[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 9th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24218 8 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
322/05:01:03
599 -0
6 6
4 6
4
N/A 6
3 0
0 219
1
000/00:02:03
198 -1
3 -0
0 201
1
Coasting Arc #1 (Orbit 2328)
---------------------------------------
Vector Time (GMT): 2011/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6491303
88 A = 6772525
53 meter
Y = -1585046
64 meter E =
0020203
Z = -1162769
40 I = 51
78081
XDOT = 158
435859 Wp = 56
11409
YDOT = 4913
210201 meter/sec RA = 158
40199 deg
ZDOT = -5875
271215 TA = 136
48995
MA = 136
33039
Ha = 219
479 n
mi
Hp = 199
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21296928
75 X = 6514194
37
Y = -5200284
25 feet Y = -1512328
95 meter
Z = -3814860
23 Z = -1131178
32
XDOT = 519
802686 XDOT = 132
025205
YDOT = 16119
456041 feet/sec YDOT = 4914
834042 meter/sec
ZDOT = -19275
824197 ZDOT = -5874
565851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11217425
32 X = -3419071
24
Y = 18861035
64 feet Y = 5748843
66 meter
Z = -3685918
15 Z = -1123467
85
XDOT = -10576
475370 XDOT = -3223
709693
YDOT = -10015
417217 feet/sec YDOT = -3052
699168 meter/sec
ZDOT = -19273
173757 ZDOT = -5874
463361
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 11311
52993827
00016717 00000-0 10270-3 0 9009
2 25544 51
6387 159
2884 0021722 30
1525 330
0876 15
59735095 23291
Satellite: ISS
Catalog Number: 25544
Epoch time: 11311
52993827 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 159
2884 deg
Eccentricity:
0021722
Arg of perigee: 30
1525 deg
Mean anomaly: 330
0876 deg
Mean motion: 15
59735095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2329
Checksum: 314
Coasting Arc #2 (Orbit 2344)
---------------------------------------
Vector Time (GMT): 2011/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5226800
30 A = 6765683
41 meter
Y = -1028766
96 meter E =
0027177
Z = 4141103
25 I = 51
78512
XDOT = 4045
394934 Wp = 55
13717
YDOT = -5349
954300 meter/sec RA = 153
39666 deg
ZDOT = 3774
683849 TA = 356
22794
MA = 356
24838
Ha = 219
629 n
mi
Hp = 199
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17148294
96 X = -5235025
17
Y = -3375219
68 feet Y = -1087262
13 meter
Z = 13586296
75 Z = 4115690
89
XDOT = 13272
293089 XDOT = 4086
581340
YDOT = -17552
343504 feet/sec YDOT = -5304
485837 meter/sec
ZDOT = 12384
133364 ZDOT = 3794
437021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14301843
34 X = 4359201
85
Y = -10184221
85 feet Y = -3104150
82 meter
Z = 13482673
67 Z = 4109518
94
XDOT = 2917
921917 XDOT = 889
382600
YDOT = 20609
575523 feet/sec YDOT = 6281
798619 meter/sec
ZDOT = 12464
972507 ZDOT = 3799
323620
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 11312
55504330
00016717 00000-0 10270-3 0 9011
2 25544 51
6377 154
1328 0021807 33
6778 326
5758 15
59784278 23453
Satellite: ISS
Catalog Number: 25544
Epoch time: 11312
55504330 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 154
1328 deg
Eccentricity:
0021807
Arg of perigee: 33
6778 deg
Mean anomaly: 326
5758 deg
Mean motion: 15
59784278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2345
Checksum: 318
Coasting Arc #3 (Orbit 2359)
---------------------------------------
Vector Time (GMT): 2011/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2171692
14 A = 6760739
72 meter
Y = 3587052
31 meter E =
0032975
Z = -5327433
82 I = 51
79454
XDOT = -6534
665314 Wp = 58
79136
YDOT = 3990
539291 meter/sec RA = 148
35364 deg
ZDOT = 39
917787 TA = 211
48980
MA = 211
68760
Ha = 219
452 n
mi
Hp = 199
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7124974
20 X = 2157299
98
Y = 11768544
32 feet Y = 3611256
99 meter
Z = -17478457
42 Z = -5316918
45
XDOT = -21439
190663 XDOT = -6578
996553
YDOT = 13092
320510 feet/sec YDOT = 3917
216788 meter/sec
ZDOT = 130
963869 ZDOT = 8
063854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13561751
94 X = -4133621
99
Y = -2614289
42 feet Y = -796835
41 meter
Z = -17435731
74 Z = -5314411
04
XDOT = 4631
981039 XDOT = 1411
827821
YDOT = -23664
808791 feet/sec YDOT = -7213
033719 meter/sec
ZDOT =
806043 ZDOT =
245682
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 11313
51604588
00016717 00000-0 10270-3 0 9025
2 25544 51
6363 149
2995 0021710 37
4079 322
8583 15
59856984 23608
Satellite: ISS
Catalog Number: 25544
Epoch time: 11313
51604588 = yrday
fracday
Element set: 902
Inclination: 51
6363 deg
RA of node: 149
2995 deg
Eccentricity:
0021710
Arg of perigee: 37
4079 deg
Mean anomaly: 322
8583 deg
Mean motion: 15
59856984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2360
Checksum: 327
Coasting Arc #4 (Orbit 2375)
---------------------------------------
Vector Time (GMT): 2011/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1583385
00 A = 6765443
12 meter
Y = -5164328
60 meter E =
0030797
Z = 4065843
79 I = 51
83668
XDOT = 6543
197348 Wp = 52
79424
YDOT = -1075
951755 meter/sec RA = 143
31222 deg
ZDOT = -3876
452881 TA = 77
30993
MA = 76
96582
Ha = 219
343 n
mi
Hp = 198
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5194832
69 X = 1621264
21
Y = -16943335
29 feet Y = -5146410
47 meter
Z = 13339382
52 Z = 4073628
03
XDOT = 21467
182899 XDOT = 6573
574141
YDOT = -3530
025443 feet/sec YDOT = -1002
611819 meter/sec
ZDOT = -12718
021263 ZDOT = -3844
591421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9302288
59 X = 2835337
56
Y = 15055727
01 feet Y = 4588985
59 meter
Z = 13371407
35 Z = 4075604
96
XDOT = -10530
834398 XDOT = -3209
798324
YDOT = 17797
739478 feet/sec YDOT = 5424
750993 meter/sec
ZDOT = -12587
962077 ZDOT = -3836
810841
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 11314
54108066
00016717 00000-0 10270-3 0 9030
2 25544 51
6366 144
1439 0021604 40
7572 319
5195 15
59923157 23761
Satellite: ISS
Catalog Number: 25544
Epoch time: 11314
54108066 = yrday
fracday
Element set: 903
Inclination: 51
6366 deg
RA of node: 144
1439 deg
Eccentricity:
0021604
Arg of perigee: 40
7572 deg
Mean anomaly: 319
5195 deg
Mean motion: 15
59923157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2376
Checksum: 305
Coasting Arc #5 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2011/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4423758
53 A = 6771995
74 meter
Y = 5008643
71 meter E =
0031237
Z = -1017412
82 I = 51
88153
XDOT = -4182
609541 Wp = 43
01669
YDOT = -2514
132890 meter/sec RA = 138
31258 deg
ZDOT = 5938
190702 TA = 305
95371
MA = 306
24307
Ha = 219
370 n
mi
Hp = 198
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14513643
46 X = -4474494
85
Y = 16432558
11 feet Y = 4958890
88 meter
Z = -3337968
58 Z = -1039027
07
XDOT = -13722
472248 XDOT = -4183
032528
YDOT = -8248
467486 feet/sec YDOT = -2560
907945 meter/sec
ZDOT = 19482
252959 ZDOT = 5917
869967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3079785
62 X = -938718
66
Y = -21693116
81 feet Y = -6612062
00 meter
Z = -3426434
07 Z = -1044377
11
XDOT = 13678
486127 XDOT = 4169
202571
YDOT = -4941
027346 feet/sec YDOT = -1506
025135 meter/sec
ZDOT = 19399
462267 ZDOT = 5912
956099
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 11315
50202028
00016717 00000-0 10270-3 0 9041
2 25544 51
6356 139
3103 0021624 44
6174 315
6717 15
59949922 23919
Satellite: ISS
Catalog Number: 25544
Epoch time: 11315
50202028 = yrday
fracday
Element set: 904
Inclination: 51
6356 deg
RA of node: 139
3103 deg
Eccentricity:
0021624
Arg of perigee: 44
6174 deg
Mean anomaly: 315
6717 deg
Mean motion: 15
59949922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 294
Coasting Arc #6 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2011/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5547546
40 A = 6769410
69 meter
Y = -2913588
78 meter E =
0023187
Z = -2596247
23 I = 51
89562
XDOT = 454
982923 Wp = 61
31035
YDOT = 5539
275294 meter/sec RA = 133
33019 deg
ZDOT = -5268
929817 TA = 147
79670
MA = 147
65489
Ha = 219
391 n
mi
Hp = 198
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18200611
54 X = 5592326
80
Y = -9559018
31 feet Y = -2851302
21 meter
Z = -8517871
49 Z = -2569188
00
XDOT = 1492
726124 XDOT = 418
603929
YDOT = 18173
475373 feet/sec YDOT = 5544
160039 meter/sec
ZDOT = -17286
515147 ZDOT = -5266
807559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4240960
90 X = -1292644
88
Y = 20162418
56 feet Y = 6145505
18 meter
Z = -8407279
85 Z = -2562538
90
XDOT = -13564
030086 XDOT = -4134
316370
YDOT = -10023
328817 feet/sec YDOT = -3055
110623 meter/sec
ZDOT = -17278
155523 ZDOT = -5266
381803
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 11316
52698661
00016717 00000-0 10270-3 0 9057
2 25544 51
6356 134
1543 0021774 48
3853 311
9164 15
60033683 24074
Satellite: ISS
Catalog Number: 25544
Epoch time: 11316
52698661 = yrday
fracday
Element set: 905
Inclination: 51
6356 deg
RA of node: 134
1543 deg
Eccentricity:
0021774
Arg of perigee: 48
3853 deg
Mean anomaly: 311
9164 deg
Mean motion: 15
60033683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 305
Coasting Arc #7 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2011/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4555660
19 A = 6761742
91 meter
Y = -496341
48 meter E =
0024544
Z = 4949423
78 I = 51
88987
XDOT = 3103
911009 Wp = 66
48665
YDOT = -6695
044906 meter/sec RA = 128
31268 deg
ZDOT = 2186
629167 TA = 2
35317
MA = 2
34164
Ha = 219
519 n
mi
Hp = 198
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14946391
71 X = -4573815
29
Y = -1628416
94 feet Y = -547387
47 meter
Z = 16238266
99 Z = 4927247
82
XDOT = 10183
435068 XDOT = 3167
923174
YDOT = -21965
370427 feet/sec YDOT = -6659
977288 meter/sec
ZDOT = 7173
980208 ZDOT = 2201
863357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10645808
16 X = 3244842
33
Y = -10753772
19 feet Y = -3277749
76 meter
Z = 16147781
08 Z = 4921843
67
XDOT = 10079
808092 XDOT = 3072
325506
YDOT = 20839
712749 feet/sec YDOT = 6351
944446 meter/sec
ZDOT = 7236
535937 ZDOT = 2205
696153
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 11317
55191788
00016717 00000-0 10270-3 0 9060
2 25544 51
6353 128
9978 0021660 52
1704 308
1408 15
60051897 24230
Satellite: ISS
Catalog Number: 25544
Epoch time: 11317
55191788 = yrday
fracday
Element set: 906
Inclination: 51
6353 deg
RA of node: 128
9978 deg
Eccentricity:
0021660
Arg of perigee: 52
1704 deg
Mean anomaly: 308
1408 deg
Mean motion: 15
60051897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 314
Coasting Arc #8 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2011/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2123992
41 A = 6761175
07 meter
Y = 3986141
35 meter E =
0031890
Z = -5054977
88 I = 51
90749
XDOT = -5247
885163 Wp = 74
03918
YDOT = 5229
848945 meter/sec RA = 123
26855 deg
ZDOT = 1937
640046 TA = 214
60995
MA = 214
81792
Ha = 219
338 n
mi
Hp = 197
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6968479
05 X = 2103817
29
Y = 13077891
57 feet Y = 4009780
64 meter
Z = -16584573
09 Z = -5044708
12
XDOT = -17217
471008 XDOT = -5315
389183
YDOT = 17158
297063 feet/sec YDOT = 5170
786321 meter/sec
ZDOT = 6357
086766 ZDOT = 1911
981765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14675639
64 X = -4473134
96
Y = -2365949
25 feet Y = -721141
33 meter
Z = -16542880
58 Z = -5042270
00
XDOT = -3259
462091 XDOT = -993
484045
YDOT = -23067
850425 feet/sec YDOT = -7031
080809 meter/sec
ZDOT = 6252
046705 ZDOT = 1905
623836
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 11318
51275701
00016717 00000-0 10270-3 0 9076
2 25544 51
6362 124
1641 0021669 56
1009 304
2204 15
60116197 24388
Satellite: ISS
Catalog Number: 25544
Epoch time: 11318
51275701 = yrday
fracday
Element set: 907
Inclination: 51
6362 deg
RA of node: 124
1641 deg
Eccentricity:
0021669
Arg of perigee: 56
1009 deg
Mean anomaly: 304
2204 deg
Mean motion: 15
60116197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 278
Coasting Arc #9 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2011/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 891662
21 A = 6768684
38 meter
Y = -6133239
78 meter E =
0032920
Z = 2705316
12 I = 51
94874
XDOT = 5442
291646 Wp = 75
59388
YDOT = -1529
252253 meter/sec RA = 118
24999 deg
ZDOT = -5200
073007 TA = 73
87360
MA = 73
51146
Ha = 219
243 n
mi
Hp = 197
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2925400
96 X = 947036
94
Y = -20122177
76 feet Y = -6122959
20 meter
Z = 8875709
04 Z = 2709782
03
XDOT = 17855
287552 XDOT = 5484
248887
YDOT = -5017
231800 feet/sec YDOT = -1468
158322 meter/sec
ZDOT = -17060
606979 ZDOT = -5173
532195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14450537
92 X = 4404523
96
Y = 14293759
81 feet Y = 4356737
99 meter
Z = 8894301
76 Z = 2710983
18
XDOT = -5625
475331 XDOT = -1714
644881
YDOT = 16359
259610 feet/sec YDOT = 4986
302329 meter/sec
ZDOT = -16952
163868 ZDOT = -5167
019547
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 11319
53761604
00016717 00000-0 10270-3 0 9082
2 25544 51
6359 119
0070 0021572 59
5386 300
7897 15
60173110 24546
Satellite: ISS
Catalog Number: 25544
Epoch time: 11319
53761604 = yrday
fracday
Element set: 908
Inclination: 51
6359 deg
RA of node: 119
0070 deg
Eccentricity:
0021572
Arg of perigee: 59
5386 deg
Mean anomaly: 300
7897 deg
Mean motion: 15
60173110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 302
Coasting Arc #10 (Orbit 2469)
---------------------------------------
Vector Time (GMT): 2011/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3250117
54 A = 6771337
51 meter
Y = 5860871
69 meter E =
0034982
Z = 856954
88 I = 51
97285
XDOT = -3795
648959 Wp = 59
98159
YDOT = -3002
514880 meter/sec RA = 113
27110 deg
ZDOT = 5975
452391 TA = 309
28449
MA = 309
59424
Ha = 219
217 n
mi
Hp = 197
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10663115
29 X = -3319576
38
Y = 19228581
66 feet Y = 5824138
48 meter
Z = 2811531
76 Z = 840997
20
XDOT = -12452
916531 XDOT = -3790
820090
YDOT = -9850
770605 feet/sec YDOT = -3044
933420 meter/sec
ZDOT = 19604
502594 ZDOT = 5957
024543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9424955
36 X = -2872726
39
Y = -19873968
93 feet Y = -6057585
73 meter
Z = 2746027
37 Z = 836989
14
XDOT = 13875
923605 XDOT = 4229
381515
YDOT = -3806
023577 feet/sec YDOT = -1160
075986 meter/sec
ZDOT = 19529
443244 ZDOT = 5952
574301
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 11320
56243925
00016717 00000-0 10270-3 0 9099
2 25544 51
6371 113
8513 0021645 63
6492 296
6883 15
60240184 24701
Satellite: ISS
Catalog Number: 25544
Epoch time: 11320
56243925 = yrday
fracday
Element set: 909
Inclination: 51
6371 deg
RA of node: 113
8513 deg
Eccentricity:
0021645
Arg of perigee: 63
6492 deg
Mean anomaly: 296
6883 deg
Mean motion: 15
60240184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2470
Checksum: 304
Coasting Arc #11 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2011/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4413095
33 A = 6764372
65 meter
Y = -3101837
97 meter E =
0029062
Z = -4112615
49 I = 51
96156
XDOT = 1014
948274 Wp = 68
01570
YDOT = 6536
859730 meter/sec RA = 108
27855 deg
ZDOT = -3852
334464 TA = 162
32147
MA = 162
22013
Ha = 219
184 n
mi
Hp = 197
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14478659
23 X = 4467431
22
Y = -10176633
76 feet Y = -3052184
10 meter
Z = -13492832
96 Z = -4091044
59
XDOT = 3329
882790 XDOT = 960
490488
YDOT = 21446
390190 feet/sec YDOT = 6547
905124 meter/sec
ZDOT = -12638
892599 ZDOT = -3847
535895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 111461
19 X = 33973
37
Y = 17763929
34 feet Y = 5414445
66 meter
Z = -13404565
64 Z = -4085711
61
XDOT = -18292
542801 XDOT = -5575
567046
YDOT = -9380
131719 feet/sec YDOT = -2859
064148 meter/sec
ZDOT = -12619
696644 ZDOT = -3846
483537
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 11321
52317686
00016717 00000-0 10270-3 0 9104
2 25544 51
6376 109
0170 0021725 66
8447 293
4995 15
60293532 24856
Satellite: ISS
Catalog Number: 25544
Epoch time: 11321
52317686 = yrday
fracday
Element set: 910
Inclination: 51
6376 deg
RA of node: 109
0170 deg
Eccentricity:
0021725
Arg of perigee: 66
8447 deg
Mean anomaly: 293
4995 deg
Mean motion: 15
60293532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 314
Coasting Arc #12 (Orbit 2495)
---------------------------------------
Vector Time (GMT): 2011/322/05:02:05
198
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4285912
14 A = 6763238
15 meter
Y = -124755
56 meter E =
0030628
Z = -5256949
30 I = 51
95578
XDOT = -1101
187584 Wp = 73
09710
YDOT = 7497
773584 meter/sec RA = 104
71186 deg
ZDOT = -1072
209093 TA = 186
63597
MA = 186
67663
Ha = 219
134 n
mi
Hp = 201
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14061391
52 X = 4312526
17
Y = -409303
02 feet Y = -76678
97 meter
Z = -17247208
99 Z = -5236063
51
XDOT = -3612
820156 XDOT = -1179
738683
YDOT = 24598
994697 feet/sec YDOT = 7485
020243 meter/sec
ZDOT = -3517
746369 ZDOT = -1077
749387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9716411
96 X = -2961562
37
Y = -10315834
55 feet Y = -3144266
37 meter
Z = -17161916
41 Z = -5230952
12
XDOT = 20020
695907 XDOT = 6102
308112
YDOT = -12947
422559 feet/sec YDOT = -3946
374396 meter/sec
ZDOT = -3540
830994 ZDOT = -1079
245287
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 11322
22770052
00016717 00000-0 10270-3 0 9113
2 25544 51
6406 105
4769 0016630 65
5803 294
7085 15
59128346 24969
Satellite: ISS
Catalog Number: 25544
Epoch time: 11322
22770052 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 105
4769 deg
Eccentricity:
0016630
Arg of perigee: 65
5803 deg
Mean anomaly: 294
7085 deg
Mean motion: 15
59128346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2496
Checksum: 306
Coasting Arc #13 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2011/323/05:02:05
198
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3161463
31 A = 6764978
60 meter
Y = -3602656
82 meter E =
0024155
Z = 4759066
30 I = 51
96900
XDOT = 3237
238629 Wp = 66
52881
YDOT = -6430
407162 meter/sec RA = 99
68223 deg
ZDOT = -2697
202587 TA = 50
02626
MA = 49
81439
Ha = 219
103 n
mi
Hp = 200
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10372254
96 X = -3144061
66
Y = -11819740
22 feet Y = -3637912
95 meter
Z = 15613734
58 Z = 4743750
00
XDOT = 10620
861644 XDOT = 3322
006780
YDOT = -21097
136359 feet/sec YDOT = -6393
732403 meter/sec
ZDOT = -8849
089852 ZDOT = -2681
270019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1611879
82 X = -491300
97
Y = 15704584
43 feet Y = 4786757
34 meter
Z = 15551415
06 Z = 4740071
31
XDOT = -21608
313541 XDOT = -6586
213967
YDOT = 6545
912731 feet/sec YDOT = 1995
194200 meter/sec
ZDOT = -8783
624981 ZDOT = -2677
248894
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 11323
25322451
00016717 00000-0 10270-3 0 9124
2 25544 51
6405 100
3251 0016563 68
6922 291
6000 15
59207941 25120
Satellite: ISS
Catalog Number: 25544
Epoch time: 11323
25322451 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 100
3251 deg
Eccentricity:
0016563
Arg of perigee: 68
6922 deg
Mean anomaly: 291
6000 deg
Mean motion: 15
59207941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 268
Coasting Arc #14 (Orbit 2526)
---------------------------------------
Vector Time (GMT): 2011/324/05:02:05
198
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1402527
82 A = 6772062
88 meter
Y = 6163255
04 meter E =
0021699
Z = -2432769
18 I = 51
99686
XDOT = -4478
708644 Wp = 65
97900
YDOT = 3126
921487 meter/sec RA = 94
68178 deg
ZDOT = 5386
078229 TA = 266
90167
MA = 267
14997
Ha = 219
041 n
mi
Hp = 200
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4601469
21 X = 1345322
97
Y = 20220653
01 feet Y = 6178619
10 meter
Z = -7981526
17 Z = -2426094
58
XDOT = -14693
925996 XDOT = -4539
506606
YDOT = 10258
928762 feet/sec YDOT = 3076
497906 meter/sec
ZDOT = 17670
860332 ZDOT = 5364
172648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11436917
48 X = 3485972
45
Y = -17311075
24 feet Y = -5276415
73 meter
Z = -7954664
04 Z = -2424581
60
XDOT = 16374
134678 XDOT = 4990
836250
YDOT = 2809
120560 feet/sec YDOT = 856
219947 meter/sec
ZDOT = 17581
204273 ZDOT = 5358
751062
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 11324
21462293
00016717 00000-0 10270-3 0 9131
2 25544 51
6404 95
4954 0016568 72
0517 288
2443 15
59216106 25279
Satellite: ISS
Catalog Number: 25544
Epoch time: 11324
21462293 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 95
4954 deg
Eccentricity:
0016568
Arg of perigee: 72
0517 deg
Mean anomaly: 288
2443 deg
Mean motion: 15
59216106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2527
Checksum: 304
Coasting Arc #15 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2011/325/05:02:05
198
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 718184
52 A = 6774130
79 meter
Y = -6667002
30 meter E =
0022495
Z = -962483
72 I = 52
00524
XDOT = 4653
330552 Wp = 99
63720
YDOT = 1342
472238 meter/sec RA = 89
71075 deg
ZDOT = -5948
361834 TA = 90
74932
MA = 90
49156
Ha = 218
990 n
mi
Hp = 200
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2356248
44 X = 797358
55
Y = -21873367
12 feet Y = -6658528
43 meter
Z = -3157754
97 Z = -958802
38
XDOT = 15266
832521 XDOT = 4666
869528
YDOT = 4404
436475 feet/sec YDOT = 1394
584328 meter/sec
ZDOT = -19515
622815 ZDOT = -5925
722640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17246137
00 X = -5256622
56
Y = 13662515
62 feet Y = 4164334
76 meter
Z = -3142282
24 Z = -957767
63
XDOT = -6666
737175 XDOT = -2032
021491
YDOT = -12790
519462 feet/sec YDOT = -3898
550332 meter/sec
ZDOT = -19423
257965 ZDOT = -5920
209028
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 11325
24007974
00016717 00000-0 10270-3 0 9147
2 25544 51
6403 90
3429 0016466 76
2437 284
0550 15
59233332 25434
Satellite: ISS
Catalog Number: 25544
Epoch time: 11325
24007974 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 90
3429 deg
Eccentricity:
0016466
Arg of perigee: 76
2437 deg
Mean anomaly: 284
0550 deg
Mean motion: 15
59233332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 295
Coasting Arc #16 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2011/326/05:02:05
198
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2611883
16 A = 6767890
65 meter
Y = 4857404
30 meter E =
0027417
Z = 3898062
80 I = 51
98347
XDOT = -3722
904277 Wp = 86
87144
YDOT = -5323
756886 meter/sec RA = 84
72600 deg
ZDOT = 4116
135537 TA = 320
23506
MA = 320
43571
Ha = 219
021 n
mi
Hp = 200
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8569170
49 X = -2684942
01
Y = 15936365
82 feet Y = 4827788
07 meter
Z = 12788919
94 Z = 3885196
59
XDOT = -12214
252878 XDOT = -3683
092177
YDOT = -17466
393982 feet/sec YDOT = -5365
166148 meter/sec
ZDOT = 13504
381684 ZDOT = 4098
145876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17330931
03 X = 5282467
78
Y = -5327933
44 feet Y = -1623954
11 meter
Z = 12736045
95 Z = 3881946
81
XDOT = -3834
864394 XDOT = -1168
866667
YDOT = 19815
931456 feet/sec YDOT = 6039
895908 meter/sec
ZDOT = 13431
277037 ZDOT = 4093
853241
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 11326
26550051
00016717 00000-0 10270-3 0 9150
2 25544 51
6400 85
1902 0016615 78
9322 281
3701 15
59298446 25599
Satellite: ISS
Catalog Number: 25544
Epoch time: 11326
26550051 = yrday
fracday
Element set: 915
Inclination: 51
6400 deg
RA of node: 85
1902 deg
Eccentricity:
0016615
Arg of perigee: 78
9322 deg
Mean anomaly: 281
3701 deg
Mean motion: 15
59298446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
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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