[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 8th 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) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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 2969)
---------------------------------------
Vector Time (GMT): 2011/097/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1612846
82 A = 6725104
75 meter
Y = 4389728
80 meter E =
0014023
Z = -4845686
63 I = 51
71672
XDOT = -7299
532483 Wp = 102
66149
YDOT = -21
133008 meter/sec RA = 165
04001 deg
ZDOT = 2413
280486 TA = 190
89459
MA = 190
92500
Ha = 192
580 n
mi
Hp = 184
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5291492
18 X = -1638274
06
Y = 14401997
36 feet Y = 4371550
57 meter
Z = -15897922
00 Z = -4853583
87
XDOT = -23948
597384 XDOT = -7310
477028
YDOT = -69
334016 feet/sec YDOT = -102
821891 meter/sec
ZDOT = 7917
586895 ZDOT = 2377
792475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1217930
57 X = -371225
24
Y = -15261606
73 feet Y = -4651737
73 meter
Z = -15929888
47 Z = -4855430
00
XDOT = 20767
433912 XDOT = 6329
913856
YDOT = -9762
187440 feet/sec YDOT = -2975
514732 meter/sec
ZDOT = 7774
146362 ZDOT = 2369
559811
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 11097
04025929
00016717 00000-0 10270-3 0 9006
2 25544 51
6453 166
0456 0002215 74
3678 285
7729 15
72896857 29705
Satellite: ISS
Catalog Number: 25544
Epoch time: 11097
04025929 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 166
0456 deg
Eccentricity:
0002215
Arg of perigee: 74
3678 deg
Mean anomaly: 285
7729 deg
Mean motion: 15
72896857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2970
Checksum: 335
Coasting Arc #2 (Orbit 2985)
---------------------------------------
Vector Time (GMT): 2011/098/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6429724
49 A = 6733775
73 meter
Y = -823213
68 meter E =
0008668
Z = -1816101
53 I = 51
77527
XDOT = -943
949100 Wp = 129
72187
YDOT = 5106
477319 meter/sec RA = 159
95584 deg
ZDOT = -5679
933945 TA = 70
36287
MA = 70
26934
Ha = 192
514 n
mi
Hp = 184
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21094896
62 X = 6447274
30
Y = -2700832
27 feet Y = -751214
53 meter
Z = -5958338
35 Z = -1784823
06
XDOT = -3096
945867 XDOT = -973
388265
YDOT = 16753
534512 feet/sec YDOT = 5095
756735 meter/sec
ZDOT = -18634
953888 ZDOT = -5684
591341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17931311
52 X = -5465463
75
Y = 11499917
08 feet Y = 3505174
73 meter
Z = -5831888
94 Z = -1777559
75
XDOT = -3647
233808 XDOT = -1111
676865
YDOT = -15107
212455 feet/sec YDOT = -4604
678356 meter/sec
ZDOT = -18653
840457 ZDOT = -5685
690571
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 11098
05677958
00016717 00000-0 10270-3 0 9014
2 25544 51
6449 160
8341 0002140 79
7956 280
3448 15
72954999 29868
Satellite: ISS
Catalog Number: 25544
Epoch time: 11098
05677958 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 160
8341 deg
Eccentricity:
0002140
Arg of perigee: 79
7956 deg
Mean anomaly: 280
3448 deg
Mean motion: 15
72954999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2986
Checksum: 356
Coasting Arc #3 (Orbit 3001)
---------------------------------------
Vector Time (GMT): 2011/099/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 58478
56 A = 6723564
64 meter
Y = -4427925
90 meter E =
0007251
Z = 5054689
75 I = 51
77084
XDOT = 7259
840586 Wp = 61
90438
YDOT = -1898
720715 meter/sec RA = 154
80613 deg
ZDOT = -1742
041056 TA = 44
85538
MA = 44
79680
Ha = 192
255 n
mi
Hp = 184
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 191858
79 X = 83433
26
Y = -14527315
96 feet Y = -4427132
33 meter
Z = 16583627
78 Z = 5055034
54
XDOT = 23818
374626 XDOT = 7288
995425
YDOT = -6229
398672 feet/sec YDOT = -1817
373797 meter/sec
ZDOT = -5715
357795 ZDOT = -1706
701761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6370248
34 X = 1941651
69
Y = 13055709
49 feet Y = 3979380
25 meter
Z = 16585078
08 Z = 5055131
80
XDOT = -17649
951803 XDOT = -5379
705310
YDOT = 15712
598872 feet/sec YDOT = 4789
200136 meter/sec
ZDOT = -5572
461496 ZDOT = -1698
486264
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 11099
07323138
00016717 00000-0 10270-3 0 9026
2 25544 51
6448 155
6214 0002201 78
1251 282
0158 15
73117322 30026
Satellite: ISS
Catalog Number: 25544
Epoch time: 11099
07323138 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 155
6214 deg
Eccentricity:
0002201
Arg of perigee: 78
1251 deg
Mean anomaly: 282
0158 deg
Mean motion: 15
73117322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3002
Checksum: 266
Coasting Arc #4 (Orbit 3017)
---------------------------------------
Vector Time (GMT): 2011/100/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6139614
66 A = 6733782
05 meter
Y = 2446833
43 meter E =
0015946
Z = 1251163
20 I = 51
83244
XDOT = -750
373440 Wp = 61
83812
YDOT = -4915
534859 meter/sec RA = 149
71401 deg
ZDOT = 5881
740297 TA = 311
84675
MA = 311
98276
Ha = 192
128 n
mi
Hp = 184
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20143092
73 X = -6172597
24
Y = 8027668
74 feet Y = 2377992
14 meter
Z = 4104866
16 Z = 1221256
79
XDOT = -2461
855117 XDOT = -723
923661
YDOT = -16127
082870 feet/sec YDOT = -4923
778000 meter/sec
ZDOT = 19297
048220 ZDOT = 5878
159313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14221898
31 X = 4334834
61
Y = -16398281
66 feet Y = -4998196
25 meter
Z = 3983910
56 Z = 1214295
94
XDOT = 8504
514002 XDOT = 2592
175868
YDOT = 12100
800350 feet/sec YDOT = 3688
323947 meter/sec
ZDOT = 19282
635753 ZDOT = 5877
347378
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 11100
08961802
00016717 00000-0 10270-3 0 9037
2 25544 51
6439 150
4081 0002204 82
0539 278
0874 15
73213322 30181
Satellite: ISS
Catalog Number: 25544
Epoch time: 11100
08961802 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 150
4081 deg
Eccentricity:
0002204
Arg of perigee: 82
0539 deg
Mean anomaly: 278
0874 deg
Mean motion: 15
73213322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3018
Checksum: 272
Coasting Arc #5 (Orbit 3032)
---------------------------------------
Vector Time (GMT): 2011/101/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1295847
75 A = 6722520
71 meter
Y = 4087934
07 meter E =
0016573
Z = -5191471
62 I = 51
82049
XDOT = -6681
491192 Wp = 97
08701
YDOT = 3614
416714 meter/sec RA = 144
57514 deg
ZDOT = 1179
538079 TA = 184
16201
MA = 184
17581
Ha = 191
995 n
mi
Hp = 184
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4251469
00 X = 1275258
53
Y = 13411857
19 feet Y = 4102309
79 meter
Z = -17032387
21 Z = -5185226
51
XDOT = -21920
902860 XDOT = -6727
141668
YDOT = 11858
322551 feet/sec YDOT = 3539
445007 meter/sec
ZDOT = 3869
875587 ZDOT = 1146
968534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10198825
36 X = -3108601
97
Y = -9736247
73 feet Y = -2967608
31 meter
Z = -17007191
35 Z = -5183791
92
XDOT = 12972
385673 XDOT = 3953
983153
YDOT = -20111
531917 feet/sec YDOT = -6129
994928 meter/sec
ZDOT = 3738
118157 ZDOT = 1139
378414
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 11101
04242075
00016717 00000-0 10270-3 0 9049
2 25544 51
6431 145
5198 0002268 83
8736 276
2686 15
73302952 30331
Satellite: ISS
Catalog Number: 25544
Epoch time: 11101
04242075 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 145
5198 deg
Eccentricity:
0002268
Arg of perigee: 83
8736 deg
Mean anomaly: 276
2686 deg
Mean motion: 15
73302952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3033
Checksum: 294
Coasting Arc #6 (Orbit 3048)
---------------------------------------
Vector Time (GMT): 2011/102/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5481456
58 A = 6733673
53 meter
Y = -3810250
06 meter E =
0011888
Z = -847714
46 I = 51
88312
XDOT = 2117
021339 Wp = 132
58406
YDOT = 4362
503111 meter/sec RA = 139
47833 deg
ZDOT = -5979
924153 TA = 56
62976
MA = 56
51605
Ha = 191
917 n
mi
Hp = 183
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17983781
43 X = 5527774
15
Y = -12500820
41 feet Y = -3748694
14 meter
Z = -2781215
41 Z = -820973
05
XDOT = 6945
608066 XDOT = 2097
130888
YDOT = 14312
674248 feet/sec YDOT = 4386
065511 meter/sec
ZDOT = -19619
173729 ZDOT = -5969
688181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9568879
36 X = -2916594
43
Y = 19715821
85 feet Y = 6009382
50 meter
Z = -2673009
76 Z = -814733
37
XDOT = -11730
531342 XDOT = -3575
465953
YDOT = -8319
537740 feet/sec YDOT = -2535
795103 meter/sec
ZDOT = -19577
841037 ZDOT = -5967
325948
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 11102
05867892
00016717 00000-0 10270-3 0 9052
2 25544 51
6432 140
3070 0002258 89
4143 270
7279 15
73372084 30494
Satellite: ISS
Catalog Number: 25544
Epoch time: 11102
05867892 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 140
3070 deg
Eccentricity:
0002258
Arg of perigee: 89
4143 deg
Mean anomaly: 270
7279 deg
Mean motion: 15
73372084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3049
Checksum: 300
Coasting Arc #7 (Orbit 3064)
---------------------------------------
Vector Time (GMT): 2011/103/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2345898
11 A = 6721746
50 meter
Y = -3487010
83 meter E =
0005194
Z = 5241746
73 I = 51
86620
XDOT = 5773
644473 Wp = 75
22323
YDOT = -5042
928638 meter/sec RA = 134
34863 deg
ZDOT = -768
878338 TA = 22
07711
MA = 22
05475
Ha = 191
818 n
mi
Hp = 183
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7696516
10 X = -2332194
64
Y = -11440324
24 feet Y = -3513167
20 meter
Z = 17197331
78 Z = 5230383
89
XDOT = 18942
403127 XDOT = 5833
341402
YDOT = -16545
041462 feet/sec YDOT = -4978
030498 meter/sec
ZDOT = -2522
566725 ZDOT = -740
684881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12507236
99 X = 3812205
83
Y = 5938282
49 feet Y = 1809988
50 meter
Z = 17151426
27 Z = 5227754
73
XDOT = -7580
037985 XDOT = -2310
395578
YDOT = 22939
718939 feet/sec YDOT = 6992
026333 meter/sec
ZDOT = -2408
457922 ZDOT = -734
097975
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 11103
07486916
00016717 00000-0 10270-3 0 9060
2 25544 51
6427 135
0922 0002292 92
8924 267
2501 15
73481524 30655
Satellite: ISS
Catalog Number: 25544
Epoch time: 11103
07486916 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 135
0922 deg
Eccentricity:
0002292
Arg of perigee: 92
8924 deg
Mean anomaly: 267
2501 deg
Mean motion: 15
73481524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3065
Checksum: 299
Coasting Arc #8 (Orbit 3080)
---------------------------------------
Vector Time (GMT): 2011/104/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4554429
30 A = 6733233
37 meter
Y = 4922566
78 meter E =
0014815
Z = 527128
10 I = 51
92534
XDOT = -3168
768640 Wp = 57
00887
YDOT = -3589
840040 meter/sec RA = 129
24518 deg
ZDOT = 6031
657041 TA = 308
70393
MA = 308
83632
Ha = 191
571 n
mi
Hp = 183
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14942353
33 X = -4611696
56
Y = 16150153
47 feet Y = 4871316
22 meter
Z = 1729422
89 Z = 504863
33
XDOT = -10396
222572 XDOT = -3157
691427
YDOT = -11777
690421 feet/sec YDOT = -3625
212772 meter/sec
ZDOT = 19788
901054 ZDOT = 6016
290392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4384993
23 X = 1336545
94
Y = -21567959
06 feet Y = -6573913
92 meter
Z = 1639286
47 Z = 499654
52
XDOT = 13529
943645 XDOT = 4123
926823
YDOT = 4279
991770 feet/sec YDOT = 1304
541492 meter/sec
ZDOT = 19726
800696 ZDOT = 6012
728852
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 11104
09099176
00016717 00000-0 10270-3 0 9072
2 25544 51
6416 129
8766 0002314 96
8556 263
2870 15
73592244 30815
Satellite: ISS
Catalog Number: 25544
Epoch time: 11104
09099176 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 129
8766 deg
Eccentricity:
0002314
Arg of perigee: 96
8556 deg
Mean anomaly: 263
2870 deg
Mean motion: 15
73592244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3081
Checksum: 321
Coasting Arc #9 (Orbit 3095)
---------------------------------------
Vector Time (GMT): 2011/105/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3112940
50 A = 6721022
91 meter
Y = 2785653
25 meter E =
0017365
Z = -5280047
58 I = 51
90286
XDOT = -4624
008885 Wp = 95
15804
YDOT = 6120
982634 meter/sec RA = 124
12173 deg
ZDOT = 503
037351 TA = 179
61212
MA = 179
61077
Ha = 191
433 n
mi
Hp = 183
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10213059
38 X = 3107208
94
Y = 9139282
33 feet Y = 2820431
55 meter
Z = -17322990
75 Z = -5264939
08
XDOT = -15170
632824 XDOT = -4694
554877
YDOT = 20081
964023 feet/sec YDOT = 6068
879759 meter/sec
ZDOT = 1650
385010 ZDOT = 480
402050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13602957
66 X = -4146181
50
Y = -2214652
12 feet Y = -675025
97 meter
Z = -17261921
41 Z = -5261433
64
XDOT = 1944
155430 XDOT = 592
578575
YDOT = -24093
785150 feet/sec YDOT = -7343
785714 meter/sec
ZDOT = 1558
721479 ZDOT = 475
098307
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 11105
04354436
00016717 00000-0 10270-3 0 9082
2 25544 51
6406 124
9866 0002456 102
4327 257
7111 15
73704247 30968
Satellite: ISS
Catalog Number: 25544
Epoch time: 11105
04354436 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 124
9866 deg
Eccentricity:
0002456
Arg of perigee: 102
4327 deg
Mean anomaly: 257
7111 deg
Mean motion: 15
73704247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3096
Checksum: 294
Coasting Arc #10 (Orbit 3111)
---------------------------------------
Vector Time (GMT): 2011/106/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3520246
11 A = 6732559
88 meter
Y = -5719155
82 meter E =
0013496
Z = -388818
46 I = 51
95953
XDOT = 3868
714262 Wp = 132
15531
YDOT = 2782
884987 meter/sec RA = 119
01669 deg
ZDOT = -6049
132369 TA = 52
05340
MA = 51
93151
Ha = 191
215 n
mi
Hp = 183
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11549363
86 X = 3585825
98
Y = -18763634
59 feet Y = -5679423
65 meter
Z = -1275651
12 Z = -371557
22
XDOT = 12692
632093 XDOT = 3866
693721
YDOT = 9130
200089 feet/sec YDOT = 2826
135464 meter/sec
ZDOT = -19846
234807 ZDOT = -6030
343217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 632295
17 X = 192723
57
Y = 22028061
85 feet Y = 6714153
25 meter
Z = -1205723
13 Z = -367504
41
XDOT = -14113
351062 XDOT = -4301
749404
YDOT = -650
112465 feet/sec YDOT = -198
154279 meter/sec
ZDOT = -19770
277744 ZDOT = -6025
980656
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 11106
05953245
00016717 00000-0 10270-3 0 9098
2 25544 51
6408 119
7711 0002387 102
7314 257
4116 15
73844619 31122
Satellite: ISS
Catalog Number: 25544
Epoch time: 11106
05953245 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 119
7711 deg
Eccentricity:
0002387
Arg of perigee: 102
7314 deg
Mean anomaly: 257
4116 deg
Mean motion: 15
73844619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3112
Checksum: 294
Coasting Arc #11 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2011/107/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3599321
88 A = 6720497
62 meter
Y = -2078630
37 meter E =
0004904
Z = 5276834
76 I = 51
93205
XDOT = 3400
476839 Wp = 92
83381
YDOT = -6902
645193 meter/sec RA = 113
89586 deg
ZDOT = -399
523546 TA =
94297
MA =
94205
Ha = 191
334 n
mi
Hp = 183
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11808798
81 X = -3601444
91
Y = -6819653
44 feet Y = -2118891
63 meter
Z = 17312449
99 Z = 5259344
07
XDOT = 11156
420077 XDOT = 3479
351638
YDOT = -22646
473730 feet/sec YDOT = -6864
178015 meter/sec
ZDOT = -1310
772789 ZDOT = -382
811732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13684079
18 X = 4170907
33
Y = -1069993
09 feet Y = -326133
89 meter
Z = 17241734
80 Z = 5255280
77
XDOT = 3443
475532 XDOT = 1049
571342
YDOT = 24004
151351 feet/sec YDOT = 7316
465332 meter/sec
ZDOT = -1243
031628 ZDOT = -378
876040
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 11107
07545343
00016717 00000-0 10270-3 0 9109
2 25544 51
6398 114
5539 0002628 112
4016 247
7426 15
73873646 31281
Satellite: ISS
Catalog Number: 25544
Epoch time: 11107
07545343 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 114
5539 deg
Eccentricity:
0002628
Arg of perigee: 112
4016 deg
Mean anomaly: 247
7426 deg
Mean motion: 15
73873646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 304
Coasting Arc #12 (Orbit 3143)
---------------------------------------
Vector Time (GMT): 2011/108/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2417266
38 A = 6732054
20 meter
Y = 6267861
78 meter E =
0013984
Z = 344995
10 I = 51
98393
XDOT = -4315
941500 Wp = 59
02523
YDOT = -2007
190784 meter/sec RA = 108
78883 deg
ZDOT = 6053
736046 TA = 304
70731
MA = 304
83897
Ha = 190
957 n
mi
Hp = 182
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7930663
97 X = -2488851
10
Y = 20563850
97 feet Y = 6240430
20 meter
Z = 1131873
68 Z = 333077
64
XDOT = -14159
913058 XDOT = -4322
584327
YDOT = -6585
271600 feet/sec YDOT = -2055
491085 meter/sec
ZDOT = 19861
338734 ZDOT = 6032
752865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5384502
66 X = -1641196
41
Y = -21374789
89 feet Y = -6515035
96 meter
Z = 1083523
86 Z = 330258
07
XDOT = 13902
223528 XDOT = 4237
397731
YDOT = -2469
626630 feet/sec YDOT = -752
742197 meter/sec
ZDOT = 19776
495161 ZDOT = 6027
875725
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 11108
09129977
00016717 00000-0 10270-3 0 9114
2 25544 51
6399 109
3364 0002674 119
2479 240
8952 15
74027538 31447
Satellite: ISS
Catalog Number: 25544
Epoch time: 11108
09129977 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 109
3364 deg
Eccentricity:
0002674
Arg of perigee: 119
2479 deg
Mean anomaly: 240
8952 deg
Mean motion: 15
74027538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3144
Checksum: 325
Coasting Arc #13 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2011/109/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3898876
33 A = 6719775
08 meter
Y = 1473791
55 meter E =
0017487
Z = -5285809
36 I = 51
95295
XDOT = -2160
381991 Wp = 98
21060
YDOT = 7364
328112 meter/sec RA = 103
66878 deg
ZDOT = 458
646920 TA = 176
14056
MA = 176
12705
Ha = 190
815 n
mi
Hp = 182
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12791589
00 X = 3907784
24
Y = 4835274
12 feet Y = 1517440
85 meter
Z = -17341894
24 Z = -5266846
72
XDOT = -7087
867425 XDOT = -2244
798808
YDOT = 24161
181470 feet/sec YDOT = 7339
697420 meter/sec
ZDOT = 1504
747112 ZDOT = 447
946409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13259228
28 X = -4041412
78
Y = 3721721
07 feet Y = 1134380
58 meter
Z = -17265212
95 Z = -5262436
91
XDOT = -8284
170533 XDOT = -2525
015179
YDOT = -22717
121438 feet/sec YDOT = -6924
178614 meter/sec
ZDOT = 1461
275650 ZDOT = 445
396818
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 11109
04359127
00016717 00000-0 10270-3 0 9123
2 25544 51
6404 104
4454 0002854 123
2663 236
8774 15
74138855 31598
Satellite: ISS
Catalog Number: 25544
Epoch time: 11109
04359127 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 104
4454 deg
Eccentricity:
0002854
Arg of perigee: 123
2663 deg
Mean anomaly: 236
8774 deg
Mean motion: 15
74138855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 305
Coasting Arc #14 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2011/110/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1378756
97 A = 6731260
48 meter
Y = -6563734
60 meter E =
0013834
Z = -494089
10 I = 51
99925
XDOT = 4563
456288 Wp = 136
26020
YDOT = 1405
270219 meter/sec RA = 98
56329 deg
ZDOT = -6043
504857 TA = 49
08950
MA = 48
96978
Ha = 190
536 n
mi
Hp = 182
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4523480
86 X = 1454451
65
Y = -21534562
33 feet Y = -6547893
26 meter
Z = -1621027
24 Z = -487207
19
XDOT = 14971
969449 XDOT = 4576
761772
YDOT = 4610
466599 feet/sec YDOT = 1456
375994 meter/sec
ZDOT = -19827
771839 ZDOT = -6021
302956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9414643
13 X = 2869583
23
Y = 19891048
47 feet Y = 6062791
57 meter
Z = -1593006
13 Z = -485548
27
XDOT = -13354
927181 XDOT = -4070
581805
YDOT = 4769
559721 feet/sec YDOT = 1453
761803 meter/sec
ZDOT = -19737
981207 ZDOT = -6016
136672
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 11110
05929619
00016717 00000-0 10270-3 0 9136
2 25544 51
6405 99
2269 0002691 125
8743 234
2670 15
74285989 31756
Satellite: ISS
Catalog Number: 25544
Epoch time: 11110
05929619 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 99
2269 deg
Eccentricity:
0002691
Arg of perigee: 125
8743 deg
Mean anomaly: 234
2670 deg
Mean motion: 15
74285989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 326
Coasting Arc #15 (Orbit 3190)
---------------------------------------
Vector Time (GMT): 2011/111/00:40:57
363
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4058418
80 A = 6719326
13 meter
Y = -1006603
47 meter E =
0004956
Z = 5255530
23 I = 51
96331
XDOT = 996
592903 Wp = 97
61299
YDOT = -7610
103586 meter/sec RA = 93
43898 deg
ZDOT = -688
086449 TA = 358
89621
MA = 358
89730
Ha = 190
666 n
mi
Hp = 182
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13315022
29 X = -4072391
79
Y = -3302504
82 feet Y = -1052065
44 meter
Z = 17242553
24 Z = 5235780
28
XDOT = 3269
661755 XDOT = 1084
959097
YDOT = -24967
531450 feet/sec YDOT = -7598
464979 meter/sec
ZDOT = -2257
501473 ZDOT = -683
030517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12586315
92 X = 3836309
09
Y = -5703460
06 feet Y = -1738414
63 meter
Z = 17162668
61 Z = 5231181
39
XDOT = 12444
860110 XDOT = 3793
193361
YDOT = 20733
104338 feet/sec YDOT = 6319
450202 meter/sec
ZDOT = -2236
821368 ZDOT = -681
783153
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 11111
07493053
00016717 00000-0 10270-3 0 9148
2 25544 51
6410 94
0089 0003010 132
1785 227
9635 15
74321736 31917
Satellite: ISS
Catalog Number: 25544
Epoch time: 11111
07493053 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 94
0089 deg
Eccentricity:
0003010
Arg of perigee: 132
1785 deg
Mean anomaly: 227
9635 deg
Mean motion: 15
74321736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3191
Checksum: 279
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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