[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 24th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 1883)
---------------------------------------
Vector Time (GMT): 2012/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4086040
31 A = 6774335
15 meter
Y = -2186147
22 meter E =
0020296
Z = -4960035
33 I = 51
97300
XDOT = 1134
107164 Wp = 74
49393
YDOT = 7227
563512 meter/sec RA = 95
02231 deg
ZDOT = -2253
681472 TA = 173
57313
MA = 173
54705
Ha = 221
374 n
mi
Hp = 209
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13405644
05 X = 4134277
07
Y = -7172399
01 feet Y = -2140184
18 meter
Z = -16273081
81 Z = -4940068
86
XDOT = 3720
824029 XDOT = 1064
150554
YDOT = 23712
478715 feet/sec YDOT = 7239
854969 meter/sec
ZDOT = -7393
968083 ZDOT = -2248
340985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7236891
52 X = -2205804
54
Y = -13470767
73 feet Y = -4105890
01 meter
Z = -16190540
73 Z = -4934876
81
XDOT = 22711
720788 XDOT = 6922
532496
YDOT = -3349
625246 feet/sec YDOT = -1020
965775 meter/sec
ZDOT = -7372
673287 ZDOT = -2247
190818
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 12174
52002407
00016717 00000-0 10270-3 0 9002
2 25544 51
6395 95
7320 0008043 75
8345 284
3701 15
55743621 18849
Satellite: ISS
Catalog Number: 25544
Epoch time: 12174
52002407 = yrday
fracday
Element set: 900
Inclination: 51
6395 deg
RA of node: 95
7320 deg
Eccentricity:
0008043
Arg of perigee: 75
8345 deg
Mean anomaly: 284
3701 deg
Mean motion: 15
55743621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1884
Checksum: 295
Coasting Arc #2 (Orbit 1899)
---------------------------------------
Vector Time (GMT): 2012/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4164509
47 A = 6772541
58 meter
Y = -285244
82 meter E =
0010328
Z = 5324539
63 I = 51
96882
XDOT = 200
757112 Wp = 78
91844
YDOT = -7672
685722 meter/sec RA = 90
02918 deg
ZDOT = -251
672969 TA = 13
47990
MA = 13
45233
Ha = 221
398 n
mi
Hp = 209
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13663088
82 X = -4186875
45
Y = -935842
57 feet Y = -331940
64 meter
Z = 17468962
04 Z = 5304254
47
XDOT = 658
651942 XDOT = 287
762291
YDOT = -25172
853420 feet/sec YDOT = -7669
954228 meter/sec
ZDOT = -825
698718 ZDOT = -250
487313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -632886
29 X = -192903
74
Y = 13786569
05 feet Y = 4202146
25 meter
Z = 17385350
19 Z = 5299054
74
XDOT = -24176
071764 XDOT = -7368
866674
YDOT = -65
977510 feet/sec YDOT = -20
109945 meter/sec
ZDOT = -820
034824 ZDOT = -249
946614
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 12175
54778906
00016717 00000-0 10270-3 0 9010
2 25544 51
6392 90
5959 0007835 79
2718 280
9317 15
55784839 19007
Satellite: ISS
Catalog Number: 25544
Epoch time: 12175
54778906 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 90
5959 deg
Eccentricity:
0007835
Arg of perigee: 79
2718 deg
Mean anomaly: 280
9317 deg
Mean motion: 15
55784839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1900
Checksum: 351
Coasting Arc #3 (Orbit 1914)
---------------------------------------
Vector Time (GMT): 2012/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3984880
59 A = 6775017
86 meter
Y = 2714104
33 meter E =
0018554
Z = -4776669
01 I = 51
97640
XDOT = -1521
550513 Wp = 97
87993
YDOT = 6996
694687 meter/sec RA = 85
03655 deg
ZDOT = 2712
708138 TA = 198
81260
MA = 198
88125
Ha = 221
339 n
mi
Hp = 209
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13073755
21 X = 3977438
53
Y = 8904541
76 feet Y = 2758624
62 meter
Z = -15671486
25 Z = -4757328
60
XDOT = -4991
963626 XDOT = -1612
853508
YDOT = 22955
035062 feet/sec YDOT = 6979
168980 meter/sec
ZDOT = 8899
961082 ZDOT = 2705
095535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8381839
42 X = 2554784
66
Y = -13507156
12 feet Y = -4116981
18 meter
Z = -15592014
70 Z = -4752446
08
XDOT = 22150
393836 XDOT = 6751
440041
YDOT = 3533
573498 feet/sec YDOT = 1077
033202 meter/sec
ZDOT = 8867
858183 ZDOT = 2702
923174
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 12176
51131112
00016717 00000-0 10270-3 0 9021
2 25544 51
6397 85
7800 0007944 82
5909 277
6147 15
55763381 19152
Satellite: ISS
Catalog Number: 25544
Epoch time: 12176
51131112 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 85
7800 deg
Eccentricity:
0007944
Arg of perigee: 82
5909 deg
Mean anomaly: 277
6147 deg
Mean motion: 15
55763381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1915
Checksum: 317
Coasting Arc #4 (Orbit 1930)
---------------------------------------
Vector Time (GMT): 2012/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3475787
54 A = 6779919
44 meter
Y = -4763806
01 meter E =
0020589
Z = 3327913
15 I = 51
98879
XDOT = 2806
538608 Wp = 89
65874
YDOT = -5363
832658 meter/sec RA = 80
05784 deg
ZDOT = -4721
692119 TA = 51
74799
MA = 51
56289
Ha = 221
406 n
mi
Hp = 209
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11403502
41 X = -3438425
51
Y = -15629284
82 feet Y = -4802465
83 meter
Z = 10918350
24 Z = 3311118
35
XDOT = 9207
803833 XDOT = 2889
246272
YDOT = -17597
876176 feet/sec YDOT = -5331
985327 meter/sec
ZDOT = -15491
115877 ZDOT = -4707
857758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14958282
12 X = -4559284
39
Y = 12331302
59 feet Y = 3758581
03 meter
Z = 10849587
82 Z = 3306954
37
XDOT = -17195
294182 XDOT = -5241
125667
YDOT = -7206
146926 feet/sec YDOT = -2196
433583 meter/sec
ZDOT = -15433
517747 ZDOT = -4704
136209
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 12177
53905644
00016717 00000-0 10270-3 0 9034
2 25544 51
6393 80
6432 0007980 86
7098 273
4968 15
55767826 19319
Satellite: ISS
Catalog Number: 25544
Epoch time: 12177
53905644 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 80
6432 deg
Eccentricity:
0007980
Arg of perigee: 86
7098 deg
Mean anomaly: 273
4968 deg
Mean motion: 15
55767826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1931
Checksum: 347
Coasting Arc #5 (Orbit 1945)
---------------------------------------
Vector Time (GMT): 2012/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2693447
90 A = 6783718
67 meter
Y = 6079738
40 meter E =
0015012
Z = -1329755
66 I = 51
99639
XDOT = -3932
584012 Wp = 61
97774
YDOT = 3010
203700 meter/sec RA = 75
09538 deg
ZDOT = 5854
371810 TA = 283
61245
MA = 283
77960
Ha = 221
258 n
mi
Hp = 209
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8836771
32 X = 2631722
47
Y = 19946648
29 feet Y = 6109513
19 meter
Z = -4362715
42 Z = -1316820
43
XDOT = -12902
178516 XDOT = -3994
391602
YDOT = 9875
996390 feet/sec YDOT = 2965
881008 meter/sec
ZDOT = 19207
256596 ZDOT = 5835
117668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19241528
76 X = 5864817
97
Y = -10304269
32 feet Y = -3140741
29 meter
Z = -4310011
12 Z = -1313691
39
XDOT = 10055
360174 XDOT = 3064
873781
YDOT = 10855
396299 feet/sec YDOT = 3308
724792 meter/sec
ZDOT = 19127
547880 ZDOT = 5830
076594
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 12178
50255634
00016717 00000-0 10270-3 0 9040
2 25544 51
6400 75
8273 0007851 89
8531 270
3522 15
55805608 19469
Satellite: ISS
Catalog Number: 25544
Epoch time: 12178
50255634 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 75
8273 deg
Eccentricity:
0007851
Arg of perigee: 89
8531 deg
Mean anomaly: 270
3522 deg
Mean motion: 15
55805608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1946
Checksum: 313
Coasting Arc #6 (Orbit 1961)
---------------------------------------
Vector Time (GMT): 2012/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1546639
44 A = 6784112
63 meter
Y = -6528968
14 meter E =
0016133
Z = -976539
81 I = 51
98907
XDOT = 4840
813642 Wp = 120
55205
YDOT = -269
972594 meter/sec RA = 70
14112 deg
ZDOT = -5942
546597 TA = 69
98070
MA = 69
80707
Ha = 221
245 n
mi
Hp = 209
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5074276
38 X = -1468772
41
Y = -21420499
15 feet Y = -6545828
15 meter
Z = -3203870
77 Z = -983864
81
XDOT = 15881
934522 XDOT = 4872
340348
YDOT = -885
736856 feet/sec YDOT = -215
662776 meter/sec
ZDOT = -19496
543953 ZDOT = -5918
953546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20874731
58 X = -6362618
19
Y = 6974357
59 feet Y = 2125784
19 meter
Z = -3233383
73 Z = -985535
36
XDOT = -1824
262060 XDOT = -556
035076
YDOT = -14332
233903 feet/sec YDOT = -4368
464894 meter/sec
ZDOT = -19399
228902 ZDOT = -5912
884969
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 12179
53028017
00016717 00000-0 10270-3 0 9058
2 25544 51
6404 70
6900 0007773 94
4720 265
7322 15
55781224 19629
Satellite: ISS
Catalog Number: 25544
Epoch time: 12179
53028017 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 70
6900 deg
Eccentricity:
0007773
Arg of perigee: 94
4720 deg
Mean anomaly: 265
7322 deg
Mean motion: 15
55781224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1962
Checksum: 301
Coasting Arc #7 (Orbit 1977)
---------------------------------------
Vector Time (GMT): 2012/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 171180
81 A = 6780491
74 meter
Y = 6046025
79 meter E =
0020778
Z = 3045877
69 I = 51
96618
XDOT = -5364
661537 Wp = 88
27028
YDOT = -2360
216034 meter/sec RA = 65
17966 deg
ZDOT = 4958
041337 TA = 306
55176
MA = 306
74285
Ha = 221
216 n
mi
Hp = 209
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 561616
82 X = 88763
93
Y = 19836042
62 feet Y = 6047478
88 meter
Z = 9993037
04 Z = 3046509
77
XDOT = -17600
595595 XDOT = -5361
955555
YDOT = -7743
490924 feet/sec YDOT = -2420
192432 meter/sec
ZDOT = 16266
539821 ZDOT = 4931
986238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19667371
31 X = 5994614
77
Y = -2634282
73 feet Y = -802929
38 meter
Z = 9994991
24 Z = 3046473
33
XDOT = -5983
129388 XDOT = -1823
657837
YDOT = 16996
299159 feet/sec YDOT = 5180
471984 meter/sec
ZDOT = 16159
355138 ZDOT = 4925
371446
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 12180
55799275
00016717 00000-0 10270-3 0 9064
2 25544 51
6406 65
5531 0007806 96
3262 263
8780 15
55814124 19783
Satellite: ISS
Catalog Number: 25544
Epoch time: 12180
55799275 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 65
5531 deg
Eccentricity:
0007806
Arg of perigee: 96
3262 deg
Mean anomaly: 263
8780 deg
Mean motion: 15
55814124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1978
Checksum: 331
Coasting Arc #8 (Orbit 1992)
---------------------------------------
Vector Time (GMT): 2012/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1440466
86 A = 6775330
82 meter
Y = -4760095
43 meter E =
0017201
Z = -4617080
51 I = 51
93586
XDOT = 5351
596019 Wp = 82
47176
YDOT = 4558
406274 meter/sec RA = 60
20070 deg
ZDOT = -3037
456137 TA = 157
31571
MA = 157
23961
Ha = 221
057 n
mi
Hp = 209
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4725941
13 X = 1516017
01
Y = -15617110
99 feet Y = -4743564
18 meter
Z = -15147901
92 Z = -4609899
89
XDOT = 17557
729721 XDOT = 5314
980595
YDOT = 14955
401162 feet/sec YDOT = 4618
046825 meter/sec
ZDOT = -9965
407274 ZDOT = -3011
546496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16097291
44 X = -4906454
43
Y = -2831587
84 feet Y = -863067
97 meter
Z = -15117768
57 Z = -4607895
86
XDOT = 12432
749604 XDOT = 3789
502079
YDOT = -18172
893799 feet/sec YDOT = -5539
098030 meter/sec
ZDOT = -9859
067311 ZDOT = -3005
043716
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 12181
52146225
00016717 00000-0 10270-3 0 9074
2 25544 51
6409 60
7372 0007581 100
0032 260
1977 15
55851415 19933
Satellite: ISS
Catalog Number: 25544
Epoch time: 12181
52146225 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 60
7372 deg
Eccentricity:
0007581
Arg of perigee: 100
0032 deg
Mean anomaly: 260
1977 deg
Mean motion: 15
55851415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1993
Checksum: 291
Coasting Arc #9 (Orbit 2008)
---------------------------------------
Vector Time (GMT): 2012/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3035023
71 A = 6772382
72 meter
Y = 2911752
50 meter E =
0010435
Z = 5299674
98 I = 51
91042
XDOT = -4738
932594 Wp = 106
05018
YDOT = -6014
107338 meter/sec RA = 55
20563 deg
ZDOT = 586
610264 TA = 338
35804
MA = 338
40211
Ha = 221
141 n
mi
Hp = 209
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9957426
88 X = -3093102
67
Y = 9552993
75 feet Y = 2877487
39 meter
Z = 17387385
10 Z = 5284790
31
XDOT = -15547
679114 XDOT = -4674
179034
YDOT = -19731
323288 feet/sec YDOT = -6066
739056 meter/sec
ZDOT = 1924
574356 ZDOT = 563
744971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10884922
43 X = 3317724
36
Y = 8606423
03 feet Y = 2623237
74 meter
Z = 17325678
82 Z = 5280866
90
XDOT = -16697
195314 XDOT = -5089
305132
YDOT = 17406
776219 feet/sec YDOT = 5305
585392 meter/sec
ZDOT = 1830
957485 ZDOT = 558
075841
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 12182
54915417
00016717 00000-0 10270-3 0 9085
2 25544 51
6412 55
6005 0007630 103
9575 256
2427 15
55868001 20096
Satellite: ISS
Catalog Number: 25544
Epoch time: 12182
54915417 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 55
6005 deg
Eccentricity:
0007630
Arg of perigee: 103
9575 deg
Mean anomaly: 256
2427 deg
Mean motion: 15
55868001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2009
Checksum: 295
Coasting Arc #10 (Orbit 2023)
---------------------------------------
Vector Time (GMT): 2012/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4469569
69 A = 6773576
57 meter
Y = -813162
73 meter E =
0020269
Z = -5042700
64 I = 51
89567
XDOT = 3429
982545 Wp = 105
44285
YDOT = 6550
010447 meter/sec RA = 50
20480 deg
ZDOT = 1985
305275 TA = 183
79144
MA = 183
80682
Ha = 220
928 n
mi
Hp = 209
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14663942
54 X = 4502826
73
Y = -2667856
72 feet Y = -762994
38 meter
Z = -16544293
42 Z = -5020907
04
XDOT = 11253
223574 XDOT = 3346
839905
YDOT = 21489
535588 feet/sec YDOT = 6587
901405 meter/sec
ZDOT = 6513
468749 ZDOT = 2001
767189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4980371
89 X = -1518017
35
Y = -14153210
13 feet Y = -4313898
45 meter
Z = -16454326
30 Z = -5015278
66
XDOT = 18403
842993 XDOT = 5609
491344
YDOT = -14121
346962 feet/sec YDOT = -4304
186554 meter/sec
ZDOT = 6580
611235 ZDOT = 2005
770304
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 12183
51260534
00016717 00000-0 10270-3 0 9097
2 25544 51
6406 50
7839 0007480 107
2070 252
9903 15
55887635 20243
Satellite: ISS
Catalog Number: 25544
Epoch time: 12183
51260534 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 50
7839 deg
Eccentricity:
0007480
Arg of perigee: 107
2070 deg
Mean anomaly: 252
9903 deg
Mean motion: 15
55887635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2024
Checksum: 304
Coasting Arc #11 (Orbit 2039)
---------------------------------------
Vector Time (GMT): 2012/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5450941
19 A = 6777994
75 meter
Y = -1244484
31 meter E =
0018386
Z = 3814747
17 I = 51
89077
XDOT = -1535
034791 Wp = 93
18700
YDOT = -6235
464902 meter/sec RA = 45
21472 deg
ZDOT = -4211
191642 TA = 41
06470
MA = 40
92644
Ha = 220
911 n
mi
Hp = 209
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17883665
32 X = -5455151
04
Y = -4082953
79 feet Y = -1305464
36 meter
Z = 12515574
69 Z = 3788256
45
XDOT = -5036
203382 XDOT = -1444
737575
YDOT = -20457
562015 feet/sec YDOT = -6252
124954 meter/sec
ZDOT = -13816
245543 ZDOT = -4218
430550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -861117
01 X = -262468
46
Y = 18397653
46 feet Y = 5607604
78 meter
Z = 12406467
31 Z = 3781491
24
XDOT = -17927
684903 XDOT = -5464
358358
YDOT = 8534
199842 feet/sec YDOT = 2601
224112 meter/sec
ZDOT = -13845
382274 ZDOT = -4220
072517
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 12184
54027563
00016717 00000-0 10270-3 0 9106
2 25544 51
6407 45
6470 0007360 110
1130 250
0816 15
55934917 20401
Satellite: ISS
Catalog Number: 25544
Epoch time: 12184
54027563 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 45
6470 deg
Eccentricity:
0007360
Arg of perigee: 110
1130 deg
Mean anomaly: 250
0816 deg
Mean motion: 15
55934917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2040
Checksum: 271
Coasting Arc #12 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2012/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5804679
27 A = 6782673
14 meter
Y = 2939637
29 meter E =
0011429
Z = -1919250
22 I = 51
88265
XDOT = -755
328363 Wp = 76
98816
YDOT = 5146
767783 meter/sec RA = 40
24011 deg
ZDOT = 5629
303162 TA = 261
93589
MA = 262
06558
Ha = 220
832 n
mi
Hp = 209
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19044223
33 X = 5780699
39
Y = 9644479
30 feet Y = 3004415
07 meter
Z = -6296752
68 Z = -1891109
41
XDOT = -2478
111427 XDOT = -840
169980
YDOT = 16885
721073 feet/sec YDOT = 5137
845854 meter/sec
ZDOT = 18468
842394 ZDOT = 5625
428696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5785861
70 X = 1763530
65
Y = -20583152
40 feet Y = -6273744
85 meter
Z = -6181032
22 Z = -1883978
62
XDOT = 15568
718160 XDOT = 4745
345295
YDOT = -1134
041654 feet/sec YDOT = -345
655896 meter/sec
ZDOT = 18452
266747 ZDOT = 5624
250905
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 12185
50370855
00016717 00000-0 10270-3 0 9119
2 25544 51
6394 40
8303 0007321 114
2939 245
8980 15
55898551 20550
Satellite: ISS
Catalog Number: 25544
Epoch time: 12185
50370855 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 40
8303 deg
Eccentricity:
0007321
Arg of perigee: 114
2939 deg
Mean anomaly: 245
8980 deg
Mean motion: 15
55898551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 313
Coasting Arc #13 (Orbit 2070)
---------------------------------------
Vector Time (GMT): 2012/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5338929
10 A = 6784108
47 meter
Y = -4155273
93 meter E =
0018363
Z = -393401
25 I = 51
86328
XDOT = 3182
575588 Wp = 129
97932
YDOT = -3537
871424 meter/sec RA = 35
27678 deg
ZDOT = -6019
650133 TA = 54
25328
MA = 54
08264
Ha = 220
778 n
mi
Hp = 209
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17516171
60 X = -5290156
15
Y = -13632788
47 feet Y = -4214704
37 meter
Z = -1290686
53 Z = -419219
31
XDOT = 10441
520957 XDOT = 3251
141864
YDOT = -11607
189712 feet/sec YDOT = -3501
897546 meter/sec
ZDOT = -19749
508310 ZDOT = -6004
023606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9661106
09 X = -2944705
13
Y = 19976169
58 feet Y = 6088736
49 meter
Z = -1396688
40 Z = -425710
63
XDOT = -12107
419924 XDOT = -3690
341593
YDOT = -7190
120812 feet/sec YDOT = -2191
548823 meter/sec
ZDOT = -19684
646797 ZDOT = -5999
880344
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 12186
53135973
00016717 00000-0 10270-3 0 9124
2 25544 51
6391 35
6928 0007392 118
8591 241
3305 15
55900066 20719
Satellite: ISS
Catalog Number: 25544
Epoch time: 12186
53135973 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 35
6928 deg
Eccentricity:
0007392
Arg of perigee: 118
8591 deg
Mean anomaly: 241
3305 deg
Mean motion: 15
55900066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2071
Checksum: 307
Coasting Arc #14 (Orbit 2086)
---------------------------------------
Vector Time (GMT): 2012/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4097276
93 A = 6781141
96 meter
Y = 4741040
79 meter E =
0019387
Z = 2576430
34 I = 51
82765
XDOT = -5307
185961 Wp = 92
08658
YDOT = 1701
064649 meter/sec RA = 30
30740 deg
ZDOT = 5274
871064 TA = 296
84169
MA = 297
03978
Ha = 220
588 n
mi
Hp = 209
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13442509
62 X = 4031441
64
Y = 15554595
77 feet Y = 4786490
62 meter
Z = 8452855
46 Z = 2596175
11
XDOT = -17412
027430 XDOT = -5351
436822
YDOT = 5580
920764 feet/sec YDOT = 1641
468256 meter/sec
ZDOT = 17306
007429 ZDOT = 5248
982226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12120405
76 X = 3694299
67
Y = -16564066
69 feet Y = -5048727
53 meter
Z = 8533741
20 Z = 2601084
32
XDOT = 8194
396954 XDOT = 2497
652192
YDOT = 14915
341046 feet/sec YDOT = 4546
195951 meter/sec
ZDOT = 17199
031930 ZDOT = 5242
264932
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 12187
55899817
00016717 00000-0 10270-3 0 9132
2 25544 51
6382 30
5541 0007248 123
0166 237
1685 15
55959499 20875
Satellite: ISS
Catalog Number: 25544
Epoch time: 12187
55899817 = yrday
fracday
Element set: 913
Inclination: 51
6382 deg
RA of node: 30
5541 deg
Eccentricity:
0007248
Arg of perigee: 123
0166 deg
Mean anomaly: 237
1685 deg
Mean motion: 15
55959499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 341
Coasting Arc #15 (Orbit 2101)
---------------------------------------
Vector Time (GMT): 2012/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2116253
79 A = 6776030
06 meter
Y = -4773333
12 meter E =
0014140
Z = -4330190
33 I = 51
78275
XDOT = 6806
439963 Wp = 94
50456
YDOT = 159
793387 meter/sec RA = 25
32106 deg
ZDOT = -3513
551898 TA = 139
83619
MA = 139
73160
Ha = 220
604 n
mi
Hp = 209
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6943089
85 X = -2041685
41
Y = -15660541
74 feet Y = -4796580
96 meter
Z = -14206661
18 Z = -4340290
23
XDOT = 22330
839775 XDOT = 6821
214978
YDOT = 524
256518 feet/sec YDOT = 235
990231 meter/sec
ZDOT = -11527
401241 ZDOT = -3480
451218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13525168
11 X = -4122471
24
Y = 10457502
43 feet Y = 3187446
74 meter
Z = -14247763
21 Z = -4342718
23
XDOT = -4174
674354 XDOT = -1272
440743
YDOT = -20869
923936 feet/sec YDOT = -6361
152816 meter/sec
ZDOT = -11390
898427 ZDOT = -3471
945840
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 12188
52240211
00016717 00000-0 10270-3 0 9149
2 25544 51
6372 25
7368 0007314 125
6351 234
5485 15
55952998 21029
Satellite: ISS
Catalog Number: 25544
Epoch time: 12188
52240211 = yrday
fracday
Element set: 914
Inclination: 51
6372 deg
RA of node: 25
7368 deg
Eccentricity:
0007314
Arg of perigee: 125
6351 deg
Mean anomaly: 234
5485 deg
Mean motion: 15
55952998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 302
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list