[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 14th 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) : 123 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 362 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
053/10:35:16
632 -1
7 2
5 2
5
N/A -0
6 -0
1 223
9
000/00:06:33
263 -1
8 -0
1 219
9
Coasting Arc #1 (Orbit 1551)
---------------------------------------
Vector Time (GMT): 2013/044/14:28:27
704
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4198681
55 A = 6786889
58 meter
Y = 3386280
73 meter E =
0003305
Z = 4122677
71 I = 51
65810
XDOT = -6017
767217 Wp = 228
20377
YDOT = 2831
364261 meter/sec RA = 1
69252 deg
ZDOT = 3802
900798 TA = 182
53155
MA = 182
53323
Ha = 221
875 n
mi
Hp = 218
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13775201
93 X = 4140476
86
Y = 11109844
91 feet Y = 3432907
96 meter
Z = 13525845
50 Z = 4142932
50
XDOT = -19743
330765 XDOT = -6067
454038
YDOT = 9289
252825 feet/sec YDOT = 2763
792345 meter/sec
ZDOT = 12476
708656 ZDOT = 3773
546569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13709247
69 X = 4178578
70
Y = 11089030
44 feet Y = 3379936
48 meter
Z = 13609675
62 Z = 4148229
13
XDOT = -18996
411258 XDOT = -5790
106151
YDOT = 8321
910230 feet/sec YDOT = 2536
518238 meter/sec
ZDOT = 12354
182405 ZDOT = 3765
554797
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 13044
65831553
00016717 00000-0 10270-3 0 9005
2 25544 51
6488 1
9226 0012565 271
7710 88
2003 15
52466428 15525
Satellite: ISS
Catalog Number: 25544
Epoch time: 13044
65831553 = yrday
fracday
Element set: 900
Inclination: 51
6488 deg
RA of node: 1
9226 deg
Eccentricity:
0012565
Arg of perigee: 271
7710 deg
Mean anomaly: 88
2003 deg
Mean motion: 15
52466428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1552
Checksum: 294
Coasting Arc #2 (Orbit 1566)
---------------------------------------
Vector Time (GMT): 2013/045/14:28:27
704
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3258778
32 A = 6784400
17 meter
Y = -3582550
39 meter E =
0005146
Z = -4751628
41 I = 51
62031
XDOT = 6715
732806 Wp = 338
40689
YDOT = -2524
680599 meter/sec RA = 356
71589 deg
ZDOT = -2696
682668 TA = 264
89601
MA = 264
95475
Ha = 221
877 n
mi
Hp = 218
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10691529
92 X = -3195393
47
Y = -11753774
23 feet Y = -3618638
10 meter
Z = -15589332
04 Z = -4767304
78
XDOT = 22033
244115 XDOT = 6756
564772
YDOT = -8283
072832 feet/sec YDOT = -2449
352983 meter/sec
ZDOT = -8847
384083 ZDOT = -2663
959293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10814286
62 X = -3296194
56
Y = -11553712
87 feet Y = -3521571
68 meter
Z = -15654079
92 Z = -4771363
56
XDOT = 21085
273302 XDOT = 6426
791302
YDOT = -7908
656824 feet/sec YDOT = -2410
558600 meter/sec
ZDOT = -8710
887324 ZDOT = -2655
078456
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 13045
62387148
00016717 00000-0 10270-3 0 9010
2 25544 51
6495 357
1218 0012539 275
6765 84
2957 15
52510402 15676
Satellite: ISS
Catalog Number: 25544
Epoch time: 13045
62387148 = yrday
fracday
Element set: 901
Inclination: 51
6495 deg
RA of node: 357
1218 deg
Eccentricity:
0012539
Arg of perigee: 275
6765 deg
Mean anomaly: 84
2957 deg
Mean motion: 15
52510402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1567
Checksum: 320
Coasting Arc #3 (Orbit 1582)
---------------------------------------
Vector Time (GMT): 2013/046/14:28:27
704
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2204535
81 A = 6782657
91 meter
Y = 3817056
10 meter E =
0008843
Z = 5162831
21 I = 51
58382
XDOT = -7192
261850 Wp = 265
61655
YDOT = 2202
438262 meter/sec RA = 351
73265 deg
ZDOT = 1444
244496 TA = 170
46643
MA = 170
44964
Ha = 222
133 n
mi
Hp = 218
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7232729
05 X = 2136609
49
Y = 12523149
94 feet Y = 3841329
19 meter
Z = 16938422
62 Z = 5173375
25
XDOT = -23596
659612 XDOT = -7223
371104
YDOT = 7225
847316 feet/sec YDOT = 2121
836035 meter/sec
ZDOT = 4738
334960 ZDOT = 1409
229826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7574312
22 X = 2308650
36
Y = 12259719
50 feet Y = 3736762
50 meter
Z = 16981781
02 Z = 5176046
86
XDOT = -22456
071765 XDOT = -6844
610674
YDOT = 7519
338449 feet/sec YDOT = 2291
894359 meter/sec
ZDOT = 4592
354739 ZDOT = 1399
749724
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 13046
65378310
00016717 00000-0 10270-3 0 9026
2 25544 51
6492 352
0005 0012639 279
0839 80
8882 15
52529953 15830
Satellite: ISS
Catalog Number: 25544
Epoch time: 13046
65378310 = yrday
fracday
Element set: 902
Inclination: 51
6492 deg
RA of node: 352
0005 deg
Eccentricity:
0012639
Arg of perigee: 279
0839 deg
Mean anomaly: 80
8882 deg
Mean motion: 15
52529953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1583
Checksum: 320
Coasting Arc #4 (Orbit 1597)
---------------------------------------
Vector Time (GMT): 2013/047/14:28:27
704
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1103235
04 A = 6781937
87 meter
Y = -4072797
65 meter E =
0003952
Z = -5311686
94 I = 51
55194
XDOT = 7436
438113 Wp = 40
44862
YDOT = -1851
348688 meter/sec RA = 346
74492 deg
ZDOT = -122
109849 TA = 228
36880
MA = 228
40265
Ha = 222
350 n
mi
Hp = 219
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3619537
54 X = -1031807
71
Y = -13362197
02 feet Y = -4084735
66 meter
Z = -17426794
42 Z = -5316872
56
XDOT = 24397
762838 XDOT = 7457
180765
YDOT = -6073
978635 feet/sec YDOT = -1768
073793 meter/sec
ZDOT = -400
622863 ZDOT = -85
934224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4217669
67 X = -1285545
72
Y = -13157783
87 feet Y = -4010492
53 meter
Z = -17447822
53 Z = -5318096
31
XDOT = 23082
815039 XDOT = 7035
642024
YDOT = -7055
195355 feet/sec YDOT = -2150
423544 meter/sec
ZDOT = -249
865340 ZDOT = -76
158956
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 13047
61931262
00016717 00000-0 10270-3 0 9035
2 25544 51
6497 347
1992 0012605 283
0403 76
9341 15
52553179 15989
Satellite: ISS
Catalog Number: 25544
Epoch time: 13047
61931262 = yrday
fracday
Element set: 903
Inclination: 51
6497 deg
RA of node: 347
1992 deg
Eccentricity:
0012605
Arg of perigee: 283
0403 deg
Mean anomaly: 76
9341 deg
Mean motion: 15
52553179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1598
Checksum: 318
Coasting Arc #5 (Orbit 1613)
---------------------------------------
Vector Time (GMT): 2013/048/14:28:27
704
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -19896
26 A = 6782359
96 meter
Y = 4360804
96 meter E =
0010647
Z = 5203280
34 I = 51
52389
XDOT = -7424
978529 Wp = 303
94432
YDOT = 1426
719199 meter/sec RA = 341
75466 deg
ZDOT = -1220
086840 TA = 157
82010
MA = 157
77400
Ha = 222
675 n
mi
Hp = 218
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -65276
44 X = -93934
05
Y = 14307102
89 feet Y = 4360168
75 meter
Z = 17071129
73 Z = 5203003
65
XDOT = -24360
165779 XDOT = -7434
453786
YDOT = 4680
837267 feet/sec YDOT = 1343
635388 meter/sec
ZDOT = -4002
909579 ZDOT = -1256
179356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 836404
23 X = 254936
01
Y = 14284857
71 feet Y = 4354024
63 meter
Z = 17069393
45 Z = 5202751
12
XDOT = -22903
867726 XDOT = -6981
098883
YDOT = 6319
677533 feet/sec YDOT = 1926
237712 meter/sec
ZDOT = -4153
259810 ZDOT = -1265
913590
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 13048
64919476
00016717 00000-0 10270-3 0 9043
2 25544 51
6496 342
0778 0012766 286
7805 73
1946 15
52593084 16146
Satellite: ISS
Catalog Number: 25544
Epoch time: 13048
64919476 = yrday
fracday
Element set: 904
Inclination: 51
6496 deg
RA of node: 342
0778 deg
Eccentricity:
0012766
Arg of perigee: 286
7805 deg
Mean anomaly: 73
1946 deg
Mean motion: 15
52593084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1614
Checksum: 343
Coasting Arc #6 (Orbit 1628)
---------------------------------------
Vector Time (GMT): 2013/049/14:28:27
704
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1087443
42 A = 6783981
99 meter
Y = -4642808
72 meter E =
0001337
Z = -4824142
45 I = 51
50070
XDOT = 7187
308906 Wp = 310
18300
YDOT = -918
155530 meter/sec RA = 336
76395 deg
ZDOT = 2504
169737 TA = 344
48430
MA = 344
48840
Ha = 222
967 n
mi
Hp = 218
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3567727
75 X = 1162713
52
Y = -15232312
06 feet Y = -4630227
58 meter
Z = -15827239
02 Z = -4818676
81
XDOT = 23580
409795 XDOT = 7184
877330
YDOT = -3012
321294 feet/sec YDOT = -837
796021 meter/sec
ZDOT = 8215
779978 ZDOT = 2539
078679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2318388
77 X = 706644
90
Y = -15495676
75 feet Y = -4723082
27 meter
Z = -15803878
71 Z = -4817022
23
XDOT = 22045
663833 XDOT = 6719
518336
YDOT = -5227
775999 feet/sec YDOT = -1593
426125 meter/sec
ZDOT = 8361
134750 ZDOT = 2548
473872
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 13049
61469755
00016717 00000-0 10270-3 0 9052
2 25544 51
6498 337
2761 0012752 290
4041 69
5741 15
52587690 16299
Satellite: ISS
Catalog Number: 25544
Epoch time: 13049
61469755 = yrday
fracday
Element set: 905
Inclination: 51
6498 deg
RA of node: 337
2761 deg
Eccentricity:
0012752
Arg of perigee: 290
4041 deg
Mean anomaly: 69
5741 deg
Mean motion: 15
52587690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1629
Checksum: 335
Coasting Arc #7 (Orbit 1644)
---------------------------------------
Vector Time (GMT): 2013/050/14:28:27
704
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2083323
53 A = 6786280
39 meter
Y = 4912394
45 meter E =
0008115
Z = 4199938
33 I = 51
48102
XDOT = -6717
554198 Wp = 347
18728
YDOT = 292
303698 meter/sec RA = 331
77548 deg
ZDOT = -3667
656410 TA = 140
57921
MA = 140
52013
Ha = 223
241 n
mi
Hp = 218
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6835050
96 X = -2158501
97
Y = 16116779
68 feet Y = 4888677
23 meter
Z = 13779325
24 Z = 4189635
11
XDOT = -22039
219809 XDOT = -6702
507343
YDOT = 959
001634 feet/sec YDOT = 217
267776 meter/sec
ZDOT = -12032
993472 ZDOT = -3700
252617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5195779
52 X = -1583673
60
Y = 16753202
94 feet Y = 5106376
26 meter
Z = 13735806
47 Z = 4186673
81
XDOT = -20522
244279 XDOT = -6255
180056
YDOT = 3629
498175 feet/sec YDOT = 1106
271044 meter/sec
ZDOT = -12168
641032 ZDOT = -3709
001787
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 13050
64455143
00016717 00000-0 10270-3 0 9064
2 25544 51
6498 332
1546 0012805 294
5777 65
4040 15
52630729 16451
Satellite: ISS
Catalog Number: 25544
Epoch time: 13050
64455143 = yrday
fracday
Element set: 906
Inclination: 51
6498 deg
RA of node: 332
1546 deg
Eccentricity:
0012805
Arg of perigee: 294
5777 deg
Mean anomaly: 65
4040 deg
Mean motion: 15
52630729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1645
Checksum: 309
Coasting Arc #8 (Orbit 1659)
---------------------------------------
Vector Time (GMT): 2013/051/14:28:27
704
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2939321
16 A = 6789014
05 meter
Y = -5113234
98 meter E =
0009221
Z = -3349890
69 I = 51
46345
XDOT = 6081
322215 Wp = 312
98410
YDOT = 447
069541 meter/sec RA = 326
78917 deg
ZDOT = 4651
623746 TA = 7
86323
MA = 7
84879
Ha = 223
543 n
mi
Hp = 218
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9643442
12 X = 3012552
54
Y = -16775705
31 feet Y = -5079956
32 meter
Z = -10990455
02 Z = -3335433
91
XDOT = 19951
844536 XDOT = 6053
275103
YDOT = 1466
763585 feet/sec YDOT = 514
918081 meter/sec
ZDOT = 15261
232763 ZDOT = 4681
097566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7597073
61 X = 2315588
04
Y = -17833617
75 feet Y = -5435686
69 meter
Z = -10929634
78 Z = -3331352
68
XDOT = 18588
005216 XDOT = 5665
623990
YDOT = -1513
733810 feet/sec YDOT = -461
386065 meter/sec
ZDOT = 15383
791438 ZDOT = 4688
979630
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 13051
61002664
00016717 00000-0 10270-3 0 9079
2 25544 51
6498 327
3524 0012911 297
8474 62
1369 15
52620170 16605
Satellite: ISS
Catalog Number: 25544
Epoch time: 13051
61002664 = yrday
fracday
Element set: 907
Inclination: 51
6498 deg
RA of node: 327
3524 deg
Eccentricity:
0012911
Arg of perigee: 297
8474 deg
Mean anomaly: 62
1369 deg
Mean motion: 15
52620170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1660
Checksum: 298
Coasting Arc #9 (Orbit 1675)
---------------------------------------
Vector Time (GMT): 2013/052/14:28:27
704
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3656855
28 A = 6791412
14 meter
Y = 5231646
12 meter E =
0003422
Z = 2322173
23 I = 51
44666
XDOT = -5288
075052 Wp = 41
87288
YDOT = -1302
111577 meter/sec RA = 321
80729 deg
ZDOT = -5386
786162 TA = 112
20331
MA = 112
16700
Ha = 223
728 n
mi
Hp = 218
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11997556
68 X = -3726365
12
Y = 17164193
30 feet Y = 5190364
33 meter
Z = 7618678
59 Z = 2304239
84
XDOT = -17349
327597 XDOT = -5246
954542
YDOT = -4272
019610 feet/sec YDOT = -1361
016508 meter/sec
ZDOT = -17673
182947 ZDOT = -5412
374670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9546037
86 X = -2909632
34
Y = 18669912
94 feet Y = 5690589
46 meter
Z = 7543386
07 Z = 2299224
07
XDOT = -16304
825683 XDOT = -4969
710868
YDOT = -1143
638909 feet/sec YDOT = -348
581139 meter/sec
ZDOT = -17779
465727 ZDOT = -5419
181154
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 13052
63985308
00016717 00000-0 10270-3 0 9088
2 25544 51
6498 322
2310 0012780 301
8047 58
1860 15
52643351 16762
Satellite: ISS
Catalog Number: 25544
Epoch time: 13052
63985308 = yrday
fracday
Element set: 908
Inclination: 51
6498 deg
RA of node: 322
2310 deg
Eccentricity:
0012780
Arg of perigee: 301
8047 deg
Mean anomaly: 58
1860 deg
Mean motion: 15
52643351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1676
Checksum: 304
Coasting Arc #10 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2013/053/10:38:33
263
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4710872
31 A = 6794911
08 meter
Y = 4865589
26 meter E =
0002948
Z = 526635
68 I = 51
43283
XDOT = -3764
193992 Wp = 176
86437
YDOT = -2999
470439 meter/sec RA = 317
62921 deg
ZDOT = -5960
723914 TA = 357
44510
MA = 357
44661
Ha = 223
922 n
mi
Hp = 219
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15455617
81 X = -4767488
44
Y = 15963219
36 feet Y = 4812592
80 meter
Z = 1727807
34 Z = 503613
39
XDOT = -12349
717823 XDOT = -3701
418581
YDOT = -9840
782279 feet/sec YDOT = -3041
213393 meter/sec
ZDOT = -19556
180821 ZDOT = -5978
856955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22200762
93 X = -6766792
54
Y = -1072602
51 feet Y = -326929
25 meter
Z = 1631398
69 Z = 497250
32
XDOT = -762
772923 XDOT = -232
493187
YDOT = -14063
792170 feet/sec YDOT = -4286
643853 meter/sec
ZDOT = -19631
228154 ZDOT = -5983
598341
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 13053
47658926
00016717 00000-0 10270-3 0 9095
2 25544 51
6486 318
0689 0011155 298
4957 61
5071 15
52172873 16899
Satellite: ISS
Catalog Number: 25544
Epoch time: 13053
47658926 = yrday
fracday
Element set: 909
Inclination: 51
6486 deg
RA of node: 318
0689 deg
Eccentricity:
0011155
Arg of perigee: 298
4957 deg
Mean anomaly: 61
5071 deg
Mean motion: 15
52172873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 348
Coasting Arc #11 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2013/054/10:38:33
263
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4895542
56 A = 6794826
70 meter
Y = -4665742
00 meter E =
0014235
Z = 550523
82 I = 51
41044
XDOT = 2960
619444 Wp = 2
46563
YDOT = 3809
041985 meter/sec RA = 312
65224 deg
ZDOT = 5962
821575 TA = 3
49260
MA = 3
48267
Ha = 224
117 n
mi
Hp = 219
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16061491
34 X = 4944677
80
Y = -15307552
49 feet Y = -4610722
19 meter
Z = 1806180
52 Z = 574425
09
XDOT = 9713
318385 XDOT = 2888
840788
YDOT = 12496
856905 feet/sec YDOT = 3841
748635 meter/sec
ZDOT = 19563
062909 ZDOT = 5977
029010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22124085
02 X = 6743421
11
Y = 1564026
19 feet Y = 476715
18 meter
Z = 1906210
75 Z = 581013
04
XDOT = -2670
606464 XDOT = -814
000850
YDOT = 13893
742213 feet/sec YDOT = 4234
812627 meter/sec
ZDOT = 19621
679776 ZDOT = 5980
687996
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 13054
50670602
00016717 00000-0 10270-3 0 9107
2 25544 51
6483 312
9488 0011252 302
7532 57
2535 15
52192025 17059
Satellite: ISS
Catalog Number: 25544
Epoch time: 13054
50670602 = yrday
fracday
Element set: 910
Inclination: 51
6483 deg
RA of node: 312
9488 deg
Eccentricity:
0011252
Arg of perigee: 302
7532 deg
Mean anomaly: 57
2535 deg
Mean motion: 15
52192025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 280
Coasting Arc #12 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2013/055/10:38:33
263
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4972345
82 A = 6793765
75 meter
Y = 4340745
38 meter E =
0004321
Z = -1606201
78 I = 51
38777
XDOT = -2187
363908 Wp = 274
48572
YDOT = -4621
481982 meter/sec RA = 307
67326 deg
ZDOT = -5704
420487 TA = 283
12798
MA = 283
17620
Ha = 224
324 n
mi
Hp = 219
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16313470
54 X = -5012713
09
Y = 14241290
61 feet Y = 4284915
61 meter
Z = -5269690
87 Z = -1630454
92
XDOT = -7176
390774 XDOT = -2107
813038
YDOT = -15162
342459 feet/sec YDOT = -4645
498244 meter/sec
ZDOT = -18715
290313 ZDOT = -5714
852573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21529688
59 X = -6562249
08
Y = -2082487
89 feet Y = -634742
31 meter
Z = -5371133
46 Z = -1637121
48
XDOT = 6041
723502 XDOT = 1841
517324
YDOT = -13968
124208 feet/sec YDOT = -4257
484259 meter/sec
ZDOT = -18758
104876 ZDOT = -5717
470366
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 13055
47242698
00016717 00000-0 10270-3 0 9115
2 25544 51
6489 308
1493 0011246 305
8024 54
2082 15
52213402 17205
Satellite: ISS
Catalog Number: 25544
Epoch time: 13055
47242698 = yrday
fracday
Element set: 911
Inclination: 51
6489 deg
RA of node: 308
1493 deg
Eccentricity:
0011246
Arg of perigee: 305
8024 deg
Mean anomaly: 54
2082 deg
Mean motion: 15
52213402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 284
Coasting Arc #13 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2013/056/10:38:33
263
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4943769
06 A = 6791896
43 meter
Y = -3846061
33 meter E =
0011208
Z = 2606518
95 I = 51
36334
XDOT = 1472
186354 Wp = 24
00397
YDOT = 5426
047392 meter/sec RA = 302
68981 deg
ZDOT = 5216
268506 TA = 5
45855
MA = 5
44634
Ha = 224
442 n
mi
Hp = 219
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16219714
77 X = 4973747
60
Y = -12618311
44 feet Y = -3790609
06 meter
Z = 8551571
36 Z = 2630608
12
XDOT = 4830
007723 XDOT = 1386
063014
YDOT = 17801
992757 feet/sec YDOT = 5442
029388 meter/sec
ZDOT = 17113
741819 ZDOT = 5223
210274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20320709
94 X = 6193752
39
Y = 2763594
33 feet Y = 842343
55 meter
Z = 8652259
67 Z = 2637208
75
XDOT = -9244
832607 XDOT = -2817
824979
YDOT = 14330
848894 feet/sec YDOT = 4368
042743 meter/sec
ZDOT = 17141
944170 ZDOT = 5224
864583
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 13056
50251655
00016717 00000-0 10270-3 0 9124
2 25544 51
6484 303
0288 0011282 310
2703 49
7462 15
52234615 17367
Satellite: ISS
Catalog Number: 25544
Epoch time: 13056
50251655 = yrday
fracday
Element set: 912
Inclination: 51
6484 deg
RA of node: 303
0288 deg
Eccentricity:
0011282
Arg of perigee: 310
2703 deg
Mean anomaly: 49
7462 deg
Mean motion: 15
52234615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 285
Coasting Arc #14 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2013/057/10:38:33
263
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4850570
68 A = 6789491
62 meter
Y = 3223415
30 meter E =
0008815
Z = -3495152
45 I = 51
34027
XDOT = -835
671410 Wp = 338
61135
YDOT = -6144
462183 meter/sec RA = 297
70192 deg
ZDOT = -4495
351170 TA = 242
61104
MA = 242
70076
Ha = 224
681 n
mi
Hp = 218
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15913945
80 X = -4869276
87
Y = 10575509
51 feet Y = 3169068
11 meter
Z = -11467035
60 Z = -3518761
55
XDOT = -2741
704101 XDOT = -745
063781
YDOT = -20158
996664 feet/sec YDOT = -6153
301162 meter/sec
ZDOT = -14748
527460 ZDOT = -4499
189831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18697448
50 X = -5698982
30
Y = -3637217
27 feet Y = -1108623
82 meter
Z = -11565640
84 Z = -3525207
33
XDOT = 12039
605766 XDOT = 3669
671837
YDOT = -14824
336614 feet/sec YDOT = -4518
457800 meter/sec
ZDOT = -14763
741751 ZDOT = -4499
988486
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 13057
46821156
00016717 00000-0 10270-3 0 9130
2 25544 51
6487 298
2290 0011390 313
3540 46
6662 15
52268690 17516
Satellite: ISS
Catalog Number: 25544
Epoch time: 13057
46821156 = yrday
fracday
Element set: 913
Inclination: 51
6487 deg
RA of node: 298
2290 deg
Eccentricity:
0011390
Arg of perigee: 313
3540 deg
Mean anomaly: 46
6662 deg
Mean motion: 15
52268690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 310
Coasting Arc #15 (Orbit 1766)
---------------------------------------
Vector Time (GMT): 2013/058/10:38:33
263
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4700838
27 A = 6786974
26 meter
Y = -2429304
13 meter E =
0005786
Z = 4245013
94 I = 51
31816
XDOT = 272
009344 Wp = 17
94129
YDOT = 6774
688911 meter/sec RA = 292
70750 deg
ZDOT = 3579
848556 TA = 35
34290
MA = 35
30456
Ha = 224
768 n
mi
Hp = 218
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15422697
74 X = 4707033
02
Y = -7970157
91 feet Y = -2376701
19 meter
Z = 13927211
08 Z = 4267865
27
XDOT = 892
419107 XDOT = 178
843393
YDOT = 22226
669656 feet/sec YDOT = 6777
210253 meter/sec
ZDOT = 11744
909959 ZDOT = 3580
942729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16589832
67 X = 5056581
00
Y = 4847214
45 feet Y = 1477430
96 meter
Z = 14022560
22 Z = 4274076
35
XDOT = -14423
213784 XDOT = -4396
195561
YDOT = 15415
032908 feet/sec YDOT = 4698
502030 meter/sec
ZDOT = 11748
640308 ZDOT = 3580
985566
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 13058
49827416
00016717 00000-0 10270-3 0 9140
2 25544 51
6483 293
1080 0011363 317
6400 42
3874 15
52278571 17679
Satellite: ISS
Catalog Number: 25544
Epoch time: 13058
49827416 = yrday
fracday
Element set: 914
Inclination: 51
6483 deg
RA of node: 293
1080 deg
Eccentricity:
0011363
Arg of perigee: 317
6400 deg
Mean anomaly: 42
3874 deg
Mean motion: 15
52278571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1767
Checksum: 313
Coasting Arc #16 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2013/059/10:38:33
263
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4538123
56 A = 6784691
58 meter
Y = 1547712
15 meter E =
0013046
Z = -4808476
39 I = 51
30003
XDOT = 200
998361 Wp = 16
54487
YDOT = -7233
376906 meter/sec RA = 287
70858 deg
ZDOT = -2507
324114 TA = 228
59511
MA = 228
70731
Ha = 224
986 n
mi
Hp = 218
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14888856
83 X = -4531735
04
Y = 5077795
76 feet Y = 1496999
09 meter
Z = -15775841
17 Z = -4830506
68
XDOT = 659
443442 XDOT = 294
048386
YDOT = -23731
551530 feet/sec YDOT = -7230
609269 meter/sec
ZDOT = -8226
128983 ZDOT = -2506
120742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14306685
80 X = -4360677
83
Y = -6314682
06 feet Y = -1924715
09 meter
Z = -15867664
10 Z = -4836464
02
XDOT = 16173
028408 XDOT = 4929
539059
YDOT = -15899
130668 feet/sec YDOT = -4846
055028 meter/sec
ZDOT = -8220
255562 ZDOT = -2505
533895
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 13059
46394357
00016717 00000-0 10270-3 0 9152
2 25544 51
6482 288
3076 0011533 320
8981 39
1336 15
52327487 17823
Satellite: ISS
Catalog Number: 25544
Epoch time: 13059
46394357 = yrday
fracday
Element set: 915
Inclination: 51
6482 deg
RA of node: 288
3076 deg
Eccentricity:
0011533
Arg of perigee: 320
8981 deg
Mean anomaly: 39
1336 deg
Mean motion: 15
52327487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1782
Checksum: 329
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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