[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 21st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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
091/21:57:19
878 -1
5 3
1 3
1
N/A -1
3 0
0 214
2
000/00:06:39
757 2
4 -0
1 207
8
Coasting Arc #1 (Orbit 403)
---------------------------------------
Vector Time (GMT): 2012/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1293639
90 A = 6762388
16 meter
Y = -4082157
77 meter E =
0018703
Z = 5232320
34 I = 51
43974
XDOT = 6883
638585 Wp = 166
76116
YDOT = 3294
854954 meter/sec RA = 210
67306 deg
ZDOT = 850
186735 TA = 274
99206
MA = 275
20554
Ha = 217
436 n
mi
Hp = 203
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4244225
39 X = 1313774
22
Y = -13392906
06 feet Y = -4067578
28 meter
Z = 17166405
31 Z = 5238654
08
XDOT = 22584
116094 XDOT = 6842
153292
YDOT = 10809
891583 feet/sec YDOT = 3371
600200 meter/sec
ZDOT = 2789
326559 ZDOT = 883
525468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4918458
80 X = 1499146
24
Y = -13125983
84 feet Y = -4000799
87 meter
Z = 17192619
48 Z = 5240310
42
XDOT = 20936
449121 XDOT = 6381
429692
YDOT = 11756
838239 feet/sec YDOT = 3583
484295 meter/sec
ZDOT = 2925
902779 ZDOT = 891
815167
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 12079
54958658
00016717 00000-0 10270-3 0 9006
2 25544 51
6399 211
4496 0016494 175
0533 185
0788 15
59373470 4049
Satellite: ISS
Catalog Number: 25544
Epoch time: 12079
54958658 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 211
4496 deg
Eccentricity:
0016494
Arg of perigee: 175
0533 deg
Mean anomaly: 185
0788 deg
Mean motion: 15
59373470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 404
Checksum: 339
Coasting Arc #2 (Orbit 418)
---------------------------------------
Vector Time (GMT): 2012/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4603088
19 A = 6764945
78 meter
Y = 1865257
92 meter E =
0022482
Z = -4611765
74 I = 51
47591
XDOT = -4997
775732 Wp = 153
12722
YDOT = -5001
157170 meter/sec RA = 205
60774 deg
ZDOT = 2951
603257 TA = 146
44384
MA = 146
30124
Ha = 217
275 n
mi
Hp = 203
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15101995
37 X = -4601201
11
Y = 6119612
61 feet Y = 1813793
29 meter
Z = -15130465
02 Z = -4634122
73
XDOT = -16396
902007 XDOT = -4955
818390
YDOT = -16407
995964 feet/sec YDOT = -5056
810399 meter/sec
ZDOT = 9683
737719 ZDOT = 2927
427157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15250738
86 X = -4648425
20
Y = 5490700
35 feet Y = 1673565
47 meter
Z = -15222288
54 Z = -4639753
55
XDOT = -15360
086056 XDOT = -4681
754230
YDOT = -15964
019676 feet/sec YDOT = -4865
833197 meter/sec
ZDOT = 9584
833978 ZDOT = 2921
457397
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 12080
51087172
00016717 00000-0 10270-3 0 9010
2 25544 51
6405 206
6199 0016454 178
4294 181
6915 15
59384374 4195
Satellite: ISS
Catalog Number: 25544
Epoch time: 12080
51087172 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 206
6199 deg
Eccentricity:
0016454
Arg of perigee: 178
4294 deg
Mean anomaly: 181
6915 deg
Mean motion: 15
59384374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 419
Checksum: 319
Coasting Arc #3 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2012/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6400197
58 A = 6772176
61 meter
Y = 653121
36 meter E =
0024692
Z = 2061266
74 I = 51
52873
XDOT = 1259
666595 Wp = 149
91474
YDOT = 5178
808831 meter/sec RA = 200
57627 deg
ZDOT = -5544
445580 TA = 7
14812
MA = 7
11297
Ha = 217
048 n
mi
Hp = 203
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20998023
57 X = 6382405
48
Y = 2142786
60 feet Y = 724593
13 meter
Z = 6762686
15 Z = 2092315
05
XDOT = 4132
764418 XDOT = 1228
595944
YDOT = 16990
842623 feet/sec YDOT = 5192
720704 meter/sec
ZDOT = -18190
438256 ZDOT = -5538
402417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20898275
59 X = 6369794
40
Y = 2651785
78 feet Y = 808264
30 meter
Z = 6890033
50 Z = 2100082
21
XDOT = 4022
478450 XDOT = 1226
051432
YDOT = 15564
006611 feet/sec YDOT = 4743
909215 meter/sec
ZDOT = -18165
929788 ZDOT = -5536
975399
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 12081
53622190
00016717 00000-0 10270-3 0 9029
2 25544 51
6411 201
4673 0016450 182
0880 178
0209 15
59397764 4351
Satellite: ISS
Catalog Number: 25544
Epoch time: 12081
53622190 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 201
4673 deg
Eccentricity:
0016450
Arg of perigee: 182
0880 deg
Mean anomaly: 178
0209 deg
Mean motion: 15
59397764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 435
Checksum: 294
Coasting Arc #4 (Orbit 450)
---------------------------------------
Vector Time (GMT): 2012/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6031551
42 A = 6773161
29 meter
Y = -2785306
82 meter E =
0013774
Z = 1340148
61 I = 51
56229
XDOT = 3110
860837 Wp = 131
91493
YDOT = -3918
821140 meter/sec RA = 195
57444 deg
ZDOT = 5808
724796 TA = 242
70737
MA = 242
84770
Ha = 216
849 n
mi
Hp = 203
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19788554
53 X = -6006467
39
Y = -9138145
74 feet Y = -2852614
92 meter
Z = 4396813
02 Z = 1310909
03
XDOT = 10206
236341 XDOT = 3126
233304
YDOT = -12857
024738 feet/sec YDOT = -3883
946811 meter/sec
ZDOT = 19057
496051 ZDOT = 5823
875044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19749522
47 X = -6019654
45
Y = -9278374
33 feet Y = -2828048
50 meter
Z = 4276995
98 Z = 1303628
37
XDOT = 9504
688173 XDOT = 2897
028955
YDOT = -11343
839130 feet/sec YDOT = -3457
602167 meter/sec
ZDOT = 19119
871877 ZDOT = 5827
736948
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 12082
56154947
00016717 00000-0 10270-3 0 9034
2 25544 51
6420 196
3148 0016249 185
8317 174
2652 15
59454777 4518
Satellite: ISS
Catalog Number: 25544
Epoch time: 12082
56154947 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 196
3148 deg
Eccentricity:
0016249
Arg of perigee: 185
8317 deg
Mean anomaly: 174
2652 deg
Mean motion: 15
59454777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 451
Checksum: 326
Coasting Arc #5 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2012/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3412109
61 A = 6766329
22 meter
Y = 4039506
84 meter E =
0014096
Z = -4217003
69 I = 51
56929
XDOT = -6532
380655 Wp = 160
71734
YDOT = 1726
910191 meter/sec RA = 190
55628 deg
ZDOT = -3647
835127 TA = 72
02655
MA = 71
87296
Ha = 216
692 n
mi
Hp = 204
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11194585
34 X = 3387170
69
Y = 13252975
20 feet Y = 4077523
16 meter
Z = -13835313
94 Z = -4200488
92
XDOT = -21431
695062 XDOT = -6533
485443
YDOT = 5665
715850 feet/sec YDOT = 1653
854412 meter/sec
ZDOT = -11967
963015 ZDOT = -3679
572052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11411737
71 X = 3478297
65
Y = 13137607
04 feet Y = 4004342
62 meter
Z = -13767771
36 Z = -4196416
71
XDOT = -20342
253831 XDOT = -6200
318968
YDOT = 5048
351757 feet/sec YDOT = 1538
737616 meter/sec
ZDOT = -12098
282072 ZDOT = -3687
556375
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 12083
52277590
00016717 00000-0 10270-3 0 9042
2 25544 51
6421 191
4847 0016225 189
8459 170
2381 15
59465000 4668
Satellite: ISS
Catalog Number: 25544
Epoch time: 12083
52277590 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 191
4847 deg
Eccentricity:
0016225
Arg of perigee: 189
8459 deg
Mean anomaly: 170
2381 deg
Mean motion: 15
59465000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 314
Coasting Arc #6 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2012/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 440225
16 A = 6761622
90 meter
Y = -4178924
64 meter E =
0015674
Z = 5298571
22 I = 51
58483
XDOT = 7638
049006 Wp = 185
41894
YDOT = 769
856592 meter/sec RA = 185
50269 deg
ZDOT = -42
718906 TA = 264
89852
MA = 265
07743
Ha = 216
311 n
mi
Hp = 204
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1444308
26 X = 461182
67
Y = -13710382
69 feet Y = -4173883
96 meter
Z = 17383763
84 Z = 5300761
23
XDOT = 25059
215898 XDOT = 7629
080153
YDOT = 2525
776221 feet/sec YDOT = 855
219825 meter/sec
ZDOT = -140
153892 ZDOT = -5
635368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 963879
78 X = 293790
56
Y = -13740851
40 feet Y = -4188211
51 meter
Z = 17392981
44 Z = 5301380
74
XDOT = 24117
220589 XDOT = 7350
928836
YDOT = 1770
410632 feet/sec YDOT = 539
621161 meter/sec
ZDOT = 11
977248 ZDOT = 3
650665
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 12084
54806206
00016717 00000-0 10270-3 0 9058
2 25544 51
6423 186
3324 0016041 193
7263 166
3458 15
59544377 4820
Satellite: ISS
Catalog Number: 25544
Epoch time: 12084
54806206 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 186
3324 deg
Eccentricity:
0016041
Arg of perigee: 193
7263 deg
Mean anomaly: 166
3458 deg
Mean motion: 15
59544377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 482
Checksum: 312
Coasting Arc #7 (Orbit 496)
---------------------------------------
Vector Time (GMT): 2012/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4257596
79 A = 6766177
80 meter
Y = 3250769
65 meter E =
0018106
Z = -4148151
26 I = 51
63046
XDOT = -5968
386672 Wp = 171
93563
YDOT = -3014
452436 meter/sec RA = 180
45118 deg
ZDOT = 3747
968978 TA = 136
71880
MA = 136
57641
Ha = 216
083 n
mi
Hp = 204
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13968493
39 X = -4273480
22
Y = 10665254
77 feet Y = 3203069
33 meter
Z = -13609420
13 Z = -4168873
50
XDOT = -19581
321102 XDOT = -5952
441755
YDOT = -9889
935813 feet/sec YDOT = -3081
105079 meter/sec
ZDOT = 12296
486149 ZDOT = 3719
013721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13397311
50 X = -4083500
55
Y = 11271715
82 feet Y = 3435618
98 meter
Z = -13694643
13 Z = -4174127
23
XDOT = -19254
254480 XDOT = -5868
696766
YDOT = -8028
009585 feet/sec YDOT = -2446
937322 meter/sec
ZDOT = 12177
825852 ZDOT = 3711
801320
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 12085
50925076
00016717 00000-0 10270-3 0 9063
2 25544 51
6420 181
5023 0015975 197
0965 162
9654 15
59558155 4976
Satellite: ISS
Catalog Number: 25544
Epoch time: 12085
50925076 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 181
5023 deg
Eccentricity:
0015975
Arg of perigee: 197
0965 deg
Mean anomaly: 162
9654 deg
Mean motion: 15
59558155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 497
Checksum: 333
Coasting Arc #8 (Orbit 512)
---------------------------------------
Vector Time (GMT): 2012/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6478009
42 A = 6772933
61 meter
Y = -1485187
41 meter E =
0022899
Z = 1221690
78 I = 51
68265
XDOT = 2135
622632 Wp = 164
62988
YDOT = 4483
369569 meter/sec RA = 175
43973 deg
ZDOT = -5870
305172 TA = 2
04778
MA = 2
03842
Ha = 215
870 n
mi
Hp = 204
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21253311
76 X = 6488200
89
Y = -4872662
12 feet Y = -1412689
22 meter
Z = 4008171
85 Z = 1253185
73
XDOT = 7006
635932 XDOT = 2113
846753
YDOT = 14709
217746 feet/sec YDOT = 4507
129144 meter/sec
ZDOT = -19259
531403 ZDOT = -5859
983644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20887679
98 X = 6366564
86
Y = -6172300
93 feet Y = -1881317
32 meter
Z = 4137519
14 Z = 1261115
83
XDOT = 7566
926139 XDOT = 2306
399087
YDOT = 12717
691280 feet/sec YDOT = 3876
352302 meter/sec
ZDOT = -19217
423087 ZDOT = -5857
470557
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 12086
53449820
00016717 00000-0 10270-3 0 9076
2 25544 51
6412 176
3499 0015906 200
6596 159
3918 15
59554164 5139
Satellite: ISS
Catalog Number: 25544
Epoch time: 12086
53449820 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 176
3499 deg
Eccentricity:
0015906
Arg of perigee: 200
6596 deg
Mean anomaly: 159
3918 deg
Mean motion: 15
59554164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 513
Checksum: 329
Coasting Arc #9 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2012/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6356327
25 A = 6771380
86 meter
Y = -718544
64 meter E =
0011813
Z = 2233637
42 I = 51
70838
XDOT = 2467
526755 Wp = 146
46818
YDOT = -4785
804963 meter/sec RA = 170
44686 deg
ZDOT = 5458
946249 TA = 238
36772
MA = 238
48303
Ha = 215
599 n
mi
Hp = 205
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20854092
02 X = -6358670
48
Y = -2357429
91 feet Y = -789637
95 meter
Z = 7328206
76 Z = 2202752
87
XDOT = 8095
560221 XDOT = 2494
340726
YDOT = -15701
459853 feet/sec YDOT = -4758
061221 meter/sec
ZDOT = 17909
928639 ZDOT = 5470
998935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21019008
72 X = -6406593
86
Y = -702314
12 feet Y = -214065
34 meter
Z = 7201477
02 Z = 2195010
19
XDOT = 6672
866181 XDOT = 2033
889612
YDOT = -14748
432837 feet/sec YDOT = -4495
322329 meter/sec
ZDOT = 17959
675907 ZDOT = 5474
109216
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 12087
55972287
00016717 00000-0 10270-3 0 9088
2 25544 51
6413 171
1962 0015767 204
8517 155
1881 15
59612208 5296
Satellite: ISS
Catalog Number: 25544
Epoch time: 12087
55972287 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 171
1962 deg
Eccentricity:
0015767
Arg of perigee: 204
8517 deg
Mean anomaly: 155
1881 deg
Mean motion: 15
59612208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 529
Checksum: 328
Coasting Arc #10 (Orbit 543)
---------------------------------------
Vector Time (GMT): 2012/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3870310
38 A = 6763879
61 meter
Y = 2866021
97 meter E =
0010594
Z = -4747431
93 I = 51
71220
XDOT = -6106
450531 Wp = 164
41919
YDOT = 3790
755530 meter/sec RA = 165
42667 deg
ZDOT = -2701
136169 TA = 79
01236
MA = 78
89321
Ha = 215
424 n
mi
Hp = 205
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12697868
71 X = 3861036
34
Y = 9402959
20 feet Y = 2909250
01 meter
Z = -15575564
08 Z = -4728652
78
XDOT = -20034
286520 XDOT = -6135
264118
YDOT = 12436
861976 feet/sec YDOT = 3722
308147 meter/sec
ZDOT = -8861
995305 ZDOT = -2730
871371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13635516
45 X = 4156105
41
Y = 8131085
55 feet Y = 2478354
88 meter
Z = -15498640
17 Z = -4723985
52
XDOT = -18101
470001 XDOT = -5517
328056
YDOT = 13302
020074 feet/sec YDOT = 4054
455718 meter/sec
ZDOT = -8984
283058 ZDOT = -2738
409476
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 12088
52085403
00016717 00000-0 10270-3 0 9092
2 25544 51
6403 166
3654 0015703 208
7293 151
2999 15
59616712 5441
Satellite: ISS
Catalog Number: 25544
Epoch time: 12088
52085403 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 166
3654 deg
Eccentricity:
0015703
Arg of perigee: 208
7293 deg
Mean anomaly: 151
2999 deg
Mean motion: 15
59616712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 544
Checksum: 317
Coasting Arc #11 (Orbit 559)
---------------------------------------
Vector Time (GMT): 2012/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -94798
54 A = 6761642
25 meter
Y = -4322032
25 meter E =
0012073
Z = 5201700
08 I = 51
73541
XDOT = 7403
335323 Wp = 205
74832
YDOT = -1617
469181 meter/sec RA = 160
37624 deg
ZDOT = -1220
702518 TA = 255
87081
MA = 256
00500
Ha = 215
012 n
mi
Hp = 205
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -311018
84 X = -71730
38
Y = -14179895
85 feet Y = -4322963
06 meter
Z = 17065945
13 Z = 5201295
84
XDOT = 24289
157885 XDOT = 7426
801861
YDOT = -5306
657418 feet/sec YDOT = -1534
549374 meter/sec
ZDOT = -4004
929521 ZDOT = -1184
680310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2015315
33 X = -614268
11
Y = -14041104
97 feet Y = -4279728
79 meter
Z = 17064540
36 Z = 5201271
90
XDOT = 22533
168899 XDOT = 6868
109880
YDOT = -7875
015682 feet/sec YDOT = -2400
304780 meter/sec
ZDOT = -3856
940976 ZDOT = -1175
595610
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 12089
54603895
00016717 00000-0 10270-3 0 9108
2 25544 51
6408 161
2118 0015613 212
9294 147
0890 15
59693857 5609
Satellite: ISS
Catalog Number: 25544
Epoch time: 12089
54603895 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 161
2118 deg
Eccentricity:
0015613
Arg of perigee: 212
9294 deg
Mean anomaly: 147
0890 deg
Mean motion: 15
59693857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 560
Checksum: 321
Coasting Arc #12 (Orbit 574)
---------------------------------------
Vector Time (GMT): 2012/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3632260
20 A = 6768187
02 meter
Y = 4603493
36 meter E =
0013204
Z = -3389115
35 I = 51
78505
XDOT = -5969
355278 Wp = 198
88418
YDOT = -1280
499371 meter/sec RA = 155
34272 deg
ZDOT = 4641
034389 TA = 121
55597
MA = 121
42697
Ha = 214
721 n
mi
Hp = 205
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11916864
18 X = -3667003
90
Y = 15103324
67 feet Y = 4562680
72 meter
Z = -11119144
86 Z = -3406845
35
XDOT = -19584
498943 XDOT = -5977
137883
YDOT = -4201
113423 feet/sec YDOT = -1347
295630 meter/sec
ZDOT = 15226
490779 ZDOT = 4612
016749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9782721
15 X = -2981773
41
Y = 16516356
43 feet Y = 5034185
44 meter
Z = -11192219
96 Z = -3411388
64
XDOT = -18851
582479 XDOT = -5745
962340
YDOT = -890
314554 feet/sec YDOT = -271
367876 meter/sec
ZDOT = 15107
417960 ZDOT = 4604
740994
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 12090
50713399
00016717 00000-0 10270-3 0 9118
2 25544 51
6399 156
3803 0015444 215
9661 144
0456 15
59712317 5751
Satellite: ISS
Catalog Number: 25544
Epoch time: 12090
50713399 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 156
3803 deg
Eccentricity:
0015444
Arg of perigee: 215
9661 deg
Mean anomaly: 144
0456 deg
Mean motion: 15
59712317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 575
Checksum: 313
Coasting Arc #13 (Orbit 590)
---------------------------------------
Vector Time (GMT): 2012/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5837131
38 A = 6773099
49 meter
Y = -3407212
45 meter E =
0020215
Z = 93510
33 I = 51
82932
XDOT = 2466
431516 Wp = 182
52884
YDOT = 4061
482251 meter/sec RA = 150
35047 deg
ZDOT = -6042
316599 TA = 356
46290
MA = 356
47717
Ha = 214
418 n
mi
Hp = 205
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19150693
52 X = 5874343
44
Y = -11178518
53 feet Y = -3341729
97 meter
Z = 306792
42 Z = 121957
34
XDOT = 8091
966916 XDOT = 2450
183985
YDOT = 13325
073003 feet/sec YDOT = 4088
972173 meter/sec
ZDOT = -19823
873355 ZDOT = -6030
374564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17294658
11 X = 5271411
79
Y = -13875072
65 feet Y = -4229122
14 meter
Z = 423815
90 Z = 129179
09
XDOT = 9072
135698 XDOT = 2765
186961
YDOT = 10708
996504 feet/sec YDOT = 3264
102134 meter/sec
ZDOT = -19775
076505 ZDOT = -6027
443319
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 12091
53228182
00016717 00000-0 10270-3 0 9124
2 25544 51
6404 151
2266 0015239 219
9984 140
0050 15
59729554 5914
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
53228182 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 151
2266 deg
Eccentricity:
0015239
Arg of perigee: 219
9984 deg
Mean anomaly: 140
0050 deg
Mean motion: 15
59729554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 591
Checksum: 302
Coasting Arc #14 (Orbit 597)
---------------------------------------
Vector Time (GMT): 2012/091/22:00:39
757
Vector Time (MET): N/A
Weight (LBS) : 886297
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5860720
98 A = 6774755
21 meter
Y = 3389180
47 meter E =
0001298
Z = 255247
48 I = 51
84069
XDOT = -2178
334743 Wp = 260
93452
YDOT = -4218
622767 meter/sec RA = 148
26210 deg
ZDOT = 6024
211441 TA = 101
81185
MA = 101
79729
Ha = 214
243 n
mi
Hp = 207
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19228087
20 X = -5899423
83
Y = 11119358
51 feet Y = 3323425
89 meter
Z = 837426
11 Z = 226682
25
XDOT = -7146
767531 XDOT = -2160
263475
YDOT = -13840
625876 feet/sec YDOT = -4242
880791 meter/sec
ZDOT = 19764
473231 ZDOT = 6013
673429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21937753
67 X = 6686627
32
Y = -3503918
26 feet Y = -1067994
29 meter
Z = 719912
61 Z = 219429
36
XDOT = 1579
925004 XDOT = 481
561141
YDOT = 13923
456097 feet/sec YDOT = 4243
869418 meter/sec
ZDOT = 19721
450294 ZDOT = 6011
098050
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 12091
98080232
00016717 00000-0 10270-3 0 9136
2 25544 51
6409 148
9722 0013654 230
7498 129
2447 15
59146912 5986
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
98080232 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 148
9722 deg
Eccentricity:
0013654
Arg of perigee: 230
7498 deg
Mean anomaly: 129
2447 deg
Mean motion: 15
59146912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 598
Checksum: 326
Coasting Arc #15 (Orbit 612)
---------------------------------------
Vector Time (GMT): 2012/092/22:00:39
757
Vector Time (MET): N/A
Weight (LBS) : 886297
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5772104
36 A = 6769900
03 meter
Y = -992416
91 meter E =
0010374
Z = -3381485
33 I = 51
85091
XDOT = -1724
433590 Wp = 218
36451
YDOT = 5855
661011 meter/sec RA = 143
27536 deg
ZDOT = -4662
423285 TA = 1
11576
MA = 1
11345
Ha = 214
062 n
mi
Hp = 207
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18937350
26 X = 5799199
17
Y = -3255960
99 feet Y = -927718
46 meter
Z = -11094111
96 Z = -3353378
97
XDOT = -5657
590517 XDOT = -1767
135736
YDOT = 19211
486258 feet/sec YDOT = 5836
138176 meter/sec
ZDOT = -15296
664322 ZDOT = -4670
904672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18973705
60 X = -5783185
47
Y = -3431082
56 feet Y = -1045793
96 meter
Z = -10978615
82 Z = -3346282
10
XDOT = 11541
798822 XDOT = 3517
940281
YDOT = -14770
689373 feet/sec YDOT = -4502
106121 meter/sec
ZDOT = -15331
852803 ZDOT = -4673
148734
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 12092
94221050
00016717 00000-0 10270-3 0 9149
2 25544 51
6418 144
1431 0013701 234
5629 125
4247 15
59179607 6133
Satellite: ISS
Catalog Number: 25544
Epoch time: 12092
94221050 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 144
1431 deg
Eccentricity:
0013701
Arg of perigee: 234
5629 deg
Mean anomaly: 125
4247 deg
Mean motion: 15
59179607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 613
Checksum: 286
Coasting Arc #16 (Orbit 628)
---------------------------------------
Vector Time (GMT): 2012/093/22:00:39
757
Vector Time (MET): N/A
Weight (LBS) : 886297
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3908556
96 A = 6763288
05 meter
Y = -1955005
28 meter E =
0012564
Z = 5170516
51 I = 51
85286
XDOT = 4808
217487 Wp = 218
58866
YDOT = -5800
343243 meter/sec RA = 138
25374 deg
ZDOT = 1433
828726 TA = 217
61487
MA = 217
70280
Ha = 213
667 n
mi
Hp = 208
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12823349
61 X = -3911522
29
Y = -6414059
31 feet Y = -1998729
23 meter
Z = 16963636
86 Z = 5151522
01
XDOT = 15774
991755 XDOT = 4865
755556
YDOT = -19029
997516 feet/sec YDOT = -5746
252922 meter/sec
ZDOT = 4704
162488 ZDOT = 1457
327066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10136177
05 X = 3089506
77
Y = 10270015
49 feet Y = 3130300
72 meter
Z = 16885737
30 Z = 5146772
73
XDOT = -20332
183683 XDOT = -6197
249587
YDOT = 12131
687380 feet/sec YDOT = 3697
738313 meter/sec
ZDOT = 4801
033992 ZDOT = 1463
355161
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 12093
96769466
00016717 00000-0 10270-3 0 9151
2 25544 51
6416 138
9915 0013622 238
2928 121
6899 15
59218783 6291
Satellite: ISS
Catalog Number: 25544
Epoch time: 12093
96769466 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 138
9915 deg
Eccentricity:
0013622
Arg of perigee: 238
2928 deg
Mean anomaly: 121
6899 deg
Mean motion: 15
59218783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 629
Checksum: 356
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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