[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 25th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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
There are no maneuvers
Coasting Arc #1 (Orbit 2863)
---------------------------------------
Vector Time (GMT): 2012/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5085902
63 A = 6801146
61 meter
Y = 4483976
79 meter E =
0024393
Z = -262137
00 I = 51
88623
XDOT = -3305
044586 Wp = 15
17843
YDOT = -3404
907624 meter/sec RA = 140
33707 deg
ZDOT = 6030
238674 TA = 342
00711
MA = 342
09330
Ha = 231
254 n
mi
Hp = 218
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16686032
24 X = -5134391
99
Y = 14711209
95 feet Y = 4426831
95 meter
Z = -860029
52 Z = -286961
76
XDOT = -10843
322133 XDOT = -3296
017993
YDOT = -11170
956773 feet/sec YDOT = -3441
816226 meter/sec
ZDOT = 19784
247619 ZDOT = 6014
204899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21601316
84 X = 6584081
37
Y = -5295160
98 feet Y = -1613965
07 meter
Z = -963016
98 Z = -293527
57
XDOT = 4145
796076 XDOT = 1263
638644
YDOT = 13406
002169 feet/sec YDOT = 4086
149461 meter/sec
ZDOT = 19718
260859 ZDOT = 6010
125910
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 12237
50056760
00016717 00000-0 10270-3 0 9001
2 25544 51
6459 141
3544 0015289 353
9795 6
1170 15
50062977 28647
Satellite: ISS
Catalog Number: 25544
Epoch time: 12237
50056760 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 141
3544 deg
Eccentricity:
0015289
Arg of perigee: 353
9795 deg
Mean anomaly: 6
1170 deg
Mean motion: 15
50062977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2864
Checksum: 312
Coasting Arc #2 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2012/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4912753
55 A = 6801147
19 meter
Y = -4708325
53 meter E =
0010234
Z = -123553
62 I = 51
90948
XDOT = 3191
418472 Wp = 49
46746
YDOT = 3479
513349 meter/sec RA = 135
40176 deg
ZDOT = -6019
615475 TA = 131
85427
MA = 131
76687
Ha = 231
346 n
mi
Hp = 218
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16117957
85 X = 4965638
09
Y = -15447262
24 feet Y = -4653092
37 meter
Z = -405359
66 Z = -99559
47
XDOT = 10470
533046 XDOT = 3181
514355
YDOT = 11415
726209 feet/sec YDOT = 3515
146472 meter/sec
ZDOT = -19749
394602 ZDOT = -6004
135838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21336446
08 X = -6503348
76
Y = 6575208
49 feet Y = 2004123
55 meter
Z = -305769
23 Z = -93198
46
XDOT = -3866
326583 XDOT = -1178
456342
YDOT = -13396
601625 feet/sec YDOT = -4083
284175 meter/sec
ZDOT = -19685
701347 ZDOT = -6000
201771
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 12238
53209139
00016717 00000-0 10270-3 0 9016
2 25544 51
6464 136
2433 0015145 357
6872 2
4206 15
50066269 28806
Satellite: ISS
Catalog Number: 25544
Epoch time: 12238
53209139 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 136
2433 deg
Eccentricity:
0015145
Arg of perigee: 357
6872 deg
Mean anomaly: 2
4206 deg
Mean motion: 15
50066269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 296
Coasting Arc #3 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2012/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4670589
39 A = 6801026
83 meter
Y = 4897463
96 meter E =
0025706
Z = 478431
79 I = 51
93048
XDOT = -3135
198542 Wp = 23
47824
YDOT = -3586
338383 meter/sec RA = 130
46751 deg
ZDOT = 6017
008714 TA = 341
66092
MA = 341
75344
Ha = 231
526 n
mi
Hp = 218
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15323456
02 X = -4727330
81
Y = 16067795
16 feet Y = 4844917
26 meter
Z = 1569658
11 Z = 455604
78
XDOT = -10286
084455 XDOT = -3124
091266
YDOT = -11766
202043 feet/sec YDOT = -3621
336084 meter/sec
ZDOT = 19740
842236 ZDOT = 6001
805185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20779304
29 X = 6333531
95
Y = -7841649
83 feet Y = -2390134
87 meter
Z = 1474860
48 Z = 449537
47
XDOT = 3712
450460 XDOT = 1131
554900
YDOT = 13596
254453 feet/sec YDOT = 4144
138357 meter/sec
ZDOT = 19678
295495 ZDOT = 5997
944467
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 12239
56360751
00016717 00000-0 10270-3 0 9029
2 25544 51
6468 131
1322 0015359 1
3142 358
8046 15
50088538 28961
Satellite: ISS
Catalog Number: 25544
Epoch time: 12239
56360751 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 131
1322 deg
Eccentricity:
0015359
Arg of perigee: 1
3142 deg
Mean anomaly: 358
8046 deg
Mean motion: 15
50088538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 304
Coasting Arc #4 (Orbit 2910)
---------------------------------------
Vector Time (GMT): 2012/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4457457
99 A = 6800809
83 meter
Y = -5069876
46 meter E =
0010575
Z = -869631
17 I = 51
94906
XDOT = 3067
729271 Wp = 46
62446
YDOT = 3710
210287 meter/sec RA = 125
53512 deg
ZDOT = -5944
379041 TA = 142
71294
MA = 142
63948
Ha = 231
581 n
mi
Hp = 218
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14624206
00 X = 4518043
51
Y = -16633452
96 feet Y = -5019691
64 meter
Z = -2853120
64 Z = -847830
22
XDOT = 10064
728580 XDOT = 3054
888913
YDOT = 12172
605929 feet/sec YDOT = 3744
443734 meter/sec
ZDOT = -19502
555908 ZDOT = -5929
507592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20249340
03 X = -6171998
84
Y = 9000670
81 feet Y = 2743404
46 meter
Z = -2762536
74 Z = -842021
20
XDOT = -3515
086100 XDOT = -1071
398243
YDOT = -13835
233570 feet/sec YDOT = -4216
979192 meter/sec
ZDOT = -19441
388518 ZDOT = -5925
735220
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 12240
53064765
00016717 00000-0 10270-3 0 9035
2 25544 51
6472 126
3409 0015179 4
6408 355
4884 15
50080537 29111
Satellite: ISS
Catalog Number: 25544
Epoch time: 12240
53064765 = yrday
fracday
Element set: 903
Inclination: 51
6472 deg
RA of node: 126
3409 deg
Eccentricity:
0015179
Arg of perigee: 4
6408 deg
Mean anomaly: 355
4884 deg
Mean motion: 15
50080537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 300
Coasting Arc #5 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2012/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4185273
32 A = 6800430
88 meter
Y = 5196320
53 meter E =
0026377
Z = 1223290
93 I = 51
96493
XDOT = -3063
633304 Wp = 31
71333
YDOT = -3860
955077 meter/sec RA = 120
60306 deg
ZDOT = 5883
475912 TA = 341
52244
MA = 341
61806
Ha = 231
765 n
mi
Hp = 218
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13731211
68 X = -4249010
95
Y = 17048295
70 feet Y = 5149161
85 meter
Z = 4013421
68 Z = 1202804
50
XDOT = -10051
290366 XDOT = -3048
811668
YDOT = -12667
175449 feet/sec YDOT = -3895
131518 meter/sec
ZDOT = 19302
742492 ZDOT = 5868
629295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19447059
39 X = 5927463
70
Y = -10083592
37 feet Y = -3073478
95 meter
Z = 3928251
51 Z = 1197331
06
XDOT = 3486
712368 XDOT = 1062
749930
YDOT = 14266
721113 feet/sec YDOT = 4348
496595 meter/sec
ZDOT = 19241
686925 ZDOT = 5864
866175
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 12241
56214972
00016717 00000-0 10270-3 0 9047
2 25544 51
6473 121
2296 0015425 8
2554 351
8847 15
50114211 29279
Satellite: ISS
Catalog Number: 25544
Epoch time: 12241
56214972 = yrday
fracday
Element set: 904
Inclination: 51
6473 deg
RA of node: 121
2296 deg
Eccentricity:
0015425
Arg of perigee: 8
2554 deg
Mean anomaly: 351
8847 deg
Mean motion: 15
50114211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 290
Coasting Arc #6 (Orbit 2941)
---------------------------------------
Vector Time (GMT): 2012/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3948552
04 A = 6799987
49 meter
Y = -5305545
59 meter E =
0011707
Z = -1611779
79 I = 51
97787
XDOT = 3055
957713 Wp = 42
82477
YDOT = 4015
403512 meter/sec RA = 115
67254 deg
ZDOT = -5747
314085 TA = 154
66673
MA = 154
60929
Ha = 231
790 n
mi
Hp = 217
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12954567
08 X = 4015415
80
Y = -17406645
64 feet Y = -5261016
64 meter
Z = -5287991
44 Z = -1592435
62
XDOT = 10026
107982 XDOT = 3038
748131
YDOT = 13173
896036 feet/sec YDOT = 4049
480637 meter/sec
ZDOT = -18856
017338 ZDOT = -5732
510660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18699872
95 X = -5699721
28
Y = 11044065
75 feet Y = 3366231
24 meter
Z = -5207526
99 Z = -1587254
23
XDOT = -3464
470534 XDOT = -1055
970619
YDOT = -14702
955622 feet/sec YDOT = -4481
460874 meter/sec
ZDOT = -18795
151035 ZDOT = -5728
762035
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 12242
52917703
00016717 00000-0 10270-3 0 9057
2 25544 51
6472 116
4384 0015243 11
5085 348
6411 15
50101595 29425
Satellite: ISS
Catalog Number: 25544
Epoch time: 12242
52917703 = yrday
fracday
Element set: 905
Inclination: 51
6472 deg
RA of node: 116
4384 deg
Eccentricity:
0015243
Arg of perigee: 11
5085 deg
Mean anomaly: 348
6411 deg
Mean motion: 15
50101595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2942
Checksum: 286
Coasting Arc #7 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2012/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3665343
15 A = 6799379
20 meter
Y = 5360767
16 meter E =
0026352
Z = 1956515
03 I = 51
98786
XDOT = -3114
899836 Wp = 39
82688
YDOT = -4191
047410 meter/sec RA = 110
74142 deg
ZDOT = 5625
805228 TA = 341
65059
MA = 341
74547
Ha = 231
965 n
mi
Hp = 217
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12025404
03 X = -3734520
08
Y = 17587818
76 feet Y = 5319392
35 meter
Z = 6419012
56 Z = 1938540
88
XDOT = -10219
487650 XDOT = -3095
131581
YDOT = -13750
155546 feet/sec YDOT = -4225
769243 meter/sec
ZDOT = 18457
366232 ZDOT = 5610
721758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17717486
03 X = 5400289
74
Y = -11873803
83 feet Y = -3619135
41 meter
Z = 6344202
44 Z = 1933712
90
XDOT = 3643
781306 XDOT = 1110
624542
YDOT = 15304
802091 feet/sec YDOT = 4664
903677 meter/sec
ZDOT = 18395
356138 ZDOT = 5606
904551
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 12243
56066525
00016717 00000-0 10270-3 0 9060
2 25544 51
6467 111
3266 0015461 15
1063 345
0546 15
50139546 29584
Satellite: ISS
Catalog Number: 25544
Epoch time: 12243
56066525 = yrday
fracday
Element set: 906
Inclination: 51
6467 deg
RA of node: 111
3266 deg
Eccentricity:
0015461
Arg of perigee: 15
1063 deg
Mean anomaly: 345
0546 deg
Mean motion: 15
50139546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 298
Coasting Arc #8 (Orbit 2972)
---------------------------------------
Vector Time (GMT): 2012/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3424750
29 A = 6798718
05 meter
Y = -5400968
23 meter E =
0013705
Z = -2333602
17 I = 51
99472
XDOT = 3174
044558 Wp = 40
68874
YDOT = 4353
770102 meter/sec RA = 105
81143 deg
ZDOT = -5426
218255 TA = 165
09878
MA = 165
05836
Ha = 231
973 n
mi
Hp = 217
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11236057
37 X = 3496226
45
Y = -17719712
04 feet Y = -5362271
09 meter
Z = -7656175
11 Z = -2316791
06
XDOT = 10413
532016 XDOT = 3151
482864
YDOT = 14284
022645 feet/sec YDOT = 4389
137632 meter/sec
ZDOT = -17802
553331 ZDOT = -5410
854288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16826236
49 X = -5128636
88
Y = 12577044
92 feet Y = 3833483
29 meter
Z = -7586165
29 Z = -2312263
18
XDOT = -3865
990796 XDOT = -1178
353995
YDOT = -15856
375351 feet/sec YDOT = -4833
023207 meter/sec
ZDOT = -17739
398689 ZDOT = -5406
968721
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 12244
52767952
00016717 00000-0 10270-3 0 9070
2 25544 51
6460 106
5350 0015325 18
4074 341
7628 15
50130115 29738
Satellite: ISS
Catalog Number: 25544
Epoch time: 12244
52767952 = yrday
fracday
Element set: 907
Inclination: 51
6460 deg
RA of node: 106
5350 deg
Eccentricity:
0015325
Arg of perigee: 18
4074 deg
Mean anomaly: 341
7628 deg
Mean motion: 15
50130115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2973
Checksum: 292
Coasting Arc #9 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2012/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3151810
74 A = 6797936
05 meter
Y = 5382466
18 meter E =
0025651
Z = 2661131
39 I = 51
99900
XDOT = -3300
262694 Wp = 47
70833
YDOT = -4532
301074 meter/sec RA = 100
88022 deg
ZDOT = 5243
012176 TA = 342
15912
MA = 342
24901
Ha = 232
128 n
mi
Hp = 217
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10340586
41 X = -3224691
38
Y = 17659009
77 feet Y = 5346813
42 meter
Z = 8730746
02 Z = 2645642
65
XDOT = -10827
633509 XDOT = -3274
805392
YDOT = -14869
754181 feet/sec YDOT = -4569
063822 meter/sec
ZDOT = 17201
483518 ZDOT = 5227
042088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15750332
73 X = 4800701
42
Y = -13107946
77 feet Y = -3995302
18 meter
Z = 8666200
40 Z = 2641457
88
XDOT = 4308
733579 XDOT = 1313
301995
YDOT = 16540
034684 feet/sec YDOT = 5041
402572 meter/sec
ZDOT = 17135
841456 ZDOT = 5223
004476
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 12245
55915391
00016717 00000-0 10270-3 0 9087
2 25544 51
6453 101
4226 0015454 21
9627 338
2183 15
50163004 29899
Satellite: ISS
Catalog Number: 25544
Epoch time: 12245
55915391 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 101
4226 deg
Eccentricity:
0015454
Arg of perigee: 21
9627 deg
Mean anomaly: 338
2183 deg
Mean motion: 15
50163004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 300
Coasting Arc #10 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2012/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2928486
51 A = 6797094
13 meter
Y = -5354255
95 meter E =
0016384
Z = -3017733
66 I = 51
99997
XDOT = 3425
679867 Wp = 41
43134
YDOT = 4679
523767 meter/sec RA = 95
94970 deg
ZDOT = -4981
891232 TA = 172
79733
MA = 172
77376
Ha = 232
133 n
mi
Hp = 217
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9607895
38 X = 3002800
64
Y = -17566456
52 feet Y = -5321092
58 meter
Z = -9900700
97 Z = -3003326
25
XDOT = 11239
107174 XDOT = 3397
298617
YDOT = 15352
768265 feet/sec YDOT = 4717
672666 meter/sec
ZDOT = -16344
787505 ZDOT = -4965
318942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14805828
35 X = -4512816
48
Y = 13522777
95 feet Y = 4121742
72 meter
Z = -9840622
53 Z = -2999421
75
XDOT = -4811
191844 XDOT = -1466
451274
YDOT = -17103
808132 feet/sec YDOT = -5213
240719 meter/sec
ZDOT = -16276
673708 ZDOT = -4961
130146
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 12246
52615509
00016717 00000-0 10270-3 0 9094
2 25544 51
6443 96
6305 0015404 25
4794 334
7112 15
50162439 30043
Satellite: ISS
Catalog Number: 25544
Epoch time: 12246
52615509 = yrday
fracday
Element set: 909
Inclination: 51
6443 deg
RA of node: 96
6305 deg
Eccentricity:
0015404
Arg of perigee: 25
4794 deg
Mean anomaly: 334
7112 deg
Mean motion: 15
50162439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 291
Coasting Arc #11 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2012/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2687378
31 A = 6796205
82 meter
Y = 5266231
44 meter E =
0024386
Z = 3319298
24 I = 51
99903
XDOT = -3615
972604 Wp = 55
18356
YDOT = -4838
121779 meter/sec RA = 91
01780 deg
ZDOT = 4737
336979 TA = 343
22416
MA = 343
30467
Ha = 232
264 n
mi
Hp = 216
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8816857
98 X = -2762191
04
Y = 17277662
21 feet Y = 5235761
52 meter
Z = 10890086
10 Z = 3306060
89
XDOT = -11863
427180 XDOT = -3584
615838
YDOT = -15873
102951 feet/sec YDOT = -4878
382057 meter/sec
ZDOT = 15542
444157 ZDOT = 4719
847421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13735384
64 X = 4186545
24
Y = -13740228
80 feet Y = -4188021
74 meter
Z = 10834846
23 Z = 3302461
13
XDOT = 5538
155835 XDOT = 1688
029899
YDOT = 17764
131098 feet/sec YDOT = 5414
507159 meter/sec
ZDOT = 15470
558443 ZDOT = 4715
426213
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 12247
55761570
00016717 00000-0 10270-3 0 9100
2 25544 51
6440 91
5178 0015418 28
9810 331
2193 15
50183926 30207
Satellite: ISS
Catalog Number: 25544
Epoch time: 12247
55761570 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 91
5178 deg
Eccentricity:
0015418
Arg of perigee: 28
9810 deg
Mean anomaly: 331
2193 deg
Mean motion: 15
50183926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 291
Coasting Arc #12 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2012/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2501742
38 A = 6795252
17 meter
Y = -5177016
01 meter E =
0019438
Z = -3646205
44 I = 51
99462
XDOT = 3799
253367 Wp = 44
84275
YDOT = 4947
175965 meter/sec RA = 86
08608 deg
ZDOT = -4418
412207 TA = 177
97442
MA = 177
96654
Ha = 232
273 n
mi
Hp = 216
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8207816
19 X = 2577159
35
Y = -16984960
67 feet Y = -5148618
60 meter
Z = -11962616
29 Z = -3633868
46
XDOT = 12464
742019 XDOT = 3765
114307
YDOT = 16230
892273 feet/sec YDOT = 4989
470322 meter/sec
ZDOT = -14496
103040 ZDOT = -4400
038951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12835677
84 X = -3912314
61
Y = 13868396
45 feet Y = 4227087
24 meter
Z = -11911098
95 Z = -3630502
96
XDOT = -6316
761063 XDOT = -1925
348772
YDOT = -18228
950531 feet/sec YDOT = -5556
184122 meter/sec
ZDOT = -14420
580861 ZDOT = -4395
393047
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 12248
52460392
00016717 00000-0 10270-3 0 9117
2 25544 51
6431 86
7253 0015461 32
8334 327
3774 15
50193367 30357
Satellite: ISS
Catalog Number: 25544
Epoch time: 12248
52460392 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 86
7253 deg
Eccentricity:
0015461
Arg of perigee: 32
8334 deg
Mean anomaly: 327
3774 deg
Mean motion: 15
50193367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 298
Coasting Arc #13 (Orbit 3050)
---------------------------------------
Vector Time (GMT): 2012/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2312139
26 A = 6794326
24 meter
Y = 5030309
12 meter E =
0022743
Z = 3912813
44 I = 51
98866
XDOT = -4042
907705 Wp = 61
95526
YDOT = -5064
722774 meter/sec RA = 81
15302 deg
ZDOT = 4114
450980 TA = 345
14483
MA = 345
21153
Ha = 232
384 n
mi
Hp = 216
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7585758
74 X = -2387224
97
Y = 16503638
83 feet Y = 5004033
79 meter
Z = 12837314
44 Z = 3901398
41
XDOT = -13264
132889 XDOT = -4005
959552
YDOT = -16616
544534 feet/sec YDOT = -5109
726200 meter/sec
ZDOT = 13498
854922 ZDOT = 4094
900802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11870743
63 X = 3618202
66
Y = -13792087
82 feet Y = -4203828
37 meter
Z = 12789614
21 Z = 3898274
41
XDOT = 7309
087379 XDOT = 2227
809833
YDOT = 18757
670469 feet/sec YDOT = 5717
337959 meter/sec
ZDOT = 13418
484768 ZDOT = 4089
954157
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 12249
55605061
00016717 00000-0 10270-3 0 9126
2 25544 51
6432 81
6127 0015384 36
2874 323
9317 15
50203127 30512
Satellite: ISS
Catalog Number: 25544
Epoch time: 12249
55605061 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 81
6127 deg
Eccentricity:
0015384
Arg of perigee: 36
2874 deg
Mean anomaly: 323
9317 deg
Mean motion: 15
50203127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3051
Checksum: 282
Coasting Arc #14 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2012/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2181706
11 A = 6793353
25 meter
Y = -4893823
12 meter E =
0022549
Z = -4201023
85 I = 51
97950
XDOT = 4268
335318 Wp = 50
17619
YDOT = 5116
728438 meter/sec RA = 76
21963 deg
ZDOT = -3743
201460 TA = 181
37992
MA = 181
38615
Ha = 232
395 n
mi
Hp = 216
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7157828
43 X = 2256675
36
Y = -16055850
12 feet Y = -4869006
99 meter
Z = -13782886
64 Z = -4190242
81
XDOT = 14003
724797 XDOT = 4228
985425
YDOT = 16787
166792 feet/sec YDOT = 5164
239382 meter/sec
ZDOT = -12280
844686 ZDOT = -3722
561934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11109110
46 X = -3386056
87
Y = 13669417
71 feet Y = 4166438
52 meter
Z = -13737812
03 Z = -4187285
11
XDOT = -8318
435506 XDOT = -2535
459142
YDOT = -19019
611406 feet/sec YDOT = -5797
177557 meter/sec
ZDOT = -12195
982117 ZDOT = -3717
335349
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 12250
52302581
00016717 00000-0 10270-3 0 9137
2 25544 51
6428 76
8203 0015501 40
4392 319
7908 15
50220109 30665
Satellite: ISS
Catalog Number: 25544
Epoch time: 12250
52302581 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 76
8203 deg
Eccentricity:
0015501
Arg of perigee: 40
4392 deg
Mean anomaly: 319
7908 deg
Mean motion: 15
50220109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 276
Coasting Arc #15 (Orbit 3081)
---------------------------------------
Vector Time (GMT): 2012/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2059326
47 A = 6792460
30 meter
Y = 4705088
30 meter E =
0020956
Z = 4423753
19 I = 51
96843
XDOT = -4547
810030 Wp = 67
54764
YDOT = -5176
283586 meter/sec RA = 71
28468 deg
ZDOT = 3383
454331 TA = 348
40097
MA = 348
44918
Ha = 232
499 n
mi
Hp = 216
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6756320
43 X = -2133276
29
Y = 15436641
39 feet Y = 4681646
37 meter
Z = 14513625
95 Z = 4413569
21
XDOT = -14920
636581 XDOT = -4506
025817
YDOT = -16982
557697 feet/sec YDOT = -5226
906234 meter/sec
ZDOT = 11100
571953 ZDOT = 3361
463015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10338740
10 X = 3151247
98
Y = -13352259
46 feet Y = -4069768
68 meter
Z = 14471030
44 Z = 4410770
08
XDOT = 9517
800972 XDOT = 2901
025736
YDOT = 19319
989893 feet/sec YDOT = 5888
732919 meter/sec
ZDOT = 11010
131281 ZDOT = 3355
888014
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 12251
55445826
00016717 00000-0 10270-3 0 9142
2 25544 51
6428 71
7077 0015386 43
8545 316
3824 15
50222083 30827
Satellite: ISS
Catalog Number: 25544
Epoch time: 12251
55445826 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 71
7077 deg
Eccentricity:
0015386
Arg of perigee: 43
8545 deg
Mean anomaly: 316
3824 deg
Mean motion: 15
50222083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 303
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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