[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 6th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 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
018/02:17:47
723 4
3 4
9 4
9
N/A 0
5 -0
0 216
2
000/00:01:35
445 -2
5 0
0 206
8
Coasting Arc #1 (Orbit 3233)
---------------------------------------
Vector Time (GMT): 2012/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2918841
87 A = 6763508
43 meter
Y = -3070821
00 meter E =
0022081
Z = 5289040
47 I = 51
36430
XDOT = 5331
819596 Wp = 239
66997
YDOT = 5497
207740 meter/sec RA = 227
30465 deg
ZDOT = 239
042279 TA = 207
98152
MA = 208
10041
Ha = 216
862 n
mi
Hp = 204
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9576252
87 X = 2927270
45
Y = -10074872
05 feet Y = -3038134
11 meter
Z = 17352494
99 Z = 5303240
28
XDOT = 17492
846445 XDOT = 5268
791234
YDOT = 18035
458466 feet/sec YDOT = 5556
478988 meter/sec
ZDOT = 784
259445 ZDOT = 264
791520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11911453
26 X = 3630610
95
Y = 7021356
90 feet Y = 2140109
58 meter
Z = 17410760
36 Z = 5306799
76
XDOT = -13231
981047 XDOT = -4033
107823
YDOT = 20160
067680 feet/sec YDOT = 6144
788629 meter/sec
ZDOT = 889
159107 ZDOT = 271
015696
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 12004
54850564
00016717 00000-0 10270-3 0 9001
2 25544 51
6421 228
0382 0023974 243
6914 116
1778 15
58907232 32345
Satellite: ISS
Catalog Number: 25544
Epoch time: 12004
54850564 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 228
0382 deg
Eccentricity:
0023974
Arg of perigee: 243
6914 deg
Mean anomaly: 116
1778 deg
Mean motion: 15
58907232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3234
Checksum: 300
Coasting Arc #2 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2012/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5146520
65 A = 6766980
24 meter
Y = 59832
64 meter E =
0018450
Z = -4388697
28 I = 51
39658
XDOT = -2935
272434 Wp = 227
85347
YDOT = -6262
173025 meter/sec RA = 222
23847 deg
ZDOT = 3335
572121 TA = 76
02069
MA = 75
81560
Ha = 216
507 n
mi
Hp = 204
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16884910
28 X = -5125487
91
Y = 196301
30 feet Y = 2399
17 meter
Z = -14398613
11 Z = -4413647
75
XDOT = -9630
158904 XDOT = -2881
232869
YDOT = -20545
187091 feet/sec YDOT = -6294
695265 meter/sec
ZDOT = 10943
478088 ZDOT = 3321
443258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4168453
82 X = -1270544
73
Y = -16273115
04 feet Y = -4960045
46 meter
Z = -14500638
20 Z = -4419794
52
XDOT = 16476
691453 XDOT = 5022
095555
YDOT = -13982
485122 feet/sec YDOT = -4261
861465 meter/sec
ZDOT = 10886
130962 ZDOT = 3318
092717
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 12005
51005987
00016717 00000-0 10270-3 0 9011
2 25544 51
6407 223
2083 0024068 247
4977 112
3630 15
58960285 32498
Satellite: ISS
Catalog Number: 25544
Epoch time: 12005
51005987 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 223
2083 deg
Eccentricity:
0024068
Arg of perigee: 247
4977 deg
Mean anomaly: 112
3630 deg
Mean motion: 15
58960285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 303
Coasting Arc #3 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2012/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5941696
48 A = 6773682
18 meter
Y = 2660347
55 meter E =
0016444
Z = 1849657
10 I = 51
44262
XDOT = -583
678970 Wp = 217
44204
YDOT = 5189
536970 meter/sec RA = 217
20915 deg
ZDOT = -5628
203760 TA = 302
10114
MA = 302
26066
Ha = 216
221 n
mi
Hp = 204
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19493754
86 X = 5902521
16
Y = 8728174
37 feet Y = 2726571
98 meter
Z = 6068428
80 Z = 1878426
67
XDOT = -1914
957252 XDOT = -614
325573
YDOT = 17026
039929 feet/sec YDOT = 5182
839245 meter/sec
ZDOT = -18465
235434 ZDOT = -5631
113045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3510458
61 X = -1069987
78
Y = 21033892
52 feet Y = 6411130
44 meter
Z = 6185901
73 Z = 1885462
85
XDOT = -15392
031723 XDOT = -4691
491269
YDOT = 2828
214998 feet/sec YDOT = 862
039931 meter/sec
ZDOT = -18477
482198 ZDOT = -5631
936574
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 12006
53569834
00016717 00000-0 10270-3 0 9021
2 25544 51
6407 218
0590 0024005 251
6751 108
1792 15
59001121 32657
Satellite: ISS
Catalog Number: 25544
Epoch time: 12006
53569834 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 218
0590 deg
Eccentricity:
0024005
Arg of perigee: 251
6751 deg
Mean anomaly: 108
1792 deg
Mean motion: 15
59001121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 282
Coasting Arc #4 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2012/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4891866
06 A = 6774240
94 meter
Y = -4455324
35 meter E =
0011178
Z = 1460533
54 I = 51
46780
XDOT = 4229
327800 Wp = 272
92851
YDOT = -2765
388069 meter/sec RA = 212
20180 deg
ZDOT = 5768
575214 TA = 103
06595
MA = 102
94116
Ha = 216
148 n
mi
Hp = 204
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16049429
33 X = -4848777
05
Y = -14617205
88 feet Y = -4509787
46 meter
Z = 4791776
71 Z = 1436873
36
XDOT = 13875
747376 XDOT = 4231
914363
YDOT = -9072
795501 feet/sec YDOT = -2718
079384 meter/sec
ZDOT = 18925
771701 ZDOT = 5789
126886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9730255
49 X = 2965781
87
Y = -19428954
48 feet Y = -5921945
33 meter
Z = 4695302
89 Z = 1431128
32
XDOT = 11034
923155 XDOT = 3363
444578
YDOT = 10089
128814 feet/sec YDOT = 3075
166462 meter/sec
ZDOT = 19010
012735 ZDOT = 5794
251882
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 12007
56131544
00016717 00000-0 10270-3 0 9039
2 25544 51
6390 212
9064 0024130 255
2104 104
6377 15
59029298 32811
Satellite: ISS
Catalog Number: 25544
Epoch time: 12007
56131544 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 212
9064 deg
Eccentricity:
0024130
Arg of perigee: 255
2104 deg
Mean anomaly: 104
6377 deg
Mean motion: 15
59029298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 284
Coasting Arc #5 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2012/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2182871
11 A = 6767689
27 meter
Y = 4851522
06 meter E =
0016360
Z = -4167912
61 I = 51
47094
XDOT = -6737
046720 Wp = 263
40107
YDOT = -152
047519 meter/sec RA = 207
17902 deg
ZDOT = -3694
798367 TA = 328
63008
MA = 328
72756
Ha = 215
953 n
mi
Hp = 204
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7161650
63 X = 2148704
72
Y = 15917067
11 feet Y = 4875741
72 meter
Z = -13674253
96 Z = -4157390
86
XDOT = -22103
171652 XDOT = -6716
897500
YDOT = -498
843566 feet/sec YDOT = -227
272218 meter/sec
ZDOT = -12122
041888 ZDOT = -3727
477329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13171688
32 X = -4014730
60
Y = 11502844
52 feet Y = 3506067
01 meter
Z = -13631532
61 Z = -4154891
14
XDOT = -4997
447838 XDOT = -1523
222101
YDOT = -20287
534682 feet/sec YDOT = -6183
640571 meter/sec
ZDOT = -12255
708595 ZDOT = -3735
539980
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 12008
52281400
00016717 00000-0 10270-3 0 9044
2 25544 51
6377 208
0777 0024013 259
0400 100
8054 15
59044711 32967
Satellite: ISS
Catalog Number: 25544
Epoch time: 12008
52281400 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 208
0777 deg
Eccentricity:
0024013
Arg of perigee: 259
0400 deg
Mean anomaly: 100
8054 deg
Mean motion: 15
59044711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 275
Coasting Arc #6 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2012/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1417728
12 A = 6763145
83 meter
Y = -3978116
56 meter E =
0021593
Z = 5301027
53 I = 51
48329
XDOT = 7142
575917 Wp = 261
08905
YDOT = 2764
550952 meter/sec RA = 202
12180 deg
ZDOT = 161
686183 TA = 187
34933
MA = 187
38104
Ha = 215
820 n
mi
Hp = 204
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4651338
98 X = 1436356
06
Y = -13051563
51 feet Y = -3962159
03 meter
Z = 17391822
60 Z = 5307959
52
XDOT = 23433
648022 XDOT = 7110
345883
YDOT = 9070
049056 feet/sec YDOT = 2844
243400 meter/sec
ZDOT = 530
466479 ZDOT = 196
305953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13814495
07 X = 4210658
10
Y = 376506
06 feet Y = 114759
05 meter
Z = 17420439
91 Z = 5309750
09
XDOT = -1514
514262 XDOT = -461
623947
YDOT = 24069
590520 feet/sec YDOT = 7336
411190 meter/sec
ZDOT = 671
923411 ZDOT = 204
802256
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 12009
54839239
00016717 00000-0 10270-3 0 9057
2 25544 51
6378 202
9255 0023943 262
7903 97
0530 15
59029397 33120
Satellite: ISS
Catalog Number: 25544
Epoch time: 12009
54839239 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 202
9255 deg
Eccentricity:
0023943
Arg of perigee: 262
7903 deg
Mean anomaly: 97
0530 deg
Mean motion: 15
59029397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 321
Coasting Arc #7 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2012/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4722706
56 A = 6766762
99 meter
Y = 2151502
16 meter E =
0016273
Z = -4331644
46 I = 51
52417
XDOT = -5212
662848 Wp = 253
63611
YDOT = -4467
353463 meter/sec RA = 197
06319 deg
ZDOT = 3449
116756 TA = 51
42809
MA = 51
28241
Ha = 215
537 n
mi
Hp = 204
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15494444
10 X = -4725372
31
Y = 7058734
11 feet Y = 2098675
39 meter
Z = -14211431
95 Z = -4354593
05
XDOT = -17101
912230 XDOT = -5179
075323
YDOT = -14656
671468 feet/sec YDOT = -4525
457140 meter/sec
ZDOT = 11315
999857 ZDOT = 3423
875554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11610072
85 X = -3538750
20
Y = -12346178
49 feet Y = -3763115
20 meter
Z = -14305467
77 Z = -4360306
58
XDOT = 7503
001770 XDOT = 2286
914940
YDOT = -20105
668456 feet/sec YDOT = -6128
207745 meter/sec
ZDOT = 11213
003485 ZDOT = 3417
723462
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 12010
50985031
00016717 00000-0 10270-3 0 9068
2 25544 51
6371 198
0945 0023953 266
2477 93
5940 15
59107850 33273
Satellite: ISS
Catalog Number: 25544
Epoch time: 12010
50985031 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 198
0945 deg
Eccentricity:
0023953
Arg of perigee: 266
2477 deg
Mean anomaly: 93
5940 deg
Mean motion: 15
59107850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 315
Coasting Arc #8 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2012/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6556617
64 A = 6773400
24 meter
Y = 23743
08 meter E =
0012809
Z = 1695288
06 I = 51
57704
XDOT = 1445
444813 Wp = 244
03188
YDOT = 4930
237943 meter/sec RA = 192
04287 deg
ZDOT = -5698
317268 TA = 277
33413
MA = 277
47969
Ha = 215
533 n
mi
Hp = 204
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21511212
72 X = 6547629
66
Y = 77897
26 feet Y = 97012
86 meter
Z = 5561968
70 Z = 1727117
40
XDOT = 4742
273010 XDOT = 1417
887108
YDOT = 16175
321336 feet/sec YDOT = 4946
248032 meter/sec
ZDOT = -18695
266627 ZDOT = -5691
362150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7136036
14 X = 2175063
82
Y = 20257084
24 feet Y = 6174359
28 meter
Z = 5692219
52 Z = 1734988
51
XDOT = -12128
561178 XDOT = -3696
785447
YDOT = 9482
940256 feet/sec YDOT = 2890
400190 meter/sec
ZDOT = -18667
112096 ZDOT = -5689
735767
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 12011
53538431
00016717 00000-0 10270-3 0 9071
2 25544 51
6377 192
9437 0024123 270
7587 89
0804 15
59178265 33435
Satellite: ISS
Catalog Number: 25544
Epoch time: 12011
53538431 = yrday
fracday
Element set: 907
Inclination: 51
6377 deg
RA of node: 192
9437 deg
Eccentricity:
0024123
Arg of perigee: 270
7587 deg
Mean anomaly: 89
0804 deg
Mean motion: 15
59178265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 320
Coasting Arc #9 (Orbit 3358)
---------------------------------------
Vector Time (GMT): 2012/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6214093
92 A = 6773580
59 meter
Y = -2104341
62 meter E =
0013781
Z = 1673852
88 I = 51
60696
XDOT = 2947
668330 Wp = 305
03917
YDOT = -4194
920072 meter/sec RA = 187
04459 deg
ZDOT = 5710
251650 TA = 73
34674
MA = 73
19549
Ha = 215
565 n
mi
Hp = 204
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20387447
26 X = -6198231
97
Y = -6904007
93 feet Y = -2173742
81 meter
Z = 5491643
30 Z = 1643704
06
XDOT = 9670
827855 XDOT = 2966
619046
YDOT = -13762
861129 feet/sec YDOT = -4161
851676 meter/sec
ZDOT = 18734
421425 ZDOT = 5724
616928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -722571
25 X = -220239
72
Y = -21543672
37 feet Y = -6566511
34 meter
Z = 5368384
23 Z = 1636283
51
XDOT = 14673
476719 XDOT = 4472
475704
YDOT = 4156
662264 feet/sec YDOT = 1266
950658 meter/sec
ZDOT = 18793
470735 ZDOT = 5728
249880
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 12012
56090009
00016717 00000-0 10270-3 0 9080
2 25544 51
6373 187
7904 0023895 274
0572 85
7852 15
59165700 33591
Satellite: ISS
Catalog Number: 25544
Epoch time: 12012
56090009 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 187
7904 deg
Eccentricity:
0023895
Arg of perigee: 274
0572 deg
Mean anomaly: 85
7852 deg
Mean motion: 15
59165700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3359
Checksum: 325
Coasting Arc #10 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2012/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3763939
03 A = 6766617
89 meter
Y = 3569754
22 meter E =
0016648
Z = -4335321
73 I = 51
61522
XDOT = -6383
684937 Wp = 292
54250
YDOT = 2513
289420 meter/sec RA = 182
02891 deg
ZDOT = -3456
030123 TA = 302
35134
MA = 302
51238
Ha = 215
531 n
mi
Hp = 204
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12348881
34 X = 3744801
30
Y = 11711792
04 feet Y = 3611737
98 meter
Z = -14223496
50 Z = -4317083
35
XDOT = -20943
848219 XDOT = -6394
526212
YDOT = 8245
700196 feet/sec YDOT = 2441
842586 meter/sec
ZDOT = -11338
681505 ZDOT = -3487
067623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6314924
18 X = -1924788
89
Y = 15871185
65 feet Y = 4837537
39 meter
Z = -14149063
38 Z = -4312634
52
XDOT = -14189
188330 XDOT = -4324
864603
YDOT = -15916
924423 feet/sec YDOT = -4851
478564 meter/sec
ZDOT = -11465
871323 ZDOT = -3494
797579
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 12013
52229952
00016717 00000-0 10270-3 0 9099
2 25544 51
6381 182
9617 0023722 277
9645 81
8818 15
59220187 33747
Satellite: ISS
Catalog Number: 25544
Epoch time: 12013
52229952 = yrday
fracday
Element set: 909
Inclination: 51
6381 deg
RA of node: 182
9617 deg
Eccentricity:
0023722
Arg of perigee: 277
9645 deg
Mean anomaly: 81
8818 deg
Mean motion: 15
59220187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 330
Coasting Arc #11 (Orbit 3389)
---------------------------------------
Vector Time (GMT): 2012/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 16293
05 A = 6762693
78 meter
Y = -4210550
58 meter E =
0021350
Z = 5309998
09 I = 51
63193
XDOT = 7654
746952 Wp = 284
21387
YDOT = -238
836795 meter/sec RA = 176
97816 deg
ZDOT = -208
452306 TA = 167
80076
MA = 167
74898
Ha = 215
587 n
mi
Hp = 204
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 53454
90 X = 37580
55
Y = -13814142
32 feet Y = -4210249
45 meter
Z = 17421253
59 Z = 5310128
88
XDOT = 25113
999187 XDOT = 7657
861359
YDOT = -783
585285 feet/sec YDOT = -153
219289 meter/sec
ZDOT = -683
898642 ZDOT = -171
258703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12735068
49 X = 3881648
88
Y = -5350127
93 feet Y = -1630718
99 meter
Z = 17422044
20 Z = 5310239
07
XDOT = 9974
539446 XDOT = 3040
239623
YDOT = 21964
258173 feet/sec YDOT = 6694
705891 meter/sec
ZDOT = -531
636727 ZDOT = -162
042874
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 12014
54777255
00016717 00000-0 10270-3 0 9108
2 25544 51
6378 177
8087 0023644 281
7716 78
0787 15
59183550 33905
Satellite: ISS
Catalog Number: 25544
Epoch time: 12014
54777255 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 177
8087 deg
Eccentricity:
0023644
Arg of perigee: 281
7716 deg
Mean anomaly: 78
0787 deg
Mean motion: 15
59183550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3390
Checksum: 337
Coasting Arc #12 (Orbit 3404)
---------------------------------------
Vector Time (GMT): 2012/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3760096
15 A = 6767090
30 meter
Y = 3818537
96 meter E =
0016007
Z = -4116027
11 I = 51
67911
XDOT = -6332
717354 Wp = 283
57204
YDOT = -2133
468884 meter/sec RA = 171
93280 deg
ZDOT = 3797
147002 TA = 25
49614
MA = 25
41727
Ha = 215
538 n
mi
Hp = 204
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12336273
46 X = -3782521
74
Y = 12528011
69 feet Y = 3776364
97 meter
Z = -13504025
95 Z = -4134347
75
XDOT = -20776
631738 XDOT = -6326
835382
YDOT = -6999
569828 feet/sec YDOT = -2204
252429 meter/sec
ZDOT = 12457
831371 ZDOT = 3766
397376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16380799
55 X = -4992867
70
Y = -6226281
23 feet Y = -1897770
52 meter
Z = -13579258
62 Z = -4138958
03
XDOT = -2372
118029 XDOT = -723
021575
YDOT = -20716
693319 feet/sec YDOT = -6314
448124 meter/sec
ZDOT = 12332
080382 ZDOT = 3758
818100
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 12015
50912959
00016717 00000-0 10270-3 0 9118
2 25544 51
6389 172
9788 0023680 285
2205 74
6332 15
59270048 34057
Satellite: ISS
Catalog Number: 25544
Epoch time: 12015
50912959 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 172
9788 deg
Eccentricity:
0023680
Arg of perigee: 285
2205 deg
Mean anomaly: 74
6332 deg
Mean motion: 15
59270048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3405
Checksum: 319
Coasting Arc #13 (Orbit 3420)
---------------------------------------
Vector Time (GMT): 2012/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6176873
24 A = 6773548
08 meter
Y = -2472813
47 meter E =
0010607
Z = 1282078
09 I = 51
73018
XDOT = 2835
970912 Wp = 274
89116
YDOT = 4074
874485 meter/sec RA = 166
92582 deg
ZDOT = -5844
582521 TA = 251
16305
MA = 251
27813
Ha = 215
771 n
mi
Hp = 204
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20265332
15 X = 6197837
63
Y = -8112905
07 feet Y = -2403622
71 meter
Z = 4206292
93 Z = 1312135
76
XDOT = 9304
366510 XDOT = 2818
585624
YDOT = 13369
010778 feet/sec YDOT = 4106
491095 meter/sec
ZDOT = -19175
139504 ZDOT = -5830
847614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15786602
99 X = 4811756
59
Y = 15041089
11 feet Y = 4584523
96 meter
Z = 4329505
80 Z = 1319633
37
XDOT = -7150
355809 XDOT = -2179
428451
YDOT = 12970
779026 feet/sec YDOT = 3953
493447 meter/sec
ZDOT = -19119
158155 ZDOT = -5827
519406
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 12016
53455597
00016717 00000-0 10270-3 0 9123
2 25544 51
6380 167
8268 0023825 289
3291 70
5288 15
59313465 34219
Satellite: ISS
Catalog Number: 25544
Epoch time: 12016
53455597 = yrday
fracday
Element set: 912
Inclination: 51
6380 deg
RA of node: 167
8268 deg
Eccentricity:
0023825
Arg of perigee: 289
3291 deg
Mean anomaly: 70
5288 deg
Mean motion: 15
59313465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 326
Coasting Arc #14 (Orbit 3436)
---------------------------------------
Vector Time (GMT): 2012/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6413373
33 A = 6772291
46 meter
Y = 325125
27 meter E =
0016545
Z = 2130769
05 I = 51
75686
XDOT = 1567
468606 Wp = 328
41576
YDOT = -5094
108763 meter/sec RA = 161
93789 deg
ZDOT = 5528
298149 TA = 55
22386
MA = 55
06824
Ha = 215
921 n
mi
Hp = 204
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21041251
10 X = -6426883
05
Y = 1066683
95 feet Y = 253331
31 meter
Z = 6990712
09 Z = 2099580
49
XDOT = 5142
613536 XDOT = 1597
460332
YDOT = -16712
955259 feet/sec YDOT = -5076
413030 meter/sec
ZDOT = 18137
461120 ZDOT = 5535
985331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10048889
32 X = -3062901
47
Y = -18565057
25 feet Y = -5658629
45 meter
Z = 6862987
00 Z = 2091838
44
XDOT = 15895
410018 XDOT = 4844
920974
YDOT = -1928
092655 feet/sec YDOT = -587
682641 meter/sec
ZDOT = 18169
256379 ZDOT = 5537
989344
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 12017
55995971
00016717 00000-0 10270-3 0 9132
2 25544 51
6392 162
6740 0023691 292
9735 66
8921 15
59360989 34376
Satellite: ISS
Catalog Number: 25544
Epoch time: 12017
55995971 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 162
6740 deg
Eccentricity:
0023691
Arg of perigee: 292
9735 deg
Mean anomaly: 66
8921 deg
Mean motion: 15
59360989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 352
Coasting Arc #15 (Orbit 3445)
---------------------------------------
Vector Time (GMT): 2012/018/02:18:35
445
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3189290
06 A = 6770278
23 meter
Y = -4529675
50 meter E =
0012512
Z = 3906376
34 I = 51
75945
XDOT = 6406
946668 Wp = 323
85597
YDOT = 982
288376 meter/sec RA = 158
90811 deg
ZDOT = -4088
618882 TA = 168
94446
MA = 168
91694
Ha = 216
176 n
mi
Hp = 206
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10463550
07 X = 3220728
57
Y = -14861140
09 feet Y = -4493835
42 meter
Z = 12816195
35 Z = 3921945
70
XDOT = 21020
166235 XDOT = 6415
347829
YDOT = 3222
730893 feet/sec YDOT = 1053
982085 meter/sec
ZDOT = -13414
103942 ZDOT = -4057
473897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16320675
48 X = -4974541
89
Y = 7894888
48 feet Y = 2406362
01 meter
Z = 12880237
42 Z = 3925896
37
XDOT = -16263
731526 XDOT = -4957
185369
YDOT = -11927
439221 feet/sec YDOT = -3635
483475 meter/sec
ZDOT = -13286
630215 ZDOT = -4049
764889
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 12018
13677078
00016717 00000-0 10270-3 0 9143
2 25544 51
6401 159
7817 0020163 294
0858 65
8187 15
58438114 34467
Satellite: ISS
Catalog Number: 25544
Epoch time: 12018
13677078 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 159
7817 deg
Eccentricity:
0020163
Arg of perigee: 294
0858 deg
Mean anomaly: 65
8187 deg
Mean motion: 15
58438114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 324
Coasting Arc #16 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2012/019/02:18:35
445
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5508007
88 A = 6776129
17 meter
Y = 3739648
90 meter E =
0020769
Z = -1190513
78 I = 51
80717
XDOT = -3587
090437 Wp = 324
07230
YDOT = -3398
610812 meter/sec RA = 153
91288 deg
ZDOT = 5884
889371 TA = 22
98513
MA = 22
89233
Ha = 216
422 n
mi
Hp = 206
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18070891
99 X = -5543632
81
Y = 12269189
31 feet Y = 3677855
89 meter
Z = -3905885
10 Z = -1217357
38
XDOT = -11768
669412 XDOT = -3577
407101
YDOT = -11150
297939 feet/sec YDOT = -3438
670275 meter/sec
ZDOT = 19307
379827 ZDOT = 5867
486800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21704497
56 X = 6615530
86
Y = -2265414
86 feet Y = -690498
45 meter
Z = -4016063
10 Z = -1224096
03
XDOT = 5027
312663 XDOT = 1532
324900
YDOT = 13864
199181 feet/sec YDOT = 4225
807910 meter/sec
ZDOT = 19236
326793 ZDOT = 5863
232407
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 12019
09861888
00016717 00000-0 10270-3 0 9154
2 25544 51
6402 154
9543 0020266 298
0372 61
8733 15
58462174 34613
Satellite: ISS
Catalog Number: 25544
Epoch time: 12019
09861888 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 154
9543 deg
Eccentricity:
0020266
Arg of perigee: 298
0372 deg
Mean anomaly: 61
8733 deg
Mean motion: 15
58462174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 321
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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