[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 3rd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 32291 73 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
343/19:50:36
042 2
8 3
8 3
8
N/A 1
2 -0
3 223
2
000/00:01:12
084 2
2 -0
0 200
8
Coasting Arc #1 (Orbit 2695)
---------------------------------------
Vector Time (GMT): 2011/334/23:53:36
767
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1416057
02 A = 6770466
43 meter
Y = 5307988
62 meter E =
0039183
Z = 3935325
13 I = 51
86989
XDOT = -6397
546622 Wp = 109
23338
YDOT = -1329
319733 meter/sec RA = 40
84807 deg
ZDOT = 4049
677111 TA = 298
52549
MA = 298
91944
Ha = 224
649 n
mi
Hp = 197
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4645856
37 X = 1337479
68
Y = 17414660
82 feet Y = 5323384
27 meter
Z = 12911171
69 Z = 3942013
78
XDOT = -20989
326187 XDOT = -6401
879040
YDOT = -4361
285214 feet/sec YDOT = -1400
885475 meter/sec
ZDOT = 13286
342227 ZDOT = 4018
587199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17820672
39 X = 5431740
94
Y = 2565731
75 feet Y = 782035
04 meter
Z = 12938060
27 Z = 3943520
77
XDOT = -12025
063037 XDOT = -3665
239214
YDOT = 16414
666141 feet/sec YDOT = 5003
190240 meter/sec
ZDOT = 13159
439924 ZDOT = 4010
997289
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 11335
05113347
00016717 00000-0 10270-3 0 9004
2 25544 51
6434 41
1317 0028347 113
3902 247
0238 15
58342420 26968
Satellite: ISS
Catalog Number: 25544
Epoch time: 11335
05113347 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 41
1317 deg
Eccentricity:
0028347
Arg of perigee: 113
3902 deg
Mean anomaly: 247
0238 deg
Mean motion: 15
58342420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2696
Checksum: 276
Coasting Arc #2 (Orbit 2710)
---------------------------------------
Vector Time (GMT): 2011/335/23:53:36
767
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1686762
61 A = 6765089
55 meter
Y = -3910458
26 meter E =
0041187
Z = -5289291
11 I = 51
82922
XDOT = 6521
170721 Wp = 105
36895
YDOT = 3907
584902 meter/sec RA = 35
82614 deg
ZDOT = -825
297755 TA = 156
83381
MA = 156
64761
Ha = 224
429 n
mi
Hp = 198
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5533998
07 X = 1756059
26
Y = -12829587
48 feet Y = -3891208
17 meter
Z = -17353317
29 Z = -5280928
64
XDOT = 21394
917064 XDOT = 6480
999819
YDOT = 12820
160441 feet/sec YDOT = 3980
284062 meter/sec
ZDOT = -2707
669799 ZDOT = -793
715226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9800774
72 X = -2987276
14
Y = -10018183
10 feet Y = -3053542
21 meter
Z = -17318830
58 Z = -5278779
56
XDOT = 19151
337296 XDOT = 5837
327608
YDOT = -14368
101965 feet/sec YDOT = -4379
397479 meter/sec
ZDOT = -2578
971999 ZDOT = -786
070665
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 11336
01302716
00016717 00000-0 10270-3 0 9012
2 25544 51
6437 36
3047 0028161 116
8739 243
5299 15
58425442 27119
Satellite: ISS
Catalog Number: 25544
Epoch time: 11336
01302716 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 36
3047 deg
Eccentricity:
0028161
Arg of perigee: 116
8739 deg
Mean anomaly: 243
5299 deg
Mean motion: 15
58425442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2711
Checksum: 295
Coasting Arc #3 (Orbit 2726)
---------------------------------------
Vector Time (GMT): 2011/336/23:53:36
767
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4469634
07 A = 6766963
85 meter
Y = 1694020
23 meter E =
0032650
Z = 4759051
99 I = 51
81134
XDOT = -4865
695180 Wp = 108
47953
YDOT = -5339
727971 meter/sec RA = 30
79498 deg
ZDOT = -2664
338256 TA = 7
66527
MA = 7
61548
Ha = 224
319 n
mi
Hp = 198
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14664153
76 X = -4511363
48
Y = 5557809
16 feet Y = 1643804
55 meter
Z = 15613687
62 Z = 4737237
08
XDOT = -15963
566862 XDOT = -4792
680705
YDOT = -17518
792557 feet/sec YDOT = -5393
730818 meter/sec
ZDOT = -8741
267243 ZDOT = -2687
798775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -76910
22 X = -23442
24
Y = 15770226
81 feet Y = 4806765
13 meter
Z = 15524429
80 Z = 4731846
20
XDOT = -20895
190364 XDOT = -6368
854023
YDOT = 8612
413631 feet/sec YDOT = 2625
063675 meter/sec
ZDOT = -8836
659044 ZDOT = -2693
413677
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 11337
03900663
00016717 00000-0 10270-3 0 9021
2 25544 51
6439 31
1568 0028000 120
5034 239
8891 15
58520396 27271
Satellite: ISS
Catalog Number: 25544
Epoch time: 11337
03900663 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 31
1568 deg
Eccentricity:
0028000
Arg of perigee: 120
5034 deg
Mean anomaly: 239
8891 deg
Mean motion: 15
58520396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2727
Checksum: 296
Coasting Arc #4 (Orbit 2741)
---------------------------------------
Vector Time (GMT): 2011/337/23:53:36
767
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6213623
77 A = 6773639
29 meter
Y = 686124
84 meter E =
0030007
Z = -2650567
72 I = 51
80706
XDOT = 1623
501858 Wp = 114
37901
YDOT = 5349
865495 meter/sec RA = 25
78669 deg
ZDOT = 5225
304725 TA = 215
84034
MA = 216
04205
Ha = 224
124 n
mi
Hp = 198
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20385904
75 X = 6218365
66
Y = 2251065
73 feet Y = 755636
00 meter
Z = -8696088
33 Z = -2620370
13
XDOT = 5326
449664 XDOT = 1538
174133
YDOT = 17552
052149 feet/sec YDOT = 5367
543198 meter/sec
ZDOT = 17143
388206 ZDOT = 5232
984704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9083401
11 X = 2768620
66
Y = -18446502
31 feet Y = -5622493
90 meter
Z = -8572790
60 Z = -2612986
57
XDOT = 16936
832612 XDOT = 5162
346580
YDOT = 411
861169 feet/sec YDOT = 125
535284 meter/sec
ZDOT = 17174
307943 ZDOT = 5234
729061
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 11338
00082687
00016717 00000-0 10270-3 0 9037
2 25544 51
6437 26
3301 0027992 123
9975 236
3845 15
58533775 27423
Satellite: ISS
Catalog Number: 25544
Epoch time: 11338
00082687 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 26
3301 deg
Eccentricity:
0027992
Arg of perigee: 123
9975 deg
Mean anomaly: 236
3845 deg
Mean motion: 15
58533775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 324
Coasting Arc #5 (Orbit 2757)
---------------------------------------
Vector Time (GMT): 2011/338/23:53:36
767
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6154080
45 A = 6776401
82 meter
Y = -2755710
78 meter E =
0038948
Z = -495702
70 I = 51
78875
XDOT = 2329
729449 Wp = 130
62708
YDOT = -4180
570806 meter/sec RA = 20
80439 deg
ZDOT = -6015
267857 TA = 54
72697
MA = 54
36321
Ha = 224
036 n
mi
Hp = 198
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20190552
67 X = -6120400
10
Y = -9041045
86 feet Y = -2824341
14 meter
Z = -1626321
20 Z = -525517
89
XDOT = 7643
469321 XDOT = 2405
525686
YDOT = -13715
783484 feet/sec YDOT = -4154
094266 meter/sec
ZDOT = -19735
130763 ZDOT = -6003
765981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15103697
28 X = -4603606
93
Y = 16151381
11 feet Y = 4922940
96 meter
Z = -1747874
39 Z = -532752
12
XDOT = -9275
438666 XDOT = -2827
153705
YDOT = -10694
465123 feet/sec YDOT = -3259
672969 meter/sec
ZDOT = -19687
789702 ZDOT = -6000
838301
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 11339
02672868
00016717 00000-0 10270-3 0 9047
2 25544 51
6437 21
1812 0028096 128
1496 232
2197 15
58547547 27588
Satellite: ISS
Catalog Number: 25544
Epoch time: 11339
02672868 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 21
1812 deg
Eccentricity:
0028096
Arg of perigee: 128
1496 deg
Mean anomaly: 232
2197 deg
Mean motion: 15
58547547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2758
Checksum: 329
Coasting Arc #6 (Orbit 2773)
---------------------------------------
Vector Time (GMT): 2011/339/23:53:36
767
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4310945
95 A = 6771338
77 meter
Y = 3981497
94 meter E =
0038130
Z = 3368405
78 I = 51
74340
XDOT = -5703
638993 Wp = 118
29122
YDOT = 2194
159058 meter/sec RA = 15
81333 deg
ZDOT = 4648
418570 TA = 281
05234
MA = 281
48094
Ha = 223
757 n
mi
Hp = 198
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14143523
44 X = 4249740
32
Y = 13062657
27 feet Y = 4029363
16 meter
Z = 11051200
06 Z = 3389200
20
XDOT = -18712
726355 XDOT = -5750
332084
YDOT = 7198
684572 feet/sec YDOT = 2130
116118 meter/sec
ZDOT = 15250
717092 ZDOT = 4620
596626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16767460
49 X = 5110721
96
Y = -9362033
81 feet Y = -2853547
91 meter
Z = 11135792
95 Z = 3394189
69
XDOT = 367
099378 XDOT = 111
891890
YDOT = 18885
610991 feet/sec YDOT = 5756
334230 meter/sec
ZDOT = 15136
883041 ZDOT = 4613
721951
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 11340
05258845
00016717 00000-0 10270-3 0 9058
2 25544 51
6430 16
0323 0027866 131
4180 228
9376 15
58641951 27745
Satellite: ISS
Catalog Number: 25544
Epoch time: 11340
05258845 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 16
0323 deg
Eccentricity:
0027866
Arg of perigee: 131
4180 deg
Mean anomaly: 228
9376 deg
Mean motion: 15
58641951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2774
Checksum: 307
Coasting Arc #7 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2011/340/23:53:36
767
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -961231
29 A = 6764798
24 meter
Y = -4318525
20 meter E =
0037210
Z = -5142288
90 I = 51
69164
XDOT = 7491
062355 Wp = 116
67985
YDOT = 167
617021 meter/sec RA = 10
78570 deg
ZDOT = -1566
087261 TA = 138
34912
MA = 138
06515
Ha = 223
600 n
mi
Hp = 198
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3153645
95 X = -887888
57
Y = -14168389
76 feet Y = -4328863
81 meter
Z = -16871026
58 Z = -5146780
80
XDOT = 24576
976231 XDOT = 7496
239148
YDOT = 549
924608 feet/sec YDOT = 251
415739 meter/sec
ZDOT = -5138
081565 ZDOT = -1529
682564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14442913
49 X = -4402200
03
Y = -1218363
58 feet Y = -371357
22 meter
Z = -16888994
32 Z = -5147765
47
XDOT = 7621
442408 XDOT = 2323
015646
YDOT = -22321
737951 feet/sec YDOT = -6803
665727 meter/sec
ZDOT = -4989
398550 ZDOT = -1520
768678
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 11341
01429489
00016717 00000-0 10270-3 0 9060
2 25544 51
6420 11
2036 0027835 135
1119 225
2293 15
58713012 27893
Satellite: ISS
Catalog Number: 25544
Epoch time: 11341
01429489 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 11
2036 deg
Eccentricity:
0027835
Arg of perigee: 135
1119 deg
Mean anomaly: 225
2293 deg
Mean motion: 15
58713012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 287
Coasting Arc #8 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2011/341/23:53:36
767
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2669995
40 A = 6765238
46 meter
Y = 3687991
42 meter E =
0029265
Z = 4978142
24 I = 51
66402
XDOT = -7040
523020 Wp = 126
43907
YDOT = -2338
808475 meter/sec RA = 5
74101 deg
ZDOT = -2052
170134 TA = 343
38324
MA = 343
47894
Ha = 223
486 n
mi
Hp = 198
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8759827
43 X = -2735220
06
Y = 12099709
38 feet Y = 3657768
74 meter
Z = 16332487
66 Z = 4965013
13
XDOT = -23098
828805 XDOT = -7003
877515
YDOT = -7673
256152 feet/sec YDOT = -2417
334834 meter/sec
ZDOT = -6732
841646 ZDOT = -2086
284685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9192198
88 X = 2801782
22
Y = 11849073
08 feet Y = 3611597
48 meter
Z = 16278533
22 Z = 4961696
92
XDOT = -12864
428712 XDOT = -3921
077871
YDOT = 19381
397282 feet/sec YDOT = 5907
449892 meter/sec
ZDOT = -6871
975037 ZDOT = -2094
577991
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 11342
04007685
00016717 00000-0 10270-3 0 9075
2 25544 51
6422 6
0547 0027800 138
9754 221
3499 15
58785396 28050
Satellite: ISS
Catalog Number: 25544
Epoch time: 11342
04007685 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 6
0547 deg
Eccentricity:
0027800
Arg of perigee: 138
9754 deg
Mean anomaly: 221
3499 deg
Mean motion: 15
58785396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 319
Coasting Arc #9 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2011/342/23:53:36
767
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5610122
80 A = 6771844
91 meter
Y = -2331478
09 meter E =
0029514
Z = -3035465
93 I = 51
65487
XDOT = 4306
947609 Wp = 133
57595
YDOT = 3955
469372 meter/sec RA =
71343 deg
ZDOT = 4932
208907 TA = 191
68163
MA = 191
75026
Ha = 223
288 n
mi
Hp = 198
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18405914
69 X = 5650522
81
Y = -7649206
34 feet Y = -2268516
03 meter
Z = -9958877
71 Z = -3008113
74
XDOT = 14130
405541 XDOT = 4238
436592
YDOT = 12977
261719 feet/sec YDOT = 4003
248685 meter/sec
ZDOT = 16181
787752 ZDOT = 4952
966342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2608247
61 X = -794993
87
Y = -19816709
25 feet Y = -6040132
98 meter
Z = -9846947
60 Z = -3001349
63
XDOT = 14723
524565 XDOT = 4487
730287
YDOT = -10003
679896 feet/sec YDOT = -3049
121632 meter/sec
ZDOT = 16266
216059 ZDOT = 4957
942655
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 11343
00171198
00016717 00000-0 10270-3 0 9084
2 25544 51
6408 1
2256 0027882 142
4816 217
8292 15
58837130 28209
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
00171198 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 1
2256 deg
Eccentricity:
0027882
Arg of perigee: 142
4816 deg
Mean anomaly: 217
8292 deg
Mean motion: 15
58837130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 297
Coasting Arc #10 (Orbit 2832)
---------------------------------------
Vector Time (GMT): 2011/343/19:51:12
084
Vector Time (MET): N/A
Weight (LBS) : 871668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4665618
20 A = 6771759
53 meter
Y = -3237424
19 meter E =
0029226
Z = -3725051
95 I = 51
62617
XDOT = 5547
792852 Wp = 138
02549
YDOT = 3063
232719 meter/sec RA = 356
53676 deg
ZDOT = 4284
628679 TA = 177
57812
MA = 177
56394
Ha = 223
163 n
mi
Hp = 200
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15307146
32 X = 4719568
76
Y = -10621470
42 feet Y = -3184948
27 meter
Z = -12221299
06 Z = -3702255
51
XDOT = 18201
420118 XDOT = 5492
312699
YDOT = 10049
976112 feet/sec YDOT = 3124
960804 meter/sec
ZDOT = 14057
180707 ZDOT = 4311
445735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12054613
80 X = 3674246
29
Y = -14285832
47 feet Y = -4354321
74 meter
Z = -12127893
04 Z = -3696581
80
XDOT = 19076
836545 XDOT = 5814
619779
YDOT = 4065
956445 feet/sec YDOT = 1239
303525 meter/sec
ZDOT = 14166
439001 ZDOT = 4317
930607
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 11343
83510122
00016717 00000-0 10270-3 0 9090
2 25544 51
6440 357
0422 0024991 146
4766 213
7977 15
58189417 28335
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
83510122 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 357
0422 deg
Eccentricity:
0024991
Arg of perigee: 146
4766 deg
Mean anomaly: 213
7977 deg
Mean motion: 15
58189417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2833
Checksum: 319
Coasting Arc #11 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2011/344/19:51:12
084
Vector Time (MET): N/A
Weight (LBS) : 871668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6443608
58 A = 6777149
93 meter
Y = 1760989
53 meter E =
0037817
Z = 1001300
02 I = 51
61405
XDOT = -2143
145982 Wp = 140
91509
YDOT = -4422
945677 meter/sec RA = 351
53455 deg
ZDOT = -5920
612474 TA = 28
18346
MA = 27
97930
Ha = 223
099 n
mi
Hp = 200
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21140448
09 X = -6467685
56
Y = 5777524
71 feet Y = 1688798
40 meter
Z = 3285105
06 Z = 969938
54
XDOT = -7031
318838 XDOT = -2064
767018
YDOT = -14510
976631 feet/sec YDOT = -4446
472626 meter/sec
ZDOT = -19424
581606 ZDOT = -5930
834138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18708226
94 X = -5702267
57
Y = 11451062
09 feet Y = 3490283
72 meter
Z = 3156845
59 Z = 962206
53
XDOT = -9852
472049 XDOT = -3003
033481
YDOT = -10643
155102 feet/sec YDOT = -3244
033675 meter/sec
ZDOT = -19465
931390 ZDOT = -5933
215888
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 11344
86123529
00016717 00000-0 10270-3 0 9107
2 25544 51
6439 351
8947 0025140 150
4219 209
8364 15
58198316 28493
Satellite: ISS
Catalog Number: 25544
Epoch time: 11344
86123529 = yrday
fracday
Element set: 910
Inclination: 51
6439 deg
RA of node: 351
8947 deg
Eccentricity:
0025140
Arg of perigee: 150
4219 deg
Mean anomaly: 209
8364 deg
Mean motion: 15
58198316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 324
Coasting Arc #12 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2011/345/19:51:12
084
Vector Time (MET): N/A
Weight (LBS) : 871668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6478630
48 A = 6775497
09 meter
Y = 78596
08 meter E =
0029560
Z = 1997466
52 I = 51
57986
XDOT = -1796
932039 Wp = 125
31133
YDOT = 4962
933770 meter/sec RA = 346
54118 deg
ZDOT = 5558
014012 TA = 256
77670
MA = 257
10661
Ha = 222
767 n
mi
Hp = 200
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21255349
36 X = 6467566
75
Y = 257861
16 feet Y = 150981
98 meter
Z = 6553367
85 Z = 2028912
89
XDOT = -5895
446321 XDOT = -1879
294856
YDOT = 16282
591110 feet/sec YDOT = 4942
378125 meter/sec
ZDOT = 18234
954109 ZDOT = 5549
085099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20344624
87 X = 6201041
66
Y = -6021017
93 feet Y = -1835206
27 meter
Z = 6681809
68 Z = 2036615
59
XDOT = -1365
888707 XDOT = -416
322878
YDOT = 15847
495082 feet/sec YDOT = 4830
316501 meter/sec
ZDOT = 18198
031644 ZDOT = 5546
760045
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 11345
88732884
00016717 00000-0 10270-3 0 9111
2 25544 51
6440 346
7473 0024866 154
0687 206
1720 15
58290104 28657
Satellite: ISS
Catalog Number: 25544
Epoch time: 11345
88732884 = yrday
fracday
Element set: 911
Inclination: 51
6440 deg
RA of node: 346
7473 deg
Eccentricity:
0024866
Arg of perigee: 154
0687 deg
Mean anomaly: 206
1720 deg
Mean motion: 15
58290104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 322
Coasting Arc #13 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2011/346/19:51:12
084
Vector Time (MET): N/A
Weight (LBS) : 871668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4663502
76 A = 6768647
85 meter
Y = -2142727
96 meter E =
0026714
Z = -4417518
65 I = 51
52856
XDOT = 5211
884650 Wp = 137
01750
YDOT = -4534
513758 meter/sec RA = 341
52283 deg
ZDOT = -3333
626395 TA = 99
41614
MA = 99
11404
Ha = 222
466 n
mi
Hp = 201
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15300205
90 X = -4617736
30
Y = -7029947
37 feet Y = -2194621
67 meter
Z = -14493171
43 Z = -4440062
99
XDOT = 17099
359087 XDOT = 5278
397232
YDOT = -14877
013641 feet/sec YDOT = -4475
858965 meter/sec
ZDOT = -10937
094472 ZDOT = -3308
146119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16646128
56 X = -5073739
98
Y = -1936676
27 feet Y = -590298
93 meter
Z = -14585066
61 Z = -4445528
30
XDOT = 11528
923489 XDOT = 3514
015879
YDOT = -18274
500478 feet/sec YDOT = -5570
067746 meter/sec
ZDOT = -10832
603555 ZDOT = -3301
777564
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 11346
84925652
00016717 00000-0 10270-3 0 9126
2 25544 51
6442 341
9208 0024785 157
9494 202
2733 15
58352983 28802
Satellite: ISS
Catalog Number: 25544
Epoch time: 11346
84925652 = yrday
fracday
Element set: 912
Inclination: 51
6442 deg
RA of node: 341
9208 deg
Eccentricity:
0024785
Arg of perigee: 157
9494 deg
Mean anomaly: 202
2733 deg
Mean motion: 15
58352983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 332
Coasting Arc #14 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2011/347/19:51:12
084
Vector Time (MET): N/A
Weight (LBS) : 871668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1705899
41 A = 6764857
29 meter
Y = 3846687
33 meter E =
0025671
Z = 5287803
51 I = 51
48823
XDOT = -7041
762539 Wp = 155
94105
YDOT = 3075
490335 meter/sec RA = 336
47432 deg
ZDOT = 11
396307 TA = 293
81593
MA = 294
08485
Ha = 222
287 n
mi
Hp = 201
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5596782
83 X = 1637071
15
Y = 12620365
24 feet Y = 3865378
33 meter
Z = 17348436
71 Z = 5295923
95
XDOT = -23102
895469 XDOT = -7075
685281
YDOT = 10090
191387 feet/sec YDOT = 2996
555352 meter/sec
ZDOT = 37
389459 ZDOT = -22
894459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9329013
63 X = 2843483
36
Y = 10120625
07 feet Y = 3084766
52 meter
Z = 17381263
08 Z = 5297808
99
XDOT = -17774
813583 XDOT = -5417
763180
YDOT = 16431
759820 feet/sec YDOT = 5008
400393 meter/sec
ZDOT = -102
958080 ZDOT = -31
381623
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 11347
87527623
00016717 00000-0 10270-3 0 9137
2 25544 51
6444 336
7735 0024850 161
6306 198
5752 15
58424293 28967
Satellite: ISS
Catalog Number: 25544
Epoch time: 11347
87527623 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 336
7735 deg
Eccentricity:
0024850
Arg of perigee: 161
6306 deg
Mean anomaly: 198
5752 deg
Mean motion: 15
58424293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 338
Coasting Arc #15 (Orbit 2910)
---------------------------------------
Vector Time (GMT): 2011/348/19:51:12
084
Vector Time (MET): N/A
Weight (LBS) : 871668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1687209
34 A = 6768611
82 meter
Y = -4896422
07 meter E =
0030745
Z = -4386760
76 I = 51
47321
XDOT = 6839
772527 Wp = 151
28239
YDOT = -673
833352 meter/sec RA = 331
42120 deg
ZDOT = 3366
225460 TA = 153
00938
MA = 152
84916
Ha = 222
117 n
mi
Hp = 201
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5535463
71 X = 1763146
65
Y = -16064376
89 feet Y = -4877129
69 meter
Z = -14392259
70 Z = -4378380
33
XDOT = 22440
198581 XDOT = 6830
446717
YDOT = -2210
739344 feet/sec YDOT = -597
399258 meter/sec
ZDOT = 11044
046785 ZDOT = 3399
430135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -252961
25 X = -77102
59
Y = -17018760
77 feet Y = -5187318
28 meter
Z = -14357593
63 Z = -4376194
54
XDOT = 19002
879781 XDOT = 5792
077757
YDOT = -9760
020809 feet/sec YDOT = -2974
854343 meter/sec
ZDOT = 11179
742631 ZDOT = 3407
585554
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 11348
83713463
00016717 00000-0 10270-3 0 9144
2 25544 51
6439 331
9462 0024761 165
3240 194
8640 15
58475334 29119
Satellite: ISS
Catalog Number: 25544
Epoch time: 11348
83713463 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 331
9462 deg
Eccentricity:
0024761
Arg of perigee: 165
3240 deg
Mean anomaly: 194
8640 deg
Mean motion: 15
58475334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 317
Coasting Arc #16 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2011/349/19:51:12
084
Vector Time (MET): N/A
Weight (LBS) : 871668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4382036
90 A = 6775063
58 meter
Y = 4759318
10 meter E =
0034663
Z = 1932605
79 I = 51
46929
XDOT = -4817
814842 Wp = 148
84129
YDOT = -2154
741273 meter/sec RA = 326
39818 deg
ZDOT = -5602
026506 TA = 9
69599
MA = 9
62927
Ha = 221
945 n
mi
Hp = 201
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14376761
49 X = -4444319
05
Y = 15614560
70 feet Y = 4709967
10 meter
Z = 6340570
19 Z = 1911167
04
XDOT = -15806
479140 XDOT = -4766
148572
YDOT = -7069
361131 feet/sec YDOT = -2208
327767 meter/sec
ZDOT = -18379
352053 ZDOT = -5625
305950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7818101
80 X = -2382957
43
Y = 19760848
24 feet Y = 6023106
54 meter
Z = 6252580
91 Z = 1905786
66
XDOT = -15747
456480 XDOT = -4799
824735
YDOT = -368
303829 feet/sec YDOT = -112
259007 meter/sec
ZDOT = -18474
256165 ZDOT = -5630
953279
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 11349
86308016
00016717 00000-0 10270-3 0 9153
2 25544 51
6441 326
7985 0024815 168
8436 191
3274 15
58516785 29277
Satellite: ISS
Catalog Number: 25544
Epoch time: 11349
86308016 = yrday
fracday
Element set: 915
Inclination: 51
6441 deg
RA of node: 326
7985 deg
Eccentricity:
0024815
Arg of perigee: 168
8436 deg
Mean anomaly: 191
3274 deg
Mean motion: 15
58516785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 344
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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