[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 3rd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 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 1266)
---------------------------------------
Vector Time (GMT): 2011/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4904818
64 A = 6761348
45 meter
Y = 674070
50 meter E =
0018543
Z = -4617284
90 I = 51
84646
XDOT = -3647
402841 Wp = 107
34629
YDOT = 6037
407403 meter/sec RA = 140
71453 deg
ZDOT = -3008
462067 TA = 132
80414
MA = 132
64810
Ha = 214
801 n
mi
Hp = 200
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16091924
68 X = 4919346
32
Y = 2211517
39 feet Y = 729000
05 meter
Z = -15148572
50 Z = -4593422
20
XDOT = -11966
544753 XDOT = -3700
028749
YDOT = 19807
767071 feet/sec YDOT = 5996
325433 meter/sec
ZDOT = -9870
282371 ZDOT = -3026
309337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14250531
85 X = -4343562
11
Y = -7980998
42 feet Y = -2432608
32 meter
Z = -15051448
57 Z = -4587681
52
XDOT = 17748
826287 XDOT = 5409
842252
YDOT = -13035
057336 feet/sec YDOT = -3973
085476 meter/sec
ZDOT = -9943
136985 ZDOT = -3030
668153
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 11243
52144655
00016717 00000-0 10270-3 0 9000
2 25544 51
6404 141
5867 0012100 137
6004 222
6089 15
60687793 12676
Satellite: ISS
Catalog Number: 25544
Epoch time: 11243
52144655 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 141
5867 deg
Eccentricity:
0012100
Arg of perigee: 137
6004 deg
Mean anomaly: 222
6089 deg
Mean motion: 15
60687793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1267
Checksum: 290
Coasting Arc #2 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2011/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1837573
86 A = 6758667
31 meter
Y = -3903977
64 meter E =
0012890
Z = 5191572
85 I = 51
86028
XDOT = 6073
510231 Wp = 123
71121
YDOT = -4540
750868 meter/sec RA = 135
66307 deg
ZDOT = -1269
574343 TA = 338
38049
MA = 338
43486
Ha = 214
648 n
mi
Hp = 200
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6028785
63 X = -1819001
90
Y = -12808325
61 feet Y = -3924422
36 meter
Z = 17032719
34 Z = 5182691
29
XDOT = 19926
214667 XDOT = 6130
001742
YDOT = -14897
476600 feet/sec YDOT = -4472
517380 meter/sec
ZDOT = -4165
270154 ZDOT = -1239
931818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1261154
31 X = 384399
83
Y = 14143369
14 feet Y = 4310898
91 meter
Z = 16996693
45 Z = 5180592
16
XDOT = -22871
733879 XDOT = -6971
304486
YDOT = 6881
085480 feet/sec YDOT = 2097
354854 meter/sec
ZDOT = -4044
431916 ZDOT = -1232
742848
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 11244
54595245
00016717 00000-0 10270-3 0 9019
2 25544 51
6398 136
4285 0011966 141
9986 218
2017 15
60735168 12831
Satellite: ISS
Catalog Number: 25544
Epoch time: 11244
54595245 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 136
4285 deg
Eccentricity:
0011966
Arg of perigee: 141
9986 deg
Mean anomaly: 218
2017 deg
Mean motion: 15
60735168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 324
Coasting Arc #3 (Orbit 1297)
---------------------------------------
Vector Time (GMT): 2011/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1735669
37 A = 6766083
95 meter
Y = 5764643
51 meter E =
0014175
Z = -3108210
25 I = 51
90611
XDOT = -5824
794535 Wp = 128
20326
YDOT = 886
200912 meter/sec RA = 130
63097 deg
ZDOT = 4902
835131 TA = 196
14075
MA = 196
18595
Ha = 214
512 n
mi
Hp = 201
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5694453
31 X = -1784902
64
Y = 18912872
40 feet Y = 5744958
79 meter
Z = -10197540
19 Z = -3116761
93
XDOT = -19110
218291 XDOT = -5858
088346
YDOT = 2907
483307 feet/sec YDOT = 820
878536 meter/sec
ZDOT = 16085
417097 ZDOT = 4874
457418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11623039
16 X = 3542702
34
Y = -15947191
73 feet Y = -4860704
04 meter
Z = -10232565
84 Z = -3118886
07
XDOT = 17912
988059 XDOT = 5459
878760
YDOT = 2822
532667 feet/sec YDOT = 860
307957 meter/sec
ZDOT = 15969
843273 ZDOT = 4867
608229
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 11245
50641595
00016717 00000-0 10270-3 0 9027
2 25544 51
6399 131
5922 0011953 145
3364 214
8573 15
60719711 12981
Satellite: ISS
Catalog Number: 25544
Epoch time: 11245
50641595 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 131
5922 deg
Eccentricity:
0011953
Arg of perigee: 145
3364 deg
Mean anomaly: 214
8573 deg
Mean motion: 15
60719711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1298
Checksum: 312
Coasting Arc #4 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2011/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4317706
72 A = 6770156
24 meter
Y = -5160037
74 meter E =
0022772
Z = -640774
72 I = 51
93829
XDOT = 3290
855634 Wp = 145
17639
YDOT = 3484
580843 meter/sec RA = 125
64452 deg
ZDOT = -6008
726717 TA = 41
73965
MA = 41
56615
Ha = 214
541 n
mi
Hp = 201
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14165704
47 X = 4378199
13
Y = -16929257
68 feet Y = -5111416
29 meter
Z = -2102279
28 Z = -619652
32
XDOT = 10796
770453 XDOT = 3280
835019
YDOT = 11432
351846 feet/sec YDOT = 3521
325054 meter/sec
ZDOT = -19713
670333 ZDOT = -5992
764192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18820209
08 X = -5736399
73
Y = 11550830
86 feet Y = 3520693
25 meter
Z = -2016076
31 Z = -614500
06
XDOT = -5878
032543 XDOT = -1791
624319
YDOT = -12933
530054 feet/sec YDOT = -3942
139960 meter/sec
ZDOT = -19648
803137 ZDOT = -5988
955196
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 11246
53089636
00016717 00000-0 10270-3 0 9034
2 25544 51
6400 126
4335 0012071 150
0022 210
1828 15
60693762 13149
Satellite: ISS
Catalog Number: 25544
Epoch time: 11246
53089636 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 126
4335 deg
Eccentricity:
0012071
Arg of perigee: 150
0022 deg
Mean anomaly: 210
1828 deg
Mean motion: 15
60693762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 267
Coasting Arc #5 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2011/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4967967
80 A = 6763402
58 meter
Y = 2219140
39 meter E =
0020487
Z = 4012845
39 I = 51
93272
XDOT = 286
464890 Wp = 128
15762
YDOT = -6572
113965 meter/sec RA = 120
64814 deg
ZDOT = 3963
056393 TA = 280
77299
MA = 281
00355
Ha = 214
357 n
mi
Hp = 201
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16299106
95 X = -5011907
00
Y = 7280644
33 feet Y = 2163339
89 meter
Z = 13165503
24 Z = 3988604
39
XDOT = 939
845438 XDOT = 340
682554
YDOT = -21562
053690 feet/sec YDOT = -6568
607363 meter/sec
ZDOT = 13002
153520 ZDOT = 3964
579774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17810664
10 X = 5428690
42
Y = -2010164
22 feet Y = -612698
05 meter
Z = 13066699
22 Z = 3982729
92
XDOT = -7462
216547 XDOT = -2274
483604
YDOT = 19001
938115 feet/sec YDOT = 5791
790737 meter/sec
ZDOT = 13008
614840 ZDOT = 3965
025803
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 11247
55536167
00016717 00000-0 10270-3 0 9044
2 25544 51
6399 121
2746 0011822 152
8904 207
2871 15
60738941 13309
Satellite: ISS
Catalog Number: 25544
Epoch time: 11247
55536167 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 121
2746 deg
Eccentricity:
0011822
Arg of perigee: 152
8904 deg
Mean anomaly: 207
2871 deg
Mean motion: 15
60738941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 307
Coasting Arc #6 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2011/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3675013
94 A = 6758028
12 meter
Y = 1988599
87 meter E =
0022417
Z = -5328333
03 I = 51
92953
XDOT = -3435
686795 Wp = 119
98717
YDOT = 6849
410512 meter/sec RA = 115
60595 deg
ZDOT = 176
294786 TA = 151
74795
MA = 151
62618
Ha = 214
079 n
mi
Hp = 201
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12057132
35 X = 3678387
73
Y = 6524277
79 feet Y = 2029714
96 meter
Z = -17481407
59 Z = -5310471
80
XDOT = -11271
938304 XDOT = -3512
879294
YDOT = 22471
819265 feet/sec YDOT = 6810
558957 meter/sec
ZDOT = 578
394967 ZDOT = 159
416846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9801253
44 X = -2987422
05
Y = -9716547
77 feet Y = -2961603
76 meter
Z = -17408744
44 Z = -5306185
31
XDOT = 16498
688021 XDOT = 5028
800109
YDOT = -17616
281526 feet/sec YDOT = -5369
442609 meter/sec
ZDOT = 509
378318 ZDOT = 155
258511
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 11248
51578388
00016717 00000-0 10270-3 0 9053
2 25544 51
6396 116
4376 0011730 157
3020 202
8657 15
60794763 13451
Satellite: ISS
Catalog Number: 25544
Epoch time: 11248
51578388 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 116
4376 deg
Eccentricity:
0011730
Arg of perigee: 157
3020 deg
Mean anomaly: 202
8657 deg
Mean motion: 15
60794763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 318
Coasting Arc #7 (Orbit 1360)
---------------------------------------
Vector Time (GMT): 2011/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1140181
78 A = 6763671
51 meter
Y = -5453888
13 meter E =
0017782
Z = 3813572
58 I = 51
96161
XDOT = 5028
994837 Wp = 122
16659
YDOT = -4005
335070 meter/sec RA = 110
56863 deg
ZDOT = -4219
532757 TA = 12
01496
MA = 11
97260
Ha = 213
894 n
mi
Hp = 201
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3740753
87 X = -1097636
00
Y = -17893333
76 feet Y = -5466400
41 meter
Z = 12511721
07 Z = 3808137
06
XDOT = 16499
326894 XDOT = 5093
906968
YDOT = -13140
863090 feet/sec YDOT = -3948
734879 meter/sec
ZDOT = -13843
611409 ZDOT = -4194
944509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1122831
91 X = -342239
17
Y = 18260660
84 feet Y = 5565849
42 meter
Z = 12489808
28 Z = 3806893
56
XDOT = -18168
023940 XDOT = -5537
613697
YDOT = 8294
223521 feet/sec YDOT = 2528
079329 meter/sec
ZDOT = -13743
294721 ZDOT = -4188
956231
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 11249
54022123
00016717 00000-0 10270-3 0 9069
2 25544 51
6401 111
2794 0011564 161
3233 198
8349 15
60840390 13619
Satellite: ISS
Catalog Number: 25544
Epoch time: 11249
54022123 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 111
2794 deg
Eccentricity:
0011564
Arg of perigee: 161
3233 deg
Mean anomaly: 198
8349 deg
Mean motion: 15
60840390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1361
Checksum: 282
Coasting Arc #8 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2011/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1581684
64 A = 6769869
11 meter
Y = 6577587
72 meter E =
0011145
Z = -310599
79 I = 51
99090
XDOT = -4660
234062 Wp = 104
81603
YDOT = -844
068262 meter/sec RA = 105
57731 deg
ZDOT = 6033
875812 TA = 251
84694
MA = 251
96833
Ha = 213
776 n
mi
Hp = 201
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5189254
07 X = -1653610
14
Y = 21580012
19 feet Y = 6559498
19 meter
Z = -1019028
17 Z = -318458
36
XDOT = -15289
481832 XDOT = -4679
760172
YDOT = -2769
252827 feet/sec YDOT = -896
290869 meter/sec
ZDOT = 19796
180485 ZDOT = 6011
189356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10445887
72 X = 3183906
58
Y = -19581671
61 feet Y = -5968493
51 meter
Z = -1051317
79 Z = -320441
66
XDOT = 12788
390402 XDOT = 3897
901395
YDOT = 5794
372500 feet/sec YDOT = 1766
124738 meter/sec
ZDOT = 19703
804767 ZDOT = 6005
719693
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 11250
50061969
00016717 00000-0 10270-3 0 9079
2 25544 51
6391 106
4425 0011647 165
2114 194
9385 15
60828267 13769
Satellite: ISS
Catalog Number: 25544
Epoch time: 11250
50061969 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 106
4425 deg
Eccentricity:
0011647
Arg of perigee: 165
2114 deg
Mean anomaly: 194
9385 deg
Mean motion: 15
60828267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 312
Coasting Arc #9 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2011/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3569575
15 A = 6765030
59 meter
Y = -4628813
74 meter E =
0013442
Z = -3399577
42 I = 51
98081
XDOT = 2683
829824 Wp = 148
91789
YDOT = 5479
913081 meter/sec RA = 100
59241 deg
ZDOT = -4662
705851 TA = 70
73691
MA = 70
59155
Ha = 213
718 n
mi
Hp = 202
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11711204
56 X = 3637584
39
Y = -15186396
79 feet Y = -4588516
46 meter
Z = -11153469
24 Z = -3382071
33
XDOT = 8805
215957 XDOT = 2645
003081
YDOT = 17978
717456 feet/sec YDOT = 5509
708003 meter/sec
ZDOT = -15297
591375 ZDOT = -4649
762593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15016297
68 X = -4576967
53
Y = 11994993
93 feet Y = 3656074
15 meter
Z = -11081956
53 Z = -3377780
35
XDOT = -3550
210042 XDOT = -1082
104021
YDOT = -18470
003941 feet/sec YDOT = -5629
657201 meter/sec
ZDOT = -15245
100159 ZDOT = -4646
706528
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 11251
52502992
00016717 00000-0 10270-3 0 9089
2 25544 51
6381 101
2833 0011611 169
5263 190
6137 15
60830412 13928
Satellite: ISS
Catalog Number: 25544
Epoch time: 11251
52502992 = yrday
fracday
Element set: 908
Inclination: 51
6381 deg
RA of node: 101
2833 deg
Eccentricity:
0011611
Arg of perigee: 169
5263 deg
Mean anomaly: 190
6137 deg
Mean motion: 15
60830412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 281
Coasting Arc #10 (Orbit 1407)
---------------------------------------
Vector Time (GMT): 2011/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4194254
18 A = 6758116
34 meter
Y = 522767
84 meter E =
0013810
Z = 5271088
41 I = 51
96204
XDOT = 97
660672 Wp = 161
82161
YDOT = -7637
116228 meter/sec RA = 95
56119 deg
ZDOT = 821
755625 TA = 280
29438
MA = 280
45005
Ha = 213
644 n
mi
Hp = 202
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13760676
44 X = -4225393
70
Y = 1715117
60 feet Y = 475691
37 meter
Z = 17293597
14 Z = 5250637
40
XDOT = 320
409029 XDOT = 179
061269
YDOT = -25056
155603 feet/sec YDOT = -7635
568936 meter/sec
ZDOT = 2696
048637 ZDOT = 822
428277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13905046
61 X = 4238258
21
Y = 1350170
19 feet Y = 411531
87 meter
Z = 17210260
48 Z = 5245687
39
XDOT = -5664
697624 XDOT = -1726
599836
YDOT = 23372
152702 feet/sec YDOT = 7123
832144 meter/sec
ZDOT = 2699
121345 ZDOT = 822
692186
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 11252
54942644
00016717 00000-0 10270-3 0 9095
2 25544 51
6380 96
1238 0011589 172
8826 187
2496 15
60835341 14088
Satellite: ISS
Catalog Number: 25544
Epoch time: 11252
54942644 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 96
1238 deg
Eccentricity:
0011589
Arg of perigee: 172
8826 deg
Mean anomaly: 187
2496 deg
Mean motion: 15
60835341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1408
Checksum: 327
Coasting Arc #11 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2011/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3374489
26 A = 6761720
47 meter
Y = 3932416
67 meter E =
0017091
Z = -4360374
47 I = 51
97512
XDOT = -2774
365323 Wp = 148
96005
YDOT = 6243
957565 meter/sec RA = 90
51572 deg
ZDOT = 3475
835517 TA = 156
22044
MA = 156
14138
Ha = 213
330 n
mi
Hp = 202
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11071158
99 X = 3351447
00
Y = 12901629
51 feet Y = 3970023
07 meter
Z = -14305690
53 Z = -4344037
75
XDOT = -9102
248435 XDOT = -2860
865011
YDOT = 20485
425083 feet/sec YDOT = 6212
449565 meter/sec
ZDOT = 11403
659832 ZDOT = 3462
147217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8331149
62 X = -2539334
40
Y = -14883191
35 feet Y = -4536396
72 meter
Z = -14239309
96 Z = -4340141
68
XDOT = 12022
448464 XDOT = 3664
442292
YDOT = -17612
403817 feet/sec YDOT = -5368
260683 meter/sec
ZDOT = 11347
618877 ZDOT = 3458
754234
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 11253
50978277
00016717 00000-0 10270-3 0 9105
2 25544 51
6366 91
2853 0011598 176
8740 183
2490 15
60889254 14239
Satellite: ISS
Catalog Number: 25544
Epoch time: 11253
50978277 = yrday
fracday
Element set: 910
Inclination: 51
6366 deg
RA of node: 91
2853 deg
Eccentricity:
0011598
Arg of perigee: 176
8740 deg
Mean anomaly: 183
2490 deg
Mean motion: 15
60889254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 328
Coasting Arc #12 (Orbit 1438)
---------------------------------------
Vector Time (GMT): 2011/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1369304
21 A = 6769099
37 meter
Y = -6523599
54 meter E =
0021966
Z = 1094610
14 I = 51
99985
XDOT = 4494
165039 Wp = 149
13894
YDOT = -1943
866341 meter/sec RA = 85
51699 deg
ZDOT = -5929
112422 TA = 18
99429
MA = 18
91249
Ha = 213
064 n
mi
Hp = 202
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4492467
89 X = -1301571
63
Y = -21402885
62 feet Y = -6538533
11 meter
Z = 3591240
61 Z = 1088123
30
XDOT = 14744
635955 XDOT = 4544
369943
YDOT = -6377
514241 feet/sec YDOT = -1893
329715 meter/sec
ZDOT = -19452
468576 ZDOT = -5907
157885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 488492
36 X = 148892
47
Y = 21868108
59 feet Y = 6665399
50 meter
Z = 3565107
51 Z = 1086644
77
XDOT = -14188
533007 XDOT = -4324
664860
YDOT = 3491
882294 feet/sec YDOT = 1064
325723 meter/sec
ZDOT = -19362
939772 ZDOT = -5901
824043
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 11254
53414851
00016717 00000-0 10270-3 0 9113
2 25544 51
6369 86
1262 0011368 181
1259 178
9874 15
60942334 14391
Satellite: ISS
Catalog Number: 25544
Epoch time: 11254
53414851 = yrday
fracday
Element set: 911
Inclination: 51
6369 deg
RA of node: 86
1262 deg
Eccentricity:
0011368
Arg of perigee: 181
1259 deg
Mean anomaly: 178
9874 deg
Mean motion: 15
60942334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 318
Coasting Arc #13 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2011/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1158118
76 A = 6766385
75 meter
Y = 6078398
95 meter E =
0015245
Z = 2740115
88 I = 51
98614
XDOT = -4645
606855 Wp = 126
12200
YDOT = -3234
077284 meter/sec RA = 80
53534 deg
ZDOT = 5181
894715 TA = 264
80389
MA = 264
97788
Ha = 212
988 n
mi
Hp = 202
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3799602
23 X = -1239313
42
Y = 19942253
77 feet Y = 6064994
47 meter
Z = 8989881
48 Z = 2734291
90
XDOT = -15241
492306 XDOT = -4634
270020
YDOT = -10610
489776 feet/sec YDOT = -3285
963358 meter/sec
ZDOT = 17000
966914 ZDOT = 5159
354413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7140302
69 X = 2176364
26
Y = -19015193
75 feet Y = -5795831
05 meter
Z = 8965875
06 Z = 2732798
72
XDOT = 11962
751308 XDOT = 3646
246599
YDOT = 12509
629813 feet/sec YDOT = 3812
935167 meter/sec
ZDOT = 16909
289287 ZDOT = 5153
951375
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 11255
55849988
00016717 00000-0 10270-3 0 9120
2 25544 51
6356 80
9653 0011640 185
0520 175
0521 15
60949983 14552
Satellite: ISS
Catalog Number: 25544
Epoch time: 11255
55849988 = yrday
fracday
Element set: 912
Inclination: 51
6356 deg
RA of node: 80
9653 deg
Eccentricity:
0011640
Arg of perigee: 185
0520 deg
Mean anomaly: 175
0521 deg
Mean motion: 15
60949983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 326
Coasting Arc #14 (Orbit 1469)
---------------------------------------
Vector Time (GMT): 2011/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3429071
11 A = 6758404
58 meter
Y = -2773694
92 meter E =
0014546
Z = -5128978
36 I = 51
95315
XDOT = 3089
645716 Wp = 126
01281
YDOT = 6829
324923 meter/sec RA = 75
51159 deg
ZDOT = -1639
145519 TA = 128
31259
MA = 128
18171
Ha = 212
910 n
mi
Hp = 203
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11250233
29 X = 3484747
82
Y = -9100048
96 feet Y = -2735038
21 meter
Z = -16827356
82 Z = -5112184
44
XDOT = 10136
632925 XDOT = 3021
011885
YDOT = 22405
921662 feet/sec YDOT = 6863
491300 meter/sec
ZDOT = -5377
774013 ZDOT = -1624
303527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12592206
27 X = -3838104
47
Y = 7288155
15 feet Y = 2221429
69 meter
Z = -16758810
02 Z = -5108085
30
XDOT = -6148
338068 XDOT = -1874
013443
YDOT = -22762
981400 feet/sec YDOT = -6938
156731 meter/sec
ZDOT = -5317
634244 ZDOT = -1620
814918
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 11256
51881639
00016717 00000-0 10270-3 0 9137
2 25544 51
6354 76
1275 0011551 187
6342 172
4640 15
60956811 14706
Satellite: ISS
Catalog Number: 25544
Epoch time: 11256
51881639 = yrday
fracday
Element set: 913
Inclination: 51
6354 deg
RA of node: 76
1275 deg
Eccentricity:
0011551
Arg of perigee: 187
6342 deg
Mean anomaly: 172
4640 deg
Mean motion: 15
60956811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1470
Checksum: 307
Coasting Arc #15 (Orbit 1485)
---------------------------------------
Vector Time (GMT): 2011/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4522708
77 A = 6760085
62 meter
Y = -1682727
22 meter E =
0009007
Z = 4726751
78 I = 51
95017
XDOT = -233
794299 Wp = 148
89646
YDOT = -7161
087495 meter/sec RA = 70
46265 deg
ZDOT = -2778
232494 TA = 328
40546
MA = 328
45950
Ha = 212
825 n
mi
Hp = 203
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14838283
36 X = -4526517
77
Y = -5520758
60 feet Y = -1733323
72 meter
Z = 15507715
83 Z = 4704771
38
XDOT = -767
041665 XDOT = -140
204076
YDOT = -23494
381545 feet/sec YDOT = -7163
178926 meter/sec
ZDOT = -9114
936005 ZDOT = -2779
140184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14060743
44 X = 4285714
60
Y = 7464285
49 feet Y = 2275114
22 meter
Z = 15418255
90 Z = 4699484
40
XDOT = -1887
060921 XDOT = -575
176169
YDOT = 22354
190014 feet/sec YDOT = 6813
557116 meter/sec
ZDOT = -9118
283185 ZDOT = -2779
252715
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 11257
54313744
00016717 00000-0 10270-3 0 9149
2 25544 51
6355 70
9672 0011560 191
9951 168
0931 15
60955595 14863
Satellite: ISS
Catalog Number: 25544
Epoch time: 11257
54313744 = yrday
fracday
Element set: 914
Inclination: 51
6355 deg
RA of node: 70
9672 deg
Eccentricity:
0011560
Arg of perigee: 191
9951 deg
Mean anomaly: 168
0931 deg
Mean motion: 15
60955595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 326
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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