[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 27th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 ET - UTC (sec) : 67 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 3375)
---------------------------------------
Vector Time (GMT): 2012/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3853529
53 A = 6796052
70 meter
Y = -4501597
27 meter E =
0022372
Z = -3350302
32 I = 51
52033
XDOT = 5856
591774 Wp = 98
53919
YDOT = 1562
617242 meter/sec RA = 337
26986 deg
ZDOT = 4660
200523 TA = 222
50629
MA = 222
67973
Ha = 233
680 n
mi
Hp = 214
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12642813
41 X = 3919855
89
Y = -14769019
93 feet Y = -4458134
21 meter
Z = -10991805
50 Z = -3331420
51
XDOT = 19214
539942 XDOT = 5816
044845
YDOT = 5126
696988 feet/sec YDOT = 1627
883097 meter/sec
ZDOT = 15289
371796 ZDOT = 4688
552842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11405083
12 X = -3476269
33
Y = 15799038
68 feet Y = 4815546
99 meter
Z = -10913245
37 Z = -3326357
19
XDOT = -18335
869541 XDOT = -5588
773036
YDOT = -2648
029039 feet/sec YDOT = -807
119251 meter/sec
ZDOT = 15406
420817 ZDOT = 4695
877065
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 12270
50692272
00016717 00000-0 10270-3 0 9002
2 25544 51
6488 337
8066 0017838 102
4831 257
8317 15
50220026 33768
Satellite: ISS
Catalog Number: 25544
Epoch time: 12270
50692272 = yrday
fracday
Element set: 900
Inclination: 51
6488 deg
RA of node: 337
8066 deg
Eccentricity:
0017838
Arg of perigee: 102
4831 deg
Mean anomaly: 257
8317 deg
Mean motion: 15
50220026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 304
Coasting Arc #2 (Orbit 3391)
---------------------------------------
Vector Time (GMT): 2012/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3880223
38 A = 6796898
50 meter
Y = 4703762
88 meter E =
0030895
Z = 2968418
99 I = 51
49633
XDOT = -5651
239476 Wp = 101
77849
YDOT = -1500
563327 meter/sec RA = 332
30516 deg
ZDOT = -4971
633046 TA = 44
21303
MA = 43
96657
Ha = 233
578 n
mi
Hp = 214
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12730391
65 X = -3946953
35
Y = 15432292
93 feet Y = 4659999
06 meter
Z = 9738907
45 Z = 2949406
38
XDOT = -18540
811929 XDOT = -5609
888773
YDOT = -4923
108029 feet/sec YDOT = -1563
528421 meter/sec
ZDOT = -16311
132041 ZDOT = -4998
985886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11143246
20 X = 3396461
44
Y = -16660771
82 feet Y = -5078203
25 meter
Z = 9659793
04 Z = 2944304
92
XDOT = 17632
771228 XDOT = 5374
468670
YDOT = 2198
519403 feet/sec YDOT = 670
108714 meter/sec
ZDOT = -16424
051065 ZDOT = -5006
050764
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 12271
53834562
00016717 00000-0 10270-3 0 9017
2 25544 51
6491 332
6948 0017766 105
5524 254
7590 15
50273910 33924
Satellite: ISS
Catalog Number: 25544
Epoch time: 12271
53834562 = yrday
fracday
Element set: 901
Inclination: 51
6491 deg
RA of node: 332
6948 deg
Eccentricity:
0017766
Arg of perigee: 105
5524 deg
Mean anomaly: 254
7590 deg
Mean motion: 15
50273910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3392
Checksum: 315
Coasting Arc #3 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2012/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3836930
99 A = 6797609
04 meter
Y = -4960717
76 meter E =
0021090
Z = -2644596
58 I = 51
47165
XDOT = 5422
010603 Wp = 97
23889
YDOT = 1440
440718 meter/sec RA = 327
33988 deg
ZDOT = 5197
777492 TA = 232
98026
MA = 233
17341
Ha = 233
538 n
mi
Hp = 214
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12588356
28 X = 3904964
51
Y = -16275320
72 feet Y = -4917430
75 meter
Z = -8676497
97 Z = -2625790
96
XDOT = 17788
748697 XDOT = 5380
250580
YDOT = 4725
855374 feet/sec YDOT = 1500
840218 meter/sec
ZDOT = 17053
075762 ZDOT = 5224
015853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10606855
95 X = -3232969
69
Y = 17669171
24 feet Y = 5385563
40 meter
Z = -8598220
17 Z = -2620737
51
XDOT = -16833
513316 XDOT = -5130
854859
YDOT = -1807
551467 feet/sec YDOT = -550
941687 meter/sec
ZDOT = 17161
388561 ZDOT = 5230
791233
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 12272
50528192
00016717 00000-0 10270-3 0 9025
2 25544 51
6482 327
9036 0017849 109
1133 251
1952 15
50289324 34073
Satellite: ISS
Catalog Number: 25544
Epoch time: 12272
50528192 = yrday
fracday
Element set: 902
Inclination: 51
6482 deg
RA of node: 327
9036 deg
Eccentricity:
0017849
Arg of perigee: 109
1133 deg
Mean anomaly: 251
1952 deg
Mean motion: 15
50289324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 302
Coasting Arc #4 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2012/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3816413
55 A = 6798342
63 meter
Y = 5157277
95 meter E =
0031653
Z = 2201750
65 I = 51
44987
XDOT = -5188
878124 Wp = 110
50854
YDOT = -1488
460809 meter/sec RA = 322
37221 deg
ZDOT = -5454
891350 TA = 44
96908
MA = 44
71317
Ha = 233
400 n
mi
Hp = 214
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12521041
82 X = -3884495
35
Y = 16920203
24 feet Y = 5114220
06 meter
Z = 7223591
38 Z = 2183044
47
XDOT = -17023
878359 XDOT = -5145
349337
YDOT = -4883
401604 feet/sec YDOT = -1546
243432 meter/sec
ZDOT = -17896
625164 ZDOT = -5479
992961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10137845
23 X = 3090015
23
Y = -18477362
90 feet Y = -5631900
21 meter
Z = 7145711
50 Z = 2178012
87
XDOT = 16074
991798 XDOT = 4899
657500
YDOT = 1790
878030 feet/sec YDOT = 545
859624 meter/sec
ZDOT = -18000
228187 ZDOT = -5486
469551
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 12273
53665367
00016717 00000-0 10270-3 0 9036
2 25544 51
6485 322
7912 0017800 112
2642 248
0399 15
50349492 34230
Satellite: ISS
Catalog Number: 25544
Epoch time: 12273
53665367 = yrday
fracday
Element set: 903
Inclination: 51
6485 deg
RA of node: 322
7912 deg
Eccentricity:
0017800
Arg of perigee: 112
2642 deg
Mean anomaly: 248
0399 deg
Mean motion: 15
50349492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 310
Coasting Arc #5 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2012/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3721665
04 A = 6798923
36 meter
Y = -5397315
16 meter E =
0020797
Z = -1823546
01 I = 51
42798
XDOT = 4955
122615 Wp = 95
21746
YDOT = 1535
264813 meter/sec RA = 317
40374 deg
ZDOT = 5622
560277 TA = 244
73775
MA = 244
95342
Ha = 233
381 n
mi
Hp = 214
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12210187
14 X = 3790600
82
Y = -17707726
90 feet Y = -5355311
97 meter
Z = -5982762
49 Z = -1805297
96
XDOT = 16256
963960 XDOT = 4910
273216
YDOT = 5036
958047 feet/sec YDOT = 1590
426048 meter/sec
ZDOT = 18446
720069 ZDOT = 5646
523194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9382952
32 X = -2859923
87
Y = 19378238
61 feet Y = 5906487
13 meter
Z = -5906757
41 Z = -1800379
66
XDOT = -15312
683848 XDOT = -4667
306037
YDOT = -1815
884079 feet/sec YDOT = -553
481467 meter/sec
ZDOT = 18545
606314 ZDOT = 5652
700805
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 12274
50354205
00016717 00000-0 10270-3 0 9041
2 25544 51
6478 317
9994 0017876 115
7472 244
5526 15
50360911 34388
Satellite: ISS
Catalog Number: 25544
Epoch time: 12274
50354205 = yrday
fracday
Element set: 904
Inclination: 51
6478 deg
RA of node: 317
9994 deg
Eccentricity:
0017876
Arg of perigee: 115
7472 deg
Mean anomaly: 244
5526 deg
Mean motion: 15
50360911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 323
Coasting Arc #6 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2012/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3651695
03 A = 6799438
14 meter
Y = 5562158
20 meter E =
0031649
Z = 1325460
62 I = 51
40857
XDOT = -4724
029254 Wp = 119
38667
YDOT = -1697
082190 meter/sec RA = 312
43326 deg
ZDOT = -5803
821235 TA = 46
13864
MA = 45
87758
Ha = 233
242 n
mi
Hp = 214
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11980626
73 X = -3720059
72
Y = 18248550
53 feet Y = 5520940
58 meter
Z = 4348624
07 Z = 1307553
86
XDOT = -15498
783643 XDOT = -4676
506931
YDOT = -5567
854953 feet/sec YDOT = -1749
644213 meter/sec
ZDOT = -19041
408251 ZDOT = -5826
655073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8719989
40 X = 2657852
77
Y = -20028732
00 feet Y = -6104757
51 meter
Z = 4274017
36 Z = 1302720
49
XDOT = 14645
644182 XDOT = 4463
992347
YDOT = 2229
198261 feet/sec YDOT = 679
459630 meter/sec
ZDOT = -19135
606576 ZDOT = -5832
532884
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 12275
53486267
00016717 00000-0 10270-3 0 9050
2 25544 51
6479 312
8864 0017894 119
1314 241
1630 15
50415995 34542
Satellite: ISS
Catalog Number: 25544
Epoch time: 12275
53486267 = yrday
fracday
Element set: 905
Inclination: 51
6479 deg
RA of node: 312
8864 deg
Eccentricity:
0017894
Arg of perigee: 119
1314 deg
Mean anomaly: 241
1630 deg
Mean motion: 15
50415995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 326
Coasting Arc #7 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2012/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3508122
91 A = 6799736
55 meter
Y = -5759274
41 meter E =
0021552
Z = -899621
52 I = 51
39002
XDOT = 4515
024310 Wp = 94
62693
YDOT = 1848
204914 meter/sec RA = 307
46216 deg
ZDOT = 5895
468055 TA = 255
63047
MA = 255
86981
Ha = 233
193 n
mi
Hp = 214
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11509589
59 X = 3576633
81
Y = -18895257
24 feet Y = -5719661
42 meter
Z = -2951514
19 Z = -882411
91
XDOT = 14813
071882 XDOT = 4465
382373
YDOT = 6063
664416 feet/sec YDOT = 1898
417788 meter/sec
ZDOT = 19342
086794 ZDOT = 5917
281443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7781906
83 X = -2371925
20
Y = 20721044
24 feet Y = 6315774
28 meter
Z = -2879771
96 Z = -877754
49
XDOT = -14059
626973 XDOT = -4285
374302
YDOT = -2636
035200 feet/sec YDOT = -803
463529 meter/sec
ZDOT = 19432
049033 ZDOT = 5922
888545
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 12276
50170243
00016717 00000-0 10270-3 0 9063
2 25544 51
6478 308
0942 0017904 122
5298 237
7585 15
50439079 34691
Satellite: ISS
Catalog Number: 25544
Epoch time: 12276
50170243 = yrday
fracday
Element set: 906
Inclination: 51
6478 deg
RA of node: 308
0942 deg
Eccentricity:
0017904
Arg of perigee: 122
5298 deg
Mean anomaly: 237
7585 deg
Mean motion: 15
50439079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 328
Coasting Arc #8 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2012/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3395948
73 A = 6799924
59 meter
Y = 5864280
76 meter E =
0030621
Z = 357263
05 I = 51
37307
XDOT = -4316
910115 Wp = 127
94888
YDOT = -2115
410655 meter/sec RA = 302
48911 deg
ZDOT = -5978
976214 TA = 48
18702
MA = 47
92590
Ha = 233
067 n
mi
Hp = 214
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11141564
08 X = -3463007
48
Y = 19239766
29 feet Y = 5825930
23 meter
Z = 1172122
88 Z = 340601
99
XDOT = -14163
090928 XDOT = -4263
889266
YDOT = -6940
323671 feet/sec YDOT = -2163
389114 meter/sec
ZDOT = -19616
063695 ZDOT = -5999
818965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6983047
14 X = 2128432
77
Y = -21111564
77 feet Y = -6434804
94 meter
Z = 1102639
83 Z = 336084
62
XDOT = 13625
134569 XDOT = 4152
941017
YDOT = 3417
293866 feet/sec YDOT = 1041
591170 meter/sec
ZDOT = -19701
985226 ZDOT = -6005
165097
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 12277
53297159
00016717 00000-0 10270-3 0 9074
2 25544 51
6475 302
9806 0017970 126
1884 234
0932 15
50477886 34856
Satellite: ISS
Catalog Number: 25544
Epoch time: 12277
53297159 = yrday
fracday
Element set: 907
Inclination: 51
6475 deg
RA of node: 302
9806 deg
Eccentricity:
0017970
Arg of perigee: 126
1884 deg
Mean anomaly: 234
0932 deg
Mean motion: 15
50477886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 344
Coasting Arc #9 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2012/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3215942
64 A = 6799806
55 meter
Y = -5992179
45 meter E =
0022973
Z = 104845
61 I = 51
35786
XDOT = 4160
302338 Wp = 97
23913
YDOT = 2357
226553 meter/sec RA = 297
51577 deg
ZDOT = 5977
184639 TA = 263
89174
MA = 264
15355
Ha = 232
961 n
mi
Hp = 214
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10550992
91 X = 3282200
09
Y = -19659381
41 feet Y = -5955846
30 meter
Z = 343981
66 Z = 120630
17
XDOT = 13649
285886 XDOT = 4104
597816
YDOT = 7733
682917 feet/sec YDOT = 2403
438637 meter/sec
ZDOT = 19610
185824 ZDOT = 5997
260063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5941114
55 X = -1810851
71
Y = 21505074
54 feet Y = 6554746
72 meter
Z = 409852
70 Z = 124923
10
XDOT = -13336
093489 XDOT = -4064
841295
YDOT = -4119
158538 feet/sec YDOT = -1255
519522 meter/sec
ZDOT = 19692
911507 ZDOT = 6002
399427
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 12278
56421361
00016717 00000-0 10270-3 0 9083
2 25544 51
6476 297
8687 0017909 129
8284 230
4446 15
50526353 35015
Satellite: ISS
Catalog Number: 25544
Epoch time: 12278
56421361 = yrday
fracday
Element set: 908
Inclination: 51
6476 deg
RA of node: 297
8687 deg
Eccentricity:
0017909
Arg of perigee: 129
8284 deg
Mean anomaly: 230
4446 deg
Mean motion: 15
50526353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 332
Coasting Arc #10 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2012/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3079234
68 A = 6799568
84 meter
Y = 6011188
92 meter E =
0028461
Z = -674741
59 I = 51
34352
XDOT = -4022
547021 Wp = 135
43384
YDOT = -2708
222916 meter/sec RA = 292
54026 deg
ZDOT = -5942
477945 TA = 51
87968
MA = 51
62343
Ha = 232
841 n
mi
Hp = 214
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10102475
97 X = -3142946
39
Y = 19721748
42 feet Y = 5976398
72 meter
Z = -2213719
11 Z = -689855
75
XDOT = -13197
332746 XDOT = -3963
096468
YDOT = -8885
245787 feet/sec YDOT = -2752
873526 meter/sec
ZDOT = -19496
318716 ZDOT = -5961
875020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5108753
83 X = 1557148
17
Y = -21555154
08 feet Y = -6570010
96 meter
Z = -2276818
12 Z = -693974
16
XDOT = 13244
120533 XDOT = 4036
807938
YDOT = 5148
647272 feet/sec YDOT = 1569
307688 meter/sec
ZDOT = -19576
206722 ZDOT = -5966
827809
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 12279
53097898
00016717 00000-0 10270-3 0 9096
2 25544 51
6470 293
0744 0017964 133
3423 226
9228 15
50544348 35165
Satellite: ISS
Catalog Number: 25544
Epoch time: 12279
53097898 = yrday
fracday
Element set: 909
Inclination: 51
6470 deg
RA of node: 293
0744 deg
Eccentricity:
0017964
Arg of perigee: 133
3423 deg
Mean anomaly: 226
9228 deg
Mean motion: 15
50544348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 335
Coasting Arc #11 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2012/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2884977
42 A = 6798971
62 meter
Y = -6047188
14 meter E =
0024480
Z = 1156561
50 I = 51
33149
XDOT = 3939
950445 Wp = 103
53361
YDOT = 3015
990315 meter/sec RA = 287
56468 deg
ZDOT = 5831
221476 TA = 269
04999
MA = 269
33048
Ha = 232
682 n
mi
Hp = 214
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9465149
01 X = 2946765
52
Y = -19839856
11 feet Y = -6014580
98 meter
Z = 3794493
12 Z = 1170727
23
XDOT = 12926
346604 XDOT = 3877
605039
YDOT = 9894
981348 feet/sec YDOT = 3059
701054 meter/sec
ZDOT = 19131
304056 ZDOT = 5850
210219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4081494
99 X = -1244039
67
Y = 21589296
59 feet Y = 6580417
60 meter
Z = 3853671
71 Z = 1174599
14
XDOT = -13331
488870 XDOT = -4063
437807
YDOT = -6012
749418 feet/sec YDOT = -1832
686023 meter/sec
ZDOT = 19209
476907 ZDOT = 5855
048561
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 12280
56216721
00016717 00000-0 10270-3 0 9101
2 25544 51
6470 287
9624 0017875 137
1510 223
1037 15
50617589 35327
Satellite: ISS
Catalog Number: 25544
Epoch time: 12280
56216721 = yrday
fracday
Element set: 910
Inclination: 51
6470 deg
RA of node: 287
9624 deg
Eccentricity:
0017875
Arg of perigee: 137
1510 deg
Mean anomaly: 223
1037 deg
Mean motion: 15
50617589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 302
Coasting Arc #12 (Orbit 3546)
---------------------------------------
Vector Time (GMT): 2012/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2751059
46 A = 6798248
45 meter
Y = 5960452
19 meter E =
0025395
Z = -1731367
86 I = 51
32015
XDOT = -3881
047133 Wp = 140
63303
YDOT = -3416
935561 meter/sec RA = 282
58647 deg
ZDOT = -5661
405992 TA = 58
43404
MA = 58
18633
Ha = 232
557 n
mi
Hp = 214
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9025785
64 X = -2809095
32
Y = 19555289
34 feet Y = 5929363
53 meter
Z = -5680340
75 Z = -1744873
86
XDOT = -12733
094269 XDOT = -3815
047652
YDOT = -11210
418507 feet/sec YDOT = -3459
967165 meter/sec
ZDOT = -18574
166640 ZDOT = -5680
099639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3352686
37 X = 1021898
80
Y = -21260039
70 feet Y = -6480060
10 meter
Z = -5736778
28 Z = -1748570
02
XDOT = 13635
719510 XDOT = 4156
167307
YDOT = 7126
168780 feet/sec YDOT = 2172
056244 meter/sec
ZDOT = -18651
084731 ZDOT = -5684
850626
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 12281
52888295
00016717 00000-0 10270-3 0 9110
2 25544 51
6462 283
1677 0017883 140
4714 219
7745 15
50621402 35478
Satellite: ISS
Catalog Number: 25544
Epoch time: 12281
52888295 = yrday
fracday
Element set: 911
Inclination: 51
6462 deg
RA of node: 283
1677 deg
Eccentricity:
0017883
Arg of perigee: 140
4714 deg
Mean anomaly: 219
7745 deg
Mean motion: 15
50621402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3547
Checksum: 322
Coasting Arc #13 (Orbit 3562)
---------------------------------------
Vector Time (GMT): 2012/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2572890
52 A = 6797205
48 meter
Y = -5889624
74 meter E =
0025558
Z = 2210792
24 I = 51
31152
XDOT = 3883
398611 Wp = 113
08654
YDOT = 3756
419541 meter/sec RA = 277
60834 deg
ZDOT = 5427
632668 TA = 271
54125
MA = 271
83400
Ha = 232
365 n
mi
Hp = 214
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8441241
86 X = 2627818
68
Y = -19322915
83 feet Y = -5860545
81 meter
Z = 7253255
37 Z = 2223425
14
XDOT = 12740
809090 XDOT = 3814
738460
YDOT = 12324
211092 feet/sec YDOT = 3799
462582 meter/sec
ZDOT = 17807
193794 ZDOT = 5446
331195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2484292
34 X = -757212
30
Y = 20921017
71 feet Y = 6376726
20 meter
Z = 7306070
29 Z = 2226890
23
XDOT = -14117
199251 XDOT = -4302
922332
YDOT = -7990
294809 feet/sec YDOT = -2435
441858 meter/sec
ZDOT = 17884
105350 ZDOT = 5451
075311
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 12282
56001641
00016717 00000-0 10270-3 0 9128
2 25544 51
6459 278
0553 0017802 144
5797 215
6539 15
50707456 35635
Satellite: ISS
Catalog Number: 25544
Epoch time: 12282
56001641 = yrday
fracday
Element set: 912
Inclination: 51
6459 deg
RA of node: 278
0553 deg
Eccentricity:
0017802
Arg of perigee: 144
5797 deg
Mean anomaly: 215
6539 deg
Mean motion: 15
50707456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3563
Checksum: 317
Coasting Arc #14 (Orbit 3577)
---------------------------------------
Vector Time (GMT): 2012/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2475901
23 A = 6796025
41 meter
Y = 5688086
63 meter E =
0022127
Z = -2762158
91 I = 51
30394
XDOT = -3907
927594 Wp = 141
93287
YDOT = -4164
365705 meter/sec RA = 272
62699 deg
ZDOT = -5111
727051 TA = 69
47750
MA = 69
24017
Ha = 232
233 n
mi
Hp = 214
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8123035
54 X = -2525904
53
Y = 18661701
53 feet Y = 5660119
76 meter
Z = -9062201
13 Z = -2774308
71
XDOT = -12821
284756 XDOT = -3836
238526
YDOT = -13662
617143 feet/sec YDOT = -4207
666148 meter/sec
ZDOT = -16770
758041 ZDOT = -5130
537282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2011442
42 X = 613087
65
Y = -20230516
26 feet Y = -6166261
35 meter
Z = -9112991
35 Z = -2777639
76
XDOT = 14795
431505 XDOT = 4509
647523
YDOT = 9003
066975 feet/sec YDOT = 2744
134814 meter/sec
ZDOT = -16848
099523 ZDOT = -5135
300735
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 12283
52668091
00016717 00000-0 10270-3 0 9134
2 25544 51
6452 273
2601 0017771 147
5891 212
6355 15
50707313 35783
Satellite: ISS
Catalog Number: 25544
Epoch time: 12283
52668091 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 273
2601 deg
Eccentricity:
0017771
Arg of perigee: 147
5891 deg
Mean anomaly: 212
6355 deg
Mean motion: 15
50707313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3578
Checksum: 311
Coasting Arc #15 (Orbit 3593)
---------------------------------------
Vector Time (GMT): 2012/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2348799
35 A = 6794655
65 meter
Y = -5506985
04 meter E =
0025835
Z = 3211566
11 I = 51
29939
XDOT = 3991
391498 Wp = 125
15822
YDOT = 4495
307292 meter/sec RA = 267
64603 deg
ZDOT = 4747
300067 TA = 272
12160
MA = 272
41742
Ha = 232
023 n
mi
Hp = 215
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7706034
60 X = 2394603
84
Y = -18067536
22 feet Y = -5480462
89 meter
Z = 10536634
24 Z = 3223088
34
XDOT = 13095
116463 XDOT = 3917
765889
YDOT = 14748
383503 feet/sec YDOT = 4539
530302 meter/sec
ZDOT = 15575
131452 ZDOT = 4766
510960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1449982
80 X = -441954
76
Y = 19562693
19 feet Y = 5962708
89 meter
Z = 10584804
21 Z = 3226248
32
XDOT = -15613
286452 XDOT = -4758
929711
YDOT = -9701
154928 feet/sec YDOT = -2956
912022 meter/sec
ZDOT = 15654
106407 ZDOT = 4771
371633
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 12284
55775837
00016717 00000-0 10270-3 0 9146
2 25544 51
6448 268
1472 0017709 151
9806 208
2302 15
50794038 35944
Satellite: ISS
Catalog Number: 25544
Epoch time: 12284
55775837 = yrday
fracday
Element set: 914
Inclination: 51
6448 deg
RA of node: 268
1472 deg
Eccentricity:
0017709
Arg of perigee: 151
9806 deg
Mean anomaly: 208
2302 deg
Mean motion: 15
50794038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3594
Checksum: 334
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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