
869716 TA = 229
04393
MA = 229
05128
Ha = 227
175 n
mi
Hp = 223
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13721506
01 X = 4164604
81
Y = -2447006
33 feet Y = -699176
95 meter
Z = 17383853
06 Z = 5318873
10
XDOT = 4510
216194 XDOT = 1290
458207
YDOT = 24725
911383 feet/sec YDOT = 7551
359613 meter/sec
ZDOT = -81
593555 ZDOT = -18
396438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10152398
69 X = 3094451
12
Y = 9393049
10 feet Y = 2863001
37 meter
Z = 17468982
33 Z = 5324545
81
XDOT = -16334
515001 XDOT = -4978
760172
YDOT = 17754
379178 feet/sec YDOT = 5411
534773 meter/sec
ZDOT = -55
478905 ZDOT = -16
909970
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 13282
85194422
00016717 00000-0 10270-3 0 9165
2 25544 51
6496 260
1387 0003044 257
4122 102
6688 15
49441185 12493
Satellite: ISS
Catalog Number: 25544
Epoch time: 13282
85194422 = yrday
fracday
Element set: 916
Inclination: 51
6496 deg
RA of node: 260
1387 deg
Eccentricity:
0003044
Arg of perigee: 257
4122 deg
Mean anomaly: 102
6688 deg
Mean motion: 15
49441185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1249
Checksum: 312
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