[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 27th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 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
032/21:57:47
723 3
1 4
9 4
9
N/A 0
4 -0
0 219
2
000/00:01:35
446 -3
8 -0
1 205
3
Coasting Arc #1 (Orbit 3561)
---------------------------------------
Vector Time (GMT): 2012/025/13:37:03
621
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -298352
19 A = 6769726
20 meter
Y = 5758800
21 meter E =
0019104
Z = -3522395
46 I = 51
93859
XDOT = -5689
385194 Wp = 333
37942
YDOT = 2476
630058 meter/sec RA = 121
53963 deg
ZDOT = 4538
168213 TA = 345
16290
MA = 345
21888
Ha = 217
803 n
mi
Hp = 204
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -978845
78 X = -345615
50
Y = 18893701
48 feet Y = 5755199
60 meter
Z = -11556415
56 Z = -3523959
58
XDOT = -18665
961922 XDOT = -5738
701362
YDOT = 8125
426699 feet/sec YDOT = 2412
732090 meter/sec
ZDOT = 14889
003324 ZDOT = 4510
410358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10851563
20 X = -3307556
46
Y = 15492468
34 feet Y = 4722104
35 meter
Z = -11563210
46 Z = -3524466
55
XDOT = -19068
675531 XDOT = -5812
132302
YDOT = -2346
347722 feet/sec YDOT = -715
166786 meter/sec
ZDOT = 14775
070097 ZDOT = 4503
441366
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 12025
57480512
00016717 00000-0 10270-3 0 9009
2 25544 51
6420 122
4687 0022301 321
8167 38
1407 15
59055017 35623
Satellite: ISS
Catalog Number: 25544
Epoch time: 12025
57480512 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 122
4687 deg
Eccentricity:
0022301
Arg of perigee: 321
8167 deg
Mean anomaly: 38
1407 deg
Mean motion: 15
59055017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3562
Checksum: 276
Coasting Arc #2 (Orbit 3577)
---------------------------------------
Vector Time (GMT): 2012/026/13:37:03
621
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2689240
98 A = 6774820
37 meter
Y = -6207931
14 meter E =
0010604
Z = 473376
37 I = 51
97082
XDOT = 4508
880337 Wp = 346
41012
YDOT = 1496
100990 meter/sec RA = 116
55903 deg
ZDOT = -6011
988567 TA = 188
50609
MA = 188
52408
Ha = 218
027 n
mi
Hp = 204
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8822969
08 X = 2756159
93
Y = -20367228
14 feet Y = -6177484
22 meter
Z = 1553072
07 Z = 486602
90
XDOT = 14792
914491 XDOT = 4521
019762
YDOT = 4908
467814 feet/sec YDOT = 1546
589868 meter/sec
ZDOT = -19724
371939 ZDOT = -5990
055649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18104987
30 X = 5518400
13
Y = -12833764
99 feet Y = -3911731
57 meter
Z = 1607703
12 Z = 490027
91
XDOT = 9262
929718 XDOT = 2823
340978
YDOT = 10614
693920 feet/sec YDOT = 3235
358707 meter/sec
ZDOT = -19634
573890 ZDOT = -5984
618122
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 12026
60038392
00016717 00000-0 10270-3 0 9010
2 25544 51
6418 117
3180 0022410 326
2115 33
7611 15
59092896 35785
Satellite: ISS
Catalog Number: 25544
Epoch time: 12026
60038392 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 117
3180 deg
Eccentricity:
0022410
Arg of perigee: 326
2115 deg
Mean anomaly: 33
7611 deg
Mean motion: 15
59092896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3578
Checksum: 289
Coasting Arc #3 (Orbit 3593)
---------------------------------------
Vector Time (GMT): 2012/027/13:37:03
621
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4143402
66 A = 6771647
35 meter
Y = 4556276
40 meter E =
0021970
Z = 2783288
63 I = 51
97260
XDOT = -2279
817283 Wp = 5
56785
YDOT = -5217
424589 meter/sec RA = 111
58482 deg
ZDOT = 5164
998892 TA = 25
95384
MA = 25
84382
Ha = 218
323 n
mi
Hp = 203
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13593840
76 X = -4207564
24
Y = 14948413
38 feet Y = 4509583
63 meter
Z = 9131524
38 Z = 2763004
62
XDOT = -7479
715496 XDOT = -2246
395484
YDOT = -17117
534742 feet/sec YDOT = -5242
731938 meter/sec
ZDOT = 16945
534421 ZDOT = 5154
005132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19324922
53 X = -5890236
39
Y = 6025953
41 feet Y = 1836710
60 meter
Z = 9048069
48 Z = 2757851
58
XDOT = 2523
442241 XDOT = 769
145195
YDOT = -17195
270434 feet/sec YDOT = -5241
118428 meter/sec
ZDOT = 16900
827462 ZDOT = 5151
372210
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 12027
62593809
00016717 00000-0 10270-3 0 9023
2 25544 51
6415 112
1663 0022380 330
2478 29
7404 15
59105576 35947
Satellite: ISS
Catalog Number: 25544
Epoch time: 12027
62593809 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 112
1663 deg
Eccentricity:
0022380
Arg of perigee: 330
2478 deg
Mean anomaly: 29
7404 deg
Mean motion: 15
59105576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3594
Checksum: 304
Coasting Arc #4 (Orbit 3608)
---------------------------------------
Vector Time (GMT): 2012/028/13:37:03
621
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4433311
96 A = 6764555
99 meter
Y = -1356173
75 meter E =
0023667
Z = -4935869
28 I = 51
95908
XDOT = -320
383532 Wp = 4
46917
YDOT = 7315
690199 meter/sec RA = 106
57981 deg
ZDOT = -2275
551694 TA = 243
27413
MA = 243
51655
Ha = 218
476 n
mi
Hp = 203
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14544986
75 X = 4472124
44
Y = -4449388
93 feet Y = -1306380
80 meter
Z = -16193796
84 Z = -4914238
49
XDOT = -1051
127072 XDOT = -391
111288
YDOT = 24001
608264 feet/sec YDOT = 7311
711972 meter/sec
ZDOT = -7465
720781 ZDOT = -2277
280002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14947641
97 X = 4556041
27
Y = 3284600
99 feet Y = 1001146
38 meter
Z = -16105035
03 Z = -4908814
68
XDOT = -12382
815588 XDOT = -3774
282191
YDOT = 19348
820510 feet/sec YDOT = 5897
520491 meter/sec
ZDOT = -7473
314078 ZDOT = -2277
866131
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 12028
58737282
00016717 00000-0 10270-3 0 9035
2 25544 51
6413 107
3373 0022411 333
8926 26
1097 15
59135598 36094
Satellite: ISS
Catalog Number: 25544
Epoch time: 12028
58737282 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 107
3373 deg
Eccentricity:
0022411
Arg of perigee: 333
8926 deg
Mean anomaly: 26
1097 deg
Mean motion: 15
59135598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3609
Checksum: 313
Coasting Arc #5 (Orbit 3624)
---------------------------------------
Vector Time (GMT): 2012/029/13:37:03
621
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3600379
49 A = 6763390
73 meter
Y = -2515143
78 meter E =
0024023
Z = 5152713
78 I = 51
96352
XDOT = 2666
877970 Wp = 349
00361
YDOT = -7022
796969 meter/sec RA = 101
54884 deg
ZDOT = -1542
734074 TA = 115
91835
MA = 115
67056
Ha = 218
602 n
mi
Hp = 203
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11812268
66 X = -3597017
45
Y = -8251784
07 feet Y = -2555386
60 meter
Z = 16905228
94 Z = 5135231
72
XDOT = 8749
599640 XDOT = 2752
704238
YDOT = -23040
672469 feet/sec YDOT = -6992
494430 meter/sec
ZDOT = -5061
463496 ZDOT = -1529
570138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6576019
85 X = -2004370
85
Y = -12914698
39 feet Y = -3936400
07 meter
Z = 16833743
64 Z = 5130925
06
XDOT = 17715
992956 XDOT = 5399
834653
YDOT = -15640
794144 feet/sec YDOT = -4767
314055 meter/sec
ZDOT = -5007
001785 ZDOT = -1526
134144
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 12029
61287766
00016717 00000-0 10270-3 0 9048
2 25544 51
6412 102
1856 0022498 337
8627 22
1555 15
59208794 36251
Satellite: ISS
Catalog Number: 25544
Epoch time: 12029
61287766 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 102
1856 deg
Eccentricity:
0022498
Arg of perigee: 337
8627 deg
Mean anomaly: 22
1555 deg
Mean motion: 15
59208794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3625
Checksum: 323
Coasting Arc #6 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2012/030/13:37:03
621
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1979873
75 A = 6769787
57 meter
Y = 5540286
18 meter E =
0021791
Z = -3323791
32 I = 51
99083
XDOT = -4222
962164 Wp = 354
22670
YDOT = 4339
432588 meter/sec RA = 96
53648 deg
ZDOT = 4736
178122 TA = 327
14417
MA = 327
27946
Ha = 218
768 n
mi
Hp = 203
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6495648
79 X = 1933920
05
Y = 18176791
94 feet Y = 5562169
42 meter
Z = -10904827
15 Z = -3314284
90
XDOT = -13854
862744 XDOT = -4294
179723
YDOT = 14236
983558 feet/sec YDOT = 4291
810616 meter/sec
ZDOT = 15538
642134 ZDOT = 4715
490428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2514762
77 X = -766499
69
Y = 19159980
69 feet Y = 5839962
12 meter
Z = -10866258
86 Z = -3312035
70
XDOT = -17531
171497 XDOT = -5343
501072
YDOT = 6428
782680 feet/sec YDOT = 1959
492961 meter/sec
ZDOT = 15453
518340 ZDOT = 4710
232390
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 12030
57426841
00016717 00000-0 10270-3 0 9055
2 25544 51
6415 97
3559 0022438 342
0628 17
9733 15
59248160 36400
Satellite: ISS
Catalog Number: 25544
Epoch time: 12030
57426841 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 97
3559 deg
Eccentricity:
0022438
Arg of perigee: 342
0628 deg
Mean anomaly: 17
9733 deg
Mean motion: 15
59248160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3640
Checksum: 309
Coasting Arc #7 (Orbit 3655)
---------------------------------------
Vector Time (GMT): 2012/031/13:37:03
621
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 78864
20 A = 6774372
13 meter
Y = -6781582
60 meter E =
0013876
Z = 135414
37 I = 52
00910
XDOT = 4717
361844 Wp = 14
85952
YDOT = -68
643643 meter/sec RA = 91
55981 deg
ZDOT = -6035
295184 TA = 163
68903
MA = 163
64433
Ha = 218
906 n
mi
Hp = 202
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 258740
82 X = 154033
55
Y = -22249286
73 feet Y = -6780280
39 meter
Z = 444272
85 Z = 135979
97
XDOT = 15476
908938 XDOT = 4747
096594
YDOT = -225
208801 feet/sec YDOT = -15
724856 meter/sec
ZDOT = -19800
837218 ZDOT = -6012
306490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10101919
76 X = 3079065
14
Y = -19825398
03 feet Y = -6042781
32 meter
Z = 447096
35 Z = 136274
97
XDOT = 12631
973036 XDOT = 3850
225382
YDOT = 5981
124119 feet/sec YDOT = 1823
046631 meter/sec
ZDOT = -19706
586712 ZDOT = -6006
567630
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 12031
59972628
00016717 00000-0 10270-3 0 9068
2 25544 51
6417 92
2039 0022582 346
0788 13
9742 15
59279701 36568
Satellite: ISS
Catalog Number: 25544
Epoch time: 12031
59972628 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 92
2039 deg
Eccentricity:
0022582
Arg of perigee: 346
0788 deg
Mean anomaly: 13
9742 deg
Mean motion: 15
59279701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3656
Checksum: 330
Coasting Arc #8 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2012/032/13:37:03
621
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2096188
23 A = 6770316
66 meter
Y = 5618928
77 meter E =
0025179
Z = 3106052
31 I = 51
99462
XDOT = -4107
775373 Wp = 21
22794
YDOT = -4248
269099 meter/sec RA = 86
58488 deg
ZDOT = 4923
509698 TA = 14
48042
MA = 14
40841
Ha = 219
197 n
mi
Hp = 202
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6877257
96 X = -2173952
73
Y = 18434805
67 feet Y = 5595053
02 meter
Z = 10190460
32 Z = 3095680
50
XDOT = -13476
953322 XDOT = -4083
882081
YDOT = -13937
890746 feet/sec YDOT = -4294
071304 meter/sec
ZDOT = 16153
247042 ZDOT = 4903
612484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14165250
68 X = -4317568
41
Y = 13687875
45 feet Y = 4172064
44 meter
Z = 10147509
91 Z = 3092961
02
XDOT = -5300
459963 XDOT = -1615
580197
YDOT = -17374
637239 feet/sec YDOT = -5295
789430 meter/sec
ZDOT = 16071
994825 ZDOT = 4898
744023
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 12032
62516120
00016717 00000-0 10270-3 0 9075
2 25544 51
6411 87
0517 0022613 350
4516 9
6207 15
59273892 36729
Satellite: ISS
Catalog Number: 25544
Epoch time: 12032
62516120 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 87
0517 deg
Eccentricity:
0022613
Arg of perigee: 350
4516 deg
Mean anomaly: 9
6207 deg
Mean motion: 15
59273892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3672
Checksum: 288
Coasting Arc #9 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2012/032/21:58:35
446
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 266321
79 A = 6776465
40 meter
Y = -6687157
36 meter E =
0011216
Z = -1110998
12 I = 52
00753
XDOT = 4737
459569 Wp = 8
17843
YDOT = 1170
409483 meter/sec RA = 84
83046 deg
ZDOT = -5905
627395 TA = 183
81509
MA = 183
82365
Ha = 219
156 n
mi
Hp = 205
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 873759
15 X = 346476
04
Y = -21939492
64 feet Y = -6683730
98 meter
Z = -3645006
94 Z = -1109509
86
XDOT = 15542
846355 XDOT = 4752
707549
YDOT = 3839
926126 feet/sec YDOT = 1223
472101 meter/sec
ZDOT = -19375
417962 ZDOT = -5882
576257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21742593
06 X = -6627142
37
Y = 3067998
49 feet Y = 935125
94 meter
Z = -3638392
53 Z = -1108982
04
XDOT = 1180
980769 XDOT = 359
962938
YDOT = -14509
803459 feet/sec YDOT = -4422
588094 meter/sec
ZDOT = -19280
999775 ZDOT = -5876
848731
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 12032
94562061
00016717 00000-0 10270-3 0 9086
2 25544 51
6428 85
4429 0019018 347
2337 12
8334 15
58379112 36774
Satellite: ISS
Catalog Number: 25544
Epoch time: 12032
94562061 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 85
4429 deg
Eccentricity:
0019018
Arg of perigee: 347
2337 deg
Mean anomaly: 12
8334 deg
Mean motion: 15
58379112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3677
Checksum: 314
Coasting Arc #10 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2012/033/21:58:35
446
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2125700
89 A = 6770622
27 meter
Y = 5142319
22 meter E =
0019284
Z = 3835835
74 I = 51
98478
XDOT = -4209
269669 Wp = 25
72241
YDOT = -4868
443061 meter/sec RA = 79
85144 deg
ZDOT = 4203
057911 TA = 20
36535
MA = 20
28856
Ha = 219
397 n
mi
Hp = 204
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6974084
28 X = -2201678
68
Y = 16871126
04 feet Y = 5118123
36 meter
Z = 12584762
93 Z = 3825324
99
XDOT = -13809
939859 XDOT = -4174
934109
YDOT = -15972
582221 feet/sec YDOT = -4915
321880 meter/sec
ZDOT = 13789
560077 ZDOT = 4182
693007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17929742
00 X = 5464985
36
Y = 3590266
70 feet Y = 1094313
29 meter
Z = 12541265
50 Z = 3822577
72
XDOT = -12661
778051 XDOT = -3859
309950
YDOT = 15458
705575 feet/sec YDOT = 4711
813459 meter/sec
ZDOT = 13706
441268 ZDOT = 4177
723299
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 12033
97162268
00016717 00000-0 10270-3 0 9096
2 25544 51
6429 80
2946 0019144 351
4965 8
5863 15
58422398 36938
Satellite: ISS
Catalog Number: 25544
Epoch time: 12033
97162268 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 80
2946 deg
Eccentricity:
0019144
Arg of perigee: 351
4965 deg
Mean anomaly: 8
5863 deg
Mean motion: 15
58422398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 338
Coasting Arc #11 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2012/034/21:58:35
446
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3657060
35 A = 6765045
94 meter
Y = -2221162
86 meter E =
0024514
Z = -5253938
13 I = 51
96062
XDOT = 2764
224910 Wp = 30
45716
YDOT = 7070
844231 meter/sec RA = 74
84072 deg
ZDOT = -1046
773034 TA = 229
44895
MA = 229
66265
Ha = 219
413 n
mi
Hp = 204
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11998229
49 X = 3707147
99
Y = -7287279
72 feet Y = -2179987
10 meter
Z = -17237329
83 Z = -5236051
07
XDOT = 9068
979365 XDOT = 2690
036760
YDOT = 23198
307844 feet/sec YDOT = 7101
340727 meter/sec
ZDOT = -3434
294732 ZDOT = -1033
524735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9706555
25 X = -2958558
04
Y = -10265179
64 feet Y = -3128826
75 meter
Z = -17163809
85 Z = -5231529
24
XDOT = 19970
756904 XDOT = 6087
086704
YDOT = -13129
983853 feet/sec YDOT = -4002
019078 meter/sec
ZDOT = -3380
532722 ZDOT = -1030
386374
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 12034
93347680
00016717 00000-0 10270-3 0 9108
2 25544 51
6433 75
4687 0019192 354
8530 5
2424 15
58490996 37082
Satellite: ISS
Catalog Number: 25544
Epoch time: 12034
93347680 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 75
4687 deg
Eccentricity:
0019192
Arg of perigee: 354
8530 deg
Mean anomaly: 5
2424 deg
Mean motion: 15
58490996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3708
Checksum: 324
Coasting Arc #12 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2012/035/21:58:35
446
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4532562
01 A = 6766618
63 meter
Y = -1337690
42 meter E =
0023514
Z = 4847012
76 I = 51
95737
XDOT = -570
213837 Wp = 13
79345
YDOT = -7229
269512 meter/sec RA = 69
81701 deg
ZDOT = -2503
614517 TA = 100
81895
MA = 100
55419
Ha = 219
519 n
mi
Hp = 204
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14870610
27 X = -4540811
97
Y = -4388748
11 feet Y = -1388422
61 meter
Z = 15902272
83 Z = 4824974
21
XDOT = -1870
780305 XDOT = -477
170607
YDOT = -23718
075827 feet/sec YDOT = -7235
125681 meter/sec
ZDOT = -8213
958388 ZDOT = -2506
158762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -819769
15 X = -249865
64
Y = 15575197
85 feet Y = 4747320
30 meter
Z = 15812009
10 Z = 4819500
37
XDOT = -21524
340636 XDOT = -6560
619026
YDOT = 7298
891771 feet/sec YDOT = 2224
702212 meter/sec
ZDOT = -8223
811098 ZDOT = -2506
617623
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 12035
95943105
00016717 00000-0 10270-3 0 9116
2 25544 51
6432 70
3199 0019261 358
3728 1
7361 15
58548497 37247
Satellite: ISS
Catalog Number: 25544
Epoch time: 12035
95943105 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 70
3199 deg
Eccentricity:
0019261
Arg of perigee: 358
3728 deg
Mean anomaly: 1
7361 deg
Mean motion: 15
58548497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3724
Checksum: 317
Coasting Arc #13 (Orbit 3738)
---------------------------------------
Vector Time (GMT): 2012/036/21:58:35
446
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4421724
38 A = 6773306
23 meter
Y = 4296114
31 meter E =
0022278
Z = -2778687
89 I = 51
96799
XDOT = -1956
985490 Wp = 12
07485
YDOT = 5338
447842 meter/sec RA = 64
81739 deg
ZDOT = 5168
235966 TA = 316
48049
MA = 316
65607
Ha = 219
697 n
mi
Hp = 203
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14506969
75 X = 4386853
62
Y = 14094863
22 feet Y = 4345365
82 meter
Z = -9116430
09 Z = -2757292
56
XDOT = -6420
556071 XDOT = -2041
641091
YDOT = 17514
592657 feet/sec YDOT = 5316
090211 meter/sec
ZDOT = 16956
154744 ZDOT = 5158
523732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10057037
50 X = 3065385
03
Y = -17594290
76 feet Y = -5362739
82 meter
Z = -9029040
23 Z = -2752051
46
XDOT = 17301
531754 XDOT = 5273
506879
YDOT = 1257
480442 feet/sec YDOT = 383
280039 meter/sec
ZDOT = 16915
895535 ZDOT = 5155
964959
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 12036
92124288
00016717 00000-0 10270-3 0 9128
2 25544 51
6430 65
4932 0019270 1
9646 358
1582 15
58536310 37396
Satellite: ISS
Catalog Number: 25544
Epoch time: 12036
92124288 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 65
4932 deg
Eccentricity:
0019270
Arg of perigee: 1
9646 deg
Mean anomaly: 358
1582 deg
Mean motion: 15
58536310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3739
Checksum: 308
Coasting Arc #14 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2012/037/21:58:35
446
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3189117
65 A = 6776453
05 meter
Y = -5979390
28 meter E =
0014334
Z = -314566
06 I = 51
96450
XDOT = 4297
760704 Wp = 42
42810
YDOT = -1983
170334 meter/sec RA = 59
84567 deg
ZDOT = -6023
869308 TA = 140
94694
MA = 140
84336
Ha = 219
665 n
mi
Hp = 203
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10462984
40 X = -3120489
84
Y = -19617422
19 feet Y = -6014669
25 meter
Z = -1032040
89 Z = -329891
47
XDOT = 14100
264777 XDOT = 4348
879255
YDOT = -6506
464351 feet/sec YDOT = -1934
824359 meter/sec
ZDOT = -19763
350747 ZDOT = -6002
867398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16163522
19 X = -4926641
56
Y = 15261888
38 feet Y = 4651823
58 meter
Z = -1094402
95 Z = -333574
02
XDOT = -8915
852405 XDOT = -2717
551813
YDOT = -10820
444808 feet/sec YDOT = -3298
071578 meter/sec
ZDOT = -19677
063627 ZDOT = -5997
568993
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 12037
94715127
00016717 00000-0 10270-3 0 9130
2 25544 51
6426 60
3443 0019051 5
9803 354
1576 15
58546955 37551
Satellite: ISS
Catalog Number: 25544
Epoch time: 12037
94715127 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 60
3443 deg
Eccentricity:
0019051
Arg of perigee: 5
9803 deg
Mean anomaly: 354
1576 deg
Mean motion: 15
58546955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 315
Coasting Arc #15 (Orbit 3770)
---------------------------------------
Vector Time (GMT): 2012/038/21:58:35
446
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 971368
39 A = 6771780
80 meter
Y = 5830285
70 meter E =
0025171
Z = 3269663
66 I = 51
93258
XDOT = -5780
260057 Wp = 38
90971
YDOT = -1715
446509 meter/sec RA = 54
86749 deg
ZDOT = 4775
444792 TA = 359
03060
MA = 359
03547
Ha = 219
821 n
mi
Hp = 203
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3186904
18 X = 890217
94
Y = 19128233
92 feet Y = 5840694
51 meter
Z = 10727242
97 Z = 3274185
08
XDOT = -18964
107800 XDOT = -5783
845365
YDOT = -5628
105345 feet/sec YDOT = -1780
104821 meter/sec
ZDOT = 15667
469790 ZDOT = 4747
356701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17486176
51 X = 5329786
60
Y = -8360105
82 feet Y = -2548160
26 meter
Z = 10745310
35 Z = 3275170
59
XDOT = -667
176494 XDOT = -203
355395
YDOT = 18597
013717 feet/sec YDOT = 5668
369781 meter/sec
ZDOT = 15552
423179 ZDOT = 4740
378585
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 12038
97303368
00016717 00000-0 10270-3 0 9145
2 25544 51
6420 55
1942 0019312 9
7924 350
3604 15
58597036 37711
Satellite: ISS
Catalog Number: 25544
Epoch time: 12038
97303368 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 55
1942 deg
Eccentricity:
0019312
Arg of perigee: 9
7924 deg
Mean anomaly: 350
3604 deg
Mean motion: 15
58597036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3771
Checksum: 310
Coasting Arc #16 (Orbit 3785)
---------------------------------------
Vector Time (GMT): 2012/039/21:58:35
446
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1740612
39 A = 6765245
39 meter
Y = -4128236
86 meter E =
0027776
Z = -5089811
96 I = 51
89198
XDOT = 5790
517865 Wp = 38
11234
YDOT = 4678
286860 meter/sec RA = 49
85646 deg
ZDOT = -1798
156402 TA = 214
43576
MA = 214
61606
Ha = 219
790 n
mi
Hp = 203
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5710670
59 X = 1811370
32
Y = -13544084
19 feet Y = -4108376
92 meter
Z = -16698858
14 Z = -5081184
27
XDOT = 18997
762025 XDOT = 5746
508772
YDOT = 15348
710171 feet/sec YDOT = 4742
793830 meter/sec
ZDOT = -5899
463262 ZDOT = -1770
134223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14659743
05 X = -4468289
68
Y = -1528894
64 feet Y = -466007
09 meter
Z = -16663140
56 Z = -5078925
24
XDOT = 8894
756130 XDOT = 2711
121669
YDOT = -21662
551102 feet/sec YDOT = -6602
745576 meter/sec
ZDOT = -5784
931051 ZDOT = -1763
246984
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 12039
93477413
00016717 00000-0 10270-3 0 9156
2 25544 51
6411 50
3664 0019210 13
1146 347
0505 15
58660070 37869
Satellite: ISS
Catalog Number: 25544
Epoch time: 12039
93477413 = yrday
fracday
Element set: 915
Inclination: 51
6411 deg
RA of node: 50
3664 deg
Eccentricity:
0019210
Arg of perigee: 13
1146 deg
Mean anomaly: 347
0505 deg
Mean motion: 15
58660070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3786
Checksum: 289
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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