[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 24th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23680 6 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
334/22:27:31
877 -2
8 3
3 3
3
N/A -1
5 0
0 226
4
000/00:01:03
754 0
9 0
0 196
4
Coasting Arc #1 (Orbit 2547)
---------------------------------------
Vector Time (GMT): 2011/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -515715
35 A = 6776550
12 meter
Y = 6679547
80 meter E =
0043447
Z = 915559
50 I = 52
00559
XDOT = -4696
359703 Wp = 69
81561
YDOT = -1209
172375 meter/sec RA = 88
28689 deg
ZDOT = 5963
311033 TA = 300
07786
MA = 300
50798
Ha = 225
432 n
mi
Hp = 196
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1691979
49 X = -594816
76
Y = 21914526
91 feet Y = 6673338
47 meter
Z = 3003804
14 Z = 912861
98
XDOT = -15408
004276 XDOT = -4711
458724
YDOT = -3967
100967 feet/sec YDOT = -1261
774387 meter/sec
ZDOT = 19564
668742 ZDOT = 5940
458977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17981018
17 X = -5480614
34
Y = -12643614
40 feet Y = -3853773
67 meter
Z = 2992344
25 Z = 912066
53
XDOT = 10405
304233 XDOT = 3171
536730
YDOT = -10023
563665 feet/sec YDOT = -3055
182205 meter/sec
ZDOT = 19471
426113 ZDOT = 5934
890679
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
56236704
00016717 00000-0 10270-3 0 9002
2 25544 51
6404 88
7524 0030590 76
6141 283
8421 15
58418173 25488
Satellite: ISS
Catalog Number: 25544
Epoch time: 11325
56236704 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 88
7524 deg
Eccentricity:
0030590
Arg of perigee: 76
6141 deg
Mean anomaly: 283
8421 deg
Mean motion: 15
58418173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2548
Checksum: 304
Coasting Arc #2 (Orbit 2562)
---------------------------------------
Vector Time (GMT): 2011/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2356992
11 A = 6770828
23 meter
Y = -5139848
15 meter E =
0036323
Z = -3760807
70 I = 51
98518
XDOT = 3960
282752 Wp = 79
60399
YDOT = 4938
097725 meter/sec RA = 83
30870 deg
ZDOT = -4295
651110 TA = 145
05773
MA = 144
81880
Ha = 225
347 n
mi
Hp = 196
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7732913
73 X = 2432561
48
Y = -16863018
85 feet Y = -5113068
20 meter
Z = -12338607
94 Z = -3749173
72
XDOT = 12993
053648 XDOT = 3925
637618
YDOT = 16201
108021 feet/sec YDOT = 4982
190422 meter/sec
ZDOT = -14093
343538 ZDOT = -4276
495642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10789122
11 X = 3288524
42
Y = 15130534
83 feet Y = 4611787
02 meter
Z = -12290743
07 Z = -3746218
49
XDOT = -19446
406618 XDOT = -5927
264737
YDOT = 2558
806952 feet/sec YDOT = 779
924359 meter/sec
ZDOT = -14015
454596 ZDOT = -4271
910561
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
52422646
00016717 00000-0 10270-3 0 9012
2 25544 51
6406 83
9251 0030478 80
0931 280
3662 15
58454093 25632
Satellite: ISS
Catalog Number: 25544
Epoch time: 11326
52422646 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 83
9251 deg
Eccentricity:
0030478
Arg of perigee: 80
0931 deg
Mean anomaly: 280
3662 deg
Mean motion: 15
58454093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2563
Checksum: 298
Coasting Arc #3 (Orbit 2578)
---------------------------------------
Vector Time (GMT): 2011/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3718012
46 A = 6764919
99 meter
Y = 2130020
97 meter E =
0033508
Z = 5205885
03 I = 51
96277
XDOT = -2446
689425 Wp = 87
77702
YDOT = -7204
084613 meter/sec RA = 78
29874 deg
ZDOT = 1194
877897 TA = 350
83167
MA = 350
89270
Ha = 225
317 n
mi
Hp = 196
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12198203
60 X = -3766844
32
Y = 6988257
77 feet Y = 2088170
57 meter
Z = 17079675
28 Z = 5187703
96
XDOT = -8027
196275 XDOT = -2371
754726
YDOT = -23635
448207 feet/sec YDOT = -7231
026074 meter/sec
ZDOT = 3920
203074 ZDOT = 1183
173226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -228079
97 X = -69518
77
Y = -14146233
46 feet Y = -4311771
96 meter
Z = 17005272
24 Z = 5183206
98
XDOT = 23567
624135 XDOT = 7183
411836
YDOT = 4296
698733 feet/sec YDOT = 1309
633774 meter/sec
ZDOT = 3872
914870 ZDOT = 1180
464452
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 11327
55017594
00016717 00000-0 10270-3 0 9029
2 25544 51
6415 78
7770 0030398 83
6187 276
8428 15
58556687 25792
Satellite: ISS
Catalog Number: 25544
Epoch time: 11327
55017594 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 78
7770 deg
Eccentricity:
0030398
Arg of perigee: 83
6187 deg
Mean anomaly: 276
8428 deg
Mean motion: 15
58556687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2579
Checksum: 355
Coasting Arc #4 (Orbit 2593)
---------------------------------------
Vector Time (GMT): 2011/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4453478
01 A = 6766266
67 meter
Y = 1423381
42 meter E =
0042033
Z = -4927883
81 I = 51
96072
XDOT = 262
418644 Wp = 92
47324
YDOT = 7269
474864 meter/sec RA = 73
27639 deg
ZDOT = 2352
418186 TA = 200
43965
MA = 200
60836
Ha = 225
185 n
mi
Hp = 196
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14611148
33 X = 4461169
82
Y = 4669886
53 feet Y = 1473226
35 meter
Z = -16167597
79 Z = -4906229
49
XDOT = 860
953558 XDOT = 169
682542
YDOT = 23849
983150 feet/sec YDOT = 7271
890680 meter/sec
ZDOT = 7717
907434 ZDOT = 2353
468384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10970068
91 X = -3343677
00
Y = 10853552
70 feet Y = 3308162
86 meter
Z = -16079262
92 Z = -4900959
34
XDOT = -20705
024783 XDOT = -6310
891554
YDOT = -9563
756938 feet/sec YDOT = -2915
033115 meter/sec
ZDOT = 7721
659705 ZDOT = 2353
561878
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 11328
51197658
00016717 00000-0 10270-3 0 9037
2 25544 51
6421 73
9514 0030534 86
9965 273
4684 15
58580074 25945
Satellite: ISS
Catalog Number: 25544
Epoch time: 11328
51197658 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 73
9514 deg
Eccentricity:
0030534
Arg of perigee: 86
9965 deg
Mean anomaly: 273
4684 deg
Mean motion: 15
58580074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 336
Coasting Arc #5 (Orbit 2609)
---------------------------------------
Vector Time (GMT): 2011/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4165995
54 A = 6773075
69 meter
Y = -4514061
33 meter E =
0043913
Z = 2812237
72 I = 51
97402
XDOT = 2215
212273 Wp = 93
38428
YDOT = -5282
745523 meter/sec RA = 68
27515 deg
ZDOT = -5131
961116 TA = 54
71554
MA = 54
30556
Ha = 225
238 n
mi
Hp = 196
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13667964
35 X = -4128870
38
Y = -14809912
51 feet Y = -4560440
77 meter
Z = 9226501
69 Z = 2792088
62
XDOT = 7267
756802 XDOT = 2299
050956
YDOT = -17331
842267 feet/sec YDOT = -5257
504350 meter/sec
ZDOT = -16837
142769 ZDOT = -5120
996318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19397407
55 X = 5912329
82
Y = -5602937
64 feet Y = -1707775
39 meter
Z = 9144548
21 Z = 2787258
30
XDOT = 11762
547275 XDOT = 3585
224409
YDOT = 12958
983845 feet/sec YDOT = 3949
898276 meter/sec
ZDOT = -16791
955254 ZDOT = -5118
187961
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 11329
53786452
00016717 00000-0 10270-3 0 9047
2 25544 51
6422 68
8022 0030591 90
7843 269
6817 15
58592926 26107
Satellite: ISS
Catalog Number: 25544
Epoch time: 11329
53786452 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 68
8022 deg
Eccentricity:
0030591
Arg of perigee: 90
7843 deg
Mean anomaly: 269
6817 deg
Mean motion: 15
58592926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2610
Checksum: 328
Coasting Arc #6 (Orbit 2625)
---------------------------------------
Vector Time (GMT): 2011/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2906710
41 A = 6776210
57 meter
Y = 6112054
21 meter E =
0040219
Z = 190613
93 I = 51
97372
XDOT = -4357
949600 Wp = 80
62855
YDOT = 1850
594824 meter/sec RA = 63
30360 deg
ZDOT = 6041
745938 TA = 281
41959
MA = 281
87107
Ha = 225
086 n
mi
Hp = 196
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9536451
49 X = 2837222
20
Y = 20052671
28 feet Y = 6144170
27 meter
Z = 625373
80 Z = 204566
85
XDOT = -14297
734907 XDOT = -4407
669520
YDOT = 6071
505329 feet/sec YDOT = 1801
582852 meter/sec
ZDOT = 19822
001108 ZDOT = 6020
454179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22202844
03 X = -6767426
86
Y = -115619
65 feet Y = -35240
87 meter
Z = 681889
73 Z = 207839
99
XDOT = 778
273270 XDOT = 237
217693
YDOT = -14005
139023 feet/sec YDOT = -4268
766374 meter/sec
ZDOT = 19734
885981 ZDOT = 6015
193247
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 11330
56371870
00016717 00000-0 10270-3 0 9057
2 25544 51
6430 63
6542 0030530 94
1032 266
3614 15
58647153 26266
Satellite: ISS
Catalog Number: 25544
Epoch time: 11330
56371870 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 63
6542 deg
Eccentricity:
0030530
Arg of perigee: 94
1032 deg
Mean anomaly: 266
3614 deg
Mean motion: 15
58647153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2626
Checksum: 287
Coasting Arc #7 (Orbit 2640)
---------------------------------------
Vector Time (GMT): 2011/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -630696
16 A = 6771495
04 meter
Y = -5906560
05 meter E =
0035120
Z = -3275813
13 I = 51
94343
XDOT = 5637
674491 Wp = 97
27269
YDOT = 2019
277013 meter/sec RA = 58
32747 deg
ZDOT = -4774
400443 TA = 120
55520
MA = 120
20817
Ha = 224
961 n
mi
Hp = 196
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2069213
11 X = -548687
53
Y = -19378477
87 feet Y = -5913153
97 meter
Z = -10747418
39 Z = -3278678
55
XDOT = 18496
307386 XDOT = 5637
868876
YDOT = 6624
924584 feet/sec YDOT = 2082
322584 meter/sec
ZDOT = -15664
043448 ZDOT = -4747
011703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18439390
93 X = 5620326
36
Y = 6289219
87 feet Y = 1916954
22 meter
Z = -10758653
49 Z = -3279237
59
XDOT = -13337
145583 XDOT = -4065
161974
YDOT = 12768
049057 feet/sec YDOT = 3891
701352 meter/sec
ZDOT = -15552
322228 ZDOT = -4740
347815
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 11331
52542702
00016717 00000-0 10270-3 0 9069
2 25544 51
6424 58
8265 0030472 97
7898 262
6719 15
58697825 26414
Satellite: ISS
Catalog Number: 25544
Epoch time: 11331
52542702 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 58
8265 deg
Eccentricity:
0030472
Arg of perigee: 97
7898 deg
Mean anomaly: 262
6719 deg
Mean motion: 15
58697825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2641
Checksum: 337
Coasting Arc #8 (Orbit 2656)
---------------------------------------
Vector Time (GMT): 2011/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1961990
79 A = 6764869
34 meter
Y = 4005430
27 meter E =
0035399
Z = 5059259
53 I = 51
90543
XDOT = -5531
930354 Wp = 104
46075
YDOT = -5035
391765 meter/sec RA = 53
31770 deg
ZDOT = 1822
008320 TA = 327
93215
MA = 328
14703
Ha = 224
873 n
mi
Hp = 196
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6436977
64 X = -2031211
53
Y = 13141175
43 feet Y = 3983102
53 meter
Z = 16598620
50 Z = 5049560
42
XDOT = -18149
377803 XDOT = -5484
063474
YDOT = -16520
314189 feet/sec YDOT = -5096
985751 meter/sec
ZDOT = 5977
717586 ZDOT = 1795
249860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9395832
79 X = -2863849
83
Y = -11276877
90 feet Y = -3437192
38 meter
Z = 16558675
25 Z = 5047084
22
XDOT = 21623
025333 XDOT = 6590
698121
YDOT = -9305
701048 feet/sec YDOT = -2836
377680 meter/sec
ZDOT = 5868
810895 ZDOT = 1788
813561
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 11332
55121685
00016717 00000-0 10270-3 0 9077
2 25544 51
6426 53
6775 0030394 101
4264 259
0307 15
58785705 26573
Satellite: ISS
Catalog Number: 25544
Epoch time: 11332
55121685 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 53
6775 deg
Eccentricity:
0030394
Arg of perigee: 101
4264 deg
Mean anomaly: 259
0307 deg
Mean motion: 15
58785705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2657
Checksum: 314
Coasting Arc #9 (Orbit 2671)
---------------------------------------
Vector Time (GMT): 2011/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4365992
11 A = 6764957
64 meter
Y = -1100799
69 meter E =
0043512
Z = -5088146
76 I = 51
88598
XDOT = 3759
283904 Wp = 104
04306
YDOT = 6393
256759 meter/sec RA = 48
28694 deg
ZDOT = 1845
544740 TA = 183
81369
MA = 183
84697
Ha = 224
755 n
mi
Hp = 196
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14324121
10 X = 4402694
30
Y = -3611547
55 feet Y = -1051770
85 meter
Z = -16693394
90 Z = -5066847
70
XDOT = 12333
608609 XDOT = 3678
548509
YDOT = 20975
251833 feet/sec YDOT = 6434
843804 meter/sec
ZDOT = 6054
936812 ZDOT = 1863
611796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2251065
24 X = -686124
68
Y = 14698874
11 feet Y = 4480216
83 meter
Z = -16606292
76 Z = -5061598
03
XDOT = -23028
087373 XDOT = -7018
961031
YDOT = 3385
763790 feet/sec YDOT = 1031
980803 meter/sec
ZDOT = 6128
225692 ZDOT = 1867
883191
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 11333
51286797
00016717 00000-0 10270-3 0 9081
2 25544 51
6419 48
8503 0030430 104
5225 255
9309 15
58803011 26727
Satellite: ISS
Catalog Number: 25544
Epoch time: 11333
51286797 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 48
8503 deg
Eccentricity:
0030430
Arg of perigee: 104
5225 deg
Mean anomaly: 255
9309 deg
Mean motion: 15
58803011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2672
Checksum: 302
Coasting Arc #10 (Orbit 2687)
---------------------------------------
Vector Time (GMT): 2011/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5650409
70 A = 6771453
51 meter
Y = -1930774
11 meter E =
0043157
Z = 3145464
47 I = 51
88747
XDOT = -713
814166 Wp = 103
73077
YDOT = -5918
804079 meter/sec RA = 43
27344 deg
ZDOT = -4869
785437 TA = 39
94501
MA = 39
62828
Ha = 224
717 n
mi
Hp = 196
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18538089
56 X = -5643679
55
Y = -6334560
73 feet Y = -1993923
03 meter
Z = 10319765
33 Z = 3118030
99
XDOT = -2341
909993 XDOT = -623
919323
YDOT = -19418
648553 feet/sec YDOT = -5926
283441 meter/sec
ZDOT = -15976
986342 ZDOT = -4873
035178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12783577
10 X = 3896434
30
Y = -14921962
04 feet Y = -4548214
03 meter
Z = 10207849
24 Z = 3111352
45
XDOT = 17778
155230 XDOT = 5418
781714
YDOT = 4188
643844 feet/sec YDOT = 1276
698644 meter/sec
ZDOT = -15989
777448 ZDOT = -4873
684166
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 11334
53859713
00016717 00000-0 10270-3 0 9099
2 25544 51
6419 43
6996 0030409 108
0939 252
3532 15
58866858 26887
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
53859713 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 43
6996 deg
Eccentricity:
0030409
Arg of perigee: 108
0939 deg
Mean anomaly: 252
3532 deg
Mean motion: 15
58866858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2688
Checksum: 350
Coasting Arc #11 (Orbit 2694)
---------------------------------------
Vector Time (GMT): 2011/334/22:28:03
754
Vector Time (MET): N/A
Weight (LBS) : 886570
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1076523
23 A = 6766324
42 meter
Y = 4332805
11 meter E =
0037594
Z = 5056975
54 I = 51
85483
XDOT = -6470
159496 Wp = 108
53890
YDOT = -3755
339256 meter/sec RA = 41
13111 deg
ZDOT = 1817
508677 TA = 323
86559
MA = 324
11905
Ha = 226
369 n
mi
Hp = 196
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3531900
35 X = -1149459
40
Y = 14215239
86 feet Y = 4320358
67 meter
Z = 16591127
09 Z = 5051568
87
XDOT = -21227
557400 XDOT = -6436
514804
YDOT = -12320
666849 feet/sec YDOT = -3827
504534 meter/sec
ZDOT = 5962
954977 ZDOT = 1786
158120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7629891
12 X = 2325590
81
Y = 12533011
05 feet Y = 3820061
77 meter
Z = 16568683
05 Z = 5050134
59
XDOT = -22758
310485 XDOT = -6936
733036
YDOT = 6042
170554 feet/sec YDOT = 1841
653585 meter/sec
ZDOT = 5835
187211 ZDOT = 1778
565062
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 11334
98736947
00016717 00000-0 10270-3 0 9103
2 25544 51
6416 41
4481 0032466 106
4619 254
0108 15
58280490 26959
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
98736947 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 41
4481 deg
Eccentricity:
0032466
Arg of perigee: 106
4619 deg
Mean anomaly: 254
0108 deg
Mean motion: 15
58280490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2695
Checksum: 316
Coasting Arc #12 (Orbit 2709)
---------------------------------------
Vector Time (GMT): 2011/335/22:28:03
754
Vector Time (MET): N/A
Weight (LBS) : 886570
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3904637
83 A = 6766244
37 meter
Y = -2146267
18 meter E =
0045750
Z = -5133145
10 I = 51
83177
XDOT = 5156
457449 Wp = 107
31526
YDOT = 5384
790574 meter/sec RA = 36
10061 deg
ZDOT = 1669
937643 TA = 178
83152
MA = 178
82079
Ha = 226
256 n
mi
Hp = 196
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12810491
56 X = 3953283
57
Y = -7041558
98 feet Y = -2102330
91 meter
Z = -16841027
24 Z = -5114058
25
XDOT = 16917
511316 XDOT = 5087
748135
YDOT = 17666
635741 feet/sec YDOT = 5442
068998 meter/sec
ZDOT = 5478
798040 ZDOT = 1694
821118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3742398
25 X = 1140682
99
Y = -14223674
41 feet Y = -4335375
96 meter
Z = -16762875
27 Z = -5109324
38
XDOT = 23399
863653 XDOT = 7132
278441
YDOT = -423
078937 feet/sec YDOT = -128
954460 meter/sec
ZDOT = 5580
006590 ZDOT = 1700
786009
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
94933027
00016717 00000-0 10270-3 0 9119
2 25544 51
6425 36
6217 0032431 109
6989 250
7670 15
58292535 27107
Satellite: ISS
Catalog Number: 25544
Epoch time: 11335
94933027 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 36
6217 deg
Eccentricity:
0032431
Arg of perigee: 109
6989 deg
Mean anomaly: 250
7670 deg
Mean motion: 15
58292535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2710
Checksum: 310
Coasting Arc #13 (Orbit 2725)
---------------------------------------
Vector Time (GMT): 2011/336/22:28:03
754
Vector Time (MET): N/A
Weight (LBS) : 886570
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5812867
13 A = 6772289
53 meter
Y = -379116
64 meter E =
0044307
Z = 3404661
14 I = 51
82695
XDOT = -2364
729582 Wp = 106
62193
YDOT = -5678
280498 meter/sec RA = 31
08558 deg
ZDOT = -4632
524979 TA = 33
44685
MA = 33
16778
Ha = 226
307 n
mi
Hp = 196
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19071086
37 X = -5824735
06
Y = -1243820
99 feet Y = -444186
17 meter
Z = 11170148
10 Z = 3376393
24
XDOT = -7758
299155 XDOT = -2278
554081
YDOT = -18629
529193 feet/sec YDOT = -5704
242353 meter/sec
ZDOT = -15198
572767 ZDOT = -4643
803783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13814747
67 X = -4210735
09
Y = 13303080
02 feet Y = 4054778
79 meter
Z = 11054702
33 Z = 3369473
27
XDOT = -17961
300480 XDOT = -5474
604386
YDOT = -5882
123126 feet/sec YDOT = -1792
871129 meter/sec
ZDOT = -15244
173043 ZDOT = -4646
423943
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
97539246
00016717 00000-0 10270-3 0 9129
2 25544 51
6422 31
4738 0032525 113
4279 247
0301 15
58328228 27260
Satellite: ISS
Catalog Number: 25544
Epoch time: 11336
97539246 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 31
4738 deg
Eccentricity:
0032525
Arg of perigee: 113
4279 deg
Mean anomaly: 247
0301 deg
Mean motion: 15
58328228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2726
Checksum: 303
Coasting Arc #14 (Orbit 2740)
---------------------------------------
Vector Time (GMT): 2011/337/22:28:03
754
Vector Time (MET): N/A
Weight (LBS) : 886570
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6267023
24 A = 6776783
01 meter
Y = 2519707
95 meter E =
0036525
Z = -628541
50 I = 51
81714
XDOT = -1282
842188 Wp = 99
83418
YDOT = 4610
791887 meter/sec RA = 26
09972 deg
ZDOT = 5982
663984 TA = 253
39641
MA = 253
79782
Ha = 226
024 n
mi
Hp = 196
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20561099
87 X = 6241434
95
Y = 8266758
36 feet Y = 2589646
60 meter
Z = -2062144
02 Z = -598158
10
XDOT = -4208
799831 XDOT = -1363
368579
YDOT = 15127
269969 feet/sec YDOT = 4595
995886 meter/sec
ZDOT = 19628
162678 ZDOT = 5976
236456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19802490
23 X = 6035799
02
Y = -9972720
72 feet Y = -3039685
27 meter
Z = -1938241
95 Z = -590776
15
XDOT = 7763
895719 XDOT = 2366
435415
YDOT = 11803
414249 feet/sec YDOT = 3597
680663 meter/sec
ZDOT = 19601
516613 ZDOT = 5974
542264
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
93729719
00016717 00000-0 10270-3 0 9133
2 25544 51
6430 26
6481 0032364 116
9891 243
4575 15
58396930 27414
Satellite: ISS
Catalog Number: 25544
Epoch time: 11337
93729719 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 26
6481 deg
Eccentricity:
0032364
Arg of perigee: 116
9891 deg
Mean anomaly: 243
4575 deg
Mean motion: 15
58396930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2741
Checksum: 331
Coasting Arc #15 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2011/338/22:28:03
754
Vector Time (MET): N/A
Weight (LBS) : 886570
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4864306
79 A = 6774195
56 meter
Y = -3992157
13 meter E =
0037442
Z = -2503593
89 I = 51
78137
XDOT = 4856
220186 Wp = 121
68318
YDOT = -2623
371396 meter/sec RA = 21
11831 deg
ZDOT = -5329
681793 TA = 86
38518
MA = 85
95706
Ha = 225
872 n
mi
Hp = 196
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15959011
76 X = -4807142
02
Y = -13097628
37 feet Y = -4046233
05 meter
Z = -8213890
70 Z = -2527086
28
XDOT = 15932
480926 XDOT = 4911
085239
YDOT = -8606
861536 feet/sec YDOT = -2568
759154 meter/sec
ZDOT = -17485
832655 ZDOT = -5305
956858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20285231
66 X = -6182938
61
Y = 3628681
21 feet Y = 1106022
03 meter
Z = -8309511
11 Z = -2532738
99
XDOT = 4101
753865 XDOT = 1250
214578
YDOT = -16313
638849 feet/sec YDOT = -4972
397121 meter/sec
ZDOT = -17388
696127 ZDOT = -5300
074580
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
96330126
00016717 00000-0 10270-3 0 9148
2 25544 51
6434 21
4992 0032251 120
9791 239
4539 15
58399077 27574
Satellite: ISS
Catalog Number: 25544
Epoch time: 11338
96330126 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 21
4992 deg
Eccentricity:
0032251
Arg of perigee: 120
9791 deg
Mean anomaly: 239
4539 deg
Mean motion: 15
58399077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2757
Checksum: 326
Coasting Arc #16 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2011/339/22:28:03
754
Vector Time (MET): N/A
Weight (LBS) : 886570
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2089467
74 A = 6767421
33 meter
Y = 4425539
30 meter E =
0040265
Z = 4654663
63 I = 51
73059
XDOT = -7126
411357 Wp = 122
18766
YDOT = 301
271677 meter/sec RA = 16
10935 deg
ZDOT = 2873
442538 TA = 299
19035
MA = 299
59257
Ha = 225
752 n
mi
Hp = 196
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6855209
11 X = 2017213
37
Y = 14519485
88 feet Y = 4448500
74 meter
Z = 15271206
13 Z = 4664639
15
XDOT = -23380
614688 XDOT = -7143
209431
YDOT = 988
424136 feet/sec YDOT = 221
485682 meter/sec
ZDOT = 9427
304914 ZDOT = 2838
781180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15512354
34 X = 4728165
60
Y = 3992719
76 feet Y = 1216980
98 meter
Z = 15311569
16 Z = 4666966
28
XDOT = -13823
391125 XDOT = -4213
369615
YDOT = 17605
406771 feet/sec YDOT = 5366
127984 meter/sec
ZDOT = 9285
698170 ZDOT = 2830
280802
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
98927620
00016717 00000-0 10270-3 0 9153
2 25544 51
6433 16
3518 0032291 124
3782 236
0435 15
58467489 27731
Satellite: ISS
Catalog Number: 25544
Epoch time: 11339
98927620 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 16
3518 deg
Eccentricity:
0032291
Arg of perigee: 124
3782 deg
Mean anomaly: 236
0435 deg
Mean motion: 15
58467489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 328
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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